NIIN Output Data
NIIN:
NSN:
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.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| L2102035-005 | 43999 | A | 3 | 2 | 2 | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 43999 | BOEING COMPANY THE DBA BOEING DIV DE |
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 |
|---|---|---|
| ABMK | OVERALL WIDTH | 10.990 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 1.700 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | HORIZONTAL STABILIZER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| ABHP | OVERALL LENGTH | 26.790 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| FEAT | SPECIAL FEATURES | U/A MACHINED SPAR; MATL: AL BARE PLATE ALLOY 7075-T7351; NHA:L2102021 |