MIL-B-1083D

MIL-B-1083D, MILITARY SPECIFICATION, BALLS, BEARING, FERROUS AND NON-FERROUS (FOR USE IN BEARINGS, VALVES AND BEARING APPLICATIONS) GENERAL SPECIFICATION FOR (16 OCT 1987) [S/S BY ASTM F 2215]., This specification covers requirements for ferrous and non-f

MIL-B-1083D (SUPPLEMENT 1)

MIL-B-1083D (SUPPLEMENT 1), MILITARY SPECIFICATION, BALLS, BEARING, FERROUS AND NON-FERROUS (FOR USE IN BEARINGS, VALVES AND BEARING APPLICATIONS) GENERAL SPECIFICATION FOR (16 OCT 1987) [S/S BY ASTM F 2215].

MIL-B-1083D (SUPPLEMENT 1)

MIL-B-1083D (SUPPLEMENT 1), MILITARY SPECIFICATION, BALLS, BEARING, FERROUS AND NON-FERROUS (FOR USE IN BEARINGS, VALVES AND BEARING APPLICATIONS) GENERAL SPECIFICATION FOR (16 OCT 1987) [S/S BY ASTM F 2215].

MIL-B-10122E

MIL-B-10122E, MILITARY SPECIFICATION: BARGE, LIQUID CARGO: NONPROPELLED, STEEL, OFFSHORE, 4,160-BARREL, 120 FOOT, DESIGN 231C (16 JAN 1991)., This specification covers a liquid cargo, non-propelled, steel barge.

MIL-B-7883C (NOTICE 1)

MIL-B-7883C (NOTICE 1), MILITARY SPECIFICATION: BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM, AND ALUMINUM ALLOYS (17 SEP 1996) [MIL-B-007883C USED IN LIEU OF MIL-B-7883B] [S/S BY AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7)]., MIL-B-00

MIL-B-7883C

MIL-B-7883C, MILITARY SPECIFICATION: BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM, AND ALUMINUM ALLOYS (30 JUL 1986) [MIL-B-007883C USED IN LIEU OF MIL-B-7883B] [S/S BY AWS-C3.4, AWS-C3.5, AWS-C3.6 and AWS-C3.7)]., This specification

MIL-A-83444 (NOTICE 1)

MIL-A-83444 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE DAMAGE TOLERANCE REQUIREMENTS (27 MAR 1987) [S/S BY MIL-A-87221]., MIL-A-83444(USAF) dated 2 July 1974 is hereby canceled. For future procurements, see MIL-A-87221 Aircraft Structures.

MIL-A-8806B (NOTICE 1)

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-S-008806B(USAF), dated 21 September 1970, is hereby canceled

MIL-A-8806B

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]., This specification covers the general requirements for maximum allowable so

MIL-A-9962A (NOTICE 1)

MIL-A-9962A (NOTICE 1), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1996) [S/S by A-A-58054]., MIL-A-9962A (4), dated 5 APRIL 1977, is hereby canceled. Future acquisitions should be made using the current revision of A-A-58054.

MIL-A-9962A (AMENDMENT 4)

MIL-A-9962A (AMENDMENT 4), MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (05 APR 1977) [S/S by A-A-58054]., This amendment forms a of Military Specification MIL-A-9962A, dated 1 December 1966, and is approved for use by all Departments a

MIL-A-9962A

MIL-A-9962A, MILITARY SPECIFICATION: ABRASIVE MATS, NON-WOVEN, NON-METALLIC (01 DEC 1966) [S/S BY S/S by A-A-58054]., This specification covers non-woven, non-metallic mats made of nylon fiber which are bonded together with waterproof adhesives containing

MIL-A-9117D

MIL-A-9117D, MILITARY SPECIFICATION: ADHESIVE; SEALING, FOR AROMATIC FUEL CELLS AND GENERAL REPAIR (19 APR 1971) [S/S BY MIL-PRF-9117E]., This specification covers a one-part sealing adhesive for fuel cell repair workand for other general repairs where re

MIL-A-9080

MIL-A-9080, MILITARY SPECIFICATION, ANTENNA, LIAISON COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF (2 FEB 1954)., This specification covers the performance requirements for the design of airborne antennas for use with liaison communication

MIL-A-907E (AMENDMENT 1)

MIL-A-907E (AMENDMENT 1), PERFORMANCE SPECIFICATION: ANTISEIZE THREAD COMPOUND, HIGH TEMPERATURE (13 JAN 1993) [S/S BY MIL-PRF-907F]., This amendment forms a part of MIL-A-907E, dated 18 June 1985, and is approved for use by the Naval Sea Systems Command,

MIL-A-907E (aka MIL-PRF-907E)

MIL-A-907E (aka MIL-PRF-907E), MILITARY SPECIFICATION: ANTISEIZE THREAD COMPOUND, HIGH TEMPERATURE (18 JUN 1985) [S/S BY MIL-PRF-907F]., This specification covers antiseize compound for use on threads of steel nuts, studs, bolts and other mating surfaces,

MIL-A-8892 (NOTICE 1)

MIL-A-8892 (NOTICE 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY, VIBRATION (18 MAY 1987) [S/S BY MIL-A-87221]., MIL-A-8892(USAF) dated 31 March 1971 and amendment 1 dated 16 November 1971are hereby canceled. For future procurement, see MIL-

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-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