NIIN Output Data
NIIN:
NSN:
Item Name:
LONGERON
Definition:
A PRINCIPAL LONGITUDINAL MEMBER OF THE STRUCTURAL FRAMEWORK OF AN AIRCRAFT FUSELAGE, NACELLE, EMPENNAGE BOOM, OR SIMILAR COMPONENT.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 204-70045-363 | 81205 | A | 3 | 2 | 2 | MF |
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 74.500 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.050 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | E-3A |
| BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE |
| CZDJ | AIRCRAFT LOCATION | LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE |
| FEAT | SPECIAL FEATURES | HEAT TREAT T62; FINISH SRF-2.30 |
| ABMK | OVERALL WIDTH | 3.700 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |