| MRC |
Requirement Statement |
Characteristics |
| CZDJ |
AIRCRAFT LOCATION |
FUEL EXTRUSION, FORWARD F2 TANK |
| 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 |
5PTMG410K10A450 ASSN STD SINGLE MATERIAL RESPONSE |
| HGTH |
HEIGHT |
1.050 INCHES NOMINAL |
| SR-5 |
THE MANUFACTURERS DATA |
|
| SR-5 |
DESIGN CONTROL REFERENCE |
5HJ42073-129 |
| MATT |
MATERIAL |
ALUMINUM ALLOY |
| FEAT |
SPECIAL FEATURES |
M/O: EXTRUDED SHAPE, FINAL COND T8511 |
| ABHP |
OVERALL LENGTH |
3.200 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
0.780 INCHES NOMINAL |
| SR-5 |
MANUFACTURERS CODE |
81755 |
