voted #1 fbo in the southeast - n7jw status reportpiaggio aero p180 avanti ii status report m.m....

PIAGGIO AERO P180 AVANTI II Status Report M.M. TR-131

Current Date 9-Jan-14 Hobbs: 891.7Aircraft Total Time 891.7 24-Sep-08Total Landings 526 P180 IIAPU Hours N/A 1169 APU Cycles N/A#1 Engine Time Since New 891.7#2 Engine Time Since New 891.7#1 Engine Cycles Since New 521 #2 Engine Cycles Since New 521 #1 Propeller Time Since New 891.7#2 Propeller Time Since New 891.7

HRS CYS Months HRS CYS Date HRS CYS CAL HRS CYS CAL200 hr Inspection 200 891.7 526 9-Jan-14 1091.7 200"B" CHECK 600 711.9 1311.9 420"C" CHECK 1500 0 1500 608"D" CHECK 3000 0 3000 2108

UNDERWATER ACOUSTIC BEACON DUKANE DK120 - CLEAN AND PERFORM BATTERY CHECK 6 9-Jan-14BATTERY (INSPECT FOR SPEWAGE) 6 9-Jan-14 9-Jul-14 181EMERGENCY POWER UNIT-CAPACITY TEST 6 9-Jan-14 9-Jul-14 181ELT (AF) TYPE 503 - TECHTEST FUNCTIONAL TEST 6 N/A N/A N/AUNDERWATER ACOUSTIC BEACON DUKANE DK100 (IF INSTALLED) - CLEAN AND PERFORM BATTERY CHECK 6 24-Sep-08FIRST AID KIT 6 9-Jan-14 9-Jul-14 181STAND BY INSTRUMENT ISI GH3100 6 1-Sep-14 1-Mar-15 416SMOKE GOGGLES - INSPECT 6 N/A

FUSELAGE BELLY - DRAIN 12 9-Jan-14 9-Jan-15 365AIRPLANE I.D. PLATE - CONDITION 12 9-Jan-14 9-Jan-15 365EXTERIOR PLACARDS, DECALS AND MARKINGS - CONDITION 12 9-Jan-14 9-Jan-15 365

#1 Prop Model: HC-E5N-3A, S/N: KU119#2 Prop Model: HC-E5N-3AL, S/N: HF259

PROGRAM

NOT APPLICABLE EQUIPMENT NOT INSTALLED

CHAPTER 05-20-00 / INSPECTION PROGRAM

DESCRIPTIONREMAINING

6 MONTH INSPECTION REQUIREMENTS

1 YEAR INSPECTION REQUIREMENTS

DAILY INSPECTION (TEMPORARY RIVISION NO. 063, DATED MAY 05, 2010


AWC IssuedAircraft Model

Aircraft Serial No.

#1 Eng. Model: PT6A-66B, PCE-RW0066

NEXT COMPLIANCELAST COMPLIANCE


DAILY INSPECTION CONSISTS OF THE PREFLIGHT CHECK AND THE AFTER SHUTDOWN CHECKS, AS PRESCRIBED IN THE CURRENT ISSUE OF THE PILOT'S OPERATING HANDBOOK AND AIRPLANE FLIGHT MANUAL

180-MAN-0200-01105 REV. B3 03/21/12


1 - 26Prepared by: Paul J. Baran

Inspector



HRS CYS Months HRS CYS Date HRS CYS CAL HRS CYS CAL


PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

INTERIOR PLACARDS AND DECALS - CONDITION 12 9-Jan-14 9-Jan-15 365BLEED AIR DUCTS LEAKAGE MONITORING SYSTEM - FUNCTIONAL CHECK

12 9-Jan-14 9-Jan-15 365AUTOPILOT SYSTEM - INSPECT FOR CONDITION CONDITION AND SECURITY. 12 9-Jan-14 9-Jan-15 365ANTENNAS - INSPECT FOR CONDITION CONDITION AND SECURITY. 12 9-Jan-14 9-Jan-15 365GROUND FAULT INTERRUPTER (if applicable) TEST THROUGH "TEST GFI" BUTTON ON THE UNIT 12 9-Jan-14 9-Jan-15 365 BATTERY INSTALLATION INSPECTION AND TEMPERATURE INDICATION OPERATIONAL TEST (MFD) 12 9-Jan-14 9-Jan-15 365STARTER/GENERATOR AIR COOLING DUCTS - CONDITION 12 9-Jan-14 9-Jan-15 365CABIN AND FLIGHT COMPARTMENT INSPECTION - CLEANLINESS 12 9-Jan-14 9-Jan-15 365FLIGHT, CABIN AND BAGGAGE COMPARTMENT - CONDITION 12 9-Jan-14 9-Jan-15 365ELT (AF) C406-N ARTEX FUNCTIONAL TEST 6 9-Jan-14 9-Jul-14 181FIRE EXTINGUISHER ELECTRICAL CIRCUIT (if installed) CONTINUITY CHECK 12 9-Jan-14 9-Jan-15 365FIRE EXTINGUISHER BOTTLES (if installed) VISUAL INSPECTION 12 9-Jan-14 9-Jan-15 365


