# CFM International CFM56-5B5 series - Type: Engine model (FAA registry) - Registry code: 13015 - Manufacturer (registry): CFM INTL - Model: CFM56-5B5 - Engine type: Turbo-fan - Power: 22,000 lb thrust - Installed in: 2 registered aircraft - Page: https://openairdocs.org/engine/cfm-international-cfm56-5b5-series The registry names only the engine series, so ADs for every model in the series are matched. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023 - [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021 - [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017 - [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016 - [AD 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013 - [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012 - [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010 - [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 2010 - [AD 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009 - [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009 - [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007 - [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007 - [AD 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005 - [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002 - [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002 - [AD 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 2002 - [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001 - [AD 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000 - [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998 - [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997 Historical (superseded or no longer in force): - [AD 2021-10-09](https://openairdocs.org/ad/2021-10-09) (historical): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 82 more. Effective Jun 24, 2021 - [AD 2019-12-05](https://openairdocs.org/ad/2019-12-05) (historical): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 39 more. Effective Jul 5, 2019 - [AD 2009-01-01](https://openairdocs.org/ad/2009-01-01) (historical): Exhaust gas temperature (EGT) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 22 more. Effective Dec 31, 2008 - [AD 2000-12-01](https://openairdocs.org/ad/2000-12-01) (historical): Critical Life-Limited Parts · CFM International CFM56-2, CFM56-2A, CFM56-2B and 54 more. Effective Dec 11, 2000 ## Information bulletins (advisory) (3) - [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014 - [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012 - [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011 ## Registered aircraft (2) - [N311NV](https://openairdocs.org/aircraft/N311NV): [Sunrise Asset Management LLC](https://openairdocs.org/faa-owner/SUNRISE%20ASSET%20MANAGEMENT%20LLC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 2006, S/N 2702 - [N330NV](https://openairdocs.org/aircraft/N330NV): [Sunrise Asset Management LLC](https://openairdocs.org/faa-owner/SUNRISE%20ASSET%20MANAGEMENT%20LLC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 2006, S/N 2786 ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20160428012329I](https://openairdocs.org/incident/20160428012329I), Apr 28, 2016: Airbus A319-111 (N311NV), Mesa, AZ, Minor damage. Phoenix, AZ (iwa): AAY175, A319, initiated a go-around runway 30L due to high crosswinds. During the go-alert, the #2 engine sparked flames and stopped. Alert… ## Service difficulty reports (246, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000429](https://openairdocs.org/sdr/2026FA0000429), May 26, 2026: TURBINE. DEFECTIVE. THE ENGINE ABY ESN 577716 WAS SLOTTED IN SAESM THE 17 APRIL 2026. DURING THE MM03 LEVEL INSPECTION OF THE LPT CASE, A DEFECT WAS IDENTIFIED ON 28TH MAY 2026. FO - [SDR WX0A2024080532144](https://openairdocs.org/sdr/WX0A2024080532144), Aug 3, 2024: ENGINE. OVERTEMP. (AIRCRAFT NOT GROUNDED) ON CLIMB OUT ENG 2 HIGH OIL TEMP ADV. RAN QRH ECAM ADV LED TO ECAM ENG 2 OIL TEMP HIGH ENG 2 SHUTDOWN / REMOVED AND REPLACED #2 ENG IDG - [SDR WX0A2021071473765](https://openairdocs.org/sdr/WX0A2021071473765), Jul 