setp may 6, 2010 mark fattal program quality/cm a configuration management system for prototype...
TRANSCRIPT
SETPMay 6, 2010
Mark FattalProgram Quality/CM
A Configuration Management System
for Prototype Programs
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Agenda
• History
• General Requirements
• CM Overview
• Engineering Release Authority
• Drawing Tree
• Hardware Software Compatibility Matrix
• Configuration Release
• Prep Items
• Summary
• Question
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
History
• NGC Purchased a Gulfstream II in 2006
• GII Goal: – To provide a multipurpose manned aircraft to be used as a flying
test bed platform to support prototype activity, engineering concepts, program risk reduction and Headstart activity.
• Independent CM Plan:– Drafted and released in March 2007 to provide configuration of the
GII Flying Test Bed (FTB) aircraft for rapid development/prototype program using the GII flight test platform.
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
GII Flying Test Bed
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Interior Configuration Example
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
General Requirements
• Program Quality Assigned Local Control– On Site Flight Test Quality Engineering Performs in a dual role as
Quality Engineer and Configuration Management.
• Engineering Release Authority with Local Tracking Number Assigned– Tracking number based upon current program.
• Quality Maintains Originals as Aircraft Records – Hardcopy Originals – Electronic Archived
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
CM Plan Overview
• Configuration Management Plan – Defines the Process for the Control and Release Authority for
• Drawings• Specifications • Tests• Instrumentation• Special Support Equipment• HSCM (Hardware Software Compatibility Matrix)• Flight Release EO
• All Released Documents Carry a Unique Identifier Applicable to a Specific Program (5TH Character in Drawing number)– Example
• GII50EXXXX1: Released for an Electrical Drawing for program ABC
• GII51EXXXX2: Released for an Electrical Drawing for program XYZ
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
FTB Drawing Tree
Flight Test Bed Drawing Tree
Supplier to NGC
InstallationDrawing
Supplier to NGC Phase 1
Installation Drawing
A/V Support Equipment
Instrum Support
Equipment
Attachment A - FTB Drawing Tree
Supplier to NGC Phase 2
Installation Drawing
SupplierMaster
Drawing List
Supplier ABC Phase 1 Master Drawing List
Supplier ABC Phase 2 Master
Drawing List
FTB Hardware/Software
Compatibility
FTB InstallationDrawing
A/V Detail
A/V Electrical
A/V Procedure
Instrum Installation
A/V Installation
Instrum Detail
Instrum Electrical
Instrum Procedure
Instrum Assembly
NGC Test Procedure
NGC Specifications
NGC Flight Config Release
Supplier to NGC ATDC Installation
Drawing
Supplier XYZ Master
Drawing List
KEY:The 5th character of the drawing number designates program specific releases, with the exception of the top tree drawing, GII50A0001.Examples of programs:0 = ABC1 = XYZ See Attachment “B” for listing
Example: GII50B0001 is a ABC program drawing, and GII51B001 is an XYZ drawing.
NGC IRAD to A/C
Installation Drawing
IRAD Master Drawing List
A/V Assembly
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
CM Plan Overview
• On Site Program Quality Rep is Responsible to Generate the HSCM (Hardware Software Compatibility Matrix)
• The Plan Allows for Multiple Configurations/Programs Simultaneously.
• Supports Either Engineering Generated Locally or Program Engineering provided for Incorporation Per Plan and Drawing Tree
• The Plan Outlines the Review/Release Requirement for Every Engineering Document Type Identified in Drawing Tree.
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
CM Plan Approved Streamlined ApproachRELEASE AUTHORITY (RA)
CAGE CODE
78022 1. RELEASE AUTHORITY NO.
2. RA REV.
3. LIAISON RA
YES NO 4. RELATED RA
5. RELEASE AUTHORITY TYPES
ERN DCN ECO DVA 6. NETWORK NUMBER
7. SHEET
1 of 1
8. STOP/LIFT ORDER
STOP LIFT PARTIAL LIFT
ESTIMATED LIFT DATE / /
9. CHANGE AUTHORITY
PCR PCR PCR PCR
10. CHANGE CLASS
CLASS I
CLASS II
11. REASON CODE
12. ECOS / RC/I INCORPORATED BY THIS DCN
13. RETROFIT/FIELD DOC REQUIRED
RETROFIT TCTO TO
14. TEMPORARY CONFIGURATION MODIFICATION
T2 MOD
15. DESCRIPTION OR REASON FOR CHANGE
16. MFG. PLANNING
YES NO
17. DF NO
18.
