# Service difficulty reports: CFM International LEAP-1A26

A list on [CFM International LEAP-1A26](https://openairdocs.org/engine/cfm-international-leap-1a26.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 63 reports

- [SDR 2026FA0000559](https://openairdocs.org/sdr/2026FA0000559.md): Potable Water · inoperative · Jun 30, 2026 · N965AV · Airbus A320251N · Potable Water System
  > NO PORTABLE WATER DURING FLIGHT. IAW TSM 38-12-00-810-814-A REV.77 PERFORMED OPERATIONAL TEST OF PORTABLE WATER DRAIN SYSTEM AS PER AMM 38-14-00-710-001-A REV.77 DATE 01-MAY 2026 AND ALL OK
- [SDR 2026FA0000475](https://openairdocs.org/sdr/2026FA0000475.md): Sensor · unserviceable · May 30, 2026 · N963AV · Airbus A320251N · Engine Pressure Ratio (EPR)
  > DURING TAKE OFF ENG 2 N2 OVERLIMIT 117.0% DURING 5 SECONDS. DUE TO PFR MESSAGES AND FOLLOWING TSM 73-21-00-810-B46-A REV 77 DATED 01/MAY/2026: THE OPERATIONAL TEST OF THE FADEC ON EEC CHANNEL B WAS PERFORMED IAW AMM 73-29-00-710-802-A REV 77 DATED 01/MAY/20
- [SDR ANCF202602031003](https://openairdocs.org/sdr/ANCF202602031003.md): Engine · shutdown · Feb 1, 2026 · N942AV · Airbus A320251N · Engine (Turbine/Turboprop)
  > ENG 2 SHUT DOWN DURING CRUISE.
- [SDR SOKF2026013001](https://openairdocs.org/sdr/SOKF2026013001.md): Fire Warning · false activation · Jan 14, 2026 · N901AV · Airbus A320251N · Fire Detection
  > FLIGHT AV653, DURING TAKEOFF ROLL, AFTER APPLICATION OF TAKEOFF THRUST, AN APU FIRE ECAM IND TRIGGERED, FLT CREW PERFORMED A LOW-SPEED ATO IAW OPS & SAFETY PROCEDURES. ECAM MESSAGE & RED APU FIRE WARNING LIGHT EXTINGUISHED, AS A PRECAUTION, AIRPORT FIRE SER
- [SDR F3LA202511280332](https://openairdocs.org/sdr/F3LA202511280332.md): Clamp · unsecure · Nov 27, 2025 · N384FR · Airbus A320251N · Pneumatic Distribution System
  > ENGINE NR 2 FIRE ON TAKEOFF. NO AGENT DISCHARGED. ENGINE NR 2 IN FLIGHT SHUTDOWN. CLAMP AT THE 6 0'CLOCK POSITION ON THE BLEED DUCT WAS LEFT REMOVED. R & R CLAMP & ECS DUCTING IAW AMM 36-11-49-400-827A STEPS 4-A(6) AND MULTIPLE HARNESSES IAW AMM 71-52-43-00
- [SDR F3LA202510300320](https://openairdocs.org/sdr/F3LA202510300320.md): Transmitter · leaking · Oct 30, 2025 · N394FR · Airbus A320251N · Fuel Flow Indicating
  > ENG 2 FAILURE IN FLIGHT, UNSUCCESSFUL RELIGHT. AIRCRAFT WAS GROUNDED AS A RESULT OF THIS EVENT. PERFORMED INSPECTION AFTER ENGINE WINDMILLING (ENG2) REF AMM 05-51-34-200-001-A. FOUND FUEL LEAK AT FUEL FLOW TRANSMITTER, REMOVED AND REPLACED FUEL FLOW TRANS
