Thank you for taking interest in The Boeing Company part number 204-91965-1, which is listed with the NSN 4920-01-020-8027 and a product description of “Test Set Subassembl.” 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.
Note : We Will Not Share Your Information To Any Third Parties.
Alongside part number 204-91965-1, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Test Set Subassembl part with the NSN 4920-01-020-8027. For example, you can browse other The Boeing Company components that were produced under CAGE Code 81205 or listings that belong to FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 204-91965-1 and other desired offerings on Aerospace Spare.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 8.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 8.750 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | 4EA TYPE 509 6-VOLT BATTERY POWER SOURCE |
| NTRD | III ENTRY DATE | 77-01-01 |
| ABHP | OVERALL LENGTH | 12.000 INCHES NOMINAL |
| SR-5 | DESIGN CONTROL REFERENCE | 204-91965-1 |
| AGAV | III END ITEM IDENTIFICATION | E-3A AIRCRAFT |
| FTLD | III FUNCTIONAL DESCRIPTION | USED DURING PERFORMANCE OF UNSCHEDULED INTERMEDIATE MAINTENANCE AT THE FLIGHTLINE TO VERIFY THE DC PARAMETER OUTPUTS WHILE TROUBLESHOOTING AND FAULT ISOLATING. THE SIGNAL OUTPUTS FROM THE EGT AND EPR INDICATORS, AND FUEL FLOW (FF) AMPLIFIER ARE REQUIRED TO EXERCISE THOSE CHANNELS OF DATA RECORDED BY THE FLIGHT RECORDER/LOCATOR SYSTEM. THE OUTPUT OF THE FLIGHT RECORDER/LOCATOR SYSTEM IS MONITORED BY THE DATA DISPLAY MONITOR (DDU-4) AS THE INPUT SIGNAL IS VARIED FROM 0 TO 5 VOLTS DC. THE SIGNALS ARE GENERATED BY OPERATING ENGINES OR BY PROVIDING A SIMULATED VOLTAGE AT THE OUTPUT OF EACH INDICATOR AND THE AMPLIFIER. THE INPUT IMPEDANCE OF THE SIGNAL DATA CONVERTER BETWEEN HIGH AND LOW IS 150,000 OHMS (+O.1%) |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | FLIGHT RECORDER/LOCATOR SYSTEM SIMULATOR TEST ADAPTER SET |
| RDAL | III REFERENCE DATA AND LITERATURE | T.O.1E-3A-2-23-1 COMMUNICATIONS SYSTEM USAF SECTION X11 AND T.O.35-1-251-1 |
| SR-5 | MANUFACTURERS CODE | 81205 |
| SR-5 | THE MANUFACTURERS DATA |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
