Part Number
Part Number:
NSN:
NIIN:
Item Name:
FORMER , AIRCRAFT
Definition:
A LIGHT, SECONDARY STRUCTURAL MEMBER THAT DOES NOT COMPLETELY PARTITION VARIOUS COMPONENTS SUCH AS THE FUSELAGE, BOOM, WING, AND THE LIKE. IT IS DESIGNED TO GIVE CROSS-SECTIONAL SHAPE AND STRENGTH TO THE ITEM OF WHICH IT IS A PART.
CAGE Information
| Code | Company |
|---|---|
| 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES |
Federal Supply Class
Title
AIRFRAME STRUCTURAL COMPONENTS
Inclusions:
INCLUDES FLIGHT CONTROL SURFACES; INTERNAL AND EXTERNAL AUXILIARY FUEL TANKS; EXHAUST SYSTEMS; PYLONS, TRIM TABS; AIRCRAFT.
Exclusions:
EXCLUDES FITTED COVERS; HELICOPTER ROTOR BRAKE SYSTEM COMPONENTS; AIRCRAFT LOOSE EQUIPMENT AND ALTERNATE MISSION CONFIGURATION EQUIPMENT STORED ON BOARD THE AIRCRAFT.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FEAT | SPECIAL FEATURES | NHA FORMER-NACELLE, FUSELAGE STATION 276.85 T-38 IMPROVED INLET |
| ABMK | OVERALL WIDTH | 16.600 INCHES MINIMUM AND 16.800 INCHES MAXIMUM |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | T-38C AND T-38N |
| ABHP | OVERALL LENGTH | 23.900 INCHES MINIMUM AND 24.100 INCHES MAXIMUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 4050 ASSN STD SINGLE MATERIAL RESPONSE |
| ABPX | MATERIAL THICKNESS | 0.900 INCHES MINIMUM AND 1.100 INCHES MAXIMUM |
| CZDJ | AIRCRAFT LOCATION | FUSELAGE STATION 276.85 |
| MATT | MATERIAL | ALUMINUM ALLOY 7050 |