MIL-DTL-7034 Revision F:2005
Current
Current
The latest, up-to-date edition.
PULLEYS, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Published date
01-04-2005
Publisher
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Describes the requirements for single grove pulleys with antifriction bearings.
| Committee |
FSC 1640
|
| DevelopmentNote |
Supersedes MIL P 7034 (D) (01/2000) F NOTICE 1 - Notice of Validation. (02/2015) NEW CHILD NOT 2 IS NOW ADDED
|
| DocumentType |
Standard
|
| Pages |
55
|
| ProductNote |
NEW CHILD NOT 2 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-7034-3 Revision A:2005 | PULLEY, GROOVE, HEAVY DUTY, CONTROL, AIRCRAFT |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| TT-P-1757 Revision B:1997 | PRIMER COATING, ALKYD BASE, ONE COMPONENT |
| SAE AS 7949 : 2004 | BEARINGS, BALL, AIRFRAME, ANTIFRICTION, GENERAL STANDARD |
| MIL-DTL-83420 Revision P:2017 | WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
| SAE AS 21443 : 2012 | BEARING, BALL, AIRFRAME, ANTI-FRICTION, PULLEY |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AS 27640 : 2012 | BEARING, BALL, AIRFRAME, ANTI-FRICTION, HEAVY DUTY |
| MIL-DTL-7034-4 Revision A:2005 | PULLEY, CONTROL, ANTI-FRICTION BEARING, AIRCRAFT |
| MIL-PRF-81322 Revision G:2005 | GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395 |
| MIL-DTL-7034-1 Revision A:2005 | PULLEY, GROOVE, SECONDARY CONTROL, AIRCRAFT |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-DTL-7034-2 Revision A:2005 | PULLEY, GROOVE, FLIGHT CONTROL, AIRCRAFT |
| SAE AMS QQ A 225/6 : 1998 | ALUMINUM ALLOY, 2024, BAR, ROD, AND WIRE; ROLLED, DRAWN, OR COLD FINISHED |
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