# Service difficulty reports: GE CF6-80A

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

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 272 reports

- [SDR ABXA20260916410](https://openairdocs.org/sdr/ABXA20260916410.md): Engine · fluctuates · Sep 16, 2026 · N745AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF FROM MIA, RT ENG STARTED TO ROLL BACK 2-3 PER N1. AFTER TAKEOFF FLUCUATED BETWEEN 2-3 TO 6-8%. BY 500FT IT WAS BOUNCING BETWEEN 95% & 68%. UPON THRUST REVERSER APPLICATION R ENGINE WAS 8% LOWER. CREW DECLARED EMERGENCY (EDC) AND PERFORMED AIR TU
- [SDR ABXA20260608251](https://openairdocs.org/sdr/ABXA20260608251.md): Actuator · defective · Jun 8, 2026 · N767AX · Boeing 767281 · Fuel Controlling System
  > DURING ENGINE START, "L ENG FUEL VAL" EICAS MSG AND DISCRETE LIGHT ON ABOVE FUEL CONTROL SWITCHES. REMOVED AND REPLACED THE LEFT ENGINE CONDITION CONTROL ACTUATOR, REF ABX B767 AMM 76-11-04. ALL FUNCTIONS AND INDICATIONS NORMAL. AIRCRAFT "NO ETOPS". A/C RETURN
- [SDR ABXA20260117015](https://openairdocs.org/sdr/ABXA20260117015.md): Circuit Breaker · faulted · Jan 17, 2026 · N774AX · Boeing 767281 · Engine Controls
  > ON PUSHBACK, ALL T/O SPEEDS DUMPED AND UNABLE TO SET ANY T/O PWR SETTING ON TMC OR SET A TEMPERATURE A/C RETURNED TO THE GATE AND MTX GROUNDED A/C.MTX RESET CIRCUIT BREAKER IAW B767 AMM 20-60-01. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME. ACFT REMAINS CA
- [SDR ABXA20250922235](https://openairdocs.org/sdr/ABXA20250922235.md): Elec Connector · defective · Sep 22, 2025 · N745AX · Boeing 767232 · Engine Indicating System Wiring
  > ON TAKE OFF, LT ENGINE EGT FLUCTUATED. AIRCRAFT ABORTED TAKE OFF AND RETURNED TO BLOCKS. (BTB). MAINTENANCE C/W HIGH ENERGY STOP INSPECTION IAW AMM 05-51-14. NO DISCREPANCIES NOTED AT THIS TIME. REMOVED AND REPLACED D4208P AND D4208J (PYLON CONNECTORS), D9
- [SDR ABXA20250813175](https://openairdocs.org/sdr/ABXA20250813175.md): Manifold · cracked · Aug 13, 2025 · N783AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > ON TAXI R ENG HAD VIBRATIONS FROM 2.8 TO 3.3. WHEN ADDING TAXI THRUST VIBRATION INDICTIONS UP NTO 4.9 AND STARTED BEING VARIABLE- VIBRATION FELT IN AIRFRAME. AIRCRAFT RETURNED TO BLOCKS. (BTB). PERFORMED D.V.I OF RT ENG & FOUND UPPER & LOWER LPT COOLING AIR
- [SDR ABXA20250512094](https://openairdocs.org/sdr/ABXA20250512094.md): Compressor · stalled · May 12, 2025 · N783AX · Boeing 767281 · Turbine Engine Compressor Section
  > DURING CLIMB, LT ENG COMPRESSOR STALL AT APPROX FL 310 WITH CLIMB AND THRUST. STOPPED WHEN APPROX BELOW 93% N1. NO EICAS EXCEEDANCES. NO FURTHER STALLS IN CRUISE OR DESCENT. CONDUCTED STALL INSPECTION PER AMM 72-00-00/601, THEN CONDUCTED T/S PER FIM 71-05 FT
- [SDR IXXA2024032600002](https://openairdocs.org/sdr/IXXA2024032600002.md): Frame Angle · cracked · Mar 26, 2024 · N255CM · Boeing 767223 · Fuselage Main, Frame
  > REPAIR, MAIN FRAME INNER CHORD TRANSITION RADIUS. STA 883.5 RBL 89
- [SDR IXXA2024032001](https://openairdocs.org/sdr/IXXA2024032001.md): Skin Panel · delaminated · Mar 20, 2024 · N255CM · Boeing 767223 · Vertical Stabilizer, Plate/Skin
  > R/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANEL
- [SDR ABXA20221026297](https://openairdocs.org/sdr/ABXA20221026297.md): Engine · hung start · Sep 22, 2022 · N752AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > HUNG START AFTER STARTER CUTOUT. EGT CONTINUED TO RISE TWD THE LIMIT. N2 AND N1 NORMAL WITH NO INCREASE IN SPEED WITH THE INCREASING EGT. FOLLOWED QRH PROCEDURE FOR THE ABORTED START AND ELECTED TO RETURN TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE
- [SDR IXXA20220820126](https://openairdocs.org/sdr/IXXA20220820126.md): Mec · failed · Aug 16, 2022 · N791AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > DESCENDING FROM 11,500 TO 7000 FT, LEFT ENGINE OIL PRESSURE FOLLOWED BY LEFT ENGINE BLEED OFF EICAS MESSAGE. OIL PRESSURE WAS INDICATING 8 PSI EVENTUALLY GOING TO 0 WITH N1 AT 20%. NO VIBRATION OR INDICATION OF FIRE. #1 ENGINE FLAMEOUT AND ALL INDICATIONS ROL
- [SDR IXXA2022060102](https://openairdocs.org/sdr/IXXA2022060102.md): Rub Strip · cracked · Jun 1, 2022 · N255CM · Boeing 767200 · Engine Thrust Reverser
  > RUB STRIP CRACKED
- [SDR IXXA2022050402](https://openairdocs.org/sdr/IXXA2022050402.md): Thrust Reverser · cracked · May 4, 2022 · N714AX · Boeing 767223 · Engine Thrust Reverser
  > THRUST REVERSER TRAILING EDGE CRACKED
- [SDR IXXA2022060306](https://openairdocs.org/sdr/IXXA2022060306.md): Web · cracked · Apr 15, 2022 · N255CM · Boeing 767223 · Engine Cowling System
  > #2 OB CORE COWL INNER WEB CRACKED
- [SDR IXXA2022060811](https://openairdocs.org/sdr/IXXA2022060811.md): Cowling · cracked · Mar 2, 2022 · N255CM · Boeing 767223 · Engine Cowling System
  > #1 ENGINE OB CORE COWL CRACKED AT LOWER CORNER OF VENT PANEL
- [SDR ABXA20211012100](https://openairdocs.org/sdr/ABXA20211012100.md): None · none · Oct 12, 2021 · N767AX · Boeing 767281 · Engine Thrust Reverser
  > ON TAKE OFF ROLL RIGHT REV (AMBER) LIGHT ILLUMINATED. ABORTED TAKE OFF AND RETURNED TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. RIGHT REVERSER WAS DEFERRED IAW ABX MEL 78-31-1A. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA202109021086](https://openairdocs.org/sdr/ABXA202109021086.md): Start Valve · uncontrollable · Sep 1, 2021 · N750AX · Boeing 767232 · Engine Start Valves/Controls
  > RH ENGINE START VALVE UNCOMMANDED POSITION DURING START, ABORTED START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED # 2 ENG. START VALVE PER AMM 80-11-02. OPS CK GOOD. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021830083](https://openairdocs.org/sdr/ABXA2021830083.md): Start Valve · binding · Aug 30, 2021 · N768AX · Boeing 767281 · Engine Start Valves/Controls
  > LH ENGINE START VALVE FAILED TO OPEN. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. FOUND L/H ENGINE START VALVE BINDING DURING MANUAL OPERATION. REMOVED OLD, THEN INSTALLED NEW L/H START CONTROL VALVE PER AMM 80-11-02. AICRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021829080](https://openairdocs.org/sdr/ABXA2021829080.md): Starter · faulted · Aug 29, 2021 · N768AX · Boeing 767281 · Engine Starter
  > LEFT ENGINE FAILED TO START, N2 NEVER GOT ABOVE 8.7 DUCT PRESSURE WAS NORMAL. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REMOVED AND REPLACED THE #1 ENGINE STARTER IAW B767 AMM 80-11-0. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA2021529055](https://openairdocs.org/sdr/ABXA2021529055.md): Starter · failed · May 29, 2021 · N744AX · Boeing 767232 · Engine Starter
  > RH ENGINE STARTER FAILED ON ENGINE START. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. STARTER WAS REPLACED IAW AMM 80-11-01 AND AIRCRAFT WAS RELEASED FOR FLIGHT.
