MIL-A-81973 Base Document:1974
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document)
Available format(s)
PDF
Published date
31-05-1974
Publisher
Withdrawn date
04-09-1996
€16.67
Excluding VAT
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Describes the requirements for the design, construction and instrumentation of track-type test vehicles used in performance/service release testing, including underwater testing, of aircrew automated escape systems in accordance with the test requirements of MIL-E-9426.
| DevelopmentNote |
NOTICE 1 - Notice of Cancellation without replacement. (06/2004)
|
| DocumentType |
Standard
|
| Pages |
48
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification establishes the requirements for the design, construction and instrumentation of track-type test vehicles used in performance/service release testing, including underwater testing, of aircrew automated escape systems in accordance with the test requirements of MIL-E-9426.
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| MIL-E-9426 Revision F:1978 | Escape System, Requirements Conformance Demonstrations and Performance Tests for, General Specification for (No S/S Document) |
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| MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (SEE NAS410 AS A POSSIBLE REPLACEMENT) |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| MIL-HDBK-700 Revision A:1975 | Plastics |
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| MIL-T-5021 Revision D:1969 | TEST, AIRCRAFT AND MISSILE WELDING OPERATORS QUALIFICATION (SEE MIL-STD 1595) |
| MIL D 8634 : LATEST | DECALCOMANIAS, AIRCRAFT, FOR USE ON EXTERIOR SURFACES |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| MIL-A-25463 Revision B:1982 | Adhesive, Film Form, Metallic Structural sandwich Construction (S/S by SAE-AMS-A-25463) |
| FED-STD-406 Revision A:1982 | PLASTICS: METHODS OF TESTING (S/S BY - SEE CANCELLATION NOTICE FOR RECOMMENDED SUPERSEDING ASTM TEST METHODS) |
| MIL-F-7190 Revision B:1985 | Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| QQ-M-40 Revision B:1962 | MAGNESIUM ALLOY FORGINGS (S/S BY ASTM-B91 AND ASTM-B661) |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| MIL-M-6857 Revision D:1990 | Magnesium Alloy Castings, Heat Treatment of (S/S by SAE-AMS2768) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING, POSITIVE-LOCKING (S/S BY NASM23460) |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL HDBK 52 : B | EVALUATION OF CONTRACTORS CALIBRATION SYSTEM |
| MIL-STD-403 Revision C:1992 | Preparation for and Installation of Rivets and Screws, Rocket, Missile, and Airframe Structures |
| MIL-STD-401 Revision B:1967 | SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS (S/S BY SAE-AMS-STD-401) |
| MIL-STD-865 Revision D:2007 | Selective Brush Plating, Electro-Deposition |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING, BLANK (S/S BY A-A-50271) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL S 23586 : E | SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
| MIL-A-21180 Revision D:1984 | Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180) |
| MIL-W-8611 Revision A:1957 | WELDING, METAL ARC AND GAS, STEELS, AND CORROSION AND HEAT RESISTANT ALLOYS; PROCESS FOR (S/S BY MIL-STD-2219) |
| DOD-D-1000 Revision B:1977 | Drawings, Engineering and Associated Lists (S/S by MIL-DTL-31000) |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| MIL-STD-490 Revision A:1985 | SpecificationPractices (S/S by MIL-STD-961) |
| MIL-H-6088 Revision G:1991 | Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088) |
| MIL-C-5501 Revision G:1989 | Caps and Plugs, Protective, Dust and Moisture Seal, General Specification for (S/S by NAS847) |
| MIL-HDBK-691 Revision B:1987 | Adhesive Bonding |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-STD-22 Revision D:1979 | WELDED JOINT DESIGN |
| MIL-STD-21 Revision A:1968 | WELDED-JOINT DESIGNS, ARMORED-TANK TYPE (S/S BY MIL-HDBK-21) |
| MIL D 1000/1 : LATEST | DRAWING, ENGINEERING & ASSOCIATED DATA |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL-HDBK-132 Revision A:1984 | Protective Finishes for Metal and Wood Surfaces (No S/S Document) |
| MIL-HDBK-17-1 Revision F:2002 | Composite Materials Handbook Volume 1 - Polymer Matrix Composites Guidelines or Characterization of Structural Materials (S/S by SAE-R422) |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL N 25027 : G | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-B-23964 Revision D:1981 | Bolt, Self-Retaining, Positive Locking (S/S by NASM23964) |
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