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Aircraft Engine Test Stands - Page 4 of 6
146 products in this catalog- Application: F100-pw-200 aircraft engine
- Features: Company item name-cabinet assembly; serd no. 4691
- Application: F101-ge-102 engine b-1b aircraft age.
- Application: F100-pw-100 aircraft eng
- Designed: Engine air/oil cooler
- Tested: F100-pw-100
- Application: F100pw100pw200 aircraft engine age.
- Designed: Engine, air cooling
- Tested: F100-pw-100 engine
- Classification: Aa-9.3
- Literature: T.O. 33d4-6-678-1; serd 3970
- Designed: Engine, air cooling
- Tested: F100-pw-100 engine
- Classification: Aa-9.3
- Literature: T.O. 33d4-6-678-1; serd 3970
- Application: Jet engine test stand 4920010415863
- Application: Starter, engine, air turbine
- Designed: Engine air turbine starter
- Tested: Wide variety of jet engine starters
- Literature: T.O. 33d4-6-594-1
- Application: J79 jet engine age
T150109 Etu-104e Engine Electronic Control Company Item Name-cart Test
View Details SKU: 4920010598953
View Details SKU: 4920010598953
- Application: F100-pw-100 turbofan engine
- Tested: F100-pw-100 and f100-pw-200
- Literature: T.O. 33d4-6-628-1/4
PWA50109 Etu-104e Engine Electronic Control Company Item Name-cart Test
View Details SKU: 4920010598953
View Details SKU: 4920010598953
- Application: F100-pw-100 turbofan engine
- Tested: F100-pw-100 and f100-pw-200
- Literature: T.O. 33d4-6-628-1/4
- Application: Air turbine starter series 3505492
- Literature: To 2ja3-65-3
- Application: Air turbine starter series 3505492
- Literature: To 2ja3-65-3
- Literature: To 33d4-6-212-41
- Designed: Engine run-up
- Tested: T-56 engine
- Features: To name: turbine starter test stand
- Literature: To 2ja3-53-3
- Application: Turbofan engine tf41-a-1
- Features: 42.000 in. W, 70.000 in. H, 30.000 in. Deep
- Literature: T.O33da3-76-1 to2jtf41-4
- Measure: 131432.2916 cubic feet
- Tested: T76 turboprop
- Literature: 33d4-6-317-1
- Application: J-85-ge series turbojet engines
- Features: For use with shaw-estes test stand
- Literature: To 2j-j85-54
- Tested: Tf33 engine, kc-135 acft
- Classification: Gg-7.3
- Designed: Air leakage
- Tested: J85-ge-5/7
- Literature: To 33d4-6-199-4
- Application: Ah-1, uh-1, ov-1 turbine engine
- Application: J-79 engine
- Literature: To 33d4-6-68-154