- [SDR ABXA2021523053](https://openairdocs.org/sdr/ABXA2021523053.md): Starter · faulty · May 23, 2021 · N744AX · Boeing 767232 · Engine Starter
  > RH ENG WOULD NOT START. WILLNOT GET ANY ROTATION,WHEN, "GND " IS SELECTED, AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. ENGINE STARTER WAS REMOVED AND REPLACED IAW AMM 80-11. AIRCRAFT RELEASED FOR FLIGHT.
- [SDR ABXA202143023](https://openairdocs.org/sdr/ABXA202143023.md): Shutoff Valve · stuck · Apr 3, 2021 · N768AX · Boeing 767281 · Engine Bleed Air System
  > RT ENG BLEED OFF LIGHT ON WITH ALSO THE RT PACK OFF LIGHT ON DURING TAXI. AIRCRAFT LINED UP FOR TAKE OFF AND RT ENG. BLEED LIGHT DID NOT EXTINGUISH DURING ENGINE ACCELERATION. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. REMOVE
- [SDR ABXA2021131006](https://openairdocs.org/sdr/ABXA2021131006.md): Engine · reads high · Jan 31, 2021 · N750AX · Boeing 767232 · Engine (Turbine/Turboprop)
  > AFTER ENGINE START LEFT ENGINE WAS IDLING HIGHER THAN RIGHT ENGINE, ITEM WAS CREW DEFERRABLE. THE DEFERRAL REQUIRED MORE FUEL TO BE ADDED FOR FLIGHT. AIRCRAFT BACK TO BLOCKS, GROUNDED BY MAINTENANCE UNTIL DEFERRAL WAS COMPLETE AND FUEL WAS ADDED.
- [SDR ABXA20200803185](https://openairdocs.org/sdr/ABXA20200803185.md): Igniter · failed · Oct 1, 2020 · N783AX · Boeing 767281 · Spark Plug/Igniter
  > NO START ON RIGHT ENGINE WITH NR 1 IGNITER, HAD TO PULL BACK TO GATE FOR TRAFFIC. AIRCRAFT GROUNDED. REMOVED AND REPLACED RIGHT ENGINE NR 1 IGNITOR PLUG, IAW AMM 74-21-02. RAN ENGINE IAW AMM 71-00-00 TABLE 501 TEST 3. ENGINE OPERATION CHECK GOOD. DI CLEAR
- [SDR UIEA2020090841951](https://openairdocs.org/sdr/UIEA2020090841951.md): Igniter Box · malfunctioned · Sep 3, 2020 · N767MW · Boeing 767277 · Low Tension Coil
  > RT ENGINE NR 1 IGNITION INOPERABLE (IGNITION SYSTEM, EXCEPT ER OPERATIONS (NOTIFY DISPATCH) R-60. TRANSFERRED TO MDDR 133851 IAW MEL 74-00-01B,CAT C,NO MAINTENANCE ACTIONS, PLACARD INSTALLED. R & R RT ENGINE NR 1, IGNITION EXCITOR BOX IAW B767 AMM 74-11-01.
