FSC: 1510 - Aircraft, Fixed Wing
AC90-89 B - AC 90-89B, ADVISORY CIRCULAR: AMATEUR-BUILT AIRCRAFT AND ULTRALIGHT FLIGHT TESTING HANDBOOK (27-APR-2015)
AC 00-34 A - AC 00-34A, ADVISORY CIRCULAR: AIRCRAFT GROUND HANDLING AND SERVICING (29 JUL 1974)
AC 43.13-1 B - AC 43.13-1B (W/ CHANGE 1), ADVISORY CIRCULAR: ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR (08 SEP 1998)
TR-79-3021 A - AFFDL-TR-79-3021 (REV. A), USAF DAMAGE TOLERANT DESIGN HANDBOOK: GUIDELINES FOR THE ANALYSIS AND DESIGN OF DAMAGE TOLERANT AIRCRAFT STRUCTURES (MAR-1979) [SUPERSEDED BY AFWAL-TR-82-3073 (REV. B)]
AFGS-87221 A - AFGS-87221A (NOTICE 1), AIR FORCE GUIDE SPECIFICATION: AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR (01-JUN-1999) [S/S BY JSSG-2006]
AFGS-87235 B - AFGS-87235B (NOTICE-1), U.S. AIR FORCE GUIDE SPECIFICATION: EMERGENCY ESCAPE, AIRCRAFT (08-OCT-1999) [S/S BY JSSG-2110/11]
TR-82-3073 B - AFWAL-TR-82-3073 (REV. B), USAF DAMAGE TOLERANT DESIGN HANDBOOK: GUIDELINES FOR THE ANALYSIS AND DESIGN OF DAMAGE TOLERANT AIRCRAFT STRUCTURES (MAY 1984)
AFWAL-TR-83-3027 - AFWAL-TR-83-3027, USAF DURABILITY DESIGN HANDBOOK: GUIDELINES FOR THE ANALYSIS AND DESIGN OF DURABLE AIRCRAFT STRUCTURES (JAN 1984)
CT93-69_VOL-I - DOT/FAA/CT-93/69.I (DOT-VNTSC-FAA-93-13.I), DAMAGE TOLERANCE ASSESSMENT HANDBOOK: VOLUME I - INTRODUCTION, FRACTURE MECHANICS AND FATIGUE CRACK PROPAGATION (OCT 1993)
CT-93/69.II - DOT/FAA/CT-93/69.II (DOT-VNTSC-FAA-93-13.II), DAMAGE TOLERANCE ASSESSMENT HANDBOOK: VOLUME II - AIRFRAME DAMAGE TOLERANCE EVALUATION (OCT 1993)
DOT/FAA/AR-05/15 - DOT/FAA/AR-05/15, FATIGUE CRACK GROWTH DATABASE FOR DAMAGE TOLERANCE ANALYSIS (AUG 2005)
DOT/FAA/AR-03/74 2004 - DOT/FAA/AR-03/74, BONDED REPAIR OF AIRCRAFT COMPOSITE SANDWICH STRUCTURES (FEB-2004) (FINAL REPORT)
FTC-TD-73-2 - FTC-TD-73-2, TECHNOLOGY DOCUMENT: BACKGROUND INFORMATION AND USER GUIDE FOR MIL-S-83691 (MAR-1974)
MIL-A-8421 F - MIL-A-8421F (NOTICE 1), MILITARY SPECIFICATION: AIR TRANSPORTABILITY REQUIREMENTS, GENERAL SPECIFICATION FOR (28 MAY 1987) [S/S BY MIL-STD-1791]
MIL-A-8806 A - MIL-A-8806A, MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (11 JUL 1966) [REFER TO MIL-STD-1789]
MIL-A-8806 A - MIL-A-8806A (AMENDMENT 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (12 SEP 1967) [REFER TO MIL-STD-1789]
MIL-A-8806 A - MIL-A-8806A (NOTICE 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (10 SEP 1997) [REFER TO MIL-STD-1789]
MIL-A-8860 B - MIL-A-8860B, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20-MAY-1987) [SUPERSEDES MIL-S-5700]
MIL-A-008861 A - MIL-A-008861A (NOTICE-1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (06-FEB-1986) [S/S BY MIL-A-87221]
MIL-A-8861 B - MIL-A-8861B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (7 FEB 1986)
MIL-A-8861 B - MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)
MIL-A-8861 B - MIL-A-8861B (NOTICE-1), DETAIL SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (09-JUL-2019)
MIL-A-8863 B - MIL-A-8863B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (06 MAY 1987) [SUPERSEDING MIL-A-8862]
MIL-A-8863 C - MIL-A-8863C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (19 JUL 1993)
