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 23001967, 23004233, 23004362, 23004540, 23004917. 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 Allison Transmission Holdings Inc, General Electric Company, Cincinnati Sub Zero Products Inc, Cfm International Inc. Our team provides superior quality assurance testing for and more. So if you are in need of Rotor Turbine Aircraft Gas Turbi or any other NSN parts, submit an Instant RFQ and receive a quote in as little as 15 minutes.
Allison Transmission Holdings Inc | General Electric Company | Cincinnati Sub Zero Products Inc |
Cfm International Inc |
Part No Part No
|
NSN NSN Parts
|
Details Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
23001967 | 2840-01-160-7986 | Iii End Item Identification: T63-A-700 And T63-A-720 (Turbine Engine), Rotary Wing Aircraft | Avl | RFQ |
23004233 | 2840-01-166-9054 | Iii End Item Identification: Oh-58D Series Turbine Engine Criticality Code Justification: Feat Special Features: An Item That Is Designed To Receive The Latent Energy Of Combustion Gas. The Item Consist Of A Disk Or Disks. Flight Safety Critical Aircraft Part. | Avl | RFQ |
23004362 | 2840-01-122-1879 | Iii End Item Identification: Acft Eng Tf41 Criticality Code Justification: Agav Overall Length: 14.590 Inches Nominal | Avl | RFQ |
23004540 | 2840-01-216-0188 | NA | Avl | RFQ |
23004917 | 2840-01-119-1223 | Iii End Item Identification: Acft Eng Tf41 Criticality Code Justification: Agav | Avl | RFQ |
23005175 | 2840-01-124-4772 | Iii End Item Identification: Acft Eng Tf 41 Criticality Code Justification: Agav | Avl | RFQ |
23005176 | 2840-01-124-4776 | Iii End Item Identification: Acft Eng Tf 41 Criticality Code Justification: Agav | Avl | RFQ |
23008128 | 2840-01-157-9212 | Iii End Item Identification: Acft Eng Tf-41 Criticality Code Justification: Agav | Avl | RFQ |
23008129 | 2840-01-157-9211 | Iii End Item Identification: Acft Eng Tf-41 Criticality Code Justification: Agav | Avl | RFQ |
23030653 | 2840-01-190-8244 | Iii End Item Identification: Acft Eng Tf41 Criticality Code Justification: Agav | Avl | RFQ |
23065833 | 2840-01-497-6180 | Iii Part Name Assigned By Controlling Agency: Rotor Assembly | Avl | RFQ |
23073352 | 2840-01-518-3996 | Iii End Item Identification: Rolls Royce 250-C20r, Aircraft Engine Section Location: Turbine | Avl | RFQ |
23073813 | 2840-01-546-1799 | Engine Section Location: Turbine Stage Number: 2 | Avl | RFQ |
23073814 | 2840-01-546-1796 | Engine Section Location: Turbine Stage Number: 2 | Avl | RFQ |
23073853 | 2840-01-485-7890 | Iii End Item Identification: Oh-58 Kiowa Warrior Engine (T-63) | Avl | RFQ |
23073854 | 2840-01-485-7891 | Iii End Item Identification: Oh-58 Kiowa Warrior Engine (T-63) | Avl | RFQ |
3048T90G01 | 2840-01-515-3538 | Iii End Item Identification: T700-Ge-701C/701D Engines For Uh60/Ah64 | Avl | RFQ |
37D401329G013 | 2840-00-456-0447 | Iii End Item Identification: J-85 Aircraft Engine Criticality Code Justification: Agav And Feat Engine Section Location: Turbine | Avl | RFQ |