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

PORTABLE FIRE EXTINGUISHER (if installed) (AIRCRAFT S/N 1105 AND SUBSEQUENT - VISUAL INSPECTION 12 9-Jan-14 9-Jan-15 365FLIGHT CONTROLS - OPERATION 12 9-Jan-14 9-Jan-15 365ANGLE OF ATTACK TRANSMITTER - CLEANLINESS 12 9-Jan-14 9-Jan-15 365HORIZONTAL STABILIZER TRIM SYSTEM -OPERATIONAL CHECK 12 9-Jan-14 9-Jan-15 365FLAP SYSTEM - OPERATIONAL TEST 12 9-Jan-14 9-Jan-15 365FORWARD WING FLAP ACTUATORS AND FITTINGS 12 9-Jan-14 9-Jan-15 365FORWARD WING FLAP FITTINGS 12 9-Jan-14 9-Jan-15 365FORWARD WING FLAPS AND SUPPORT FITTINGS 12 9-Jan-14 9-Jan-15 365HYDRAULIC PRESSUIZATION LINES 12 9-Jan-14 9-Jan-15 365NACELLE AIR INTAKE VANES - VISUAL INSPECTION 12 9-Jan-14 9-Jan-15 365LANDING GEAR - OPERATIONAL TEST 12 9-Jan-14 9-Jan-15 365LANDING GEAR - PERFORM HAND PUMP GEAR EXTENSION 12 9-Jan-14 9-Jan-15 365LANDING GEAR - LUBRICATION 180 12 526 9-Jan-14 706 9-Jan-15 180 365MAIN LANDING GEAR STRUTS - CHECK NITROGEN PRESSURE 12 9-Jan-14 9-Jan-15 365NOSE LANDING GEAR STRUT - CHECK NITROGEN PRESSURE 12 9-Jan-14 9-Jan-15 365TIRES -INSPECT CONDITION 12 9-Jan-14 9-Jan-15 365EXTERNAL LIGHTS - OPERATIONAL CHECK 12 9-Jan-14 9-Jan-15 365NAVIGATION SYSTEM ANTENNAS -CONDITION 12 9-Jan-14 9-Jan-15 365


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

RVSM AIR DATA SYSTEM (RVSM OPEARTIONS)- GROUND TEST 12 9-Jan-14 9-Jan-15 365RVSM CRITICAL REGION (RVSM OPERATIONS) 12 9-Jan-14 9-Jan-15 365PITOT & STATIC LINES - DRAIN 12 9-Jan-14 9-Jan-15 365WEATHER RADAR - OPERATIONAL TEST

12 9-Jan-14 9-Jan-15 365TCAS I SYSTEM (if installed) SYSTEM TEST 12 9-Jan-14 9-Jan-15 365DOOR SEAL PRESSURIZATION TEST 12 9-Jan-14 9-Jan-15 365NOSE LANDING GEAR BAY - CORROSION INSPECTION 12 9-Jan-14 9-Jan-15 365MAIN LANDING GEAR BAY -CORROSION INSPECTION 12 9-Jan-14 9-Jan-15 365METALLIC TAIL CONE (INCLUDING VERTICAL STABILIZER) - CORROSION 12 9-Jan-14 9-Jan-15 365HORIZONTAL STABILIZER ASSEMBLY - VISUAL INSPECTION 12 9-Jan-14 9-Jan-15 365ELEVATOR - GENERAL CONDITION 12 9-Jan-14 9-Jan-15 365WINDSHIELDS - CONDITION 12 9-Jan-14 9-Jan-15 365WINDSHIELDS - LATERAL PANELS (AIRCRAFT S/N 1002 ONLY) 12 N/A N/A N/ACABIN WINDOWS - CONDITION 12 9-Jan-14 9-Jan-15 365PROPELLER - GENERAL CONDITION SEE NOTE (b) FROM MM PG 41 150 6 891.7 9-Jan-14 1041.7 9-Jul-14 150 181

150 6 891.7 9-Jan-14 1041.7 9-Jul-14 150 181

PROPELLER - LUBRICATION SEE NOTE (a) (b) FROM MM PG 41

LUBRICATE EVERY 6 MONTHS IF ANNUAL OPERATION IS SIGNIFICANTLY LESS THAN 400 HOURS OR IF THE AIRCRAFT IS OPERATED OR STORED UNDER ADVERSE ATMOSPHERIC CONDITIONS


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

AUTOFEATHER HIGH & LOW TORQUE PRESSURE SWITCHES - BENCH CALIBRATION 12 9-Jan-14 9-Jan-15 365ENGINES - INSTALLATION INSPECTION 12 9-Jan-14 9-Jan-15 365ENGINE MOUNTS AND VIBRATION ISOLATORS - CONDITION 12 9-Jan-14 9-Jan-15 365ENGINE CONTROLS LEVERS, CABLES AND POWER LEVER SWITCHES - OPERATION

12 9-Jan-14 9-Jan-15 365MAGNETIC CHIP DETECTOR MONITORING SYSTEM 12 9-Jan-14 9-Jan-15 365

CABIN BAROMETRIC PRESSURE SWITCH - TEST BENCH 24 16-Nov-12 16-Nov-14 311AUTOPILOT SYSTEM (RVSM OPERATIONS) PERFORMANCE TEST (ALTITTUDE HOLD) 24 16-Nov-12 16-Nov-14 311CABIN BAROMETRIC PRESSURE SWITCH - (IF INVERTER P/N SS50 IS INSTALLED) 24 N/A N/A N/APILOT & COPILOT AIR DATA SYSTEM - ST. BY INSTRUMNET AIR DATA SECTION 24 16-Nov-12 16-Nov-14 311PITOT / STATIC SYSTEM TEST. REF FAR 91.411 24 15-Nov-12 15-Nov-14 310STATIC PORTS (RVSM OPERATIONS) 24 15-Nov-12 15-Nov-14 310MAGNETIC COMPASS- CONDITION 24 16-Nov-12 16-Nov-14 311ATC TRANSPONDER SYSTEM - REF. FAR 91.413 24 15-Nov-12 15-Nov-14 310OXYGEN BAROMETRIC PRESSURE SWITCH - OPERATIONAL CHECK 24 16-Nov-12 16-Nov-14 311



Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

OXYGEN SYSTEM CREW MASKS - OPERATIONAL TEST 36 18-Nov-11 18-Nov-14 313

CONTROL SURFACES HINGES - 60 9-Jan-14 9-Jan-19 1826FUEL COLLECTOR AND AUXILIARY TANKS

60 9-Jan-14 9-Jan-19 1826BOTTOM FUSELAGE SKIN AND STRUCTURAL MEMBERS - CORROSION 60 9-Jan-14 9-Jan-19 1826FORWARD PRESSURIZED BULKHEAD - CORROSION 60 9-Jan-14 9-Jan-19 1826REAR PRESSURIZED BULKHEAD - CORROSION 60 9-Jan-14 9-Jan-19 1826FUSELAGE INTEGRAL TANK - CONDITION

