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National Stock Number:
9905-01-211-2011
Federal Supply Class:
9905
National Item Identification Number:
012112011
Description:
PLATE,IDENTIFICATION
Detail:
AN ITEM WHICH IS RIGID OR SEMIRIGID, GENERALLY FLAT AND SMOOTH. ITS THICKNESS IS SMALL IN COMPARISON TO ITS LENGTH AND WIDTH OR DIAMETER. IT IS DESIGNED TO BE ATTACHED TO AN ITEM AND INDICATES NAME AND/OR NOMENCLATURE OF THE ITEM. SEE ALSO MARKER, IDENTIFICATION; PLATE, DESIGNATION; PLATE, INSTRUCTION; PLATE SET, IDENTIFICATION; AND TAG, MARKER. EXCLUDES LABEL.
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Manufacturer Information:
| 75A430816-2003 | 76301 | THE BOEING COMPANY |
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Techincal Specification:
| BASIC SHAPE STYLE | RECTANGULAR | | COLOR | BLACK SINGLE SIDE INSCRIPTION BACKGROUND | | COLOR | SILVER SINGLE SIDE INSCRIPTION | | INSCRIPTION | /PARTIAL LEGEND/DESIGNATION SHOCK STRUT,WING GEAR DIMENSION X INS 6,6.5,7,7.5,8,8.5,9,9.5,10,10.5,11,11.5,12,12.4 STRUT PRESS PSI 363PORM15,338PORM14,316PORM13 SINGLE SIDE | | LENGTH | 8.170 INCHES MINIMUM AND 8.230 INCHES MAXIMUM | | MARKING DESIGNATION | DESIGN SINGLE SIDE | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/1, ALLOY 1100, H14 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY | | SPECIAL FEATURES | BOTTOM OF PLATE HAS LEGEND STATING WARNING-RELEASE NITROGEN IN STRUT BEFORE DIASSEMBLING | | WIDTH | 4.970 INCHES MINIMUM AND 5.030 INCHES MAXIMUM | | THICKNESS | 0.010 INCHES MINIMUM AND 0.030 INCHES MAXIMUM |
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