NIIN Output Data
Definition:
A DEVICE OF VARIOUS SHAPES TO BE PERMANENTLY ATTACHED TO THE STRUCTURE OF AN AIRCRAFT. IT IS DESIGNED TO PERMANENTLY MOUNT AND/OR SUPPORT AN INTEGRAL MEMBER, OR GROUP OF MEMBERS OF THE AIRFRAME IN A PROPER POSITION AND BEAR THE STRESS IMPOSED BY THE COMPONENTS BEING SUPPORTED. IT MAY HAVE MOUNTING PROVISIONS, SUCH AS SLOTS, HOLES, AND/OR ATTACHMENTS TO FACILITATE INSTALLATION. EXCLUDES ITEMS WHICH ARE PRIMARILY DESIGNED FOR DAMPENING SHOCK AND/OR VIBRATION. EXCLUDES BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; AND BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
4F73473-101A | 98897 | A | 3 | 2 | 2 | SB |
CAGE Information
Code | Company |
---|---|
98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
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 |
---|---|---|
FEAT | SPECIAL FEATURES | MATL-AL ALLOY,COMP 6063-T52 PER QQ-A-200/9; FINISH-CHROMATE PER MIL-C-5541,CL 3 AND 2 COATS ZINC CHROMATE PRIMER; BOTH LEGS 4.000 IN. W AND 1.500 IN. LG BY 0.125 IN. THK; ONE LEG HAS 3 HOLES 0.280 IN. MIN AND 0.287 IN. MAX DIA 1.250 IN. APART STARTING 0.750 IN. FROM END |
AGAV | END ITEM IDENTIFICATION | C-5A AIRCRAFT |
ZZZV | FSC APPLICATION DATA (NON-CORE) | AIRCRAFT STRUCTURAL COMPONENT |