- [SDR ABXA20200803154](https://openairdocs.org/sdr/ABXA20200803154.md): Pump · failed · Jul 31, 2020 · N797AX · Boeing 767281 · Engine Fuel Pump
  > LEFT ENGINE HAD NO FUEL FLOW ON START. AIRCRAFT WAS GROUNDED.
- [SDR UIEA2020012310103](https://openairdocs.org/sdr/UIEA2020012310103.md): Engine · vibration · Jan 20, 2020 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop)
  > HEARD SEVERAL BANGS AND FELT THE AIRFRAME SHUDDER EACH TIME FOLLOWED BY ABNORMAL ENGINE INDICATIONS ON RIGHT ENGINE, WHICH RESULTED IN THE ENGINE SHUTTING DOWN IN FLIGHT. NR 2 ENG REMOVED & REPLACED IAW WORK CARD A-71-999-03-01.
- [SDR ABXA20190717126](https://openairdocs.org/sdr/ABXA20190717126.md): Transducer · faulty · Jul 17, 2019 · N767AX · Boeing 767281 · Power Lever
  > DURING TAKEOFF, NEITHER ENGINE REACHED TAKEOFF N1 SPEED (109.7). THE RIGHT ENGINE N1 INDICATED 108.8 AND THE RIGHT EGT INDICATED 925 CELSIUS. THE LEFT ENGINE N1 INDICATED 107.9. THE CREW ABORTED THE TAKEOFF AT 125 KIAS. THE AIRPLANE WAS REMOVED FROM SERVICE (G
- [SDR UIEA2019021543218](https://openairdocs.org/sdr/UIEA2019021543218.md): Fuel Filter · warning message · Feb 13, 2019 · N767MW · Boeing 767277 · Engine Fuel Distribution
  > DURING CLIMB POWER EICAS MSG "L ENG FUEL FILTER" DISPLAYED (<P>ACCOMPLISHED FIM 73-11 F/T 804 BLOCKS 1 AND 21. REMOVED AND REPLACED LH ENG FUEL FILTER I.A.W. AMM 73-11-02, FILTER CONTAMINANTS NOT FOUND. PERFORMED GROUND ENG RUN I.A.W AMM 71-00-00, NO LEAKS NOT
- [SDR UIEA2018110902556](https://openairdocs.org/sdr/UIEA2018110902556.md): Engine · unknown · Nov 7, 2018 · N767MW · Boeing 767277 · Engine (Turbine/Turboprop)
  > DURING TAKEOFF, RIGHT ENGINE THRUST 94.2 N1, AUTOTHROTTLE SET 92.2 N1, AND REQUIRED A MANUAL ADJUSTMENT TO SET REQUIRED THRUST, LEFT ENGINE NORMAL, DISCONNECTED CDP SENSE LINE AND EXAMINED FOR BLOCKAGE AND LEAKAGE WITH NO NO DEFECTS NOTED, INSTALLED CDP S
- [SDR ABXA20180828096](https://openairdocs.org/sdr/ABXA20180828096.md): Engine · making metal · Aug 28, 2018 · N795AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT AT APPROXIMATELY FLIGHT LEVEL 190, THE CREW HEARD A BOOM AND SMELLED A STRONG SMOKE ODOR. AT THE SAME TIME, THE AIRPLANE YAWED AND SHUTTERED. THE RIGHT ENGINE HAD HIGH EGT (1100 DEG) AND N2 INDICATION (113.1). THE RIGHT ENGINE WAS SHUT DOWN AND TH
- [SDR ABXA20180821095](https://openairdocs.org/sdr/ABXA20180821095.md): Engine · failed · Aug 21, 2018 · N783AX · Boeing 767281 · Engine (Turbine/Turboprop)
  > IN THE BEGINNING OF THE TAKEOFF ROLL WITH THRUST SELECTED, THE RIGHT ENGINE DID NOT RESPOND TO THROTTLE ADVANCEMENT & THE TAKEOFF WAS REJECTED. THEN DURING THE SECOND TAKEOFF ROLL WITH THE AUTO THROTTLE SELECTED OFF, THE RIGHT ENGINE FAILED TO ACCELERATE, CAUS
- [SDR UIEA2018031000358](https://openairdocs.org/sdr/UIEA2018031000358.md): Cable · not reported · Mar 13, 2018 · N767MW · Boeing 767277 · Compressor Bleed Valve
  > VBV FLEX CABLE FAILED RIG TEST ON THE NR 2 ENGINE. REMOVED AND REPLACED VBV FLEX CABLE, RIGGED VBV AND VSV SYSTEM, FUNCTIONAL CHECK GOOD.
