Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number 204-91965-1, a Test Set Subassembl item that is listed with the NSN 4920-01-020-8027 for an ease of identification. Manufactured by The Boeing Company and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number 204-91965-1 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number 204-91965-1 is manufactured by The Boeing Company, it is specifically done so under CAGE Code 81205, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 4920-01-020-8027, one can also determine that this part falls under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
| 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 |
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