| MRC |
Requirement Statement |
Characteristics |
| HGTH |
HEIGHT |
2.500 INCHES NOMINAL |
| ABPX |
MATERIAL THICKNESS |
0.125 INCHES NOMINAL |
| CXCY |
III PART NAME ASSIGNED BY CONTROLLING AGENCY |
BRACKET |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
F-22A |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
5PTM4G10K10A132 ASSN STD SINGLE MATERIAL RESPONSE |
| FEAT |
SPECIAL FEATURES |
HEIGHT & MATERIAL THICKNESS DIM. ARE STOCK MATERIAL; M/O: EXTRUDED SHAPE, FINAL COND T8511 |
| AGAV |
III END ITEM IDENTIFICATION |
F-22 RAPTOR |
| CZDJ |
AIRCRAFT LOCATION |
FUEL - FORWARD F2 TANK |
| ABMK |
OVERALL WIDTH |
2.060 INCHES NOMINAL |
| ABHP |
OVERALL LENGTH |
2.490 INCHES NOMINAL |
| SR-5 |
DESIGN CONTROL REFERENCE |
5HJ42071-191 |
| SR-5 |
THE MANUFACTURERS DATA |
|
| MATT |
MATERIAL |
ALUMINUM ALLOY |
| SR-5 |
MANUFACTURERS CODE |
81755 |
