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
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 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
Features
-
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.