- [SDR 2025FA0000652](https://openairdocs.org/sdr/2025FA0000652.md): Tube · failed · Sep 18, 2025 · Engine (Turbine/Turboprop)
  > FOLLOWING A REPAIR CARRIED OUT BY SQY SHOP. THE ENGINE SERIAL NUMBER 59B069 WAS SENT FOR TESTING TO SAB. DURING THE TEST, A LEAKAGE AND FIRE OCCURED, THE PRELIMINARY CAUSES OF LEAKAGE AND FIRE HAVE NOT BEEN DETERMINED AT THIS JUNCTURE. INVESTIGATION OF THE
- [SDR ANCF20250915128](https://openairdocs.org/sdr/ANCF20250915128.md): Pump · faulted · Sep 11, 2025 · N764AV · Airbus A320251N · Hydraulic Pump (Electric/Engine), Main
  > HYD B SYS LO LVL FOLLOWED BY B SYS LO PR BLUE ELEC PUMP WAS TURNED OFF REQUEST BY ECAM WAS REMOVED THE HYD PUMP BLUE SYS (2075GJ) DUE WAS FOUND WITH HYD LEAK AT DRAIN IAW AMM TASK 29-12-51-000-001-A REV 73 WAS INSTALLED THE HYD PUMP BLUE SYS (2075GJ) IAW AM
- [SDR 2025FA0000467](https://openairdocs.org/sdr/2025FA0000467.md): Support · failed insp · Jul 10, 2025 · Engine (Turbine/Turboprop)
  > IMPELLER TUBE SUPPORT P/N: ITEM # 050B0 2468M46P01 S/N: XAEFW492 CSN: 1A_72310001210, EQUIPMENT NUMBER 6007225146 (CHAPTER 5 MANDATORY INSPECTION REQUIRED AND NOT PERFORMED PER LEAP-1A-05-21-02-01A-281B-C). ENGINE 598807 WAS RETURNED TO BRITISH AIRWAYS AFTE
- [SDR ANCF20250707321](https://openairdocs.org/sdr/ANCF20250707321.md): Pump · faulted · Jul 3, 2025 · N937AV · Airbus A320251N · Hydraulic Pump (Electric/Engine), Main
  > HYD Y RSVR LOW LVL AND LO PRESS SYSTEM HYD Y RSVR LOW LVL AND LO PRESS SYSTEM, IAW TSM 29-13-00-810-804-A, REPLACED ENGINE PUMP ON ENGINE #2 FOLLOWING INSTRUCTIONS GIVEN IN AMM 29-13-51-000-809-A AND AMM 29-13-51-400-809-A. PENDING ENGINE RUN UP AND TEST.
- [SDR F3LA202507080266](https://openairdocs.org/sdr/F3LA202507080266.md): Eec · defective · Jul 3, 2025 · N351FR · Airbus A320251N · Fuel Controlling System
  > ENG 2 FADEC SYS FAULT ON DEPARTURE CLIMBOUT, EMERGENCY CHECKLIST APPLIED, RETURNED TO ATL. REMOVED AND REPLACED ELECTRONIC ENGINE CONTROL (EEC) CHANNEL A IAW AMM 73-21-55-080-802-A/400-802-A OPS CHECKED GOOD.
- [SDR ANCF2025062719](https://openairdocs.org/sdr/ANCF2025062719.md): Blower · faulted · Jun 19, 2025 · N919AV · Airbus A320251N · Air Distribution Fan
  > VENT BLOWER FAULT DURING CRUISE, PRESENTING NOISE AND FUMES. IAW AMM 21-26-51-000-001-A/400-001-A REMOVAL AND INSTALLATION BLOWER FAN WAS REPLACED SATISFACTORILY. OPERATIONAL TEST OF THE AEVC WAS PERFORMED TEST OK.
