iiiiiiiiiiif -fl1g-hft-cti-vi (aefa) - dtic.mil · april 1989 aviation ... 61-07 ao-iaf cold...

-W-A-207 46if4 iFS ARMY AVIATION EiNGNEERING -FL1G-HfT-CTI-VI (AEFA) 112REPORT BIBLIOGRAPHY (U) ARMY AVIATION ENGINEERINGFLIGHT ACTIVITY EDWARDS AFB CA S LEWIS ET AL APR 89

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MICROCOPY FCESO.UTION TEST CHARTNATIONAL RUPF l iJ ' TANDARDS 1963 A

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rEFA Project No. 89-90,U

U.S. ARMYAVIATION ENGINEERING FLIGHT ACTIVITY

(AEFA)REPORT BIBLIOGRAPHY

1961 - 1988

AEF Compiled By: Sheila Lewis

AndA Maryanna Lake

April 1989

AVIATION ENGINEERING FLIGHT ACTIITYEdwards Air Force Base, California 93523-5000

PREFACE

"' The mission of the U.S. Army Aviation Engineering Flight Activity (AEFA) is toconduct airworthiness qualification flight tests of air vehicles developed and/or procuredas integrated systems and airworthiness evaluations of those vehicles proposed orconsidered for Army application or which incorporate advanced concepts having potentialmilitary application; produce test data on basic air vehicle performance, handlingqualities, system/subsystem interface, and integrated system performance; and conduct atest pilot orientation course to prepare Army aviators for attendance at U.S. Naval TestPilot School.

4 This bibliography is listed by both project number and aircraft type tested orinvolved in the test of equipment or procedures. The project listing is in chronologicalorder from 1961 through 1988: Missing numbers in the sequential project listing occurbecause of cancellations or restructuring of programs. The aircraft listing contains projectnumbers as well as all other information and allows the user an alternate method forobtaining necessary project information. Appendix A provides a quick reference list ofthe aircraft by contractorABibliography holders of record will automatically receive futurecopies of updated bibliographies.

The reports listed are defined as:

Formal Test Report. A report that is formally publishedfor widespread distribution to other DOD agencies andstaff, the Defense Technical Information Center (DTIC),appropriate contractors, and other agencies as directedby the U.S. Army Aviation Systems Command(AVSCOM). These reports are identified by only theproject number. "

Letter Report. A report that is prepared to provide ..

immediate information to the customer for milestone . -events or for portions of a test in progress. They are also i>12 9to report on very limited tests or tests where the datahave very restricted application or little historical value. [These reports are identifiable by the LR, LOE, or TWRwith the project number and are identified in the subjectline as letter report, report, letter of effort, test witnessreport, or memorandum for record.

Formal reports are on file with DTIC or the National Technical Information Service(NTIS). They may be obtained from DTIC by use of the AD Number and from NTISthrough their normal procedures. Letter Reports are controlled by AVSCOM and may beobtained by contacting:

U.S. Army Aviation Systems CommandATTN: AMSAV-84300 Goodfellow Blvd.St. Louis, MO 63120-1798

-- A

TABLE OF CONTENTS

PREFACE

REPORT NUMBERS

1961 (61-01 thru 61-10) ....................................... 11962 (62-01 thru 62-72) ....................................... 1

1963 (63-01 thru 63-93) ....................................... 21964 (64-01 thru 64-44) ....................................... 51965 (65-01 thru 65-47) ... .................................... 5

1966 (66-04 thru 66-29) ....................................... 71967 (67-02 thru 67-29 ........................................ 91968 (68-02 thru 68-55) ....................................... 101969 (69-01 thru 69-21) ....................................... 121970 (70-02 thru 70-43) ....................................... 141971 (71-01 thru 71-47) ......... ............................. 161972 (72-01 thru 72-44) ....................................... 181973 (73-01 thru 73-71) ....................................... 211974 (74-02 thru 74-94) ....................................... 231975 (75-01 thru 75-28) ....................................... 251976 (76-02 thru 76-13) ....................................... 271977 (77-02 thru 77-38) ....................................... 281978 (78-01 thru 78-23) ....................................... 311979 (79-01 thru 79-86) ....................................... 33

1980 (80-01 thru 80-21) ....................................... 351981 (81-01-1 thru 81-90-1A) .................................. 361982 (82-01 thru 82-86) . ....................................... 391983 (83-03 thru 83-30) ....................................... 401984 (84-02 thru 84-90) ................................... /. 431985 (85-02 thru 85-25) .. 461986 (86-01 thru 86-25) ....................................... 471987 (87-01 thru 87-34) ....................................... 491988 (88-07 thru 88-18) ....................................... 50

AIRCRAFT LISTING

Fixed WingBeech Aircraft Corp ................ ........................ 51Bell Helicopter Corp........... . . ......... 53Breguet Aviation ................ ... .............. 53Canadair, Ltd .................... ..t . . 53Cessna Aircraft Co ............... ..................... 53DeHavilland Aircraft of Canada ..... 54

Grumman Aerospace Corporation ........................... 54Lockheed Corporation .................................... 56North American Aviation .................................. 57Pilatus .................................................. 57Ryan Aeronauticai Co . .................................... 57ROTEC Engineering, Inc ................................... 58RUTAN Aircraft Factory .................................. 58Schweizer Aircraft Corp .................................... 58

Rotary WingBell Helicopter Textron .................................... 59Boeing-Vertol Co ......................................... 81Bolkow-Messerschmitt-Blohm .............................. 85H iller Aviation ........................................... 86McDonnell Douglas Aircraft Corp ............................ 86Kaman Aerospace Corp .................................... 90Lockheed Corporation .................................... 91Piasecki Aircraft Corp ..................................... 91Rotorway Inc . ........................................... 91Sikorsky Aircraft ......................................... 92

M iscellaneous Aircraft ............................................. 99

A ppendix A ..................................................... i02

1961

Project Aircraft AdNumber Type Report Title Date Author(s) Number

61-01 L-19A Evaluation of L-19A Equipped with Continental Feb 1961 J. Kidwcll 722 8250-470-1 ICI Fuel Injection Engine CPT W. Clay

61-02 Model Bell Model 47G-3 High Altitude Flight Feb 1961 J. Kidwell 722 82647G-3 Evaluation

61-03 UH-12E High Altitude Evaluation of the Hiller Mar 1961 J. Kidwell 722 827Model 1961 UH-12E Helicopter MAJ J. Seigler

D. Armstrong

61-04 Limited Cold Weather Evaluation of Multi- Jun 1961 A. Ruddell 884 882Purpose Ground Service Unit Model 2100-5

61-05 Evaluation of the Republic Electronic Industries Jul 1961 CWO D. Scott 884 883Pitot and Static System Tester

61-06 L-19A Evaluation of the Mark XII Auxiliary Fuel and Jul 1961 CPT J. Johnston 884 884H-13G Oil System

61-07 AO-IAF Cold Weather Suitability Test of the AO-IAF Nov 1961 A. Ruddell 884 888

61-08 Evaluation of the Aerosonic Corporation Nov 1961 CWO D. Scott 884 889Pitot and Static System Tester

61-09 Evaluation of the North American Aviation 1961 W. Swope 884 885Inc. Dynamic Flight Simulator

61-10 Evaluation of the North American Aviation 1961 W. Swope 884 890Inc. Visual Presentation Flight Simulator

1962

62-01 XV-3 Pilot Evaluation of the Bell Model Feb 1962 MAJ E. Kleuver 884 870XV-3 Vertical Take-Off and Landing Aircraft

62-02 H-37 Drop Test Evaluation of Mark XII Auxiliary Feb 1962 2LT J. Mellon 884 871Torso Fuel Tank MAJ E. Kleuve-

62-03 H-23D Qualitative Flight Evaluation of the Torque-Bias, Apr 1962 W. Swope 884 872Throttle-Governor and Yaw-Damper Systems for CPT J. Johnstonthe Hiller H-23D Helicopter CWO E. Nelson

62-04 H-37B Evaluation of the SWE-1165 Blade Tracker May 1962 R. Finnestead 884 873H-23DH-21B

1962(continued)


62-05 Model Limited Evaluation of the Bell Model 47J-2 May 1962 E. Smith 88489147J-2 J. Kidwell

62-06 Evaluation of the Helicopter Load and Hovering May 1962 W. Golyer 884 875Computer A. Higgins

62-07 UH-12E-4 Evaluation of the Hiller Model UH-12E 1962 J. Kidwell 884 876Helicopter CPT J. Johnston

62-08 TB-25N Flight Test Evaluation of a TB-25N Aerial Sep 1962 K. Jordon 884 877Tanker MAJ E. Kluever

62-09 H-34 H-34 Helicopter 50-Caliber Machine-Gun Kit Oct 1962 J. Kidwell 951 582Calibration CWO E. Nelson

62-11 TBM-3 Evaluation of a Grumman TBM-3 Air Tanker Nov 1962 J. Blaha 884 894CWO E. Nelson

62-12 Model Limited High-Altitude Evaluation of the J. Kidwell 884 89647G-3B Bell 47G-3B Helicopter CWO E. Nelson

A. Averill

62-13 OH-13H Final Report Engineering Test of the Stability Apr 1964 L. Schroers 951 587aka and Control Characteristics of the OH-13H CWO E. Nelson62-30 Equipped with the XM-l Armament Kit

62-28 CH-37B Final Report Engineering Test of the CH-37B Mar 1965 R. Turk 884 897CWO J. Watts

62-30 SEE USAAEFA PROJECT NO. 62-13

62-35 XV-SA Letter Report,Preliminary Pilot Qualitative Oct 1965 R. FnnesteadLR Evaluation of the XV-SA Research Aircraft K. Ferrell

62-72/ XV-SA Engineering Flight Research Evaluation of the Aug 1966 R. Finnestead 800 973Pt I XV-SA Lift-Fan Aircraft, Pt 1, Stability and K. Ferrell

Control MAJ W. WelterW. Anderson

62-72/ XV-5A Engineering Flight Research Evaluation of the Aug 1967 K. Ferrell 821 123Pt 2 XV-SA Lift-Fan Aircraft, Pt II, Performance MAJ W. Welter

1963

63-01 OH-13H OH-13H Gross Weight Increase/XM-! Jun 1963 R. Finnestead 951 596Armament Kit Performance Test CWO E. Nelson

2

1963(continued)


63-04 CV-2B Take-Off and Landing Capabilities of the Sep 1963 J. Kidwell 440 406aka Caribou CV-2B Aircraft onUnprepared Surfaces, J. Blaha

63-73 USATECOM Project No. 4-4-1142-01 R. FinnesteadCPT M. Antoniou

63-05 PC-6/A Report of USATECOM Project No. 4-3-1048-01 Sep 1963 L. Schroers 951 586aka Takeoff and Landing Evaluation of the CPT J. Johnston

63-70 Pilatus Turbo Porter Model PC-6/A Airplane CWO J. Watts

63-06 Model Flying Qualities and Performance Evaluation Jan 1964 CPT M. Antoniou 951 590aka 941 of the Breguet 941 Turbo-Prop Troop Transport

63-85

63-07 UH-13R Report of USATECOM Project No. 4-4-0240-02, Jan 1964 L. Schroers 951 588aka Flight Evaluation of the T63-A-5 Turbo Shaft CPT M. Antoniou

63-16 Engine Installed in a UH-13R Helicopteraka

64-01

153-12 H-23D Helicopter Airspeed System Investigation Dec 1962 2LT J. MeltonCPT J. Johnston

63-13 YCV-7A Engineering Test Requirements for the Nov 1963 J. Blaha 951 587DeHavilland YCV-7A Tactical Troop Transport,USATECOM Project No. 4-3-1170-01

63-14 CV-7A Letter Report on Preliminary Engineering Flight Oct 1964 J. Blaha LREvaluation of the CV-7A Tactical TransportAirplane, DA Project No. I-R-1-41815-D-193,USATECOM Project No. 4-3-1170-04


63-20 OV-1C Final Report of the Airworthiness Certification Jan 1965 J. Blaha 465 079Test of the QRC-160-1 Installed on the OV-IC MAJ J. JohnstonAirplane, USATECOM Project No. 6-3-6711-03

63-23/ OH-4A Report of the Engineering Flight Test Stability Aug 1964 R. Finnestead 909 271Pt 1 and Control Phase of the OH-4A Helicopter, MAJ J. Foster

Unarmed (Clean) and Armed with the XM-7 orXM-8 Weapon Subsystem, USATECOM ProjectNo. 4-3-0250-11/12/13

63-231 OH-4A Report of the Engineering Flight Test Perform- Aug 1964 J. Melton 909 272Pt 2 ance Phase of the OH-4A Unarmed (Clean) CWO J. Watts

and Armed with the XM-7 or XM-8 WeaponSubsystem, USATECOM Project No. 4-3-0250-12/13

63-24/ OH-SA Report of the Engineering Flight Test of the Aug 1964 R. Turk 909 269Pt 1 OH-SA Helicopter, Unarmed (Clean) and MAJ J. Johnston

Armed with the XM-7 or XM-8 Weapon J. BlahaSubsystem, Part I Stability and Control, J. ReichertUSATECOM Project No. 4-3-0250-31/32/33

3

1963(continued)


63-24/ OH-5A Report of Engineering Flight Test of the OH-SA, Aug 1964 L. Schroers 909 -70Pt 2 Helicopter Unarmed (Clean) and Armed with CWO E. Nelsonthe XM-7 or XM-8 Weapons Subsystem, Part IIPerformance PhaseUSATECOM ProjectNo. 4-3-0250-31/32/33

63-25/Pt I OH-6A Report of the Engineering Flight Test Stability Aug 1964 C. Statur 951 591and Control Phase of the OH-6A Helicopter, W. AndersonUnarmed (Clean) and Armed with the XM-7or XM-8 Weapon Subsystem, USATECOMProject No. 4-3-0250-51/52/53

63-25/ OH-6A Report of the Engineering Flight Test Perform- Aug 1964 J. Kudirka 951 592Pt 2 ance Phase of the OH-6A Helicopter Unarmed CPT D. Wray(Clean) and Armed with the XM-7 or XM-8Weapon Subsystem, USATECOM ProjectNo. 4-3-0250-51/52/53

63-38 T-34B Evaluation of the U.S. Forest Service T-34B Sep 1963 J. Kidwell 951 583T-34B Airplane with Smoke Generator Installed



63-74 CV-2B Final Report Performance Tests of the CV-2B Jun 1965 R. Finnestead 467 490Airplane USATECOM Project No. 4-4-114-01 CPT M. Antoniou

63-77 UH-ID Letter Report on the High-Altitude Evaluation Jun 1965 L. SchroersLR of the U.S. Army UH-ID Helicopter Equipped

with the 48-Foot Rotor Blade, USATECOMProject No. 4-4-0205-01

63-81 UH-IB Engineering Flight Test of UH-IB Helicopter Jun 1966 0. Yamakawa 488 791aka Equipped with XM-16 Armament Subsystem MAJ J. Foster65-01 and XM-21 Armament Subsystem, USATECOM

Project No. 4-4-1532-03 and 4-5-1535-04

63-85 SEE USAAEFA PROJECT NO. 63-06aka63-06

63-92 CV-2B Final Test Report of the Integrated Engineering/ Jul 1964 J. KramerLR Service Test of Low Level Extraction Techniques

(LOLEX) from CV-2B Aircraft, USATECOMProject No. 4-4-7475

63-93 UH-IB Military Potential Test of the Model 540, Feb 1964 J. Kidwell 951 593"Door Hinge" Rotor System, USATECOM CPT D. WrayProject No. 4-40108-01

4

1964


64-01 SEE USAAEFA PROJECT NO. 63-07 aka 63-16

64-0 UH-IB Engineering Test of UH-1B Helicopter Aug 1966 J. Blaha 805 698Equipped with Flotation Landing Gear, LT R. RichUSATECOM Project No. 4-5-5301-01

64-05 CH-37B Final Report, USATECOM Project , Apr 1964 R. Turk 951 589No. 4-4-0180-01 Engineering Flight Tests of CWO J. Wattsthe CH-37B

64-20 UH-ID Final Report of Engineering Test of the Mar 1965 J. KudirkaYT53-L-13 Engine Installed in the UH-ID D. WilsonHelicopter, USATECOM Project No. 4-3-0150-10

64-20 UH-ID Engineering Test of the UH-1D Helicopter with Apr 1966 J. Melton 845 032XT67 Power Plant Installed, USATECOM W. AndersonProject No. 4-3-0150-17

64-28 UH-IB Engineering Evaluation of the UH-IB Helicopter Jun 1966 L. Schroers 804 242Equipped with the Model 540 Rotor System, CPT M. AntoniouPhase B,USATECOM Project No. 4-4-0108-03

64-28 UH-IB Engineering Flight Test of the UH-IB Dec 1966 L. Schroers 811 782Helicopter Equipped with the Model 540 Rotor J. MeltonSystw", Phasc D, USATECOM Project J. WattsNo. 4-4-0105-03 J. Shapley

MAJ A. DarlingMAJ D. DuganMAJ E. SampsonW. Anderson

64-31 OH-6A Final Report of Climatic Hangar Test of the Jul 1965 S. Kennedy 813 862OH-6A Light Observation Helicopter, C. Martin

USATECOM Project No. 4-3-0250-72/80 K. Dorris

64-44 YOH-6A Continued Flight Test of the YOH-6A Hell- May 1967 F. Dominick A951 581copter, USATECOM Project No. 4-3-0250-78 J. Watts

1965


65-07 U-6 Final Report of Qualitative Flying Qualities Jun 1965 MAJ E. KleuverLR Evaluation of the Turbine Powered U-6 Airplane,

USATECOM Project No. 4-5-1020-02

5

1965(continued)


65-10 CV- 7A Stability and Control and Performance Test Mar 1966 MAJ N. Mattmuller 483 183

(Phase D) of the CV-7A Transport Airplane, D. WilsonUSATECOM Project No. 4-3-1170-08 J. Blaha

65-11 YOH-6A Letter Report of Engineering Test of YOH-6A Jun 1966 D. MacphersonLR Helicopter in the Desert Environment,


65-12 UH-lB Engineering Flight Test of UH-IB/540 Rotor Dec 1966 J. Nagata 811 7N1

Helicopter Equipped with XM-16/M-5, XM-21/ MAJ G. Hall

M-5 or XM-3/M- SArmament Subsystem. MAJ R. ChubboyUSATECOM Project No. 4-5-1591-01 MAJ D. Wray

65-12 UH-1C Engineering Flight Test of the U4-IC Feb 1967 J. Petrie 815 629aka Helicopter Equipped with the M-5 Grenade MAJ G. Hall66-09 Launcher and the XM-158 or XM-159 Airborne

Rocket Launcher Pods Suspended from the

XM-1 56 Multiarmament Mount, USATECOMProject No. 4-4-1542-06 and -09

65-22 UH-1B Engineering Flight Test of UH-IB Helicopter Nov 1966 M. Reif 809 915

Equipped with XM-47 Antipersonnel Mine MAJ N. Mattmuller

Di.pensing Subsystem, USATECOM J. ShapleyProject No. 4-4-6516-05

65-27 S-61 Engineering Evaluation of S-61 Mar 1966(No final published copy)

65-30 Model Engineering Flight Evaluation of the Bell May 1966 J. Kidweil 811 482209 Model 209 Armed Helicopter, USATECOM MAJ J. Foster

Project No. 4-6-0300-01

65-31 UH-2B Engineering Flight Evaluition of UH-2B Mar 1966 J. Johnson 831 862Armed Helicopter, USATECOM Project W. Anderson

No. 4-6-0300-01

65-37 OH-6A Letter Report, OH-6A XM-27 Army Mar 1969 J. Shapley

ake LR Preliminary Evaluation J. Nagata65-41B

65-37 OH-6A Engineering Flight Test (Product Improvement Mar 1968 J. Nagata 834 574

aka Test) of Production OH-6A Helicopter H. Wolf

65-41 Unarmed and Armed with the XM-27E1 J. ShapleyWeapon System, Phase D

65-37 OH-6A Engineering Flight Test of the OH-6A Apr 1969 J. Nagata 855 043

Helicopter (Cayuse), Phase D J. Shapley

65-41A SEE USAAEFA PROJECT NO. 65-37/PT I

65-41B SEE USAAEFA PROJECT NO. 65-37 (LETTER REPORT) AND 65-37/PT 1

65-46 A Note on Rotary Wing Hovering and Takeoff 1965 J. Kidwell

Performance, Data Acquisition and Analysis

6

1965(continued)

Project Aircraft AdNumber Type Report Title Date Author(s) NUMbCr

65-47 XV-5A A Review of AGARD Recommendations for 1965 W. AndersonV/STOL Handling Qualities (Rep. 408) in theLight of U.S. Army Experience with the XV-SAand other V/STOL Aircraft Including Helicopters

1966

66-04 UH-IH Engineering Flight Test of the UH-IH Aug 1967 F. DominickHelicopter, Phase D Product Improvement Test, L. ThomasInterim Report USATECOM Project CWO E. NelsonNo. 4-5-0150-04

66-04 YUH-IH Engineering Flight Test of the YUH-IH Nov 1970 F. Dominick 879 656Phase D. Limited LTC E. Nelson

66-05 UH-IC Engineering Test (Airworthiness and Performance Jan 1967 G. Yamakawa 808 293Tests) of UH-IC Helicopter with Cluster, MAJ W. WelterCanister, Riot Control CS, 130 IB, E-159,USAETCOM Project No. 5-5-3405-10

66-06 AH-IG Letter Report of Pilot Qualitative Evaluation of Sep 1966 MAJ G. HallLR Handling Qualities and Cockpit Environment of J. Melton

AH-IG Helicopter After Contractor Optimiza-tion of Stability Augmentation System andImprovement of Cockpit Ventilation System,USATECOMProject No. 4-6-0500-01

66-06 AFI-IG Engineering Flight Test of the AH-IG Jan 1968 J. Melton 830 136Helicopter Hucycobra, Phase B Part 1, MAJ G. HallUSATECOM Project No. 4-6-0500-01

66-06 AH-IG Engineering Flight Test of the AH-IG May 1969 J. Melton 855 629Helicopter Hueycobra, Phase B, Part 2, MAJ G. HallUSATECOM Project No. 4-6-0500-01

66-06 AH-1G Engineering Flight Test of the AH-IG Mar 1968 J. Melton 834 379aka (Hueycobra) Helicopter Equipped with the MAJ G. Hall

67-26 XM-28 Chin Turret with Twin XM-134 Miniguns,Phase B, Part 3

66-06 AH-1G Engineering Flight Test of AH-IG Mar 1968 J. Melton 836 901aka Hueycobra Helicopter Equipped with XM-28 MAJ G. Hall

67-27 Chin Turret with Twin XM-129, 40MM GrenadeLauncher, Phase B, Part 4

7

1966(continued)


66-06 AH-IG Engineering Flight Test of the AH-IG Helicopter Apr 1968 SP5 P. Passinisi 838 004aka Equipped with the XM-28 Chin Turret with One CW4 W. Connor68-03 7.62MM Automatic Gun (M-134) and One 40MM

Grenade Launcher (XM-129) Hybrid, Phase B,Part 5, USATECOM Project No. 4-6-0500-01

66-06 AH-IG Engineering Flight Test AH-IG Heli- Nov 1969 R. Finnestead 862 700copter Hueycobra Phase B, Pat 6. USATECOM CW4 W. ConnorNo. 4-6-0500-01

66-06 AH-IG Engineering Flight Test AH-IG Helicopter Dec 1970 R. Finnestead 880 558(Hucycobra) Phase D, Part 1, Handling R. PelikanQualities, USATECOM Project No. 4-6-0500-01 MAJ D. Wray

M. Buss

66-06 AH-IG Engineering Flight Test AH-IG Helicopter Apr 1970 R. Finnestead 874 210(Hueycobra) Phase D, Part 2 Performance, E. LaingUSATECOM Project No. 4-6-0500-01 CW4 W. Connor

M. Buss

66-06 AH-IG Engineering Flight Test AH-IG Helicopter Mar 1971 R. Finnestead 882 220(Huey,;obra) Phase D Part 2 Performance M. BussAddendum, USATECOM Project CW4 W. ConnorNo. 4-6-0500-01 7

66-06 AH-IG Engineering Flight Test AH-IG Helicopter, Sep 1970 R. Finnestead 878 122Phase D, Part 3 Vibration Characteristics, E. BailesUSATECOM Project No. 4-6-0500-01 MAJ D. Wray

M. Buss

66-06 AH-IG Engineering Flight Test of the AH-1G Helicopter Feb 1968 J. Melton 832 419to Determine the Area of Inadequate Directional MAJ G. HallControl Power at 8100 Lb. Gross Weight

66-06 AH-IG Feasibility Test of Tractor Tall Rotor Mar 1968 MAJ G. Hall 832 820Modification on the AH-IG Helicopter 1. Melton


66-14 U-21A Engineering Flight Test U-21A Airplane Oct 1969 MAJ A. Darling 951 584Phase B and Limited Phase D MAJ W. Welter

66-17 CH-47A Letter Report of USA Preliminary Engineering Sep 1966 K. FerrellLR Evaluation (Product Improvement Test (PIT) MAJ N. Mattmuller

Limited, Phase B), of the Proposed CH-47A, J. Shapley36,000-pound Flight Envelope, USATECOMProject No. 4-3-0200-32

66-23 CH-47B Engineering Flight Test of the CH-47B Mar1968 G. Yamakawa 834 597(Chinook) Helicopter, Phase D, Interim Report, LTC L. MillerUSATECOM Project No. 4-6-0200-03 MAJ H. Chambers

66-23 CH-47B Airworthiness and Qualification Test, (Phase D), Mar 1970 G.Yamakawa 871 209CH-47B Helicopter, USATECOM Project LTC L. MillerNo. 4-6-0200-03

8

1966(continued)


66-26 YCH-47B Engineering Flight Test of the YCH-47B, Army Jun 1967 MAJ N. MattmullerLR Preliminary Evaluation I & 11, USATECOM G. Yamakawa

Project No. 4-6-0200-02 MAJ D. DuganMAJ H. Chambers

66-26 YCH-47B Engineering Flight Test of the YCH-47B Jan 1969 G. Yamakawa 848 849Helicopter Army Preliminary Evaluation 1, ii, & MAJ N. MattmullerII, USATECOM Project No. 4-6-0200-02 MAJ D. Dugan

MAJ H. Chambers

66-28 YCH-47C Engineering Flight Test of the YCH-47C Mar 1968 MAJ R. ForsythMedium Transport Helicopter Army MAJ H. ChambersPreliminary Evaluation I, Interim Report ILT J. Jester

SP4 F. Wilson

66-28 YCH-47C Engineering Flight Test of the YCH-47C, Mar1968 CPT J. Jester 844 427Medium Transport Helicopter Army SP4 F. WilsonPreliminary Evaluation i, USATECOM LTC H. ChambersProject No. 1-5-0201-02 MAJ R. Forsyth

66-28 YCH-47C Engineering Flight Test of the YCH-47C, Feb 1969 CPT J. Jester 855 630Medium Transport Helicopter, Army ILT T. LanePreliminary Evaluation Part II, USATECOM LTC H. ChambersProject No. 4-6-0201-02 MAJ R. Forsyth

66-28 YCH-47C Army Preliminary Evaluation III and IV Oct 1970 CPT J. Jester 878 571YCH-47C, Medium Transport Helicopter, LTC R. ForsythUSATECOM Project No. 4-6-0201-02

66-29 CH-47C Airworthiness and Flight Characteristics Test Sep 1971 LTC R. Forsyth 892 400CH-47C (Chinook) Helicopter, Performance, J. NagataUSATECOM Project No. 4-6-0201-03 LTC G. Marr

MAJ J. Burden

66-29 CH-47C Airworthiness and Flight Characteristics CH-47C Mar 1972 J. Nagata 903 488Helicopter (Chinook), Stability and Control, G. SkinnerUSATECOM Project No. 4-6-0201-03 SP4 P. Bohn

MAJ A. ToddMAJ D. Broadhurst

LTC D. Hendrickson

1967

67-02 UH-1C Letter, Report Engineering Flight Test of the Aug 1967 J. PetrieLR UH-IC/XM-26 (TOW/H) Armament System, MAJ R. Holasek

Army Preliminary Evaluation MAJ R. Forsyth

9

1967(continued)

Project Aircraft AdNumber Type Report Title Date Author(u) Number

67-04 CH-47 Engineering Flight Test of the CH-47 (Chinook) Mar 1968 A. Higgins 832 821Helicopter Integral Weight and Balance ILT S. SchwartzSystems (ENSURE) H. Catey

67-06 Model Letter Report Bell 206A SAS Evaluation Apr 1967 MAJ R. ChubboyLR 206A

67-07 UH-1C Analytical Study of Range Performance of the May 1968 R. Finnestead 839 031LR UH-IC Helicopter Equipped withLycoming

T53-L-13 Engine

67-08 UH-1H Sling-Load Performance Capability of the Dec 1970 F. Dominick 878 570UH-IH Helicopter, Analytical Study

67-09 UH-IC Engineering Flight Test of the UH-IC Helicopter Nov 1967 K. Ferrell 827 184Equipped with the XM-30 Weapon System, MAJ D. DuganArmy Preliminary MAJ R. Holasek Evaluation

67-13 Model Light Observation Helicopter (LOH) Model 206A, Dec 1967 LTC E. Preisendorfer 951 595206A Armed (XM-27EI) and Unarmed, Performance LTC W. Crouch

and Stability and Control F. Dominick

67-22 TlI-55A Engineering Flight Test TH-55A Primary Nov 1969 CPT S. Schwartz 864 071Helicopter Trainer Limited Performance MAJ D.WrayEvaluation

67-23 OV-IB Engineering Flight Test of an IR Suppression Kit Jul1969 SPS G. Higley 857 774Installation on the OV-IB Aircraft MAJ R. Forsyth

67-25 RU-21B Engineering Flight Test, RU-21B and RU-21C Mar 1970 CPT J. Brecker 869 281RU-21C Aircraft Army Preliminary Evaluation LTC G. Swecker

MAJ R. Holt

67-26 SEE USAAEFA PROJECT NO. 66-06/PHASE B/PT 3

67-29 OH-6A Engineering Flight Test of the Production OH-6A Jul 1969 ILT T. Lane 859 435Helicopter with Fairings Removed MAJ D. Wray

M. Buss

1968

68-02 CH-47B CH-47B Height Velocity Evaluation Feb 1970 CPT A. Hoffman 866 347MAJ W. DavisJ. Shapley

68-03 SEE USAAEFA PROJECT NO. 66-06, PHASE B PT 5

10

1968(continued)

Project Aircraft Ad

Number Type Report Title Date Author(s) Number

68-04 UH-lB Special Study of Autorotational Procedures Apr 1968 J. Shapley 676 820K. Ferrell