- [SDR ABXA20170102144](https://openairdocs.org/sdr/ABXA20170102144.md): Mec · malfunctioned · Dec 28, 2017 · N774AX · Boeing 767281 · Fuel Controlling System
  > LEFT ENGINE FLAME OUT (SHUTDOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 18,000 FEET. THE ENGINE WOULD NOT RESTART IN FLIGHT. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE LEFT ENGINE'S MAIN ENGINE CONTROL (MEC), COMPRESSOR INLET TEMPERATURE
- [SDR UIEA2017120302342](https://openairdocs.org/sdr/UIEA2017120302342.md): Filter · warning message · Dec 3, 2017 · N767MW · Boeing 767277 · Engine Fuel Distribution
  > INTERMITTENT RIGHT ENGINE FUEL FILT EICAS MESSAGE AT HIGH THRUST SETTINGS (<P>ACCOMPLISHED FIM 73-11 F/T 804. FOUND CONTAMINATION ON FILTER ELEMENT (NO METAL) REMOVED AND REPLACED FILTER ELEMENT IAW AMM 73-11-02. PERFORMED OPS OF DIFFERENTIAL PRESSURE SWITCH I
- [SDR ABXA20171201142](https://openairdocs.org/sdr/ABXA20171201142.md): Stator Vane · out of adjust · Dec 1, 2017 · N783AX · Boeing 767281 · Turbine Engine Compressor Section
  > THE RIGHT ENGINE HAD COMPRESSOR STALLS DURING CLIMB BETWEEN FL340 AND FL350. THE THROTTLE WAS RETARDED 10% AND THE COMPRESSOR STALLS STOPPED. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE RIGHT ENGINE'S VARIABLE STATOR VANE SYSTEM WAS INSPECTED AND
- [SDR ABXA20171127141](https://openairdocs.org/sdr/ABXA20171127141.md): Sensor · malfunctioned · Nov 27, 2017 · N794AX · Boeing 767281 · Fuel Controlling System
  > PASSING THROUGH FLIGHT LEVEL 230, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. THE CREW COULD NOT RESTORE NORMAL ENGINE OPERATION VIA THE QUICK REFERENCE HANDBOOK PROCEDURES. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE RIGHT ENGINE'S MAIN ENGINE CONTROL
- [SDR ABXA20171124140](https://openairdocs.org/sdr/ABXA20171124140.md): Stator Vane · out of adjust · Nov 24, 2017 · N794AX · Boeing 767281 · Turbine Engine Air Inlet Section
  > DURING CLIMB THROUGH FLIGHT LEVEL 200, THREE LOUD BANGS OCCURRED THAT JOLTED THE AIRCRAFT. THE AIRPLANE SEEMED TO YAW EACH TIME. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE LEFT ENGINE'S VARIABLE STATOR VANE SYST
- [SDR ABXA20171122139](https://openairdocs.org/sdr/ABXA20171122139.md): Compressor · stalled · Nov 22, 2017 · N794AX · Boeing 767281 · Turbine Engine Compressor Section
  > RIGHT ENGINE HAD A COMPRESSOR STALL. THE AIRPLANE WAS REMOVED FROM SERVICE AND THE FAULT ISOLATION MANUAL DIAGRAM 71-05, FAULT TREE 808 WAS ACCOMPLISHED. ALL FINDINGS WERE WITHIN LIMITS. THE CAUSE OF THE COMPRESSOR STALL IS UNKNOWN.
