• There are no items in your cart

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

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.

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

View more information
US$20.00
Excluding Tax where applicable

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.