68-09 AH-IG Letter Report Engineering Flight Test of Mar 1968 MAJ G. Hall 830 120

LR the AH-IG Helicopter Equipped with XM-20 S. DorrisArmament Subsystem Automatic 20MM Cannon

68-12 UH-1C Wind Tunnel and Flight Evaluation Rosemount Apr 1969 K. Ferrell 708 859Shielded Pitot-Static Tube Model 850N J. Shapley

1. Mishlof

68-13 UH-IC Flight Evaluation, AN/APN 191 Radar Sep 1970 G. Bender 714 638Altimeter MAJ J. Burden

68-14 A Mathematical Model for Estimating Jan 1968 R. KykerHelicopter Power Components

68-21 TH-13T Letter Report Final Flight Test Results for Jun 1969 CPT J. BreckerLR TH-13T Helicopter

68-22 UH-IC Rotary Wing Vehicle External Stores Jettison Aug 1970 CPT A. Hoffman 713 872

CH-47C Envelope Pilot Established Requirements MAJ W. Davis

68-24 CH-47A Qualitative Flight Evaluation of the Flight Nov 1968 ILT T. Lane 844 426

LR Engagement Tactical Cargo Hook (FETCH) MAJ R. Forsyth

on a CH-47A Helicopter LTC T. Wright

68-25 UH-IC A Flight Research Investigation of Autorotational Mar 1976 K. Ferrell A071 153

Performance and Height-Velocity Testing of A. Fredericksona Single Main Rotor Single Engine Helicopter R. Kyker

J. Shapley

68-30 OH-58A Airworthiness and Flight Characteristics Test Sep 1970 G. Yamakawa 878 560Production OH-58A Helicopter Unarmed and J. WattsArmed with XM27EI Weapon System,

Performance

68-30 OH-58A Airworthiness and Flight Characteristics Test Oct 1970 E. Laing 875 793Production OH-58A Helicopter Unarmed and LTC W. Graham

Armed with XM27EIArmament Subsystem, MAJ P. Stringer

Stability and Control

68-31 AH-IG Engineering Flight Test AH-IG (Hueycobra) Nov 1969 N. Donaldson 865 018Helicopter Equipped with the XM35 Armament MAJ. 0. HallSubsystem (20MM Automatic Gun)

68-32 YCH-47C Letter Report of the YCH-47C Helicopter Jan 1969 MAJ G. Marr

LR 50,000-Pound Gross Weight Evaluation

68-37 All-lU Army Preliminary Evaluation of the AII-IG Jun 1969 J. Nagata 860 948

Tractor Tail Rotor Modification M. Buss

68-41 OH-58A Army Preliminary Evaluation PrototypeOH-58A Jan 1970 J. Nagata 865 456Helicopter with XM27E1 Weapon Subsystem E. Bailes

J. Watts

11

1968(continued)


68-42 OH-6A Performance Evaluation of the OH-6A with Jan 1969 1LT T. Lane 847 558LR Expanded Tolerance Main Rotor Blades J. Shapley

MAJ I. Rundgren

68-43 OV-1D Army Preliminary Evaluation Preproduction Mar 1970 G. Yamakawa 870 260OV-1D (Mohawk) LTC W. Graham

LTC T. Wright

68-46 Model Army Preliminary Evaluation of the Mar 1969 J. Nagata 849 063211 Prototype BHC Model 211 Hueylug LTC T. Wright

MAJ I. Rundgren

68-47 YO-3A Army Preliminary Evaluation I YO-3A Aug 1970 CPT G. Condon 876 022Airplane LTC I. Rundgren

MAJ W. Davis

68-49 Letter Report Evaluation, High-Speed Apr 1971 E. BailesLR Swivel-Head Pitot Probe

68-51 RU-8D Letter Report Airworthiness Qualification Jul 1969 CW4 W. Connor 857 693LR Test RU-8D Airplane (Winebottle Configuration)

68-51 RU-8D Airworthiness and Flight Qualification Tests Oct 1970 LTC J. Wing 876 954RU-SD Airplane Winebottle Configuration, S. DorrlsPhase 11 LTC D. Boyle

CW4 W. Connor

68-53 OH-58A Climatic Laboratory Test OH-58A Helicopter Jul 1970 SP4 D. Tyson 875 578Equipped with XM27E1 Machine Gun SP4 J. PincavageArmament System N. Donaldson

CW3 J. Thomson

68-55 AH-IG Flight Evaluation, Compliance Test Techniques Apr 1974 K. Ferrell 109 440for Army Hot Day Hover Criteria A. Frederickson

J. KishiJ. Watts

1969

69-01 AH-1G Airworthiness and Flight Characteristics AH-IG Dec 1969 G. Bender 864 070Helicopter with Stabilized Nigh ISight (SNS), M. BussPhase I

69-01 AH-IG Airworthiness and Flight Characteristics Test Aug 1970 G. Bender 874 211AH-IG Helicopter with Stabilized Night Sight M. Buss(SNS), Phase I

12

1969(continued)


69-01 AH-1G NASA Report Static Load Tests of a Jul 1969 R. RosecransSimulation Package on an AH-IG Helicopter

69-07 UH-IC Jettison Test XM19/MK45 Flare Dispenser Dec 1969 MAJ D. Wray 864 077Installed in the UH-IC Helicopter

69-08 UH-1H Letter Report Flight Evaluation on the Big Nov 1969 MAJ G. HallLR Ear Cannister Deployment Subsystem

69-09 OH-6A 5.56/7.62MM Weapons Comparative Evaluation Jun 1971 LTC J. Wing 884 980OH-6A Helicopter V. Diekmann

MAJ R. Holasek

69-11 AH-IG Engineering Flight Test AH-IG Helicopter Mar 1971 R. Lewis 882 771(Hueycobra) Maneuvering Limitations E. Bailes

R. McClellanCPT J. ClaxtonM. BussCW4 W. ConnorLTC J. Johnston

69-13 AH-IG Height-VelocityTest AH-IG Helicopter Feb 1971 CPT G. Condon 881 633E. BailesCW4 W. Connor

69-14 YO-3A Army Preliminary Evaluation, II. YO-3A Aug 1970 CPT G. Condon 874 733Airplane LTC I. Rundgren

CW4 W. Connor

69-15 UH-IH Letter Report Airworthiness Qualification Oct 1969LR of the UH-IH Helicopter with the Airborne

Searchlight System (AN/ASS-2) Installed

69-16 OI-58A Height Velocity Test OH-58A Helicopter Jun 1971 J. Watts 884 973CPT G. CondonSP5 J. Pincavage

69-17 CH-47C Height-Velocity Evaluation CH-47C Sep 1972 J. Nagata 904 930Helicopter with T55-L-1 IA Engines A. Steinmetz

MAJ A. ToddMAJ J. Burden

69-18 RU-21A CEFIRM Leader Airworthiness Qualification Dec 1970 LTC J. WingLR RU-21B Test RU-21-ABC Aircraft

RU-21C

69-21 UH-IM Letter Report Airworthiness Evaluation of Feb 1970 CW4 W. ConnorLR the UH-IM with Infant Subsystem Installed

13

1970


70-02 AH-56A Army Preliminary Evaluation I and Mar 1972 F. Dominick 905 910aka Research and Development Acceptance Test I, G. Bender71-17 AH-56A Cheyenne Compound Helicopter LTC G. Hall

R. McClellanMAJ P. StringerM. Buss

70-03 OV-ID Army Preliminary Evaluation Ii Production Mar 1971 G. Yamakawa 881 649OV-11D (Mohawk), Performance and Handling ILT K. BrauerQualities LTC W. Graham

70-03-2 OV-ID Army Preliminary Evaluation, Production Apr 1972 G. Yamakawa 903 107OV-ID (Mohawk) Performance Addendum ILT K. Brauer

LTC W. GrahamMAJ J. Henderson

70-08 AH-IG Letter Report, QualitativeAirworthiness Sep 1970 M. BussLR Assessment of AH-IG Cobra Night Fire Control

System (CONFICS)

70-09 YO-3A Army Preliminary Evaluation Ill YO-3A Sep 1970 LTC I. Rundgren 876 095Airplane MAJ A. Deel

70-10 AH-IG Airworthiness and Flight Characteristics Test Oct 1970 G. Bender 951 594(Limited) AH-IG Helicopter with the Southeast M. BussAsia Multisensor Armament System Helicopter(SMASH)

70-12 CH-47C CH-47C 50,000-Pound Gross Weight Mar 1971 MAJ A. ToddLR Evaluation CH-47C ILT D. D'Amore

LTC H. Chambers

70-14 UH-IH Airworthiness Qualification Test of the UH-IH Jan 1971LR Helicopter with Airborne Searchlight Infrared

Filter Installed

70-15-I OH-58A Instrument Panel and Avionics Compartment Sep 1972 E. Laing 907 738Environmental Survey Production OH-58A CPT J. ClaxtonHelicopter MAJ L. Hepler

LTC W. Graham

70-15-2 UH-IH Vibration and Temperature Survey Production Jan 1973 E. Laing 909 441UH-IH Helicopter MAJ L. Hepler

MAJ R. Merrill

70-15-3 CH-54B Vibration and Temperature Survey CH-54B Mar 1973 E. Laing 910 495Helicopter MAJ R. Merrill

CW4 J. Reid

70-15-4 OH-6A Vibration and Temperature Survey Aug 1973 E. Laing 914 172Production OH-6A Helicopter MAJ J. Smith

CW3 J. Hill

14

1970(continued)


70-15-5 AH-IG Vibration and Temperature Survey Production Mar 1974 E. Laing A002 063AH-1G Helicopter CPT A. Weand

70-15-6 CH-47C Vibration and Temperature Survey Sep 1975 E. Laing A022 348Production CH-47C Helicopter CPT M. Hawley

R. SmithCPT J. O'ConnorCPT L. Kronenberger

70-16 Interim Report, Comparison of VSTOL Sep 1970LR Specifications to Helicopter Flight Test Data

70-17 A Portable Instrumentation Kit Feasibility Jun 1972 R. Jefferis 751 188Study W. Rivers

70-19 Letter Report, Advanced Instrumentation and Mar 1972 V. DiekmannLR Data Analysis System Demonstration

70-20 UH-1D Letter Report, Handling Qualities of the UH-ID Aug 1970LR Helicopter with Terminal Communications System

(TACSAT) Antenna Installation

70-22 UH-IH Letter Report, UH-1H Helicopter with the Oct 1972 J. PetrieLR Airborne Ambush Detector (AAD), Qualitative MAJ A. Todd

Handling Qualities Evaluation

70-23 UH-1C Investigation of Engine Rigging, Airspeed and Dec 1970 LTC J. Fitch 717 047Rotor RPM Effects on Steady State Autorotational J. ShapleyPerformance

70-24 TH-55A Autorotational Entry Improvement Program Dec 1972 B. Boirun 908 657TH-55A Helicopter LTC W. Benoit

70-25 AH-IG Engineering Flight Test AH-1G (Hueycobra) Apr 1971 CPT B. Nicholson 887 550Helicopter Autorotational Entry Characteristics M. Buss

70-29 UH-IM Letter Report, Vibration Survey Tests on the Nov 1970 LTC D. HendricksonLR UH-IM Helicopter with the ForwardLooking

Infrared (FLIR) System Installed

70-29 UH-IM Vibration and Elevator Loads Survey Tests of Jun 1971 R. Finnestead 885 839the UH-IM Helicopter with the Forward- LTC D. HendricksonLooking Infrared (FLIR) System Installed

70-32 U-8 Letter Report, U-8 Aircraft Procedures Dec 1970 K. FerrellLR Evaluation

70-33 UH-IC Evaluation of Fuel Flowmeter Instrumentation Jan 1971 A. Winn 219 280R. Jefferis

70-38 Model Letter Report, Reevaluation of Boeing-Vertol Oct 1971 G. YamakawaLR 347 Model 34 LTC D. Hendrick

15

1970(continued)


70-38 Model Tech Eval Boeing-Vertol Model 347 Advanced Jan 1972 G. Yamakawa 900 263347 Technology Helicopter, Phase I A. Steinmetz

SP4 R. GreenlandLTC D. Hendrickson

70-40 UH-IH Letter Report, Helicopter-Mounted Insecticide Feb 1973 MAJ R. WaddellLR Spray System Evaluation SP4 J. Lehman

70-43 Scorpion Evaluation of the Scorpion Helicopter Mar 1972 MAJ R. ChaplinLR MAJ J. Alvis

1971

71-01 CH-54B Letter Report, Qualitative Evaluation of Aug 1971 J. WattsLR Instrument Flying Qualities of the MAJ J. Henderson

CH-54B Helicopter

71-01 CH-54B Instrument-Flight-Rules Capability Evaluation Dec 1972 E. Bailes 908 658CH-54B (TARHE) Helicopter V. Diekmann

J. WattsMAJ J. Henderson

71-03 OH-6A Study, Pilot Perceived Jettison Envelope Jun 1973 A. Winn 768 171OH-58A J. KishiAH-56

71-04 UH-IB Letter Report, Airworthiness Qualification Test Apr 1971 MAJ D. BroadhurstLR UH-IB Helicopter with XM26 Armament TOW ILT R. Thomas

System Installed Under Asymmetric Loading

1-05 OH-6A Letter Report, Evaluation of Stability and Jan 1974 V. DiekmannLR Control Test Methods LTC R,. Waddell

71-07 UH-IM Letter Report, Army Preliminary Evaluation May 1971 MAJ D. BroadhurstLR of the UH-IM Helicopter Multifunction System CPT B. Nicholson

(HELMS)

71-09 UH-IM Letter Report, Follow-On Vibration Survey May 1971 R. FinnesteadLR of the UH-IM/FLIR MAJ R. Holasek

S. Streulker

71-11 OH-6A Letter Report, Evaluation, AN/APN 171 Oct 1971 J. WattsLR Radar Altimeter S. Streutker

71-16 TS-2A Letter Report, Phase I TS-2A Airtanker Jul 1972 MAJ Rt. HolasekLR Evaluation SP4 J. Lehman

16

1971(continued)

Project Aircraft AdNumber Type Report Title Date Author(s) Numbcr

71-17 SEE USAAEFA PROJECT NO. 70-02aka

70-02

71-18 UH-IH Letter Report, UH-IH Tail Rotor Hover Oct 1971 R. FinnesteadLR Performance LTC W.Graham

71-18 UH-IH Tail Rotor Performance and Translational Flight Jan 1972 R. Finnestead 901 787Handling Qualities Tests UH-IH Helicopter LTC W. Graham

71-21 OH-58A Letter Report Monitoring of OH-58A Snow Dec 1971 MAJ HeplerLR Ingestion Test

71-22 NUH-IB Letter Report, Airworthiness Test of the NUH-IB Aug 1971 MAJ R.HolasekLR Helicopter Equipped with an Automatic Terrain- SP4 J. Lehman

Avoidance/Following System

71-24 OH-58A Evaluation of theOH-58A Helicopter with Dec 1972 E. Laing 907 291an Allison 250-C20 Engine T. Benson

SP5 A. WernerMAJ D. Broadhurst

71-27 UH-IC Airworthiness Evaluation UH-IC XM156/ Jan 1972 A. Winn 892 242Hornet Missile System J. Kishi

71-29 UH-IH Letter Report, Reevaluation of the DSPG Aug 1971 MAJ J. BurdenLR SPIKE-EXRAY Program

71-30 UH-IC Flight Evaluation, Elliott Low-Airspeed Sep 1972 A. Winn 753 343Sensor, Final Report I J. Kishi

71-30 UH-IC Flight Evaluation, Aeroflex True Airspeed Mar 1973 K. Ferrell 764 240OH-58A Vector System Low-Airspeed System, Final A. WinnF-51D Report ii J. Kishi

B. Jefferis

71-30 UH-IC Flight Evaluation, Pacer Systems Inc. LORAS I1 Mar 1974 B. Boirun 780 018Airspeed System, Low-Airspeed F. DominickSensor, Final Report III J. Kishi

MAJ J. SmithMAJ R. Merrill

71-30 NUH-IC Flight Evaluation, J-Tee Airspeed System Apr 1974 F. Dominick 780 019Low-Airspeed Sensor, Final Report IV B. Boirun

J. KishiR. Jefferis

71-30-5 NUH-IM Flight Evaluation, Rosemount Orthogonal Low Nov 1974 CPT J. O'Connor 009 711Airspeed System, Low-Airspeed Sensor, Final SP4 J. BullockReport V R. Jefferis

71-30-6 NUH-IM Flight Evaluation, Elliott Dual-Axis Low Sep 1975 F. Dominick A019 360Airspeed System, LASSIE I!, Low Airspeed K. FerrellSensor, Final Report VI CPT J. O'Connor

17

1971(continued)


71-31 UH-li- ALARM System Airworthiness Test Feb 1972 MMJ R. HolasekLR MAJ J. Alvis

PFC J. Lehman

7 1-32 Utility Tactical Transport Aircraft System Apr 1972 0. Yamakawa. 902 767(UTTAS) Maneuver Criteria MA] G. Broadhurst

MAJ J. Smith

71-34 OH-6C Army Preliminary Evaluation, Prototype Feb 1972 GJ. Skinner 901 268Hughes, Model 369C (OH-6C) Helicopter R. McClellan

LTC A. Deel

71-41 CH-47C CH-47C Improved Flight Control System Dec 1972 MMJ W. HortonLR SP4 C. Bowers

71-42 UK-lit UH-l/XM56, Army Preliminary Evaluation Fcb 1972 MA] R. ChaplinLR PFC J. Lehman

71-43 AH-1G AK-IG Lateral Flight Performance Test Jun 1972 MAJ L. HeplerLR J. Kishi

A. Winn

71-45 UH-IH XM56 Mini-Dispersion Test Feb 1972 MMJ R. ChaplinLR SF4 1. Lehman

71-46 OH-58A OH-58 Autorotational Evaluation Feb 1972 J. Watts 035 727LR V. D-ekmann

7 1-47 RU-21B CEFIRM LEADER RU-21B and RU-21C Air- Sep 1972 MMJ R. ChaplinLR RU-21iC worthiness Tests SF4 3. Lehman

1972

72-01 OH-58A Instrument Flight Evaluation OH-58A Sep1972 T. Benson 907 317Helicopter MAJ J. Smith

72-02 CL-215 Limited Evaluation of Canadair's CL-215 Nov 1970 MA] R. HolasekLR Water Bomber/Utility Aircraft

72-02 CL-215 Limited Evaluation Canadair CL-215 Oct 1972 MA] J. AlvisAmphibious Airplane MMJ R. Holasek

J. Kishi

72-03 OH-58A Fluidic Yaw Damper Evaluation Installed Dec 1972 MA] J. SmithLR on the OH-58A Helicopter MMJ R. Chaplin

R. Smith

18

1972(continued)


72-05 UH-IM Rotor Flow Survey Program UH-IM Helicopter May 1974 B. Boirun 787 428R. JefferisMAJ R. Holasek

72-06 OH-6A Instrument Flight Evaluation OH-6A Helicopter, Nov 1973 A. Wl.n 780 C16Part I LTC W. Griffith

MAJ C. Mittag

72-06 OH-6A Flight Evaluation, OH-6A Helicopter Kaiser Feb 1973 A. Winn 781 990FP-50B Flight Director System, Part 11 LTC W. Griffith

MAJ C. Mittag

72-08 AH-56A Attack Helicopter Evaluation AH-56A Jun 1972 J. Johnson 771 914Cheyenne Compound Helicopter G. Bender

R. McClellanMAJ J. BurdenCPT M. Larsen

72-09 S-67 Attack Helicopter Evaluation Blackhawk Jul 1972 G. Yamakawa 771 161S-67 Helicopter A. Winn

R. SmithSP4 R. AndersonMAJ W. GriffithMAJ W. Horton

72-10 Model Attack Helicopter Evaluation Model 309 Jul 1972 J. Nagata 771 151309 KingCobra Helicopter G. Skinner

PFC G. SmithR. JungelMAJ L. HeplerLTC P. Stringer

72-12 Model EngineeringFlight Test Boeing-Vertol Model 347 Oct 1972 A. Steinmetz 909 933347 Advanced Technology Helicopter Phase 11 SP4 C. Bowers

LTC A. DeelMAJ W. Horton

72-13 RU-21E Modified LEFT-FOOT RU-21E Direction Jun 1972 MAJ R. ChaplinLR Finding (DF) Demonstration PFC G. Smith

72-14 OH-58A Helicopter Autorotational Demonstration Jun 1972 J. WattsLR S. Streutker

72-15 CH-47C CH-47C Weight and Balance System Mar 1973 J. NagataLR

72-16 AH-IG AH-IG Vertical Climb Height-Velocity Sep 1972 K. FerrellLR Diagram A. Frederickson

J. Kishi

72-18 AH-IG Army Preliminary Evaluation Improved Dec 1972 G. Yamakawa 907 694AH-IQ Cobra Armament System ILT L. Toman

SP5 A. WernerMAJ R. Holasek

19

1972(continued)


72-19 OV-ID OV-ID 300-Gallon External Drop Tank Sep 1972 MAJ R. ChaplinLR Performance Evaluation SP4 J. Lehman

72-20 OH-58A Handling Qualities Evaluation of the OH-58A Feb 1973 R. Smith 909 536Helicopter Incorporating the Model 570B Three- T. BensonAxis Stability and Control Augmentation System MAJ J. Smith

72-21 Oll-6A OH-6A/Bifurcated Exhaust Duct Jul 1972 MAJ R. ChaplinLR T. Benson

72-24 OH-58A OH-58A/Insulated Infrared ExhaustAirworthiness Aug 1972 J. WattsLR Evaluation S. Streutker

72-26 S-67 Attack Helicopter High-AltitudeEvaluation Jul 1972 G. Yamakawa 771 051Blackhawk S-67 Helicopter A. Winn

MAJ W. Horton

72-28 OH-6A Engineering Flight Test OH-6A Helicopter Aug 1973 SP4 R. Anderson 913 954with Cambered Tail Rotor Blades and Pedal LTC R. WaddellForce Compensators

72-29 AH-IG Instrument Flight Evaluation AH-IG Jul 1975 G. Skinner A026 633Helicopter CPT M. Larsen

SP4 G. SmithSP4 P. BoninCW4 J. ReidLTC R. WaddellMAJ L. HeplerMAJ R. Merrill

72-30 AH-IG Engineering Flight Test AH-IG Helicopter with Jun 1973 G. Skinner 776 359Model 212 Tail Rotor, Part I, Load Survey SP4 G. Smith

MAJ L. HeplerPFC P. Bonin

72-30 AH-IG Engineering Flight Test AH-IG Helicopter with Sep 1973 J. Nagata 776 360Model 212 Tail Rotor, Part 11, Performance G. Skinnerand Handling Qualities SP4 G. Smith


72-31 Model Sideward Flight, High-Altitude Evaluationand Aug 1972 J. Nagata A109 512aka 309 Simulated Engine Failures KingCobra Model 309 R. Jungel

72-34 Attack Helicopter MAJ L. HeplerPFC G. SmithG. Skinner

72-32 OH-6A OH-6A Autorotational Evaluation Nov 1972 MAJ W. GriffithLR R. McClellan

72-34 SEE USAAEFAPROJECT NO. 72-31

20

1972(continued)


72-35 CH-47C Helicopter Icing Spray System Qualification Oct 1973 J. Hayden 775 803E. BailesJ. WattsCPT L. Brewer

72-38 01-58A OH-58A/ISTAR Airworthiness Evaluation Dec 1972 MAJ R. ChaplinLR G. Bender

72-39 CH-47C CH-47C Tandem Cargo Hook Demonstration May 1973 J. NagataLR CPT L. Brewer

'2-40 CH-54B Limited Performance Tests CH-54B (TARHE) Feb 1973 J. Johnson 910 263Helicopter V. Diekmann

SP4 J. JohnsonMAJ R. MerrillCW4 J. Reid

72-43 AH-IQ Airworthiness and Flight Characteristics Jul 1973 G. Yamakawa 914 458Evaluation AH-IQ Helicopter CPT K. Schrantz

1LT M. HanksSP4 A. WernerMAJ R. MerrillCW4 J. Reid

72-44 AII-56A Engineering Evaluation AH-56A Compound Mar 1973 J. Johnson 910 Zo2Helicopter with Advanced Mechanical Control G. BenderSystem MAJ J. Burden

1973

73-01 NUH-IM Helicopter Lift Margin System and Low-Speed Aug 1977 F. Dominick A060 553Performance Evaluation NUH-1M Helicopter D. Belie

R. JefferlsJ. O'ConnorA. KrynytzkyLTC W. Griffith

73-02 OH-58A Evaluation of the Teledyne Ryan Model 622 Nov 1973 MAJ C. Mittag 775 806Terrain-Following Radar System Installed on T. Bensonan OH-58A Helicopter CPT R. Tart

CW3 J. Meiss

73-04 CH-47C Icing Tunnel Test Hot-Film Anemometer Feb 1974 SP4 P. Bonin A005 )44R. Jefferis

21

1973(continued)

Project Alrcrart AdNumber 'ype Report 'Title Date Author(s) Numberi

73-04-1 CH-47C Artificial Icing Tests CH-47C Helicopter Aug 1974 MAJ C. Mittag A004 008CPT M. HanksCPT J. O'ConnorCPT L. Kronenberger

73-04-2 AH-IG Artificial Icing Tests AH-IG Helicopter Nov 1974 R, Smith A009 712CPT M. HanksMAJ C. MittagCW4 J. Reid

73-04-4 UH-IH Artificial Icing Tests UH-1H Helicopter Jan 1974 R. Smith 779 502Part I CPT M. Hanks

CPT L. BrewerCW4 J. ReidLTC W. Griffith

73-04-4 UH-IH Artificial Icing Tests UH-IH Helicopter, Jan 1974 CPT M. Hanks 779 503Part 11 Heated Glass Windshield MAJ C. Mittag

ILT M. HawleyLTC W. Griffith

73-04-7 All- 10 Artificial Icing Tests AII-IQ Helicopter (U) Jan 1974 CPT M. Hanks 531 5,10CW4 J. ReidMAJ R. Merrill

73-05 CH-47C CH-47C Terminal Radar Area Correlator Apr 1973 CPT L. BrewerLR Experiment (TRACE)

73-07 UH-1H Helicopter Night Landing System Airworthiness Jun 1973 MAJ R. ChaplinLR Evaluation R. Smith

73-09 OV-I NASA OV-l Accident Investigation Jun 1973 MAJ R. ChaplinLR LTC W. Griffith

73-10 UH-IH Tail Rotor Shaft Vibration Survey, Production Jul 1974 E. Laing A002 574UH-IH Helicopter CPT M. Hawley

CPT A. Weand

73-41 Instrumentation Specification for Climatic Aug 1973 K. Ferrell 771 053Laboratory Tests T. Lynch

73-71 Minutes of AVSCOM Helicopter IFR Conference Jan 1973

22

1974

Project Aircraft Ad


74-02 AH-IG AH-IG Helicopter Main Rotor Flow Survey Apr 1978 B. Boirun A057 443E. BailesR. JefferisMAI J. ArnoldCW3 3. Meiss

74-06-1 YUH-60A Government Competitive Test, Utility Tactical Nov 1976 J. Nagata B059 73SLTransport Aircraft System (UTTAS) Sikorsky, G. SkinnerYUH-60A Helicopter S. Kolwey

R. BuckaninMAJ C. MittagLCdr M. CoumnatosCW3 J. Meiss

74-06-2 YUH-61A Government Competitive Test, Utility Tactical Nov 1976 A. Winn B035 08 11.Transport Aircraft System (UTTAS) Boeing- MMJ J. JenksVertol, YUH-61A Helicopter F. Deprospero

CPT E. TavaresCPT J. O'ConnorLCdr J. Ludwig

74-07-1 YAH-63 Development Test 1 Advanced Attack Helicopter Dec 1976 G. Bender A 109 531Competitive Evaluation Bell YAH-63 Helicopter V. Diekmann

CPT M. Mathew%R. SmithMAJ C. ThomasR. WoratschekMAJ J. ArickCPT J. Arnold

74-07-2 YAH-64 Development Test I Advanced Attack Helicopter Dec 1976 MAJ R. Stewart A109 532Competitive Evaluation Hughes YAH-64 MAJ R. TarrHelicopter ILT M. Hill

B. BoirunT. BensonE. BailesW. Abbott

74-10 AH-IG AH-IG Heavyweight Autorotational Jan 1974 MAJ L. Hepler 785 553

LR Evaluation G. Yamakawa

74-10 AH-IG Engineering Flight Test AH-IG Helicopter May 1974 G. Yamakawa 785 553

Heavyweight Autorotational Evaluation I LT L. FreeJ. WattsMAJ L. Hepler

74-1 3 UHf-lH Artificial Icing Tests, Lockheed Advanced Jun 1975 CPT L. Kronenbcrgcr B00t7 2441.

