Aerospace Performance Parts is pleased to offer immediate purchasing options for The Boeing Company part number 145HS287, which you have taken interest in. This Transducer Dual item is listed alongside the NSN 1650-01-119-7368 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 145HS287 or any other FSC 1650 Aircraft Hydraulic Vacuum and De icing System Components components we carry from The Boeing Company under CAGE Code 77272, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 1650-01-119-7368 part number 145HS287 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1650-01-119-7368 Item PartTypeName: TRANSDUCER,DUAL | 1650 | 011197368 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
220K140-2 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | TRANSDUCER ASSEMBLY,DUAL,LINEAR,ILCA |
FEAT | SPECIAL FEATURES | CRITICAL APPLICATION ITEM |
FTLD | FUNCTIONAL DESCRIPTION | MOISTURE: THE DESIGN CONFIGURATION SHALL BE SUCH THAT MOISTURE CANNOT COLLECT IN DEPRESSIONS OR IRREGULAR SURFACES TO THE EXTENT OF CAUSING MALFUNCTION FROM CORROSION,FREEZING OR OTHER INJURIOUS EFFECTS; VIBRATION AND SHOCK: TRANSDUCER ASS |
SPCL | SPECIAL TEST FEATURES | MISSION RELIABILITY: EACH TRANSDUCER SHALL HAVE NO LESS THAN .99999 PROBABILITY OF COMPLETING A 1 HOUR MISSION WITHOUT INCURRING A MISSION FAILURE |
SUPP | SUPPLEMENTARY FEATURES | CLEANING OF SAND AND DUST: AIRBORNE SAND AND DUST PARTICLES ENCOUNTERED IN DESERT OPERATIONS,PER METHOD 510,PROCEDURE I,OF MIL-STD-810B; SALT SPRAY: ATMOSPHERE CONTAINING SALT LADEN MOISTURE,PER METHOD 509,PROCEDURE I OF MIL-STD-810B |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | THE TRANSDUCER ASSEMBLY SHALL BE CAPABLE OF CONTINUOUS OPERATION THROUGHOUT THE AMBIENT TEMPERATURE RANGE OF-50 DEGREES FAHRENHEIT TO 275 DEGREES FAHRENHEIT; UNIT SHALL BE CAPABLE OF OPERATION FROM SEA LEVEL TO 50,000 FEET ALTITUDE COMBI |
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