60 9-Jan-14 9-Jan-19 1826CABIN WINDOWS - WATER TIGHTNESS CHECK 60 9-Jan-14 9-Jan-19 1826WING INTERNAL STRUCTURE - CORROSION 60 9-Jan-14 9-Jan-19 1826

PERFORM AIRCRAFT LIGHT INSPECTION AND SERVICING (Ref. to AMM Chapter 12-20-00 Page Block 200) 200 891.7 1091.7 200PERFORM LH NACELLE LIGHT INSPECTION AND SERVICING (Ref. to AMM Chapter 12-21-00 Page Block 200) 200 891.7 1091.7 200PERFORM RH NACELLE LIGHT INSPECTION AND SERVICING (Ref. to AMM Chapter 12-21-00 Page Block 200) 200 891.7 1091.7 200

200 FH INSPECTIONS




Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

AUTOPILOT SYSTEM (aircraft 1002 only) CHAPTER 22-10-00 200 N/A N/A N/ARADOME DIVERTER STRIPS (AIRCRAFT S/N 1002 ONLY) 200 N/A N/A N/A

INBOARD FLAP SCREWJACKS - LUBRICATE400 891.7 1291.7 400

WING ENGINE MOUNT FITTINGS (ENGINE REMOVAL REQUIRED) (SUGGESTED AT ENGINE OVERHAUL) 4800 0 4800 3908ANTI-VIBRATION ISOLATOR ATTACHMENT THREADED HOLES - ENDOSCOPE - (ENGINE REMOVAL REQUIRED) (SUGGESTED AT ENGINE OVERHAUL)

4800 0 4800 3908ENGINE MOUNTS - DYE PENETRANT -(ENGINE REMOVAL REQUIRED) (SUGGESTED AT ENGINE OVERHAUL) 4800 0 4800 3908REAR TITANIUM FRAME - DYE PENETRANT -(ENGINE REMOVAL REQUIRED) (SUGGESTED AT ENGINE OVERHAUL) 4800 0 4800 3908

AFT ELEVATOR BELLCRANKS, BRACKETS, BOLTS, SUPPORT AND ASSEMBLY

6000 0 6000 5108FLAP SCREWJACKS - CONDITION 6000 0 6000 5108

2D (6000 hrs) INSPECTION REQUIREMENTS

400 FH INSPECTIONS

4800 FH INSPECTIONS


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

FLAP TRANSMISSION SHAFTS - INSPECTION 6000 0 6000 5108WING / FUSELAGE UPPER / LOWER L-SHAPED PROFILES - NDT 6000 0 6000 5108AILERON HINGE FITTING SUPPORTS & LUGS - EDDY CURRENT 6000 0 6000 5108

AUTOPILOT SYSTEM ROCKWELL COLLINS SMT 65 SERVO MOUNTS - TEST

9000 0 9000 8108CABIN UPPER ENTRY DOOR STRUCTURE AND PIN GUIDES - INSPECTION 9000 0 9000 8108FLIGHT COMPARTMENT UPPER STRINGERS AND FRAMES - CORROSION 9000 0 9000 8108FORWARD PRESSURIZED BULKHEAD - EDDY CURRENT INSPECTION 9000 0 9000 8108WINDSHIELD UPPER & LOWER BEAMS AND UPPER BEAM CROSS - CRACKS 9000 0 9000 8108CABIN ENTRY DOOR CUT OUT - EDDY CURRENT 9000 0 9000 8108WING AFT SPAR TO BULKHEAD FS 6710 - ENDOSCOPE 9000 0 9000 8108

WING FORWARD SPAR - WING TO FUSELAGE ATTACHMENTS 12000 0 12000 11108

PRATT & WHITNEY CANADA PERIODIC MINOR / ROUTINE INSPECTION 150 891.7 1041.7 150



LH ENGINE INSPECTION, MODEL PT6A-66B, S/N PCE-PRW0066


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

P3 FILTER CLEANING (Dependent on condition, service experience or enviroment) 150 891.7 1041.7 150P3 FILTER DRAIN VALVE HOUSING POST SB14054 150 N/A N/A N/A N/A N/A N/ACHIP DETECTOR INSPECTION 150 891.7 1041.7 150AGB INTERNAL SCAVENGE PUMP INLET 200 891.7 1091.7 200 FUEL NOZZLE FUNCTIONAL / LEAK TEST 400 891.7 1291.7 400BORESCOPE INSPECTION OF HOT SECTION 400 891.7 1291.7 400CHIP DETECTOR BRIDGED CHECK 600 12 891.7 9-Jan-14 1491.7 9-Jan-15 600 365FUEL PUMP INLET SCREEN 600 891.7 9-Jan-14 1491.7 600FUEL PUMP DRIVE COUPLING INSITU CHECK (If Sundstrand Pump Installed) 600 N/A N/A N/APOWER TURBINE BLADES PRE-SB14172 1500 N/A N/A N/A FUEL PUMP DRIVE COUPLING INSPECTION (If Sundstrand Pump Installed) 1800 N/A N/A N/APOWER TURBINE BLADES POST-SB14172 AND PT6A-66B 4000 0 4000 3108

PRATT & WHITNEY CANADA PERIODIC MINOR / ROUTINE INSPECTION 150 891.7 1041.7 150P3 FILTER CLEANING (Dependent on condition, service experience or enviroment) 150 891.7 1041.7 150P3 FILTER DRAIN VALVE HOUSING POST SB14050 150 N/A N/A N/A 150 N/A N/A N/ACHIP DETECTOR INSPECTION 150 891.7 1041.7 150

RH ENGINE INSPECTION, MODEL PT6A-66B, S/N PCE-RW0065


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

AGB INTERNAL SCAVENGE PUMP INLET SCREEN 200 891.7 1091.7 200 FUEL NOZZLE FUNCTIONAL / LEAK TEST 400 891.7 9-Jan-14 1291.7 400BORESCOPE INSPECTION OF HOT SECTION 400 891.7 9-Jan-14 1291.7 400CHIP DETECTOR BRIDGED CHECK 600 12 891.7 9-Jan-14 1491.7 9-Jan-15 600 365FUEL PUMP INLET SCREEN 600 891.7 1491.7 600FUEL PUMP DRIVE COUPLING INSITU CHECK (If Sundstrand Pump Installed) 600 N/A N/A N/APOWER TURBINE BLADES PRE-SB14172 1500 N/A N/A N/A FUEL PUMP DRIVE COUPLING INSPECTION (If Sundstrand Pump Installed) 1800 N/A N/A N/APOWER TURBINE BLADES POST-SB14172 AND PT6A-66B 4000 4000 3108

