Part Number
Part Number:
NSN:
NIIN:
Item Name:
SPAR , AIRCRAFT
Definition:
A PRINCIPAL SPANWISE MEMBER OF THE STRUCTURAL FRAMEWORK OF A WING, STABILIZER, OTHER AIRFOIL, AND THE LIKE. IT IS DESIGNED TO ABSORB BENDING LOADS APPLIED TO THE AIRFOIL.
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 |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | WING |
| CZDJ | AIRCRAFT LOCATION | WING |
| ABPX | MATERIAL THICKNESS | 1.050 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | MANUFACTUER SUGGESTED NAME - SPAR-21%,W.O.P.,W.S. 85.00 TO 114.50 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEJ | AIRCRAFT STATION NUMBER | WS 85.00 TO 114.50 |
| ABMK | OVERALL WIDTH | 2.500 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-5 |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| ABHP | OVERALL LENGTH | 25.925 INCHES NOMINAL |