MIL-B-6812 Revision E:1994
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
BOLTS, AIRCRAFT
Available format(s)
PDF
Superseded date
22-02-1999
Superseded by
Publisher
Committee |
FSC 5306
|
DocumentType |
Standard
|
Pages |
21
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
MIL-T-81364 Base Document:1966 | T-BOLT, 180,000 PSI TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS |
MIL-DTL-25027 Revision H:1997 | NUT, SELF-LOCKING, 250 DEG F, 450 DEG F, AND 850 DEG F |
NASM 3 THRU NASM 20:2014 | BOLT, MACHINE, AIRCRAFT |
MIL-HDBK-270 Revision A:1991 | METALLIC MATERIALS FOR LOW MAGNETIC APPLICATIONS, MAGNETIC PERMEABILITY AND ELECTRICAL CONDUCTIVITY, CHARACTERISTICS OF (METRIC) |
MIL C 8783 : A | CLAMP, HOSE, FLAT BAND 500 DEG. F |
MIL-W-48271 Revision A:1984 | WARHEAD METAL PARTS ASSEMBLY M251 PARTS AND ASSEMBLING |
MIL-W-48866 Revision A:1980 | WARHEAD SECTION, GM, PRACTICE LIGHTWEIGHT, M252 AND SHIPPING AND STORAGE CONTAINER, XM612, SPARE PARTS FOR |
MIL-W-48757 Base Document:1975 | WARHEAD SECTION, GM, HE: M251 AND M251A1 SPARE PARTS FOR |
MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
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