NSN Part Number 1559M63G02-110 with NSN 2840014388400 by General Electric Company - Get a Quote

Part Number: 1559M63G02-110

Alternate P/N: 1559M63G02110

Manufacturer: General Electric Company

NSN: 2840-01-438-8400

NIIN: 014388400

Item Name : Rotor Compressor Aircraft Gas Tu

CAGE Code: 07482

FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components

FSG: 28 Engines Turbines and Components

Country: USA

NCB Code: 01

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Buy National Stock Numbers should be your go-to choice for part sourcing, as we are one of the only major distributors that operates with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, in addition to adhering to a strict No China Sourcing policy. For your ease of search, our catalogs feature items with the CAGE Code 07482 and FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Get started with a competitive quote for NSN 2840-01-438-8400, a component manufactured by General Electric Company, and see how we can serve as your strategic sourcing solution. For questions about our other offered services, contact us via phone or email!

NSN Information for Part Number 1559M63G02-110 with NSN 2840-01-438-8400, 2840014388400

NSN	FSC	NIIN	CLS	Hazmat	DEMIL	Cancelled NSN
2840-01-438-8400 Item PartTypeName: ROTOR,COMPRESSOR,AIRCRAFT GAS TU	2840	014388400	0	N
	CIIC	HCC	ESD	PMIC	Criticality	ENAC
	I			A	0
Part Number	ISC	RNVC	RNCC	HCC	MSDS	SADC
1559M63G02-110	5	2	3

Characteristics Data of NSN 2840-01-438-8400, 2840014388400

MRC	Criteria	Characteristic
ABMZ	Diameter	17.300 INCHES NOMINAL
CZCJ	Stage Number	1
FEAT	Special Features	T.O. 2J-F110-14, FIG 67, IND 5 UNDER P/N 1559M63G02; INCLUDES STAGE 2; ALSO CONSISTS NO. 1 DISK AND NO. 2 DISK AND FORWARD SHAFT THAT MAKES A 1 PIECE CONSTRUCTION THAT HOLDS BOTH STGS; WEIGHS 40.3 LBS; BASIC P/N CAN BE USED ON ALL ENGINE TYPES, BUT ONCE USED ON THE F110, IT CAN ONLY BE USED ON AN F110 ENGINE; REIDENTIFICATION WILL CONSIST OF ADDING THE ENGINE TYPE AS A DASH NUMBER FOLLOWING THE P/N
CXCY	Part Name Assigned By Controlling Agency	ORIGINAL NAME SPOOL,COMPRESSOR ROTOR
MATT	Material	TITANIUM ALLOY OVERALL
AGAV	End Item Identification	F110-GE-100 AIRCRAFT GAS TURBINE ENGINE
CZBJ	Engine Section Location	HIGH PRESSURE COMPRESSOR
ABHP	Overall Length	6.143 INCHES MINIMUM AND 6.163 INCHES MAXIMUM
APGF	Design Type	AXIAL COMPRESSOR
MRC	Decoded Requirement	Clear Text Reply
MDCL	Material Document And Classification	TI-17 MFR REF SINGLE MATERIAL RESPONSE OVERALL
CRTL	Criticality Code Justification	FEAT AND ABHP AND ABMZ AND CZBJ