ASAP Part Services, owned and operated by ASAP Semiconductor, has over 6 billion parts inventoried. This includes new, old, used, and obsolete parts, such as ATK-97 A37U-35, 458-50060-1, 300300-1003, 300300-1001, ZC8-87-002-3-2. As an ISO 9001:2015 certified and FAA AC 00-56B accredited company, we go to great lengths to ensure we are delivering quality parts. We partner exclusively with reliable manufacturers such as Aeronautical And Support Equipment, Aidc Aerospace Industrial, Airbus Deutschland Gmbh, Airbus Helicopters Inc, Allied Signal Inc. Our team provides superior quality assurance testing for III End Item Identification: KC-135R aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; T.O. 9H2-4-246-3, III End Item Identification: KC-135R aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; T.O. 9H2-4-246-3, III End Item Identification: KC-135R aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; T.O. 9H2-4-246-3, III End Item Identification: KC-135R aircraft III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; T.O. 9H2-4-246-3, III End Item Identification: Pacer dawn III Fsc Application Data: Aircraft hydraulic, vacuum, deicing systems Special Features: Servocylinder rudder and more. So if you are in need of Servocylinder or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
Manufacturers for Servocylinder | |||
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aeronautical and support equipment | aidc aerospace industrial | ||
airbus deutschland gmbh | airbus helicopters inc | ||
allied signal inc |
Part Number | NSN | Details | QTY | RFQ |
---|---|---|---|---|
ATK-97 A37U-35 | 1650-01-142-8094 | iii end item identification: kc-135r aircraft iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; t.o. 9h2-4-246-3 | Avl | RFQ |
458-50060-1 | 1650-01-142-8094 | iii end item identification: kc-135r aircraft iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; t.o. 9h2-4-246-3 | Avl | RFQ |
300300-1003 | 1650-01-142-8094 | iii end item identification: kc-135r aircraft iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; t.o. 9h2-4-246-3 | Avl | RFQ |
300300-1001 | 1650-01-142-8094 | iii end item identification: kc-135r aircraft iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: dc current; 28.0 vdc; 0.5 minimum to 0.7 maximum amps; 18.634 inches minimum to 22.650 inches maximum stroke, manual override included; used on rudder assembly; t.o. 9h2-4-246-3 | Avl | RFQ |
ZC8-87-002-3-2 | 1650-01-353-2244 | iii end item identification: pacer dawn iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: servocylinder rudder | Avl | RFQ |
ZC8-87-002-2-5 | 1650-01-393-1663 | iii end item identification: pacer dawn iii fsc application data: aircraft hydraulic, vacuum, deicing, systems special features: servoactuator flight control-horizontal tail, model 10-184e | Avl | RFQ |
ZC8-87-002-2-3 | 1650-01-382-7789 | iii end item identification: pacer dawn special features: horizontal tail servo cylinder zzzvgaircraft hydraulic, vacuum, deicing systems design characteristics: double acting single cylinder | Avl | RFQ |
B79440-2 | 1650-01-393-1663 | iii end item identification: pacer dawn iii fsc application data: aircraft hydraulic, vacuum, deicing, systems special features: servoactuator flight control-horizontal tail, model 10-184e | Avl | RFQ |
B43170-2 | 1650-01-353-2244 | iii end item identification: pacer dawn iii fsc application data: aircraft hydraulic, vacuum, deicing systems special features: servocylinder rudder | Avl | RFQ |
B33914-1 | 1650-01-382-7789 | iii end item identification: pacer dawn special features: horizontal tail servo cylinder zzzvgaircraft hydraulic, vacuum, deicing systems design characteristics: double acting single cylinder | Avl | RFQ |
65652-07101-042 | 1650-00-089-5054 | NA | Avl | RFQ |
704A44-831-128 | 1650-14-448-1729 | NA | Avl | RFQ |
704A44-831-118 | 1650-14-397-0763 | NA | Avl | RFQ |
704A44-831-117 | 1650-14-397-0762 | NA | Avl | RFQ |
CH02062-2-4 | 1650-00-430-5150 | design characteristics: double acting tandem cylinder extended length: 22.250 inches nominal compressed length: 19.910 inches nominal | Avl | RFQ |
CH02062-2-3 | 1650-00-430-5151 | design characteristics: double acting tandem cylinder extended length: 22.250 inches nominal compressed length: 19.910 inches nominal | Avl | RFQ |
CH02062-2-2 | 1650-00-246-1506 | design characteristics: double acting tandem cylinder extended length: 22.250 inches nominal compressed length: 19.910 inches nominal | Avl | RFQ |
CH02062-2-1 | 1650-00-246-1504 | design characteristics: double acting tandem cylinder extended length: 22.250 inches nominal compressed length: 19.910 inches nominal | Avl | RFQ |