MIL-A-8863 C - MIL-A-8863C (NOTICE-1), DETAIL SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (09-JUL-2019)
MIL-A-8864 - MIL-A-8864 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY WATER AND HANDLING LOADS FOR SEA PLANES (10 JUN 1982) [NO S/S DOCUMENT]
MIL-A-8865 B - MIL-A-8865B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20-MAY-1987) [SUPERSEDING MIL-A-008865A AND MIL-S-5705]
MIL-A-8866 C - MIL-A-8866C (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE
MIL-A-8866 C - MIL-A-8866C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE (20 MAY 19
MIL-A-8867 C - MIL-A-8867C (AMENDMENT 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993)
MIL-A-8867 C - MIL-A-8867C, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (23 MAR 1987)
MIL-A-8867 C - MIL-A-8867C (NOTICE 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (03-OCT-1994)
MIL-A-8868 B - MIL-A-8868B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (20-MAY-1987) [SUPERSEDING MIL-A-8868] [NO S/S DOCUMENT]
MIL-A-8868 B - MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24-MAY-1991) [NO S/S DOCUMENT]
MIL-A-8868 B - MIL-A-8868B (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (04-MAY-1998) [NO S/S DOCUMENT]
MIL-A-8869 B - MIL-A-8869B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (20-MAY-1987)
MIL-A-8869 B - MIL-A-8869B (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (20-JUN-1994)
MIL-A-8870 A - MIL-A-8870A (NOTICE-1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLUTTER, DIVERGENCE, AND OTHER AEROELASTIC INSTABILITIES (18-MAY-1987)
MIL-A-8870 B - MIL-A-8870B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (20-MAY-1987)
MIL-A-8870 C - MIL-A-8870C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)
MIL-A-8871 A - MIL-A-8871A, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (01 JUL 1971) [S/S BY MIL-A-87221]
MIL-A-8871 A - MIL-A-8871A (NOTICE 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (18 MAY 1987) [S/S BY MIL-A-87221]
MIL-A-8892 - MIL-A-8892 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, VIBRATION (18 MAY 1987) [S/S BY MIL-A-87221]
MIL-A-8893 - MIL-A-8893 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY , SONIC FATIGUE (18-MAY-1987) [SUPERSEDED BY MIL-A-87221]
MIL-D-8708 B - MIL-D-8708B, MILITARY SPECIFICATION: DEMONSTRATION REQUIREMENTS FOR AIRPLANES (31 JAN 1969)
MIL-D-8708 B - MIL-D-8708B (AMENDMENT 1) MILITARY SPECIFICATION: DEMONSTRATION REQUIREMENTS FOR AIRPLANES (03 JUN 1982)
MIL-D-8708 C - MIL-D-8708C, MILITARY SPECIFICATION: DEMONSTRATION: AIRCRAFT WEAPON SYSTEMS, GENERAL SPECIFICATION FOR (12 AUG 1991)
MIL-E-87235 - MIL-E-87235 (NOTICE-1), MILITARY SPECIFICATION: EMERGENCY ESCAPE, AIRCRAFT (15-MAR-1989) [S/S BY AFGS-87235]
MIL-F-83691 A - MIL-F-83691A, MILITARY SPECIFICATION: FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR DEPARTURE RESISTANCE AND POST-DEPARTURE CHARACTERISTICS OF PILOTED AIRPLANES (15-APR-1972) [NO S/S DOCUMENT]
MIL-F-83691 B - MIL-F-83691B, MILITARY SPECIFICATION: FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR DEPARTURE RESISTANCE AND POST-DEPARTURE CHARACTERISTICS OF PILOTED AI
MIL-F-83691 B - MIL-F-83691B (NOTICE 1), MILITARY SPECIFICATION: FLIGHT TEST DEMONSTRATION REQUIREMENTS FOR DEPARTURE RESISTANCE AND POST-DEPARTURE CHARACTERISTICS OF