Ice Protection System Installed on a UH-IH CPT M. HanksHelicopter MAJ R. Merrill

74-16 B30-105C BO-105C Evaluation Jan 1975 CPT M. Mathews

LR

23

1974(continued)


74-19 AH-1C Height-Velocity Test AH-IG Helicopter at Jun 1974 ILT L. Free A034 424Heavy Gross Weight, Low Elevation MAJ L. Hepler

74-20 OV-ID Hot Brick III Airworthiness Evaluation Nov 1974 D. Macpherson A012 202OV-11D Airplane CW4 J. Reid

74-21 Model Army Preliminary Evaluation I Model 200 Jun 1974 T. Benson A009 713200 Cefly Lancer CPT M. Hawley

G. YamakawaMAJ L. Brewer

74-21 Model Army Preliminary Evaluation II Model 200 Aug 1974 G. Yamakawa A009 714200 Cefly Lancer T. Benson

MAJ L. Brewer

74-22 JOH-58A Engineering Evaluation JOH-58A Helicopter Jun 1975 T. Benson A019 407with an Automatic Engine Relight System R. Buckanin

MAJ C. Mittag

74-23 OH-58A Handling Qualities Evaluation OH-58A Feb 1975 E. Bailes A033 827Helicopter Incorporating a Ministab 3-Axis R. BuckaninStability Augmentation System MAJ C. Mittag

74-25 T-42A T-42A Single-Engine Operation and Stall Feb 1974 MAJ W. HortonL Evaluation SP4 P. Bonin

74-27 CH-47C CH-47C Prototype Infrared Countermeasures Jun 1974 MAJ W. HortonLR (ICRM) Airworthiness Demonstration J. Nagata

SP4 P. Bonin

74-30 Model Airworthiness and Flight Characteristics Jul 1975 LTC W. Horton B014 228L214A Evaluation, Iranian Model 214A Helicopter G. Bender

ILT L. FreeCPT J. O'ConnorJ. NagataCPT R. Ward

74-31 UH-1H Natural Icing Tests, UH-IH Helicopter Jun 1974 LTC W. Griffith A002 007CPT M. HanksMAJ C. MittagCW4 J. Reid

74-32 Model Climatic Laboratory Evaluation, Iranian Aug 1976 MAJ R. Ward B030 107L214A Model 214A Helicopter CW4 J. Coleman

D. BelteK. Dorris

74-33 YAH-IR Army Preliminary Evaluation YAH-IR Improved May 1975 F. Dominick A018 420Cobra Agility and Maneuverability Helicopter R. Smith

MAJ R. Stewart

74-33 YAH-IR Army Preliminary Evaluation, YAH-IR Aug 1975 F. Dominick A024 850Improved Cobra Agility and Maneuverability R. SmithHelicopter Addendum MAJ R. Stewart

24

1974(continued)

Project Aircraft AdNumber Type Report Title Date Author(s) NtJnlh.1

74-34 YAH-IS Airworthiness and Flight Characteristics Aug 1975 G. Skinner A025 476Evaluation, YAH-IS Improved Cobra Agility W. Abbottand Maneuverability Helicopter CPT R. Tarr

74-35 RU-21H Guardrail IIA RU-21H Evaluation Jul 1974 G. Yamakawa A004 009T. BensonMAJ L. Brewer

74-36 RV-ID Army Preliminary Evaluation 1, RV-1D/ Aug 1974 G. Bender A005 220Quick Look 11 Aircraft CPT J. O'Connor

74-48 OH-58A Evaluation of an OH-58A Helicopter with Apr 1975 T. Benson A018 861an Allison 250-C20B Engine R. Buckanin

MAJ C. MittagCPT J. Jenks

74-77 Rotary Wing Icing Symposium Summary Jun 1974 COL D. WrightReport Commander

Volume I A061 445Volume 1I A061 422Volume III A061 423

74-87 Flight Evaluation of Non-dimensional Static Jul 1979 B. Boirun A082 831Longitudinal Stability Test Methods K. Ferrell

MAJ J. Jenks

74-94 An Advanced Instrumentation and Data Jul 1973 R. Lew.s 882 771Analysis System for Army Flight Testing Study

1975

75-01 AH-1G Performance and Handling Qualities AH-1G Apr 1975 A. Winn A019 482Helicopter Equipped with Three Metal/Plume MAJ R. StewartInfrared Suppressors Hot

75-03 RU-21A Flying Qualities Evaluation RU-21A Dec 1974 J. JohnsonCEFIRM LEADER Airplane CPT M. Hawley

MAJ R. Stewart

75-04 CH-47C Modified Helicopter Icing Spray System Mar 1977 G. Bender A055 039Evaluation CPT M. Mathews

CW4 J. Tulloch

75-05 CH-147 Qualitative Army Preliminary Evaluation Oct 1974 MAJ W. HortonLR (CH-47C) of the Canadian Production CH-147 Helicopter J. Watts

25

1975(continued)


75-06 CH-47C Letter of Effort, CH-47C, Active Arm External Apr 1976 CPT G. NeperenyLOE Load Stabilization System (AAELSS) II Flight

Evaluation Program

75-08 C-12A Airworthiness and Flight Characteristics Oct 1976 V. Diekmann A040 239Evaluation C-12A Aircraft R. Smith

J. WattsMAJ J. HannonCPT W. Norton

75-09 AH-IG Performance and Handling Qualities Evaluation Aug 1975 A. Winn A021 407

AH-1G Helicopter with Low Reflective ILT E. TavaresInfrared/Optical Paint MAJ R. Stewart

G. Skinner

75-10 U-21A Airworthiness and Qualification Evaluation Jan 1976 R. Smith A047 656U-21A Airplane with Low Reflective Paint CPT W. Nortonand Hot Metal Suppressors

75-11 JOH-58A Army Preliminary Evaluation, JOH-58A Hell- Dec 1975 T. Benson A024 727copter with Low Reflective Paint and Infrared MAJ C. ThomasCountermeasure Exhaust System R. Buckanin

75-12-1 YUH-60A Climatic Laboratory Evaluation, Utility Tactical Jul 1977 MAJ R. Ward B033 049LTransport Aircraft System (UTTAS) Sikorsky, J. GivensYUH-60A Ground Test Vehicle E. Walbey

C W4 R. Seefeldt

75-12-2 YUH-61A Climatic Laboratory Evaluation, Utility Tactical Jul 1977 D. Belte B031 052LTransport Aircraft System (UTTAS) Boeing- R. FollowillVertol, YUH-61A Ground Test Vehicle R. Seefeldt

D. Wallis

75-15 OV-IC Advanced Report, Engineering Flight Evaluation, May 1976C PT G. NeperenyLR OV-IC Aircraft Equipped with Angle-of-Attack/ MAJ R. Stewart

Stall Warning System

75-17-1 AH-1G Flight Evaluation, Pacer Systems, Low-Range May 1977 W. Abbott A045 222Airspeed System, LORAS 1000 B. Boirun

CPT G. HillCPT E. Tavares

75-17-2 AH-1G Flight Evaluation, J-TEC VT-1003 Vector May 1977 W. Abbott A046 553Airspeed Sensing System CPT S. Spring

MAJ R. Stewart

75-17-3 NUH-1M Flight Evaluation Rosemount Low Range Mar 1977 W. Abbott A046 491Orthogonal Airspeed System with 853 Sensor MAJ J. Guin

75-18 YAH-IQ Army Preliminary Evaluation, YAH-10 Heli- Aug 1975 ILT L. Free A020 111copter with a Flat Plate Canopy CPT J. Arnold

75-18 YAH-IQ YAH-IQ Fiat Plate Canopy Follow-on Feb 1976 CPT J. ArnoldEvaluation

26

1975(continued)

Project Aircrart AdNumber Type Report Title Date Author(s) Number

75-19-1 AH-IG Low Airspeed Sensor Location Tests AH-IG Feb 1977 K. Ferrell A052 467Helicopter B. Boirun

CPT G. Hill

75-19-2 AH-1G Flight Evaluation Honeywell Ultrasonic Jun 1976 CPT G. Hill A052 467Wind Vector Sensor System Fire Control CW3 J. MeissWind Sensor ReportB. Boirun

75-20 YOH-58A Army Preliminary Evaluation, YOH-58A Dec 1975 G. Skinner A024 501Helicopter with Flat-Plate CPT J. Arnold

75-21 YAH-1R Letter of Effort, YAH-IR Lateral Agility/IR Mar 1977 MAJ R. StewartLOE

75-22 NUH-IM Letter of Effort, Engine Characteristics Test Jun 1977 F. DominickLOE

75-24 JOH-58A Integrated Controller Evaluation Sep 1976 CPT J. Arnold A035 064CPT M. MathewsMAJ C. Thomas

75-25 AH-IG Letter of Effort, Qualitative Evaluation of Oct 1975LOE AH-IG with Kaiser Ministab

75-26 UH-1H Lockheed Advanced ice Protection System May 1976 CPT L. Kronenberger

75-27 JUH-1H Letter of Effort, Qualitative Evaluation of Jan 1976LOE JUH-IH with Kaiser 3-Axis MINISTAB

75-28 Letter of Effort, Phase 11 of Joint Acoustic Test Jan 1976 CPT J. ArnoldLOE Program with AMRDL/AMES

1976

76-02 Model Performance and Systems Evaluation Iranian Mar 1977 G. Yamakawa B027 647L214C Model 214C Helicopter R. Woratschek

CPT S. Spring

76-03 C-12A Landing Gear Capability Tests Mar 1977 V. Diekmann A046 554J. Watts

76-04 SEE JSAAEFA PROJECT NO. 75-26

76-07 YAII-IR Army Preliminary Evaluation, Improved Main Jun 1977 J. Watts A072 83(0Rotor Blade Installed on a YAH-IR Helicopter F. Dominick

MAJ J. Guin

27

1976(continued)


76-08 YAH-IR Airworthiness and Flight Characteristics Nov 1977 G. Yamakawa A074 895Evaluation Improved Main Rotor Blade J. NiernannInstalled on a YAH-IR Helicopter R. Smith

R. WoratschekMMJ J. JenksCPT W. NortonCW4 J. Tulioch

76-09-1 YUH-60A Artificial Icing Test, Utility Tactical Transport Feb 1977 R. Buckanin A109 530Aircraft System (UTTAS), Sikorsky YUH-60A W4 J. Tulloch

76-09-2 YUH-61A Artificial Icing Test, Utility Tactical Transport Jan 1977 CPT J.O'ConnerAircraft System (UTTAS), Boeing-Vertol CPT E. TavaresYUH-61A Helicopter MMJ J. Hagen

76-10 OV-11D OV-ID Low Reflective Paint Evaluation undated J. WattsLR

76-11-I OH-58C Preliminary Airworthiness Evaluation Mar 1978 G. Yamakawa A071 699OH-58C Helicopter MAJ J. Hagen

R. BuckaninCPT T. Burch

76-11-2 OH-58C Airworthiness and Flight Characteristics Apr 1979 MAJ S. Spring A080 138OH-58C Interim Scout Helicopter CPT T. Burch

R. BuckaninJ. Niemann

76-13 NUH-IH Airworthiness Evaluation NUH-1H Helicopter May 1977 T. Benson A047 971with Global Positioning System MMJ C. Thomas

1977

77-02 Temperature Effects of Sunlight on Helicopter Feb 1977 MMJ M. MathewsLR Rotor Blades

77-04 YAH-IS Army Preliminary Evaluation, YAH-IS, NH- Aug 1977 MMJ J. Arnold A066 573copter with Modified Flat Plate Canopy Installed MMJ J. Gumn

CW4 J. BishopG. Skinner

77-OS U-21A Icing Evaluation U-21A Airplane with Low May 1977 T. Benson A046 852Reflective Paint R. Woraisehek

MAM C. ThomasMMJ R. Stewart

28

1977(continued)


77-07 TS-2A TS-2A Air Tanker Evaluation, Phase II May 1978 J. Watts A060 940E. BailesMAJ S. SpringMAJ J. Guin

77-09 UH-1H Preliminary Airworthiness Evaluation, UH-IH May 1978 V. Diekmann A078 476Helicopter Equipped with Multiple Target MAJ M. MathewsElectronic Warfare System (MULTEWS) MAJ S. Spring

MAJ J. HagenCW4 J. Tulloch

77-10 UH-IH Qualitative Evaluation of Flying Qualities of a Jul 1977 MAJ R. StewartLR UH-IH Helicopter with GE Infrared Exhaust

Suppressor Installed

77-11 OH-58A Flight Evaluation, MK II Integrated Controller Apr 1978 MAJ J. Hagen A065 072Installed on an OH-58 Helicopter CPT P. Moe

R. Woratschek

77-14 Letter of Effort, Lightweight Launcher Jun 1977 MAJ C. ThomasLOE Vibration Study T. Benson

MAJ P. Moe

77-15 EH-IH Preliminary Airworthiness Evaluation, Oct 1977 MAJ J. Guin A058 785EH-IH Helicopter Quick Fix, Phase IA R. Buckanin

77-17-3 UH-60A Letter Report UH-60A Aft CG Aug 1980 CPT M. HanksLR MAJ B. Picasso

J. Niemann K. Flaig

77-17-5 UH-60A Report, Experimental Testing of the UH-60A Nov 1981 R. BuckaninLR Black Hawk Helicopter at Heavy Gross Weight MAJ R. Robbins

and Extended Forward Center of Gravity MAJ J. BensonCPT R. Vincent

77-18 YUH-60A Preliminary Airworthiness Evaluation, YUH-60A Jan 1978 A. WinnBlack Hawk Helicopter with Electronic Flight MAJ C. MittagControl System CW4 J. Bishop

J. Nagata

77-19 RU-21H Preliminary Airworthiness Evaluation, RU-21H Mar 1978 J. Niemann A068 347Guard Rail V Aircraft R. Smith

CPT W. NortonMAJ F. Doten

77-20 U-21A Evaluation of Experimental Radio Meteorological May 1977 MAJ C. MittagMeasurement Package Antenna Installed on aU-21A Wing

77-22 OV-ID Preliminary Airworthiness Evaluation, OV-ID Feb 1978 MAJ R. WardAirplane with AN/ALQ 147 XE-I and XE-2 G. YamakawaSystems Installed MAJ R. Taff

29

1977(continued)


77-23 UH-60A Production Validation Test-Government (PVT-G) Oct 1979 G. YamakawaPerformance Guarantees UH-60A Black Hawk 0. BenderHelicopter R. Buckanln

CPT R. RobbinsE. BailesCW4 J. Tulloch

77-24 CH-47C CH-47C Inlet Flow Distortion Evaluation May 1978 MAJ J. GuinLR

77-25 AH-1S Preliminary Airworthiness Evaluation, AH-lS May 1980 G. Bender A089 625Helicopter with Ogee Tip Shape Rotor Blades R. Woratschek

D. OttomeyerH. ArnaizMAJ L. HigginsCW4 J. Tulloch

77-26 OH-58C OH-58C Rain Removal System Test Oct 1977 MAJ J. HagenLR

77-27 Letter of Effort, Hellfire Launcher Vibration Oct 1977 CPT P. MoeLR Survey

77-29 CH-47C Airworthiness and Flight Characteristics Aug 1978 MAJ R. TarrLR Evaluation, CH-47C Helicopter with MAJ J. Guln

T55-L-712 Engines G. Skinner

77-30 UH-1H Artificial Icing Test Ice Phobic Coatings Jun 1978 CW4 J. Tulloch A059 875on UH-IH Rotor Blades R. Smith

MAJ F. DotenCW4 J. Bishop

77-31 CH-47C Preliminary Airworthiness Evaluation CH-47C Apr 1979 MAJ S. Spring A069 891with Fiberglass Rotor Blades (with T55-L-712 J. NiemannEngines) MAJ G. Wilson

77-32 Model Limited Airworthiness and Flight Character- May 1979 MAJ J. Guin A071 271214A istics Evaluation Model 214A Helicopters G. Bender

with Fiberglass Rotor Blades E. BallesCPT R. Robbins

77-33 AH-IS Preliminary Airworthiness Evaluation, AH-IS May 1978 G. Bender A067 757Helicopter Equipped with Garrett Infrared E. BallesRadiation Suppressor System and AN/ALO-144 LTC C. FrankenbergerJammer MAJ S. Spring

77-34 OH-58A Preliminary Airworthiness Evaluation OH-58A/ Dec 1977 G. BenderLR XM-130 Chaff Dispenser CPT T. Burch

77-35 AH-IS AH-ISIXM-130 Chaff Dispenser, Preliminary Mar 1978 J. NiemannLR Airworthiness Evaluation CPT T. Burch

30

1977(continued)


77-36 YAH-64 Engineering Design Test 1, Hughes YAH-64 Sep 1978 MAJ R. Tarr A064 359Advanced Attack Helicopter V. Diekmann

MAJ R. StewartR. Woratschek

77-37 Model Handling Qualities Test on a Model 214A Dec 1977 CPT S. SpringLR 214A Helicopter

77-38 AH-IS Production Validation Test - Government Oct 1979 V. Diekmann A097 689Kaman K747 Improved Main Rotor Blade MAJ G. Mullen

CW4 J. TullochT. BensonCPT F. BowersR. Woratschek

1978

78-01 UH-60A UH-60A Command Instrument System Mar 1978 LTC W. GriffithLR Preliminary Evaluation MAJ R. Stewart

78-02 AH-IG Preliminary Airworthiness Evaluation, AH-IG Jul 1979 MAJ P. Moe A078 340with the Airborne Targe tAcquisition Fire R. SmithControl System and the Hellfire Modular MissileSystem Installed

78-03 Al-IS Preliminary Airworthiness Evaluation, AH-IS Feb 1979 CPT P. Moe A071 343Helicopter Installed with Enhanced Cobra R. SmithArmament System (AH-IS/ECAS) CW3 R. Williams

R. Woratschek

78-04 UH-IH Preliminary Airworthiness Evaluation UH-IH Jul 1978 J. NagataLR Helicopter with Interim-Interim-Standoff MAJ J. Hagen

Target Acquisition System (12 SOTAS)

78-05 UH-60A Letter Report, Artificial and Natural Icing Tests Oct 1979 CW4 J. TullochLR Production UH-60A LTC G. Mullen

D. Belite

78-07 OV-IC Airworthiness and Flight Characteristics Test May 1979 R. Smith A069 827OV-IC Takeoff Performance J. Watts

J. NlemannMAJ J. GuinG. Yamakawa

31

1978(continued)


78-09 OH-58C Preliminary Airworthiness Evaluation OH-58C May 1980 CW4 J. Bishop A094 172Helicopter with a Mast Mounted Sight CPT M. Hanks

T. BensonA. Arrigo

78-10 AH-1G AH-IG Helicopter, 19-Round Lightweight Mar 1979 G. Skinner A069 828Airborne Launcher Jettison Envelope MAJ F. DotenDetermination

78-11 YUH-60A Preliminary Airworthiness Evaluation IIA Dec 1978 CW4 J. BishopLR YUH-60A Helicopter with Production Avionics, CPT T. Burch

Electronic Flight Control System and CW3 R. WilliamsCommand Instrument Systems

78-12 OH-58C Letter Report Airworthiness and Flight Feb 1981 MAJ R. CarpenterLR Characteristics Test of OH-58C with XM-130 G. Yamakawa

Chaff Dispenser System

78-15 AH-IS Preliminary Airworthiness Evaluation Aug 1978 LTC C. FrankenbergerLR Production AH-IS Helicopter Equipped with T.Benson

AN/ALQ-136 (XE-2) Countermeasures System

78-16 AH-IS Preliminary Alrwotthite$$ Evaluation Modified Aug 1978 LTC C. FrankenbergerLR AH-IS Helicopter Equipped with AN/ALQ-136 T. Benson

Countermeasures System

78-17-1 JAH-IS Airworthiness Demonstration, JAH-IS PNVS May 1979 CPT T. BurchSurrogate Trainer (Martin-Marietta) COMP SENS R. Smith

78-17-2 JAH-IS Airworthiness Demonstration, JAH-IS PNVS Aug 1979 MAJ F. DotenSurrogate Trainer (Northrop) COMP SENS CPT F. Bowers

78-18 CH-47C Artificial Icing Tests with CH-47C Helicopter Jul 1979 J. Niemann A081 860with Fiberglass Rotor Blades CPT F. Bowers

MAJ S. Spring

78-19 OV-IC Airworthiness and Flight Characteristics OV-lC Apr 1979 MAJ R. Taffwith Angle-of-Attack/Stall Warning and G. SkinnerSpeed Control System

78-21 UH-IH Artificial and Natural Icing Tests for Aug 1979 MAJ G. WilsonLR Qualification of UH-IH Kit A Aircraft R. Woratschek

78-21-2 UH-IH Microphysical Properties of Artificial and Aug 1979 MAJ G. Wilson A084 633Natural Clouds and Their Effects on UH-IH R. Woratschek

Helicopter Icing

78-22 UH-60A Preliminary Airworthiness Evaluation III Apr 1979 J. NagataLR UH-60A Black Hawk Helicopter CW4 J. Bishop

CW3 R. WilliamsG. Skinner

32

1978(continued)

Project Aircraft AdNurnber Type Report Title Date Author(s) Number

78-23 YAH-64 Engineer Design Test 2 Hughes YAH-64 Jun 1979 V. Diekmann A098 923

Advanced Attack Helicopter T. BensonR. Woratschek

S. Snakenberg

MAJ R. TarrMAJ P. MoeCW3 R. Williams

1979

79-01 AH-IS Letter Report, Preliminary Airworthiness Oct 1979 V. DiekmannLR Evaluation of AH-IS with Fixed Wings Removed LTC G. Mullen

79-02 JUH-IH JUH-IH Ice Phobic Coating Icing Tests Jul 1980 MAJ P. Morris A096 361R. Woratschek

79-02-2 CH-47C Helicopter Icing Spray System (HISS) Nozzle Sep 1981 D. Belte A109 405Improvement Evaluation

79-03 AH-IS AH-1 Lightweight Airborne Launcher MAJ L. Higgins A101 461

Jettison Evaluation D. Ottomeyer

79-04 AH-IS Letter Report of Preliminary Airworthiness Mar 1980 R. WoratschekLR Evaluation of Production AH-IS Helicopter with MAJ P. Morris

90 degree Gearbox and Skid Cross-Tube FairingsRemoved

79-06 YCH-47D Preliminary Airworthiness Evaluation 1 May 1980 J. Niemann A092 633

(PAE 1) of the YCH-47D Helicopter MAJ G. WilsonMAJ C. Adam

CPT F. BowersS. Arthur

79-08 AH-lS AH-IS PRODUCTION Airworthiness and Flight Nov 1980 CW4 J. Tulloch A100 946

Characteristics for Instrument Flight D. OttomeyerLTC C. FrankenbergerMAJ B. Picasso

79-09 AH-IS Preliminary Airworthiness Evaluation AH-IS Jun 1980 MAJ P. Morris A092 614(Prod) Helicopter with a Substitute Straight LTC C. Frankenberger

Exhaust Pipe J. NlemannR. Woratschek

79-10 OV-ID Airworthiness and Flight Characteristics Oct 1979 MAJ G. WilsonLR Evaluation OV-ID with Ange-of-Attack/ LTC C. Frankenberger

Stall Warning System CPT F. Bowers

33

1979(continued)


79-I UH-60A Letter Report Preliminary Airworthiness Dec 1979 J. NagataLR Evaluation (PAE) IliA, UH-60A Helicopter LTC G. Mullen

with the Infrared (IR) Reduction Subsystem CW3 R. WilliamsG. Skinner

79-12 OH-58C Letter Report, OH-58C Directional and Mar 1981 CW4 J. BishopLR Longitudinal Control Mapping Evaluation T. Benson

D. Ottomeyer

79-14 AH-IS Letter Report AH-1S Helicopter Tail Boom Oct 1979 J. NiemannLR 3-Way Temperature Survey MAJ P. Morris

79-15 OH-58C Preliminary Airworthiness Evaluation, OH-58C Dec 1979 T. BensonLR Helicopter with Installed Bell Helicopter Textron CW4 J. Bishop

Model 206L-1 Tail Rotor

79-16 AH-IS Letter of Effort and Data Transmittal AH-IS Oct 1979 R. WoratschekLOE Main Transmission Top Cover Flange Stress

Measurements Evaluation

79-8 OH-58C Letter Report Preliminary Airworthiness Jul 1980 T. BensonLR Evaluation OH-58C Helicopter with 206L-1 CW4 J. Bishop

Tail Rotor and Bell Helicopter Textron 570B D. OttomeyerStability and Control Augmentation System MAJ J. Benson

79-19 UH-60A Artificial and Natural Icing Tests Production Jun 1980 CPT M. Hanks A090 527UH-60A Helicopter MAJ L. Higgins A096 239

V. Diekmann

79-22 Hughes Potential Airworthiness Evaluation of the Jul 1980 MAJ B. PicassoLR 500D Hughes 500D CW4 J. Tulloch

G. BenderD. Ottomeyer

79-23 OH-58C Letter Report Preliminary Airworthiness Jun 1980 MAJ J. BensonLR Evaluation OH-58C Configured with a Wire T. Benson

Strike Protection System

79-24A UH-60A Report Flight Evaluation of UH-60 with the Dec 1981 G. SkinnerLR Roll Trim Actuator Disconnected MAJ J. Benson

D. Macpherson

79-86 UH-1H Ice Phobics Blade Tracking and Comparison May 1981 W. Abbott AI08 121of Vibration Analysis Techniques F. Dominick

34

1980


80-01 OV-IC Letter Report OV-IC (Short Wing) Fuel Apr 1980 MAJ R. CarpenterLR Siphoning Evaluation

80-02 Model Letter Report Preliminary Airworthiness Aug 1980 G. YamakawaLR 249 Evaluation (PAE) of Bell Helicopter MAJ B. Picasso

Textron (BHT) Model 249 Cobrai. Brown

80-03 YAH-64 Engineering Development Test 4, YAH-64 Jan 1980 G. Bender A098 922Advanced Attack Helicopter MAJ B. Picasso

MAJ L. HigginsV. DiekmannD. Ottomeyer

80-04 CH-47C Helicopter Icing Spray System (HISS) Jun 1981 R. WoratschekLR Evaluation and Improvements LTC G. Wilson

80-04-2 CH-47C Helicopter Icing Spray System (HISS) Evaluation Jun 1982 R. Woratschekand Improvement

80-05 YCH-47D Letter Report Preliminary Airworthiness Jul 1980 LTC G. WilsonLR (EvaluationPAE) II of the YCH-47D with MAJ C. Adam

Modified Advanced Flight Control J. Niemann

80-06 UH-IH Preliminary Airworthiness Evaluation of UH-IH Jun 1981 MAJ B. Picasso Al I) 213with Hot Metal Suppressor and Infrared Jammer CPT L. A. Haworth

D. OttomeyerCPT R. Vincent

80-07 YAH-64 Climatic Laboratory Survey, Hughes Mar 1982 G Bender A124 670CPT R. SavageMAJ C. Adam

80-08 YAH-64 YAH-64 Icing Survey Sep 82 MAJ M. Hanks

80-11 AH-IS Letter Report Drag Characteristics Evaluation Nov 1980 G. BenderLR of Prototype Hellfire Modular Missile System CW4 J. Tulloch

(HMMS) Launcher

80-11-2 AH-1S Letter Report Drag Characteristics Evaluation Nov 1980 G. BenderLR of Prototype Hellfire Modular Missile System MAJ B. Picasso

(HMMS) Launcher - Masking/Unmasking D. Ottomeyer

80-12 YAH-64 Engineer Design Test, Government EDT-5 Mar 1981 MAJ P. MorrisLR of the Advanced Attack Helicopter (AAH) D. Ottomeyer

80-13 CH-47C Helicopter Icing Spray System Calibration, Ice Aug 81 J. HendersonPhobics and FAA R&D Evaluation R. Woratschek

CPT L. Haworth

80-14 UH-60A Limited Artificial and Natural Icing Tests Aug 1981 MAJ M. Hanks A112 582Production UH-60A Helicopter (Re-evaluation) V. Dlekmannn

MAJ J. Benson

35

1980


80-15 O1t-58C Preliminary Airworthiness Evaluation of the Jul 1981 LTC R. WardLR OH-58C Helicopter with Fixed Short Landing MAJ J. Benson

Gear with Two Position Landing Gear G. Yamakawa

80-16 OV-1D Letter Report Limited Artificial Icing Jul 1981 E. GilmoreLR Tests of the OV-ID CPT R. Robbins

80-17-1 YAH-64 Airworthiness and Flight Characteristics Test, Sep 81 MAJ P. MorrisPart 1, YAH-64 Attack Helicopter J. Ottomeyer

MAJ L. HigginsMAJ B. PicassoCPT R. SavageG. Bender

80-17-2 YAH-64 Airworthienss and Flgiht Characteristics Test, Feb 82 MAJ B. Picasso A125 270Part 2, YAH-64 Advanaed Attack Helicopter B. Buckanin

J. OttomeyerMAJ G. Downs

80-17-3 YAH-64 Airworthiness and Flgiht Characteristcs Test Oct 82 MAJ B. Picasso(A&FC), YAH-64 Advanced Attack Helicopter R. BuckaninPrototype Qualification Test M. Herbst

MAJ G. Downs

80-18 Model Memo for Record, Preliminary Airworthiness Feu 1981 CW4 R. WilliamsLR 500D Evaluation (PAE), of Hughes Helicopters (HH) W. Norton

50OMD Modified to a Light Combat R. BuckaninHelicopter (LCH)

80-19 JOH-58(- Report Preliminary Airworthiness Evaluation of Jun 1981 G. YamakawaLR JOH-58C Modified to a Light Combat CPT A. Marshall

Helicopter with a M197 20MM Gun MAJ R. Carpenter

80-20 AH-IS Letter Report AH-IS Vibration Evaluation Mar 1981 CW3 J. WebreLR MAJ B. Picasso

G. BenderG. Yamakawa

83-21 OH-58C Preliminary Airworthiness Evaluation of OH-58C May 1981 MAJ J. BensonLR Expanded Gross Weight and Lateral CG Envelope G. Yamakawa

1981

81-01-1 UH-IH Fuel Conservation Evaluation of USA Helicopter Jan 1982 MAJ G. DownsPart I, UH-IH Flight Operation ImprovementAnalysis

36

1981(continued)

Project Aircraft Ad


81-01-3 UH-IH Fuel Conservation Evaluation of USA Helicopter Aug 1982 CPT F. StellarPart 3, UH-IH Flight Testing MAJ D. Underwood

F. Dominick

81-01-4 OH-58C Fuel Conservation of USA Helicopaters, Part 4 Aug 1982 MAJ M. StrattonOH-58C Flight Testing D. Belte

81-01-5 AH-IS Fuel Conservation Evaluation of USA Helicopter Jan 1983 MAJ L. ToddPart 5, AH-IS Flight Testing CPT R. Savage

CPT R. Vincent

CW4 R. WilliamsM. Herbst

81-01-6 Fuel Conservation Evaluation of US Army Jul 1986 F. Dominick

Part 6, Performance Calculator Evaluation MAJ R. Lockwood

81-04 OH-6A Airworthiness and Flight Characteristics Test of Nov 1983 CW3 J. Webre A161 255OH-6A Configured to a Light Combat Helicopter CPT E. Mitchell

(JOH-6A LCH) R. Woratschek

R. Adler

81-05 OH-58C Report OH-58C Wire Strike Protection System Jul 1981 LTC R. WardLR (WSPS) Lower Cutter Ground Contact MAJ J. Benson

Investigation

81-06-1 OV-1 Preliminary Airworthiness Evaluation of a Jul 1984 MAJ D. UnderwoodNational Aeronautics and Space Administration R. Adler

Automated Stall Warning Sytem for an OV-1Aircraft

81-06-2 OV-1D Maximum Performance Takeoff and Landing Oct 1984 G. Bender

Capabilities for OV-ID

81-07 OH-58C Airworthiness and Flight Characteristics of an Oct 1981 MAJ A. Marshall A 112 581

OH-58C Configured to a Light Combat LTC R. Ward

Helicopter (LCH) R. Woratschek

81-08 RU-21H Report Preliminary Airworthiness Evaluation of Oct 1981 MAJ M.rianks

LR theRU-21H Guardrail V Single Engine Climb MAJ D. Underwood

Performance and Static VMC Performance CW3 J. WebreG. Yamakawa

81-09 JOH-8A Preliminary Airworthienss Evaluation of JOH-8A Sep 81 MAJ A. MarshallClassified

81-10 JOH-58A Report Preliminary Airworthiness Evaluation Sep 1981 MAJ M. Stratton

