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2.239in. ⁓2-1/4"
F100GE100 engine
0.808 in. dia; wt .11 lbs max; spring retainer cap must withstand a min 15 in. lbs; removal torque; shall withstand magnetic strength using 40 g static load without actuation; prevents actuation below 120 deg f; permits actuation above 140 deg f; once actuated with the test fluid pressure released, the button shall withstand a 5 lb reset load without resetting and shall remain in the actuated position until the indicator is inverted and manually depressed; actuation pressure 47-55 lbs square in. differential using test fluid at 140 deg f to 150 deg f; reset pressure 32 pound square in. differential min using test fluidat 140 deg f to 150 deg f; environmental condition, fluid oil lub MIL-L-7808, MIL-L-23699; pressure operating 0 psiato 1000 psia, proof 1500 psia, burst 3000 psia; temp operating -65 deg f to 415 deg f
1EA
Schedule B number: 8803909060
nmfc 190500
Other parts, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communicat
FSC 2945 ⁓ Engine air and oil filters, cleaners, aircraft prime moving
Note-items placed in this fsc should be specifically designed for use on aircraft or guided missile prime movers only.
Excluding fuel filters (fsc 2915); items designed for other than engines.
Used on f100ge100 engine. 0.808 in. dia; wt .11 lbs max; spring retainer cap must withstand a min 15 in. lbs; removal torque; shall withstand magnetic strength using 40 g static load without actuation; prevents actuation below 120 deg f; permits actuation above 140 deg f; once actuated with the test fluid pressure released, the button shall withstand a 5 lb reset load without resetting 2.239" overall length
1. | TD 314UL091 | Cage 18350 |
Nothing similar to this part number was found in our inventory
A mechnical indicator used on aircraft engine for dry or liquid type cleaners to provide a visual warning signal when a filter needs cleaning or changing.