Thank you for taking interest in General Electric Company part number 3R1403P01, which is listed with the NSN 4920-01-502-2429 and a product description of “Template Aircraft M.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 0.125 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | F110-GE-100, -129, -400 ENGINES |
ABMK | OVERALL WIDTH | 1.300 INCHES NOMINAL |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | TEMPLATE, CONTOUR CIRCUMFERENTAIL, EXHAUST NOZZLE PRIMARY FLAP |
FTLD | III FUNCTIONAL DESCRIPTION | USED TO INSPECT WORN EXHAUST NOZZLE PRIMARY FLAP CAM TRACKS FOR WEAR. TEMPLATE IS USED WITH CAM TRACK AXIAL CONTOUR TEMPLATE 3R1404P01 |
ABHP | OVERALL LENGTH | 1.600 INCHES NOMINAL |
MATT | MATERIAL | STEEL |
RDAL | III REFERENCE DATA AND LITERATURE | SERD 6179 |
SR-5 | THE MANUFACTURERS DATA | |
SR-5 | MANUFACTURERS CODE | 07482 |
SR-5 | DESIGN CONTROL REFERENCE | 3R1403P01 |
RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | PROTOTYPE FOR THIS MARKED WITH SUFFIX DEV. ALTERNATE PART IS L250168B |
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