Belac LLC (Subsidiary Of Chromalloy Gas Turbine LLC)
PMA PQ1667CE · 9 approved parts replacing 9 OEM numbers · General Electric, International Aero Engines Ag (Iae), General Electric Company Ge Aerospace, Pratt & Whitney, Cfm International S.A., Pratt & Whitney Division
| PMA part | Replaces | Name | Make / model | Status | On PartsAndPlanes |
|---|---|---|---|---|---|
| BLC1538M90P12 | General Electric P/N 1538M90P12 | First Stage High Pressure Turbine Blade | General Electric CF6-80C2A1, -80C2A2, -80C2A3, -80C2A5, -80C2A8, -80C2B1, -80C2B2, -80C2B4, -80C2B6, -80C2B1F, -80C2B2F -80C2B4F, -80C2B5F, -80C2B6F, -80C2B6FA, -80C2B7F, -80C2A5F, and -80C2D1F Engines | Current, Dec 2008 | — |
| BLC1538M90P12(-X) | 1538M90P12 | First Stage High Pressure Turbine Blade | General Electric CF6-80C2A1, -80C2A2, -80C2A3, -80C2A5, -80C2A8, -80C2B1, -80C2B2, -80C2B4, -80C2B6, -80C2B1F, -80C2B2F, -80C2B4F, -80C2B5F, -80C2B6F, -80C2B8F, -80C2B6FA, -80C2B7F, -80C2A5F, -80C2D1F | Current, Mar 2018 | — |
| BLC1538M90P12(-X) | PM1538M90P12 | First Stage High Pressure Turbine Blade | General Electric Company Ge Aerospace CF6-80C2A1 | CF6-80C2A2 | CF6-80C2A3 | CF6-80C2A5 | CF6-80C2A5F | CF6-80C2A8 | CF6-80C2B1 | CF6-80C2B1F | CF6-80C2B2 | CF6-80C2B2F | CF6-80C2B4 | CF6-80C2B4F | CF6-80C2B5F | CF6-80C2B6 | CF6-80C2B6F | CF6-80C2B6FA | CF6-80C2B7F | CF6-80C2B8F | CF6-80C2D1F | Current, May 2017 | — |
| BLC1881M52G05 | General Electric P/N 1881M52G05 | Second Stage High Pressure Turbine Blade | General Electric CF6-80C2A1, -80C2A2, -80C2A3, -80C2A5, -80C2A8, -80C2B1, -80C2B2, -80C2B4, -80C2B6, -80C2B1F, -80C2B2F -80C2B4F, -80C2B5F, -80C2B6F, -80C2B6FA, -80C2B7F, -80C2A5F, and -80C2D1F Engines | Current, Dec 2008 | — |
| BLC1881M52G05(-X) | PM1881M52G05 | Second Stage High Pressure Turbine Blade | General Electric Company Ge Aerospace CF6-80C2A1 | CF6-80C2A2 | CF6-80C2A3 | CF6-80C2A5 | CF6-80C2A5F | CF6-80C2A8 | CF6-80C2B1 | CF6-80C2B1F | CF6-80C2B2 | CF6-80C2B2F | CF6-80C2B4 | CF6-80C2B4F | CF6-80C2B5F | CF6-80C2B6 | CF6-80C2B6F | CF6-80C2B6FA | CF6-80C2B7F | Current, May 2017 | — |
| BLC1881M52G05(-X) | 1881M52G05 | Second Stage High Pressure Turbine Blade | General Electric CF6-80C2A1, -80C2A2, -80C2A3, -80C2A5, -80C2A8, -80C2B1, -80C2B2, -80C2B4, -80C2B6, -80C2B1F, -80C2B2F, -80C2B4F, -80C2B5F, -80C2B6F, -80C2B6FA, -80C2B7F, -80C2A5F, -80C2D1F | Current, Mar 2018 | — |
