Part Number
Part Number:
NSN:
NIIN:
Item Name:
FITTING , STRUCTURAL COMPONENT , AIR
Definition:
AN ITEM OF UNIQUE SHAPES AND CROSS-SECTIONAL CONFIGURATIONS SPECIFICALLY DESIGNED WITH DIMENSIONAL TOLERANCES AND FINISHES. IT MAY BE METALLIC AND/OR NONMETALLIC AND MUST BE ABLE TO MATE WITH OR JOIN TO LIKE ITEMS WITH AIRCRAFT APPLICATION. THE ITEM MAY CONSIST OF MORE THEN ONE (1) PIECE TO FORM AN ASSEMBLY. DO NOT USE IF A MORE SPECIFIC ITEM NAME EXISTS. EXCLUDES BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
| ABHP | OVERALL LENGTH | 5.000 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | FITTING ASSEMBLY |
| FEAT | SPECIAL FEATURES | FRACTURE/DURABILITY CRITICAL ITEM; C/O: -123 FITTING, 4065-091 BUSHING (2), 4091-002 BUSHING (4); DIM. ARE STOCK MATERIAL; M/O 6-2222 STA TITANIUM PLATE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
| ABMK | OVERALL WIDTH | 4.000 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | 5PT-7T01 ASSN STD SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | TITANIUM |
| CZDJ | AIRCRAFT LOCATION | ACTUATOR NO. 5 LEADING EDGE, WING BOX |