# Service difficulty reports: GE CF6-80A2

A list on [GE CF6-80A2](https://openairdocs.org/engine/ge-cf6-80a2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 307 reports

- [SDR IXXA20260809001](https://openairdocs.org/sdr/IXXA20260809001.md): Stringer · cracked · Aug 9, 2026 · N761CX · Boeing 767223 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L CRACKED AT FUSELAGE BS 676.
- [SDR ABXA20260404148](https://openairdocs.org/sdr/ABXA20260404148.md): Warning Message · illuminated · Apr 4, 2026 · N312AA · Boeing 767223 · Engine Oil Pressure
  > DURING TAXI OUT, LEFT ENGINE OIL PRESS ILLUMINATED. A/C RETURNED TO GATE. (BTB) MAINTENANCE DEFERRED IAW ABX-79-33-1-1. A/C RETURNED TO SERVICE.
- [SDR ABXA20251030282](https://openairdocs.org/sdr/ABXA20251030282.md): Oil System · low · Oct 30, 2025 · N744AX · Boeing 767232 · Turbine Engine Oil System
  > DURING TAXI, RIGHT ENGINE OIL QUANTITY INDICATION INOP. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE OIL QTY. INDICATION IAW MEL 79-31-1-1. MBCB 11/02/2025. REPETITIVE INSPECTION REQUIRED BEFORE EACH FLIGHT. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250929241](https://openairdocs.org/sdr/ABXA20250929241.md): Bleed Valve · warning message · Sep 29, 2025 · N744AX · Boeing 767232 · Compressor Bleed Valve
  > ON T/O ROLL, (R ENG BLEED VAL) CAUTION MSG APPEARED. ABORTED TAKE-OFF AT 68 KNTS AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C.MTX DEFERRED RH ENGINE BLEED IAW MEL ABX - 36-11-2-1. AND RETURNED A/C TO SERVICE.
- [SDR ABXA2025521098](https://openairdocs.org/sdr/ABXA2025521098.md): Actuator · malfunctioned · May 21, 2025 · N750AX · Boeing 767232 · Turbine Engine Oil System
  > STATUS MSG: "R HYD SYS MAINT" DISPLAYED IN CRUISE. RH HYD PRESSURE AT 1620 AT CRUISE. NOTICED RT ENGINE OIL PRESSURE INDICATED RED, AND MAINT FAULT OF RT IDG, AND R HYD PRIM PUMP CAUTION MESSAGE. AIR TURN BACK TO CVG. (ATB) REMOVED AND REPLACED RH ACMP IAW
- [SDR ABXA20241207244](https://openairdocs.org/sdr/ABXA20241207244.md): Oil System · low · Dec 7, 2024 · N744AX · Boeing 767232 · Turbine Engine Oil System
  > AFTER BLOCK OUT, ON ENGINE STARTS & ENGINES RUNNING 8 MINUTES (APPROX) LEFT ENGINE QUANTITY 11, RIGHT ENGINE 14, CONTACTED MAINTENANCE & TOLD TO RETURN TO GATE FOR SERVICING. MAINTENANCE GROUNDED THE AIRCRAFT. MAINTENANCE SERVICED LEFT ENGINE OIL IAW 767-AMM 1
- [SDR IXXA20241107001](https://openairdocs.org/sdr/IXXA20241107001.md): Pad · chafed · Nov 7, 2024 · N761CX · Boeing 767223 · Engine Thrust Reverser
  > #1 ENG OTBD T/R UPPER V BAND TAB CHAFFING IN THE FAN CASE AT THE 12:00 POSITION (
- [SDR IXXA20240915064](https://openairdocs.org/sdr/IXXA20240915064.md): Engine · faulted · Sep 13, 2024 · N761CX · Boeing 767223 · Engine (Turbine/Turboprop)
  > WHILE CLIMBING THROUGH 31,000 FEET CREW REPORTED A LOUD BANG SUSPECT FROM RH ENGINE FOLLOWED BY A VIBRATION, RISE IN EGT AND LOSS OF ENGINE POWER. FOLLOWING ATI QUICK REFERENCE HANDBOOK COMPLIANCE, THE CREW SECURED RIGHT ENGINE, DECLARED AN EMERGENCY LANDING W
- [SDR IXXA202301276013](https://openairdocs.org/sdr/IXXA202301276013.md): Engine · faulted · Jan 26, 2023 · N761CX · Boeing 767223 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRECAU
- [SDR ABXA2023013016](https://openairdocs.org/sdr/ABXA2023013016.md): Regulator Valve · defective · Jan 26, 2023 · N749AX · Boeing 767232 · Compressor Bleed Valve
  > LEFT ENGINE BLEED OFF, 0 DUCT PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT HPSOV IAW B767 AMM 36-11-07. OPS AND BITE CHECK GOOD. ACCOMPLISHED BLEED SHIFT CHECK IAW B767 AMM 36-11-00, CHECKS G
- [SDR IXXA20230126013](https://openairdocs.org/sdr/IXXA20230126013.md): None · none · Jan 26, 2023 · N761CX · Boeing 767223 · Engine Oil System (Airframe Furnished)
  > RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT ENGINE. AIR TURN BACK WITH EMERGENCY DECLARATION. LANDING WAS WITHOUT INCIDENT AND NO ADDITIONAL PRE
- [SDR ABXA20221222156](https://openairdocs.org/sdr/ABXA20221222156.md): Electronic Unit · failed · Dec 21, 2022 · N740AX · Boeing 767232 · Fuel Controlling System
  > ON TAXI OUT N1 ON RT ENG FAILED. INDICATED ZERO. STBY ALSO, ALL OTHER INDICATIONS NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLACED RT. EEC OPS CHECK GOOD IAW 73-21-07. AIRCRAFT RETURNED TO SERVICE
- [SDR ABXA20221117126](https://openairdocs.org/sdr/ABXA20221117126.md): Controller · failed · Nov 16, 2022 · N750AX · Boeing 767232 · Engine Bleed Air System
  > LT ENG BLEED OFF EICAS MSG DISPLAYED AFTER BOTH ENGINES WERE STARTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R&R'D LH HIGH PRESSURE CONTROLLER IAW B767 AMM 36-11-08.0 SYSTEM OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR IXXA20221101143](https://openairdocs.org/sdr/IXXA20221101143.md): Pump · damaged · Oct 28, 2022 · N714AX · Boeing 767223 · Turbine Engine Oil System
  > DESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGENCY. OIL PSI AT 6 PSI AT SHUTDOWN & #2 ENG WINDMILLED APROX 7 MIN. LANDING UNEVENTFUL. ACFT RF
- [SDR ABXA2022091191](https://openairdocs.org/sdr/ABXA2022091191.md): Mec · faulted · Sep 11, 2022 · N740AX · Boeing 767232 · Fuel Controlling System
  > AFTER ENGINE START, RIGHT ENGINE SURGE AND EGT NOT GOING OVER 500. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MAIN ENGINE CONTROL (MEC) IAW AMM 73-21-01. REF. FIM TASK 73-11-FT 812,811 PERFORMED ENGINE RUNS IAW AMM 71
- [SDR 2022F00265](https://openairdocs.org/sdr/2022F00265.md): None · none · Jun 20, 2022 · N750AX · Boeing 767232 · Fuselage Structure (General)
  > DURING RT ENG START, NO N2; NO START VALVE; NO ROTATION VERIFIED ON GRIND. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE RE-SECURED CANNON PLUG ON START VALVE IAW B767 AMM 20-60-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR IXXA2022050301](https://openairdocs.org/sdr/IXXA2022050301.md): None · cracked · May 3, 2022 · N714AX · Boeing 767 · Engine Cowling System
  > #1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED
- [SDR IXXA2022041502](https://openairdocs.org/sdr/IXXA2022041502.md): Seal Bracket · cracked · Apr 15, 2022 · N714AX · Boeing 767 · Engine (Turbine/Turboprop)
  > FAN COWL SEAL RETAINER BRACKET CRACKED
- [SDR ABXA20210913091](https://openairdocs.org/sdr/ABXA20210913091.md): Warning Message · false activation · Sep 13, 2021 · N312AA · Boeing 767223 · Central Warning
  > RT. ENG FUEL VALVE EICAS MSG APPEARS DURING ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF FUEL CONDITION MOTOR IAW B767 AMM 76-11-00 OPS CHECK NORMAL A/C REMAINS ETOPS 180. AICRAFT RETURNED TO SERVICE.