- [SDR 2025FA0000453](https://openairdocs.org/sdr/2025FA0000453.md): Tube · broken · May 6, 2025 · Airbus A320* · Engine (Turbine/Turboprop)
  > FOLLOWING A REPAIR CARRIED OUT BY SQY SHOP, THE ENGINE S/N 59B069 WAS SENT FOR TESTING TO SAB. DURING THE TEST A LEAKAGE AND FIRE OCCURRED. THE PRELIMINARY CAUSES OF LEAKAGE AND FIRE HAVE NOT BEEN DETERMINED AT THIS JUNCTURE. A TECHNICAL INVESTIGATION AND A
- [SDR F3LA202502280193](https://openairdocs.org/sdr/F3LA202502280193.md): Hydraulic Line · leaking · Feb 26, 2025 · N349FR · Airbus A320251N · Hydraulic System, Main
  > AIRCRAFT GROUNDED DUE TO ISSUE, REFERENCE LP 529545 ITEM 1: ECAM IN FLIGHT FOR HYD RSVR LO LVL. YELLOW HYD SYS PRESSURE PIPE LEAKING. REMOVED AND REPLACED YELLOW HYD SYS PRESSURE PIPE. REF AMM 29-13-49-000-813-A/ 29-13-49-400-813-A. OPS LEAK CHECK GOOD. T/R C
- [SDR 2025FA0000139](https://openairdocs.org/sdr/2025FA0000139.md): Not Reported · not reported · Feb 25, 2025 · Standard Practices/Structures
  > PER CFM WIRE SOW/2025/02 WE HAVE BEEN INFORMED ON DATE OF FEBRUARY 25, 2025 OF A POTENTIAL INCORRECT CONFIGURATION DURING SHOP MAINTENANCE ACTIVITIES OF LEAP-1A FLEET. AFTER CHECK PER CFM RECOMMENDATION WE CONFIRM TO BE CONCERNED OF INCORRECT CONFIGURATION WH
- [SDR F3LA202501230181](https://openairdocs.org/sdr/F3LA202501230181.md): B-Nut · misinstalled · Jan 20, 2025 · N350FR · Airbus A320251N · Engine Fuel Distribution
  > AIRCRAFT GROUNDED. ON CLIMBOUT, RECEIVED AN ENG2 LOOP CAUTION FOR A FEW SECONDS. AFTER A FEW MINUTES WE RECEIVED AN ENG2 FIRE WARNING LASTING ABOUT 6 SECONDS.AFTER A FEW MINUTES WE RECEIVED IT AGAIN AND DID NOT EXTINGUISHED. COMPLIED WITH ECAM ACTIONS. UP
- [SDR F3LA2024081600115](https://openairdocs.org/sdr/F3LA2024081600115.md): Seal · leaking · Aug 15, 2024 · N378FR · Airbus A320251N · Engine Bleed Air System
  > DISCREPANCY: REFERENCE LP 448414 AFTER TAKEOFF, WE GOT A FIRE INDICATION ON THE #2 ENGINE. AC WAS GROUNDED AS A RESULT OF THIS EVENT. ALL INDICATIONS WERE NORMAL, WE FOLLOWED ECAM AND SHUT DOWN #2 ENGINE. THE FLIGHT CREW DID NOT ACTIVATE THE EXTINGUISHING BOT
- [SDR 2024F00197](https://openairdocs.org/sdr/2024F00197.md): Valve · malfunctioned · Aug 15, 2024 · N932AV · Airbus A320251N · Engine Fuel Distribution
  > DURING TAKE OFF ROLL ENG 2 FUEL RETURN VALVE NOT CLOSED APPEARED ON ECAM FUEL RETURN VALVE INOP IN OPEN POSITION TRANSFERRED TO DMI IAW MEL 73-11-01 -P-2 MEL REV 59 NO MAINT PROC REQUIERED. 932-TSR-2024-08-418. ENG 2 FUEL RETURN VALVE NOT CLOSED. IAW