CABIN BLOWER: (including brushes) ELECTROMECH - P/N EM675-1, OVERHAUL

2000 2000 1108DOOR PRESSURE REGULATING AND HEATING SYSTEMS HOSES: P/N NP622002-8-200 - REPLACE 120 24-Sep-08 24-Sep-18 1719PRESSURIZATION SYSTEM PRIMARY OUTFLOW VALVE FILTER ELEMENT: ALLIED SIGNAL - P/N 147240-1 OR P/N: 1115-1 - REPLACE 600 711.9 1311.9 420

CHAPTER 05-10-00 / COMPONENT TIME LIMITS AIR CONDITIONING (CHAPTER 21)


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

HEATING SYSTEM GROUND BLOWER: ENVIRO - P/N 1250435 - BRUSHES - REPLACE 3000 3000 2108HEATING SYSTEM GROUND BLOWER: ENVIRO - P/N 1250435 - OVERHAUL 9000 9000 8108FREON AIR CONDITIONING SYSTEM CONDENSER / COMPRESSOR ELECTRICAL MOTOR: KEITH - P/N JBS5004-1/ JBS5006-1 - REPLACE BRUSHES AND BEARINGS MOTOR P/N: ES61100-1 600 711.9 1311.9 420

COCKPIT VOICE RECORDER OR CVDR UNDERWATER ACOUSTIC BEACON DUKANE DK120 -(REPLACE BATTERY)

STARTER/GENERATORS: LEAR SIEGLER - P/N 23080-019 - OVERHAUL 1000 1000 108STARTER/GENERATORS: LEAR SIEGLER - P/N 23080-019 - Brushes, Brush Holders and Springs - TSN/TSO (1st check) subsequent check ref to12-22-00 400 891.7 9-Jan-14 1291.7 400

ELT (AF) TYPE 503- TECHTEST - P/N 503-1- REPLACE BATTERY P/N A0673-1 60 N/AELT (AF) TYPE 503-"g" SWITCH: TECHTEST - P/N 503-7- REPLACE BATTERY - P/N A0701- *2, 5 Years from Battery Manufacture Date)

* N/A



ELECTRICAL POWER (CHAPTER 24)

EQUIPMENT AND FURNINGS (CHAPTER 25)

REFER TO REPLACEMENT DATE LABEL ON THE UNDERWATER ACOUSTIC BEACON

COMMUNICATIONS (CHAPTER 23)


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

UNDERWATER ACOUSTIC BEACON DUKANE DK100 - Remove and return to factory battery replacement - *Refer to replacement date label on UAB. * ELT (AF) C406-N TRANSMITTER BATTERY PACK: ARTEX P/N 452-0133 PART OF P/N 453-5060 - REPLACE BATTERY - *5 Years of useful life or 7 flashes on the "ON" LED following the ELT operational test

* Due 28-Feb-19 1876LIFE VEST - p/n 3500-133, s/n's Y0084768, LN0601037, and LV0706380 - Refer to applicable CMM's 27 9-Jan-14 9-Apr-16 821LIFE VEST - p/n P0723-111, s/n's M84601, M84591, M38657, M84643, M75745, AND M75834 - Refer to applicable CMM's 60 16-Jun-11 16-Jun-16 889LIFE RAFT - p/n 1900-1/2000-1, s/n 1955DN/1640DN - Refer to applicable CMM's 12 9-Jan-14 9-Jan-15 365

LH ENGINE FIRE EXTINGUISHER CARTRIDGES P/N 13083-5 - (4 years in service / 6 year life limit) P/N M13083-5. S/N27894 Mf d t A il 2013

48 30-Apr-13 30-Apr-17 1207RH ENGINE FIRE EXTINGUISHER CARTRIDGES P/N 13083-5 - (4 years in service / 6 year life limit) 48 16-Nov-12 16-Nov-16 1042

AILERON TRIM ACTUATOR: RATIER FIGEAC - P/N FE187-001 - REPLACE 15000 N/A N/A

FIRE PROTECTION (CHAPTER 26)

FLIGHT CONTROLS (CHAPTER 27)



Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

AILERON TRIM ACTUATOR: PRECILEC - P/N 702543-01, S/N B78309 - OVERHAUL 6000 96 24-Sep-08 6000 24-Sep-16 5108 989AILERON TRIM ACTUATOR: PRECILEC - P/N 702543-01, S/N B78309 - REPLACE 30000 30000 29108 RUDDER TRIM ACTUATOR: RATIER FIFEAC -P/N FE187-000 - REPLACE 15000 N/A N/A RUDDER TRIM ACTUATOR: PRECILEC - P/N 702542-01 - OVERHAUL 6000 96 23-Sep-08 6000 23-Sep-16 5108 988RUDDER TRIM ACTUATOR: PRECILEC - P/N 702542-01 - REPLACE 30000 30000 29108 HORIZONTAL TAIL TRIM ACTUATOR (HTTA): VICKERS/ELECTROMECH - P/N EM4011-3, S/N 32A - OVERHAUL 2000 2000 1108HORIZONTAL TAIL TRIM ACTUATOR (HTTA): VICKERS/ELECTROMECH - P/N EM4011-3, S/N 32A - REPLACE 30000 30000 29108HORIZONTAL TAIL TRIM ACTUATOR (HTTA): PRECILEC - P/N 702201 00 2000 2000 1108HORIZONTAL TAIL TRIM ACTUATOR (HTTA): PRECILEC - P/N 702201 00 30000 30000 29108FLAP CONTROL SYSTEM DRIVE UNIT: MICROTECNICA P/N C155720-2, S/N 1211 - OVERHAUL 4500 4500 3608FORWARD WING FLAP ACTUATORS: MICROTECNICA - P/N C132275-5, S/N 1199(LH) AND C132275-6, S/N 1198(RH) - REPLACEMENT OF MOTOR BRUSHES 6000 6000 5108