CH02062-1-4 | 1650-00-241-8848 | design characteristics: double acting tandem cylinder extended length: 19.312 inches nominal compressed length: 17.442 inches nominal | Avl | RFQ |
CH02062-1-3 | 1650-00-241-8840 | design characteristics: double acting tandem cylinder extended length: 19.312 inches nominal compressed length: 17.442 inches nominal | Avl | RFQ |
A51H9004-9 | 1650-01-089-6812 | design characteristics: single acting single cylinder bore diameter: 2.431 inches nominal extended length: 21.625 inches nominal | Avl | RFQ |
A51H9004-11 | 1650-01-282-1212 | iii end item identification: f-14 acft reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
A51H9000-9 | 1650-00-367-2955 | iii fsc application data: hydraulic systems, acft special features: left hand installation design characteristics: double acting single cylinder | Avl | RFQ |
A51H9000-8 | 1650-01-253-5837 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
A51H9000-7 | 1650-01-253-5836 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
A51H9000-18 | 1650-01-253-5837 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
A51H9000-17 | 1650-01-253-5836 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
A51H9000-16 | 1650-01-089-6827 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
A51H9000-15 | 1650-01-091-2001 | reference number differentiating characteristics: as differentiated by the source control drawing no. criticality code justification: amdx and amgs first end hole diameter: 1.8745 inches minimum and 1.8750 inches maximum | Avl | RFQ |
A51H9000-14 | 1650-01-089-6828 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
A51H9000-13 | 1650-01-089-6829 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
A51H9000-12 | 1650-00-113-7674 | iii fsc application data: hydraulic systems, aircraft special features: right hand installation design characteristics: double acting single cylinder | Avl | RFQ |
A51H9000-11 | 1650-00-113-7673 | iii fsc application data: hydraulic systems, aircraft special features: left hand installation design characteristics: double acting single cylinder | Avl | RFQ |
A51H9000-10 | 1650-00-393-2645 | iii fsc application data: hydraulic systems, acft special features: right hand installation design characteristics: double acting single cylinder | Avl | RFQ |
3329520 | 1650-01-148-8853 | iii end item identification: f-111 acft design characteristics: single acting single cylinder body material: steel, corrosion resisting | Avl | RFQ |
3329418-2 | 1650-01-147-2661 | iii end item identification: f-111 aircraft; t.o.9h2-4-166-4 special features: cres 15-5ph, type a r.h. | Avl | RFQ |
3187000-9 | 1650-00-367-2955 | iii fsc application data: hydraulic systems, acft special features: left hand installation design characteristics: double acting single cylinder | Avl | RFQ |
3187000-8 | 1650-01-253-5837 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
3187000-7 | 1650-01-253-5836 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
3187000-18 | 1650-01-253-5837 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
3187000-17 | 1650-01-253-5836 | reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
3187000-16 | 1650-01-089-6827 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
3187000-15 | 1650-01-091-2001 | reference number differentiating characteristics: as differentiated by the source control drawing no. criticality code justification: amdx and amgs first end hole diameter: 1.8745 inches minimum and 1.8750 inches maximum | Avl | RFQ |
3187000-14 | 1650-01-089-6828 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
3187000-13 | 1650-01-089-6829 | design characteristics: single acting single cylinder bore diameter: 5.474 inches nominal extended length: 43.740 inches minimum and 43.860 inches maximum | Avl | RFQ |
3187000-12 | 1650-00-113-7674 | iii fsc application data: hydraulic systems, aircraft special features: right hand installation design characteristics: double acting single cylinder | Avl | RFQ |
3187000-11 | 1650-00-113-7673 | iii fsc application data: hydraulic systems, aircraft special features: left hand installation design characteristics: double acting single cylinder | Avl | RFQ |
3187000-10 | 1650-00-393-2645 | iii fsc application data: hydraulic systems, acft special features: right hand installation design characteristics: double acting single cylinder | Avl | RFQ |
3186800-9 | 1650-01-089-6812 | design characteristics: single acting single cylinder bore diameter: 2.431 inches nominal extended length: 21.625 inches nominal | Avl | RFQ |
3186800-11 | 1650-01-282-1212 | iii end item identification: f-14 acft reference number differentiating characteristics: as differentiated by the source control dwg no. | Avl | RFQ |
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