Part Number
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.
CAGE Information
| Code | Company |
|---|---|
| 97499 | BELL HELICOPTER TEXTRON INC. |
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 | STEEL AMS6415;SURFACE TREATMENT BPS FW 4140,SURFACE FINISH 204-947- 002;4 HOLES THRU FLANGE 0.405 IN. MIN,0.412 IN. MAX DIA;1 HOLE THRU FLANGE 1.480 IN. MIN,1.510 IN. MAX DIA; FLANGE 0.310 IN. NOM THK;SPINDLE ARM 2.430 IN. NOM LG,0.510 IN. MIN,0.540 MAX OD |
| FEAT | SPECIAL FEATURES | STEEL AMS6415;SURFACE TREATMENT BPS FW 4140,SURFACE FINISH 204-947- 002;4 HOLES THRU FLANGE 0.405 IN. MIN,0.412 IN. MAX DIA;1 HOLE THRU FLANGE 1.480 IN. MIN,1.510 IN. MAX DIA; FLANGE 0.310 IN. NOM THK;SPINDLE ARM 2.430 IN. NOM LG,0.510 IN. MIN,0.540 MAX OD |
| AGAV | END ITEM IDENTIFICATION | OH-58 SERIES AIRCRAFT |