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

FORWARD WING FLAP ACTUATORS: MICROTECNICA - P/N C132275-5, S/N 1199(LH) AND C132275-6, S/N 1198(RH) - REPLACEMENT OF MICROSWITCHES 15000 15000 14108FORWARD WING FLAP ACTUATORS: MICROTECNICA - P/N C132275-31 (LH) AND C132275-41 (RH) - OVERHAUL 3000 N/A N/A N/A

COLLECTOR TANK INTERCONNECTING VALVE: SECONDO MONA - P/N SM2646-1, S/N 200 - REPLACE 10000 10000 9108FUEL BOOST PUMPS: PARKER - P/N 1C12-43, S/N 2BD18(LH), S/N 2BD39(RH), - OVERHAUL 3000 3000 2108FUEL FILTER ELEMENT: PUROLATOR - P/N 1743645-02 - REPLACE (1500 FH OR AT LIGHT INDICATION) 1500 1500 608

RCCB No K31: P/N SM600BA100A1, S/N 102582. Note: Replace with P/N SM600BA100A1,(S/N > 80000) (REF: To SB 80-0166 LATEST REVISION. 3000 3000 2108RCCB No K31: P/N 4930-02-100A, 3000 3000 2108HYDRAULIC FILTER ELEMENT: VICKERS - P/N M060024 - REPLACE HYDRAULIC POWER PACKAGE ELECTRIC MOTOR: VICKERS - P/N 520811 (29-1-3), S/N 246 - OVERHAUL 1500 1500 974

FUEL (CHAPTER 28)

HYDRAULIC POWER (CHAPTER 29)

REPLACE AT LIGHT INDICATION


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

HYDRAULIC POWER PACKAGE ASSEMBLY: VICKERS - P/N 520814, S/N G0820625 - OVERHAUL 6000 6000 5474

WING A/I PROTECTION VALVES: BARBER COLMAN - P/N BYLB51824, S/N 400(LH), S/N 382(RH) OVERHAUL 3000 3000 2108ENGINE A/I VANE ACTUATOR: VICKERS / ELECTROMECH - P/N EM4032-2 - OVERHAUL 5000 N/A N/A N/AENGINE A/I VANE ACTUATOR: VICKERS / ELECTROMECH - P/N EM4032-2 - REPLACE

30000 N/A N/A N/AENGINE A/I VANE ACTUATOR: PRECILEC P/N 702544-00, S/N b48639(LH), S/N B77766(RH) REPLACE 30000 30000 29108

MAIN LANDING GEAR: DOWTY - 201416003 / 004 - WHICH INCLUDES - MLG SHOCK ABSORBER DOWTY P/N 201417002 - OVERHAUL 6000 144 N/A N/A N/A N/A N/A N/AMAIN LANDING GEAR: DOWTY - 201416005 / 006 - S/N MDG0304(LH). S/N MDG0305(RH) WHICH INCLUDES - MLG SHOCK ABSORBER DOWTY P/N 201417003 OR 201417004 - OVERHAUL 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450MLG ACTUATORS: DOWTY - P/N 114346003(LH), S/N SA0802974 AND 114246004(RH) S/N SA0802590 - OVERHAUL -REFER TO DOWTY CMM. 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450

ICE AND RAIN PROTECTION (CHAPTER 30)

LANDING GEAR (CHAPTER 32)


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

MLG ACTUATORS: DOWTY - P/N 114346001(LH) AND 114246002(RH) - OVERHAUL- 6000 144 N/A N/A N/A N/A N/A N/AMLG DRAG BRACES: DOWTY - P/N 201418003(LH), S/N MDG0301 AND 201418004(RH), S/N MDG0300 - OVERHAUL

6000 144 24-Sep-08 6000 24-Sep-20 5474 2450NOSE LANDING GEAR: DOWTY - P/N 201033002, S/N MDG0254 - OVERHAUL 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450STEERING MANIFOLD: DOWTY - P/N 114180003, S/N SM262 - OVERHAUL 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450STEERING ACTUUATOR: DOWTY - P/N 114068003, S/N SM225 - OVERHAUL 3000 144 24-Sep-08 3000 24-Sep-20 2474 2450INSULATION RESISTANCE INSPECTION (REFER 32-50-00 PAGE BLOCK 500) 600 711.9 1311.9 420NLG ACTUATOR: DOWTY - P/N 114067004, S/N SA0802415 - OVERHAUL 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450NLG DRAG BRACE: DOWTY - P/N 201050002, S/N MDG0252 - OVERHAUL 6000 144 24-Sep-08 6000 24-Sep-20 5474 2450NOSE WHEELS: B F GOODRICH - P/N 3-1460, S/N 0553(LH), S/N 0116 (RH) - OVERHAUL 1500 1500 974MAIN WHEELS: B F GOODRICH - P/N 3-1461-1, S/N 0599(LH), S/N 0600(RH) OVERHAUL

1500 1500 974WHEEL BRAKES: B F GOODRICH - P/N 2-1504-4, S/N 0512(LH), S/N 0520(RH)

OVERHAUL WHEN WEAR PIN INDICATES 100% WORN


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

STEERING FILTER: FACET ENTERPRISE - P/N: 038108-1 FILTER ELEMENT: P/N 037913-05 OR 037913-05-45 OR P/N: 1730791-04 - REPLACE 1000 N/A N/A N/A

OXYGEN SYSTEM FILLER VALVE - PACIFIC PRECISION - P/N P21010 - FUNCTIONAL TEST NOTE: THE VALVE OVERHAUL WHEN SELECTED, DOES NOT REQUIRE TO PERFORM THE FUNCTIONAL TEST EVERY 5 YEARS AND VICE - VERSA (FUNCTIONAL TEST) 60 9-Jan-14 9-Jan-19 1826OXYGEN SYSTEM FILLER VALVE: PACIFIC PRECICSION - P/N P21010 - OVERHAUL - NOTE: THE VALVE OVERHAUL WHEN SELECTED, DOES NOT REQUIRE TO PERFORM THE FUNCTIONAL TEST EVERY 5 YEARS AND VICE - VERSA (OVERHAUL)