MIL-HDBK-1791 - MIL-HDBK-1791, DEPARTMENT OF DEFENSE HANDBOOK: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (17 FEB 1997) (SUPERSEDES MIL-STD-1791)
MIL-HDBK-1791 - MIL-HDBK-1791 (NOTICE-1), DEPARTMENT OF DEFENSE HANDBOOK: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (19-DEC-2012) [S/S BY MIL-STD-1791A]
MIL-HDBK-1793 - MIL-HDBK-1793 (NOTICE-1), DEPARTMENT OF DEFENSE HANDBOOK: FLIGHT PERFORMANCE, AIR VEHICLE (29-MAY-2003) [S/S BY MIL-STD-3013]
MIL-HDBK-2066 - MIL-HDBK-2066 (NOTICE 2), MILITARY HANDBOOK: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (17 MAR 1999) [SUPERSEDIN
MIL-HDBK-2066 - MIL-HDBK-2066, DEPARTMENT OF DEFENSE HANDBOOK: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (07 MAR 1999) [SUPERSED
MIL-S-8698 - MIL-S-8698, MILITARY SPECIFICATION: STRUCTURAL DESIGN REQUIREMENTS, HELICOPTERS (ASG) (01 JUL 1954) [NO S/S DOCUMENT]
MIL-A-8806 B - MIL-A-8806B, MILITARY SPECIFICATION: SOUND PRESSURE LEVELS IN AIRCRAFT, GENERAL SPECIFICATION FOR (21 SEP 1970) [MIL-S-008806B USED IN LIEU OF MIL-A-8806A] [S/S BY MIL-STD-1789]
MIL-A-8806 B - MIL-A-8806B (NOTICE 1), MILITARY SPECIFICATION: SOUND PRESSURE LEVELS IN AIRCRAFT, GENERAL SPECIFICATION FOR (21 SEP 1970) [MIL-S-008806B USED IN LIEU OF MIL-A-8806A] [S/S BY MIL-STD-1789]
MIL-A-83444 - MIL-A-83444 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE DAMAGE TOLERANCE REQUIREMENTS (27-MAR-1987) [S/S BY MIL-A-87221]
MIL-STD-203 G - MIL-STD-203F, MILITARY STANDARD: AIRCREW STATION CONTROLS AND DISPLAYS: LOCATION, ARRANGEMENT AND ACTUATION OF, FOR FIXED WING AIRCRAFT (28 DEC 1973)
MIL-STD-203 G - MIL-STD-203G, MILITARY STANDARD: AIRCREW STATION CONTROLS AND DISPLAYS: LOCATION, ARRANGEMENT AND ACTUATION OF, FOR FIXED WING AIRCRAFT (1 MAR 1991)
MIL-STD-1791 - MIL-STD-1791 (NOTICE 3), MILITARY STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (14 FEB 1997) [S/S BY MIL HDBK-1791]
MIL-STD-1791 - MIL-STD-1791 (NOTICE 2), MILITARY STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (23 MAR 1995) [S/S BY MIL HDBK-1791]
MIL-STD-1791 - MIL-STD-1791 (NOTICE 1), MILITARY STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (15 APR 1986) [S/S BY MIL HDBK-1791]
MIL-STD-1791 A - MIL-STD-1791A, DEPARTMENT OF DEFENSE INTERFACE STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (19-NOV-2012)
MIL-STD-1791 B - MIL-STD-1791B, DEPARTMENT OF DEFENSE INTERFACE STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (02-DEC-2014)
MIL-STD-1791 C - MIL-STD-1791C, DEPARTMENT OF DEFENSE INTERFACE STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (23-OCT-2017)
MIL-STD-1791 C_CHG-1 - MIL-STD-1791C (W/ CHANGE-1), DEPARTMENT OF DEFENSE INTERFACE STANDARD: DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT (29-DEC-2017)
MIL-STD-1793 - MIL-STD-1793 (NOTICE-2), DEPARTMENT OF DEFENSE MILITARY STANDARD: FLIGHT PERFORMANCE, AIR VEHICLE (19-DEC-1997) [S/S BY MIL-HDBK-1793]
MIL-STD-2066 - MIL-STD-2066, MILITARY STANDARD: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (20 MAR 1981) [S/S BY MIL-HDBK-2066]
MIL-STD-2066 - MIL-STD-2066 (NOTICE 1), MILITARY STANDARD: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (08 MAR 1982) [S/S BY MIL