37D401329G015 | 2840-01-009-2470 | Iii End Item Identification: Aircraft Engine Model J85-Ge-4 | Avl | RFQ |
37D401329G019 | 2840-01-005-3050 | Iii End Item Identification: Engine Turbojet, Model No. J85ge-13 And J85ge-17A Criticality Code Justification: Agav And Feat Special Features: Fscap | Avl | RFQ |
37D401329G021 | 2840-01-224-2200 | Iii End Item Identification: Acft.Eng.J-85 Criticality Code Justification: Agav Reference Data And Literature: T.O. 2J-J85-64 | Avl | RFQ |
37D401329G024 | 2840-01-281-2772 | Iii End Item Identification: Acgt Eng J85-Ge-5J/-13D/-17A Criticality Code Justification: Agav And Feat Special Features: Fscap | Avl | RFQ |
4001T93G08 | 2840-00-758-1600 | NA | Avl | RFQ |
4003T71G05 | 2840-00-824-1924 | NA | Avl | RFQ |
4003T72G01 | 2840-00-907-2639 | NA | Avl | RFQ |
4003T72G04 | 2840-00-825-2782 | NA | Avl | RFQ |
4006T34G02 | 2840-00-824-3282 | Iii End Item Identification: Acft Eng J79, J85, T58, T64 Criticality Code Justification: Agav | Avl | RFQ |
4006T34G06 | 2840-01-006-4537 | Iii End Item Identification: Engine Model T58 | Avl | RFQ |
5001T68G11 | 2840-00-168-9987 | NA | Avl | RFQ |
5003T33G23 | 2840-01-141-9790 | NA | Avl | RFQ |
5003T33G28 | 2840-01-226-5071 | NA | Avl | RFQ |
5003T33G31 | 2840-01-526-6266 | NA | Avl | RFQ |
5013T22G12 | 2840-01-005-8172 | Iii End Item Identification: Acft Eng J85ge21 Criticality Code Justification: Agav | Avl | RFQ |
5013T22G13 | 2840-01-063-1127 | Iii End Item Identification: Engine, Aircraft, Model No. J85ge21 | Avl | RFQ |
5013T22G15 | 2840-01-048-1923 | Iii End Item Identification: Aircraft Engine J85-Ge-21A Criticality Code Justification: Agav Special Features: T.O. 2J-J85-94; Includes Disks, Blades, Hubs & The Like, Located On A Turbine Shaft | Avl | RFQ |
5013T22G17 | 2840-01-084-6852 | Iii End Item Identification: Acft Eng J85 Criticality Code Justification: Agav Special Features: T.O. 2J-J85-94; Includes Disks, Blades, Hubs & The Like, Located On A Turbine Shaft | Avl | RFQ |
5056T83G12 | 2840-01-494-7400 | Iii End Item Identification: Used On Engine Model Ct7-5Ct7-7 | Avl | RFQ |
5101T32G01 | 2840-01-443-2713 | Iii End Item Identification: Low Pressure Turbine Module;F414-Ge-400 Engine Criticality Code Justification: Agav Special Features: A1-F414a-Ipb-400, Figure 047/Index 2 | Avl | RFQ |
5111T23G05 | 2840-01-443-4229 | Iii End Item Identification: Preprovisioning Support Navicp Is Poe Criticality Code Justification: Agav Engine Section Location: Turbine | Avl | RFQ |
5921T79G01 | 2840-01-387-9721 | NA | Avl | RFQ |
6825185 | 2840-00-799-0276 | Iii End Item Identification: J-33 Aircraft Engine Criticality Code Justification: Czbj Engine Section Location: Turbine | Avl | RFQ |
6841275 | 2840-00-065-2929 | Iii End Item Identification: Acft Eng T56 Criticality Code Justification: Agav | Avl | RFQ |
6843393 | 2840-00-940-8724 | NA | Avl | RFQ |
