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 040505-166, 107200-103, 107200-105, 107240-105, 107820. 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 Hydraulics International Inc, Aerospace Filtration Systems Inc, General Electric Company, General Electric Engine Services, United Technologies Corporation. Our team provides superior quality assurance testing for and more. So if you are in need of Duct Turbine Aircraft Gas Turbin or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
Part No Part No
|
NSN NSN Parts
|
Details Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
040505-166 | 2840-01-572-2896 | End Item Identification: Hydraulic Fluid Purifier | Avl | RFQ |
107200-103 | 2840-01-530-2853 | Special Features: Assy-Transition Duct End Item Identification: Inlet Barrier, Uh-60 Blackhawk Helicopter | Avl | RFQ |
107200-105 | 2840-01-530-2853 | Special Features: Assy-Transition Duct End Item Identification: Inlet Barrier, Uh-60 Blackhawk Helicopter | Avl | RFQ |
107240-105 | 2840-01-573-4517 | NA | Avl | RFQ |
107820 | 2840-01-530-2853 | Special Features: Assy-Transition Duct End Item Identification: Inlet Barrier, Uh-60 Blackhawk Helicopter | Avl | RFQ |
1350M45P01 | 2840-01-625-2660 | NA | Avl | RFQ |
1676M19G02 | 2840-01-669-3156 | NA | Avl | RFQ |
1826M21G01 | 2840-01-529-0618 | NA | Avl | RFQ |
1B6380 | 2840-01-419-3525 | NA | Avl | RFQ |
1B6573 | 2840-01-411-1781 | NA | Avl | RFQ |
1B6574 | 2840-01-411-1783 | NA | Avl | RFQ |
2193M18G02 | 2840-01-534-3232 | NA | Avl | RFQ |
2193M18G02 | 2840-01-534-3232 | NA | Avl | RFQ |
255D9205-505 | 2840-01-625-2659 | NA | Avl | RFQ |
305-408-301-0 | 2840-01-187-3025 | Criticality Code Justification: Agav End Item Identification: Acft Eng F108 | Avl | RFQ |
305-408-301-0 | 2840-01-187-3025 | Criticality Code Justification: Agav End Item Identification: Acft Eng F108 | Avl | RFQ |
3074766-1 | 2840-01-594-3880 | NA | Avl | RFQ |
3075292-1 | 2840-01-594-3881 | NA | Avl | RFQ |
3075292-2 | 2840-01-594-3874 | NA | Avl | RFQ |
3075292-4 | 2840-01-594-3875 | NA | Avl | RFQ |
3077063-1 | 2840-01-594-3876 | NA | Avl | RFQ |
3077063-2 | 2840-01-594-3877 | NA | Avl | RFQ |
35923 | 2840-01-472-9160 | Engine Section Location: Turbine Special Features: Item Bends At 64 Degree Angle With Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
35956-3 | 2840-01-472-8686 | Special Features: Duct Is The Same As P/N 7-511712043-1 Except Length Is .18 In. Shorter Due To Part Reconfiguration, Must Meet The Following Requirements: Operating Medium-Air, Temp-550 Degrees Fahrenheit, Pressure-60 Psig Max, Proof Pressure-120 Psig Min., Burst Pressure-180 Psig Material: Steel Comp 321 Duct Overall Length: 9.130 Inches Nominal | Avl | RFQ |
4026508 | 2840-00-321-4577 | Criticality Code Justification: Agav Engine Section Location: Turbine Material: Nickel Alloy Overall | Avl | RFQ |
4035375 | 2840-00-338-5989 | Criticality Code Justification: Agav End Item Identification: Engine, Turbofan Model F100 | Avl | RFQ |
4061807 | 2840-01-231-6096 | NA | Avl | RFQ |
4070422 | 2840-01-270-7659 | Engine Section Location: Turbine Special Features: Stage 2 Material: Nickel Alloy Overall | Avl | RFQ |
4079332 | 2840-01-390-7448 | Criticality Code Justification: Feat And Agav Special Features: Duct And Support Set, Turbine; 1St Stage End Item Identification: F100pw229 Aircraft Engine | Avl | RFQ |
4079937 | 2840-01-390-7448 | Criticality Code Justification: Feat And Agav Special Features: Duct And Support Set, Turbine; 1St Stage End Item Identification: F100pw229 Aircraft Engine | Avl | RFQ |
