Chromalloy Georgia
PMA PQ1574CE · 9 approved parts replacing 8 OEM numbers · Pratt & Whitney, Iae
| PMA part | Replaces | Name | Make / model | Status | On PartsAndPlanes | DLA paid (OEM no.) |
|---|---|---|---|---|---|---|
| CFL 808636 | Pratt & Whitney P/N 808636 | Case, Turbine Rear | Pratt & Whitney JT8D-217C, JT8D-219 | Current, Feb 2009 | — | — |
| CFL 808636-001 | Pratt & Whitney P/N 808636-001 | Case, Turbine Rear | Pratt & Whitney JT8D-217C, JT8D-219 | Current, Feb 2009 | — | — |
| CFL 808636-001-AA1479 | Pratt & Whitney P/N 808636-001 | Case, Turbine Rear | Pratt & Whitney JT8D-217A, JT8D-217C, JT8D-219 | Current, Feb 2009 | — | — |
| CFL 815399-001 | Pratt & Whitney P/N 815399-001 | Case, Turbine Rear | Pratt & Whitney JT8D-217C, JT8D-219 | Current, Feb 2009 | — | — |
| CFL 815399-01 | Pratt & Whitney P/N 815399-01 | Case, Turbine Rear | Pratt & Whitney JT8D-209, JT8D-217, JT83-217A, JT8D-217C, JT8D-219 | Current, Feb 2009 | — | — |
| CGA6A4211C01 | International Aero Engines AG (IAE) P/N 6A4211C01 | Hpc Stage 9 Blade | Iae V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5 | Current, Jul 2009 | — | — |
| CGA6A4211C02 | International Aero Engines AG (IAE) P/N 6A4211C02 | Hpc Stage 9 Blade | Iae V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5 | Current, Jul 2009 | — | — |
| CGA6A6545 | International Aero Engines AG (IAE) P/N 6A6545 | Hpc Stage 9 Blade | Iae V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5 | Current, Jul 2009 | — | — |
| CGA6A6566 | International Aero Engines AG (IAE) P/N 6A6566 | Hpc Stage 9 Blade | Iae V2522-A5, V2524-A5, V2527-A5 V2527E-A5, V2527M-A5, V2530-A5, V2525-D5, V2528-D5, V2533-A5 | Current, Jul 2009 | — | — |
Sell any of these? List it free and this table names you, as does the page of every OEM number it replaces.
Source: the FAA PMA database, refreshed weekly. A PMA part is approved for the specific eligibility on its FAA record; whether it may be installed on a particular aircraft, engine or component is the installer's determination.