| MRC |
Requirement Statement |
Characteristics |
| FLEX |
(NON-CORE DATA) FLEXIBILITY |
FLEXIBLE |
| ADJS |
EXTERIOR COLOR |
CLEAR |
| SR-1 |
SPEC/STD CONTROLLING DATA |
|
| SR-1 |
NON-DEFINITIVE GOVERNMENT SPEC/STD REFERENCE |
A-A-55697 |
| CRTL |
CRITICALITY CODE JUSTIFICATION |
FEAT |
| FEAT |
SPECIAL FEATURES |
USED OMN EJECTION SEAT SYSTEM F/A-18 AIRCRAFT;WEAPON SYSTEM ESSENTIAL |
| CRXX |
MEASURING METHOD AND LENGTH |
600.000 INCHES NOMINAL OVERALL |
| SR-1 |
MANUFACTURERS CODE |
58536 |
| ABKV |
OUTSIDE DIAMETER |
0.281 INCHES NOMINAL |
| AAGR |
CROSS-SECTIONAL SHAPE STYLE |
ROUND |
| AGAV |
END ITEM IDENTIFICATION |
ENGINE, AIRCRAFT F110-GE-100/129 (F-16 C/D) |
| SR-1 |
DEFINITIVE GOVERNMENT SPEC/STD REFERENCE |
A55697-02-A-1 |
| ZZZT |
NONDEFINITIVE SPEC/STD DATA |
2 TYPE |
| MATT |
MATERIAL |
PLASTIC POLYVINYL CHLORIDE TUBE |
| AARX |
INSIDE DIAMETER |
0.156 INCHES NOMINAL |
