Maintenance Parts Pro is pleased to offer procurement options for Boeing Company The part number 14H02000-001, a Testing Machine Ele product we carry that is listed with the NSN 4920-01-336-6555 for seamless identification. As this item is available for purchase today, be sure to fill out and submit the Request for Quote (RFQ) form on this page if you are interested in obtaining pricing information. All that we ask is that you share details like your budget, desired quantity, and expected fulfillment speed so that we can respond with the most fitting solutions for your comparisons.
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Alongside streamlined quotation processes, we aim to support our customers by providing as much relevant listing information and data with product offerings as possible. For example, part number 14H02000-001 specifically traces back to Boeing Company The through CAGE Code 43999, as well as belongs to the FSC [FSC] as per its NSN of 4920-01-336-6555. Referencing such details, you can locate and procure exact specifications with ease. With our various practices in mind, do not hesitate to request a quote on part number 14H02000-001 using our provided form.
MRC | Criteria | Characteristic |
---|---|---|
RDAL | Reference Data And Literature | SERD NO. 14H02C |
MRC | Decoded Requirement | Clear Text Reply |
TEXT | General Characteristics Item Description | ETHE EQUIPMENT IS HOUSED IN A 72.000 INCH HIGH SINGLE BAY METAL RACK CONSOLE MOUNTED ON HEAVY DUTY CASTERS WITH LOCK-UP; THE EQUIPMENT IS TO BE OPERATED WITHIN A SHELTERED ENVIRONMENT AT50 F TO 95 F |
FTLD | Functional Description | USED TO ALIGN THE HYDRAULIC ACTUATORS FOR SPOILERS,RUDDER AND HORIZONTAL STABILIZER AFTER REMOVAL AND REPLACEMENT AS A FUNCTION OF PERIODIC CHECK; WILL INTERFACE WITH THE AIRCRAFT HYDRAULIC PRESSURE TRANSDUCERS AND PROCESS THE OUTPUT SIGNALS OF THESE TRANSDUCERS AND CALCULATE AND DISPLAY INDIVIDUAL CYLINDER PRESSURES,TOTAL FORCES AND TORQUE MEASUREMENTS |
AGAV | End Item Identification | U/O B-1B ACFT |
FEAT | Special Features | SET IS A COMPUTER-BASED AUTOMATIC DATA ACQUISITION AND CONTROL SYSTEM WITH CABLES TO INTERFACE TEST SET AND AIRCRAFT TRANSDUCERS PROVIDED; LENGTH OF CABLES SHALL BE APPROXIMATELY 50 FEET |
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