6844065 | 2840-00-065-2929 | Iii End Item Identification: Acft Eng T56 Criticality Code Justification: Agav | Avl | RFQ |
6846932 | 2840-00-012-7110 | NA | Avl | RFQ |
6847449 | 2840-00-940-8452 | Iii End Item Identification: T63-A-700 And T63-A-720 Engines Criticality Code Justification: Feat Special Features: Cres, Ems73634 Fscm 73342, 44 Blades, 7.170 In. Min, 7.172 In. Max O/A Od, 1.319 In. Min, 1.321 In. Max O/A Lg, 1St End Hub, Ext Splines, 20 Teeth, 30 Deg Pressure Angle, 1.938 In.-24 Ext Thd Located 0.090 In. Nom Distance From 1St End, 0.250 In. Nom Thd Lg, 10 Holes 0.200 In. Nom Dia Equally Spaced On Od Hub, 0.520In. Nom C To C Distance From 1St End To Holes, 2Nd End Hub, Ext Splines, 20 Teeth, 30 Deg Pressure Angle, Stepped Id, 1.1585 In. Min, 1.1590 In. Max Smallest Id.Flight Safety Critical Aircraft Part | Avl | RFQ |
6851830 | 2840-00-938-3864 | Iii End Item Identification: Acft Eng T56 Criticality Code Justification: Agav And Feat Special Features: Fscap | Avl | RFQ |
6852171 | 2840-00-941-8746 | NA | Avl | RFQ |
6852555 | 2840-00-908-1324 | Iii End Item Identification: T-56 Aircraft Engine Criticality Code Justification: Agav And Feat Special Features: Fscap | Avl | RFQ |
6859000 | 2840-00-109-6465 | Iii End Item Identification: T56 Engine Criticality Code Justification: Agav Special Features: Fscap | Avl | RFQ |
6867967 | 2840-00-408-3676 | Iii End Item Identification: Tf-41 Aircraft Engine Criticality Code Justification: Agav | Avl | RFQ |
6867969 | 2840-00-157-1055 | Iii End Item Identification: Acft.Eng. Tf-41 Criticality Code Justification: Agav | Avl | RFQ |
6873135 | 2840-00-493-4569 | Iii End Item Identification: Acft Eng T56 Criticality Code Justification: Agav And Feat Special Features: Fscap | Avl | RFQ |
6873338 | 2840-01-089-3950 | Iii End Item Identification: Applicable To The T56a15 Engine | Avl | RFQ |
6877092 | 2840-00-217-6691 | NA | Avl | RFQ |
6886407 | 2840-01-034-4661 | Special Features: 38 Blades; 6.189 Min 6.192 Max In. O/A Od; 1St End Stepped Hub; Ext Thd 1St Step 1St End, 3/4-20 Unjef Series Cl 3A Thd, Lh; 0.375 In. Nom Lg 1St Step 1St End; 0.66 In. Nom Od 2Nd Step 1St End; 0.125 In. Nom Lg 2Nd Step 1St End; 0.7874 Min 0.7876 Max In. Od 3Rd Step 1St End; 0.6 In. Nom Lg 3Rd Step 1St End; 2 Circular Grooves On Od 3Rd Step 1St End; 0.1 In. Nom W By 0.75 In. Nom Dia Grooves; 0.8195 Min 0.82 Max In. Od 4Th Step 1St End; 0.47 In. Nom Lg 4Th Step 1St End; 1 Circular Groove Located On Od 4Th Step 1St End; 0.2 In. Nom W By 0.75 In. Nom Dia Groove; 0.92 In. Max Lg 5Th Step 1St End; 2Nd End Grooved Hub; 1.809 Min 1.811 Max In. O/A Od Hub; 0.318 Min 0.326 Max In. Lg From 2Nd End To Disk; 2 Circular U-Grooves On Od Hub; 0.07 In. Nom W By 1.65 In. Nom Dia Grooves; Stepped Id 0.52 Min 0.522 Max In. Id Countersunk 60 Deg To 0.575 Overall Length: 2.734 Inches Minimum And 2.736 Inches Maximum Material Document And Classification: Cres, Ems73646-1 Cage 73342 Mfr Ref Single Material Response Overall | Avl | RFQ |