120 24-Sep-08 24-Sep-18 1719OXYGEN SYSTEM THREE POSITION VALVE: PACIFIC PRECISION - P/N P21021- OVERHAUL 60 9-Jan-14 9-Jan-19 1826OXYGEN SYSTEM CREW MASKS: EROS - P/N MC10-15-13 - OVERHAUL 72 24-Sep-08 24-Sep-14 258PROTECTIVE BREATHING EQUIPMENT - EMERGENCY ESCAPE HOOD: Eros - p/n 15-40F (if installed) - REPLACE 120 24-Sep-08 24-Sep-18 1719

OXYGEN (CHAPTER 35)

PNEUMATIC (CHAPTER 36)


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PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

CABIN DOOR SEAL PRESSURIZATION LINE, HOSE - P/N 80-197056-027 OR HOSE P/N 80-197605-001 AND P/N 80-197605-003 - REPLACE 120 24-Sep-08 24-Sep-18 1719

ADASD PROCESSOR: ALTAIR P/N DAAS-A-010-1 - REPLACE BATTERY 120 24-Sep-08 24-Sep-18 1719DTU PROCESSOR: ALTAIR P/N DTU-A-012-1 - REPLACE BATTERY 120 24-Sep-08 24-Sep-18 1719

3600 72 325.5 3-Oct-10 3925.5 3-Oct-16 3034 998HARTZELL - P/N HC-E5N-3 (A) (L) / (H,L) E8218 - BLADE INSPECTION / PAINT INSPECTION and CORROSION REMOVAL IF NECESSARY. (ref. Hartzell SB HC-SB-61-181A latest revision) 600 24 711.9 16-Nov-12 1311.9 16-Nov-14 420 311PROPELLER GONERNOR: WOODWARD - P/N 8210-411, S/N 15870626(LH), S/N 15897682(RH) - OVERHAUL (REF: P&WC SB 14603 latest revision) 4100 4100 3208

6500 72 24-Sep-08 6500 24-Sep-14 5608 258

NOTE: THE OVERHAUL CALENDER LIMIT FOR PROPELLERS MANUFACTURED OR OVERHAULED SINCE OCTOBER 1991 IS 6 YEARS , WHILE FOR PROPELLERS MANUFACTURED OR OVERHAULED PRIOR TO OCTOBER1991 REMAINS 5 YEARS (REF. HARTZELL SB HC-61-61Y LAST

REVISION

CENTRAL MAINTENANCE SYSTEM (CHAPTER 45)

PROPELLERS (CHAPTER 61)

OVERSPEED GOVERNOR: WOODWARD - P/N 210962, S/N 15703595(LH), S/N 15703597(RH) - OVERHAUL

NOTE: THIS TBO IS BASED ON THE ASSUMTION OF CONTINUOUS OPERATION MINIMUM OF 10 HOURS PER MONTH. THE RECOMMENDED CALENDER TIME LIMTI OF 6 YEARS FOR UNITS NOT IN CONTINUOUS SERVICE WITH A MINIMUM OF 120 HOURS PER YEAR. FOR UNITS IN

CONTINUOUS SERVICE WITH A MINIMUM OF 120 HOURS PER YEAR, THE UNIT CAN BE OPERATED TO THR RECOMMENDED TBO IN HOURS PROVIDED THERE HAS BEEN NO 6 MONTH PERIOD WHEN THE UNIT WAS NOT OPERATED A MINIMUM OF 10 HOURS

HARTZELL - P/N HC-E5N-3 (A) (L) / (H,L) E8218 - OVERHAUL


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PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

PROPELLER RPM TRANSDUCER: FAREM - P/N 15TG02TYP1542 OR ELECTROMECH P/N EM8028-1 ( ) - OVERHAUL 3000 3000 2108

ENGINE VIBRATION ISOLATORS - BARRY CONTROLS AEROSPACE: P/N 95007-17 / P/N 95007-18 - REPLACE - (SUGGESTED AT ENGINE OVERHAUL) 4800 4800 3908

ENGINE VIBRATION ISOLATORS - BARRY CONTROLS AEROSPACE: P/N 95007-17 / P/N 95007-18 - REPLACE - (SUGGESTED AT ENGINE OVERHAUL) 4801 4801 3909

ENGINE - OVERHAUL - REF: P&WC SB 14603 3600 3600 2708ENGINE - HOT SECTION INSPECTION - REF: P&WC SB 14603 1800 1800 908BLADES, POWER TURBINE P/N (3056693-01) 12000 12000 11108FUEL CONTROL UNIT - OVERHAUL (TBO + 500) 4100 4100 3208FUEL HEARTER - OVERHAUL (TBO + 500) 4100 4100 3208PROPELLER GOVERNOR - OVERAHUL (TBO + 500) 4100 4100 3208OVERTORQUE LIMITER-OVERHAUL (where applicable) (TBO + 500) 4100 4100 3208

RH ENGINE (CHAPTER 71), MODEL PT6A-66B, S/N PCE-RW0065

LH ENGINE (CHAPTER 71), MODEL PT6A-66B, S/N PCE-RW0066

LH ENGINE (CHAPTER 72), MODEL PT6A-66B, S/N PCE- RW0066


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

IGNITION EXCITER - OVERHAUL (TBO + 500) 4100 4100 3208COMPRESSOR BLEED VALVE - OVERHAUL (TBO + 500) 4100 4100 3208FLOW DIVIDER/START CONTROL INSTALLATION - OVERHAUL (TBO + 500) 4100 4100 3208FUEL PUMP (ARGO-TECH ONLY) OVERAHUL (TBO + 500) 4100 4100 3208