- [SDR UIEA2017093001907](https://openairdocs.org/sdr/UIEA2017093001907.md): Engine · odor · Sep 25, 2017 · N659GT · Boeing 767281 · Engine (Turbine/Turboprop)
  > STRONG ELECTRICAL ODOR DETECTED WHIILE CLIMBING THROUGH FL 320 AND UNTIL A RETURN LANDING, THE ODOR DISSIPATED AT 4000 FT, NO SMOKE OR OTHER ABNORMALLY OBSERVED. REMOVED AND REPLACED THE NR 2 ENGINE IAW 71-00-00, PERFORMED REQUIRED TEST 1, 3, 4, 7, AND 12.
- [SDR UIEA2017092201787](https://openairdocs.org/sdr/UIEA2017092201787.md): Pressure Switch · no test · Sep 22, 2017 · N767MW · Boeing 767277 · Fuel Controlling System
  > NR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE NR 2 ENGINE FUEL FILTER BYPASS DIFFERENTIAL PRESSURE SWITCH, OPS CHECKED GOOD IAW AMM 73-34-01 AND AMM 71-00-00.
- [SDR UIEA2017092201780](https://openairdocs.org/sdr/UIEA2017092201780.md): Shutoff Valve · no test · Sep 22, 2017 · N767MW · Boeing 767277 · Pneumatic Distribution System
  > NR 1 ENGINE PRSOV FAILED A FUNCTIONAL CHECK. REMOVED AND REPLACED THE PRSOV. OPS CHECKED GOOD IAW AMM 36-11-09.
- [SDR UIEA2017092201774](https://openairdocs.org/sdr/UIEA2017092201774.md): Cable Assy · malfunctioned · Sep 22, 2017 · N767MW · Boeing 767277 · Compressor Bleed Control
  > NR 2 ENGINE SLOW TO SPOOL. REMOVED AND REPLACED THE NR 2 ENGINE VSV FEED BACK CABLE ASSY, OPS CHECKED GOOD AND ACCELERATION NORMAL IAW AMM 75-31-03, AND AMM 71-00-00.
- [SDR UIEA2017073001383](https://openairdocs.org/sdr/UIEA2017073001383.md): Warning Message · false activation · Jul 30, 2017 · N767MW · Boeing 767277 · Compressor Bleed Valve
  > RIGHT ENGINE BLEED VALVE CAUTION DESCENDING OUT OF FL 390. ACCOMPLISHED FIM 36-11 FT 954. NO DEFECTS NOTED TO SENSE, MUSCLE OR LINES. NO DEFECTS TO WIRING OR CONNECTORS PERFORMED HPSOV OPS CHECK IAW AMM 36-11-07, OPS CHECKED NORMAL. GROUND RUN ENGINE, RT ENG
- [SDR IXXA20170513999](https://openairdocs.org/sdr/IXXA20170513999.md): Engine · making metal · May 9, 2017 · N763CX · Boeing 767232 · Engine (Turbine/Turboprop)
  > FLIGHT ATN3706 EN ROUTE FROM DEPARTURE STATION KABE TO DESTINATION STATION KONT EICAS MESSAGE DISPLAYED "R OIL FILTER". AS DIRECTED BY QRH, THE RIGHT ENGINE WAS SHUTDOWN. NOTIFIED ATC, DECLARED EMERGENCY. DIVERSION TO KILN. LANDED WITHOUT FURTHER INCIDENT. AIR
- [SDR UIEA2017042900677](https://openairdocs.org/sdr/UIEA2017042900677.md): Solenoid · failed · Apr 29, 2017 · N767MW · Boeing 767277 · Fuel Controlling System
