MIL-DTL-81014 Revision B:2001
Current
The latest, up-to-date edition.
Hook, Helicopter External Cargo, 20,000 Pound Capacity, Type C (No S/S Document)
English
02-02-2001
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Establishes the requirements for a 20,000 pound capacity helicopter external hook, type C.
| DevelopmentNote |
Inactive for New Design (06/2001) Supersedes MIL H 81014 (A) (07/2004)
|
| DocumentType |
Standard
|
| Pages |
19
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL L 7961 : C | LIGHT, INDICATOR, PRESS TO TEST |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MS3106 Revision D:1992 | Connector, Plug, Electric, Straight, Solder Contacts, AN Type (S/S by SAE-AS31061) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-S-4040 Revision G:2012 | Solenoid, Electrical General Specification for (No S/S Document) |
| MIL-P-6906 Revision B:1969 | Plates, Identification, Aircraft |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| SAE AMSSTD2219 | Fusion Welding for Aerospace Applications |
| AFGS-87242 Revision A:1991 | Flight Control System General Specification for (S/S by JSSG-2008) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-W-6873 Revision C:1991 | Welding; Flash, Carbon and Alloy Steel (See Notice 2 for Replacement Information) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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