- [SDR ABXA2021830-28081](https://openairdocs.org/sdr/ABXA2021830-28081.md): Controller · faulty · Aug 28, 2021 · N744AX · Boeing 767232 · Engine Bleed Air System
  > LH ENG BLEED VALVE EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.R&R LH HIGH PRESSURE CONTROLLER IAW AMM 36-11-08 LEAK & BITE CHECK GOOD. AICRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021430029](https://openairdocs.org/sdr/ABXA2021430029.md): Bleed Valve · intermittent · Apr 30, 2021 · N749AX · Boeing 767232 · Compressor Bleed Valve
  > AFTER ENGINE START EICAS MSG "L ENG BLEED VAL" AND L DISCRETE LIGHT " BLEED" ILLUMINATED.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED DEFERRAL PROCEDURES IAW MEL FOR LEFT HIGH PRESSURE SHUT OFF REGULATING VALVE. AIRCRAFT RELEASED B
- [SDR ABXA20200803217](https://openairdocs.org/sdr/ABXA20200803217.md): Actuator · failed · Nov 19, 2020 · N750AX · Boeing 767232 · Engine Controls
  > RT ENGINE WOULD NOT START, AIRCRAFT BACK TO BLOCK AND AIRCRAFT GROUNDED. TROUBLESHOT, PER B767 FIM 76-11-FT803 VERIFIED 28 VDC ON PIN 8, GROUND ON PIN 7. REMOVED AND REPLACED RIGHT ENGINE FUEL CONDITION MOTOR ACTUATOR, IAW AMM 76-11-04. REMOVED AND REPLACED
- [SDR ABXA20200803213](https://openairdocs.org/sdr/ABXA20200803213.md): Warning Message · false activation · Nov 13, 2020 · N750AX · Boeing 767232 · Aircraft Fuel System
  > LT FUEL VALVE EICAS DURING START NO FUEL FLOW. AIRCRAFT BACK TO BLOCK AND GROUNDED. TROUBLESHOT BOTH LT ENGINE SPAR VALVE & ENGINE VALVE NO DEFECTS NOTED. PERFORMED GROUND IDLE ENGINE IDLE RUN, IAW B767 AMM 71-00-00, NO DEFECTS NOTED ENGINE. OPERATES NORM
- [SDR ABXA20200803198](https://openairdocs.org/sdr/ABXA20200803198.md): Warning Message · false activation · Oct 19, 2020 · N749AX · Boeing 767232 · Engine Thrust Reverser
  > RT REV ISOLATION VALVE EICAS MESSAGE AFTER ENGINE START. AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS GROUNDED. MAINTENANCE INVESTIGATED PROBLEM. OPERATIONAL CHECK OF RT REVERSER GOOD, IAW AMM 78-31-00. REV CYCLED 3X TIMES WITH NO MESSAGES. AIRCRAFT RELEASED F
- [SDR ABXA20200803181](https://openairdocs.org/sdr/ABXA20200803181.md): Warning Light · illuminated · Sep 24, 2020 · N750AX · Boeing 767232 · Engine Thrust Reverser
  > LEFT REVERSER ISOLATION VALVE LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. REVERSER WAS DEFERRED AND A/C RELEASED FOR FLIGHT.
- [SDR ABXA202005153061](https://openairdocs.org/sdr/ABXA202005153061.md): Guide Vane · damaged · May 13, 2020 · N749AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > #1 ENGINE 12 OCLOCK POSITION EXIT GUIDE VANE FAIRING DAMAGED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA201912106177](https://openairdocs.org/sdr/ABXA201912106177.md): Eec · malfunctioned · Nov 26, 2019 · N749AX · Boeing 767232 · Fuel Controlling System
  > THE RIGHT ENGINE DID NOT REACH CLIMB POWER AT HIGH ALTITUDE (FL260) WITH THE ELECTRONIC ENGINE CONTROL ON. THE ENGINE ONLY PRODUCED 105% WITH THE THRUST LEVER FULL FORWARD. THRUST LEVERS WERE SPLIT OVER 1.5 INCHES. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUND
- [SDR HALA20181009483](https://openairdocs.org/sdr/HALA20181009483.md): Sleeve · torn · Oct 8, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.
