Rotor Compressor Ai, with the part number 1559M63G02-129 manufactured by General Electric Inc, is in stock and available for immediate purchase. Please fill out the provided Instant RFQ form to start the purchasing process for 2840-01-438-8399 under NIIN 014388399 or any other listed NSN part. Once a staff member has received your request, they will reach out to you in 15 minutes or less to provide a competitive and personalized quote for comparison. We ask that you fill out the form in its entirety so that your quote for 1559M63G02-129 will best represent your individual needs.
Fasteners 360 is a leading distributor of NSN parts like 2840-01-438-8399. NSN stands for National Stock Number and is a 13-digit code used by all NATO nations as a standard to identify material items. Additionally, the manufacturer for this item can be found and indexed by CAGE code 07482. CAGE codes are five-character ID numbers used by the U.S. federal government assigned to suppliers. When you purchase through Fasteners 360, we guarantee that the items are of high quality. We operate as an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited and certified enterprise and only offer components from an approved vendor list of top global manufacturers such as General Electric Inc.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-438-8399 Item Description: Rotor Compressor Ai | 2840 | 014388399 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559m63g02-129 | 3 | 2 | 3 |
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-GE-129, IT CAN ONLY BE USED ON A F110-GE-129 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-129 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 |
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