LR of JOH-58A with Composite Tail Boom J. Niemann

81-11 JUH-IH JUH-IH Pneumatic Boot Deicing System Flight May 1983 MAJ R. Oliver A140 986Test Evaluation R. Woratschek

CPT L. Haworth

81-12 Aerial Preliminary Airworthiness Evaluation System Jun 82 MAJ D. Underwood B073 .2iS

Platform Platform If Individual Lift Device (ILD) J. Nagata

37

1981(continued)


81-13 Model Letter of Effort for Support of Bell Helicopter Apr 82 LTC R. WArdLOE 214 Textron, Icing Certification of the 214ST

Helicopter

81-14 OH-58C OH-58C with Installed Mast Mounted Sight Aug 82 MAJ M. StrattonLR (MMS) Masking and Unmasking Time Line J. Ottomeyer

Analysis Evaluation

81-15 S-76 Letter of Effort for Support of United Techologies Apr 82 LTC R. WardLOE Corp., Sikorsky Aircraft Division, Icing Certifi-

Cation Effort of the S-76 Helicopter

81-16 UH-60A UH-60A Expanded Gross Weight and Center Aug 1985 R. Buckaninof Gravity Evaluation M. Herbst

MAJ R. MacMullinCW4 J . MiessG. SkinnerMAJ E. TavaresCW4 R. Williams

81-17 OV-! OV-1 Propeller Reverser Fault Protection Jun 1982 MAJ D. UnderwoodCircuit Evaluation G. Bender

81-18 UH-60A UH-60A Light Icing Envelopes Evaluation with Jun 82 R. Robbins A125 630Deicing Kit Installed but Inoperative

81-19 EH-1X EH-IX Qualitative Flight Evaluation Dec 1981 CW4 R. WilliamsLR G. Yamakawa

81-20 UH-60A Report, UH-60A Engine and APU Exhaust Gas Dec 1981I.R Temperature Survey

81-21 OV-ID Limited Artificial and Natural Icing Test of Aug 82 MAJ R. Carpenter A127 191OV-1D (Re-Evaluation) LTC. R. Ward

R. Robbins

81-22 AH-IS Preliminary Airworthiness Evaluation of Kamen Apr 1982 MAJ G. DownsLR K747 Tip Weight Retention System CPT W. Clay

81-89 OH-58C Preliminary Airworthiess Evaluation of the Apr 1982 MAJ A. MarshallOH-58C with Prototpye AN/AVR-2 Detection G. BenderSystem Installation

81-90 US Army Aviation Engineering Flight Activity Jun 1982 K. Ferrell A129 859(USAAEFA) Report Bibliography I. Tucker

81-90-1 US Army Aviation Engineering Flight Activity Mar 1984 K. Ferrell A129 859(USAAEFA) Report Bibliography Update i. Tucker1981-1982

81-90-IA US Army Aviation Engineering Flight Activity Junj 1984 K. Ferrell A129 859(USAAEFA) Author Report Bibliography I. Tucker

38

1982


82-01 AH-IS Airworthiness and Flight Characteristics of Aug 82 CW3 J. WebreAH-IS with Aircraft General Purpose Dispenser J. OttomeyerSystem (AGPDS)

82-02 OH-58C Preliminary Airworthiness Evaluation of the Apr 82 MAJ R. MarshallLR OH-58C with Prototpye AN/ANR-2 Laser G. Bender

Detection System Installation

82-03 UH-60A Letter of Effort for Support of the UH-60A/C-130 May 82 MAJ A. MarshallLOE Air Refueling Proximity Test

82-04 AH-IS Letter Report, Preliminary Airworthiness Eval- Jul 82 CW3 P. SullivanLR uation of AH-IS Configured with Helicopter G. Bender

Wire Strike Protection System

82-05-1 CH-47C Helicopter Icing Spray System (HISS) Boom Aug 82 R. WoratschekLR Structural Dynamics Evaluation with Fiberglass MAJ M. Hanks

Blades

82-05-2 Report, Helicopter Icing Spray System (HISS) Oct 85 D. BelteLR Evaluation and Improvements

82-05-3 JCH-47C Helicopter Icing Spray System (HISS) Evaluation Apr 86 D. BelteHISS and Improvements R. Woratschek

82-06 AH-1 AH-I Ground Engagement Simulation/AIr Sep 82 CPT R. Savage 122 623Defense (AGES/ADES) Pod Jettison Evaluation

82-07 CH-47D Airworthiness and Flight Characteristics Test Feb 84 G. Bender(A&FC) of the CH-47D Helicopter G. Yamakawa

M. HerbstR. RobbinsCW3 P. SullivanCW4 R. Williams

82-09 UH-60A Preliminary Airworthiness Evaluation of UH-60A Apr 83 CPT R. MacMulli A148 676with an Improved Airspeed System G. Skinner

MAJ M. Hanks

82-11 UH-60A Preliminary Airworthiness Evaluation of UH-60A Oct 82 CPT R. OliverLR Pilot and Copilot Cockpit Doors Removed CPT A. Marshall

82-12 UH-IH Evaluation of UH-IH Hover Performance Aug 83 D. Belte A141 252Degradation Caused by Rotor Icing CW4 R. Williams

CPT F. StellarW. Abbott

82-13 EH-IX/ Airworthiness and Flight Characteristics of the Jan 84 LTC G. Downs A144 881EH-IH EH-IX/EH-IH Helicopter Configuration CPT J. Kimberly

CPT R. SavageCW4 J. AdklnsJ. NagataJ. Linehan

39

1982(continued)


82-14 UH-60 Preliminary Airworthiness Evaluation UH-60 Mar 83 MAJ A. Marshall A132 964with External Stores Support System (ESSS) MAJ R. Olier

R. BuckaninR. Adler

82-15 UH-60A Airworthiness and Flight Characteristics Test of Dec 83 MAJ A. Marshallthe Prototype External Stores Support System (ESSS) MAJ R. Oliver

J. NagataC. Cassil

82-15-1 UH-60A UH-60A External Stores Support System Fixed May 84 CW4 R. Williams A147 188Provision Fairings Drag Determination CPT R. MacMullin

CW4 J. MlessR. BuckaninG. SkinnerW. Abbott

82-17 YEH-60B Preliminary Airworthiness Evaluation YEH-60B Feb 83 CW3 J. WebreLR with AN/ASN-132 Integrated Inertial Navigation J. Nagata

System Installed MAJ J. Benson

82-18 LONG-EZ Preliminary Airworthiness Evaluation of the Jun 83 MAJ D. Underwood A140 765Rutan Factory (RAF) Inc., LONG-EZ Airplane LTC R. Ward

M. GrahamV. Diekmann

82-19 YEH-60A Letter of Effort, Transmittal of Selected Vibra- Aug 84 G. SkinnerLOE tion Data of the YEH-60A Quick Fix System MAJ E. Tavares

CW4 R. WilliamsCPT G. Bishop

82-86 UH-I Main Rotor lade Container Program Investigation Oct 82 CPR R. Savage

1983

83-03 OH-58 Report, OH-58 Vertical Fin Blockage Oct 83 MAJ A. MarshallLR Evaluation LTC R. Carpenter

MAJ M. Hanks

MAJ J. BensonJ. NagataCPT R. SavageCPT F. StellarM. GrahamMAJ L. ToddR. Adler

40

1983(continued)


83-02 UH-60A Test Witness Report, UH-60A ESSS External Apr 83 MAJ G. DownsTWR Stores Separation Flight Test

83-04 CH-47D Preliminary Airworthiness Evaluation, CH-47D May 83 CPT R. Williamsat 54,000 Pounds Gross Weight CW3 P. Sullivan

R. RobbinsG. YamakawaM. HerbstG. Bender

83-05 JOH-6A Airworthiness and Flight Characteristics of the Nov 83 CW3 J. WebreJOH-6A Light combat Helicopter Configured CPT E. Mitchellwith a Wire Strike Protection System R. Woratschek

R. Adler

83-07 MH-6E MH-6E Extended Pilot Tube Modification May 83 MAJ R. OliverCalibration and Evaluation MAJ L. Todd

MAJ A. Marshall

83-08 OH-eA Letter of Effort, Government Pilot Evaluation Jun 83 MAJ R. OliverLOE OH-6A/NOTAR D. Belte

83-09 UH-60A Test Witness Report, UH-60A ESSS, M-56 May 83 W. AbbottTWR Helicopter Mine Dispensing Subsystem Flight

Test

83-10 UH-60 Test Witness Report, UH-60A ESSS, M-56 May 83 CPT F. StellarTWR Helicopter Mine Dispensing Subsystem Flight

Test

83-10-1 UH-60A Test Witness Report ESSS, External Stores Jun 3 MAJ A. MarshallTWR Separation Flight Test

83-13 JUH-IH JUH-IH Redesigned Pneumatic Boot Deicing Aug 87 M. GrahamCPT L. HaworthCPT J. Kimberly

83-14 AH-IS Report, Airworthiness and Flight Characteristics Apr 84 CW4 R. WilliamsLR Test of AH-IS (Modernized Cobra) with Skid G. Bender

Cross-Tube Fairings Removed

83-12 Government Pilot Evaluation of the BHTI 206/ Jan 85 J. NagataRinig Fin Tail Rotor CW4 J. Adkins

83-15 OH-58C Preliminary Airworthiness Evaluation of the Oct 83 MAJ M. HanksOH-58C with 3-Axis Stability Control MAJ L. ToddAugmentation System and Improved Tall J. NagataRotor System M. Graham

83-16 Rally Preliminary Airworthiness Evaluation Inc., Aug 83 J. JohnsonUltralight Rally 3 and Rally Sport Ultralight Aircraft MAJ G. Downs

83-17 UH-60 Preliminary Airworthiness Evaluation of the Aug 83 CW3 J. MlessUH-60 Hellopter with T700-GE-701A Engines CPT L. HaworthInstalled

41

1983(continued)


83-18 LONG-EZ Report, Preliminary Airworthiness Evaluation of Dec 83 MAJ D. UnderwoodLR Rutan Aircraft Factory Inc., LONG-EZ Airplane V. Diekmann

(S/N 1241)

83-19 OH-58C Report, OH-58C Oil Cooling System Evaluation Apr 84 MAJ A. MarshallLR C. Cassil

83-20 Limited Airworthiness and Flight Characteristics Oct 84 G. Skinner(A&FC) Test of the Quick Fix Configuration MAJ E. Tavares

CW4 R. MurrellCPT G. Bishop

83-21 YEH-60A Artificial and Natural Icing Tests YEH-60A Jun 84 MAJ E. TavaresQuick Fix Helicopter CW3 P. Sullivan

MAJ M. HanksR. Woratschek

83-22 UH-60A Limited Artificial and Natural Icing Tests of the Jun 84 MAI M. HanksExternal Stores Support System (ESSS) Installed R. Woratschekon a UH-60A Aircraft

83-23 UH-1H Evaluation of the UH-IH Level Flight Perform- Jul 84 W. Abbottance Degradation Caused by Rotor Icing J. Linehan

CPT R. LockwoodMAJ L. Todd

83-24 UH-60A Airworthiness and Flight Characteristics Test of Jun 85 MAJ A. Marshall A180 18182-23748 A Sixth Year Production UH-60A MAJ R. MacMullin

MAJ R. LockwoodMAJ T. ReynoldsMAJ E. TavaresR. BuckaninG. SkinnerM. HerbstC. CassilCW4 P. SullivanCW4 R. Williams

83-26 OH-58D Preliminary Airworthiness Evaluation (PAE) of Dec 84 G. Bender A178 740the OH-58D Helicopter (AHIP) CPT J. Kimberly

MAJ E. MitchellMAJ G. Sharon

83-27 OH-58D Interim Report, Airworthiness and Flight Oct 84 J. NagataLR Characteristics (A&FC) of the OH-58D MA F. Stellar

Helicopter MAJ G. BishopCPT L. CaytonCPT T. Walsh

83-29 CH-53 Letter of Effort for Support of Marine CH-53 Apr 84 LTC R. WardLOE Icing Test

83-30 OH-58C Report, Pilot-Static System Evaluation of Dec 83 C. CassilLR OH-58C with Air-to-Ground Engagement System MAJ A. Marshall

(AGES) Installed

42

1984


84-02 RC-12D Airworthiness and Flight Characteristics of the Jul 84 G. Yamakawa A148 046RC-12D Guardrail V CW4 J. Webre

MAJ R. RatcliffR. Adler

84-03 NASA-Ames Letter of Effort, Test Pilot Support for Scout/ Mar 84 MAJ A. MarshallLOE VMS Attack Helicopter Simulation Study Simulator

84-04 LONG-EZ Preliminary Airworthiness Evaluation of the May 84 MAJ D. UnderwoodRutan Aircraft Factory (RAF) Inc., LONG-EZ 0. YamakawaAirplane with External Sight CPT T. Reynolds

CPT W. Carmona

84-05 MH-6E Report, Preliminary Airworthiness Evaluation Sep 84 CW4 J. WebreLR Test of MH-6E with Light Weight Airborne MAJ R. Olivere

FLIR System (LAFS) Installed R. WoratschekR. Adler

84-06 CH-47D Report, Preliminary Airworthiness Evaluation Aug 84 CW4 P. SullivanLR Test of the CH-47D with Light Weight Airborne R. Woratschek

Forward Looking Infrared (FLIR) System (LAFS) R. RobbinsInstalled

84-07 UH-60 Report, Preliminary Airworthiness Evaluation of Aug 84 R. RobbinsLR the UH-60A with Light Weight Airborne Forward R. Woratschek

Looking Infrared (FLIR) System (LAPS) Installed CPT T. Reynolds

84-08 AH-64A Letter of Effort T-28 High Speed Pace Support Jul 84 J. JohnsonLOE for the AH-64A

84-09 AH-IS(MC) Preliminary Airworthiness Evaluation of AH-IS Jul 84 MAJ J. Voss A148 091(MC) Helicopter with Exteral Fuel Tanks CW4 R. WilliamsInstalled J. Nagata

84-10 AH-64A First Article Preproduclion Tests of the AH-64A Nov 84 G. BenderHelicopter MAJ J. Voss

MAJ R. MacMullinCW4 J. Adktns

84-11 AH-IS Preliminary Airworthiness Evaluation of the Oct 84 MAJ R. MacMullin A160 862AH-IS (Modernized Cobra) with the Hellfire. MAJ J. LawrenceTOW, and Stinger Missiles Installed LTC G. Downs

MAJ L. Todd

MAJ E. TavaresCPT W. Carmona

84-13 OV-1D Evaluation of the OV-ID Stall Warning Jan 86 J. LinehanCharacteristics R. Robbins

G. Yamakawa

43

1984(continued)


84-14 UH-IH Preliminary Airwothiness Evaluation of the Jan 85 CW4 J. Adkins A179 498UH-IH HIND-D Surrogate CPT M. White

D. MacphersonCPT D. CrippsMAJ W. Grogan

84-16 AH-1F AH-IF Instrument Meteorological Conditions Feb 87 MAJ J. Lawrence(IMC) Flight Evaluations MAJ J. Martin

MAJ A. OmlieCW4 P. SullivanMAJ T. ReiningerR. Adler

84-16-1 AH-IS(MC) AH-IS(MC) Degraded Hydraulic Modt Jan 86 R. Adler A178 764Evaluation CW4 P. Sullivan

CPT A. Omlie

84-16-2 AH-IS(MC) Preliminary Reort, AH-IS(MC) Roll SCAS Jan 86 CPT A. OmlieLR Card Evaluation

84-16-2 AII-IS(MC) Letter Report, AH-IS (MC) Roll SCAS Card Apr 86 R. AdlerLR Evaluation CPT A. Omlie

CW4 P. SullivanW. Kelly

84-17 UH-60A Report, Infrared Measurement Test of the Sep 84 MAJ E. TavaresLR UH-60A Helicopter with Garret AiResearch

Infrared Suppressor System Installed

84-20 SH-60B Letter of Effort for Support of Navy SH-60B Feb 85 MAJ E. TavaresLOE Icing Test

84-21 AH-IS Letter of Effort, Al--IS Air-to-Air Combat Jan 85 CP4 P. SullivanLOE Test (AACT) III Fvaluation MA G. Sharon

W. AbbottMAJ J. LawrenceR. Adler

84-22 BK-I 17 Preliminary Airworthiness Evaluation of the Nov 85 MAJ G. Sharon B105 .302)1MBB BK-117 Helicopter (Germany/Japan) MAJ E. Tavares

W. AbbottR. Adler

84-23 AH-64A Report, Artificial & Natural Icing Tests of the Sep 85 CW4 J. AdkinsLR AH-64 R. Woratschek

84-23 AH-64A Report, Artificial & Nataural Icing Tests of the Jul 86 CW4 AdkinsLR Phase II AH-64A (Phase I1) R. Woratschek

84-23 AH-64 Artificial and Natural Icing Tests of AH-64 Mar 87 CW4 J. Adkins A188 231Phase II (Phase II) R. Woratschek

84-24 AH-IS Letter of Effort, Firing Evaluation of the All-IS Jan 85 MAJ R. RatcliffLOE (MC) with the HELLFIRE, TOW, & Stinger CW4 R. Murrell

Missile Configuration

44

1984(continued)


84-24-1 AH-IS(MC) Report, Evaluation of the AH-IS(MC) May 85 CW4 R, MurrellLR Helicopter, TOW Helicopter/Stinger Head-Up CPT A. Omlie

Display

84-25 UH-IH Preliminary Airworthiness Evaluation of the Jun 86 C. Cassil A182 369UH-IH Helicopter with the T53-L-703 Engine MAJ R. LockwoodInstalled

84-28 UH-60A. Flight Evaluation of the UH-60A Helicopter Sep 86 CW4 R. Murrell A183 954with the Pitch Bias Actuator Centered and MAJ R. LockwoodElectrically Disconnected CW4 R. Williams

M. HerbstG. SkinnerCPT D. Cripps

84-29 OH-58C Report, Pitot-Static System Evaluation of the Dec 83 MAI A. MarshallLR OH-58C with Air-to-Ground Engagement System C. Cassil

(AGES) Installed

84-30 Letter of Effort, Evaluation of the MCT Jul 86 K. FerrellLOE ROTORTUNER

84-31 UH-IH Report, Evaluation of the UH-IH with the Hub Sep 85 J. JohnsonLR Spring Improvement CW4 R. Murrell

84-33 UH-1H Combined Preliminary Airworthiness Evaluation Jul 88 G. Skinner A202 316and Airworthiness Flight Caracteristics Evaluation J. Piotrowskiof the UH-IH with Preproduction Hub Spring CPT M. Whiteand Composite Main Rotor Blades Installed MAJ A. Omlie

MAJ J. Brown

84-34 OH-58C Flight Test Evaluation of the OH-58C Main Feb 86 M. GrahamRotor Blade Erosion Tape MAJ J. Martin

MAJ F. StellarR. Woratschek

84-35 JOH-58C Letter of Effort, Transmittal of the Results of Jan 85 MAJ E. MitchellLOE the Qualitative Evaluation for the JOH-58C

Helicopter

84-90 U.S. Army Aviation Engineering Flight Activity Jan 85 1. Tucker(USAAEFA) Report Bibliography 1983-1984 M.A. Lake

K. Ferrell

45

1985


85-02 UH-60A Test Witness Report, Continuation of UH-60A Apr 85 MAJ T. ReynoldsTWR ESSS, Externai Stores Separation Test

85-03 JOH-58C Airworthiness and Flight Characteistics of the Feb 86 CW4 J. Webre A180 259JOH-58C (OH-58X Surrogate) Helicopter MAJ F. Stellar

MAJ J. MartinR. WoratschekM. Graham

85-07 UH-60A Flight Characteristics Test of the UH-60A Oct 86 MAJ R. Lockwood A180 791with Tail Boom Mounted Strake W. Kelly

MAJ R. Cason

85-08 AH-64A Engine/Airframe Response Evaluation of the Jun 84 CW4 J. AdkinsAH-64A Helicopter G. Bender

MAJ J. Correia

A 5-09 CH-47D Aerial Refueling Evaluation of the CH-47D Aug 85 M. Herbst A167 575Helicopter R. Robbins

CW4 P. Sullivan

85-10 214ST Airworthiness and Flight Characteristics Test of Feb 5 CW4 R. Williams A175 349

BHTI 214ST Helicopter R. BuckaninCPT R. Cason

85-11 AH-IS Report, Evaluation of the AH-IS with the Hub Sep 85 J. JohnsonLR Spring Improvement CW4 R. Murrell

85-14 UH-60A Report, Phase 11 Evaluation of Solar Heating of Dec 86 MAJ R. CasonLR UH-60A Fusleage Skin (High Temperature W. Kelly

Testing) MAJ R. Lockwood

85-15 Rotor System Evaluation, Phase I Mar 88 R. BuckaninW. GouldMAJ P. LosierCPT D. DowneyMAJ R. LockwoodCW4 J. WebreCOL J. HagenMAJ R. CasonC. Young

85-16 OV-1D Evaluation of the Safe Flight Instrument Feb 86 J. Linehan A177 364Corporation Stall Warning System for the OV- ID CW4 J. MiessAircraft R. Robbins

85-17 OV-ID Evaluation of the OV-ID Aircraft with the Jun 86 CW4 J. MiessPhase I OV-ID Aircraft with the Yt53-L-704 Engines G. Yamakawa

and Rudder Augmentalon System, Phase I

85-17 OV-ID Evaluation of the OV-1D Aircraft with the Nov 86 CW4 J. MiessPhase II OV-1D Aircraft with the YtS3-L-704 Engines G. Yamakawa

and Rudder Augmentalon System, Phase !I J. iUnehanJ. Piotrowski

46

1985(continued)


85-17-1 OV-I Flaps-Up Takeoff Performance of the OV-ID May 87 CW4 J. Miess A 185 960Aircraft with YT53-L-701 Engine Installed G. Yamakawa

J. LinehanR. Robbins

85-18 AH-64A Engine/Airframe Response Evaluation of the Nov 85 CW4 J. AdkinsAH-64A Helicopter G. Bender

MAJ J. Correia

85-19 Letter of Effort, Advanced Digital-Optical Dec 85 CW4 R. WilliamsLOE Control System (ADOCS) Single Pilot Simulator CW4 J. Webre

85-20 SH-60B Letter of Effort for Support of Navy SH-60B May 86 MAJ T. ReynoldsLOE Test

85-21 UH-60A Test Witness Report, UH-60A H ELLFIRE Jan 86 MAJ T. ReynoldsTWR Jettison Test

85-22 Report, Evaluation of the Light Helicopter Jan 86 J. NagataLR Family (LHX) Specification Demonstration MAJ R. Lockwood

Maneuvers CPT G. BishopCW4 R. WilliamsCW4 R. MurrellW. KellyT. Griffen

85-24 UH-1H Report, Structural Flight Loads Correlation of Jan 87 M. Grahamthe Structural Integrity Recording System (SIRS) W. Abbotton the UH-IH Helicopter MAJ R. Simmons

CW4 Adkins

85-25 Letter of Effot, Test Pilot Support for NASA Mar 86 MAJ G. SharonLOE Ames Simulation for LHX Type Handling MAJ F. Stellar

1986

86-01 UH-60A Level Flight Performance Evaluation of the Sep 86 R. BuckaninUH-60A Helicopter with the Production External W. KellyStores Support Sysatem and Ferry Tanks Installed CW4 J. Webare

MAJ T. ReynoldsMAJ R. LockwoodCPT R. Cason

86-02 HH-60A Engine/Airframe Response Evaluation of the Oct 86 G. Bender A184 443HH-60A Helicoplaer Equipped with the CW4 J. AdkinsT700-GE-701 Transient Droop Improvement MAJ R. LockwoodElectronic Control Unit

47

1986(continued)

Project Aircraft AdNumber Type Report Title Date Author(*) Nuniber

86-03 UH-IH Letter of Effort, UH-IH Composite Main Rotor May 86 CPT A. OmlieLOE Blades Rain Errosion Pattern

86-04 Letter of Effort, Test Pilot Support for NASA- Jul 86 CW4 J. WebreLOE Ames Single-Pilot Advancaed Cockpit Engineering MAJ T. Reynolds

Simulation (SPACES) Evaluation LTC D. UnderwoodCPT R. Cason

86-05 UH-60A Preliminary Airworthiness Evalautin of the Aug 87 G. BenderUH-60A with Advanced Digital Optical Control R. RobbinsSystem (ADOCS)

86-06 AH-IS Airworthiness and Flight Characteristics Test Aug 86 CW4 P. Sullivan B114 673of the AH-1S with Hub Spring Installed CW4 J. Lyle

MAJ A. OmlieR. Adler

86-08 Bell Report, Technology Flight Evalaution of the CAE Aug 86 R. RobbinsLR 205A Electronic Ltd., Hand Controller on a Bell 205A MAJ F. Stellar

Helicopter

86-10 UIi-60A Preliminary Airworthiness Evaluation of the Aug 87 MAJ T. Reynolds A 190 t(,4UH-60A Equipped with the XM-139 VOLCANO J. NagataMine Dispensing System MAJ R. Cason

D. Belte

86-14 UH-60A Airworthiness and Flight Characteristics Test of Aug 87 MAJ R. Cason A191 414a Ski Assembly for the UH-60A Black Hawk J. Nagat-.Helicopter MAJ T. Reynolds

D. Belte

86-15 SA 2-37A Report, Flight Evaluation of the Schweizer Aug 86 MAJ R. SimmonsLR SA 2-37A Airplane with Wing Leading Edge Cuffs

86-18 CH-47D Interim Report, Aerial Refueling Evaluation Jan 87 R. RobbinsLR of the CH-47D Helicipter, Phase II

86-18 CH-47D Aerial Refueling Evaluation of the CH-47D Jan 87 R. RobbinsHelicopter, Phase 11 MAJ R. Cason

MAJ T. Reininger

86-19 UH-60A Test Witness Report, UH-60A VOLCANO Jan 87 MAJ T. ReynoldsJettison Test

86-20 UH-i Preliminary Airworthiness Evaluation of a UH-I Feb 87 MAJ F. Stellar A 186 274Equipped with a Terrain Mapping Receier MAJ J. BrownAntenna C. Butler

86-25 UH-60A Preliminary Airwothiness Evaluation of the Oct 87 D. BelteUH-60/ESSS with HELLFIRE Launcher Installed CPT T. Walsh

MAJ T. ReynoldsMAJ P. LosierMAJ R. Cason

48

1987

Project Aircraft AdNumber Type Report Title Date Author(s) Ntinibvr

87-01 TG-8A Preliminary Airworthiness Evaluation of the Oct 87 MAJ R. Simmons B120 244TG-8A Airplane MAJ T. Reininger

87-03 Letter of Effort, Aviation Engineering Flight Jul 87 CW4 J. LyleLOE Activity Participation in Air-to-Air Combat

Test IV (AACT IV)

87-06 EH-60A Report, Preliminary Airworthiness Evaluation Apr 87 CW4 R. Murrellof the EH-60A CW4 J. Webre

M. Herbst

87-08 JUH-IH Letter of Effort, Loads Survey of a JUH-1H Jan 88 G. BenderLOE Helicopter with the Modified Second-Generation M. Herbst

Pneumatic Boot Deicing System

87-09 EH-60A Report, Preliminary Airworthiness Evaluation of Sep 87LR the EH-60A Aircraft in a Low Drag Configuration

87-10 Report, Technology Flight Evaluation of the Jun 87 CPT D. DowneyLR NOTAR Anti-Torque System COL A. Todd

Mr. C. Cassil

87-11 RC-12H Preliminary Airworthiness Evaluation of the Jun 88 CW4 J. MiessRC-12H Airplane CW4 R. Murrell

R. Buckanin

87-16 EH-60 Report, Preliminary Airworthienss Evaluation of Oct 87 CW4 J. WebreLR DELTA the EH-60 DELTA CPT D. Downey

F. Dominick

87-23 UH-60A Report, Evaluation of the UH-60A Cyclic Sep 87 CW4 R. MurrellLR Stabilator Slew Switch

87-23 EH-60A Report, EH-60A Stabilator Evaluation, Adjunct Apr 88 CPT D. CrippsLR to AEFA Proj. No. 84-23

87-25 OV-1D Evaluation of the Improved OV-lD Anti-Icing Apr 88 CW4 J. MiessSystem M. Blacker

J. Plotrowski

87-28 Letter of Effort for Joint NASA-Lewis/U.S. 18 Aug 88 R. RobbinsLOE Army Aviation Engineering Flight Activity Icing D. Belte

Flight Research

87-29 01-58D Report, Preliminary Airworthiness Evaluation Jan 88 MAJ F. StellarLR (PAE) of an Increased Gross Weight External G. Bender

Stores Configuration for the OH-58D Helicopter

87-33 Bell 222 Report, Technology Flight Evaluation of the Apr 88 MAJ J. LawrenceLR Helicopter Bell Helicopter Textron Inc. (BHTI)/Lucas MAJ W. Carmona

Aerospace Adaptive Fuel Control on a Bell 222 R. BuckaninHelicopter R. Woratschek

49

1987(continued)


87-34 0-2A Report, Preliminary Airworthiness Evaluation of Mar 88 CW4 J. MiessLR the 0-2A Aircraft Eq6 oped with the AMIDARS J. Piotrowski

System

1988

88-07 Letter of Effort, Support to the US Naval Air Jun 88 MAJ T. WallaceLOE T-st Center Evaluation of an Acoustic Air Data

Sensor Device (Mini-SODAR)

88-09 Letter of Effort, Support to the Naval Weapons Jun 88 MAJ T. Wallace

LOE Test Center (NWC)

88-11 CH-47D Report, C H-47D Emergency Descent Evaluation Sep 88 MAJ R. Cason

LR CW4 P. SullivanR. RobbinsJ. Piotrowski

88-12 Letter of Effort Pilot Support of Adaptive Fuel Aug 88 MAJ J. LawrenceLOE Control Development Flight Tests R. Buckanin

88-12 Report, Pilot Support of Adaptive Fuel Control Sep 88 MAJ J. LawrenceLR Development Flight Tests R. Buckanin

88-18 Letter of Effort, Support to the USAF Space Nov 88 CPT M. WhiteLOE Fest Office, Military Man in Space (MMIS) MAJ T. Wallace

Equipment and Procedures Evaluation

50

BEECH AIRCRAFT CORPORATION

Alircraft Project AdType Number Report Title Date Author(s) Number

T-34B 63-38 Evaluation of the U.S. Forest Service T-34B Sep 1963 J. Kidwell 951 583Airplane with Smoke Generator Installed

T-42A 74-25 T-42A Single-Engine Operation and Stall Feb 1974 MAJ W. HortonLR Evaluation SP4 P. Bonin

U-8 70-32 Letter Report, U-8 Aircraft Procedures Dec 1970 K. FerrellLR Evaluation