- [SDR HALA2018100900483](https://openairdocs.org/sdr/HALA2018100900483.md): Sleeve · torn · Oct 8, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER TASK CARD E105-C60012-PERM ITEM 1.
- [SDR DALA201806200001](https://openairdocs.org/sdr/DALA201806200001.md): Mount · damaged · Jun 19, 2018 · Engine Mount Section
  > DURING ACCOMPLISHMENT OF REPAIR 3-2 PER DAL CMM 310T1020-3 ATA 71-21-11, AFTER REMOVAL OF ALL DAMAGE BEARING LUG INDEX 14 WAS FOUND TO MEASURE 0.714 INCH, WHICH IS 0.021 INCH BELOW THE MINIMUM DIMENSION GIVEN IN FIGURE 601, SHEET 2. ADDITIONALLY, ATTACH LUG IN
- [SDR HALA2018062000289](https://openairdocs.org/sdr/HALA2018062000289.md): Mec · malfunctioned · Jun 19, 2018 · N594HA · Boeing 767332 · Fuel Control/Reciprocating Engines
  > RIGHT ENGINE DID NOT REDUCE TO IDLE ON INITIAL DESCENT, FL370 - 11,000, CORRECTED ITSELF FOR FINAL DESCENT N1 53.0 & N2 80.9, FF 1.2. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00, UP TO STOP 2E(14)(C) COMPLETED UP TO STEPS 2F(9). COMP
- [SDR HALA2018062000290](https://openairdocs.org/sdr/HALA2018062000290.md): Mec · malfunctioned · Jun 19, 2018 · N594HA · Boeing 7673CB · Fuel Controlling System
  > IDENTICAL RT ENGINE IDLE POWER PROBLEM AS PREVIOUS FLIGHT 23 BUT WITH EEC OFF THRUST LEVER IDLE N1 42.7, N2 79.1, FF 1.3. REMOVED & REPLACED THE RT ENGINE MEC IAW AMM 73-21-01-404-032-G00 UP TO STOP 2E(14)(C). COMPLETED UP TO STEPS 2F(9). COMPLETED 73-21-01-4
- [SDR HALA2018060400274](https://openairdocs.org/sdr/HALA2018060400274.md): Engine · malfunctioned · Jun 3, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE PARAMETERS HIGH DURING DECENT AND LANDING, N1 32.0 (L), N2 65.1 (L), N1 48 (R), N2 79.4 (R), > 18000. SUSPECT LEFT ENGINE WENT TO GROUND IDLE ON APPROACH. BITE OF EEC MONITOR SHOWS NO FUALTS. REPLACED RELAYS K433 RT ENG AND K434 L ENG. PERFO
- [SDR HALA2018060400273](https://openairdocs.org/sdr/HALA2018060400273.md): Sensor · malfunctioned · Jun 1, 2018 · N594HA · Boeing 767332 · Engine Indicating System
  > DURING DECENT, AT IDLE POWER. THE RIGHT ENGINE INDICATION WAS 47% N1, THE LEFT ENGINE WAS 33% N1. AUTO THROTTLE OFF, RIGHT ENGINE HAD AT HIGH FLIGHT IDLE. TROUBLESHOT IAW FIM 73-21-00-815-817-G00, REMOVED AND REPLACED THE LEFT ENGINE CIT SENSOR IAW AMM 73-21-
- [SDR HALA2018060400272](https://openairdocs.org/sdr/HALA2018060400272.md): Engine · malfunctioned · May 31, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > DURING DESCENT, THE RIGHT ENGINE STAYED AT 41% N1 AND LEFT AT30 % N1, EQUALIZE AT 10000 FEET. TROUBLESHOT IAW FIM 71.01 F/T 804 EEC BITE WITH NO FAULT. PERFORMED PSEU BITE NO FAULT NOTED. PER TASK 71-00-00-735-001-G00 PERFORMED TEST 3, GROUND TEST FOR IDLE P
- [SDR HALA2017052200239](https://openairdocs.org/sdr/HALA2017052200239.md): Engine · power loss · May 21, 2018 · N594HA · Boeing 767332 · Engine (Turbine/Turboprop)
