MIL-A-18717 Revision C:1993
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ARRESTING HOOK INSTALLATIONS, AIRCRAFT
01-02-2017
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PACKAGING
6 NOTES
APPENDIX A - PROCEDURES FOR ARRESTING HOOK INSTALLATION ANALYSIS
INDEX
Describes design, development, construction, analysis, test and documentation requirements for arresting hook installations in aircraft for which detail specifications or pertinent contractual documents require that arresting hooks be fitted.
Committee |
FSC 1710
|
DevelopmentNote |
C NOTICE 1 - Notice of Cancellation/Superseded by MIL STD 18717. (03/2017)
|
DocumentType |
Standard
|
Pages |
41
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
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MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
SAE AIR 4403 : 2012 | SELECTION, TESTING, LUBRICATION, AND SEALING OF SINGLE ROW TAPERED ROLLER BEARINGS FOR AEROSPACE WHEEL APPLICATIONS |
MIL-L-87139 Base Document:1979 | LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
SAE AIR 1489 : 2012 | AEROSPACE LANDING GEAR SYSTEMS TERMINOLOGY |
JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-B-8906 Revision C:1988 | BOLT, ALLOY STEEL, SHEAR AND TENSILE, (132 KSI MIN FSU AND 220 KS MIN FTU), 45 DEGREE F, SPLINE DRIVE |
MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
MIL-STD-203 Revision G:1991 | AIRCREW STATION CONTROLS AND DISPLAYS FOR FIXED WING AIRCRAFT |
MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
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