ENGINE - OVERHAUL - REF: P&WC SB 14603 3600 3600 2708ENGINE - HOT SECTION INSPECTION - REF: P&WC SB 14603 1800 1800 908 BLADES, POWER TURBINE P/N (3056693-01) 12000 12000 11108FUEL CONTROL UNIT - OVERHAUL (TBO + 500) 4100 4100 3208FUEL HEARTER - OVERHAUL (TBO + 500) 4100 4100 3208PROPELLER GOVERNOR - OVERAHUL (TBO + 500) 4100 4100 3208OVERTORQUE LIMITER-OVERHAUL (where applicable) (TBO + 500) 4100 4100 3208IGNITION EXCITER - OVERHAUL (TBO + 500) 4100 4100 3208COMPRESSOR BLEED VALVE - OVERHAUL (TBO + 500) 4100 4100 3208FLOW DIVIDER/START CONTROL INSTALLATION - OVERHAUL (TBO + 500) 4100 4100 3208

RH ENGINE (CHAPTER 72), MODEL PT6A-66B, S/N PCE-RW0065


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

FUEL PUMP (ARGO-TECH ONLY) OVERHAUL (TBO + 500) 4100 4100 3208

FUEL FLOW TRANSMITTERS: P/N 1 / 2-1-81-302 - REPLACE BEARINGS AND SHAFT - CALIBRATION 5000 5000 4108P3 FILTER CLEAN OR REPLACE 1000 0 1000 108ENGINE FUEL PUMP FILTERS (REFER TO P&WC MAINTENANCE MANUAL)

FUEL FLOW TRANSMITTERS: P/N 1 / 2-1-81-302 - REPLACE BEARINGS AND SHAFT - CALIBRATION 5000 5000 4108P3 FILTER CLEAN OR REPLACE 1000 1000 108ENGINE FUEL PUMP FILTERS (REFER TO P&WC MAINTENANCE MANUAL)

ENGINE RPM TRANSDUCER: FAREM - P/N 15TG02TYP1542 OR ELECTROMECH P/N EM8028-1 ( ) - OVERHAUL 3000 3000 2108

ENGINE RPM TRANSDUCER: FAREM - P/N 15TG02TYP1542 OR ELECTROMECH P/N EM8028-1 ( ) - OVERHAUL 3000 3000 2108

OIL FILTER REPLACEMENT 1000 0 1000 108

OIL FILTER REPLACEMENT 1000 1000 108

SEE ENGINE INSPECTION CHAPTER 5-20-00 ABOVE

RH ENGINE FUEL & CONTROL (CHAPTER 73), MODEL PT6A-66B, S/N PCE- RW0065

LH ENGINE FUEL & CONTROL (CHAPTER 73), MODEL PT6A-66B, S/N PCE-RW0066

LH ENGINE INDICATING (CHAPTER 77), MODEL PT6A-66B, S/N PCE- RW0066

RH ENGINE INDICATING (CHAPTER77), MODEL PT6A-66B, S/N PCE-RW0065

LH ENGINE OIL (CHAPTER 79), MODEL PT6A-66B, S/N PCE-RW0066

RH ENGINE OIL (CHAPTER 79), MODEL PT6A-66B, S/N PCE-RW0065

SEE ENGINE INSPECTION CHAPTER 5-20-00 ABOVE


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

COMPOSITE PART EXTERIOR PAINT

LOGO COLOR, PAINT AND DEMENSION ALLOWABLE LIMITS FOR COMPOSITES PARTS

PORTABLE FIRE EXTINGUISHER AMEREX CORP. - 352T, HYDROSTATIC TEST (if installed) P/N C352TS. S/N Y-439198,Mfg. 60 9-Jan-14 9-Jan-19 1826LH ENGINE FIRE EXTINGUISHER CONTAINER: P/N 30104100, HYDROSTATIC TEST S/N51408A1 60 9-Jan-14 9-Jan-19 1826RH ENGINE FIRE EXTINGUISHER CONTAINER: P/N 30104100, HYDROSTATIC TEST S/N 51982A1 60 9-Jan-14 9-Jan-19 1826

MAIN LANDING GEAR: DOWTY - P/N'S 201416003 / 004 AND 2011416005 / 006 COMPONENTS - LIFE LIMIT 30000 30000 29474MAIN LANDING GEAR LEVER HINGE FITTING (LH) P/N 201034320 8250 8250 7724MAIN LANDING GEAR LEVER HINGE FITTING (RH) P/N 201034321 8250 8250 7724

FIRE PROTECTION (CHAPTER 26)

LANDING GEAR (CHAPTER 32)

CHAPTER 04-00-00 / LIFE LIMITSREFERENCE CHAPTER 04-00-00 PAGE 2 FOR REQUIREMENTS - NO PAINTS OTHER THAN THOSE LISTED ON ITEM 05-006 (CHAPTER 91-00-

00, CHART 201) CAN BE USED.

PLACARDS AND MARKINGS (CHAPTER 11)

REFERENCE CHAPTER 04-00-00 PAGE 2 FOR REQUIREMENTS - NO MORE THAN 20% OF THE EXTERNAL SURFACE OF EACH COMPOSITE COMPONENT CAN BE COVERED WITH PAINTS OTHER THAN THOSE LISTED ON ITEM 05-006 (CHAPTER 91-00-00, CHART 201) OR DECALS. APPLICATION OF PAINTS OTHER THAN THOSE LISTED ON ITEM 05-006 (CHAPTER 91-00-00, CHART 201) OR DECALS TO MORE THAN 20%

OF A COMPOSITE SURFACE AREA COULD RESULT IN EXCESSIVE ABSORPTION OF RADIATION, WITH SUBSEQUENT DAMAGE TO THE COMPONENT. THE COMPOSITE AREAS ARE SHOWN IN CHAPTER 51-00-00 CAN BE USED.