EFFECT SCHED
19. MODEL CODE
20. ENGINEERING EFFECTIVITY
CI NO SERIALIZATION RANGE
23. MANUFACTURING EFFECTIVITY
21. ENGINEERING CHANGE PROPOSAL APPLICABLE
ECP NUMBER 22. DEVIATION APPLICABLE
DEVIATION NUMBER
24. DOCUMENT/DWG NO
25. DOCUMENT/DWG TITLE
26. DOC/DWG REV
27. PL REV
28. NEXT ASSY PART NO (FOR REFERENCE ONLY)
29. NEXT ASSEMBLY FOLLOW-UP RA
YES ENTER SCHEDULED RA NO
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CAGE CODE PART NUMBER
NOMENCLATURE / DESCRIPTION CUT STOCK SIZE
RAW MATERIAL
CODE SPECIFICATIONS ZO
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30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46.
47. ADDITIONAL DETAILED INSTRUCTIONS (FOR PARTS DISPOSITION, MANUFACTURING OR PROCUREMENT INSTRUCTIONS SUCH AS FOR REWORK, SPARES, AMRS, ETC)
48. RELEASE AUTHORITY SIGNATURES
ORIGINATOR
DATE
/ / MATERIAL AND PROCESSES
DATE
/ / STRESS
DATE
/ / PROGRAM INTEGRATION
DATE
/ / DESIGN LEAD/MANAGER
DATE
/ / PROGRAM PLANNING
DATE
/ / PRODUCT ASSURANCE
DATE
/ / PROGRAM MANAGEMENT
DATE
/ / CHECK
DATE
/ / PRODUCT SUPPORT/ILS
DATE
/ / SAFETY
DATE
/ / SOFTWARE CONFIGURATION MGMT
DATE
/ / CHIEF ENGINEER
DATE
/ / MANUFACTURING ENGINEERING
DATE
/ / RELIABILITY
DATE
/ / SOFTWARE QUALITY ASSURANCE
DATE
/ / MASS PROPERTIES
DATE
/ / MEC
DATE
/ / MATERIEL
DATE
/ / RESPONSIBLE ORG TEST MGR
DATE
/ / SYS ENG/REQUIREMENTS MGMT
DATE
/ / BUSINESS MANAGEMENT
DATE
/ / PRODUCT TEST
DATE
/ / DATA MANAGEMENT
DATE
/ / DADT
DATE
/ / OTHER
DATE
/ / OTHER
DATE
/ / CONFIGURATION RELEASE
DATE
/ / CLICK HERE FOR FORM INSTRUCTIONS
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Takeoff
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Hardware Software Compatibility Matrix
• HSCM (Hardware Software Compatibility Matrix)– Program Quality is responsible for the generating and maintaining
this Matrix.– The approved/released authorizes the applicable
hardware/software configuration– Archived Matrix’s maintain the configuration history to ensure the
ability to return to a prior flight test configuration or verify the as flown condition.
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Example HSCM (Notional)
LRU Manufacture Part No.SW
VersionFJT/Qual
Responsible Eng. Notes
Sensor World 2514-A2103 7.1v1.10 FJT Tom Smith 2/16/2010
Transponder Waves 500107-103 1.1.2a FJT Shirley JonesSW 6500-118-402
v1.1.2a
Mass Storage Store Blade RAID GII 103.01 FJT Larry Chase dtd 2/2/10
UHF/VHF Antenna Systems 4511-310 N/A FJT Jen Swift
GPS Antenna Systems 4545-100 N/A FJT David Sandy
Switch Cisco CISCO 3750G-24TS N/A FJT Mike Lumper
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
HSCM Engineering Release
E1-F037 (9-07)
RELEASE AUTHORITY (RA)
CAGE CODE
78022 1. RELEASE AUTHORITY NO.
RA-IRAD-026 2. RA REV.
