MIL-A-8882A (NOTICE 1)

MIL-A-8882A (NOTICE 1), MILITARY SPECIFICATION: ALUMINUM ALLOY PLATE AND SHEET, 2020 (06 DEC 1974) [NO S/S DOCUMENT]., Specification MIL-A-8882A (ASG), dated 29 March 1963, is hereby cancelled . The document is no longer required. There is nosuperseding d

MIL-HDBK-130B (NOTICE 1)

MIL-HDBK-130B (NOTICE 1), MILITARY STANDARDIZATION HANDBOOK: STANDARDIZED GASOLINE AND DIESEL ENGINES (24 OCT 1975)., MIL-HDBK-130B, dated 22 April 1964, is hereby canceled. There is no superseding document.

MIL-HDBK-129 (NOTICE 1)

MIL-HDBK-129 (NOTICE 1) DEPARTMENT OF DEFENSE HANDBOOK MILITARY MARKING., MIL-HDBK-129, dated 15 May 1997, is hereby canceled. Future acquisitions should refer to MIL-STD-129, Military Marking for Shipment and Storage, Standard Practice.

MIL-HDBK-118 (NOTICE 1

MIL-HDBK-118 (NOTICE 1, MILITARY HANDBOOK: DESIGN GUIDE FOR MILITARY APPLICATIONS OF HYDRAULIC FLUIDS (13 APR 2004)., MIL-HDBK-118, dated 22 September 1993, has been reviewed and determined to be valid for use in acquisition

MIL-HDBK-115 (NOTICE 1)

MIL-HDBK-115 (NOTICE 1), MILITARY HANDBOOK: U.S. ARMY REVERSE ENGINEERING HANDBOOK (GUIDELINES AND PROCEDURES) (24 OCT 2000)., MIL-HDBK-115, dated 20 April 1987, has been reviewed and determined to be valid for use in acquisition.

MIL-HDBK-114A (NOTICE 1)

MIL-HDBK-114A (NOTICE 1), MILITARY HANDBOOK FUELS, MOBILITY, USER HANDBOOK (12 APR 1990)., MIL-HDBK-114A, dated 20 July 1990, has been reviewed and determined to be valid for use in acquisition

MIL-HDBK-113C (NOTICE 1)

MIL-HDBK-113C (NOTICE 1), MILITARY HANDBOOK, GUIDE FOR SELECTION OF LUBRICANTS, FUNCTIONAL FLUIDS, PRESERVATIVES AND SPECIALTY PRODUCTS FOR USE IN GROUND EQUIPMENT SYSTEMS (12 APR 2004)., MIL-HDBK-113C, dated 24 April 1989, has been reviewed and determine

MIL-HDBK-110 (NOTICE-1)

MIL-HDBK-110 (NOTICE-1), MILITARY HANDBOOK, CHAINS, POWER TRANSMISSION AND CONVEYING, APPLICATION, INSTALLATION, AND MAINTENANCE (1 FEB 1982).

MIL-HDBK-107 (NOTICE 1)

MIL-HDBK-107 (NOTICE 1), INSPECTION QUALITY CONTROL SINGLE LEVEL CONTINUOUS SAMPLING PROCEDURES & TABLES FOR INSPECTION BY ATTRIBUTES (11 FEB 1983) [S/S BY MIL-STD-1235]., MIL-HDBK-107, dated 30 April 1959, is hereby canceled. MIL-STD-1235 provides for si

HDBK-106 (NOTICE 1)

MIL-HDBK-106 (NOTICE 1), MILITARY HANDBOOK: MULTI-LEVEL CONTINUOUS SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES (16 SEP 1986)., MIL-HDBK-106, dated 31 October 1958, is superseded by MIL-STD-1235.

