MIL P 7034 : D
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT
Available format(s)
PDF
Superseded date
05-05-1998
Superseded by
Language(s)
English
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.Describes non metallic and metallic sheave, single groove pulleys for antifriction bearings.
| DocumentType |
Standard
|
| Pages |
22
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MS24566 Revision E:1984 | PULLEY CONTROL ANTIFRICTION BEARING |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| PPP-B-665 Revision D:1972 | BOXES, PAPERBOARD, METAL EDGED AND COMPONENTS |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-STD-1186 Revision A:1981 | CUSHIONING, ANCHORING, BRACING, BLOCKING, AND WATERPROOFING, WITH APPROPRIATE TEST METHODS |
| PPP-B-636 Revision J:1981 | BOX, SHIPPING, FIBERBOARD |
| TT-P-1757 Revision B:1997 | PRIMER COATING, ALKYD BASE, ONE COMPONENT |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| PPP-B-566 Revision E:1974 | BOX, FOLDING, PAPERBOARD |
| SAE AMS 4037 : 2014 | ALUMINUM ALLOY, SHEET AND PLATE, 4.4CU - 1.5MG - 0.60MN (2024; -T3 FLAT SHEET, -T351 PLATE) SOLUTION HEAT TREATED |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MS20220 Revision C:1992 | PULLEY, GROOVE FLIGHT CONTROL AIRCRAFT |
| QQ A 225/6 : E | ALUMINUM ALLOY BAR, ROD, AND WIRE, ROLLED, DRAWN OR COLD FINISHED, 2024 |
| MIL-B-7949 Revision E:1981 | BEARING, BALL, AIRFRAME, ANTIFRICTION |
| MIL-I-45208 Revision A:1963 | INSPECTION SYSTEM REQUIREMENTS |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| PPP-B-676 Revision E:1992 | BOXES SET-UP |
| MS20221 Revision E:1984 | PULLEY GROOVE HEAVY DUTY CONTROL AIRCRAFT |
| MS20219 Revision F:1982 | PULLEY, GROOVE SECONDARY CONTROL AIRCRAFT |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS21443 Revision B:1995 | BEARING, BALL, AIRFRAME, ANTI-FRICTION, PULLEY |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL G 23827 : B | GREASE, AIRCRAFT AND INSTRUMENT, GEAR AND ACTUATOR SCREW |
| QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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