I/R 3. LIAISON RA
X YES NO 4. RELATED RA
n/a 5. RELEASE AUTHORITY TYPES
X ERN DCN ECO DVA 6. NETWORK NUMBER
7. SHEET
1 of 1
8. STOP/LIFT ORDER
STOP LIFT PARTIAL LIFT
ESTIMATED LIFT DATE / /
9. CHANGE AUTHORITY
PCR PCR
PCR PCR
10. CHANGE CLASS
CLASS I
CLASS II
11. REASON CODE
N/A
12. ECOS / RC/I INCORPORATED BY THIS DCN
13. RETROFIT/FIELD DOC REQUIRED
RETROFIT TCTO TO
14. TEMPORARY CONFIGURATION MODIFICATION
T2 MOD
15. DESCRIPTION OR REASON FOR CHANGE
THE ATTACHED EXCEL SPREADSHEET IS USED TO CONTROL THE CONFIGURATION/COMPATIBILITY ALONG WITH TRACKING FJT/QUAL STATUS OF BOTH HARDWARE/SOFTWARE TO BE TESTED ON THE GII FTB DURING IRAD HEAD-START TESTING. SW VERSION UPDATE LRU 1
16. MFG. PLANNING
YES NO
17. DF NO
18.
EFFECT SCHED
19. MODEL CODE
20. ENGINEERING EFFECTIVITY
CI NO SERIALIZATION RANGE
23. MANUFACTURING EFFECTIVITY
21. ENGINEERING CHANGE PROPOSAL APPLICABLE
ECP NUMBER n/a 22. DEVIATION APPLICABLE
DEVIATION NUMBER n/a
24. DOCUMENT/DWG NO
GII50HWSWCM-0015 25. DOCUMENT/DWG TITLE
FTB HARDWARE/SOFTWARE COMPATIBILTY MATRIX 26. DOC/DWG REV
15 27. PL REV
n/a 28. NEXT ASSY PART NO (FOR REFERENCE ONLY)
GII50A0001 29. NEXT ASSEMBLY FOLLOW-UP RA
YES ENTER SCHEDULED RA NO
EF
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CODE PART NUMBER NOMENCLATURE /
DESCRIPTION CUT STOCK SIZE
RAW MATERIAL
CODE SPECIFICATIONS ZO
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30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46.
47. ADDITIONAL DETAILED INSTRUCTIONS (FOR PARTS DISPOSITION, MANUFACTURING OR PROCUREMENT INSTRUCTIONS SUCH AS FOR REWORK, SPARES, AMRS, ETC)
48. RELEASE AUTHORITY SIGNATURES
ORIGINATOR
M. FATTAL DATE
4/30/10 MATERIAL AND PROCESSES
DATE
/ / STRESS
DATE
/ / PROGRAM INTEGRATION
DATE
/ / DESIGN LEAD/MANAGER
DATE / /
PROGRAM PLANNING
DATE
/ / PRODUCT ASSURANCE
DATE
PROGRAM MANAGEMENT
DATE
/ / CHECK
DATE / /
PRODUCT SUPPORT/ILS
DATE
/ / SAFETY
DATE
/ / SOFTWARE CONFIGURATION MGMT
DATE
/ / CHIEF ENGINEER
DATE / /
MANUFACTURING ENGINEERING
DATE
/ / RELIABILITY
DATE
/ / SOFTWARE QUALITY ASSURANCE
DATE
/ / MASS PROPERTIES
DATE
/ / MEC
DATE
/ / MATERIEL
DATE
/ / RESPONSIBLE ORG TEST MGR
DATE
/ / SYS ENG/REQUIREMENTS MGMT
DATE
/ / BUSINESS MANAGEMENT
DATE
/ / PRODUCT TEST
DATE
/ / DATA MANAGEMENT
DATE
/ / DADT
DATE
/ / PROGRAM MANAGER
DATE
4/30/10 OTHER
DATE
/ / CONFIGURATION RELEASE
M. FATTAL DATE / /
CLICK HERE FOR FORM INSTRUCTIONS Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
HWSW - Notional Sub Tier Software
Processor NGC N030300G01 NGC1234567
GII_FLT_1.0 2/14/07
IAW Flight Certification Report
- 15-DEC 2009John Henry
Avionics Processor (AI) 4.1.5
Data processor (DP)
Signal Processor ISR
Signal Processor OFP 1.0.1
Output Processor (OP)
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
FJT/Qualification
• FJT (Flight Justification Testing)– Responsible Engineer (RE) generates FJT/Qual sheet – Every LRU (Line Replaceable Unit)/Test Critical Component is
reviewed a by the RE and approved by System Safety for operation in expected flight envelope.
