| MRC |
Requirement Statement |
Characteristics |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
F-15A,B |
| ABPX |
MATERIAL THICKNESS |
0.040 INCHES NOMINAL |
| SR-5 |
DESIGN CONTROL REFERENCE |
68A332013-2002 |
| SR-5 |
MANUFACTURERS CODE |
76301 |
| ABHP |
OVERALL LENGTH |
12.200 INCHES NOMINAL |
| MATT |
MATERIAL |
ALUMINUM ALLOY 2024 |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-250/5,COND 0,T62 FED SPEC 1ST MATERIAL RESPONSE |
| SR-5 |
THE MANUFACTURERS DATA |
|
| ABMK |
OVERALL WIDTH |
8.500 INCHES NOMINAL |
| CZEJ |
AIRCRAFT STATION NUMBER |
837 |
| CZDJ |
AIRCRAFT LOCATION |
FORMER-FS837,AFT EMPENAGE CLOSUREBEAM |
| FEAT |
SPECIAL FEATURES |
NEXT HIGHER ASSY,68A332001 U/O F-15A CUM 1-BLK 11,F-15B CUM 1-BLK 11,DIM.STOCK MATERIAL |
| BWJF |
SIDE FOR WHICH DESIGNED |
RIGHT SIDE |
