NIIN Output Data
NIIN:
NSN:
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.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 25-2602-806 | 81205 | A | 3 | 2 | 2 | SB |
CAGE Information
| Code | Company |
|---|---|
| 81205 | THE BOEING COMPANY 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 |
|---|---|---|
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287-0 FED SPEC SINGLE MATERIAL RESPONSE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-52 |
| ABHP | OVERALL LENGTH | 9.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.700 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| FEAT | SPECIAL FEATURES | HEAT TREATED TO CONDITION T6; FINISH F-2.115 |
| CZDJ | AIRCRAFT LOCATION | ANGLE,RIB NO. 4,INBOARD STRUT |
| ABPX | MATERIAL THICKNESS | 0.063 INCHES NOMINAL |