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
FJT/Qual Sheet
QUALIFICATION CERTIFICATE CERTIFICATE NO.
SPEC. & DASH NO.
DATE
TITLE
SUPPLIER
Mission Ops
SUPPLIER PART NO.
see above title block
BUYER
NGC
THIS ITEM SUCCESSFULLY COMPLETED THE TEST SPECIFIED IN THE INDIVIDUAL EQUIPMENT SUBJECT SPECIFICATION,
AND FULFILLS THE QUALIFICATION REQUIREMENTS FOR: FJT FQ
QUALIFIED BY QUALIFIED BY ANALYSIS SIMILARITY
QUALIFIED BY TEST QUALIFIED BY TEST/ SIMILARITY
DATA CERTIFIED
BY TEST OR BY ANALYSIS
QUALIFIED BY ANALYSIS/SIMILARITY
ACTUAL TEST COMPLETION DATE 08/20098
REPORT APPROVAL DATE 11/2009
QUALIFIED BY SIMILARITY TO
SUPPLIER REPORT NUMBERS .
D/W YES NO LIMITATIONS YES NO
DISPOSITION
DISPOSITION
Within the context of the requirements, implied or otherwise, of the G2 test program, there are no limitations with regard to flight worthiness and safety. Performance profiles and possible performance limitations do exists, but have no bearing on flight safety or flight intergrity.
FLIGHT WORTHY
THIS ITEM HAS NOT SUCCESSFULLY COMPLETED THE TEST SPECIFIED IN THE INDIVIDUAL EQUIPMENT SPECIFICATION. HOWEVER, IT IS DEEMED FLIGHT WORTHY FOR THE REASON(S) BELOW:
RISK ANALYSIS Low risk. This set of COTS hardware has been subjected to representitive flight variables during other flight activities. This equipment produced no risks to flight activities and remained stable during all flights.
EMBEDDED FIRMWARE VERSION: SYSTEM SAFETY
DATE
TEST REPORT NO.
TEST RPT APPROVAL DATE
RESPONSIBLE ENGINEER/EMPLOYEE NO.
DATE
S/W CONFIGURATION MGMT (IF APPLICABLE)
DATE
ELECTROMAGNETIC EFFECTS & NUCLEAR HARDNESS
DATE
H/W CONFIGURATION MGMT
DATE
S/W INTEGRATION (IF APPLICABLE)
DATE
CM BASELINE CONTROL
DATE
DEFINITIONS
FLIGHT JUSTIFICATION TEST (FJT) - COMPONENT HAS SUCESSFULLY COMPLETED MINIMUM NUMBER OF QUALIFICATION TESTS REQUIRED TO BE CONSIDERED SAFE FOR OPERATION DURING FLIGHT.
FULL QUALIFICTION (FQ) - COMPONENT HAS SUCESSFULLY COMPLETED SPECIFICATION QUALIFICATION TESTS.
FLIGHT WORTHY (FW) - COMPONENT IS NOT QUALIFIED FOR FUNCTIONAL USE DURING FLIGHT.
DSF-1820 (11-2000)* Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Approved Program Configuration Release
• Engineering Release Authority That Captures at a Top Level Modification/Configuration Changes to the A/C since last flight– Top level project/program release.– Signatures required dictated by plan and some optional dependent
on TRR/FRR actions.• Stress • System Safety
• Rev Letter Continues on Subsequent Release’s Thereby, Maintaining/Tacking Multiple Configuration Simultaneously.
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Configuration Release Notional
RELEASE AUTHORITY (RA)
CAGE CODE
78022 1. RELEASE AUTHORITY NO.
RA-IRAD-031 2. RA REV.