6887113 | 2840-01-041-0198 | Special Features: 30 Blades Equally Spaced On Outer Periphery; Tapered Od, 7.51 Min 7.512 Max In. Largest Od; 10 Slots Equally Spaced On Outer Periphery; 1.159 Min 1.1595 Max In. Id Material Document And Classification: Cres, Ems736483 Cage 73342 Mfr Ref Single Material Response Overall | Avl | RFQ |
6887150 | 2840-00-515-0440 | Iii End Item Identification: Engine, Aircraft, Turboprop, Model T56a15 Criticality Code Justification: Agav | Avl | RFQ |
6888600 | 2840-01-053-3489 | Iii End Item Identification: Aircraft Engine Model T56-A-7A Criticality Code Justification: Feat Special Features: Fscap | Avl | RFQ |
6891588 | 2840-01-041-0198 | Special Features: 30 Blades Equally Spaced On Outer Periphery; Tapered Od, 7.51 Min 7.512 Max In. Largest Od; 10 Slots Equally Spaced On Outer Periphery; 1.159 Min 1.1595 Max In. Id Material Document And Classification: Cres, Ems736483 Cage 73342 Mfr Ref Single Material Response Overall | Avl | RFQ |
6892415 | 2840-01-044-9872 | Iii End Item Identification: Engine Model Tf-41 | Avl | RFQ |
6892600 | 2840-01-053-3489 | Iii End Item Identification: Aircraft Engine Model T56-A-7A Criticality Code Justification: Feat Special Features: Fscap | Avl | RFQ |
6892764 | 2840-01-166-3563 | Iii End Item Identification: Oh-58D Series Turbine Engines Criticality Code Justification: Feat Special Features: An Item That Is Designed To Receive The Latent Energy Of Combustion Gas.The Item Consists Of A Disk Or Disks. Flight Safety Critical Aircraft Part | Avl | RFQ |
6893556 | 2840-01-064-3140 | Iii End Item Identification: Engine Model Tf41 Criticality Code Justification: Agav | Avl | RFQ |
6893561 | 2840-01-044-9871 | Iii End Item Identification: Engine Model Tf-41 | Avl | RFQ |
6893856 | 2840-01-057-7833 | Iii End Item Identification: Tf41-A-2 Engine | Avl | RFQ |
6894160 | 2840-01-059-1355 | Iii End Item Identification: Acft Engine T56a15 Criticality Code Justification: Agav | Avl | RFQ |
6894578 | 2840-01-064-3139 | Iii End Item Identification: Engine Model Tf41 | Avl | RFQ |
6895015 | 2840-01-057-7834 | Iii End Item Identification: T56-A-16 | Avl | RFQ |
6898567 | 2840-01-074-1402 | NA | Avl | RFQ |
6898663 | 2840-01-166-9055 | Iii End Item Identification: Oh-58D Series Turbine Engine Criticality Code Justification: Feat Special Features: An Item That Is Designed To Receive The Latent Energy Of Combustion Gas.The Item Consist Of A Disk Or Disks. Flight Safety Critical Aircraft Part | Avl | RFQ |
6898725 | 2840-01-435-2792 | Iii End Item Identification: T63-A-700 And T63-A-720 (Turbine Engine), Rotary Wing Aircraft | Avl | RFQ |
6898753 | 2840-01-067-9990 | NA | Avl | RFQ |
6898763 | 2840-01-067-9990 | NA | Avl | RFQ |
6898782 | 2840-01-076-5887 | Iii End Item Identification: T63-A-700 And T63-A-720 Engines Criticality Code Justification: Feat Special Features: Cres Ems73649-2, Fscm 73342, 48 Blades Equally Spaced On Outer Periphery, 6.409 In. Min, 6.411 In. Max Od, External Spline, 17 Teeth, 0.562 In. Min, 0.567 In. Max Od, 0.5313 In. Nom Pitch Dia, 30 Deg Pressure Angle, External Thd, 0.8438 In.-32 Unjs Class 3A Thd, 0.8378 In. Min, 0.8438 In. Max Od. Flight Safety Critical Aircraft Part | Avl | RFQ |
