Extex Ltd.
PMA PQ2108NM · 27 approved parts replacing 23 OEM numbers · Pratt & Whitney Canada, Bombardier, Inc., Rolls-Royce, Airbus, Lockheed
| PMA part | Replaces | Name | Make / model | Status | On PartsAndPlanes |
|---|---|---|---|---|---|
| 3500058-5R | 3500058-5 | Shaft Assembly | Lockheed Honeywell ATS100-242 series starter as installed in: 188A, 188C, Honeywell ATS100-277 series starter as installed in: 382, 382B, 382E, 382F, 382G, 382J | Current, Sep 2007 | — |
| E23055438-UC | 23055438-UC | Nozzle Assembly, Turbine, Second Stage | Rolls-Royce 250-C30, C30G, C30G/2, C30L, C30M, C30P, C30R, C30R/1, C30S, C30U | Current, Aug 2007 | — |
| E23064622 | 23064622 | Nozzle Assembly, Turbine, 2nd Stage | Rolls-Royce 250-C30R/3, C30U, C40B, C47B, C47M | Current, Aug 2007 | — |
| E3019348CL2 | 3019438CL2 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019348CL3 | 3019438CL3 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019348CL5 | 3019438CL5 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019348CL6 | 3019438CL6 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019348CL7 | 3019438CL7 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019348CL8 | 3019438CL8 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019438CL1 | 3019438CL1 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3019438CL1 | 3019438CL1 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Nov 2007 | — |
| E3019438CL3 | 3019438CL3 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3019438CL4 | 3019438CL4 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3019438CL6 | 3019438CL6 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3019438CL7 | 3019438CL7 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3019438CL8 | 3019438CL8 | Shroud Segment | Pratt & Whitney Canada PT6A-11, -11AG, -15AG, -21, -25, -25A, -27, -28, -110, -112, -121 | Current, Jul 2008 | — |
| E3023682 | 3023682 | Seal, Air, Turbine Interstage Stator | Pratt & Whitney Canada PT6A-38, 41, 42, 42A, 45A, 45B, 45R, 50, 60A, 60AG, 61, 64, 65AG, 65AR, 65B, 65R, 66, 66B, 67, 67A, 67AF, 67AG, 67B, 67D, 67R, 67T, 68 | Current, Jun 2008 | — |
| E3045741-01 | 3045741-01 | Blade, Turbine, Compressor | Pratt & Whitney Canada PT6A-11, 11AG, 15AG, 21, 25, 25A, 25C, 27, 28, 34, 34AG, 34B, 36, 38, 41, 110, 112, 114, 114A, 121 PT6D-114A | Current, Jun 2008 | — |
| E3111231-01 | 3111231-01 | Runner, Propeller Shaft Oil Seal | Pratt & Whitney Canada PT6A-65AR, 67, 67A, 67A, 67AF, 67AG, 67B, 67D, 67R, 67T | Current, Aug 2008 | — |
| E3114664-01 | 3114664-01 | Runner, Propeller Shaft Oil Seal | Pratt & Whitney Canada PT6A-45A, 45B, 45R, 60A, 60AG, 65B, 65R, 65AR, 65AG | Current, Aug 2008 | — |
| E3119920-01 | 3119920-01 | Fuel Nozzle Sheath | Pratt & Whitney Canada PT6A-38, 40,. 41, 41AG, 42, 42A, 45A, 45B, 45R, 50, 60A, 60AG, 61, 64, 65AG, 65AR, 65B, 65R, 66, 66A, 66B, 66D, 67, 67A, 67AF, 67AG, 67B, 67D, 67R | Current, Jun 2008 | — |
| E3616104-1 | 3616104-1 | Rotor Seal | Bombardier, Inc. Honeywell APU as installed on: GTCP36-150[RJ] CL-600-2B19 | Current, Oct 2007 | — |
| E3822493-1 | 3822493-1 | Rotor Seal | Airbus Honeywell APU as installed on: GTCP36-300[A] A319-111,-112,-113, -114,-131,-132, A320-111,-211,-212, -214,-231,-232,-233, A321-111,-112,-131, -211,-231 | Current, Oct 2007 | — |
| E3830156-2 | 3830156-2 | Secondary Fuel Manifold | Bombardier, Inc. Honeywell as installed on: GTCP36-150[RJ] CL-600-2B19) Embraer Empresa (Honeywell as installed on: GTCP36-150[A],-150[AA] EMB-120, -120RT, -120ER, -120FC) Dassault Aviation (Honeywell APU as installed on: GTCP36-150[F] Mystere-Falcon 900, 900EX) Cessna (Honeywell APU as installed on: GTCP36-150[CX] 750 (Citation X)) BAE Systems (Operations) Limited (Honeywell APU as installed on: GTCP36-150[M] BAe 146-200A BAe146-300a Avro 146-RJ70A, -RJ85A, -RJ100A) Saab Aircraft AB (Honeywell APU as installed on: GTCP 36-150[W] SAAB SF340A SAAB 340B) (DHC-8-100 series, -200 series, -300 series, -400 series) Cessna (650 (Citation III)) Raytheon (BAE 125 Series -800A -800B, -1000A, -1000B) Gulfstream Aerospace LP (Astra 1125) Dassault Aviation (Mystere-Falcon 20-C5, -D5, -E5, -F5) Fokker (Honeywell APU as installed on: GTCP36-150(R) F.28 Mark 0100 | Current, Oct 2007 | — |
| E3842347-1 | 3842347-1 | Outer Pilot Ring | Bombardier, Inc. Honeywell as installed on: GTCP36-150[RJ] CL-600-2B19 | Current, Oct 2007 | — |
| E3842348-1 | 3842348-1 | Inner Pilot Ring | Bombardier, Inc. Honeywell as installed on: GTCP36-150[RJ] CL-600-2B19 | Current, Oct 2007 | — |
| E3846206-3 | 3846206-3 | Airflow Deflector | Bombardier, Inc. Honeywell as installed on: GTCP36-150[RJ] CL-600-2B19) Embraer Empresa (Honeywell as installed on: GTCP36-150[A], -150[AA] EMB-120, -120RT, -120ER, -120FC) Dassault Aviation (Honeywell APU as installed on: GTCP36-150[F] Mystere-Falcon 900, 900EX) Cessna (Honeywell APU as installed on: GTCP36-150[CX] Pre GTE 1267 750 (Citation X)) BAE Systems (Operations) Limited (Honeywell APU as installed on: GTCP36-150[M] BAe 146-200A, -300A Avro 146-RJ70A, -RJ85A, -RJ100A) Saab Aircraft AB (Honeywell APU as installed on: GTCP36-150[W] SAAB SF340A SAAB 340B) (DHC-8-100 series, -200 series, -300 series, -400 series) Cessna (650 (Citation III) | Current, Oct 2007 | — |
| E3860404-1 | 3860404-1 | Gearshaft, Generator Idler | Bombardier, Inc. Honeywell as installed on: GTCP36-150[RJ] CL-600-2B19 | Current, Oct 2007 | — |
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.