| MRC |
Requirement Statement |
Characteristics |
| ABHP |
OVERALL LENGTH |
3.000 INCHES NOMINAL |
| CXCY |
III PART NAME ASSIGNED BY CONTROLLING AGENCY |
BRACKET |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
F-22A |
| AGAV |
III END ITEM IDENTIFICATION |
F-22 RAPTOR |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS-T-9046 ASSN STD SINGLE MATERIAL RESPONSE |
| SR-5 |
THE MANUFACTURERS DATA |
|
| SR-5 |
MANUFACTURERS CODE |
81205 |
| ABMK |
OVERALL WIDTH |
2.000 INCHES NOMINAL |
| MATT |
MATERIAL |
TITANIUM |
| FEAT |
SPECIAL FEATURES |
DIM. ARE STOCK MATERIAL; C/O: -207 BRACKET, NUT (1), RIVET (2); M/O: 6AL-4V (AB-1), ANN TITANIUM SHEET |
| CZDJ |
AIRCRAFT LOCATION |
OUTBOARD FRAME, STA 567.50 |
| SR-5 |
DESIGN CONTROL REFERENCE |
5HF72221-107 |
