ACCOMPLISHED WO 134669. R/R #1 ENG IAW WC 71-099-02-01 & OPS & LEAK CHECK GOOD IAW AMM 71-00-02.
) - [SDR IPXA2024032545819](https://openairdocs.org/sdr/IPXA2024032545819.md): Engine · power loss · Mar 24, 2024 · N583UP · Boeing 7474R7F · Engine (Turbine/Turboprop) > *IN FLIGHT SHUT DOWN* AT FL350, #4 ENGINE SHOWED REDUCED THRUST AND DID NOT RESPOND TO THRUST LEVEL INPUT. THERE WERE NO EICAS MSG€™S OR CAUTION INDICATIONS ON THE ENG PAGE. CREW ELECTED TO SHUT DOWN #4 ENGINE. R&R #4 ENGINE PS3 LINE NEAR 8 O€™CLOCK POSITION - [SDR UIEA2024012600044](https://openairdocs.org/sdr/UIEA2024012600044.md): Rotor · unknown · Jan 26, 2024 · N415MC · Boeing 74747UF · Fuel Controlling System > ENG 3 CONTROL STS MSG. SUSPECT EEC FAILURE(R/R #3 EEC & ROTOR OF CONTROL ALTERNATOR. OPS CHECK GOOD IAW AMM 73-21-08 & AMM 73-21-15. DMI 201757 CLOSED.
) - [SDR FDEA202312071921](https://openairdocs.org/sdr/FDEA202312071921.md): Carbon Seal · leaking · Dec 7, 2023 · N148FE · Boeing 7673S2F · Turbine Engine Oil System > AT 34,000 FT AND CRUISE MODE, OIL QUANTITY OF LEFT ENGINE WAS NOTICED TO BE AT ZERO WITH NO OTHER ABNORMAL ALERTS. OIL PRESSURE WAS AT 35-37 WHICH WAS ABOUT 20 PSI LESS THAN THE RIGHT ENGINE. THE PRESSURE SLOWLY CONTINUED TO DROP UNTIL RED LINE AT ABOUT - [SDR CALA2023011100082](https://openairdocs.org/sdr/CALA2023011100082.md): Rub Strip · missing · Jan 10, 2023 · N77066 · Boeing 767424ER · Engine Collector/Tailpipe/Nozzle > PDA 3 #2 ENG EXHAUST NOZZLE 1 WEAR PAD MISSING AND 1 WEAR PAD LOOSE AT 7 O-CLOCK POS AFT LOOKING FWD. REPLACE THE LOOSE, DAMAGED, AND/OR MISSING RUB STRIPS WITHIN 10 DAYS OR 10 CYCLES, WHICH EVER COMES FIRST. INSTALLED NEW WEAR PADS. - [SDR FDEA202207201787](https://openairdocs.org/sdr/FDEA202207201787.md): Controller · faulted · Jul 20, 2022 · N658FE · Airbus A300F4605R · Compressor Bleed Valve > PDIS 658 36-10 4286 19JUL22 BOS FACT U DURING DEPARTURE PASSING 4,000 MSL IN HIGH THRUST SETTING, BLEED VALVE #1 FAULT. COMPLIED WITH ECAM WHICH - [SDR 9WGA2022071778301](https://openairdocs.org/sdr/9WGA2022071778301.md): Duct · blown · Jul 17, 2022 · N783SN · Doug MD11F · Fire Detection > ENGINE 2 FIRE (WARNING) AT APPROXIMATELY 200FT AFTER TAKE-OFF. FOUND HPT DUCT BLOWN. INSTALLED SERVICEABLE HPT COOLING DUCT PER MD-11 AMM 75-23-00. LEAK CHECK OK. - [SDR CALA2022062701595](https://openairdocs.org/sdr/CALA2022062701595.md): Scavenge Pump · overtemp · Jun 27, 2022 · N66057 · Boeing 767424ER · Engine Oil Temperature > RT ENG OIL TEMP REACHED AMBER BAND. #2 LUBE SCAVENGE PUMP REPLACED AND HI POWER RUNS ACCOMPLOISHED. OIL TEMPS AND PRESSURE NOTIFIED. NORMAL. NO OBSEVED INDICATION FAULTS NOTED AND NO EXISTING STATUS MESSAGES. - [SDR CALA2022061701524](https://openairdocs.org/sdr/CALA2022061701524.md): Sensor · failed · Jun 17, 2022 · N66057 · Boeing 767424ER · Engine Oil Temperature > ON CLIMB RT ENGINE OIL TEMP APPROACHED 160. RAN QRH. REDUCED THR UST TO 40 N1. TEMP REDUCED. ACCOMPLISHED