  > LEFT THRUST LEVER REQUIRED MANUAL ADJUSTMENT TO OBTAIN TAKEOFF THRUST AT FULL FORWARD STOP. EGT, N1, FUEL FLOWS MATCHED. THREE INCH THRUST LEVER SPLIT FROM FM 1 THR HLD INDICATED AT 100 KTS. LEFT ENGINE ACCELERATION ON TAKEOFF SLOW. LEFT ENGINE RESPONSE A
- [SDR HALA2018051600228](https://openairdocs.org/sdr/HALA2018051600228.md): Filter · contaminated · May 12, 2018 · N594HA · Boeing 767332 · Engine Fuel Distribution
  > RIGHT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT FLIGHT. REMAINED FOR LAST 2 HOURS OF FLIGHT. REPLACED THE FUEL FILTER, FOUND DEBRIS ON THE FILTER ELEMENT IAW AMM 73-11-08. ACCOMPLISHED A NR 2 ENGINE RUN UP TEST, NR 3, OPS & LEA
- [SDR 9JLA201801269691](https://openairdocs.org/sdr/9JLA201801269691.md): Fuel Control · defective · Dec 19, 2017 · N118DL · Raythn HAWKER800XP · Fuel Control/Turbine Engines
  > DURING THE LANDING PHASE, THE FLIGHT CREW REPORTED THAT THE RT ENGINE COMPUTER INDICATED A FAIL ANNUNCIATION. INVESTIGATED AND DETERMINED THAT THE RT ENGINE FUEL CONTROL UNIT HAD FAILED. THE FUEL CONTROL UNIT WAS REPLACED. OPS AND LEAK CHECKED SATISFACTORY.
- [SDR PCSA2018102525](https://openairdocs.org/sdr/PCSA2018102525.md): Engine · vibration · Oct 25, 2017 · N741AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO VIBRATION.
- [SDR PCSA20171024001](https://openairdocs.org/sdr/PCSA20171024001.md): Connector · contaminated · Oct 24, 2017 · N741AX · Boeing 767232 · Turbine Engine System Wiring
  > LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO A VIBRATION. ACCOMPLISHED FIM 71-05 FT 814, NO METAL PARTICLES FOUND IN THE INLET OR EXHAUST AREAS, NO COMTAMINATION FOUND ON THE MASTER CHIP DETECTOR. ACCOMPLISHED LT ENGINE BORESCOPE INSPECTION OF THE LPC, HPC, HPT BL
- [SDR PCSA2017053101](https://openairdocs.org/sdr/PCSA2017053101.md): Fire Warning · false activation · May 31, 2017 · N743AX · Boeing 767232 · Fire Detection
  > THE LEFT ENGINE FIRE WARNING, THE ENGINE WAS SHUTDOWN IAW THE ENGINE SECURING CHECKLIST. THE FIRE WARNING EXTINGUISHED AFTER THE DISCHARGE OF THE SECOND FIRE BOTTLE. THE OIL PRESSURE WAS NORMAL. THE ENGINE WINDMILLED FOR APPROXIMATELY 28 MINUTES.
- [SDR HALA2017012600017](https://openairdocs.org/sdr/HALA2017012600017.md): Blade · bent · Jan 26, 2017 · N594HA · Boeing 767332 · Turbine Engine Air Inlet Section
  > RIGHT ENGINE FAN BLADE DAMAGED, THE TIP IS BENT AND APPEARS TO BE HITTING RUB STRIP. THE RUB STRIP FOUND DAMAGED AND A BIG PIECE AT 6:00 MISSING. RT ENG FAN BLADE REMOVED AND BLENDED AS REQUIRED. READY FOR INSTALL. THE ACOUSTIC LINEAR WAS REPAIRED.
- [SDR HALA2017010200571](https://openairdocs.org/sdr/HALA2017010200571.md): Liner · damaged · Jan 2, 2017 · N594HA · Boeing 767332 · Turbine Engine Compressor Section
  > ETOPS, NR 2 ENG ABRAIDABLE LINER DAMAGED AT 6'OCLOCK POSITION. REPAIRED PER E105-594240-PERM AND AMM 72-33-04.
