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MIL-A-23121 Revision C:1970

Withdrawn

Withdrawn

Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document)

Available format(s)

PDF

Published date

06-23-1970

Withdrawn date

09-11-1996

US$20.00
Excluding Tax where applicable

1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES

Describes the general requirements for the design, construction, installation, and performance of aircraft cockpit capsule aircrew environmental, escape and survival systems.

DevelopmentNote
C NOTICE 1 - Notice of Cancellation without replacement. (05/2004)
DocumentType
Standard
Pages
63
PublisherName
US Military Specs/Standards/Handbooks
Status
Withdrawn

This specification establishes the general requirements for the design, construction, installation, and performance of aircraft cockpit capsule aircrew environmental, escape and survival systems.

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MIL-HDBK-2067 Base Document:1999 Aircrew Automated Escape Systems Reliability and Maintainability (R/M) Program Requirements for
MIL-A-81815 Base Document:1974 Aircrew Automated Escape Systems, General Specification for (No S/S Document)
MIL-A-81573 Base Document:1968 Aircrew Escape System Descriptive and Performance Data Presentations, Requirement and Formats for General Specification (No S/S Document)
MIL-STD-1333 Revision B:1987 AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT (NO S/S DOCUMENT)
MIL-P-83126 Revision A:1980 PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
MIL-STD-2067 Base Document:1978 AIRCREW AUTOMATED ESCAPE SYSTEMS RELIABILITY AND MAINTAINABILITY (R/M) PROGRAM REQUIREMENTS FOR (S/S BY MIL-HDBK-2067)
MIL-E-18927 Revision E:1983 Environmental Control Systems, Aircraft, General Requirements for
MIL-D-19326 Revision H:1990 Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for

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MIL-STD-1166 Revision A:1991 Radiographic Testing Requirements for Solid Propellants
MIL-H-6875 Revision H:1989 Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875)
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MIL-M-18012 Revision B:1964 Markings for Aircrew Station displays Design and Configuration of (S/S by SAE-AS18012)
MIL-A-9067 Revision C:1961 Adhesive Bonding, Process and Inspection Requirements for (no S/S Document)
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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)
QQ-C-320 Revision B:1974 CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320)
MIL A 8862 : 0 AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS
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MIL-STD-838 Revision C:1983 LUBRICATION OF MILITARY EQUIPMENT
MIL-E-18927 Revision E:1983 Environmental Control Systems, Aircraft, General Requirements for
MIL I 6870 : E INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
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MIL-D-81514 Revision B:1969 Device, Restraint Harness Take-Up, Inertia-Locking, Powered-Retracting, General Specification for
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MIL-STD-882 Revision E:2012 System Safety
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MIL-H-6088 Revision G:1991 Heat Treatment of Aluminum Alloys (S/S by SAE-AMS-H-6088)
MIL C 7958 : A CONTROL, PUSH PULL, FLEXIBLE AND RIGID
MIL-L-81561 Revision G:1994 Life Preserver Assemblies, Inflatable, Aircrewmen and Passenger, Cemented and Heat Sealed
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US$20.00
Excluding Tax where applicable