- [SDR F3LA2024072900112](https://openairdocs.org/sdr/F3LA2024072900112.md): Manifold · fire · Jul 26, 2024 · N351FR · Airbus A320251N · Engine (Turbine/Turboprop)
  > #2 ENGINE FIRE WARNING DURING TAXI - OPENED #2 ENG COWLS AND TR'S ALLOWIING HALOGEN VAPORS TO DISPERSE PER AMM 72-00-00-200-819-A. DISCOVERED #1 FUEL NOZZLE B-NUT HAD BROKEN TORQUE (SAFETY WIRE INTACT) AND LEAKING FUEL PROVIDING THE SOURCE OF THE FIRE. REPLA
- [SDR F3LA2024072200107](https://openairdocs.org/sdr/F3LA2024072200107.md): Eec · inoperative · Jul 19, 2024 · N365FR · Airbus A321211 · Fuel Controlling System
  > ENG 2 FADEC SYS FAULT. AIRCRAFT WAS GROUNDED AS A RESULT OF THIS EVENT. RESET BREAKER AND PERFORMED BITE CHECK OF ENG 2 FADEC CHAN A&B IAW AMM 73-29-00-710-822-A OPS CHECK GOOD. NO DISCREPANCIES AT THIS TIME NOTED. LP 173585 ITEM 1 / REF. MEL 71-00-00C C/N
- [SDR F3LA2024072300111](https://openairdocs.org/sdr/F3LA2024072300111.md): Check Valve · inoperative · Jul 19, 2024 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)
  > LP481863 ITEM 1ENGINE #1 STALL ENROUTE TWICE AT FL 370, NO ABNORMAL ENGINE PARAMETERS OBSERVED. THIS AIRCRAFT WAS GROUNDED AS A RESULT OF THIS DEFECT. LP481863 ITEM 1. IAW TSM 77-11-00-810-815-A, REMOVED AND REPLACED IP CHECK VALVE IAW AMM TASK 36-11-41-200-
- [SDR ANCF20240606014](https://openairdocs.org/sdr/ANCF20240606014.md): Controller · faulted · Jun 4, 2024 · N779AV · Airbus A320251N · Air Conditioning System
  > VENT AVNCS SYS FAULT REPLACED THE AEVC(10HQ) REF AMM 21-26-34-000-001 AND AMM 21-26-34-100-001 AND PERFORMED OPERATIONAL TEST IAW AMM 21-26-51-710-051-A AEVC ON: P/N 87292325V07 S/N 1161 UNIT LOANED BY AMERICAN AIRLINES
- [SDR F3LA2024042500059](https://openairdocs.org/sdr/F3LA2024042500059.md): Check Valve · defective · Apr 18, 2024 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)
  > DURING CRUISE LEVEL OFF AT FL380, ECAM ENG 1 STALL FOR APPROX 6-10 SECS. N1 WAS APPROX 74%. THIRD OCCURRENCE IN 7 DAYS. REF LP 388967 AND 388971. N1 WAS BEING COMMANDED TO HIGHER N1 (APPROXIMATELY 82%) AND N1 STUCK AT 74% FOR APPROX 10 SECONDS. FA'S REPORTED
- [SDR F3LA2024040800046](https://openairdocs.org/sdr/F3LA2024040800046.md): Fmu · inoperative · Apr 6, 2024 · N324FR · Airbus A320251N · Fuel Controlling System
  > ENGINE 1 IN FLIGHT SHUTDOWN. AC WAS GROUNDED DUE TO AN SDR REPORTABLE EVENT. CORRECTED ACTION: LP 393669 ITEM 2 - REMOVED AND REPLACED FMU - ENG # 1 IAW AMM 73-21-05-000-802-A / 400-802-A. ACCOMPLISHED IDLE TEST REF AMM 73-29-00-740-803 - NO LEAKS FOUND. A/C
