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
|