12, 2021: ENGINE. POWER LOSS. (EMERGENCY DECLARED) #2 ENGINE ROLLED BACK DURING DECENT. ENGINE #2 WINDMILLED FOR ABOUT :17 MIN / AIRCRAFT IS CURRENTLY AOS AT TOL. TROUBLESHOOTING IN PROGRESS - [SDR QEMY29012021](https://openairdocs.org/sdr/QEMY29012021), Jan 22, 2021: FRAME. DAMAGED. ON INCOMING INSPECTION AT GE AVIATION WALES EASYJET ESN 699785, THE LPT FRAME WAS FOUND DAMAGED. THE LPT FRAME HAS BEEN REMOVED FROM SERVICE. DAMAGE CONSISTENT - [SDR WX0A2019062173399](https://openairdocs.org/sdr/WX0A2019062173399), Jun 21, 2019: GASKET. FAILED. EMERGENCY DECLARED, NR 1 ENGINE FAILED. R & R FUEL NOZZLE FILTER GASKET. - [SDR A8ZR20170414001](https://openairdocs.org/sdr/A8ZR20170414001), Apr 4, 2017: BEARING. MIGRATED. DURING PRE-FLIGHT CHECK, THE RUDDER TRAVEL DID NOT TOUCH FULL CONTROL BOX ON LOWER ECAM PAGE AND THE LAST 1/10 OF PEDAL TRAVEL WAS HARD. TROUBLESHOOTING AND INS - [SDR AALA201701229008](https://openairdocs.org/sdr/AALA201701229008), Jan 21, 2017: ENGINE. STALLED. AIRCRAFT WAS GROUNDED. NEAR TOP OF DESCENT, MOMENTARY ONE TIME NR 1 ENGINE STALL, CORRECTED BEFORE ENGINE INDICATIONS CHANGED, ECAM CAME ON VERY BRIEFLY. MAINTE - [SDR WX0A2016042973145](https://openairdocs.org/sdr/WX0A2016042973145), Apr 28, 2016: ENGINE. FAILED. NUMBER 2 ENG FAILED DURING GO AROUND. DISCHARGED NR 1 FIRE BOTTLE. R&R NR 2 ENGINE PER T/C 71-400-001. ALL OPS AND LEAK CHECKS GOOD. - [SDR F3LA2014081201050](https://openairdocs.org/sdr/F3LA2014081201050), Aug 8, 2014: VALVE. CLOSED. IN CRUISE AT 31000 FT UNABLE TO MAINTAIN CABIN PRESS. CABIN ALTITUDE ROSE TO 10,200. R & R NR 2 ENG PRV IAW AMM 36-11-52-PB 401. OPERATIONS & LEAK CHECKED VLV & - [SDR CA111103009](https://openairdocs.org/sdr/CA111103009), Oct 29, 2011: BRAKE. FAILED. (CAN) ON APPROACH, FLIGHT CREW REPORTED A FLIGHT CONTROL PROBLEM WHICH REQUIRED A GO-AROUND. AS A PRECAUTION, THE CREW DECLARED AN EMERGENCY WITH ATC (PAN-PAN) - [SDR F3LA200800505](https://openairdocs.org/sdr/F3LA200800505), Jul 20, 2008: SIGN. BROKEN. DURING C-CHECK, INSP NOTED R1 DOOR FWD LOWER EXIT LIGHT IS BROKEN. MAINT REMOVED AND REPLACED R1 DOOR FWD LOWER EXIT LIGHT IAW AMM 33-51-13-400-001. UPON COMPLE - [SDR F3LA200800501](https://openairdocs.org/sdr/F3LA200800501), Jul 19, 2008: SILL. DAMAGED. DURING C-CHECK, INSP NOTED THE R2 DOOR SILL PLATE REQUIRED REPLACEMENT DUE TO MISDRILLED HOLE. MAINT REMOVED AND REPLACED R2 DOOR SILL PLATE IAW A319 SRM 51-42- - [SDR F3LA200800500](https://openairdocs.org/sdr/F3LA200800500), Jul 19, 2008: SHEAR PLATE. CORRODED. DURING C-CHECK, INSP NOTED THE RT LATERAL SHEAR PLATE AT Y-1162, FROM FRAME 69 TO FRAME 70, HAD CORROSION AND FOUR SHEARED FASTENERS AT THE FWD EDGE. MAINT REMO - [SDR F3LA200800499](https://openairdocs.org/sdr/F3LA200800499), Jul 18, 2008: FLOOR PANEL. BROKEN. DURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION - [SDR F3LA200800490](https://openairdocs.org/sdr/F3LA200800490), Jul 16, 2008: SKIN. DENTED. DURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK POSITION. MAINT REPAIRED DAMAGED AREA IAW - [SDR F3LA200800489](https://openairdocs.org/sdr/F3LA200800489), Jul 16, 2008: FITTING. CORRODED. DURING C-CHECK INSP NOTED THE R1 DOOR GIRT BAR FITTING IB MOUNT HOLES ON SILL PLATE HAD CORROSION. MAINT BLENDED CORROSION IAW SRM 51-74-00. MAINT REPAIRED AREA - [SDR F3LA200800486](https://openairdocs.org/sdr/F3LA200800486), Jul 16, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT RT SIDE PROFILE HAD CORROSION AT FRAME 59 ON RT SIDE IAW A319 SRM 51-72-11 AND 51-44-11. UPON COMPLETION OF - [SDR F3LA200800491](https://openairdocs.org/sdr/F3LA200800491), Jul 15, 2008: FITTING. CRACKED. DURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAINT REPAIRED NR 1 ENGINE PYLON PANEL NR 4 - [SDR F3LA200800488](https://openairdocs.org/sdr/F3LA200800488), Jul 15, 2008: DOOR FRAME. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON TOP LEG OF FRAME C55A AT FWD EDGE OF C2 DOOR. MAINT REPAIRED DAMAGE ON TOP LEG OF FRAME C55A IAW EA NR A9-53R-30442. UPON - [SDR F3LA200800483](https://openairdocs.org/sdr/F3LA200800483), Jul 15, 2008: PROFILE. GOUGED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C63 IS GOUGED AND HAS A RIVET PULLING THROUGH. MAINT REMOVED AND REPLACED PROFILE AT FRAME - [SDR F3LA200800484](https://openairdocs.org/sdr/F3LA200800484), Jul 15, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C59 HAD CORROSION AT BOTH ENDS OF THE PROFILE. MAINT REMOVED AND REPLACED THE PROFILE IAW S - [SDR F3LA200800485](https://openairdocs.org/sdr/F3LA200800485), Jul 15, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT SMALL PROFILE RT SIDE JUST INSIDE DOOR FWD OF FRAME C56 HAS CORROSION. MAINT REMOVED SMALL PROFILE, FABRICAT - [SDR F3LA200800482](https://openairdocs.org/sdr/F3LA200800482), Jul 15, 2008: BATTERY BOX. WORN. DURING C-CHECK INSP, NOTED AFT BATTERY TRAY OB FWD AND AFT MOUNTS HAVE WEAR. MAINT REMOVED AND REPLACED AFT BATTERY TRAY, OB FWD AND AFT MOUNTS IAW SRM 51-72-11 - [SDR F3LA200800469](https://openairdocs.org/sdr/F3LA200800469), Jul 14, 2008: FLOORBEAM. CORRODED. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM HAS CORROSION BETWEEN FRAME C57 AND FRAME C58. MAINT REMOVED AND REPLACED CORRODED FLOORBEAM AT - [SDR F3LA200800470](https://openairdocs.org/sdr/F3LA200800470), Jul 14, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON AFT MOST PROFILE AT FWD CARGO COMPARTMENT AFT OF FRAME C30. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51- - [SDR F3LA200800465](https://openairdocs.org/sdr/F3LA200800465), Jul 14, 2008: FRAME. CORRODED. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT INSIDE OF C2 DOOR SHORT ANGLE PIECE AT FRAME C59 HAS CORROSION. MAINT REMOVED SHORT ANGLE PIECE APPLIED PROTECTI - [SDR F3LA200800449](https://openairdocs.org/sdr/F3LA200800449), Jul 13, 2008: DEU. INOPERATIVE. DURING FLIGHT MANY CABIN LIGHTS WERE COMING ON AND OFF ON AC RT. THE F/A NOTICED A BURNING SMELL OVER ROWS 16,17 AND 18 ON AC RT. MAINT FOUND DEU-A 200RH12 INOP - [SDR F3LA200800480](https://openairdocs.org/sdr/F3LA200800480), Jul 11, 2008: SEAT TRACK. CORRODED. DURING C-CHECK INSP NOTED THE RT LONGERON BEAM Y-765 AT FRAME 66 HAD CORROSION AROUND THE HOLE. MAINT REMOVED AND REPLACED CORRODED LONGERON BEAM AT Y-765 FRAME - [SDR F3LA200800478](https://openairdocs.org/sdr/F3LA200800478), Jul 11, 2008: PROFILE. CORRODED. DURING C-CHECK INSP, NOTED CORROSION ON AFT CARGO COMPARTMENT LT PROFILE, FWD AREA OF AFT CARGO, AT FRAME C47 TO FRAME C51. MAINT REMOVED AND REPLACED PROFILE A - [SDR F3LA200800477](https://openairdocs.org/sdr/F3LA200800477), Jul 11, 2008: FITTING. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE AT FRAME C29 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED FITTING, REINSTALLED PLATE AND - [SDR F3LA200800476](https://openairdocs.org/sdr/F3LA200800476), Jul 11, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON PROFILE PARALLEL WITH FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED CORRODED PROFILE ON FRAME C28 IN FWD CA - [SDR F3LA200800475](https://openairdocs.org/sdr/F3LA200800475), Jul 11, 2008: GIRT BAR. STICKING. DURING C-CHECK INSP NOTED R1 GIRT BAR FITTING FOR DOOR SLIDE STOP LEVER STICKS, DOES NOT SNAP BACK WHEN PRESSED DOWN AND RELEASED. MAINT REMOVED AND REPLACED WI - [SDR F3LA200800474](https://openairdocs.org/sdr/F3LA200800474), Jul 11, 2008: CARGO TRACK. CORRODED. DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE UNDER FRAME C25 FWD CARGO PIT. MAINT REMOVED PLATE AND BLENDED CORROSION, MORE THAN 50 PERCENT - [SDR F3LA200800473](https://openairdocs.org/sdr/F3LA200800473), Jul 11, 2008: LONGERON. CORRODED. DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1162 FROM FRAME 68 TO FRAME 69 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOORBEAM LONGERON Y-1162 FROM - [SDR F3LA200800472](https://openairdocs.org/sdr/F3LA200800472), Jul 11, 2008: FLOOR SUPPORT. CORRODED. DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1292 FROM FRAME 66 TO FRAME 68 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOOR SUPPORT