MIL-A-23121 Revision C:1970
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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 ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR
09-11-1996
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.
Committee |
FSC 1680
|
DevelopmentNote |
C NOTICE 1 - Notice of Cancellation without replacement. (05/2004)
|
DocumentType |
Standard
|
Pages |
63
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Withdrawn
|
MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
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 |
MIL-A-81573 Base Document:1968 | AIRCREW ESCAPE SYSTEM DESCRIPTIVE AND PERFORMANCE DATA PRESENTATIONS, REQUIREMENT AND FORMATS FOR; GENERAL SPECIFICATION FOR |
MIL-STD-1333 Revision B:1987 | AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
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 |
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 |
MIL-STD-850 Revision B:1970 | AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT |
MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
MIL-E-9426 Revision F:1978 | ESCAPE SYSTEM, REQUIREMENTS CONFORMANCE DEMONSTRATIONS AND PERFORMANCE TESTS FOR, GENERAL SPECIFICATION FOR |
NAS1091:2012 | STREAMER ASSEMBLY, WARNING |
MIL M 81203 : A | MANUAL, TECHNICAL, IN PROCESS REVIEWS, VALIDATION AND VERIFICATION SUPPORT OF |
MIL-I-8500 Revision D:1980 | INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
MIL-C-81590 Base Document:1968 | Cockpit Canopy System, Fixed Wing Single and Multi-Place, Fighter, Attack, and Trainer Aircraft, General Specification for |
MIL-C-18263 Revision F:1971 | COLOR, EXTERIOR, NAVAL AIRCRAFT, REQUIREMENTS FOR |
MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
AS 2556-2000 | Electric resistance welded steel air heater tubes |
MIL-HDBK-694 Revision A:1966 | ALUMINUM AND ALUMINUM ALLOYS |
L-P-383 Base Document:1967 | PLASTIC MATERIAL, POLYESTER RESIN, GLASS FIBER BASE, LOW PRESSURE LAMINATED |
MIL-C-81467 Revision B:1971 | CHAFF, COUNTERMEASURES RR-129/ALE-29A |
MIL C 8073 : D | CORE MATERIAL, PLASTIC HONEYCOMB, LAMINATED CLASS FABRIC BASE, FOR AIRCRAFT STRUCTURAL AND ELECTRONIC APPLICATIONS |
MIL-M-3171 Revision C:1966 | MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION |
MIL-STD-1166 Revision A:1991 | RADIOGRAPHIC TESTING REQUIREMENTS FOR SOLID PROPELLANTS |
MIL-H-6875 Revision H:1989 | HEAT TREATMENT OF STEEL RAW MATERIALS |
MIL A 8064 : B NOTICE 1 | ACTUATOR AND ACTUATING SYSTEMS, AIRCRAFT ELECTROMECHANICAL, GENERAL REQUIREMENTS FOR |
MIL-HDBK-700 Revision A:1975 | PLASTICS |
MIL P 19834 : B | PLATE, IDENTIFICATION, METAL FOIL, ADHESIVE BACKED |
MIL-M-18012 Revision B:1964 | MARKINGS FOR AIRCREW STATION DISPLAYS DESIGN AND CONFIGURATION OF |
MIL-A-9067 Revision C:1961 | ADHESIVE BONDING, PROCESS AND INSPECTION REQUIREMENTS FOR |
MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
MIL I 18464 : G NOTICE 1 | INSIGNIA AND MARKINGS FOR NAVAL WEAPONS SYSTEMS |
MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
MIL-D-23615 Revision C:1993 | DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES |
MIL-S-83490 Base Document:1968 | SPECIFICATION, TYPES AND FORMS |
MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
MIL I 23659 : C | INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
MIL-D-21625 Revision G:1993 | DESIGN AND EVALUATION OF CARTRIDGES FOR CARTRIDGE ACTUATED DEVICES |
MIL D 8634 : LATEST | DECALCOMANIAS, AIRCRAFT, FOR USE ON EXTERIOR SURFACES |
MIL-A-25463 Revision B:1982 | ADHESIVE, FILM FORM, METALLIC STRUCTURAL SANDWICH CONSTRUCTION |
FED-STD-406 Revision A:1982 | PLASTIC, METHODS OF TESTING |
QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) |
MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
MIL-F-7190 Revision B:1985 | FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
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 |
QQ-M-40 Revision B:1962 | MAGNESIUM ALLOY FORGINGS |
MIL-D-81514 Revision B:1969 | Device, Restraint Harness Take-Up, Inertia-Locking, Powered-Retracting, General Specification for |
MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
MIL-M-6857 Revision D:1990 | MAGNESIUM ALLOY CASTINGS, HEAT TREATMENT OF |
MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
MIL-P-23460 Revision E:1991 | PIN, QUICK-RELEASE, SELF-RETAINING POSITIVE-LOCKING |
MIL-STD-882 Revision E:2012 | System Safety |
MIL-C-8779 Revision E:1988 | COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
MIL HDBK 52 : B | EVALUATION OF CONTRACTORS CALIBRATION SYSTEM |
MIL-A-81573 Base Document:1968 | AIRCREW ESCAPE SYSTEM DESCRIPTIVE AND PERFORMANCE DATA PRESENTATIONS, REQUIREMENT AND FORMATS FOR; GENERAL SPECIFICATION FOR |
MIL-STD-401 Revision B:1967 | SANDWICH CONSTRUCTIONS AND CORE MATERIALS, GENERAL TEST METHODS |
MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING BLANK |
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 |
MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
MIL-A-8866 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE |
AS 1578-1974 | Laminated timber scaffold planks |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
MIL-M-8650 Revision C:1976 | Mockups, Aircraft, General Specification for |
MIL-STD-490 Revision A:1985 | SPECIFICATION PRACTICES |
MIL-H-6088 Revision G:1991 | HEAT TREATMENT OF ALUMINIUM ALLOYS |
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 |
MIL-HDBK-691 Revision B:1987 | Adhesive Bonding |
QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
MIL D 1000/1 : LATEST | DRAWING, ENGINEERING & ASSOCIATED DATA |
MIL-HDBK-132 Revision A:1984 | PROTECTIVE FINISHES FOR METAL AND WOOD SURFACES |
MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
MIL-STD-849 Revision C:2009 | INSPECTION REQUIREMENTS, DEFINITIONS AND CLASSIFICATION OF DEFECTS FOR PARACHUTES |
MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
MIL A 25165 : B NOTICE 1 | AIRCRAFT EMERGENCY ESCAPE SYSTEM, IDENTIFICATION OF |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.