  > RIGHT ENGINE EEC OFF EICAS AND OFF LIGHT ILLUMINATED ON POWER TRANSFER DURING ENGINE START. RESET AND OPS NORMAL FOR FULL FLIGHT, COMPLIED WITH FIM 73-21 FT 805 AND FIM 71-01FT 804 REMOVED AND REPLACED THE RT ENGINE PMC IAW AMM 73-21-02, NO HELP, RE INSTALL
- [SDR UIEA2017040900531](https://openairdocs.org/sdr/UIEA2017040900531.md): Line · loose · Apr 7, 2017 · N656GT · Boeing 767281 · Fuel Controlling System
  > DURING TAKE OFF AT 80 KTS, THE RT ENGINE ROLLED BACK TO 96.8 N1, UNABLE TO PUSH BACK TO MATCH, LT ENGINE AT 100.4. ACCOMPLISHED EEC BITE IAW FIM 71-01, 804, NO FAULTS NOTED. FOUND LOOSE CBT LINE ON MEC. RAN ENGINE TO POWER IAW AMM 71-01-00, ALL INDICATION
- [SDR UIEA2017022000218](https://openairdocs.org/sdr/UIEA2017022000218.md): Inlet · corroded · Mar 1, 2017 · N656GT · Boeing 767281 · Turbine Engine Air Inlet Section
  > NR 2 ENGINE INLET LOWER TWO BOLT HOLES HAVE CORROSION. FREEZE PLUGS FABRICATED AND INSTALLED IAW SRM 51-20-07, PARA B, FIG 5 & FIG C, AND PARA 3B AND RDR PMO-TLS-17-007-14B.
- [SDR ABXA20170114002](https://openairdocs.org/sdr/ABXA20170114002.md): Bolt · missing · Jan 14, 2017 · N775AX · Boeing 767281 · Fuel Heater
  > LEFT ENGINE FLAME OUT (SHUT DOWN) OCCURRED WHILE DESCENDING THROUGH APPROXIMATELY 10,000 FEET. THE QUICK REFERENCE HANDBOOK’S ENGINE FAILURE AND ENGINE IN FLIGHT START CHECK LIST WAS COMPLETED. THE ENGINE RESTART WAS SUCCESSFUL. THE AIRPLANE WAS REMOVED FROM
- [SDR UIEA2016092000763](https://openairdocs.org/sdr/UIEA2016092000763.md): Engine · power loss · Sep 20, 2016 · N656GT · Boeing 767281 · Engine (Turbine/Turboprop)
  > RTO ON TAKEOFF RT ENGINE DID NOT PRODUCE TAKEOFF THRUST, RTO BELOW 80 KNOTS. COMPLIED WITH GROUND TEST NR 4 VERIFIED BOTH ENGINE MAKE T/O POWER 108.6 NO THROTTLE SPLIT ELECTRONIC ENGINE CONTROL OFF REF AMM 71-00-00. TRANSFERED TO MDDR 70393 IAW MEL 73-21-01
- [SDR IXXA20160420019](https://openairdocs.org/sdr/IXXA20160420019.md): Skin · corroded · Apr 20, 2016 · N762CX · Boeing 767232 · Fuselage Main, Plate/Skin
  > THE FOLLOWING WORK WAS ACCOMPLISHED DURING VISIT BY MX & ENGINEERING SERVICES. FUSELAGE SKIN, PN 146T3531-3, CORRODED AT STATION 1414, STRINGER 35R INBD OF AFT DRAIN MAST AT SKIN LAP. THE FUSELAGE SKIN WAS REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201 & 469

Next page: https://openairdocs.org/engine/ge-cf6-80a/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 = 'CF680A'
ORDER BY difficulty_date DESC
```

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

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