- [SDR ANCF20232811035](https://openairdocs.org/sdr/ANCF20232811035.md): Unknown · unknown · Nov 23, 2023 · N762AV · Airbus A320251N · Indicating/Recording System
  > DURING TAKE OFF AND CLIMB ECAM "DOOR AFT CARGO APPEARED. DUE TO MCC REQUEST PERFORM DOWNLOADING OF THE CVR DATA AND READOUT PROCEDURE OF THE DFDR. DUE TO FLIGHT RETURN MCC REQUEST W/O 17347755 PERFORM INSPECTION OF LOAD REPORT 15 HARD OVERWEIGHT LANDING SUS
- [SDR F3LA2023112200209](https://openairdocs.org/sdr/F3LA2023112200209.md): Unknown · unknown · Nov 9, 2023 · N303FR · Airbus A320251N · Compressor Bleed Valve
  > DISCREPANCY: REFERENCE LP369300. SDR REPORTABLE EVENT. FUME EVENT SMELLED LIKE SOLVENT STARTED AT BACK OF AC SLOWLY MOVING FORWARD AR STANDING HEAD LEVEL FA'S NOT FEELING WELL CLOSER TO SAT. PACK 2 OFF MADE IT WORSE PACK 1 OFF NI DIFFERANCE CORRECTIVE ACTION
- [SDR ANCF20231810029](https://openairdocs.org/sdr/ANCF20231810029.md): Oil System · warning message · Oct 18, 2023 · N762AV · Airbus A320251N · Turbine Engine Oil System
  > REJECTED TAKE OFF (AT APRPROXIMATELY 90 KTS) DUE TO ENGINE 2 HIHG OIL PRESSURE ADVISORY (APROX 140 PSI) HIGHEST TEMPERATURE REACHED BY WHEELS WAS 450°C (WHEEL 1) IN ACCORDANCE WITH AMM 73-29-00-740-819A EXCEEDANCE REPORT NO FAULT WERE FOUND AND AMM 72-00-00-2
- [SDR F3LA2023091300161](https://openairdocs.org/sdr/F3LA2023091300161.md): Engine · stalled · Sep 8, 2023 · N353FR · Airbus A320251N · Engine (Turbine/Turboprop)
  > FLIGHT 2310. AIRCRAFT WAS GROUNDED AS A RESULT OF AN SDR REPORTABLE EVENT. ENG 2 STALL AT 15000MSL WITH MOMENTARY LOSS OF THRUST, WITH MOMENTARY FLAME FLASH VISIBLE FROM CABIN. ENG PARAMETERS - PRIOR TO STALL ENG FF 200LBS / GREATER THAN ENG 1 FF, ENG 2 EGT 6
- [SDR F3LA2023083000152](https://openairdocs.org/sdr/F3LA2023083000152.md): Unknown · unknown · Aug 29, 2023 · N350FR · Airbus A320251N · Hydraulic Power System
  > IN FLT AR ROUGHLY 0800 FEET ECAM HYD Y ENG 2 PUMP LO PR - OPEN
- [SDR F3LA2023082900150](https://openairdocs.org/sdr/F3LA2023082900150.md): Valve · stuck · Aug 27, 2023 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)
  > REFERENCE LP 35036 ENG 1 STALL ECAM UPON REACHING CRUISE AT FL370. ECAM LASTED 3-5 SEC NO OTHER ECAM REMAINDER OF FLIGHT. REMOVED AND REPLACED IP VALVE IAW AMM 36-11-41-000 /400-803-A OPS CHECK GOOD NO FAULTS AT THIS TIME AC OK FOR SERVICE.