I/R 3. LIAISON RA
YES X NO 4. RELATED RA
n/a 5. RELEASE AUTHORITY TYPES
ERN DCN X ECO DVA 6. NETWORK NUMBER
NA 7. SHEET
1 of 1
8. STOP/LIFT ORDER
STOP LIFT PARTIAL LIFT
ESTIMATED LIFT DATE / /
9. CHANGE AUTHORITY
PCR N/A PCR
PCR PCR
10. CHANGE CLASS
CLASS I
CLASS II
11. REASON CODE
N/A
12. ECOS / RC/I INCORPORATED BY THIS DCN
13. RETROFIT/FIELD DOC REQUIRED
RETROFIT TCTO TO
14. TEMPORARY CONFIGURATION MODIFICATION
T2 MOD
15. DESCRIPTION OR REASON FOR CHANGE
GII AIRCRAFT S/N 0080, MODIFICATION/INCORPORATION PER ATTACHED FLIGHT TEST BED DRAWING TREE GII50A0001 Rev S. GII AIRFRAME AND POWER MODIFICATIONS WERE PERFORMED BY SUPPLER. DELVERED MASTER DRAWING LIST NG-0100, BROUGT INTO ACCOUNTABILITY WITHIN CM PLAN CREW CHIEF FERRY FLIGHT SEAT INSTALLED PER GULFSTREAM REQT’S (RACK 4L) .*RELEASED FOR NEW ENGINEERING INCORPORATIONS PRIOR TO FLIGHT 055*
16. MFG. PLANNING
YES NO
17. DF NO
18.
EFFECT SCHED
19. MODEL CODE
20. ENGINEERING EFFECTIVITY
CI NO SERIALIZATION RANGE
23. MANUFACTURING EFFECTIVITY
N/A
21. ENGINEERING CHANGE PROPOSAL APPLICABLE
ECP NUMBER 22. DEVIATION APPLICABLE
DEVIATION NUMBER
24. DOCUMENT/DWG NO
GII50F0001 25. DOCUMENT/DWG TITLE
NGC FLIGHT CONFIGURATION RELEASE 26. DOC/DWG REV
U 27. PL REV
N/A 28. NEXT ASSY PART NO (FOR REFERENCE ONLY)
G1159 29. NEXT ASSEMBLY FOLLOW-UP RA
YES ENTER SCHEDULED RA X NO
EF
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CAGE
CODE PART NUMBER NOMENCLATURE /
DESCRIPTION CUT STOCK SIZE
RAW MATERIAL
CODE SPECIFICATIONS ZO
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UID
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30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46.
47. ADDITIONAL DETAILED INSTRUCTIONS (FOR PARTS DISPOSITION, MANUFACTURING OR PROCUREMENT INSTRUCTIONS SUCH AS FOR REWORK, SPARES, AMRS, ETC)
REFERENCE FOLD DOCUMENT A7550P0005, REV C. A/C WEIGHT AND BALANCE REQUIRED PER GULF STREAM CMP, BEFORE FLIGHT AND AMENDED FOR SUBSEQUENT AIRCRAFT INSTALLATIONS. ATTACHED MATRIX INDICATES RA’S (DWG) RELEASED TO A/C ONLY ITEMS WITH SPECIFC PREP ITEMS HAVE BEEN INCORPORATED INTO A/C (N/A’S INDICATED CONFIGURATION TRACKING PURPOSES PER CM PLAN).