RU-8D 68-51 Letter Report Airworthiness Qualification Test Jul 1969 CW4 W. Connor 857 693LR RU-8D Airplane (Winebottle Configuration)

RU-8D 68-51 Airworthiness and Flight Qualification Tests Oct 1970 LTC J. Wing 876 954RU-8D Airplane Winebottle Configuration, S. DorrisPhase II LTC D. Boyle

CW4 W. Connor

U-21A 66-14 Engineering Flight Test U-21A Airplane Oct 1969 MAJ A. Darling 951 584Phase B and Limited Phase D MAJ W. Welter

U-21A 75-10 Airworthiness and Qualification Evaluation Jan 1976 R. Smith A047 656U-21A Airplane with Low Reflective Paint CPT W. Nortonand Hot Metal Suppressors

U-21A 77-05 Icing Evaluation U-21A Airplane with Low May 1977 T. Benson A046 852Reflective Paint R. Woratschek

MAJ C. ThomasMAJ R. Stewart

U-21A 77-20 Evaluation of Experimental Radio Meteorological May 1977 MAJ C. MittagMeasurement Package Antenna Installed on aU-21A Wing

RU-21A 69-18 CEFIRM Leader Airworthiness Qualification Dec 1970 LTC J. WingRU-21B LR Test RU-21-ABC AircraftRU-21C

RU-21A 75-03 Flying Qualities Evaluation RU-21A CEFIRM Dec 1974 J. Johnson A109 514LEADER Airplane CPT M. Hawley

MAJ R. Stewart

RU-21B 67-25 Engineering Flight Test, RU-21B and RU-21C Mar 1970 CPT J. Brecker 869 281RU-21C Aircraft Army Preliminary Evaluation LTC G. Swecker

MAJ R. Holt

RU-21B 69-18 CEFIRM Leader Airworthiness Qualification Dec 1970 LTC J. WingRU-21A LR Test RU-21-ABC AircraftRU-21C

RU-21B 71-47 CEFIRM LEADER RU-21B and RU-21C Air- Sep 1972 MAJ R. ChaplinRU-21C LR worthiness Tests SP4 J. Lehman

RU-21C 67-25 Engineering Flight Test, RU-21B and RU-21C Mar 1970 CPT J. Brecker 869 281RU-21B Aircraft Army Preliminary Evaluation LTC 0. Swecker

MAJ R. Holt

51

BEECH AIRCRAFT CORPORATION

Aircraft Project AdType Number Report Title Date Author(s) Number

RU-21C 71-47 CEFIRM LEADER RU-21B and RU-21C Air- Sep 1972 MAJ R. ChaplinRU-21B LR worthiness Tests SP4 J. Lehman

RU-21E 72-13 Modified LEFT-FOOT RU-21E Direction Jun 1972 MAJ R. ChaplinLR Finding (DF) Demonstration PFC G. Smith

RU-21H 74-35 Guardrail IIA RU-21H Evaluation Jul 1974 G. Yamakawa A004 009T. BensonMAJ L. Brewer

RU-21H 77-19 Preliminary Airworthiness Evaluation, RU-21H Mar 1978 J. Niemann A068 347Guard Rail V Aircraft R. Smith

CPT W. NortonMAJ F. Doten

RU-21H 81-08 Report Preliminary Airworthiness Evaluation of Oct 1981 MAJ M. HanksLR the RU-21H Guardrail V Single Engine Climb MAJ D. Underwood

Performance and Static VMC Performance CW3 J. WebreG. Yamakawa

Model 74-21 Army Preliminary Evaluation I Model 200 Jun 1974 T. Benson A009 713200 Cefly Lancer CPT M. Hawley

G. YamakawaMAJ L. Brewer

Model 74-21 Army Preliminary Evaluation II Model 200 Aug 1974 G. Yamakawa A009 714200 Cefly Lancer T. Benson

MAJ L. Brewer

C-12A 75-08 Airworthiness and Flight Characteristics Oct 1976 V. Diekmann A040 239Evaluation C-12A Aircraft R. Smith

J. Watts

MAJ J. HannonCPT W. Norton

C-12A 76-03 Landing GearCapability Tests Mar 1977 V. Diekmann A046 554J. Watts

RC-12D 84-02 Airworthiness and Ilight Characteristics Test of Jul 1984 G. Yamakawa A148 046the RC-12D Guardrail V CW4 J. Mless

MAJ R. RatcliffR. Adler

RC-12H 87-11 Preliminary Airwortiness Evaluation of the Jun 1988 CW4 J. Mless A202 957RC-12H Airplane CW4 R. Murrell

R. Buckanin

52

BELL hIELICOPTER CORPORATION


XV-3 62-01 Pilot Evaluation of the Bell Model XV-3 Feb 1962 MAI E. Kleuver 884 8-0Vertical Take-Off and LandingAircraft

BREGUET AVIATION(France)

Model 63-06 Flying Qualities and Performance Evaluation Jan 1964 CPT M. Antoniou 951 590941 aka of the Breguet 941 Turbo-Prop

63-85 Troop Transport

CANADAIR, LTD(Canada)

CL-215 72-02 Limited Evaluation of Canadair's CL-215 Nov 1970 MAJ R. HolasekLR Water Bomber/Utility Aircraft

CL-215 72-02 Limited Evaluation Canadair CL-215 Oct 1972 MAJ J. Alvis A109 513Amphibious Airplane MAJ R. Holasek

J. Kishi

CESSNA AIRCRAFT COMPANY

L-19A 61-01 Evaluation of L-19A Equipped with Continental Feb 1961 J. Kidwell 722 8250-470-11CI Fuel Injection Engine CPT W. Clay

L-19A 61-06 Evaluation of the Mark XII Auxiliary Fuel and Jul 1961 CPT J. Johnston 884 884H-13G Oil System

0-2A 87-34 Report, Preliminary Airworthiness Evaluation of Mar 1988 CW4 J. MiessLR the 0-2A Aircraft Equipped with the AMIDARS J. Piotrowski

System

53

DeHAVILLAND AIRCRAFT OFCANADA LTD


CV-2B 63-04 Take-Off and Landing Capabilities of the Sep 1963 J. Kidwell 440 406aka Caribou CV-2B Aircraft on Unprepared J. Blaha

63-73 Surfaces, USATECOM Project No. 4-4-1142-01 R. Finnestead

CPT M. Antoniou

CV-2B 63-74 Final Report Performance Tests of the CV-2B Jun 1965 R. Finnestead 467 490Airplane USATECOM Project No. 4-4-114-01 CPT M. Antoniou

CV-2B 63-92 Final Test Report of the Integrated Engineering/ Jul 1964 J. KramerLR Service Test of Low Level Extraction Techniques

(LOLEX) from CV-2B Aircraft, USATECOMProject No. 4-4-7475

YCV-7A 63-13 Engineering Test Requirements for the Nov 1963 J. Blaha 951 587DeHavilland YCV-7A Tactical Troop Transport,USATECOM Project No. 4-3-1170-01

CV-7A 63-14 Letter Report on Preliminary Engineering Flight Oct 1964 J. BlahaLR Evaluation of the CV-7A Tactical Transport

Airplane, DA Project No. 1-R-1-41815-D-193,USATECOM Project No. 4-3-1170-04

CV-7A 65-10 Stability and Control and Performance Test Mar 1966 MAJ N. Mattmuller 483 183(Phase D) of the CV-7A Transport Airplane, D. WilsonUSATECOM Project No. 4-3-1170-08 J. Blaha

U-6 65-07 Final Report of Qualitative Flying Qualities Jun 1965 MAJ E. KleuverLR Evaluation of the Turbine Powered U-6 Airplane,


GRUMMAN AEROSPACECORPORATION

AO-1AF 61-07 Cold Weather Suitability Test of the AO-IAF Nov 1961 A. Ruddell 884 888

OV-I 73-09 NASA OV-1 Accident Investigation Jun 1973 MAJ R. ChaplinLR LTW W. Griffith

OV-1 81-06-1 Preliminary Airworthiness Evaluation of a Jul 1984 MAJ D. UnderwoodNational Aeronautics and Space Administration R. AdlerAutomated Stall Warning System for an OV-1Aircraft

OV-I 81-17 OV-1 Propeller Reversser Fault Protection Circuit Jun 1982 MAJ D. Underwood

Evaluation G. Bender

OV-IB 67-23 Engineering Flight Test of an IR Suppression Jul 1969 SP5 G. Higley 857 774Kit Installation on the OV-IB Aircraft MAJ R. Forsyth

54

GRUMMAN AEROSPACECORPORATION

(continued)


OV-1C 63-20 Final Report of the Airworthiness Certification Jan 1965 J. Blaha 465 079Test of the QRC-160-1 Installed on the OV-1C MAJ J. JohnstonAirplane, USATECOM Project No. 6-3-6711-03

QV-1C 75-15 Advanced Report, Engineering Flight Evaluation. May 1976 CPT G. NeperenyLR OV-IC Aircraft Equipped with Angle-of-Attack/ MAJ R. Stewart

Stall Warning System

OV-IC 78-07 Airworthiness and Flight Characteristics Test May 1979 R. Smith A069 827OV-1C Takeoff Performance J. Watts

J. NiemannMAJ J. GuinG. Yamakawa

OV-lC 78-19 Airworthiness and Flight Characteristics OV-IC Apr 1979 MAJ R. Tarrwith Angle-of-Attack/Stall Warning and Speed G. SkinnerControl System,

OV-IC 80-01 Letter Report OV-1C (Short Wing) Apr 1980 MAJ R. CarpenterLR Fuel Siphoning Evaluation

OV-1D 68-43 Army Preliminary Evaluation Preproduction Mar 1970 G. Yamakawa 870 260OV-ID (Mohawk) LTC W. Graham

LTC T. Wright

OV-ID 70-03 Army Preliminary Evaluation 1H Production Mar 1971 G. Yamakawa 881 649OV-ID (Mohawk), Performance and Handling ILt K. BrauerQualities LTC W. Graham

OV-ID 70-03 Army Preliminary Evaluation II Production Apr 1972 G. Yamakawa 903 107OV-1D (Mohawk) Performance Addendum ILT K. Brauer

LTC W. GrahamMAJ J. Henderson

OV-ID 72-19 OV-ID 300-Gallon External Drop Tank Sep 1972 MAJ R. ChaplinLR Performance Evaluation SP4 J. Lehman

OV-ID 74-20 Hot Brick III Airworthiness Evaluation Nov 1974 D. Macpherson A012 202OV- I D Airplane CW4 J. Reid

OV-ID 76-10 OV-ID Low Reflective Paint Evaluation undated J. WattsLR

OV-ID 77-22 Preliminary Airworthiness Evaluation, OV-1D Feb 1978 MAJ R. Ward A109 522Airplane with AN/ALQ 147 XE-I and XE-2 G. YamakawaSystems Installed MAJ R. Tarr

OV-1D 79-10 Airworthiness and Flight Characteristics Oct 1979 MAJ G. WilsonLR Evaluation OV-1D with Angle-of-Attack/ LTC C. Frankenberger

Stall Warning System CPT F. Bowers

OV-ID 80-16 Letter Report Limited Artificial Icing Tests of Jul 1981 E. GilmoreLR the OV-ID CPT R. Robbins

OV-ID 81-06-2 Maximum Performance Takeoff and Landing Oct 1984 G. BenderCapabilities for OV- ID

55

GRUMMAN AEROSPACE(ORPORATION

(continued)


OV-1D 81-21 Limited Artificial and Natural Icing Test of Aug 1982 MAJ R. Carpenter A127 191OV-ID (Re-Evaluation) LTC R. Ward

R. Robbins

OV-1D 84-13 Evaluation of the OV-1D Stall Warning Jan 1986 J. LinehanCharacteristics R. Robbins

G. Yamakawa

OV-ID 85-17-1 Flaps-Up TAkeoff Performance of the OV-ID May 1987 CW4 J. Miess A185 960Aircraft with YT53-L-701 Engine Installed G. Yamakawa

J. LinehanR. Robbins

OV-ID 85-16 Evaluation of the Safe Flight Instrument Feb 1986 J. Linehan A177 364Corporation Stall wArning System for the OV-1D CW4 J. MiessAircraft R. Robbins

OV-1D 85-17 Evaluation of the OV-ID Aircraft with the Jun 1986 CW4 J. MiessPhase I YT53-L-704 Engine and Rudder Augmentation G. Yamakawa

System, Phase I J. LnehanJ. Piotrowski

OV-ID 87-25 Evaluation of the Improved OV-1D Anti-Icing Apr 1988 CW4 J. MiessSystem M. Blacker

3. Piotrowski

OV-ID 85-17 Evaluation of the OV-ID Aircraft with the Jun 1986 CW4 J. MiessPhase II YT53-L-704 Engine and Rudder Augmentation G. Yamakawa

System, Phase II

RV-1D 74-36 Army Preliminary Evaluation I, RV-ID/ Aug 1974 G. Bender A005 220Quick Look II Aircraft CPT J. O'Connor

TBM-3 62-11 Evaluation of a Grumman TBM-3 Air Tanker Nov 1962 J. Blaha 884 894CWO E. Nelson

TS-2A 71-16 Letter Report, Phase I TS-2A Airtanker Jul 1972 MAJ R. HolasekLR Evaluation SP4 J. Lehman

TS-2A 77-07 TS-2A Air Tanker Evaluation, Phase I! May 1978 J. Watts A060 940E. BailesMAJ S. SpringMAJ J. Guin

LOCKHEED CORPORATION

YO-3A 68-47 Army Preliminary Evaluation I YO-3A Airplane Aug 1970 CPT G. Condon 876 022LTC i. RundgrenMAJ W. Davis

56



YO-3A 69-14 Army Preliminary Evaluation, 1I, YO-3A Aug 1970 CPT G. Condon 874 733Airplane LTC I. Rundgren

CW4 W. Connor

YO-3A 70-09 Army Preliminary Evaluation III YO-3A Sep 1970 LTC 1. Rundgren 876 095Airplane MAI A. Deel

NORTH AMERICAN AVIATION

TB-25N 62-08 Flight Test Evaluation of a TB-25N Aerial Sep 1962 K. JordonTanker MAJ E. Kluever

F-51D 71-30 Flight Evaluation, Aeroflex True Airspeed Mar 1973 K. Ferrell 764 240Vector System Low-Airspeed System, Final A. WinnReport II J. Kishi

B. Jefferis

PILATUS

PC-6/A 63-05 Report of USATECOM Project No. 4-3-1048-01 Sep 1963 L. Schroers 951 586aka Takeoff and Landing Evaluation of the Pilatus CPT J. Johnston63-70 Turbo Porter Model PC-6/A Airplane CWO J. Watts

RYAN AERONAUTICAL CO.

XV-SA 62-35 Letter Report, Preliminary Pilot Qualitative Oct 1965 R. FinnesteadLR Evaluation of the XV-5A Research Aircraft K. Ferrell

XV-SA 62-72/Pt I Engineering Flight Research Evaluation of the Aug 1966 R. Finnestead 800 973XV-SA Lift-Fan Aircraft, Pt 1, Stability and K. FerrellControl MAJ W. Welter

W. Anderson

57

RYAN AERONAUTICAL CO.(continued)


XV-SA 62-72/Pt 2 Engineering Flight Research Evaluation of the Aug 1967 K. Ferrell 821 123XV-5A Lift-Fan Aircraft, Pt H1, Performance MAJ W. Welter

XV-5A 65-47 A Review of AGARD Recommendations for 1965 W. AndersonV/STOL Handling Qualities (Rep. 408) in theLight of U.S. Army Experience with the XV-SAand other V/STOL Aircraft Including Helicopters

ROTEC ENGINEERING, INC.

Rally 83-16 Report, Preliminary Airworthiness Evaluation of Apr 1983 MAJ G. DownsUltralight LR ROTEC Engineering Inc., Rally 3 and Rally

Sport Ultralight Aircraft

RUTAN AIRCRAFT FACTORY,

INC.

LONG-EZ 82-18 Preliminary Airworthiness Evaluation of the Jun 1983 MAJ D. Underwood A140 765Rutan Aircraft Factory (RAF) Inc, LONG-EZ LTC R. WardAirplane M. Graham

V. Diekmann

LONG-EZ 83-18 Report, Preliminary Airworthiness Evaluation Dec 1983 MAJ D. UnderwoodLR of Rutan Aircraft Factory Inc., LONG-EZ V. Diekman

Airplane (S/N 1241)

LONG-EZ 84-04 Preliminary Airworthiness Evaluation of the May 1984 MA D. UnderwoodRutan Aircraft Factory (RAF), Inc., LONG-EZ G. YamakawaAirplane with External Sight CPT T. Reynolds

CPT W. Carmona

SCHWEIZER AIRCRAFTCORPORATION

SA 2-37A 86-15 Report, Flight Evaluation of the Schwelzer Aug 1986 MAJ R. SimmonsLR SA 2-37A Airplane with Wing Leading Edge

Cuffs

TG-8A 87-01 Preliminary Airworthiness Evaluatin of the TG-8A Oct 1987 MAJ R. Simmons ABI20 244Evaluation of the TG-8A Airplane MAJ T. Reininger

58

BELL HELICOPTER TEXTRONINC.


AH-1 82-06 AH-1 Ground Engagement Simulation/Air Sep 1982 CPT R. Savage 122623Defense (AGES/ADES) Pod Jettison Evaluation

AH-IF 84-16 AH-IF Instrument Meteorological Conditions Feb 1987 MAJ J. Lawrence(IMC) Flight Evaluations MAJ J. Martin

MAJ A. OmlieCW4 P. SullivanMAJ T. ReningerR. Adler

AH-IG 66-06 Letter Report of Pilot Qualitative Evaluation of Sep 1966 MAJ G. HallLR Handling Qualities and Cockpit Environment of J. Melton

AH-lG Helicopter After Contractor Optimizationof Stability Augmentation System and Improvementof Cockpit Ventilation System, USATECOMProject No. 4-6-0500-01

AH-1G 66-06 Engineering Flight Test of the AH-IG Jan 1968 J. Melton 830 136Helicopter Hueycobra, Phase B Part 1, MAJ G. HallUSATECOM P;oject No. 4-6-0500-01

AH-IG 66-06 Engineering Flight Test of the AH-IG Helicopter May 1969 J. Melton 855 629Hueycobra, Phase B, Part 2, USATECOM MAJ G. HallProject No. 4-6-0500-01

AH-IG 66-06 Engineering Flight Test of the AH-1G Mar 1968 J. Melton 834 379aka (Hueycobra) Helicopter Equipped with the MAJ G. Hall67-26 XM-28 Chin Turret with Twin XM-134 Miniguns,

Phase B, Part 3

AH-IG 66-06 Engineering Flight Test of AH-IG Hueycobra Mar 1968 J. Melton 836 901aka Helicopter Equipped with XM-28 Chin Turret MAJ G. Hall67-27 with Twin XM-129, 40MM Grenade Launcher,

Phase B, Part 4

AH-IG 66-06 Engineering Flight Test of the AH-IG Helicopter Apr 1968 SP5 P. Passinisi 838 004aka Equipped with the XM-28 Chin Turret with One CW4 W. Connor68-03 7.62MM Automatic Gun (M-134) and One

40MM Grenade Launcher (XM-129) Hybrid,Phase B, Part 5, USATECOM Project No.4-6-0500-01

AH-IG 66-06 Engineering Flight Test AH-lG Helicopter Nov 1969 R. Finnestead 862 700Hueycobra Phase B, Part 6, USATECOM CW4 W. ConnorNo. 4-6-0500-01

AH-IG 66-06 Engineering Flight Test AH-IG Helicopter Dec 1970 R. Finnestead 880 558(Hueycobra) Phase D. Part 1. Handling R. PelikanQualities, USATECOM Project No. 4-6-0500-01 MAJ D. Wray

M. Buss

59

IEI.I. II:I.ICOPTER TEXTRONINC.

(continued)


AH-1G 66-06 Engineering Flight Test AH-IG Helicopter Apr 1970 R. Finnestead 874 210(Hueycobra) Phase D, Part 2 Performance, E. LaingUSATECOM Project No. 4-6-0500-01 CW4 W. Connor

M. Buss

AH-IG 66-06 Engineering Flight Test AH-IG Helicopter Mar 1971 R. Finnestead 882 220(Hueycobra) Phase D Part 2 Performance M. BussAddendum, USATECOM ProjectNo. 4-6-0500-01 CW4 W. Connor

AH-IG 66-06 Engineering Flight Test AH-IG Helicopter, Sep 1970 R. Finnestead 878 122Phase D, Part 3 Vibration Characteristics, E. BailesUSATECOM Project No. 4-6-0500-01 MAJ D. Wray

M. Buss

AH-IG 66-06 Engineering Flight Test of the AH-IG Helicopter Feb 1968 J. Melton 832 419to Determine the Area of Inadequate Directional MAJ G. HallControl Power at 8100 Lb. Gross Weight

AH-1G 66-06 Feasibility Test of Tractor Tail Rotor Mar 1968 MAJ G. Hall 832 820Modification on the AH-1G Helicopter J. Melton

AH-IG 68-09 Letter Report Engineering Flight Test of the Mar 1968 MAJ G. Hall 830 120LR AH-IG Helicopter Equipped with XM-20 S. Dorris

Armament Sutsystcm Autom=atic 20MM Cannon

AH-IG 68-31 Engineering Flight Test AH-IG (Hucycobra) Nov 1969 N. Donaldson 865 018Helicopter Equipped with the XM35 Armament MAJ. G. HallSubsystem (20MM Automatic Gun)

AH-IG 68-37 Army Preliminary Evaluation of the AH-IG Jun 1969 J. Nagata 860 948Tractor Tail Rotor Modification M. Buss

AH-IG 68-55 Flight Evaluation, Compliance Test Techniques Apr 1974 K. Ferrell 109 440for Army Hot Day Hover Criteria A. Frederickson

J. KishiJ. Watts

AH-IG 69-01 Airworthiness and Flight Characteristics AH-IG Dec 1969 G. Bender 864 070Helicopter with Stabilized Night Sight (SNS), Phase I M. Buss

AH-IG 69-01 Airworthiness and Flight Characteristics Test Aug 1970 G. Bender 874 211AH-IG Helicopter with Stabilized Night M. BussSight (SNS), Phase II

AH-1G 69-01 NASA Report Static Load Tests of a Simulation Jul 1969 R. RosecramsPackage on an AH-IG Helicopter

60

BELL . ElICOPTER TEXTRONINC.

(continued)


AH-1G 69-11 Engineering Flight Test AH-IG Helicopter Mar 1971 R. Lewis 882 771(Hueycobra) Maneuvering Limitations E. Bailes

R. McClellanCPT 1. ClaxtonM. BussCW4 W. ConnorLTC J. Johnston

AH-IG 69-13 Height-Velocity Test AH-1G Helicopter Feb 1971 CPT G. Condon 881 633E. BailesCW4 W. Connor

AH-IG 70-08 Letter Report, Qualitative Airworthiness Sep 1970 M. BussLR Assessment of AH-IG Cobra Night Fire Control

System (CONFICS)

AH-IG 70-10 Airworthiness and Flight Characteristics Test Oct 1970 G. Bender 951 594(Limited) AH-IG Helicopter with the M. BussSoutheast Asia Multisensor Armament SystemHelicopter (SMASH)

AH-IG 70-15-5 Vibration and Temperature Survey Production Mar 1974 E. Laing A002 063AH-IG Helicopter CPT A. Weand

AH-IG 70-25 Engineering Flight Test AH-IG (Hueycobra) Apr 1971 CPT B. Nicholson 887 550Helicopter Autorotational Entry Characteristics M. Buss

AH-IG 71-43 AH-IG Lateral Flight Performance Test Jun 1972 MAJ L. HeplerLR J. Kishi

A. Wlnn

AH-IG 72-16 AH-IG Vertical Climb Height-Velocity Sep 1972 K. FerrellLR Diagram A. Frederickson

J. Kishi

AH-IG 72-18 Army Preliminary Evaluation Improved AH-IQ Dec 1972 G. Yamakawa 907 694Cobra Armament System 1LT L. Toman

SPS A. WernerMAJ R. Holasek

AH-IG 72-29 Instrument Flight Evaluation AH-IG Helicopter Jul 1975 G. Skinner A026 633CPT M. LarsenSP4 G. SmithSP4 P. BoninCW4 J. ReidLTC R. WaddellMAJ L. HeplerMAJ R. Merrill

61


(continued)


AH-1G 72-30 Engineering Flight Test AH-IG Helicpter with Jun 1973 G. Skinner 776 359Model 212 Tail Rotor, Part 1, Load Survey SP4 G. Smith


AH-IG 72-30 Engineering Flight Test AH-IG Helicopter with Sep 1973 J. Nagata 776 360Model 212 Tail Rotor, Part II, Performance G. Skinnerand Handling Qualities SP4 G. Smith


AH-IG 73-04-2 Artificial Icing Tests AH-IG Helicopter Nov 1974 R. Smith A009 712CPT M. HanksMAJ C. MittagCW4 J. Reid

AH-1G 74-02 AH-IG Helicopter Main Rotor Flow Survey Apr 1978 B. Boirun A057 443E. BailesR. Jefferis

MAJ J. ArnoldCW3 J. Meiss

AH-IG 74-10 AH-IG Heavyweight Autorotational Jan 1974 MAJ L. HeplerLR Evaluation G. Yamakawa

AH-1G 74-10 Engineering Flight Test AH-IG Helicopter May 1974 G. Yamakawa 785 553Heavyweight Autorotational Evaluation ILT L. Free

J. Watts

MAJ L. Heplcr

AH-IG 74-19 Height-Velocity Test AH-IG Helicopter at Heavy Jun 1974 ILT L. Free A034 424Gross Weight, Low Elevation MAJ L. Hepler

AH-1G 75-01 Performance and Handling Qualities AH-IG Apr 1975 A. Winn A019 482Helicopter Equipped with Three Metal/Plume MAJ R. StewartInfrared Suppressors Hot

AH-IG 75-09 Performance and Handling Qualities Evalution Aug 1975 A. Winn A021 407

AH-IG Helicopter with Low Reflective Infrared/ ILT E. TavaresOptical Paint MAJ R. Stewart

G. Skinner

AH-IG 75-17-1 Flight Evaluation, Pacer Systems, Low-Range May 1977 W. Abbott A045 222Airspeed System, LORAS 1000 B. Boirun

CPT G. HillCPT E. Tavares

AH-IG 75-17-2 Flight Evaluation, J-TEC VT-1003 Vector May 1977 W. Abbott A046 553

Airspeed Sensing System CPT S. SpringMAJ R. Stewart

AH-IG 75-19-1 Low Airspeed Sensor Location Tests AH-IG Feb1977 K. Ferrell A052 467Helicopter B. Boirun

CPT G. Hill

62

BELl. IIEIICOPTER TEXTRONINC.

(continued)


AH-IG 75-19-2 Flight Evaluation Honeywell Ultrasonic Wind Jun 1976 CPT G. Hill A052 467Vector Sensor System Fire Control Wind Sensor CW3 J. MeissReport B. Boirun

AH-IG 75-25 Letter of Effort, Qualitative Evalution of AH-IG Oct 1975LR with Kaiser Ministab

AH-IG 78-02 Preliminary Airworthiness Evaluation, AH-IG Jul 1979 MAI P. Moe A078 340with the Airborne Target Acquisition Fire R. SmithControl System and the Hellfire ModularMissile System Installed

AH-1G 78-10 AH-IG Helicopter, 19-Round Lightweight Mar 1979 G. Skinner A069 828Airborne Launcher Jettison Envelope MAJ F. DotenDetermination

AH-IQ 72-18 Army Preliminary Evaluation Improved AH-IG Dec 1972 G. Yamakawa 907 694Cobra Armament System ILT L. Toman

SPS A. WernerMAJ R. Holasek

AH-1Q 72-43 Airworthiness and Flight Characteristics Jul 1973 G. Yamakawa 914 458Evaluation AH-IQ Helicopter CPT K. Schrantz

ILT M. HanksSP4 A. WernerMAJ R. MerrillCW4 J. Reid

AH-IQ 73-04-? Artiticial Icing Tests AH-lQ Helicopter (U) Jan 1974 CPT M. Hanks 531 589CW4 J. Reid

MAJ R. Merrill

YAH-1Q 75-18 Army Preliminary Evaluation, YAH-1Q Heli- Aug 1975 ILT L. Free A020 Illcopter with a Flat Plate Canopy CPT J. R. Arnold

YAH-IQ 75-18 YAH-IQ Flat Plate Canopy Follow-on Evaluation Feb 1976 CPT J. R. Arnold

YAH-1R 74-33 Army Preliminary Evaluation YAH-IR Improved May 1975 F. Dominick A018 420Cobra Agility and Maneuverability Helicopter R. Smith

MAJ R. Stewart

YAH-IR 74-33 Army Preliminary Evaluation, YAH-IR Improved Aug 1975 F. Dominick A024 850Cobra Agility andManeuverability Helicopter R. SmithAodendum MAJ R. Stewart

YAH-IR 75-21 Letter of Effort, YAH-IR Lateral Agility/IR Mar 1977 MAJ R. StewartLR

YAH-1R 76-07 Army Preliminary Evaluation, Improved Main Jun 1977 J. Watts A072 830Rotor Blade Installed on a YAH-IR Helicopter F. Dominick

MAJ J. Guin

63

BELL IIELICOPTER TEXTRONINC.