- [SDR ANCF20230108021](https://openairdocs.org/sdr/ANCF20230108021.md): Unknown · unknown · Jul 25, 2023 · N764AV · Airbus A320251N · Hydraulic Power System
  > HYD G RSVR LO LVL WAS PRESENTED ON ECAM ECAM ACTIONS WAS PERFORMED. IAW TSM 29-11-00-810-803-A WAS FOUND A LEAK COMING FROM PRESSURE PIPE IN THE GREEN HYD SISTEM IN THE NGINE PYLON, IAW TFU 29.11.00.018 AND AMM TASK 29-11-49-000-814-A REMOVAL OF THE PRESSU
- [SDR ANCF20230721018](https://openairdocs.org/sdr/ANCF20230721018.md): Vent · unserviceable · Jul 19, 2023 · N920CG · Airbus A320251N · Flight Control System
  > REJECTED TAKE OFF DUE TO VENT SKIN VALVE FAULT LOW SPEED RTO AFTER ECAM, BLOWER AND EXTRACT FAULT. LOW SPEED RTO RWY 14L SPEED BELOW 72 KNOTS (APP. SSK). WHEEL TEMP 250 C (BRAKE FAN ON) AFTER RTO. IN ACCORDANCE WITH AMM 21-26-64-000/400-001-A AEVC (10HQ) W
- [SDR 2023FA0000472](https://openairdocs.org/sdr/2023FA0000472.md): Disk · scratched · Jun 23, 2023 · Engine (Turbine/Turboprop)
  > ENGINE WAS AT SIA ENGINEERING COMPANY, ENGINE SERVICES WORKSHOP, UNDERGOING INCORPORATION OF SB 72-0412. SCRATCHES WERE FOUND ON LPT STAGE 1 DISK SURFACE H. LPT STAGE 1 DISK IS A LIFE-LIMITED PART. REQUESTED FOR FURTHER ASSISTANCE WITH CFM INTERNATIONAL AS F
- [SDR F3LA2023030800029](https://openairdocs.org/sdr/F3LA2023030800029.md): None · faulty · Mar 4, 2023 · N351FR · Airbus A320251N · Engine Bleed Air System
  > DISCREPANCY: ENG 1 FAIL AFTER NORMAL START CORRECTIVE ACTION: REF LP361869 #1 TSWS MDDR# 1192603 FOR T/S OF REPLACEMENT OF ENGINE #1 VSV ACTUATOR R/H. OPS CHECK GOOD. AC OK FOR SERVICE TSM 75-32-00-810-862-A//END//
- [SDR ANCF20231002003](https://openairdocs.org/sdr/ANCF20231002003.md): Valve · unserviceable · Feb 7, 2023 · N764AV · Airbus A320251N · Aircraft Fuel System
  > PILOT REPORT 07.FEB.2023 WO 17'032'404=> FUEL CTR L AND R XTR FAULT FUEL CTR L XFR FAULT ECAM CAUTION CAME ON DURING CRUISE; ECAM PROCEDURE PERFORMED. AFTER ECAM WAS PERFORMED FUEL L WING TANK OVERFLOW ECAM CAUTION CAME ON AND VIBRATION IN THE AIRCRAFT STAR
- [SDR F3LA2023013010016](https://openairdocs.org/sdr/F3LA2023013010016.md): Fmu · defective · Jan 24, 2023 · N316FR · Airbus A320251N · Fuel Controlling System
  > ENGINE 2 STALL ECAM. STALL WAS HEARD AND FELTED, 14,000 FEET 340 KNOTS, ECAM WANT AWAY IMMEDIATELY AND ENGINE PARAMETERS NORMAL. REMOVED & REPLACED ENG #2 FMU PER STEP 4.B.(5).(A). OPS CHECK AND LEAK CHECK GOOD.//END//
- [SDR F3LA2023130100011](https://openairdocs.org/sdr/F3LA2023130100011.md): Warning Message · illuminated · Jan 10, 2023 · N324FR · Airbus A320251N · Central Warning
  > CLIMBING THRU APPROXIMATELY 10,000 FT ENGINE LOW OIL LEVEL ADVISORY WAS FLASHING & LOST OIL RAPIDLY SHORTLY AFTER THAT WE HAD A MASTER WARNING FOR ENG 2 OIL LO PR SHUT ENGINE DOWN PER ECAM. OPEN
