MS21254U
ETC
EYE END / TURNBUCKLE / CLIP LOCKINGINCH-POUND MS21254U 20 November 2002 SUPERSEDING MS21254T 5 November 2001 DETAIL SPECIFICATION SHEET EYE END, TURNBUCKLE, CLIP LOCKING This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acq
MS21253
(MS21253 / MS21254) Clip LockingClevis End for Bearings, Eye End for Pin, Turnbuckle, Clip Locking
MATERIAL: STEEL, CARBON OR ALLOY
MS21253 and MS21254
Genuine Aircraft Hardware Co.
130
All Original Text, Tables and Drawings are Copyright © by Genuine Aircraft Hardware Co. 2005
Documents in this book for REFERENCE ONLY, not
Aircraft
PDF
MS21254
(MS21253 / MS21254) Clip LockingClevis End for Bearings, Eye End for Pin, Turnbuckle, Clip Locking
MATERIAL: STEEL, CARBON OR ALLOY
MS21253 and MS21254
Genuine Aircraft Hardware Co.
130
All Original Text, Tables and Drawings are Copyright © by Genuine Aircraft Hardware Co. 2005
Documents in this book for REFERENCE ONLY, not
Aircraft
PDF
MS21250
BOLTMS21250 SUPERSEDES NAS624 THRU NAS 644
BOLT , STEEL, TENSION, 180 KSI FTU 450°F, 12 POINT EXTERNAL WRENCHED
LENGTH GRIP A T
NOTES:
B
1. Material - steel alloy MIL-S-5626 2. CAD plate TYPE 11, Class 2. 3. Dimensions are in INCHES unless otherwise noted. 4. Tolerances decimals ± .010. 5. Dimensio
AVIAQUIP
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