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Phone No.: +1-714-705-4780 Email: sales@justpartsunlimited.com
Phone No.: +1-714-705-4780 Email: sales@justpartsunlimited.com
| Part No. : 1559M63G02-129 | Alternate P/N : 1559M63G02129 | Manufacturer : General Electric Co |
| CAGE Code : 07482 | Item Name : Rotor Compressor Aircraft Gas Tu | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NSN : 2840-01-438-8399 |
You can send a request for quote for p/n 1559M63G02-129 to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by General Electric Co (CAGE Code 07482). The description of it is Rotor Compressor Aircraft Gas Tu. The national stock number associated with this part is NSN 2840014388399. This part belongs to FSC Gas Turbines and Jet Engines Aircraft Prime Moving and Components part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with 1559M63G02-129 part requirements.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-438-8399 Item Description: Rotor Compressor Aircraft Gas Tu | 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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