(continued)


YAH-IR 76-08 Airworthiness and Flight Characteristics Nov 1977 G. Yamakawa A074 895Evaluation Improved Main Rotor Blade J. NiemannInstalled on a YAH-IR Helicopter R. Smith

R. WoratschekMAJ J. Jenks

CPT W. NortonCW4 J. Tulloch

AH-IS 77-25 Preliminary Airworthiness Evaluation, AH-1S May 1980 G. Bender A089 625Helicopter with Ogee Tip Shape Rotor Blades R. Woratschek

D. OttomeyerH. ArnaizMAJ L. HigginsCW4 J. Tulloch

AH-IS 77-33 Preliminary Airworthiness Evaluation, AH-IS May 1978 G. Bender A067 757Helicopter Equipped with Garrett Infrared E BailesRadiation Suppressor System and AN/ALO-144 LTC C. FrankenbergerJammer MAJ S. Spring

AH-IS 77-35 AH-1S/XM-130 Chaff Dispenser. Preliminary Mar 1978 J. NiemannLR Airworthiness Evaluation CPT T. Burch

AH-1S 77-38 Production Validation Test - Government Oct 1979 V. Diekmann 097 689Kaman K747 Improved Main Rotor Blade MAJ G. Mullen

CW4 J. TullochT. BensonCPT F. BowersR. Woratschek

AH-I S 78-03 Preliminary Airworthiness Evaluation, AH-IS Feb 1979 CPT P. Moe A07I 343Helicopter Installed with Enhanced Cobra R. SmithArmament System (AH-IS/ECAS) CW3 R. Williams

R. Woratschek

AH-IS 78-15 Preliminary Airworthiness Evaluation Production Aug 1978 LTC C. FrankenbergerLR AH-IS Helicopter Equipped with AN/ALQ-136 T. Benson

(XE-2) Countermeasures System

AH- IS 78-16 Preliminary Airworthiness Evaluation Modified Aug 1978 LTC C. FrankenbergerLR AH-IS Helicopter Equipped with AN/ALQ-136 T. Benson

Countermeasures System

AH-IS 79-01 Letter Report, Preliminary Airworthiness Oct 1979 V. DlekmannLR Evaluation of AH-IS with Fixed Wings Removed LTC G. Mullen

AH-IS 79-03 AH-I Lightweight Airborne Launcher MAJ L. Higgins A101 461Jettison Evaluation D. Otuomeyer

AH-IS 79-04 Letter Report of Preliminary Airworthiness Mar 1980 R. WoratschekLR Evaluation of Production AH-IS Helicopter MAJ P. Morris

with 90 degree Gearbox and Skid Cross-TubeFairings Removed

64


(continued)


AH-IS 79-08 AH-IS PRODUCTION Airworthiness and Flight Nov 1980 CW4 J. Tulloch AIOO 94oCharacteristics for Instrument Flight D. Ottomeyer

LTC C. FrankenbergerMAJ B. Picasso

Ali-IS 79-09 Preliminary Airworthiness Evaluation Al-IS Jun 1980 MAJ P. Morris A092 614(Prod) Helicopter with a Substitute Straight LTC C. FrankenbergerExhaust Pipe J. Niemann

R. Woralschek

AH-IS 79-14 Letter Report AH-1S Helicopter Tail Boom Oct 1979 R. NiemannLR 3-Way Temperature Survey MAJ P. Morris

AH-IS 79-16 Letter of Effort and Data Transmittal AH-IS Oct 1979 R. WoratschekLR Main Transmission Top Cover Flange Stress

Measurements Evaluation

AH-1S 80-11 Letter Report Drag Characteristics Evaluation Nov 1980 G. BenderLR of Prototype Hellfire Modular Missile System CW4 J. Tulloch

(HMMS) Launcher

AH-IS 80-11-2 Letter Report Drag Characteristics Evalualion Nov 1980 G. BenderLR of Prototype Hellfire Modular Missile System MAJ B. Picasso

(HMMS) Launcher - Masking/Unmasking D. Ottomeyer

AH-IS 80-20 Letter Report AH-IS Vibration Evaluation Mar 1981 CW3 J. WebreLR MAJ B. Picasso

G. BenderG. Yamakawa

AH-1S 80-11-2 Letter Report, Drag Characteristaics Evaluation Nov 1980 G. BenderLR of Prototype Hellfire Modular Missile System MAJ B. Picasso

(HMMS) Launcher-Masking/Unmasking

AH-IS 81-01-5 Fuel Conservation Evaluation of USA Jan 1983 MAJ L. ToddHelicopters, Part 5, AH-IS Flight Testing CPT R. Savage

CPT R. VincentCW4 R. WilliamsM. Herbst

AH-IS 81-22 Preliminary Airworthiness of Kaman K747 Apr 1982 MAI G. DownsLR Tip Weight Retention System

AH-IS 82-01 Airworthiness and Flight Characteristics of Aug 1982 CW3 J. WebreAH-1S with Aircraft General Purpose Dispenser J. OttomeyerSystem (AGPDS)

AH-IS 82-04 Letter Report, Preliminary Airworthiness Jul 1982 CW3 P. SullivanLR Evaluation of AH-IS Configured with Helicopter G. Bender

Wire Strike Protection System

AH-IS 83-14 Report, Airworthiness and Flight Characteristics Apr 1984 CW4 R. WilliamsLR of AH-IS (Modernized Cobra) with Skid Cross- G. Bender

Tube Fairings Removed

65


(continued)


AH-IS 84-09 Preliminary Airworthiness Evaluation of Jul 1984 MAJ J. Voss A148 091(MC) AH-IS(MC) Helicopter with Exernal Fuel Tanks CW4 R. Williams

Installed J. Nagata

AH-1S 84-11 Preliminary Airworthiness Evaluation of the Oct 1984 MAJ R. MacMullin A160 862AH-IS (Modernized Cobra) with the Hellfire, MAJ J. LawrenceTOW, and Stinger Missiles Installed LTC G. Downs

MAJ L. ToddMAJ E. TavaresCPT W. Carmona

AH-iS 84-16-1 AH-IS (MC) Degraded Hydraulic Mode Jan 1986 R. Adler A178 764(MC) Evaluation CW4 P. Sullivan

CPT A. Omlie

AH-IS 84-16-2 Preliminary Report, AH-IS(MC) Roll SCAS Jan 1986 CPT A. Omlie(MC) Prelim LR Card Evaluation

AH-IS 84-16-2 Report, AH-1S(MC) Roll SCAS Card Evaluation Arp 1986 R. Adler(MC) LR CPT A. Omlie

CW4 P. SullivanW. Kelly

AH-IS 84-21 Letter of Effort, AH-IS Air-to-Air Combat Jan 1985 CW4 P. SullivanLOE Test (AACT) III Evaluation MAJ G. Sharon

W. AbbottR. AdlerMAJ J. Lawrence

AH-IS 84-24 Letter of Effort, Firing of the AH-IS (MC) with Jan 1985 MAJ R. RatclilffLOE the HELLFIRE, TOW and Stinger Missile CW4 R. Murrell

Configuration

AH-1S 84-24-1 Report, Evaluation of the AH-IS(MC) Helicopter May 1985 CW4 R. Murrell(MC) LR TOW Helicopter/Stinger Head-Up Display CPT A. Omlie

AH-IS 85-11 Report, Evaluation of the AH-1S with the Hub Sep 1985 J. JohnsonLR Spring Improvement CW4 R. Murrell

AH-IS 86-06 Airworthiness and Flight Characteristics Test of Aug 1986 CW4 P. Sullivan B114 673the AH-IS with Hub Spring Installed CW4 J. Lyle

MAJ A. OmlieR. Adler

JAH-IS 78-17-1 Airworthiness Demonstration, JAH-IS PNVS May 1979 CPT T. BurchSurrogate Trainer (Martin-Marietta) COMP SENS R. Smith

JAH-IS 78-17-2 Airworthiness Demonstration, JAH-IS PNVS Aug 1979 MAJ F. DotenSurrogate Trainer (Northrop) COMP SENS CPT F. Bowers

YAH-IS 74-34 Airworthiness and Flight Characteristics Aug 1975 G. Skinner A025 476Evaluation, YAH-IS Improved Cobra Agility W. Abbottand Maneuverability Helicopter CPT R. Tart

66


(continued)


YAH-1S 77-04 Army Preliminary Evaluation, YAH-IS, Heli- Aug 1977 MAJ J. Arnold A066 573copter with Modified Flat Plate Canopy Installed MAJ J. Guin

CW4 J. BishopG. Skinner

UH-1 82-86 Letter Report, Main Rotor Blade Container Oct 1982 CPT R. SavageLR Program Investigation

UH-1 86-20 Preliminary Airworthiness Evaluation of a UH-1 Feb 1987 MAJ F. Stellar A186 274Equipped with a Terrain Mapping Receiver MAJ J. BrownAntenna C. Butler

UH-1B 63-81 Engineering Flight Test of UH-IB Helicopter Jun 1966 G. Yamakawa 488 791aka Equipped with XM-16 Armament Subsystem MAJ J. Foster65-01 and XM-21 Armament Subsystem, USATECOM

Project No. 4-4-1532-03 and 4-5-1535-04

UH-1B 63-93 Military Potential Test of the Model 540 "Door Feb 1964 J. Kidwell 951 593Hinge" Rotor System, USATECOM Project CPT D. WrayNo. 4-40108-01

UH-1B 64-02 Engineering Test of UH-IB Helicopter Equipped Aug 1966 J. Blaha 805 698with Flotation Landing Gear, USATECOM 1LT R. RichProject No. 4-5-5301-01

UH-IB 64-28 Engineering Evaluation of the UH-IB Helicopter Jun 1966 L. Schroers 804 242Equipped with the Model 540 Rotor System, CPT M. AntoniouPhase B, USATECOM Project No. 4-4-0108-03

UH-1B 64-28 Engineering Flight Test of the UH-IB Helicopter Dec 1966 L. Schroers 811 782Equipped with the Model 540 Rotor System, J. MeltonPhase D, USATECOM Project No. 4-4-0105-03 J. Watts

J. ShapleyMAJ A. DarlingMAJ D. DuganMAJ E. SampsonW. Anderson

UH-IB 65-12 Engineering Flight Test of UH-IB/540 Rotor Dec 1966 J. Nagata 811 781Helicopter Equipped with XM-16/M-5,XM-21/M-5, or XM-3/M-5 Armament Subsystem,USATECO Project No. 4-5-1591-01

UH-IB 65-22 Engineering Flight Test of UH-IB Helicopter Nov 1966 M. Reif 809 915Equipped with XM-47 Antipersonnel Mine MAJ N. MattmullerDispensing Subsystem, USATECOM Project J. ShapleyNo. 4-4-6516-05

UH-IB 68-04 Special Study of Autorotational Procedures Apr 1968 J. Shapley 676 820K. Ferrell

UH-IB 71-04 Letter Report, Airworthiness Qualification Test Apr 1971 MAJ D. BroadhurstLR UH-IB Helicopter with XM26 Armament TOW ILT R. Thomas

System Installed Under Asymmetric Loading

67


(continued)

Aircraft Project AdType Number Report Title Date Author(s) Numbcr

NUH-1B 71-22 Letter Report, Airworthiness Test of the NUH-IB Aug 1971 MAJ R. HolasekLR Helicopter Equipped with an Automatic Terrain- SP4 J. Lehman

Avoidance/Following System

UH-IC 65-12 Engineering Flight Test of the UH-IC Helicopter Feb 1967 J. Petrie 815 629aka Equipped with the M-5 Grenade Launcher and MAJ G. Hall66-09 the XM-158 or XM-159 Airborne Rocket Launcher

Pods Suspended from the XM-156 Multiarmament

Mount, USATECOM Project No. 4-4-1542-06and -09

Ul-1C 66-05 Engineering Test (Airworthiness and Performance Jan 1967 G. Yamakawa 808 293Tests) of UH-IC Helicopter with Cluster, MAJ W. WelterCanister, Riot Control CS, 130 1B, E-159,USAETCOM Project No. 5-5-3405-10

UH-IC 67-02 Letter, Report Engineering Flight Test of the Aug 1967 J. Petrie LRUH-IC/XM-26 (TOW/H) Armament System, MAJ R. HolasekArmy Preliminary Evaluation

UH-IC 67-07 Analytical Study of Range Performance of the May 1968 R. Finnestead 839 031LR UH-1C Helicopter Equipped with Lycoming

T53-L-13 Engine

UH-IC 67-09 Engineering Flight Test of the UH-IC Helicopter Nov 1967 K. Ferrell 827 184Equipped with the XM-30 Weapon System, MAJ D. DuganArmy Preliminary Evaluation MAJ R. Holasek

Ulf-IC 68-12 Wind Tunnel and Flight Evaluation Rosemount Apr 1969 K. Ferrell 708 859Shielded Pitot-Static Tube Model 850N J. Shapley

J. Mishlof

UH-IC 68-13 Flight Evaluation, AN/APN 191 Radar Sep 1970 G. Bender 714 638Altimeter MAJ J. Burden

UH-IC 68-22 Rotary Wing Vehicle External Stores Jettison Aug1970 CPT A. Hoffman 713 872CH-47C Envelope Pilot Established Requirements MAJ W. Davis

Ui-IC 68-25 A Flight Research Investigation of Autorotational Mar 1976 K. Ferrell A071 153Performance and Height-Velocity Testing of a A. FredericksonSingle Main Rotor Single Engine Helicopter R. Kyker

J. Shapley

UH-IC 69-07 Jettison Test XMI9/MK45 Flare Dispenser Dec 1969 MAJ D. Wray 864 077Installed in the UH-IC Helicopter

UH-IC 70-23 Investigation of Engine Rigging, Airspeed and Dec 1970 LTC J. Fitch 717 047Rotor RPM Effects on Steady State J. ShapleyAutorotatlional Performance

UH-IC 70-33 Evaluation of Fuel Flowmeter Instrumentation Jan 1971 A. Winn 219 280R. Jefferis

68

BELL HELICOPTER 1EXTRONINC.

(continued)


UH-1C 71-27 Airworthiness Evaluation UH-IC XM156/ Jan 1972 A. Winn 892 242Hornet Missile System J. Kishi

UH-IC 71-30 Flight Evaluation, Elliott Low-Airspeed Sensor, Sep 1972 A. Winn 753 343Final Report I J. Kishi

UH-IC 71-30 Flight Evaluation, Aeroflex True Airspeed Mar 1973 K. Ferrell 764 240OH-58A Vector System Low-Airspeed System, Final A. WinnF-51D Report II J. Kishi

B. Jefferis

UH-1C 71-30 Flight Evaluation, Pacer Systems Inc. LORAS II Mar 1974 B. Boirun 780 018Airspeed System, Low-Airspeed Sensor, Final F. DominickReport III J. Kishi

MAJ J. SmithMAJ R. Merrill

NUH-IC 71-30 Flight Evaluation, J-Tec Airspeed System Apr 1974 F. Dominick 780 019Low-Airspeed Sensor, Final Report IV B. Boirun

J. KishiR. Jefferis

UH-ID 63-77 Letter Report on the High-Altitude Evaluation Jun 1965 L. SchroersLR of the U.S. Army UH-ID Helicopter Equipped

with the 48-Foot Rotor Blade, USATECOMProject No. 4-4-0205-01

UH-ID 64-20 Final Report of Engineering Test of the Mar 1965 J. KudirkaYT53-L-13 Engine Installed in theUH-1D D. WilsonHelicopter, USATECOM Project No. 4-3-0150-10

UH-ID 64-20 Engineering Test of the UH-ID Helicopter with Apr 1966 J. Melton 845 032XT67 Power Plant Installed, USATECOM Project W. AndersonNo. 4-3-0150-17

UH-ID 70-20 Letter Report, Handling Qualities of the UH-ID Aug 1970LR Helicopter with Terminal Communications System

(TACSAT) Antenna Installation

EH-IH 77-15 Preliminary Airworthiness Evaluation, EH-IH Oct 1977 MAJ J. Guin A058 785Helicopter Quick Fix, Phase IA R. Buckanin

UH-IH 66-04 Engineering Flight Test of the UH-IH Helicopter, Aug 1967 F. DominickPhase D Product Improvement Test, Interim L. ThomasReport USATECOM Project No. 4-5-0150-04 CWO E. Nelson

UH-IH 67-08 Sling-Load Performance Capability of the Dec 1970 F. Dominick 878 570UH-IH Helicopter, Analytical Study

UH-IH 69-08 Letter Report Flight Evaluation on the Big Nov 1969 MAJ G. HallLR Ear Cannister Deployment Subsystem

69


(continued)


UH-IH 69-15 Letter Report Airworthiness Qualification of the Oct 1969LR UH-1H Helicopter with the Airborne Searchlight

System (AN/ASS-2) Installed

UH-1H 70-14 Airworthiness Qualification Test of the UH-IH Jan 1971LR Helicopter with Airborne Searchlight Infrared

Filter Installed

UH-IH 70-15-2 Vibration and Temperature Survey Production Jan 1973 E. Laing 909 441UH-IH Helicopter MAJ L. Hepler

MAJ R. Merrill

UH-IH 70-22 Lcticr R, eport, L'I-IH Helicopter with the Oct 1972 J. PetrieLR Airborne Ambush Detector (AAD), Qualitative MAJ A. Todd

Handling Qualities Evaluation

UH-IH 70-40 Letter Report, Helicopter-Mounted Insecticide Feb 1973 MAJ R. WaddellLR Spray System Evaluation SP4 J. Lehman

UH-1H 71-18 Letter Report, UH-IH Tail Rotor Hover Oct 1971 R. FinnesteadLR Performance LTC W. Graham

UH-1H 71-18 Tall Rotor Performance and Translational Jan 1972 R. Finnestead 901 787Flight Handling Qualities Tests UH-IH LTC W. GrahamHelicopter

UH-1H 71-29 Letter Report, Reevaluation of the DSPG Aug 1971 MAJ J. BurdenLR SPIKE-EXRAY Program

UH-IH 71-31 ALARM System Airworthiness Test Feb 1972 MAJ R. HolasekLR MAJ J. Alvis

PFC J. Lehman

UH-IH 71-42 UH-I/XM56, Army Preliminary Evaluation Feb 1972 MAJ R. ChaplinLR PFC J. Lehman

UH-IH 71-45 XM56 Mini-Dispersion Test Feb 1972 MAJ R. ChaplinLR SP4 J. Lehman

TIH-IH 73-04-4 Artificial Icing Tests UH-IH Helicopter Part I Jan 1974 R. Smith 779 502CPT M. HanksCPT L. Brewer

CW4 J. ReidLTC W. Griffith

UH-IH 73-04-4 Artificial Icing Tests UH-IH Helicopter, Jan 1974 CPT M. Hanks 779 503Part II Heated Glass Windshield MAJ C. Mittag

ILT M. HawleyLTC W. Griffith

UH-IH 73-07 Helicopter Night Landing System Jun 1973 MAJ R. ChaplinLR Airworthiness Evaluation R. Smith

70


(continued)


UH-IH 73-10 Tail Rotor Shaft Vibration Survey, Production Jul 1974 E. Laing A002 574UH-IH Helicopter CPT M. Hawley

CPT A. Weand

UH-IH 74-13 Artificial Icing Tests, Lockheed Advanced Ice Jun 1975 CPT L. Kronenberger B007 244LProtection System Installed on a UH-1H CPT M. HanksHelicopter MAJ R. Merrill

UH-1H 74-31 Natural Icing Tests, UH-1H Helicopter Jun 1974 LTC W. Griffith A002 007CPT M. HanksMAJ C. MittagCW4 J. Reid

UH-1H 75-26 Lockheed Advanced Ice Protection System May 1976 CPT L. Kronenberger

UH-IH 77-09 Preliminary Airworthiness Evaluation, UH-IH May 1978 V. Diekmann A078 476Helicopter Equipped with Multiple Target MAJ M. MathewsElectronic Warfare System (MULTEWS) MAJ S. Spring

MAJ J. HagenCW4 J. Tullock

UH-IH 77-10 Qualitative Evaluation of Flying Qualities of a Jul 1977 MAJ R. StewartLR UH-IH Helicopter with GE Infrared Exhaust

Suppressor Installed

UH-IH 77-30 Artificial Icing Test Ice Phobic Coatings on Jun 1978 CW4 J. Tulloch A059 875UH-1H Rotor Blades R. Smith

MAJ F. DotenCW4 J. Bishop

UH-1H 78-04 Preliminary Airworthiness Evaluation UH-1H Jul 1978 J. NagataLR Helicopter with Interim-Interim-Standoff MAJ J. Hagen

Target Acquisition System (12 SOTAS)

UH-1H 78-21 Artificial and Natural Icing Tests for Aug 1979 MAJ G. WilsonLR Qualification of UH-IH Kit A Aircraft R. Woratscheck

UH-IH 78-21-2 Microphysical Properties of Artificial and Aug 1979 MAJ G. Wilson A084 633Natural Clouds and Their Effects on UH-IH R. WoratschekHelicopter Icing

UH-IH 79-86 Ice Phobics Blade Tracking and Comparison May 1981 W. Abbott A108 121of Vibration Analysis Techniques F. Dominick

S. Arthur

UH-1H 80-06 Preliminary Airworthiness Evaluation of UH-IH Jun 1981 MAJ B. Picasso A 110 213with Hot Metal Suppressor and Infrared Jammer CPT L. A. Haworth

D. OttomeyerCPT R. Vincent

UH-IH 81-01-1 Fuel Conservation Evaluation of US Army Jan 1982 MAJ G. DownsLR Helicopters, Part I, Flight Operation Improvement

Analysis

71


(continued)


UH-1H 81-01-3 Fuel Conservation Evaluation of USA Helicopter Aug 1982 CPT F. StellarPart 3. UH-IH Flight Testing

IJH-lH 82-12 Evaluation of UH-IK Hover Performance Aug 1983 D. Belt. A141 252Degradation Caused by Rotor Icing CW4 R. Williams

CPT F. StellarW. Abbott

UH-IH 83-23 Evaluation of the UH-IH Level Flight Perform- Jul 1984 W. Abbottance Degradation Caused by Rotor Icing L. Linehan

CPT R. LockwoodMAM L. Todd

UH-1H 84-14 Preliminary Airworthiness Evaluation of the Jan 1985 CW4 J. Adkins A179 495UH-IH HIND-D Surrogate CPT M. White

D. MacphersonCPT D. CrlppsMMJ W. Grogan

UH-lH 34-25 Preliminary Airworthiness Evalautlon of the Jun 1986 C. Cassil A182 369UH-IH Helicopter with the T53-L-703 Engine MMJ R. LockwoodInstalled

UH-IH 84-31 Report, Evaluation of the UH-IH with the Hub Sep 83 J. JohnsonLI Spring Improvement CW4 R.. Murrell

tJH-1H 84-33 Combined Preliminary Airworthiness Evaluation Jul 1988 G. Skinner A202 316and Airworthiness and Plight Characteristics J. PiotrowskiEvaluation of the UH-1H with preproduction CPT M. WhiteHub Spring and Composite Main Rotor lades MMJ A. OmlieInstalled MAM J. Brown

UH-IH 85-24 Report, Structural Flight Loads Correlation of Jan 1987 M. GrahamLR the Structural Integrity Recording System (SIRS) W. Abbott

on the UN-IH4 Helicopter

UH-IH 86-03 Letter of Effort, UH-IH Composite Main Rotor May 1986 CPT A. OmnlieLOB Blades Rain Erosion Pattern

.JUH-IH 75-27 Letter of Effort, Qualitative Evaluation of Jan 1976LI JUH-IN with Kaiser 3-Axis MINISTAB

JUH-IH 79-02 JUH-IN Ice Phobic Coating Icing Tests Jul 1980 MMJ P. Morris A096 361R. Woratschek

JUH-1H 31-11 JUH-IN Pneumatic Boot Deicing System May 1983 MMJ R. Oliver A140 986Pligt Test Evaluation R.. Woratschek

CPT L. Haworth

.IUH-IH 83-13 JUN-IH Redesigned Pneumatic Boot Deicing Aug 1937 M. GrahamSystem Flight Test Evaluation CPT L. Haworth

CPT J1. Kimberly

72


(continued)

Aircraft Project Ad

Type Number Report Title Date Author(s) Number

JUH-IH 87-08 Letter of Effort, Loads Survey of a JUH-IH Jan 1988 G. Bender

LOE Helicopter with the Modified Second-Generation M. Herbst

Pneumatic Boot Deicing System

NUH-IH 76-13 Airworthiness Evaluation NUH-IH Helicopter May 1977 T. Benson A047 971

with Global Positioning System MAJ C. Thomas

YUH-IH 66-04 Engineering Flight Test of the YUH-IH Nov 1970 F. Dominick 879 656Phase D. Limited LTC E. Nelson

UH-IM 69-21 Letter Report Airworthiness Evaluation of Feb 1970 CW4 W. Connor

LR the UH-IM with Infant Subsystem Installed

UH-IM 70-29 Letter Report, Vibration Survey Tests on the Nov 1970 LTC D. HendricksonLR UH-IM Helicopter with the Forward-Looking

Infrared (FLIR) System Installed

UH-IM 70-29 Vibration and Elevator Loads Survey Tests of the Jun 1971 R. Finnestead a85 839UH-IM Helicopter with the Forward-Looking I TC D. HendricksonInfrared (FLIR) System Installed

UH-IM 71-07 Letter Report, Army Preliminary Evaluation May 1971 MAI D. Broadhurst

LR of the UH-IM Helicopter Multifunction CPT B. Nicholson

System (HELMS)

UH-IM 71-09 Letter Report, Follow-On Vibration Survey May 1971 R. FinnesteadLR of the UH-IM/FLIR MAJ R. Holasek

S. Streutker

UH-IM 72-05 Rotor Flow Survey Program UH-IM Helicopter May 1974 B. Boirun 787 428R. JefferisMAJ R. Holasek

NUH-1M 71-30-5 Flight Evaluation, Rosemount Orthogonal Low Nov 1974 CPT J. O'Connor 009 711

Airspeed System, Low-Airspeed Sensor, Final SP4 J. BullockReport V R. Jefferis

NUH-IM 71-30-6 Flight Evaluation, Elliott Dual-Axis Low Sep 1975 F. Dominick A019 360

Airspeed System, LASSIE II, Low Airspeed K. FerrellSensor, Final Report VI CPT J. O'Connor

NUH-1M 73-01 Helicopter Lift Margin System and Low-Speed Aug 1977 F. Dominick A060 553

Performance Evaluation NUH-IM Helicopter D. BelleR. JefferisJ. O'ConnorA. KrynytzkyLTC W. Griffith

NUH-1M 75-17-3 Flight Evaluation Rosemount Low Range Mar 1977 W. Abbott A046 491

Orthogonal Airspeed System with 853 Sensor MAJ J. Guin

NUH-IM 75-22 Letter of Effort, Engine Characteristics Test Jun 1977 F. 9ominickLR

73

IIlL ILIIC()TFrIR TEXTRONINC.

(continmed)


EH-1X 81-19 EH-IX Qualitative Flight Evaluation Dec 1981 CW4 R. WilliamsLR G. Yamakawa

EH-IX/ 82-13 Airworthiness and Flight Characteristics of the Jan 1984 LTC G. Downs A147 188EH-IH EH-IX/EH-1H Helicopter Configuration CPT J. Kimberly

CPT R. SavageCW4 J. AdkinsJ. NagalaJ. Inehan

OH-4A 63-23/Pt I Report of the Engineering Flight Test Stability Aug 1964 R. Finnestead 909 271and Control Phase of the OH-4A Helicopter, MAJ J. FosterUnarmed (Clean) and Armed with the XM-7or XM-8 Weapon Subsystem, USATECOMProject No. 4-3-0250-11/12/13

OH-4A 63-23/1l 2 Report of the Engineering Flight Test Perform- Aug 1964 J. Melton 909 272ance Phase of the OH-4A Unarmed (Clean) CWO J. Wtttsand Armed with the XM-7 or XM-8 WeaponSubsystem, USATECOM ProjectNo. 4-3-0250-12/13

JOH-8A 81-09 Preliminary Airworthiness Evaluation of JOH-8A Sep 1981 MAJ A. MarshallClassified

H-13G 61-06 Evaluation of the Mark XII Awdilary Fuel and Jul 1961 CPT J. Johnston 884 884L- 19A On System

OH-13H 62-13 Final Report Engineering Test of the Stability Apr 1964 L. Schroers 951 587aka and Control Characteristics of the OH-13H CWO E. Nelson62-30 Equipped with the XM-l Armament Kit

OH-13H 63-01 OH-13H Gross Weight Increame/XM-1 Jun 1963 R. Finnestead 951 596Armament Kit Performance Test CWO E. Nelson

UH-13R 63-07 Report of USATECOM Project No.4-4-0240-02, Jan 1964 L. Schroers 951 588aka Flight Evaluation of the T63-A-5 Turbo Shaft CPT M. Antoniou63-16 Engine Installed in a UH-13R Helicopteraka64-01

TH-13T 68-21 Letter Report Final Flight Test Results for Jun 1969 CPT J. BreckerLR TH-13T Helicopter

OH-58 83-03 Report, OH-58 Vertical Fin Blockage Evaluation Oct 1983 MAJ A. MarshallLR LTC R. Carpenter

MAJ M. HanksMAJ J. BensonJ. NagataCPT R. SavageCPT F. StellarM GrahamMAJ L. Todd

74


(continued)


OH-58A 68-30 Airworthiness and Flight Characteristics Test Sep 1970 G. Yamakawa 878 560Production OH-58A Helicopter Unarmed and J.WattsArmed with XM27EI Weapon System, Performance

OH-58A 68-30 Airworthiness and Flight Characteristics Oct 1970 E. Laing 875 793Test Production OH-58A Helicopter Unarmed LTC W. Grahamand Armed with XM27EI Armament Subsystem, MAJ P. StringerStability and Control

OH-58A 68-41 Army Preliminary Evaluation Prototype OH-58A Jan 1970 J. Nagata 865 456Helicopter with XM27EI Weapon Subsystem

OH-58A 68-53 Climatic Laboratory Test OH-58A Helicopter Jul 1970 SP4 D. Tyson 875 578Equipped with XM27EI Machine Gun SP4 J. PincavageArmament System N. Donaldson

CW3 J. Thomson

OH-58A 69-16 Height Velocity Test OH-58A Helicopter Jun 1971 J. Watts 884 973CPT G. C.ondonSP5 J. Pincavage

OH-58A 70-15-1 Instrument Panel and Avionics Compartment Sep 1972 E. Laing 907 738Environmental Survey Production OH-58A CPT J. ClaxtonHelicopter MAJ L. Hepler

LTC W. Graham

OH-58A 71-03 Study, Pilot Perceived Jettison Envelope Jun 1973 A. Winn 768 171OH-6A J. KishiAH-56A

OH-58A 71-21 Letter Report, Monitoring of OH-58A Snow Dec 1971 MAJ L. HeplerLR Ingestion Test

OH-58A 71-24 Evaluation of the OH-58A Helicopter with Dec 1972 E. Laing 907 291an Allison 250-C20 Engine T. Benson

SPS A. WemerMAJ D. Broadhurst

OH-58A 71-30 Flight Evaluation, Aeroflex True Airspeed Mar 1973 K. Ferrell 764 240UH-IC Vector System Low-Airspeed System, Final A. WinnF-S1D Report II J. Kishi

B. Jefferis

OH-58A 71-46 OH-58 Autorotational Evaluation Feb 1972 J. Watts 035 727LR V. Diekmann

OH-58A 72-01 Instrument Flight Evaluation OH-58A Helicopter Sep 1972 T. Benson 907 317

MAJ J. Smith

OH-58A 72-03 Fluidic Yaw Damper Evaluation Installed on the Dec 1972 MAJ J. SmithLR OH-58A Helicopter MAJ R. Chaplin

R. Smith

75

BELL hELIACOPTER TEXTRONINC.