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

MAIN LANDING GEAR WHEEL LEVER (LH) - P/N 201034312 10900 10900 10374MAIN LANDING GEAR WHEEL LEVER (RH) - P/N 201034313 10900 10900 10374MAIN LANDING GEAR AXLE - P/N 201034641

7350 7350 6824MAIN LANDING GEAR HINGE PIN - P/N 201034637 13150 13150 12624MAIN LANDING GEAR PINTLE PIN - P/N 201034635 22500 22500 21974MAIN LANDING GEAR PIN (SHOCK ABSORBER UPPER ATTACHMENT) - P/N 201034604 25150 25150 24624MAIN LANDING GEAR SHOCK ABSORBERS: DOWTY - P/N 201417002 (with P/N 201416003/004 - P/N 201417003 (with P/N 201416005/006 - P/N 201417004 (with P/N 201416005/006 22200 22200 21674MAIN LANDING GEAR SHOCK ABSORBER CYLINDER - P/N 201068600 13100 13100 12574MAIN LANDING GEAR SHOCK ABSORBER PISTON - P/N 201068601, 201068621, 201068622 10100 10100 9574MAIN LANDING GEAR DRAG BRACES DOWTY - P/N'S 201418003 / 004 30000 30000 29474MAIN LANDING GEAR DRAG BRACE UPPER LINK - P/N 201035311 14050 14050 13524MAIN LANDING GEAR DRAG BRACE UPPER LINK - P/N 201035312 14050 14050 13524


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

MAIN LANDING GEAR DRAG BRACE LOWER LINK - P/N 201035308 18500 18500 17974MAIN LANDING GEAR DRAG BRACE CENTER PIN - P/N 201035652 6700 6700 6174MAIN LANDING GEAR DRAG BRACE UPPER PIN (LH) - P/N 201035676 7200 7200 6674MAIN LANDING GEAR DRAG BRACE UPPER PIN (RH) - P/N 201035677 7200 7200 6674MAIN LANDING GEAR ACTUATORS DOWTY -P/N 114346001 / 002 OR 114346003 / 004.L/H S/N SA0802974 10250 10250 9724NOSE LANDING GEAR DOWTY - P/N 201033002 30000 30000 29474NOSE LANDING GEAR MAIN FITTING - P/N 201033300 6850 6850 6324NOSE LANDING GEAR PIN (DRAG BRACE TO MAIN FITTING) - P/N 201033649 24750 24750 24224NOSE LANDING GEAR DRAG BRACE DOWTY - P/N 201050002 30000 30000 29474NOSE LANDING GEAR DRAG BRACE UPPER LINK - P/N 201050301 10600 10600 10074NOSE LANDING GEAR DRAG BRACE CLEVIS- LOWER LINK - P/N 201050608 18600 18600 18074NOSE LANDING GEAR ACTUATOR DOWTY - P/N 114067003 AND 114067004 26500 26500 25974

OXYGEN CYLINDER ASSEMBLY - SCOTT AVIATION - P/N 89511040 (OVERHAUL / HYDROSTATIC TEST) 60 18-Nov-11 18-Nov-16 1044

OXYGEN (CHAPTER 35)


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

PORTABLE OXYGEN CYLINDER AND PRESSURE REGULATOR ASSEMBLY: SCOTT AVIATION - P/N 900019-01 (if installed) (OVERHAUL / HYDROSTATIC

S )60 9-Jan-14 9-Jan-19 1826

OXYGEN CYLINDER ASSEMBLY - SCOTT AVIATION - P/N 89511040 (REPLACEMENT) 180 24-Sep-08 24-Sep-23 3545

AIRPLANES S/N 1002: S/N 1105 AND SUBSEQUENTS - LIFE LIMIT 15000 15000 14474

HARTZELL - P/N HC-E5N-3 (A) (L) / (H,L) E8218 SERVICE LIFE (BLADE ONLY) 9000 9000 8108PROPELLER HUB SERVICE LIFE S/N: 1018 AND SUBSEQUENTS 18000 18000 17108

SHAFT, COMPRESSOR ROTOR P/N (3043063) S/N (PKAAA180367) 24000 24000 23474ROTOR, (1st Stage) COMPRESSOR P/N (3042701) S/N (EAAB000K478) 24000 24000 23474ROTOR, (2st Stage) COMPRESSOR P/N (3040942) S/N (EAAB000K732) 24000 24000 23474ROTOR, (3rd Stage) COMPRESSOR P/N (3040933) S/N (EAAB000F104) 24000 24000 23474ROTOR, (4th Stage) COMPRESSOR P/N (3040944) S/N (TXA1B5646) 24000 24000 23474IMPELLER, CENTRIFUGAL P/N (3036898) S/N (EAAB000K134) 24000 24000 23474DISK, COMPRESSOR TURBINE P/N (3053740-01) S/N (A002CXBK) 8000 8000 7474

STRUCTURES (CHAPTER 51)

PROPELLERS (CHAPTER 61)

LH ENGINE (CHAPTER 72), MODEL PT6A-66B, S/N PCE- RW0066


Inspector





PROGRAM




Aircraft Serial No.




180-MAN-0200-01105 REV. B3 03/21/12

DISK, POWER TURBINE (1st Stage) P/N (3037312) S/N (A00D7BB) 15000 15000 14474DISK, POWER TURBINE (2nd Stage) P/N (3037313) S/N (A002CY1Y) 15000 15000 14474

SHAFT, COMPRESSOR ROTOR P/N (3043063) S/N (PKAAA170417) 24000 24000 23474ROTOR, (1st Stage) COMPRESSOR P/N (3042701) S/N (EAAB000K480) 24000 24000 23474ROTOR, (2st Stage) COMPRESSOR P/N (3040942) S/N (EAAB000K650) 24000 24000 23474ROTOR, (3rd Stage) COMPRESSOR P/N (3040933) S/N (EAAB000F016) 24000 24000 23474ROTOR, (4th Stage) COMPRESSOR P/N (3040944) S/N (TXA1B5654) 24000 24000 23474IMPELLER, CENTRIFUGAL P/N (3036898) S/N (EAAB000H943) 24000 24000 23474DISK, COMPRESSOR TURBINE P/N (3053740-01) S/N (A002CXBE) 8000 8000 7474DISK, POWER TURBINE (1st Stage) P/N (3037312) S/N (A002D14A) 15000 15000 14474DISK, POWER TURBINE (2nd Stage) P/N (3037313) S/N (A002CY22) 15000 15000 14474

RH ENGINE (CHAPTER 72), MODEL PT6A-66B, S/N PCE- RW0065


Inspector

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