MIL P 7034 : D
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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PULLEY, GROOVE, ANTIFRICTION BEARING, GREASE LUBRICATED, AIRCRAFT
English
05-05-1998
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Superseded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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MS24566 Revision E:1984 | PULLEY - CONTROL, ANTI-FRICTION BEARING (S/S BY MIL-DTL-7034/4) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| PPP-B-665 Revision D:1972 | Boxes, Paperboard, Metal Edged and Components (S/S by A-A-669and A-A-2807) |
| 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 (NO S/S DOCUMENT) |
| PPP-B-636 Revision J:1981 | Boxes, Shipping, Fiberboard (S/S by ASTM-D1974 and ASTM-D5118) |
| 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 | Boxes, Folding, Paperboard |
| SAE AMS4037Q | 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 (S/S BY MIL-DTL-7034/2) |
| 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 (S/S by SAE-AS7949) |
| MIL-I-45208 Revision A:1963 | Inspection System Requirements (No S/S Document) |
| MIL W 83420 : E | WIRE, ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL |
| PPP-B-676 Revision E:1992 | Boxes, Setup |
| MS20221 Revision E:1984 | PULLEY, GROOVE, HEAVY DUTY, CONTROL, AIRCRAFT (S/S BY MIL-DTL-7034/3) |
| MS20219 Revision F:1982 | PULLEY, GROOVE, SECONDARY CONTROL, AIRCRAFT (S/S BY MIL-DTL-7034/1) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS21443 Revision B:1995 | BEARING, BALL, AIRFRAME, ANTI-FRICTION, PULLEY (S/S BY SAE-AS21443) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL G 23827 : B | GREASE, AIRCRAFT AND INSTRUMENT, GEAR AND ACTUATOR SCREW |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
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