Serving our customers with quality and safety first.
aluminum alloy
unthreaded mounting holes
2.080in. and 2.100in.
F101-GE-102 engine, B1-B acft
6.3725in.
9.463in. and 9.497in.
two hole
hydraulic
double acting single cylinder
internal threaded
unjf
0.4375in.
20
3b
RIGHT-Hand
lug cylinder head end
lug piston rod end
0.375in.
0.360in.
6.030in.
1 cylinder head end
2 piston rod end
rod thd per MIL-S-8879, 2-in. min depth, end 6-sided 0.520 - 0.530 in. across w/slots 0.093 - 0.098 in. w and 0.069 - 0.074 in. dp; used for variable stator actuation
as differentiated by source control no. 9962M33
1EA
Schedule B number: 8803909060
nmfc 133300
Other parts, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communicat
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding 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).
Used on f101-ge-102 engine,b1-b acft. rod thd per mil-s-8879, 2-in. min depth, end 6-sided 0.520 - 0.530 in. across w/slots 0.093 - 0.098 in. w
1. | 1211124-10 | Cage 98391 |
2. | 1211124-6 | Cage 98391 |
3. | 9962M33P01 | Cage 07482 |
4. | 9962M33P03 | Cage 07482 |
5. | 1211124-11 | Cage 98391 |
Nothing similar to this part number was found in our inventory
A cylinder containing a piston and other component parts designed to develop linear motion required to operate a given object(s) with energy generated from either pneumatic or hydraulic pressure(s). see also cylinder, actuating, linear. do not use if a more specific name applies.