Aircraft Prime Moving Gas Turbines and Jet Engines and Components: 2840PL0786512, 2840PL0786531, 2840PL0788957
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2840PL0786512 | 2840-00-111-5709 | Support, Turbine Component, Aircra | Inside Diameter: 35.047 inches minimum and 35.063 inches maximum Overall Length: 0.540 inches minimum and 0.560 inches maximum Outside Diameter: 38.725 inches minimum and 38.755 inches maximum | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0786515 | 2840-00-117-4916 | Seal, Air, Aircraft Gas Turbine En | Overall Length: 1.830 inches minimum and 1.860 inches maximum End Item Identification: Acft eng TF-39 Criticality Code Justification: AGAV | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0786519 | 2840-00-116-7915 | Shield, Heat, Aircraft Gas Turbine | Overall Length: 1.950 inches minimum and 2.010 inches maximum End Item Identification: Acft eng TF-39 Criticality Code Justification: AGAV | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0786531 | 2840-00-111-5707 | Shroud Segment, Turbine, Aircraft | Overall Length: 1.785 inches minimum and 1.815 inches maximum Overall Width: 0.270 inches minimum and 0.290 inches maximum End Item Identification: Acft eng TF-39 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788856 | 2840-00-340-7326 | Housing Assembly, Transfer Tube L | End Item Identification: Acft eng F100 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788942 | 2840-00-365-2124 | Channel, Loop Clamp | End Item Identification: F100-PW-100/-200/-220 aircraft engines General Characteristics Item Description: Cobalt alloy, AMS5382, 1.330 in. min, 1.350 in. max lg, 0.660IN. min, 0.670 in. max W, 0.255 in. min, 0.275 in. max, H | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788943 | 2840-01-215-3549 | Seal, Air, Aircraft Gas Turbine En | Overall Length: 0.040 inches nominal Diameter: 54.140 inches minimum and 54.240 inches maximum End Item Identification: Acft eng F100-PW-200/-220/-229 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788944 | 2840-01-216-0466 | Retainer, Turbine Blade, Aircraft | Overall Length: 0.650 inches nominal End Item Identification: F100-PW-100/-200 aircraft engines Criticality Code Justification: AGAV | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788945 | 2840-01-240-3591 | Tank, Lubricating Oil, Aircraft Ga | End Item Identification: Acft.eng. F100-220 Criticality Code Justification: AGAV | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788946 | 2840-01-316-9910 | Synchronizing Ring, Compressor, Ai | End Item Identification: Acft eng F100PW0229 Criticality Code Justification: AGAV Stage Number: 4 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788947 | 2840-01-316-9945 | Seal, Metallic, Aircraft Gas Turbi | End Item Identification: Acft eng F100PW0229/FAN module Criticality Code Justification: AGAV | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788949 | 2840-01-318-4860 | Plate, Component Mounting, Aircraf | End Item Identification: F100PW0229 engine Criticality Code Justification: AGAV Material: Titanium alloy overall | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788950 | 2840-01-318-7541 | Shroud Segment, Turbine, Aircraft | End Item Identification: Acft eng F100PW0229 Criticality Code Justification: AGAV Engine Section Location: Compressor | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788951 | 2840-01-320-0758 | Lock, Nozzle Hinge Pin, Turbine En | Overall Length: 0.640 inches nominal Overall Width: 0.190 inches nominal End Item Identification: F100PW0229 engine/aug mod | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788952 | 2840-01-320-5344 | Seal, Air, Aircraft Gas Turbine En | Overall Length: 1.866 inches minimum and 1.906 inches maximum Diameter: 18.335 inches minimum and 18.345 inches maximum Material Thickness: 0.040 inches minimum and 0.050 inches maximum | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788953 | 2840-01-320-6432 | Seal, Air, Aircraft Gas Turbine En | Overall Length: 20.570 inches minimum and 20.630 inches maximum End Item Identification: F100-229 aircraft gas turbine engine Criticality Code Justification: Abhp and feat | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788954 | 2840-01-387-5713 | Plug, Turbine Case, Aircraft Gas T | Criticality Code Justification: FEAT Part Name Assigned BY Controlling Agency: Original name plug borescope, aircraft gas turbine engine Special Features: T.O. 2J-F100-54; includes spacer, spring, cover and rivet | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788955 | 2840-01-364-7166 | Retainer, Compressor Blade, Aircra | End Item Identification: Acft eng F100PW229 Criticality Code Justification: AGAV Part Name Assigned BY Controlling Agency: Original name retainer, turbine blade, aircraft gas turbine engine | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788956 | 2840-01-365-6878 | Vane Segment, Compressor, Aircraft | Overall Length: 5.412 inches minimum and 5.448 inches maximum End Item Identification: Acft eng F100PW0229 Engine Section Location: Compressor | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2840PL0788957 | 2840-01-366-2958 | Shroud Segment, Turbine, Aircraft | Overall Length: 1.006 inches minimum and 1.010 inches maximum Diameter: 18.802 inches nominal End Item Identification: F100PW0229 aircraft engine | Inspektorat Wsparcia SIL Zbrojnych (9009H) |