(continued)


OH-58A 72-14 Helicopter Autorotational Demonstration Jun 1972 J. WattsLR S. Streutker

OH-58A 72-20 Handling Qutalities Evaluation of the OH-58A Feb 1973 R. Smith 909 536Helicopter Incorporating the Model 5703 T. BensonThree-Axis Stability and Control Augmentation MAJ J. SmithSystem

OH-58A 72-24 OH-58A/Insulated Infrared Exhaust Airworthi - Aug 1972 J. WattsLR ness Evaluation S. Streutker

OH-58A 72-31 OH-SIA/ISTAR Airworthiness Evaluation Dec 1972 MAJ R. ChaplinLR G. Bender

OH-58A 73-02 Evaluation of the Teledyne Ryan Model 622 Nov 1973 MMJ C. Mittag 775 806Terrain-Following Radar System Installed T. Bensonon an OH-5IA Helicopter CPT Rt. Taff

CW3 1. Meiss

OH-58A 74-23 Handling Qualities Evaluation OH-58A Feb 1975 E. Balles A033 827Helicopter Incorporating a Ministab 3-Axis R. BuckaninStability Augmentation System CPT C. Mittag

OH-SSA 74-48 Evaluation of an OH-SSA Helicopter with Apr 1975 T. Benson A018 861an Allison 230-C203 Engine Rt. Buckanin

MMJ C. MittagCPT 3. Jenks

OH-58A 77-11 Flight Evaluation, MK 11 Integrated Controller Apr 1978 MMJ J. Hagen A065 072Installed on an OH-S8 Helicopter CPT P. Moe

R. Woratachek

OH-59A 77-34 Preliminary Airworthiness Evaluation OH-5SA/ Dec 1977 G. BenderLR XM-130 Chaff Dispenser CPT T. Burch

JOH-58A 74-22 Engineering Evaluation JOH-59A Helicopter Jun 1975 T. Benson A019 407with an Automatic Engine Relight System R. Buckanin

MMJ C. Mittag

JOH-58A 75-1' Army preliminary Evaluation, JOH-59A Hell- Dec 1975 T. Benson A024 727copter with Low Reflective Paint and Infrared MMJ C. ThomasCotiermesuwe Exhaust System R. Buckanin

JOH-58A 75-24 Integrated Controller Evaluation Sep 1976 CPT J. Arnold A035 064CPT M. MathewsMMJ C. Thomas

JOH-58A 11-10 Report Preliminary Airworthiness Evaluation Sep 1981 MMJ M. StrattonLR of JOH-58A ofth Composite Tall Boom J. Nlemann

YOH-59A 75-20 Army preliminary Evaluation, YOH-58A Dec 1975 G. Skinner A024 501Helicopter with Flat-Plate CPT J. Arnold

76


(continued)


OH-58C 76-11-1 Preliminary Airworthiness Evaluation OH-58C Mar 1978 G. Yamakawa A071 699Helicopter MAJ J. Hagen

R. BuckaninCPT T. Burch

OH-58C 76-11-2 Airworthiness and Flight Characteristics OH-58C Apr 1979 MAJ S. Spring A080 138Interim Scout Helicopter CPT T. Burch

R. BuckaninJ. Niemann

OH-58C 77-26 OH-58C Rain Removal System Test Oct 1977 MAJ J. HagenLR

OH-58C 78-09 Preliminary Airworthiness Evaluation OH-58C M.y 1980 CW4 J. Bishop A094 I lHelicopter with a Mast Mounted Sight CPT M. Hanks

T. BensonA. Arrigo

OH-58C 78-12 Letter Report Airworthiness and Flight Feb 1981 MAJ R. CarpenterLR Characteristics Test of OH-58C with XM-130 G. Yamakawa

Chaff Dispenser System

OH-58C 79-12 Letter Report, OH-58C Directional and Mar 1981 CW4 J. BishopLR Longitudinal Control Mapping Evaluation T. Benson

D. Ottomeyer

OH-58C 79-15 Preliminary Airworthiaess Evaluation, OH-58C Dec 1979 T. BensonLR Helicopter with Installed Bell Helicopter CW4 J. Bishop

Textron Model 206L-1 Tail Rotor

OH-58C 79-18 Letter Report Preliminary Airworthiness Jul 1980 T. BensonLR Evaluation OH-58C Helicopter with 206L-1 CW4 J. Bishop

Tail Rotor and Bell Helicopter Textron 570B D. OttomeyerStability and Controi Augmentation System MAJ 1. Benson

OH-58C 79-23 Letter Report Preliminary Airworthiness Jun 1980 MAJ J. BensonLR Evaluation OH-58C Configured with a Wire T. Benson

Strike Protection System

OH-58C 80-15 Preliminary Airworthiness Evaluation of the Jul 1981 LTC R. WardLR OH-58C Helicopter with Fixed Short Landing MAJ J. Benson

Gear with Two Position Landing Gear G. Yamakawa

OH-58C 80-21 Preliminary Airworthiness Evaluation of OH-58C May 1981 MAJ J. BensonLR Expanded Gross Weight and Lateral CG G. Yamakawa

Envelope

OH-58C 81-05 Report OH-58C Wire Strike Protection System Jul 1981 LTC R. WardLR (WSPS) Lower Cutter Ground Contact MAJ J. Benson

Investigation

Off 58C 81-07 Airworthiness and Flight Characteristics of an Oct 1981 MAJ A. Marshall Al 12 58IOH-58C Configured to a Light Combat LTC R. WardHelicopter (LCH) R. Woratschek

77


(continued)


OH-58C 80-19 Report Preliminary Airworthiness Evaluation of Jun 1981 G. YamakawaLR JOH-SIC Modified to a Light Combat Helicopter CPT A. Marshall

with a M197 20MM Gun MAJ R. Carpenter

OH-58C 81-01-4 Fuel Conservation of USA Helicopters, Part 4, Aug 1982 MAJ M. StrattonOH-58C Flight Testing D. Belie

OH-58C 81-14 OH-58C with Installed Mast Mounted Sight Aug 1982 MAJ M. StrattonLR (MMS) Masking & Unmasking Time Line J. Ottomeyer

Analysis Evaluation

OH-58C 81-89 Preliminary Airworthiness Evaluation of the Apr 1982 MAJ A. MarshallOH-5I with Prototype AN/AVR-2 Laser Detection G. BenderSystem Installation

OH-58C 82-02 Preliminary Airworthiness Evaluation of the Apr 1932 MAJ R. MarshallLR OH-5SC with Prototype AN/AVR-2 Laser G. Bender

Detection System Installation

OH-58C 83-15 Preliminary Airworthiness Evaluation of the Oct 1983 MAJ M. HanksOH-58C with 3-Axis Stability Control MAJ L. ToddAugmentation System and Improved Tall J. NagataRotor System M. Graham

OH-58C 83-19 Report, OH-SIC Oil Cooling System Evaluation Apr 1984 MAJ A. MarshallLR C. Cassil

OH-5C 83-30 Report, Pitet-Static System Evaluation of Dec 1983 C. CassilLR OH-58C wit) Air-to-Ground Engagement System MAJ A. Marshall

(AGES) Installed

OH-58C 84-29 Report, Piltot-Static System Evaluation of the Dec 1983 MAJ A. MarshallLR OH-S8C with Air-to-Ground Engagement C. Cassil

System (AGES) Installed

OH-58C 84-34 Flight Test Evaluation of the OH-58C Main Feb 86 M. GrahamRotor Blade Erosion Tape MAJ J. Martin

MAJ F. StellarR. Woratschek

JOH-58C 84-35 Letter of Effort, Transmittal of the Rsults of the Jan 1985 MAJ E. MitchellLOE Qualitative Evaluation for the JOH-S8C Helicopter

JOH-58C 85-03 Airworthiness and Flight Characteristics of the Feb 1986 CW4 J. Webre A180 259JOH-58C (OH-S8X Surrogate) Helicopter MAJ F. Stellar

R. WoratschekM. GrahamMAJ J. Martin

OH-58D 83-26 Preliminary Airworthiness Evaluation (PAE) Dec 1984 G. Bender A178 740of the OH-58D Helicopter (AHIP) CPT J. Kimberly

MAJ E. MitchellMAJ G. Sharon

78


(continued)


OH-58D 83-27 Interim Report, Airworthiness and FIgiht Oct 1984 J. NagataLR Characteristics (A&FC) of the OH-58D Helicopter MAJ G. Bishop

CPT L. CaytonCPT T. WalshMAJ F. Stellar

OH-58D 87-29 Report, Preliminary Airworthiness Evaluation Jan 1988 MAJ F. StellarLR (PAE) of an Increased Gross Weight External G. Bender

Stores Configuration for the OH-58D Helicopter

JYAH -63 74-07-1 Development Test 1 Advanced Attack Helicopter Dec 1976 G. Bender A109 531Competitive Evaluation Bell YAH-63 Helicopter V. Diekmann

CPT M. MatthewsR. SmithMAJ C. ThomasR. WoratschekMAJ J. ArickCPT J. Arnold

Bell 86-08 Report, Technology Flight Evaluation of the CAE Aug 1986 R. Robbins205A LR Electronic Lid, Hand Controller on a Bell 205A MAJ F. Stellar

Helicopter

Bell 87-33 Report, Technology Flight Evaluation of the Apr 1988 MAJ J. Lawrence222 LR Bell Helicopater Textron Inc. (3HTI)/Lucas MAJ W. Carmona

Aerospace Adaptive Fuel Control on a Bell 222 R. BuckaninHelicopter R. Woratschek

Model 61-02 Bell Model 47G-3 High Altitude Flight Evaluation Feb 1961 J. Kidwell 722 8t476-3

Model 62-12 Limited High-Altitude Evalua'ion of the J. Kidwell 884 89647G-3B Bell 47G-3B Helicopter CWO E. Nelson

A. Averill

Model 62-05 Limited Evaluation of the Bell Model 47J-2 May 1962 E. Smith 884-89147J-2 J. Kidwell

Model 83-12 Government Pilot Evaluation of the BHTI 206/ Jan 1985 J. Nagata206 Ring Fin Tail Rotor CW4 J. Adkins

Model 67-06 Letter Report Bell 206A SAS Evaluation P pr 1967 MAJ R. Chubboy206A LR

Model 67-13 Light Observation Helicopter (LOH) Model 206A, Dec 1967 LTC E. Preisendorfer 951 595206A Armed (XM-27E1) and Unarmed, Performance LTC W. Crouch

and Stability and Control F. Dominick

Model Engineering Flight Evaluation of the Bell May 1966 J. Kidwell 811 482209 Model 209 Armed Helicopter USATECOM

Project No. 4-6-0300-01

Model 68-46 Army Preliminary Evaluation of the Prototype Mar 1969 J. Nagata 849 (3211 BHC Model 211 Hucylug LTC T. Wright

MAJ I Rundgren

79


(continued)


214ST 85-10 Airworthiness and Flight Characteristics Test Feb 1985 CW4 R. Williams A175 349of the BHTI 214ST Helicopter R. Buckanin

CPT R. Cason

Model 81-13 Letter of Effort for Support of Bell Helicopter Apr 1982 LTC R. Ward214 LOE Textron, Icing Certification of the 214st Helicopter

Model 74-30 Airworthiness and Flight Characteristics Jul 1975 LTC W. Horton B014 228L"14A Evaluation, Iranian Model 214A Helicopter G. Bender

ILt L. FreeCPT J. O'ConnorJ. NagataCPT R. Ward

Model 74-32 Climatic Laboratory Evaluation, Iranian Aug 1976 MAJ R. Ward B030 107L214A Model 214A Helicopter CW4 J. Coleman

D. BelteK. Dorris

Model 77-32 Limited Airworthiness and Flight Characteristics May 1979 MAJ J. Guin A071 271214A Evaluation Model 214A Helicopters with G. Bender

Fiberglass Rotor Blades E. BailesCPT R. Robbins

Model 77-37 Handling Qualities Test on a Model 214A Dec 1977 CPT S. Spring214A LR Helicopter

Model 76-02 Performance and Systems Evaluation Iranian Mar 1977 G. Yamakawa B027 647L214C Model 214C Helicopter t. Woratschek

CPT S. Spring

Model 80-02 Letter Report Preliminary Airworthiness Aug 1980 G. Yamakawa249 LR Evaluation (PAE) of Bell Helicopter Textron MAJ B. Picasso

(BHT) Model 249 Cobra J. Brown

Model 72-10 Attack Helicopter Evaluation Model 309 Jul 1972 J. Nagata 771 151309 KingCobra Helicopter G. Skinner

PFC G. SmithR. JungelMAJ L. HeplerLTC P. Stringer

M ndz. 72-31 Sideward Flight, High-Altitude Evaluation and Aug 1972 J. Nagata A109 512309 aka Simulated Engine Failures KingCobra R. Jungel

72-34 Model 309 Attack Helicopter MAJ L. HeplerPFC 6. SmithG. Skinner

80

BOEING-VERTOL


CH-47 67-04 Engineering Flight Test of the CH-47 (Chinook) Mar 1968 A. Higgins 832 821Helicopter Integral Weight and Balance Systems ILT S. Schwartz(ENSURE) H. Catey

MAJ R. Forsyth

CH-47A 66-17 Letter Report of USA Preliminary Engineering Sep 1966 K. FerrellLR Evaluation (Product Improvement Test (PIT) MAJ M. Mattmuller

Limited, Phase B), of the Proposed CH-47A, J. Shapley36,000-pound Flight Envelope, USATECOMProject No. 4-3-0200-32

CH-47A 68-24 Qualitative Flight Evaluation of the Flight Nov 1968 ILT T. Lane 844 426LR Engagement Tactical Cargo Hook (FETCH) on MAJ R. Forsyth

a CH-47A Helicopter LTC T. Wright

CH-47B 66-23 Engineering Flight Test of the CH-47B Mar 1968 G. Yamakawa 834 597(Chinook) Helicopter, Phase D, Interim Report, LTC L. MillerUSATECOM Project No. 4-6-0200-03 MAJ H. Chambers

CH-47B 66-23 Airworthiness and Qualification Test, (Phase D), Mar 1970 G. Yamakawa 871 209CH-47B Helicopter, USATECOM Project LTC L. MillerNo. 4-6-0200-03

CH-47B 68-02 CH-47B Height Velocity Evaluation Feb 1970 CPT A. Hoffman 866 347

MAJ W. DavisJ. Shapley

YCH-47B 66-26 Engineering Flight Test of the YCH-47B, Army Jun 1967 MAJ M. MattmullerLR Preliminary Evaluation I & II, USATECOM G. Yamakawa

Project No. 4-6-0200-02 MAJ D. Dugan

MAJ H. Chambers

YCH-47B 66-26 Engineering Flight Test of the YCH-47B Jan 1969 G. Yamakawa 848 849Helicopter Army Preliminary Evaluation 1, 11, & MAJ M. MattmullerIll, USATECOM Project No. 4-6-0200-02 MAJ D. Dugan

MAJ H. Chambers

CH-47C 66-29 Airworthiness and Flight Characteristics Test Sep 1971 LTC R. Forsyth 892 400CH-47C (Chinook) Helicopter, Performance, J. NagataUSATECOM Project No. 4-6-0201-03 LTC G. Marr

MAJ J. Burden

CH-47C 66-29 Airworthiness and Flight Characteristics CH-47C Mar 1972 J. Nagata 903 488Helicopter (Chinook), Stability and Control, G. SkinnerUSATECOM Project No. 4-6-0201-03 SP4 P. Bohn

MAJ A. ToddMAJ D. Broadhurst

LTC D. Hendrickson

CH-47C 68-22 Rotary Wing Vehicle External Stores Jettison Aug 1970 CPT A. Hoffman 713 872UH-IC Envelope Pilot Established Requirements MAJ W. Davis

81

BOEING-VERTOL(continued)

Aircrart Project AdType Number Report Title Date Author(s) Numbtr

CH-47C 69-17 Height-Velocity Evaluation CH-47C Helicopter Sep 1972 1. Nagata 904 930with TSS-L-11A Engines A. Steinmetz

MAJ A. ToddMAJ J. Burden

CH-47C 70-12 CH-47C 50,000-Pound Gross Weight Evaluation Mar 1971 MMJ A. ToddLR CH-47C ILT D. D'Amore

LTC H. Chambers

CH-47C 70-15-6 Vibration and Temperature Survey Production Sep 1975 E. Laing A022 348CH-47C Helicopter CPT M. Hawley

R. SmihbCPT J. O'ConnorCPT L. Kronenberger

CH-47C 71-41 CH-47C Improved Flight Control System Dec 1972 MAJ W. HortonLR SF4 C. Bowers

CH-47C 72-15 CH-47C Weight and Balance System Mar 1973 J. NagataLR

CH-47C 72-35 Helicopter Icing Spray System Qualification Oct 1973 J. Hayden 775 803E. BailesJ. Watts

CPT L. Brewer

CH-47C 72-39 CH-47C Tandem Cargo Hook Demonstration May 1973 J. NagataLR CPT L. Brewer

CH-47C 73-04 Icing Tunnel Test Hot-Film Anemometer Feb 1974 SP4 P. Bonin A005 044R. Jefferts

CH-47C 73-04-1 Artificial Icing Tests CH-47C Helicopter Aug 1974 MMJ C. Mittag A004 008CPT M. HanksCPT J. O'ConnorCFPT L. Kronenberger

CH-47C 73-05 CH-47C Terminat Radar Area Coffelator Apr 1973 CPT L. BrewerLRt Experiment (TRACE

CH-47C 74-27 CH-47C Prototype Infrared Countermeasures Jun 1974 MMJ W. HortonLR (ICRM) Airworthiness Demonstration Evaluation J. jNagata

SF4 P. Bonin

CH-47C 75-04 Modified Helicopter Icing Spray System Mar 1977 G. Bender A055 039Evaluation CPT M. Mathews

CW4 J. Tulloch

CH-47C 75-06 Letter of Effort, CH-47C, Active Arm External Apr 1976 CPT G. Nepereny LRLoad Stabilization System (AAELSS) 11 FlightEvaluation Program

CH-47C 77-24 CH-47C Inlet Flow Distortion Evaluation May 1978 MMJ J. GuinLR

82



CH-47C 77-29 Airworthiness and Flight Characteristics Aug 1978 MAJ R. TarrLR Evaluation, CH-47C Helicopter with MAJ J. Guin

T55-L-712 Engines G. Skinner

CH-47C 77-31 Preliminary Airworthiness Evaluation CH-47C Apr 1979 MAJ S. Spring A069 S0 Iwith Fiberglass Rotor Blades (with T55-L-712 J. NiemannEngines) MAJ G. Wilson

CH-47C 78-18 Artificial Icing Tests with CH-47CHelicopter Jul 1979 J. Niemann A081-860with Fiberglass Rotor Blades CPT F. Bowers

MAJ S. Spring

CH-47C 79-02-2 Helicopter Icing Spray System (HISS) Nozzle Sep 1981 D. Belte A109 405Improvement Evaluation

CH-47C 80-04 Helicopter Icing Spray System (HISS) Evaluation Jun 1981 R. WoratschekLR and Improvements LTC 0. Wilson

CH-47C 80-13 Helicopter Icing Spray System Calibration, Ice Aug 1981 J. HendersonPhobics and FAA R&D Evaluation R. Woratschek

CPT L. Haworth

CH-47C 80-04-2 Helicopter Icing Spray System(HISS) Evaluation Jun 1982 R. Woratschekand Improvement

CH-47C 82-15-1 Helicopter Icing Spray System (HISS) Structural Aug 1982 R. WoratschekLR Dynamics Evaluation with Fiberglass Blades MAJ M. Hanks

JCH-47C 82-05-3 Helicopter Icing Spray System (HISS) Evaluation Apr 1986 D. BeliteHISS and Improvements

YCH-47C 66-28 Engineering Flight Test of the YCH-47C Mar 1968 MAJ R. ForsythMedium Transport Helicopter Army Preliminary MAJ H. ChambersEvaluation I, Interim Report ILT J. Jester

SP4 F. Wilson

YCH-47C 66-28 Engineering Flight Test of the YCH-47C, Mar 1968 CPT J. Jester 844 427Medium Transport Helicopter Army Preliminary SP4 F. WilsonEvaluation I, USATECOM Project LTC H. ChambersNo. 1-5-0201-02 MAJ R. Forsyth

YCH-47C 66-28 Engineering Flight Test of the YCH-47C, Feb 1969 CPT J. Jester 855 630Medium Transport Helicopter, Army Preliminary ILT T. LaneEvaluation Part II, USATECOM Project LTC H. ChambersNo. 4-6-0201-02 MAJ R. Forsyth

CH-147 75-05 Qualititalve Army Preliminary Evaluation of the Oct 1974 MAJ W. Horton(CH-47C) LR Canadian Production CH-147 Helicopter J. Watts

YCH-47C 66-28 Army Preliminary Evaluation III and IV Oct 1970 CPT J. Jester 878 571YCH-47C, Medium Transport Helicopter, LTC R. ForsythUSATECOM Project No. 4-6-0201-02

83

BOEI NG-VERTOL(continued)


YCH-47C 68-32 Letter Report of the YCH-47C Helicopter Jan 1969 MAJ G. MarrLR 50,000-Pound Gross Weight Evaluation

CH-47D 82-07 Airworthiness and Flgiht Characteristics (A&FC) Feb 1984 G. BenderTest of the CH-47D Helicopter G. Yamakawa

M. HerbstR. Robbins

CW3 P. Sullivan

CW4 R. Williams

CH-47D 83-04 Preliminary Airworthiness Evaluation, CH-47D May 1983 CW4 R. Williamsat 54,000 pounds Gross Weight CW3 P. Sullivan

R. Robbins

G. YamakawaM. HerbstG. Bender

CH-47D 84-06 Report, Preliminary Airworthiness Evaluation Aug 1984 CW4 P. SullivanLR Test of te CH-47D with Light Weight Airborne R. Woratschek

Forward Looking Infrared (FLIR) System (LAFS) R. RobinsInstalled

CH-47D 85-09 Aerial Refueling Evaluation of the CH-47D Aug 1985 M. Herbst A167 575Helicopter R. Robbins

CW4 P. Sullivan

CH-47D 86-18 Interim Report, Aerial Refueling Evaluation of Jan 1987 R. Robbins1.R the CH-47D Helicopter, Phase I1

CH-47D 86-18 Aerial Refueling Evaluation of the CH-47D Jan 1987 R. RobbinsHelicopter, Phase II MAJ R. Cason

MAJ T. Reininger

CH-47D 88-11 Report, CH-47D Emergency Descent Evaluation Sep 1988 MAJ R. CasonLR CW4 P. Sullivan

R. Robbins

J. Piotrowski

YCH-47D 79-06 Preliminary Airworthiness Evaluation I (PAE 1) May 1980 J. Niemann A092 633of the YCH-47D Helicopter MAJ G. Wilson

MAJ C. AdamCPT F. BowersS. Arthur

YCH-47D 80-05 Letter Report Preliminary Airworthiness Jul 1980 LTC G. WilsonLR Evaluation (PAE) II of the YCH-47D with MAJ C. Adam

Modified Advanced Flight Control J. Nlemann

YUH-61A 74-06-2 Government Competitive Test, Utility Tactical Nov 1976 A. Winn B035 081LTransport Aircraft System (UTTAS) Boeing- MAJ J. JenksVertol, YUH-61A Helicopter F. Deprospero

CPT E. TaveresCPT J. O'Connor

LCdr J. Ludwig

84



YUH-61A 75-12-2 Climatic LaLoratory Evaluation, Utility Tactical Jul 1977 D. Belte B031 052LTransport Aircraft System (UTTAS) Boeing- R. Followill

Vertol, YUH-61A Ground Test Vehicle R. SeefeldtD. Wallis

YUH-61A 76-09-2 Artificial Icing Test, Utility Tactical Transport Jan 1977 CPT J. O'Conner At09 515Aircraft System (UTTAS), Boeing-Vertol CPT E. TavaresYUH-61A Helicopter MAJ J. Hagen

Model 70-38 Letter Report, Reevaluation of Boelng-Vertol Oct 1971 G. Yamakawa

347 LR Model 347 LTC D. Hendrickson

Model 70-38 Tech Eval Boeing-Vertol Model 347 Advanced Jan 1972 G. Yamakawa 900 263347 Technology Helicopter, Phase I A. Steinmetz

SP4 R. GreenlandLTC D. Hendrickson

Model 72-12 Engineering Flight Test Boeing-Vertol Model Oct 1972 A. Steinmetz 909 933347 347 Advanced Technology Helicopter Phase II SP4 C. Bowers

LTC A. DeelMAJ W. Horton

BOLKOW-MESSERSCHMIDT-BLOHM

(Germany)

BO-105C 74-16 BO-105C Evaluation Jan 1975 CPT M. MatthewsLR

BK-I 17 84-22 Preliminary Airworthiness Evaluation of the Nov 1985 MAJ G. Sharon B105 302LMBB BK-117 Helicopter (Germany/Japan) MAJ E. Tavares

W. Abbott

R. Adler

85

IliLLER AVIATION


OH-5A 63-24/Pt I Report of the Engineering Flight Test of the Aug 1964 R. Turk 909 269OH-5A Helicopter, Unarmed (Clean) and MAJ J. JohnstonArmed with the XM-7 or XM-B Weapon J. BlahaSubsystem, Purl I Stabilitly and Control, J. ReichertUSATECOM Project No. 4-3-0250-31/32/33

OH-5A 63-24/Pt 2 Report of Engineering Flight Test of the OH-5A, Aug 1964 L. Schroers 909 27()

Helicopter Unarmed (Clean) and Armed with CWO E. Nelsonthe XM-7 or XM-8 Weapons Subsystem, Part 11

Performance Phase, USATECOM ProjectNo. 4-3-0250-31/32/33

UH-12E 61-03 High Altitude Evaluation of the Hiller Mar 1961 J. Kidwell 722 82'Model 1961 UH-12E Helicopter MAJ J. Seigler

D. Armstrong

UH-12E 62-07 Evaluation of the Hiller Model UH-12E 1962 J. Kidwell 884 876-4 Helicopter CPT J. Johnston

H-23D 62-03 Qualitative Flight Evaluation of the Torque-Bias, Apr 1962 W. Swope 884 872

Throttle -Governor and Yaw-Damper Systems CPT J. Johnstonfor the Hiller H-23D Helicopter CWO E. Nelson

H-23D 62-04 Evaluation of the SWE-1165 Blade May 1962 R. Finnestead 884 873H-37B TrackerH-21B

lI-23D 63-12 Helicopter Airspeed System Investigation Dec 1962 2LT J. Melton

CPT J. Johnston

McDONNELL DOUGLAS HELICOPTERCOMPANY

(Previously Hughes Helicopter)

OH-6A 63-25/Pt I Report of the Engineering Flight Test Stability Aug 1964 C. Statum 951 591and Control Phase of the OH-6A Helicopter, W. Anderson

Unarmed (Clean) and Armed with the XM-7 orXM-8 Weapon Subsystem, USATECOMProject No. 4-3-0250-51/52/53

OH-6A 63-25/Pt 2 Report of the Engineering Flight Test Perform- Aug 1964 J. Kudirka 951 592

ance Phase of the OH-6A Helicoper Unarmed CPT D. Wray(Clean) and Armed with the XM-7 or XM-8Weapon Subsystem, USATECOM Project

No. 4-3-0250-51/52/53

011-6A 64-31 Final Report of Climatic Hangar Test of the Jul 1965 S. Kennedy 813 ,2

OH-6A Light Observation Helicopter, C. MartinUSATECOM Project No. 4-3-0250-72/80 K. Dorris

86


(Previously Hughes Helicopter)(continued)


OH-6A 65-37 Letter Report, OH-6A XM-27 Army Preliminary Mar 1969 J. Shapley

LR aka Evaluation J. Nagata65-41B

OH-6A 65-37 Engineering Flight Test (Product Improvement Mar 1968 J. Nagata 834 574

aka Test) of Production OH-6A Helicopter Unarmed H. Wolf

65-41 and Armed with the XM-27E1 Weapon System, J. ShapleyPhase D

OH-6A 65-37 Engineering Flight Test of the OH-6A Helicopter Apr 1969 J. Nagata 855 043(Cayuse), Phase D J. Shapley

OH-6A 67-29 Engineering Flight Test of the Production Jul 1969 ILT T. Lane 859 435

OH-6A Helicopter with Fairings Removed MAJ D. WrayM. Buss

OH-6A 68-42 Performance Evaluation of the OH-6A with Jan 1969 ILT T. Lane 847 558

LR Expanded Tolerance Main Rotor Blades J. ShapleyMAJ I. Rundgren

OH-6A 69-09 5.56/7.62MM Weapons Comparative Evaluation Jun 1971 LTC J. Wing 884 980

OH-6A Helicopter V. DiekmannMAJ R. Holasek

OH-6A 70-15-4 Vibration and Temperature Survey Production Aug 1973 E. Laing 914 172OH-6A Helicopter MAJ J. Smith

CW3 J. Hill

OH-6A 71-03 Study, Pilot Perceived Jettison Envelope Jun 1973 A. Winn 768 171

OH-58A J. KishiAH-56A

OH-6A 71-05 Letter Report, Evaluation of Stability and Jan 1974 V. Diekmann

LR Control Test Methods LTC R. Waddell

OH-6A 71-11 Letter Report, Evaluation, AN/APN 171 Oct 1971 J. Watts

LR Radar Altimeter S. Streutker

OH-6A 72-06 Instrument Flight Evaluation OH-6A Nov 1973 A. Winn 780 016Helicopter, Part I LTC W. Griffith

MAJ C. Mittag

OH-6A 72-06 Flight Evaluation, OH-6A Helicopter Kaiser Feb 1973 A. Winn 781 990

FP-50B Flight Director System, Part I! LTC W. GriffithMAJ C. Mittag

OH-6A 72-21 OH-6A/Bifurcated Exhaust Duct Jul 1972 MAJ R. Chaplin

LR T. Benson

OH-6A 72-28 Engineering Flight Test OH-6A Helicopter Aug 1973 SP4 R. Anderson 913 954

with Cambered Tail Rotor Blades and Pedal LTC R. WaddellForce Compensators

87




01-6A 72-32 OH-6A Autorotational Evaluation Nov 1972 MAJ W. Griffith

LR R. McClellan

OH-6A 81-04 Airworthiness and Flight Characteristics Test Nov 1983 CW3 J. Webre A161 255of the OH-6A Configured to a Light Combat CPT E. MarshallHelicopter (JOH-6A LCH) R. Woratschek

R. Adler

JOH-6A 83-05 Airworthiness and Flight Characteristics Test Nov 1983 CW3 J. Webreof the JOH-6A Light Combat Helicopter CPT E. Mitchell

Configured with a Wire Strike Protection System R. WoratschekR. Adler

OH-6A 83-08 Letter of Effort, Government Pilot Evaluation Jun 1983 MAJ R. OliverLOE OH-6A/NOTAR D. Belte

MH-6E 83-07 MH-6E Extended Pilot Tube Modification Aug 83 MAJ R. OliverCalibration and Evaluation MAJ L. Todd