- [SDR F3LA2022113000156](https://openairdocs.org/sdr/F3LA2022113000156.md): Check Valve · damaged · Nov 26, 2022 · N337FR · Airbus A320251N · Turbine Engine Compressor Section
  > ON LANDING ROLLOUT, AN ECAM FOR A NR 1 ENGINE STALL WITH LARGE SURGE FELT. TOWER HEARD AN AUDIBLE BANG FELT THE CONCUSSION. FOUND IP CHECK VALVE TO BE DAMAGED, REPLACED IAW AMM 36-11-41-000-040. PERFORMED ACCEL/DECCEL TEST IAW AMM 71-00-00-710-814 ALL PAR
- [SDR F3LA2022110100143](https://openairdocs.org/sdr/F3LA2022110100143.md): Pipe · cracked · Oct 30, 2022 · N379FR · Airbus A320251N · Hydraulic Power System
  > DISCREPANCY:REFERENCE LP 289852 HYD. Y RESVR. LO LEVEL CORRECTIVE ACTION: REMOVED AND REPLACED #2 ENG FWD. PRESS. HYD. PIPE WITH POST SB PIPE IAW AMM 29-13-49-000/400-812-A. PERFORMED OPERATIONAL TEST PER SUBTASK 29-13-49-710-088-A STEPS (1) THRU (4) OPERA
- [SDR ANCF20221102032](https://openairdocs.org/sdr/ANCF20221102032.md): None · none · Oct 30, 2022 · N776AV · Airbus A320251N · Standard Practices/Structures
  > PILOT REPORT 31.OCT.2022 WO 16'683'222=> OVER WEIGHT LANDING OVER WEIGHT LANDING DUE TO MEDICAL EMERGENCY LAN WEIGHT 70.0TONS MAX LDGW 67.4 TONS VERT SPEED LESS THAN 300 ACTION TAKEN 01.NOV.2022 WO 16'683'222=> IN ACCORDANCE WITH AIRBUS REFERENCE: 811353
- [SDR F3LA2022101100130](https://openairdocs.org/sdr/F3LA2022101100130.md): Pump · leaking · Oct 10, 2022 · N336FR · Airbus A320251N · Engine Fuel Pump
  > CLEAR FLUID LEAKING FROM UNDER #1 ENGINE. CORRECTIVE ACTION: REMOVED MAIN FUEL PUMP REF AMM 73-11-05-000-801A. INSTALLED NEW PUMP REF AMM 73-11-05-400-801A. LEAK CHECK GOOD AT THIS TIME.
- [SDR F3LA2022100400127](https://openairdocs.org/sdr/F3LA2022100400127.md): Engine · stalled · Sep 29, 2022 · N328FR · Airbus A320251N · Turbine Section
  > ENG #1 STALL ECAM ON DESCENT LEVELING AT FTL 190 FELT AND HEARD ONE BUMP FROM THE #1ENGINE DID NOT OBSERVE ANY ABNORMALITIES WHEN WE LOOKED AT THE ENGINE PAREMETERS ECAM WENT AWAY BEFORE WE COULD START IT. CORRECTED ACTION: PERFORMED TSM 77-11-11-810-815-A FOU
- [SDR F3LA2022080900080](https://openairdocs.org/sdr/F3LA2022080900080.md): Engine · low pressure · Aug 7, 2022 · N331FR · Airbus A320251N · Engine Oil Pressure
  > DISCREPANCY: REFEREMCE LP 225270 SHORTLY AFTER TAKEOFF WE GOT A LOW OIL PRESSURE ECAM ON ENG#2.A PRECAUTIONARY SHUT DOWN WAS PERFORMED AND WE RETURNED TO ATL. REMOVED AND REPLACED #2 ENGINE, OPS CHECK & LEAK CHECKS GOOD, REF TASK CARDS MP71042-03, MP71042-0
- [SDR ANCF20220712024](https://openairdocs.org/sdr/ANCF20220712024.md): Harness · burned · Jul 7, 2022 · N776AV · Airbus A320251N · Fuel Control/Turbine Engines
  > PILOT REPORT 07.JUL.2022 WO 58'386'282=> (AFTER TAKE OFF AND BEFORE READING THRUST REDUCTION) AFTER TAKE OFF AND BEFORE READING THRUST REDUCTION ALTITUDE ENG # 1FIRE WAS PRESENTED ON ECAM; ANNUNCIATION STAYED ON UNTIL ENGINE 1 WAS SET TO IDLE. REQUESTED BY