4079968 | 2840-01-390-7448 | Criticality Code Justification: Feat And Agav Special Features: Duct And Support Set, Turbine; 1St Stage End Item Identification: F100pw229 Aircraft Engine | Avl | RFQ |
4080527 | 2840-01-387-0025 | Criticality Code Justification: Agav Special Features: Contains P/N's 4080526 & 4077682 Material: Steel Overall | Avl | RFQ |
4080635 | 2840-01-390-7448 | Criticality Code Justification: Feat And Agav Special Features: Duct And Support Set, Turbine; 1St Stage End Item Identification: F100pw229 Aircraft Engine | Avl | RFQ |
4082486 | 2840-01-390-7448 | Criticality Code Justification: Feat And Agav Special Features: Duct And Support Set, Turbine; 1St Stage End Item Identification: F100pw229 Aircraft Engine | Avl | RFQ |
4082862 | 2840-01-411-1802 | Criticality Code Justification: Agav Special Features: Used On 1St Stage End Item Identification: F100-Pw-229 | Avl | RFQ |
4082922 | 2840-01-426-1409 | Criticality Code Justification: Czbj And Feat Engine Section Location: Turbine Special Features: T.O. 2J-F100-24, Fig 109, Ind 19; Includes Hard Coat Face To Extend Life; Replaces P/N 4070422 | Avl | RFQ |
4082975 | 2840-01-441-0108 | Criticality Code Justification: Abmz Engine Section Location: Turbine Material: Steel Duct | Avl | RFQ |
4082982 | 2840-01-438-6189 | Criticality Code Justification: Abhp And Abmz And Abmk And Czbj Engine Section Location: Turbine Special Features: 2Nd Stage Segment | Avl | RFQ |
4084714 | 2840-01-446-5313 | NA | Avl | RFQ |
4084714 | 2840-01-446-5313 | Criticality Code Justification: Czbj And Abmk And Abhp And Abkw And Feat Engine Section Location: Turbine Special Features: Stage 2 | Avl | RFQ |
4086296 | 2840-01-504-2792 | NA | Avl | RFQ |
4086297 | 2840-01-504-2791 | Criticality Code Justification: Agav End Item Identification: F-100 | Avl | RFQ |
4086467 | 2840-01-504-5226 | Criticality Code Justification: Agav Engine Section Location: Turbine End Item Identification: F-100-Pw-220 | Avl | RFQ |
4086836 | 2840-01-527-3969 | Criticality Code Justification: Agav Engine Section Location: Turbine End Item Identification: F100pw229 Engine | Avl | RFQ |
4119080 | 2840-01-622-8191 | NA | Avl | RFQ |
4130415 | 2840-01-622-8239 | NA | Avl | RFQ |
4131603 | 2840-01-622-8276 | NA | Avl | RFQ |
4322293-04 | 2840-01-652-8814 | NA | Avl | RFQ |
5050M17G06 | 2840-01-593-7057 | NA | Avl | RFQ |
6049T48G15 | 2840-01-626-5621 | NA | Avl | RFQ |
6068T28G01 | 2840-01-510-8689 | End Item Identification: Ct 7 Aircraft Part Name Assigned By Controlling Agency: Inner Turbine Duct | Avl | RFQ |
6068T28G03 | 2840-01-510-8689 | End Item Identification: Ct 7 Aircraft Part Name Assigned By Controlling Agency: Inner Turbine Duct | Avl | RFQ |
6069T41G03 | 2840-01-443-5956 | Criticality Code Justification: Agav End Item Identification: General Electric F414a Aircraft Turbine Engine. Part Name Assigned By Controlling Agency: Duct, High Pressure Turbine, Rotor, Air | Avl | RFQ |
6865407 | 2840-00-929-0325 | Criticality Code Justification: Agav End Item Identification: Acft Eng Tf41 | Avl | RFQ |
7 511711042 3 | 2840-01-472-3043 | NA | Avl | RFQ |
7-511711042-3 | 2840-01-472-3043 | Engine Section Location: Turbine Special Features: Tubular-Shaped Item That Bends At A 38 Degree Angle With A Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
7-511712034 | 2840-01-471-7324 | Engine Section Location: Turbine Special Features: Opened Tubular-Shaped Item That Has Flanges On Both Ends With An Additional Internally Threaded Opening Material: Steel Comp 321 Duct | Avl | RFQ |