MAJ A. Marshall

MH-6E 84-05 Report, Preliminary Airworthiness Evaluation Sep 84 CW4 J. WebreI.R Test of MH-6E with light Weight Airborne MAJ R. Oliver

FLIR System (LAFS) Installed R. WoratschekR. Adler

N'I I-6A 64-44 Continued Flight Test of the YOH-6A Helicopter, May 1967 F. Dominick A951 S IUSATECOM Project No. 4-3-0250-78 J. Walls

YOH-6A 65-11 Letter Report of Engineering Test of YOH-6A Jun 1966 D. MacphersonLR Helicopter in the Desert Environment, USATECOM

Project No. 4-3-0250-75

OH-6C 71-34 Army Preliminary Evaluation, Prototype Hughes. Feb 1972 G. Skinner 901 268Model 369C (OH-6C) Helicopter R. McClellan

LTC A. Deel

TH-55A 67-22 Engineering Flight Test TH-55A Primary Nov 1969 CPT S. Schwartz 864 071Helicopter Trainer Limited Performance MAJ D. WrayEvaluation

TH-55A 70-24 Autorotational Entry Improvement Program Dec 1972 B. Boirun 908 657TH-55A Helicopter LTC W. Benoit

AH-64 84-10 First Article Preprouction Test of the AH-64 Nov 1984 G. Bener

Helicopter MAJ J. VossMAJ R. MacMullinCW4 J. Adkins

AFf-64 84-23 Report, Artificial and Natual Icing Tests of the Sep 1985 CW4 J. Adkins

L1 AH-64 R. Woratschek

AH-64 84-23 Report, Artificial and Natural Icing Tests of the Jul 1986 CW4 J. Adkins(Phasell) LR AH-64 (Phase II) R. Woratschek

88



Aircrart Project AdType Number Report Title Date Author(s) Numrhc

A1"[-64 84-23 Artificial and Natural Icing Tests of AH-64 Mar 1987 CW4 J. Adkins A188 231(Phase 11) R. Woratschek

AH-64 85-08 Engine/Airframe Response Evaluation of the Jun 1984 CW4 J. AdkinsAH-64 Helicopter 0. Bender

MAJ J. Correia

AH-64 85-18 Engine/Airframe Response Evaluation of the Nov 1985 CW4 J. AdkinsAH-64 Helicopter G. Bender

MAJ J. Correia

AH-64A 84-08 Letter of Effort, T-28 High Speed Pace Support Jul 1984 J. JohnsonLOE for the AH-64A

YAH-64 74-07-2 Development Test 1 Advanced Attack Helicopter Dec 1976 MAJ R. Stewart A109 532Competitive Evaluation Hughes YAH-64 MAJ R. TarrHelicopter LT M. Hill

B. BoirunT. BensonE. BailesW. Abbott

YA11-64 77-36 Engineering Design Test I, Hughes YAH-64 Sep 1978 MAJ R. Tarr A064 351)Advanced Attack lVelicopter V. Diekmann

MAJ R. StewartP. Woratschek

YAH-64 78-23 Engineer Design Test 2 Hughes YAH-64 Jun 1979 V. Diekmann A098 923Advanced Attack Helicopter T. Benson

R. WoratschekS. SnakenbergMAJ R. TarrMAJ P. MoeCW3 R. Williams

YAH-64 80-03 Engineeing Development Test 4, YAH-64 Jan 1980 G. Bender A098 922Advanced Attack Helicopter MAJ B. Picasso

MA L. HigginsV. DiekmannD. Ottomeyer

YAH-64 80-12 Engineer Design Test, Government EDT-5 Mar 1981 MAJ P. MorrisLR of the Advanced Attac- Helicopter (AAH) D. Ottomeyer

Helicopter (LCH)

YAH-64 80-07 Climatic Laboratory Survey, Hughes Mar 1982 G. Bender A124 6701CPT R. SavageR. Adler

YAH-64 80-08 YAH-64 Icing Survey Sep 1982 MAJ M. Hanks

89



Aircraft Project AdT'ypc Number Report Title Date Author(s) Nimtwr

YAII-64 80-17-1 Airworthiness and Flight Characteristics Test, Sep 1981 MAJ P. MorrisPart 1, YAH-64 Attack Helicopter J. Ottomeyer

MAJ L. HigginsMAJ B. PicassoCPT R. SavageG. Bender

YAH-64 80-17-2 Airworthiness and Flight Characteristics Test, Feb 1982 MAJ B. Picasso A125 270Pat 2, YAH-64, Advanced Attack Helicopter R. Buckanin

J. OttomeyerMAJ G. Downs

YAH-64 80-17-3 Airworthiness and Flight Characteristics Test, Oct 1982 MAJ B. PicassoPart 3, YAH-64 Advanced Attack Helicopter, R. BuckaninPrototype Qualification Test M, Herbst

MAJ G. Downs

Hughes 79-22 Potential Airworthiness Evaluation of the Jul 1980 MAJ B. Picasso500D LR Hughes 500D CW4 J. Tulloch

G. BenderD. Ottomeyer

Model 80--18 Memo for Record, Preliminary Airworthiness Feb 1981 CW4 R. Wiliais500D LR Evaluation (PAE), of Hughes Helicoplers (HH) W. Norton

5GOMD Modified to a Light Combat Helicopter R. Buckanin(LCH)

KAMAN AEROSPACECORPORATION

UH-2B65-31 Engineering Flight Evaluation of UH-2B Mar 1966 J. Johnson 951 585Armed Helicopter, USATECOM Project W. Anderson No. 4-6-0300-01

90


Aircraft Project AdType Number Report Title Date Author(s) Numcr

AH-56A 70-02 Army Preliminary Evaluation I and Research Mar 1972 F. Dominick 905 91oaka and Development Acceptance Test I, G. Bender

71-17 AH-56A Cheyenne Compound Helicopter LTC G. HallR. McClellan

MAJ P. StringerM. Buss

AH-56A 71-03 Study, Pilot Perceived Jettison Envelope Jun 1973 A. Winn 768 121OH-58AOH-6A

AH-56A 72-08 Attack Helicopter EvaluationJ AH-56A Jun 1972 J. Johnson 771 914Cheyenne Compound Helicopter G. Bender

R. McClellan

MAJ J. BurdenCPT M. Larsen

AH-56A 72-44 Engineering Evaluation AH-56A Compound Mar 1973 J. Johnson 910 262Helicopter with Advanced Mechanical G. BenderControl System MAJ J. Burden

PIASECKI AIRCRAFTCORPORATION

H-21B 62-04 Evaluation of the SWE-1165 Blade Tracker May 1962 R. Finnestead 884-873H-23DH-37B

ROTORWAY INC.

Scorpion 70-43 Evaluation of the Scorpion Helicopter Mar 1972 MAJ R. ChaplinLR MAJ J. Alvis

91

SIKORSKY AIRCRAFT DIVISION OFUNITED TECHNOLOGIES

CORPORATION


11-34 62-09 H-34 Helicopter 50-Caliber Machine-Gun Oct 1962 J. Kidwell 951 582Gun Kit Calibration CWO E. Nelson

11-37 62-02 Drop Test Evaluation of Mark Xli Auxiliary Feb 1962 2LT J. Melton 884 871Torso Fuel Tank MAJ E. Kleuver

11-37B 62-04 Evaluation of the SWE-1165 Blade Tracker May 1962 R. Finnestead 884 873lt-23DHl-21B

Ci-37B 62-28 Final Report Engineering Test of the CH-37B Mar 1965 R. Turk 884 897CWO J. Watts

Cl 1-37B 64-05 Final Report, USATECOM Project No. Apr 1964 R. Turk 951 5894-4-0180-01, Engineering Flight Tests of the CWO J. WattsCH-37B

CH-53 83-29 Letter of Effort for Support of Marine CH-53 Apr 1984 LTC R. WardLOE Icing Test

CH-54B 70-15-3 Vibration and Temperature Survey CH-54B Mar 1973 E. Laing 910 495Helicopter MAJ R. Merrill

CW4 J. Reid

CH-54B 71-01 Letter Report, Qualitative Evaluation of Aug 1971 J. WattsLR Instrument Flying Qualities of the CH-54B MAJ J. Henderson

Helicopter

CII-54B 71-01 Instrument-Flight-Rules Capability Evaluation Dec 1972 E. Bailes 908 658CH-54B (TARHE) Helicopter V. Diekmann

J. WattsMAJ J. Henderson

CII-54B 72-40 Limited Performance Tests CH-54B (TARHE) Feb 1973 J. Johnson 910 263Helicopter V. Diekmann

SP4 J. JohnsonMAJ R. MerrillCW4 J. Reid

EH-60A 87-06 Report, Preliminary Airwortiness Evalautlion of Apr 1987 CW4 R. MurrellLR the EH-60A CW4 J. Webre

M. Herbst

YEI--60B 87-16 Report, Preliminary Airworthiness Evaluation of Oct 1987 CW4 J. WebreI)LTA IR the EH-60 DELTA CPT D. Downey

F. Dominick

EIt-60A 87-09 Report, Secure Test Site Support of the EH-60A Apr 1987 LTC D. UnderwoodLR

EH-60A 87-09 Preliminary Airworthiess Evaluation of the Sep 1987LR EH-60A Aircraft in a Low Drag Configuration

92

AtD-A207 464 U S ARMV FAVIA1 ENGINEERAhG FLIGHT #tl~t (R~REPORT BIBLIOGRAPHY R(U)AARMYAAVIATION ENGINEERING .FLIGHT ACTIVITY EDWIADS AFB CA S LEW~IS ET AL APR 8

iUNCLASSIFIED F/G 5/2 N

La~ U

liii, . I LS

11111L2 ..6'IH1 12511111. UIII 1.6

MICROCOPY RESOLUTION TEST CHARTNATIONAL BUREAU Of STANDAROS-1963 A


CORPORATION(continued)


HH-60A 86-02 Engine/Airframe Response Evaluation of the Oct 1986 G. Bender A184 443HH-60A Helicopter Equipped with the T700-GE-701 CW4 J. AdklnsTransient Droop Improvement Electonic Control MAJ R. LockwoodUnit

SH-60B 84-20 Letter of Effort for Support of Navy SH-60B Feb 1985 MAJ E TavaresLOE Icing Test

SH-60B 85-20 Letter of Effort for Support of Navy SH-60B May 1986 MAJ T. ReynoldsLOE Icing Test

UH-60 82-14 Preliminary Airworthiness Evaluation UH-60 Mar 83 MAJ A. Marshall i32 964Configured with External Stores Support System R. Buckanin(ESSS) MAJ R. Oliver

R. Adler

UH-60 83-17 Preliminary Airworthiness Evaluation of the Aug 1983 CW3 J. MiessUH-60 Helicopter with T700-GE-701A Engine CPT L. HaworthInstalled

UH-60 84-07 Report, Preliminary Airworthiness Evaluation of Aug 1984 R. RobbinsLR the UH-60A With Light Weight Airborne R. Woratschek

Forward Looking Infrared (FLIR) System (LAFS) CPT R. ReynoldsInstalled

UH-60A 77-17 Airworthiness and Flight Characteristics Sep 1981 J. NagataEvaluation UH-60A (Black Hawk) Helicopter G. Skinner

R. BuckaninR. RobbinsCW4 R. Williams

UH-60A 77-17-3 Letter Report UH-60A Aft CG Aug 1980 CPT M. HanksLR MAJ B. Picasso

J. NiemannK. Flaig

UH-60A 77-17-5 Report, Experimental Testing of the UH-60A Nov 1981 R. BuckaninLR Black Hawk Helicopter at HeavyG ross Weight MAJ R. Robbins

and Extended Forward Center of Gravity MAJ J. BensonCPT R. Vincent

UH-60A 77-23 Production Validation Test Government (PVT-G) Oct 1979 G. Yamakawa B050 426Performance Guarantees UH-60A Black Hawk G. BenderHelicopter R. Buckanin

CPT R. RobbinsE. BailesCW4 J. Tulloch

UH-60A 78-01 UH-60A Command Instrument System Mar 1978 LTC W. GriffithLR Preliminary Evaluation MAJ R. Stewart

UH-60A 78-05 Letter Report, Artificial and Natura licing Oct 1979 CW4 J. TullochLR Tests Production UH-60A LTC G. Mullen

D. Belle

93




UII-60A 78-22 Preliminary Airworthiness Evaluation IfI Apt 1979 J. NagataLR UH-60A Black Hawk Helicopter CW4 J. Bishop

CW3 R. WilliamsG. Skinner

UH-60A 79-11 Letter Report Preliminary Airworthiness Dec 1979 J. NagataLR Evaluation (PAE) liA, UH-60A Helicopter LTC G. Mullen

with the Infrared (IR) Reduction Subsystem CW3 R. WilliamsG. Skinner

UH-60A 79-19 Artificial and "latural Icing Tests Production Jun 1980 CPT M. Hanks A090 527UH-60A Helicopter MAJ L. Higgins A096 239

V. Diekmann

UH-60A 79-24 Validation Flight Test of UH-60A for Rotorcraft Sep 1982 W. AbbottSystems Integration Simulator (RSIS) MAJ J. Benson

CPT R. OliverCW4 R. Williams

UH-60A 79-24-1 Report Flight Evaluation of UH-60 with the Dec 1981 G. SkinnerLR Roll Trim Actuator Disconnected MAJ J. Benson

D. Macpherson

UII-60A 80-14 Limited Artificial and Natural Icing Tests Aug 1981 MAJ M. Hanks Al 12 582Production UH-60A Helicopter (Re-evaluation) V. Diekmannn

MAJ J. Benson

UH-60A 81-16 UH-60A Expanded Gross Weight and Center Aug 1985 R. Buckaninof Gravity Evaluation M. Herbst

MAJ R. MacMullinCW4 J. MiessG. SkinnerMAJ E. TavaresCW4 R. Williams

UH-60A 81-18 UH-60A Light Icing Envelopes Evaluation with Jun 1982 R. Robbins A125 630Deicing Kit Installd but Inoperative

UH-60A 81-20 Report, UH-60A Engine and APU Exhaust Gas Dec 1981LR Temperature Survey

UH-60A 82-03 Letter of Effort for Support of the UH-60A/ May 1982 MAJ A. MarshallLOE C-130 Air Refueling Proximity Test

UH-60A 82-09 Preliminary Airworthiness Evaluation of Apr 1983 CPT R. MacMullin A148 676UH-60A with an Improved Airspeed System G. Skinner

MAJ M. Hanks

UH-60A 82-11 Preliminary Airworthiness Evaluation of UH-60A Oct 1982 CPT R. OliverLR Pilot and Copilot Cockpit Doors Removed CPT A. Marshall

94




UH-60A 82-15 Airworthiness and Flight Characteristics of the Dec 1983 MAJ A. MarshallUH-60A Configured with the Prototype External MAJ R. OliverStores Support System (ESSS) J. Nagata

C. Cassil

UH-60A 82-15-1 UH-60A External Stores Support System Fixed MAy 1984 CW4 R. Williams A147 188Provisions Fairings Drag Determination CPT R. MacMullin

CW4 J. Miess

R. Buckanin

G. SkinnerW. Abbott

UH-60A 83-02 Test Witness Report, UH-60A ESSS External Apr 1983 MAJ G. DownsTWR Stores Separation Flight Test

UH-60A 83-09 Report, UH-60A Engineering Flight Support for Apr 1984 W. AbbottLR Simulation Validation

UH-60A 83-10 Test Witness Report, ESSS, M-56 Helicopter May 1983 CPT F. StellarTWR Mine Dispensing Subsystem Flight Test

UH-60A 83-10-1 Test Witness Report, ESSS, External Stores Jun 1983 MAJ A. MarshallTWR Separation Flight Test

UH-60A 83-22 Limited Artificial and Natural Icing Tests of Jun 1984 MAJ M. Hanksthe External Stores Support System (ESSS) R. WoratschekInstalled on a UH-60A Aircraft

UH-60A 83-24 Airworthiness and Flight Characteristics Test of Jun 1985 MAJ A. Marshall A180 181a Sixth Year Production UH-60A MAJ R. MacMullin

MAJ R. LockwoodMAJ T. ReynoldsMAJ E. TavaresR. Buckanin

G. SkinnerM. HerbstC. CassilCW4 P. Sullivan

CW4 R. Williams

UH-60A 84-17 Report, Infrared Measurement Test of the Sep 1984 MAJ E. TavaresLR UH-60A Helicopter with Garret AiResearch

Infrared Suppressor System Installed

UH-60A 84-28 Flight Evalaution of the UH-60A Helicopter with Sep 1986 CW4 R. Murrell A183 954the Pitch Bias Actuator Centered and Electrically MAJ R. LockwoodDisconnected CW4 R. Williams

M. HerbstG. SkinnerCPT D. Cripps

95




UH-60A 86-01 Level Flight Performance Evaluation of the Sep 1986 R. BuckaninUH-60A Helicopter with the Production External W. KellyStores Support System and Ferry Tanks Instaled CW4 J. Webre

MAI T. ReynoldsMAJ R. LockwoodCPT R. Cason

UH-60A 86-05 Preliminary Airworthiness Evaluation of the Aug 1987 G. BenderUH-60A with Advanced Digital Optical Control R. RobbinsSystem (ADOCS)

UFI--60A 86-10 Preliminary Airworthiness Evaluation of the Aug 1987 MAJ T. Reynolds A190 604UH-60A Equipped with the XM-139 VOLCANO J. NagataMine Dispensing System MAJ R. Cason

D. Belle

Ull-60A 86-14 Airworthiness and Flight Characteristics Test Aug 1987 MAJ R. Cason A191 414of a Ski Assembly for the UH-60A Black Hawk J. NagataHelicopter MAJ T. Reynolds

D. Belte

UH-60A 86-19 Test Witness Report, UH-60A VOLCANO Jan 1987 MAJ T. ReynoldsTWR Jettison Test

UH-60A 86-21 Letter of Effort for UH-60 Flight Simulator Dec 1986 CW4 R. MurrellEvaluation

UH-60A 86-25 Preliminary Airworthiness Evaluation of the Oct 1987 D. BelteUH-60/ESSS with HELLFIRE Launcher CPT T. WalshInstalled MAJ T. Reynolds

MAJ P. LosierMA R. Cason

UHI-60A 87-23 Report, Evaluation of the UH-60A Cyclic Sep 1987 CW4 R. MurrellLR Stabilator Slew Switch

UII-60A 87-23 Report, EH-60A Stabilator Evaluation, adjunct Apr 1988 CPT D. CrippsLR to AEFA Project No. 87-23

YEII-60A 82-19 Letter of Effort, Transmittal of Selected Aug 1984 G. SkinnerLOE Vibration Date of the YEH-60A Quick Fix System MAJ E. Tavares

CW4 R. WilliamsCPT G Bishop

YEH-60A 83-20 Limited Airworthiness and Flight Characteristics Oct 1984 0. Skinner(A&FC) Test of the Quick Fix Configuration CPT G. Bishop

MAJ E. TavaresCW4 R. Murrell

YEH-60A 83-21 Artificial and Natural Icing Tests YEH-60A Jun 1984 MAJ E TavaresQuick Fix Helicopter CW3 P. Sullivan

MAJ M. HanksR. Woratschek

96




YEH-60B 82-17 Report, Preliminary Airworthiness Evalaution, Feb 1983 CW3 J. WebreLR YEH-60B with AN/ASN-132 Integrated J. Nagata

Navigation System Installed MAJ J. Brown

UHI-60A 84-29 Report, Evaluation of Solar Heating of UH-60A Nov 1984 MAJ J. VossLR Fuselage Skin CPT G. Bishop

MAJ T. ReynoldsCPT R. LockwoodCPT W. Carmona

CW4 P. Sullivan

UH-60A 85-02 Test Witness Report, Continuation of UH-60A Apr 1985 MAJ T. ReynoldsTWR ESSS, External Stores Separation Test

UH-60A 85-07 Flight Characteristics Test of the UH-60A with Oct 1986 MAJ R. Lockwood A180 791Tail Boom Mounted Strake W. Kelly

MAJ R. Cason

UH-60A 85-14 Report, Phase I! Evaluation of Solar Heating of Dec 1986 MAJ R. CasonLR UH-60A Fuselage Skin (High Temperature W. Kelly

Testing)

UH-60A 85-15 Rotor System Evalaution, Phase I Mar 1988 R. BuckaninW. GouldMAJ P. LosierCPT D. DowneyMAJ R. LockwoodCW4 J. WebreCOL J. HagenMAJ R. CasonC. Young

UH-60A 85-21 Test Witness Report, UH-60A HELLFIRE Jan 1986 MAJ T. Reynolds

TWR Jettison Test

UH-60A 85-22 Report, Evaluation of the Light Helicopter Family Jan 1986 J. Nagata

LR (LHX) Specification Demonstration Maneuvers MAJ R. LockwoodCPT G. Bishop

CW4 R. WilliamsCW4 R. MurrellW. KellyT. Griffin

YUH-60A 74-06-1 Government Competitive Test, Utility Tactical Nov 1976 J. Nagata B059 738LTransport Aircraft System (UTTAS) Sikorsky, G. SkinnerYUH-60A Helicopter S. Kolwey

R. BuckaninMAJ C. MittagLCdr M. CoumatosCW3 J. Meiss

97

SIKORSKY AIRCRAFT DIVISION OFUNITED TECIINOLOGIES



YUH-60A 75-12-1 Climatic Laboratory Evaluation, Utility Tactical Jul 1977 MAJ R. Ward R033 049!LTransport Aircraft System (UTTAS) Sikorsky, J. GivensYUH-60A Ground Test Vehicle E. Walbey

CW4 R. Scefeldt

YUH-60A 76-09-1 Artificial Icing Test, Utility Tactical Transport Feb 1977 R. Buckanin A109 530Aircraft System (UTTAS), Sikorsky YUH-60A CW4 J. Tulloch

YUH-60A 77-18 Preliminary Airworthiness Evaluation, YUH-60A Jan 1978 A. WinnBlack Hawk Helicopter with Electronic Flight MAJ C. MittagControl System CW4 J. Bishop

J. Nagata

YUH-60A 78-11 Preliminary Airworthiness Evaluation IIA Dec 1978 CW4 J. BishopLR YUH-60A Helicopter with Production Avionics, CPT T. Burch

Electronic Flight Control System and Command CW3 R. WilliamsInstrument Systems

S-61 65-27 Engineering Evaluation of S-61 Armed Mar 1966 D. MacphersonHelicopter J. Watts

S-67 72-09 Attack Helicopter Evaluation Blackhawk S-67 Jul 1972 G. Yamakawa 771 161Helicopter A. Wlnn

R. SmithSP4 R. Anderson

MAJ W. GriffithMAJ W. Horton

S-67 72-26 Attack Helicopter High-Altitude Evaluation Jul 1972 G. Yamakawa 771 051Blackhawk S-67 Helicopter A. Winn

MAJ W. Horton

S-76 81-15 Letter of Effort for Support of United Apr 1982 LTC R. WardLOE Technologies Corporation, Sikorsky Aircraft

Division, Icing Certification Effort of the S-76Helicopter

98

MISCELLANEOUS


61-04 Limited Cold Weather Evaluation of Multi- Jun 1961 A. Ruddell 884 882Purpose Ground Service Unit Model 2100-5

61-05 Evaluation of the Republic Electronic Industries Jul 1961 CWO D. Scott 884 881Pitot and Static System Tester

61-08 Evaluation of the Aerosonic Corporation Pilot Nov 1961 CWO D. Scott 884 889and Static System Tester

61-09 Evaluation of the North American Aviation 1961 W. Swope 884 885Inc. Dynamic Flight Simulation

61-10 Evaluation of the North American Aviation 1961 W. Swope 884 8L)0Inc. Visual Presentation Flight Simulator

62-06 Evaluation of the Helicopter Load and Hovering May 1962 W. Golyer 884 875Computer A. Higgins

65-46 A Note on Rotary Wing Hovering and Takeoff 1965 J. KidwellPerformance, Data Acquisition and Analysis

68-49 Letter Report, Evaluation, High-Speed Swivel- Apr 1971 E. BailesLR Head Pilot Probe

70-16 Interim Report, Comparison of VSTOL Sep 1970LR Specification to Helicopter Flight Test Data

70-17 A Portable Instrumentation Kit Feasibility Study Jun 1972 R. Jefferis 751 188W. Rivers

70-19 Letter Report, Advanced Instrumentation and Mar 1972 V. DiekmannLR Data Analysis System Demonstration

71-32 Utility Tactical Transport Aircraft System Apr 1972 G. Yamakawa 902 767(UTTAS) Maneuvear Criteria MAJ G. Broadhurst

MAJ J. Smith

73-71 Minutes of AVSCOM Helicopter IFR Conference Jan 1973

74-77 Rotary Wing Icing Symposium Summary Jun 1974 COL D. WrightReport CommanderVolume I A061 445

Volume II A061 422Volume III A061 423

74-87 Flight Evaluation of Non-Dimensional Static- Jul 1979 B. Boirun A082 831Longitudinal Stability Test Methods K. Ferrell

MAJ J. Jenks

74-94 An Advanced Instrumentation and Data Jul 1973 R. Lewis 882 771Analysis System for Army Flight Testing SlDX

75-28 Letter of Effort, Phase II of Joint Acoustics Jan 1976 CPT J. ArnoldLOE Test Program with AMRDL/AMES

99

MISCELLANEOUS

(continued)


77-02 Temperature Effects of Sunlight on Helicopter Feb 1977 MAJ M. MathewsLR Rotor Blades

77-14 Letter of Effort, Lightweight Launcher Vibration Jun 1977 MAJ C. ThomasLR Study T. Benson

MAJ P. Moe

81-01-6 Fuel Conservation Evaluation of US Army, Jul 1986 F. DominickPart 6, Performance Calculator Evaluation MAJ R. Lockwood

81-12 Preliminary Airworthiness Evaluation System Jun 1982 MAJ D. Underwood B073 268Platform II Individual Lift Device (ILD) J. Nagata

81-90 US Army Aviation Engineering Flight Activity Jun 1982 K. Ferrell A129 859(USAAEFA) Report Bibliography I. Tucker

81-90-1 US Army Aviation Engineering Flight Activity Mar 1984 K. Ferrell(USAAEFA) Report Bibliography Update 1981-1982 1. Tucker

82-05-2 Report, Helicopter Icing Spra System (HISS) Oct 1985 D. BelieLR Evaluation and Improvements

84-03 Letter of Effort, Test Pilot Support for Scout/ Mar 1984 MAJ A. MarshallLOE Attack Helicopter Simulation Study Simulator

84-30 Letter of Effort, Evaluation of the MCT Jul 1986 K. FerrellLOE ROTORTUNER

84-90 US Army Aviation Engineering Flight Activity Jan 1985 1. Tucker(USAAEFA) Report Bibliography 1983-1984 M.A. Lake

K. Ferrell

85-19 Letter of Effort, Advanced Digital-Optical Dec 1985 CW4 R. Williams

Control System (ADOCS) Single Pilot Simulator CW4 J. Webre

85-25 Letter of Effort, Test Pilot Support for NASA- Mar 1986 MAJ G. SharonLOE Ames Simulation of LHX Tyne Handling MAJ F. Stellar

Qualities

86-04 Letter of Effort, Test Pilot Support for NASA- Jul 1986 CW4 J. WebreLOE Ames Single-Pilot Advanced Cockpit Engineering MAJ T. Reynolds

Simulation (SPACES) Evaluation LTC D. UnderwoodCPT R. Cason

87-03 Letter of Effort, Aviation Engineering Flight Jul 1987 CW4 J. LyleLOE Activity Participation in Air-to-Air Combat

Test IV (AACT IV)

87-10 Report, Technology Flight Evaluation of the Jun 1987 CPT D. DowneyLR NOTAR Anti-Torque System COL A. Todd

C. Cassil

87-28 Letter of Effort for Joint NASA-Lewis/U.S. Aug 1988 R. RobbinsArmy Aviation Engineering Flight Activity D. BelieIcing Flight Research

100

MISCELLANEOUS(continued)

Aircrart Project AdType Number Report Title Date Author(s) Number

88-07 Letter of Effort, Support to the U.S. Naval Jun 1988 MAJ T. WallaceAir Test Center Evaluation of an AcousticAir Data Sensor Device (Mini-SODAR)

88-09 Letter of Effort, IR Imager Support to Naval Jun 1988 MAJ T. WallaceLOE Weapons Test Center (NWC)

88-12 Report, Pilot Support of Adaptive Fuel Control Sep 1988 MAJ J. LawrenceLOE Development Flight Tests R. Buckanin

88-12 Report, Pilot Support of Adaptive Fuel Control Aug 1988 MAJ J. LawrenceLR Development Flight Tests R. Buckanin

88-18 Letter of Effort, Support to the USAF Space Nov 1988 CPT M. WhiteLOE Test Office, Militaty Man in Space (MMIS) MAJ T. Wallace

Equipment and Procedures Evaluation

101

APPENDIX A

Quick Reference List of Aircraft By Contractor

FIXED WING

BEECH AIRCRAFT' ROTEC ENGINEERING, INC.Rally Ultralight

T-34T-4 2 RYAN AERONAUTICAL CORP.U-8 XV-5AU2-21Model 300 RUTAN AIRCRAFT FACTORY INC.C-i 12 LONG-EZRC- 12

SCHWEIZER AIRCRAFT CORPORATIONBELL HELICOPTER CORP SA 2-37A

XV-3 TG-8A

BREGUET AVIATIONModel 941

CANADAIR, LTDCL-215

CESSNA AIRCRAFT CO.L- 190-2A

DeHAVILLAND AIRCRAFTCV-2CV-7U-6

GRUMMAN CORPOV- ITBM-3TS-2A

LOCKHED CORPORATIONYO-3

NORTH AMERICAN AVIATIONTB-25F-5 1

P1 LATUSqPC-6A

102

BELL HELICOPTER TEXTRON ROTORWAY INC.AH-1 ScorpionUH-1H-13 SIKORSKY AIRCRAFTOH-58 H-34AH-63 H-37EH-IX CH-54JOH-8A UH-60Model 47G3 EH-60Model 47J2 HH-60Model 205A S-61Model 206 S-67Model 209 S-76Model 211 SH-60BModel 214Model 222Model 249Model 309

BOEING VERTOL CO.CH-47UH-1Model 347

BOLKOW-MESSERSCHMITT-BLOHMBO-105BK- 117

HILLER AVIATIONOH-5UH-12H-23

McDONNELL DOUGLAS HELICOPTER CORPORATIONOH-6TH-55AH-64MH-6EModel 500

KAMAN AEROSPACE CORP.UH-2B

LOCKHEED CORPORATIONAH-56

PIASECKI AIRCRAFT CORPORATIONH-21

103

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