145HS287-2 Manufactured by Curtiss Wright Controls Inc - Order Online

Part Number: 145HS287-2

Alternate P/N: 145HS2872

Manufacturer: curtiss wright controls inc

NSN: 1650-01-119-7368

Item Name : transducer dual

CAGE Code: 00288

FSC: 1650 Aircraft Hydraulic Vacuum and De-icing System Components

INC Code: 77777

Country: USA

NCB Code: 01

FSG: 16 Aircraft Components and Accessories

The NSN Part 145HS287-2 Transducer Dual is ready-to-ship today! Please request a quote by filling out the form. All fields are important. The NSN number for 145HS287-2 is 1650-01-119-7368. The manufacturer of this part is Curtiss Wright Controls Inc. A dedicated customer service executive will contact you within 15 minutes of receiving the RFQ.

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NSN Information for Part Number 145HS287-2 with NSN 1650-01-119-7368, 1650011197368

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

Characteristics Data of NSN 1650-01-119-7368, 1650011197368

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