MIL-STD-2066 - MIL-STD-2066 (NOTICE 2), MILITARY STANDARD: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (17 MAR 1999) [S/S BY MIL-HDBK-2066]
MIL-T-7378 A - MIL-T-7378A, MILITARY SPECIFICATION: TANK, FUEL, AIRCRAFT, EXTERNAL, AUXILIARY, REMOVEABLE (20-OCT-1958) [NO S/S DOCUMENT]
MS33573 B - MS33573B, MILITARY STANDARD: DIMENSION, CLEARANCE, COCKPIT, FIXED WING AIRCRAFT (27 JUN 1978) [S/S BY MIL-STD-1333 FOR ARMY AND DH2-2 FOR AIR FORCE]
MS33574 - MS33574B, MILITARY STANDARD: DIMENSIONS, BASIC, COCKPIT, STICK-CONTROLLED, FIXED WING AIRCRAFT (02 JUL 1969)
MS33574 B - MS33574B (NOTICE 2), MILITARY STANDARD: DIMENSIONS, BASIC, COCKPIT, STICK-CONTROLLED, FIXED WING AIRCRAFT (07 MAY 1997)
MS33574 B - MS33574B (NOTICE 1), MILITARY STANDARD: DIMENSIONS, BASIC, COCKPIT, STICK-CONTROLLED, FIXED WING AIRCRAFT (25 AUG 1987)
MS33574 B - MS33574B (NOTICE-3), MILITARY SPECIFICATION SHEET: DIMENSIONS, BASIC, COCKPIT, STICK-CONTROLLED, FIXED WING AIRCRAFT (20-JAN-2013) [NO S/S DOCUMENT]
MS33576 B - MS33576B, MILITARY STANDARD: DIMENSION, BASIC, COCKPIT, WHEEL CONTROLLED, FIXED WING AIRCRAFT (27 JAN 1978) [S/S BY MIL-STD-1333 FOR ARMY & NAVY AND DH2-2 FOR AIR FORCE]
TM 1-1500-204-23-8 CHG-1 - TM 1-1500-204-23-8 (W/ CHANGE-1), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (MACHINE AND WELDING SHOP PRACTICES) - VOLUME 8 (15-MAR-2001)
TM 1-1500-204-23-4 CHG-5 - TM 1-1500-204-23-4 (W/ CHG-5), TECHNICAL MANUAL AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (ELECTRICAL AND INSTRUMENT MAINTENANCE PROCEDURES AND PRACTICES) - VOLUME 4 (08-JUN
TM 1-1500-204-23-3 CHG-3 - TM 1-1500-204-23-3 (W/ CHG-3), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (MAINTENANCE PRACTICES FOR FUEL AND OIL SYSTEMS) - VOLUME 3 (30-NOV-2006)
TM 1-1500-204-23-6 CHG-4 - TM 1-1500-204-23-6 (W/ CHANGE-4), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (HARDWARE AND CONSUMABLE MATERIALS) - VOLUME 6 (20-AUG-2004)
TM 1-1500-204-23-1 CHG-1 - TM 1-1500-204-23-1 (W/ CHANGE-1), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (GENERAL MAINTENANCE AND PRACTICES) - VOLUME 1 (01-MAR-2000)
TM 1-1500-204-23-2 CHG-3 - TM 1-1500-204-23-2 (W/ CHANGES 1 AND 2), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (PNEUDRAULICS MAINTENANCE AND PRACTICES) - VOLUME 2 (29-JAN-1999)
TM 1-1500-204-23-10 CHG-3 - TM 1-1500-204-23-10 (W/ CHANGE-3), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (SHEET METAL SHOP PRACTICES) - VOLUME 10 (20-AUG-2004)
TM 1-1500-204-23-5 CHG-3 - TM 1-1500-204-23-5 (W/ CHANGE-3), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (PROPELLER, ROTOR, AND POWERTRAIN MAINTENANCE PRACTICES) - VOLUME 5 (15-JUN-1999
TM 1-1500-204-23-9 CHG-4 - TM 1-1500-204-23-9 (W/ CHANGE-4), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (TOOLS AND GROUND SUPPORT EQUIPMENT) - VOLUME 9 (15-MAR-2001)
TM 1-1500-204-23-10 CHG-4 - TM 1-1500-204-23-10 (W/ CHANGE-4), TECHNICAL MANUAL: AVIATION UNIT MAINTENANCE (AVUM) AND AVIATION INTERMEDIATE MAINTENANCE (AVIM) MANUAL FOR GENERAL AIRCRAFT MAINTENANCE (SHEET METAL SHOP PRACTICES) - VOLUME 10 (08-MAR-2010)
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