Part Number
Part Number:
NSN:
NIIN:
Item Name:
PITCH CONTROL LINK , TAIL ROTOR
CAGE Information
| Code | Company |
|---|---|
| 97499 | BELL HELICOPTER TEXTRON INC. |
Federal Supply Class
Title
HELICOPTER ROTOR BLADES, DRIVE M
Inclusions:
INCLUDES HELICOPTER DYNAMIC COMPONENTS AND SPECIALLY DESIGNED PARTS THAT TRANSMIT POWER FROM THE AIRCRAFT POWER PLANT TO THE ROTARY WING AND ROTARY RUDDER. ALSO INCLUDED IN THIS CLASS ARE ROTORS; BLADES; ROTOR BLADE, TRIM, TABS; BLADE SETS; YOKES; CLUTCHES AND TRANSMISSIONS.
Exclusions:
EXCLUDES PROPELLERS (FSC 1610); ROTOR BRAKE SYSTEMS COMPONENTS (FSC 1630); ROTOR BLADE HYDRAULIC FOLDING SYSTEM COMPONENTS (FSC 1650); HYDRAULIC SERVO SYSTEM COMPONENTS (FSC 1650).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,CORROSION RESISTING AMS5355COMP 17-4PH,DIM.,3.800 IN. NOM OD,0.757 IN. NOM O/A W,0.075 IN. NOM WALL THK,TWO ARM EXTENSIONS ON OD 1.000 IN. W LOCATED 1.437 IN. FROM CENTER BAR AND EXTENDING THRU RING 0.875 IN. LG,ARMS LOCATED AT 78 AND 258.0 DEG,ONE HOLE 0.193 IN. DIA DRILLED THRU EACH ARM CENTER 1.858 IN. FROM BAR CENTER,ONE 0.600 IN. W BAR ACROSS ID CENTER,TWO HOLES 0.2507 IN. DIA DRILLED THRU BAR W/1.2505 IN. C TO C DISTANCE,ONE STUD NO. 206-010-744-1 MOUNTED IN RIGHT END OF BAR AT 45.0 DEG ANGLE |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL,CORROSION RESISTING AMS5355COMP 17-4PH,DIM.,3.800 IN. NOM OD,0.757 IN. NOM O/A W,0.075 IN. NOM WALL THK,TWO ARM EXTENSIONS ON OD 1.000 IN. W LOCATED 1.437 IN. FROM CENTER BAR AND EXTENDING THRU RING 0.875 IN. LG,ARMS LOCATED AT 78 AND 258.0 DEG,ONE HOLE 0.193 IN. DIA DRILLED THRU EACH ARM CENTER 1.858 IN. FROM BAR CENTER,ONE 0.600 IN. W BAR ACROSS ID CENTER,TWO HOLES 0.2507 IN. DIA DRILLED THRU BAR W/1.2505 IN. C TO C DISTANCE,ONE STUD NO. 206-010-744-1 MOUNTED IN RIGHT END OF BAR AT 45.0 DEG ANGLE |