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Part Number

Part Number:
NSN:
NIIN:
Item Name:
CONTROL ARM , THROTTLE

CAGE Information

Code Company
97499 BELL HELICOPTER TEXTRON INC.

Federal Supply Class

Title

MISCELLANEOUS ENGINE ACCESSORIES

Inclusions:

INCLUDES ENGINE DYNAFOCAL SUSPENSION MOUNTS; ENGINE COWLING MOUNTS; ENGINE MOUNTED CONTROL ASSEMBLIES; PNEUMATIC STARTERS; PUSH-PULL CONTROL ASSEMBLIES;SPECIALLY DESIGNED JET ENGINE AIR, OIL, ANTI-ICING AND HYDRAULIC REGULATORS; VALVES AND PUMPS; STARTING UNITS.

Exclusions:

EXCLUDES EXHAUST SYSTEM; (FSC 1560); JET ENGINE HYDRAULIC RESERVOIRS (FSC 2840); JET ENGINE OIL TANKS (FSC 2840); ELECTRICAL STARTERS (FSC 2925); COCKPIT MOUNTED CONTROL QUADRANTS (FSC 1680); AIRCRAFT ENGINE COVERS (FSC 1730).

Characteristics (Decoded)

MRC Requirements Statement Clear Text Reply
TEXT GENERAL CHARACTERISTICS ITEM DESCRIPTION SHAFT 1.687 LG; 0.4997 IN. MIN 0.5002 IN. MAX DIA; SHAFT TONGUE 0.1868 IN. MIN 0.1873 IN. MAX W AFTER PLATING BY 0.550 IN. LG; ONE 0.094 IN. MIN 0.097 IN. MAX DIA THRU HOLE IN SHAFT; RIGHT ANGLE CLEVIS,ROD END,1.409 IN. LG; 0.628 IN. W; 0.1896 IN. MIN 0.1901 IN. MAX DIA INLINE HOLES IN EA CLEVIS ARM SPACED 1.910 IN. CENTER TO CENTER W/SHAFT,63.0 MICROIN SURF FINISH IN HOLE; CLEVIS OFFSET 0.480 IN.
TEXT GENERAL CHARACTERISTICS ITEM DESCRIPTION SHAFT 1.687 LG; 0.4997 IN. MIN 0.5002 IN. MAX DIA; SHAFT TONGUE 0.1868 IN. MIN 0.1873 IN. MAX W AFTER PLATING BY 0.550 IN. LG; ONE 0.094 IN. MIN 0.097 IN. MAX DIA THRU HOLE IN SHAFT; RIGHT ANGLE CLEVIS,ROD END,1.409 IN. LG; 0.628 IN. W; 0.1896 IN. MIN 0.1901 IN. MAX DIA INLINE HOLES IN EA CLEVIS ARM SPACED 1.910 IN. CENTER TO CENTER W/SHAFT,63.0 MICROIN SURF FINISH IN HOLE; CLEVIS OFFSET 0.480 IN.

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