| MRC |
Requirement Statement |
Characteristics |
| ABPX |
MATERIAL THICKNESS |
0.090 INCHES NOMINAL |
| CXCY |
III PART NAME ASSIGNED BY CONTROLLING AGENCY |
BRACKET |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
F-22A |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-250/12 ASSN STD SINGLE MATERIAL RESPONSE |
| AGAV |
III END ITEM IDENTIFICATION |
F-22 RAPTOR |
| ABHP |
OVERALL LENGTH |
5.000 INCHES NOMINAL |
| MATT |
MATERIAL |
ALUMINUM ALLOY 7075 |
| SR-5 |
THE MANUFACTURERS DATA |
|
| SR-5 |
DESIGN CONTROL REFERENCE |
5HF71471-353 |
| SR-5 |
MANUFACTURERS CODE |
81205 |
| FEAT |
SPECIAL FEATURES |
DIM. ARE STOCK MATERIAL; P/O: -301 BRACKET ASSY; M/O: 7075-T73 ALUMINUM SHEET |
| CZDJ |
AIRCRAFT LOCATION |
UPPER SKIN ALUMINUM, FORWARD BOOM |
| ABMK |
OVERALL WIDTH |
3.000 INCHES NOMINAL |