| BLC2100M96P05 | 2100M96P05 | High Pressure Turbine, Blade, Stage 1 | Cfm International S.A. CFM56-5B1/2P | CFM56-5B1/3 | CFM56-5B1/P | CFM56-5B2/2P | CFM56-5B2/3 | CFM56-5B2/P | CFM56-5B3/2P | CFM56-5B3/2P1 | CFM56-5B3/3 | CFM56-5B3/3B1 | CFM56-5B3/P | CFM56-5B3/P1 | CFM56-5B4/2P | CFM56-5B4/2P1 | CFM56-5B4/3 | CFM56-5B4/3B1 | CFM56-5B4/P | CFM56-5B4/P1 | CFM56-5B5/3 | CFM56-5B5/P | CFM56-5B6/2P | CFM56-5B6/3 | CFM56-5B6/P | CFM56-5B7/3 | CFM56-5B7/P | CFM56-5B8/3 | CFM56-5B8/P | CFM56-5B9/2P | CFM56-5B9/3 | CFM56-5B9/P | CFM56-7B20 | CFM56-7B20/2 | CFM56-7B20/3 | CFM56-7B22 | CFM56-7B22/2 | CFM56-7B22/3 | CFM56-7B22/3B1 | CFM56-7B22/B1 | CFM56-7B24 | CFM56-7B24/2 | CFM56-7B24/3 | CFM56-7B24/3B1 | CFM56-7B24/B1 | CFM56-7B26 | CFM56-7B26/2 | CFM56-7B26/3 | CFM56-7B26/3B1 | CFM56-7B26/3B2 | CFM56-7B26/3F | CFM56-7B26/B1 | CFM56-7B26/B2 | CFM56-7B27 | CFM56-7B27/2 | CFM56-7B27/3 | CFM56-7B27/3B1 | CFM56-7B27/3B1F | CFM56-7B27/3B3 | CFM56-7B27/3F | CFM56-7B27/B1 | CFM56-7B27A/3 | CFM56-7B27B3 | CFM56-B26/3B2F | Current, Oct 2025 | — |
| BLC2A4822 | 2A4822 | High Pressure Turbine, Blade, Stage 2 | International Aero Engines Ag (Iae) V2522-A5 | V2524-A5 | V2527-A5 | V2527E-A5 | V2527M-A5 | V2530-A5 | V2533-A5 | Current, Dec 2024 | — |
| BLC2A4822 | 2A4822 | High Pressure Turbine, Blade, Stage 2 | International Aero Engines Ag (Iae) V2522-A5 | V2524-A5 | V2527-A5 | V2527E-A5 | V2530-A5 | V2533-A5 | Current, Sep 2024 | — |
| BLC2A9721 | 2A9721 | High Pressure Turbine, Blade, Stage 1 | International Aero Engines Ag (Iae) V2522-A5 | V2524-A5 | V2527-A5 | V2527E-A5 | V2527M-A5 | V2530-A5 | V2533-A5 | Current, Aug 2026 | — |
| BLC55L201 | Pratt & Whitney 55L201 | High Pressure Turbine Blade, Stage 1 | Pratt & Whitney PW4052 | PW4056 | PW4060 | PW4060C | PW4062 | PW4152 | PW4156A | PW4158 | PW4164 | PW4168 | PW4168A | PW4460 | PW4462 | Current, Jul 2009 | — |
| BLC56L601 | 56L601 | Hpt Stage 1 Turbine Blade | Pratt & Whitney Division PW4052 | PW4056 | PW4060 | PW4062 | PW4062A | PW4152 | PW4156A | PW4158 | PW4164 | PW4168 | PW4168A | PW4460 | PW4462 | Current, Oct 2020 | — |
| BLC56L601 | 56L601 | Hpt Stage 1 Turbine Blade | Pratt & Whitney PW4052(-3) | PW4056(-3) | PW4060(-3) | PW4062(-3) | PW4062A(-3) | PW4152(-3) | PW4156A(-3) | PW4158(-3) PW4460(-3) | PW4164 | PW4168 | PW4168A | PW4170 PW4164-1D PW4168-1D PW4168A-1D | PW4462(-3) | Current, Feb 2021 | — |
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.