48. RELEASE AUTHORITY SIGNATURES
ORIGINATOR
M. FATTAL DATE
MATERIAL AND PROCESSES
DATE
/ / STRESS
DATE
/ / PROGRAM INTEGRATION
DATE
/ / DESIGN LEAD/MANAGER
DATE
/ / PROGRAM PLANNING
DATE
/ / PRODUCT ASSURANCE
DATE
12/15/09 PROGRAM MANAGEMENT
DATE
/ / CHECK
DATE
/ / PRODUCT SUPPORT/ILS
DATE
/ / SAFETY
DATE
/
/
SOFTWARE CONFIGURATION MGMT
DATE
/ / CHIEF ENGINEER
DATE
/ / MANUFACTURING ENGINEERING
DATE
/ / RELIABILITY
DATE
/ / SOFTWARE QUALITY ASSURANCE
DATE
/ / MASS PROPERTIES
DATE
/ / MEC
DATE
/ / MATERIEL
DATE
/ / RESPONSIBLE ORG TEST MGR
DATE
/ / SYS ENG/REQUIREMENTS MGMT
DATE
/ / BUSINESS MANAGEMENT
DATE / /
PRODUCT TEST
DATE
/ / DATA MANAGEMENT
DATE
/ / DADT
DATE
/ / PROGRAM MANAGER
DATE
/ / OTHER
DATE
/ / CONFIGURATION RELEASE
M. FATTAL DATE
/ /
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
IRAD -1 ASSIGNED RELEASE AUTHORITY NUMBERS
LAST UPDATE: APRIL 20,
RELEASE AUTHORITY NUMBER DWG NUMBER DWG REV DRAWING TITLE
DATE RA ASSIGNED
DATE DWG RELEASED Flt/P.I. NUMBER
RA-IRAD-001 GII50A0001 B A/V INSTALLATIONS 20-APR-10 21-APR-10 027-002/004
RA-IRAD-002 XXXX I/R IRAD TRANSDUCER INSTALLATION XXX XXX 027-003
RA-IRAD-003 XXXX I/R FTB INSTALLATION DRAWING XXX XXX N/A
RA-IRAD-004 XXXX N FLIGHT TEST BED DRAWING TREE XXX XXX N/A
RA-IRAD-005 GII50F0001 K NGC FLIGHT CONFIGURATION RELEASE XXX XXX N/A
RA-IRAD-006 XXXX IR FTB INSTALLATION DRAWING XXX XXX N/A
RA-IRAD-007 XXXX B FAIRING MOD XXX XXX 035-018
RA-IRAD-008 XXXX A A/V INSTALLATIONS XXX XXX N/A
RA-IRAD-009 XXXX IR A/V INSTALLATIONS XXX XXX N/A
RA-IRAD-010 XXXX A FTB INSTALLATION DRAWING XXX XXX N/A
RA-IRAD-011 XXXX I/R DEMONSTRATION SYSTEM ATP XXX XXX N/A
RA-IRAD-012 XXXX I/R IRAD MASTER DRAWING LIST XXX XXX 040-024
RA-IRAD-013 XXXX I/R NGC IRAD to FTB INSTALLATION DRAWING XXX XXX 040-024
RA-IRAD-014 XXXX S FLIGHT TEST BED DRAWING TREE XXX XXX N/A
RA-IRAD-015 GII50F0001 R NGC FLIGHT CONFIGURATION RELEASE XXX XXX N/A
RA-IRAD-016 XXXX I/R DETAIL, RACK 5L C/B PANEL DETAIL XXX XXX 052-024
RA-IRAD-017 XXXX I/R XYZ ENGINE RUN GROUND ATP XXX XXX 052-025
RA-IRAD-018 GII50HWSWCM 14 HARDWARE SOFTWARE COMPATIBILITY MATRIX XXX XXX 052-026
RA-IRAD-019 XXXX B INTERCOM SYSTEM MODIFICATION XXX XXX 054-003
RA-IRAD-020 XXXX B FTA XYZ MASTER DRAWING LIST XXX XXX N/A
RA-IRAD-021 XXXX A UHF COM SYSTEM INSTALLATION XXX XXX 054-003
Engineering Release Tracking Matrix (Notational)
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Flight Prep Sheet used to Track Configuration Changes on Vehicle
FLIGHT PREPARATION SHEET DATE
PREP ITEM NUMBER
JCN
MODEL NUMBER
SERIAL NUMBER
FLIGHT NUMBER.
CONFIGURATION CHANGE
HARDWARE
SOFTWARE
INSTRUMENTATION CHANGE
HARDWARE PLANNING ITEM W & B
SOFTWARE FRACAS ITEM OTHER REFERENCE DOCUMENTS
ZONE
RELATED FILES
PILOT SQUAWK DELAYED ACTION DCN/ADCN LTWO
INSP. SQUAWK OK FOR FLIGHT ITWO
INSP OK TASK DESCRIPTIONS
TEST SHOP INSP
AUTHORIZED BY
SPECIAL COMMENTS
ENTERED IN DATABASE (INITIAL)
OK TO FILE (STAMP)
DSF-1718 (6-01)*
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Interior Configuration Example
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Interior Configuration Example
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Interior Configuration Example
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Interior Configuration Example
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Summary
• This CM Approach Has a Proven History of Success.– Several programs concurrently tracked on our GII.– Other programs have adopted this methodology
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10
Questions
• Questions
Approved for Public Release: Northrop Grumman Aerospace Systems Case 10-0617 Dated 5/5/10