- [SDR ABXA20161106170](https://openairdocs.org/sdr/ABXA20161106170.md): Engine · power loss · Nov 6, 2016 · N749AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > ON FINAL APPROACH, THERE WAS A COMPRESSOR STALL AND LOSS OF THRUST FROM THE LEFT ENGINE. ON THE GROUND, THE EGT INCREASED TO 700 DEGREES AFTER ROLLOUT AND THE ENGINE WAS SHUT DOWN. THE AIRPLANE WAS GROUNDED AND A MAXIMUM POWER ASSURANCE TEST WAS PERFORMED IAW
- [SDR ABXA20161023151](https://openairdocs.org/sdr/ABXA20161023151.md): Engine · malfunctioned · Oct 23, 2016 · N749AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > LEFT ENGINE LOST POWER ON FINAL APPROACH. EGT WAS 690 DEGREES CELSIUS. AFTER LANDING, ENGINE WOULD NOT PRODUCE THRUST. THE AIRPLANE WAS REMOVED FROM SERVICE AND A VISUAL INSPECTION OF THE LEFT ENGINE INLET AND EXHAUST WAS PERFORMED. NO DISCREPANCIES WERE FOUND
- [SDR HALA2016062800258](https://openairdocs.org/sdr/HALA2016062800258.md): Unknown · unknown · Jun 28, 2016 · N594HA · Boeing 767332 · Engine Indicating System
  > ETOPS SIGNIFICANT SYS. ON TAKEOFF LEFT ENGINE MAX THRUST 103 PERCENT UNABLE TO INCREASE ABOVE 103 PERCENT.29 DEGREES-C AERO DATA REDUCED TARGET 104.1, MAX 107.3. T/S IAW FIM 73-21, FT 811. PERFORMED TESTS AMM 71-00-00 GROUND TESTS 3, 4 CHECKED INLET PROBES
- [SDR IXXA2016041300099](https://openairdocs.org/sdr/IXXA2016041300099.md): Hose · blown · Apr 13, 2016 · N762CX · Boeing 767232 · Hydraulic System, Main
  > EICAS MESSAGE "C HYD QTY", LOSS OF ALL QTY LEADING TO C HYD FAILURE. FOUND HOSE BLOWN.
- [SDR HALA2016031200077](https://openairdocs.org/sdr/HALA2016031200077.md): Pump · malfunctioned · Mar 12, 2016 · N594HA · Boeing 767332 · Fuel Boost Pump
  > LT FWD FUEL PUMP EICAS MESSAGE ACCOMPLISHED QRH, CONTINUE NORMAL OPERATION, FUEL 6 OF THE QRH. CHECKED CONNECTOR ON BOOST PUMP, NO SHORTS BETWEEN PHASES AND NO SHORTS TO GROUND. CHECKED WIRING BACK TO ACFT, NO SHORTS BETWEEN PHASES & NO SHORTS TO GROUND. RA
- [SDR PCSA2015061701](https://openairdocs.org/sdr/PCSA2015061701.md): Engine · power loss · Jun 15, 2015 · N743AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > TAKEOFF CANCELLED AT 70 KNOTS DUE TO POWER LOSS RT ENG. PRIOR TO POWER LOSS, ENG PARAMETERS LOOKED NORMAL.
- [SDR HALA2015040400051](https://openairdocs.org/sdr/HALA2015040400051.md): Wire · broken · Apr 4, 2015 · N594HA · Boeing 767322 · Pneumatic System Wiring
  > EICAS MESSAGE, BLEED VALVE AND OVERHEAD PANEL LT ENGINE. BLEED LIGHT ILLUMINATED DURING CRUISE AT FLT 340, PRIOR TO ETOPS AIRSPACE ATB. REPAIRED BROKEN WIRE AT PRSOV VALVE TERMINAL 1, IAW STANDARD PRACTICE 12-00. RAN ENGINE AND OPS CHECKED IAW AMM 36-11-09.

Next page: https://openairdocs.org/engine/ge-cf6-80a2/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 = 'CF680A2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80a2/reports

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