MIL-DTL-7034 Revision F:2005
Current
The latest, up-to-date edition.
Pulleys, Groove, Antifriction Bearing, Grease Lubricated, Aircraft, General Specification for
04-01-2005
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Describes the requirements for single grove pulleys with antifriction bearings.
| 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 |
56
|
| ProductNote |
NEW CHILD NOT 2 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers requirements for single groove pulleys with antifriction bearings.
| MIL-DTL-9490 Revision E:2008 | Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for |
| SAE AS94900 | 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 AS7949B | Bearings, Ball, Airframe, Antifriction, General Standard for |
| 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 AMS4037Q | Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate) Solution Heat Treated |
| SAE AS21443B | BEARING, BALL, AIRFRAME ANTI-FRICTION, PULLEY |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AS27640C | 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 AMSQQA225/6A | Aluminum Alloy, 2024, Bar, Rod, and Wire; Rolled, Drawn, or Cold Finished |
Access your standards online with a subscription
-
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.
Important note : All end users must be registered with an Account prior to user licenses being assigned.Logging out.