6898911 | 2840-01-176-3578 | NA | Avl | RFQ |
6899373 | 2840-01-074-1402 | NA | Avl | RFQ |
75921T79G01 | 2840-01-387-9721 | NA | Avl | RFQ |
933A427P1 | 2840-00-955-3098 | NA | Avl | RFQ |
9545M18G21 | 2840-01-451-8810 | NA | Avl | RFQ |
9547M18G08 | 2840-01-347-2228 | Iii End Item Identification: F110-Ge-129 Acft Eng Criticality Code Justification: Agav Engine Section Location: High Pressure Turbine | Avl | RFQ |
9547M19 | 2840-01-394-5886 | Iii End Item Identification: Acft Eng F110 Criticality Code Justification: Agav | Avl | RFQ |
9547M19 | 2840-01-423-9307 | Iii End Item Identification: Acft Eng F110 Criticality Code Justification: Agav | Avl | RFQ |
9547M19 | 2840-01-447-2504 | Iii End Item Identification: Acft Eng F110 Criticality Code Justification: Agav | Avl | RFQ |
9547M19 | 2840-01-450-8982 | Iii End Item Identification: Acft Eng F110 Criticality Code Justification: Agav | Avl | RFQ |
9547M19G03 | 2840-01-394-5886 | Iii End Item Identification: Acft Eng F110 Ge129 Criticality Code Justification: Agav Engine Section Location: Low Pressure Turbine | Avl | RFQ |
9547M19G08 | 2840-01-447-2504 | Iii End Item Identification: F110-Ge-129 Aircraft Gas Turbine Engine Criticality Code Justification: Feat And Czbj Engine Section Location: Low Pressure Turbine | Avl | RFQ |
9547M19G09 | 2840-01-450-8982 | NA | Avl | RFQ |
9550M19 | 2840-01-380-4693 | NA | Avl | RFQ |
9550M19G16 | 2840-01-380-4693 | NA | Avl | RFQ |
9550M58G07 | 2840-01-349-5826 | Iii End Item Identification: Acft Eng F101 Engine Section Location: High Pressure Turbine Overall Length: 18.993 Inches Minimum And 19.028 Inches Maximum | Avl | RFQ |
9550M58G08 | 2840-01-349-5826 | Iii End Item Identification: Acft Eng F101 Engine Section Location: High Pressure Turbine Overall Length: 18.993 Inches Minimum And 19.028 Inches Maximum | Avl | RFQ |
9995M22G01 | 2840-01-139-2392 | Iii End Item Identification: Acft Eng F108-Cf-100 Criticality Code Justification: Agav Engine Section Location: Compressor | Avl | RFQ |
9995M22G04 | 2840-01-139-2392 | Iii End Item Identification: Acft Eng F108-Cf-100 Criticality Code Justification: Agav Engine Section Location: Compressor | Avl | RFQ |
9995M22G06 | 2840-01-139-2392 | Iii End Item Identification: Acft Eng F108-Cf-100 Criticality Code Justification: Agav Engine Section Location: Compressor | Avl | RFQ |
9995M22G07 | 2840-01-139-2392 | Iii End Item Identification: Acft Eng F108-Cf-100 Criticality Code Justification: Agav Engine Section Location: Compressor | Avl | RFQ |
9995M22G07C | 2840-01-598-7366 | NA | Avl | RFQ |
9995M22G07C-2A | 2840-01-601-7068 | NA | Avl | RFQ |
PMA9995M22G06 | 2840-01-575-4544 | NA | Avl | RFQ |
PMA9995M22G07 | 2840-01-575-4544 | Iii End Item Identification: F108 Engine | Avl | RFQ |
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