LONGERON Y-1292 - [SDR F3LA200800471](https://openairdocs.org/sdr/F3LA200800471), Jul 11, 2008: PROFILE. CORRODED. DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON PROFILE LT SIDE AFT OF FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED OLD PROFILE AT FRAME C28 ON LT SIDE, - [SDR F3LA200800487](https://openairdocs.org/sdr/F3LA200800487), Jul 11, 2008: SKIN. CHAFED. DURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAIRED IAW SRM 51-75-12. UPON COMPLETION OF - [SDR F3LA200800481](https://openairdocs.org/sdr/F3LA200800481), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP, NOTED FLOOR PANEL 261PF HAD COMPOSITE DAMAGE. MAINT REMOVED AND REPLACED FLOOR PANEL 261PF WITH NEW PANEL, REFERENCED ON EAC NON ROUTINE IT - [SDR F3LA200800464](https://openairdocs.org/sdr/F3LA200800464), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOU - [SDR F3LA200800451](https://openairdocs.org/sdr/F3LA200800451), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR - [SDR F3LA200800452](https://openairdocs.org/sdr/F3LA200800452), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPA - [SDR F3LA200800453](https://openairdocs.org/sdr/F3LA200800453), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT W - [SDR F3LA200800454](https://openairdocs.org/sdr/F3LA200800454), Jul 11, 2008: PANEL. DAMAGED. DURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPA - [SDR F3LA200800455](https://openairdocs.org/sdr/F3LA200800455), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAI - [SDR F3LA200800456](https://openairdocs.org/sdr/F3LA200800456), Jul 11, 2008: PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAI - [SDR F3LA200800457](https://openairdocs.org/sdr/F3LA200800457), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAI - [SDR F3LA200800458](https://openairdocs.org/sdr/F3LA200800458), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAI - [SDR F3LA200800459](https://openairdocs.org/sdr/F3LA200800459), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAI - [SDR F3LA200800460](https://openairdocs.org/sdr/F3LA200800460), Jul 11, 2008: FLOOR PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED A - [SDR F3LA200800461](https://openairdocs.org/sdr/F3LA200800461), Jul 11, 2008: PANEL. DAMAGED. DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPE All 246: https://openairdocs.org/engine/cfm-international-cfm56-5b5-series/reports.md ## PMA parts (OpenAirDocs) (over 1,000, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first. - [2564M19G01SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183308050320261019152741.0001): Seal - Stg 2 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M19G01 · Oct 15, 2026 - [2564M19G01SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183308050320261019152741.0001): Seal - Stg 2 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M19G01 · Oct 15, 2026 - [2564M15G02SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182481008320261019152741.0001): Seal - Retainer Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M15G02 · Oct 15, 2026 - [2564M15G02SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182481008320261019152741.0001): Seal - Retainer Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M15G02 · Oct 15, 2026 - [2564M19G02SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171586083020261019152741.0001): Seal - Stg 2 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M19G02 · Oct 15, 2026 - [2564M19G02SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171586083020261019152741.0001): Seal - Stg 2 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M19G02 · Oct 15, 2026 - [2564M15G01SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139341463420261019152740.0001): Seal - Stg 3 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M15G01 · Oct 15, 2026 - [2564M15G01SD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139341463420261019152740.0001): Seal - Stg 3 Cprsr Sttr. Seal Dynamics Inc. A HEICO Aerospace Company · PMA PQ1715CE · Replaces 2564M15G01 · Oct 15, 2026 - [KT9974M10P207](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156771068620261019153205.0001): Ring, Piston. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9974M10P207 · Oct 7, 2026 - [KT9974M10P207](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156771068620261019153205.0001): Ring, Piston. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 9974M10P207 · Oct 7, 2026 - [337-141-601-0KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157822411420261008134816.0001): Bolt. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 337-141-601-0 · Sep 29, 2026 - [337-141-601-0KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157822411420261008134816.0001): Bolt. Turbine Kinetics Inc., A HEICO Aerospace Company · PMA PQ0816NE · Replaces 337-141-601-0 · Sep 29, 2026 - [649-788-399-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103937182820260909145920.0001): Packing-Preformed O-Ring. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 649-788-399-0 · Aug 24, 2026 - [649-788-399-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103937182820260909145920.0001): Packing-Preformed O-Ring. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 649-788-399-0 · Aug 24, 2026 - [2002M87P02JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199317637820260806140031.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P02 · Jul 30, 2026 - [2002M87P02JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199317637820260806140031.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P02 · Jul 30, 2026 - [2002M87P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133871277820260806140030.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P01 · Jul 30, 2026 - [2002M87P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133871277820260806140030.0001): Gasket - Igniter Adapter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2002M87P01 · Jul 30, 2026 - [3051-1051KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121122166320260805155543.0001): Seal, Trapezoidal. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 3051-1051 · Jul 21, 2026 - [3051-1051KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121122166320260805155543.0001): Seal, Trapezoidal. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 3051-1051 · Jul 21, 2026 - [3177421JP-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144029116620260805181453.0001): Setscrew. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 3177421-1 · Jul 16, 2026 - [3177421JP-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144029116620260805181453.0001): Setscrew. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 3177421-1 · Jul 16, 2026 - [301-547-905-0JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163539788920260806140647.0001): Nut. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 301-547-905-0 · Jul 14, 2026 - [301-547-905-0JP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163539788920260806140647.0001): Nut. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces 301-547-905-0 · Jul 14, 2026 - [337-079-905-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162121163220260706131723.0001): Plug. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 337-079-905-0 · Jun 25, 2026 - [337-079-905-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162121163220260706131723.0001): Plug. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 337-079-905-0 · Jun 25, 2026 - [301-808-602-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141457374720260706131723.0001): Cover-Filter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 301-808-602-0 · Jun 25, 2026 - [301-808-602-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141457374720260706131723.0001): Cover-Filter. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 301-808-602-0 · Jun 25, 2026 - [1211342-240-014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101824618120260706131723.0001): Packing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1211342-240-014 · Jun 25, 2026 - [1211342-240-014JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101824618120260706131723.0001): Packing. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1211342-240-014 · Jun 25, 2026 - [3236051-1HA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186586940920260909154537.0001): BOOT, FLEXIBLE. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces 3236051-1 · Jun 24, 2026 - [3236051-1HA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186586940920260909154537.0001): BOOT, FLEXIBLE. Hutchinson Aerospace & Industry Inc. · PMA PQ0524NM · Replaces 3236051-1 · Jun 24, 2026 - [1476M79P05JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107210147820260616140659.0001): Damper - Forward Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1476M79P05 · May 29, 2026 - [1476M79P05JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107210147820260616140659.0001): Damper - Forward Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 1476M79P05 · May 29, 2026 - [AAP-3504163-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180945408320260406133714.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3504163-1 · Apr 1, 2026 - [AAP-3504163-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180945408320260406133714.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3504163-1 · Apr 1, 2026 - [336-031-701-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144123523920260324201242.0001): Weight-Balance 2.9G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-701-0 · Feb 25, 2026 - [336-031-701-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144123523920260324201242.0001): Weight-Balance 2.9G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-701-0 · Feb 25, 2026 - [336-031-710-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129285223420260324201243.0001): Weight-Balance 6.5G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-710-0 · Feb 25, 2026 - [336-031-710-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129285223420260324201243.0001): Weight-Balance 6.5G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-710-0 · Feb 25, 2026 - [336-031-708-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112259513820260324201242.0001): Weight-Balance 5.7G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-708-0 · Feb 25, 2026 - [336-031-708-0JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112259513820260324201242.0001): Weight-Balance 5.7G. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 336-031-708-0 · Feb 25, 2026 - [2949M03P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165472228620260225205426.0001): Blade Lock-Compressor Stg 8,9. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2949M03P01 · Feb 4, 2026 - [2949M03P01JA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165472228620260225205426.0001): Blade Lock-Compressor Stg 8,9. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 2949M03P01 · Feb 4, 2026 - [E140375-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181608826420251229153151.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-3 · Dec 17, 2025 - [E140375-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181608826420251229153151.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-3 · Dec 17, 2025 - [E140375-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149149609920251229153152.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-4 · Dec 17, 2025 - [E140375-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149149609920251229153152.0001): Flexible Shaft Assembly. BW Elliott Manufacturing Co LLC · PMA PQ2009NE · Replaces 121762-4 · Dec 17, 2025 - [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199148521820251125143636.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025 - [AAP-3502129-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199148521820251125143636.0001): Bearing. Approved Air Parts, LLC · PMA PQ4173NE · Replaces Honeywell 3502129-1 · Nov 6, 2025 All of them: https://openairdocs.org/engine/cfm-international-cfm56-5b5-series/pma.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.