- [SDR F3LA2022060200051](https://openairdocs.org/sdr/F3LA2022060200051.md): Bellcrank · worn · May 30, 2022 · N305FR · Airbus A320251N · Engine Fuel and Control
  > DISCREPANCY: REFERENCE LP247205-1: ENGING 2 STALL ECAM AT FL 220 FOR 5 SECONDS. CORRECTIVE ACTION: REPLACED #2 ENGINE L/H VBV BELLCRANK & TURNBUCKLE REFERENCE LP247210/1 AND REPLACED R/H VBV ACTUATOR REFERENCE LP247211/1 PERFORMED AMM 73-29-00-740-802-A. NO
- [SDR F3LA2022052600046](https://openairdocs.org/sdr/F3LA2022052600046.md): Pitot Tube · obstructed · May 24, 2022 · N301FR · Airbus A320251N · Indicating/Recording System
  > DISCREPANCY: REFERENCE LP 191599 ITEM 1; REJECTED TAKE OFF @ 100 KTS FOR UNRELIABLE AIRSPEED CA AIRSPEED 100KTS FOR AIR SPEED 120KTS BRAKES REACHED 600 DEGREES CORRECTIVE ACTION: PERFORMED BLOWOUT OF PITOT PROBES IAW AMM 38-10-00-170-002-A FUNCTIONAL CHECK OF
- [SDR F3LA2022052000040](https://openairdocs.org/sdr/F3LA2022052000040.md): Nozzle · leaking · May 17, 2022 · N324FR · Airbus A320251N · Fire Detection
  > DISCREPANCY: REFERENCE LP 242985 ITEM 1 AFTER LANDING. ENG 1 FIRE ECAM DISCHARGED BOTH AGENT 1 AND AGENT 2 AFTER AGENT 2 DISCHARGED INDICATION WENT OUT. CORRECTIVE ACTION: REFERENCE LP232985 ITEM 1; REMOVED ENG #1 INSPECTED REPAIRED AND REINSTALLED REF AMM 7
- [SDR F3LA2022040800024](https://openairdocs.org/sdr/F3LA2022040800024.md): Tube · damaged · Apr 7, 2022 · N347FR · Airbus A320251N · Hydraulic System, Main
  > DISCREPANCY: LP188829-2, HYD G RSVR LO LVL. CORRECTIVE ACTION: SERVICED HYD G RSVR IAW AMM 12-12-29-611-001-A, ADDITIONAL CORRECTIVE ACTION FROM LP188830-2: #1 ENG HYD LEAK FOUND. CORRECTIVE ACTION: R/R PRESS ASSY IAW AMM 20-23-11-911-001-A./END/
- [SDR F3LA2022011700102](https://openairdocs.org/sdr/F3LA2022011700102.md): None · none · Feb 16, 2022 · N311FR · Airbus A320251N · Pneumatic System
  > DISCREPANCY: ON DESCENT FLIGHT ATTENDANTS REPORTED DIRTY SOCK SMELL COMING FROM GALLEY AREA. CORRECTIVE ACTION: PER TSM DECISION TABLE ENG 1 MOST LIKELY TO BE THE SOURCE. PLACED ENG
- [SDR F3LA2022012600095](https://openairdocs.org/sdr/F3LA2022012600095.md): Gasket · leaking · Feb 9, 2022 · N352FR · Airbus A320251N · Engine Bleed Air System
  > ENG 2 FIRE ECAM ON DEPARTURE. REF LP182248 #2; INSTALLED #2 ENG TRANSIENT BLEED VALVE DUCT AND INSTALLED NEW GASKET IAW A320 AMM 36-11-49-400-827. REF LP182248 #3; REMOVED AND REPLACED #2 ENG COMBUSTOR THERMAL INSULATOR BLANKET LEAP 1A 72-41-00-05A-71AA-L REF

Next page: https://openairdocs.org/engine/cfm-international-leap-1a26/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'LEAP1A26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/cfm-international-leap-1a26/reports

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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.