7-511712034-1 | 2840-01-471-7324 | Engine Section Location: Turbine Special Features: Opened Tubular-Shaped Item That Has Flanges On Both Ends With An Additional Internally Threaded Opening Material: Steel Comp 321 Duct | Avl | RFQ |
7-511712042 | 2840-01-472-9160 | Engine Section Location: Turbine Special Features: Item Bends At 64 Degree Angle With Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
7-511712042-1 | 2840-01-472-9160 | Engine Section Location: Turbine Special Features: Item Bends At 64 Degree Angle With Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
7-511712043 | 2840-01-472-8686 | Special Features: Duct Is The Same As P/N 7-511712043-1 Except Length Is .18 In. Shorter Due To Part Reconfiguration, Must Meet The Following Requirements: Operating Medium-Air, Temp-550 Degrees Fahrenheit, Pressure-60 Psig Max, Proof Pressure-120 Psig Min., Burst Pressure-180 Psig Material: Steel Comp 321 Duct Overall Length: 9.130 Inches Nominal | Avl | RFQ |
7-511712043-3 | 2840-01-472-8686 | Special Features: Duct Is The Same As P/N 7-511712043-1 Except Length Is .18 In. Shorter Due To Part Reconfiguration, Must Meet The Following Requirements: Operating Medium-Air, Temp-550 Degrees Fahrenheit, Pressure-60 Psig Max, Proof Pressure-120 Psig Min., Burst Pressure-180 Psig Material: Steel Comp 321 Duct Overall Length: 9.130 Inches Nominal | Avl | RFQ |
70044 | 2840-01-472-9160 | Engine Section Location: Turbine Special Features: Item Bends At 64 Degree Angle With Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
70044-1 | 2840-01-472-9160 | Engine Section Location: Turbine Special Features: Item Bends At 64 Degree Angle With Flange On One End Material: Steel Comp 321 Duct | Avl | RFQ |
70500-03180 | 2840-01-502-4982 | NA | Avl | RFQ |
70500-03180 | 2840-01-502-4990 | NA | Avl | RFQ |
70500-03180-041 | 2840-01-502-4982 | NA | Avl | RFQ |
70500-03180-101 | 2840-01-502-4990 | NA | Avl | RFQ |
74A838133-1007 | 2840-01-647-9244 | NA | Avl | RFQ |
74A838134-1005 | 2840-01-647-9246 | NA | Avl | RFQ |
802186-5 | 2840-01-483-1337 | Overall Length: 4.410 Inches Nominal End Item Identification: C-295 Aircraft Part Name Assigned By Controlling Agency: Turbine Outlet Duct | Avl | RFQ |
8A1874 | 2840-01-389-6106 | NA | Avl | RFQ |
8A2289 | 2840-01-399-4857 | NA | Avl | RFQ |
8A2868 | 2840-01-399-4857 | NA | Avl | RFQ |
9079M30P01 | 2840-00-419-5935 | Criticality Code Justification: Agav End Item Identification: Tf-30 Aircraft Engine | Avl | RFQ |
9079M30P02 | 2840-00-419-6027 | Criticality Code Justification: Agav End Item Identification: Tf-30 Aircraft Engine | Avl | RFQ |
9514M54G02 | 2840-01-184-8963 | Criticality Code Justification: Agav End Item Identification: Acft Eng F-108 | Avl | RFQ |
9514M54G02 | 2840-01-184-8963 | Criticality Code Justification: Agav End Item Identification: Acft Eng F-108 | Avl | RFQ |
9693M73P01 | 2840-00-419-5935 | Criticality Code Justification: Agav End Item Identification: Tf-30 Aircraft Engine | Avl | RFQ |
9693M73P02 | 2840-00-419-6027 | Criticality Code Justification: Agav End Item Identification: Tf-30 Aircraft Engine | Avl | RFQ |
LJ75951 | 2840-01-596-8640 | NA | Avl | RFQ |
LJ76369 | 2840-01-596-8641 | NA | Avl | RFQ |
LJ76644 | 2840-01-619-9670 | NA | Avl | RFQ |
LJ76676 | 2840-01-596-8642 | NA | Avl | RFQ |
LJ76679 | 2840-01-596-8643 | NA | Avl | RFQ |
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