MIL-A-8871A (NOTICE 1)

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-8871A(USAF) dated 1 July 1971 is hereby canceled. For futureprocurements, see MIL-A-87221 Aircraft

MIL-A-8871A

MIL-A-8871A, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS TESTS (01 JUL 1971) [S/S BY MIL-A-87221]., This specification covers the flight test requirements for the structural integrity flight and ground evaluation a

MIL-A-8870C

MIL-A-8870C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE (25 MAR 1993)., This specification contains the general and detail designrequirements and criteria in the design and construction of airplanes to:a. Pre

MIL-A-8869B

MIL-A-8869B, MILITARY SPECIFICATION AIRPLANE STRENGTH AND RIGIDITY NUCLEAR WEAPONS EFFECTS (20 MAY 1987)., This specification establishes the basic nuclear weapons effects requirements for airplanes which are Intended to deliver nuclear weapons or operate

MIL-A-8868B

MIL-A-8868B, MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (20 MAY 1987)., This specification contains the requirements for data necessary to show compliance with the design and test requirements of MIL-A-8860 through MIL-A-8870

MIL-A-8868B (AMENDMENT 1)

MIL-A-8868B (AMENDMENT 1), MILITARY SPECIFICATION, AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS (24 MAY 1991).

MIL-A-8867C (AMENDMENT 1)

MIL-A-8867C (AMENDMENT 1), MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (25 MAR 1993).

MIL-A-8867C

MIL-A-8867C, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY GROUND TESTS (23 MAR 1987)., This specification contains the requirements which, in combination with other applicable specifications, define the ground tests required for structural evalu

MIL-A-8866C (NOTICE 1)

MIL-A-8866C (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE (03 OCT 1994)., MIL-A-8866C(AS),dated 20 May 1987. has been reviewed and determined to bevalid for use i

MIL-A-8866C

MIL-A-8866C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE, AND DAMAGE TOLERANCE (20 MAY 1987)., This specification defines the strength and rigidity requirements for repeated loading condition ap

MIL-A-8865B

MIL-A-8865B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, MISCELLANEOUS LOADS (20 MAY 1987) [SUPERSEDING MIL-S-5705]., This specification contains the strength and rigidity requirements for miscellaneous loads applicable to acquisition of airpl

MIL-A-8864 (NOTICE 1)

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]., Specification MIL-A-8864 (ASG), dated 18 May 1960, is hereby canceled without replacement.

MIL-A-8863C

MIL-A-8863C, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (19 JUL 1993)., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the follow

MIL-A-8863B

MIL-A-8863B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES (06 MAY 1987)., This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the follow

MIL-A-8861B (AMENDMENT 1)

MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)., This amendment forms a part of MIL-A-886lB(AS), dated7 February 1986, and is approved for use within the Naval Air SystemsCommand, Department of

MIL-A-8861B

MIL-A-8861B, MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (7 FEB 1986)., This specification covers the requirements for strength and rigidity for flight loading conditions applicable to airplanes.

MIL-A-8860B

MIL-A-8860B, MILITARY SPECIFICATION: AIRCRAFT STRENGTH AND RIGIDITY, GENERAL SPECIFICATION FOR (20 MAY 1987) [SUPERSEDES MIL-S-5700]., This specification contains general requirements, which, in combination with other applicable specifications, define the

MIL-A-8836B (NOTICE 1)

MIL-A-8836B (NOTICE 1), MILITARY SPECIFICATION: ABBREVIATED SUMMARY BILL OF MATERIALS FOR ITEMS IN DEPARTMENTS OF THE ARMY, NAVY, AND AIR FORCE CONTRACTS (18 MAY 1987) [S/S BY MIL-STD-295]., MIL-A-8836 dated 30 April 1971 and amendment 2 dated 22 January

MIL-A-8806A (NOTICE 1)

MIL-A-8806A (NOTICE 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (10 SEP 1997) [REFER TO MIL-STD-1789]., This notice should be filed in front of MIL-A-8806A, dated 11 July 1966, and Amendment-1, dated 12 Septem

MIL-A-8806A (AMENDMENT 1)

MIL-A-8806A (AMENDMENT 1), MILITARY SPECIFICATION: ACOUSTICAL NOISE LEVEL IN AIRCRAFT, GENERAL SPECIFICATION FOR (12 SEP 1967) [REFER TO MIL-STD-1789].