FIM 79-34 808. TROUBLESHOT TO A BAD OIL TEMP SENSOR.REPLACED #2 ENGINE TEMP SENSOR AND NO FURTHER DEFECTS NOTED REF AMM 79-34-01-424-15-H03. ALL WORK ACCO - [SDR UIEA2022061300589](https://openairdocs.org/sdr/UIEA2022061300589.md): Rod · unserviceable · Jun 13, 2022 · N664GT · Boeing 76731B · Engine Cowl Flaps > ENG # 2 O/B FAN COWL, AFT HOLD OPEN ROD DON'T RETRACT. REMOVED AND REPLACED # 2 ENG O/B CORE COWL HOLD OPEN ROD. OPS CHECK NORMAL IAW B767-300 AMM 71-11-11. - [SDR UIEA2022061300584](https://openairdocs.org/sdr/UIEA2022061300584.md): Fastener · missing · Jun 13, 2022 · N664GT · Boeing 76731B · Engine Collector/Tailpipe/Nozzle > ENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POSITION MISSING FASTENER (1).INSTALLED MISSING FASTENER AT ENGINE # 1 EXHAUST NOZZLE WEAR PAD AT THE 7 O' CLOCK POS AS PER B767-300 SRM 51-40-02-0G-0.) - [SDR UIEA2022061300581](https://openairdocs.org/sdr/UIEA2022061300581.md): Fuel Filter · installed · Jun 13, 2022 · N664GT · Boeing 76731B · Engine Fuel/Oil Cooler > LEFT & RIGHT ENGINE FUEL FILTERS REQUIRES REPLACEMENT AT APPROX. 150 FLT HOURS DUE TO FUEL TANK ENTRY TO BE REPLACE PRIOR TO 108387 FLT HOURS. REMOVED AND REPLACED #1 ENGINE FUEL FILTER PER 767 M/M 73-11-03-404-009-1100, REQUIRES LEAK CHECK. REMOVED & - [SDR DALA2022061204108](https://openairdocs.org/sdr/DALA2022061204108.md): Eec · failed · Jun 11, 2022 · N1604R · Boeing 767332 · Fuel Control/Turbine Engines > SHIP 1604 - ATO - ABORTED TAKE OFF AT 75 KNOTS DUE TO RIGHT ENGINE UNABLE TO MAKE TAKEOFF POWER. TARGET N1 108.1 MAX OBTAINED 96.5. CORRECTIVE ACTION: EEC UNIT FAIL FADEC FAULT 354-18B. REPLACED EEC AND HMU PER B767 AMM 73-21. OPS CHECK NORMAL. (9282962) - [SDR UIEA2022052300504](https://openairdocs.org/sdr/UIEA2022052300504.md): Frame · chipped · Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant System > #4 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) MID LOW SECTION FOUND CHIPPED (UNDER AREA OF HOLD OPEN ROD) FRAME REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG.201 REV 94, DATE 20 FEB 2022 - [SDR UIEA2022052300503](https://openairdocs.org/sdr/UIEA2022052300503.md): Cowling · gouged · Jun 2, 2022 · N416MC · Boeing 74747UF · Powerplant System > #3 ENG R/H CORE COWL MOST AFT FRAME MID LOW SECTION FOUND GOUGE MARK(FRAME REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG.201 REV.94 DATE: 20 FEB 2022) - [SDR UIEA2022060200568](https://openairdocs.org/sdr/UIEA2022060200568.md): Indicator · fault message · Jun 2, 2022 · N416MC · Boeing 74747UF · Engine (Turbine/Turboprop) > ENGINE #2 OIL QUANTITY INDICATED 19 PRIOR TO START, 14 AFTER START, 10 AT THE TOP OF THE CLIMB, AND DECREASED TO 7 BY LANDING AFTER 2:51 FLIGHT TIME. RETURNED TO RKSI WITH ENGINE #2 AT IDLE POWER. REMOVED AND REPLACED WITH NO.2 ENG AND THEN LEAK CHECK NORMAL - [SDR UIEA2022052400538](https://openairdocs.org/sdr/UIEA2022052400538.md): Rod End Bearing · elongated · May 25, 2022 · N418MC · Boeing 74747UF · Engine Thrust Reverser > NO.4 ENG LH C-DUCT OPEN ACTUATOR ROD END BOLT HOLE FOUND ELONGATED. NO.4 ENG L/H C-DUCT REPLACED IAW 78-31-01 - [SDR UIEA2022051400477](https://openairdocs.org/sdr/UIEA2022051400477.md): Blade · dented · May 14, 2022 · N649GT · Boeing 767300 · Turbine Engine Compressor Section > FAN BLADE MARKED # 11 HAS A DENT AT L/E AREA D.BLENDED OUT ENG. # 1; FAN BLADE # 11 AT LEADING EDGE; AREA FOUND WITHIN LIMITS PER B767-300 & AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION IN AREA NO CRACK OR INDICATION NOT - [SDR UIEA2022051400476](https://openairdocs.org/sdr/UIEA2022051400476.md): Blade · nicked · May 14, 2022 · N649GT · Boeing 767300 · Turbine Engine Compressor Section > FAN BLADE MARKED # 10 HAS A NICK AT L/E AREA D.BLENDED OUT # 1 ENG. FAN BLADE # 10 AT LEADING EDGE AREA FOUND WITHIN LIMITS PER B767-300&; AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED. REF. AM - [SDR UIEA2022051400475](https://openairdocs.org/sdr/UIEA2022051400475.md): Blade · nicked · May 14, 2022 · N649GT · Boeing 767300 · Turbine Engine Compressor Section > FAN BLADE MARKED # 1 HAS A NICK AT L/E AREA D. BLENDED OUT #1 ENG. FAN BLADE #1 AT L/E; AREA; FOUND WITHIN LIMITS PER B767-300 AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED AT THIS TIME. AMM 70-11 - [SDR UIEA2022051400474](https://openairdocs.org/sdr/UIEA2022051400474.md): Blade · nicked · May 14, 2022 · N649GT · Boeing 767300 · Turbine Engine Compressor Section > FAN BLADE MARKED # 8 HAS A NICK AT L/E AREA D.BLENDED OUT # 1 ENG. FAN BLADE # 8 AT L/E AREA; FOUND WITHIN LIMITS PER B767-300 SRM 72-31-02-308-045-H000. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSP OF THE AREA NO NICK ON CRACK IND NOTED REF. AMM 70-11- - [SDR UIEA2022051400470](https://openairdocs.org/sdr/UIEA2022051400470.md): Engine · installed · May 14, 2022 · N649GT · Boeing 767300 · Powerplant System > REINSTALL ALL REMOVED HYDRAULIC, PNEMAUTIC AND ELECTRIAL CONNECTORS AND LINKS DUE TO #1 ENGINE CHANGE CANCELATION. REINSTALLED ALL; HYDRAULIC; PNEUMATIC AND ELECTRICAL CONNECTORS AS PER 71-00-02. PENDING ENGINE RUN UP LEAK CHECK.PERFORMED IDLE;LEAK CH - [SDR UIEA2022051400469](https://openairdocs.org/sdr/UIEA2022051400469.md): Cowling · installed · May 14, 2022 · N649GT · Boeing 767300 · Engine Cowling System > ENGINE #1 REINSTALL ALL ENGINE COWLS DUE TO ENGINE CHANGE CANCELATION. INSTALL INLET COWL ON ENGINE #1 AS PER B767-300 AMM 71-11-01. INSTALLED FAN COWL ( LEFT RIGHT) ON ENGINE # AS PER B767-300 AMM 71-11-04. INSTALLED LEFT AND RIGHT CORE COWLS ON ENGIN - [SDR UIEA2022051400468](https://openairdocs.org/sdr/UIEA2022051400468.md): Rod · unserviceable · May 14, 2022 · N649GT · Boeing 767375 · Engine Cowling System > #2 ENGINE I/B CORE COWL HOLD OPEN STRUT DOES NOT LOCK IN OPEN POSITION. REMOVED AND REPLACED #2 ENG I/B CORE COWL HOLD OPEN ROD STRUT IAW B763 AMM 20-11-00 - [SDR DALA2022050703193](https://openairdocs.org/sdr/DALA2022050703193.md): Manifold · leaking · May 5, 2022 · N173DZ · Boeing 767332 · Turbine Engine Air Inlet Section > A/C 1703 **SMOKE SMELL EVENT** CABIN CREW ADVISES OF A CHEMICAL SMELL IN THE CABIN. FLIGHT IS CONTINUED TO JFK. CREW DONNED OXYGEN NO EMERGENCY DECLARED. FUMES DISSIPATED IN CRUISE, FLIGHT ATTENDANT COMPLAINED ABOUT HEADACHES. FLIGHT ATTENDANT WAS GIVEN OXYGEN - [SDR FDEA202204231037](https://openairdocs.org/sdr/FDEA202204231037.md): Engine · surges · Apr 23, 2022 · N732FD · Airbus A300B4605R · Engine (Turbine/Turboprop) > DURING DESCENT BETWEEN FL 200 AND 12,000 FT NUMBER 2 ENGINE SURGED FROM ABOUT 38 N1 TO 55 N1 WITH ACCOMPANYING EGT, N2, AND FF. INSTALLED MEC UP TO AND INCLUDING STEP 3.C.(19)(Z) IAW AMM. 73-21-01-04. SPECIFIC GRAVITY SET AT.82. STILL REQUIRES VBV HEA - [SDR 9WGA2021010841201](https://openairdocs.org/sdr/9WGA2021010841201.md): Warning Message · illuminated · Jan 8, 2021 · N412SN · Doug MD11F · Turbine Engine Oil System > AIR RETURN DUE TO LEVEL 2 ENGINE 2 OIL FILTER ALERT. SHUTDOWN ENGINE IN FLIGHT PER CHECKLIST. - [SDR UIEA2020111602401](https://openairdocs.org/sdr/UIEA2020111602401.md): O-Ring · leaking · Nov 15, 2020 · N1409A · Boeing 767306 · Engine Fuel Distribution > DUE TO SUSPECTED FUEL LEAK PERFORMED GVI OF WINGS AND LT & RT ENGINE. FOUND LEAK ON RT ENGINE FUEL FILTER DP SWITCH. REMOVED AND REPLACED FUEL FILTER DP SWITCH O-RING, IAW 73-34-01. PERFORMED DRY MOTOR, IAW AMM 71-00-00, NO LEAKS NOTED. OPERATIONS CHECK NO - [SDR FDEA202010302723](https://openairdocs.org/sdr/FDEA202010302723.md): Compressor · stalled · Oct 30, 2020 · N687FE · Airbus A300F4605R · Fuel Controlling System > AFTER DEPARTURE PASSING 10,000 RECEIVED ENG #2 MODE FAULT FOLLOWED ECAM AND REDUCED POWER AND RESELECT N1 MODE. FAULT CLEARED AFTER 10 SECOND HAD SEVERE BANK AND YAW ON RIGHT SIDE.SUSPECT COMPRESSOR STALL. ACCOMPLISHED BORESCOPE AND ENGINE STALL INSPECTI - [SDR 9WGA2020100241101](https://openairdocs.org/sdr/9WGA2020100241101.md): Oil System · leaking · Oct 2, 2020 · N411SN · Doug MD11F · Turbine Engine Oil System > ENGINE 1 OIL QTY REDUCED FROM 20 TO 0/ OIL QTY ZERO. - [SDR DALA2020093003228](https://openairdocs.org/sdr/DALA2020093003228.md): Relay · malfunctioned · Sep 28, 2020 · N1604R · Boeing 767332 · Engine Starting System Wiring > ATO, AT THROTTLE UP DUE TO A RIGHT STARTER CUT OUT EICAS MESSAGE. CORRECTIVE ACTION: PERFORMED IDLE RUN AT 52% N2 THE FAULT RETURNED. REPLACED K666 RELAY AND NR 2 ENGINE SPEED CARD, CLEANED RELATED CONNECTORS AND RAN ENGINE AT POWER WITH NO FAULTS. - [SDR ABXA202006296099](https://openairdocs.org/sdr/ABXA202006296099.md): Sensor · defective · Jun 26, 2020 · N767AX · Boeing 767281 · Engine Pressure Ratio (EPR) > LEFT ENGINE SLOW TO SPOOL WITH SOME STRANGE INDICATION COMPARED TO RIGHT ENGINE WITH N1'S MATCHED N2 (LEFT ENGINE) IS 10% HIGHER, OIL TEMP IS 10 DEGREES C HIGHER, OIL PRESSURE IS 10 PSI HIGHER AND N1 SHOWS A COMMAND BOX INDICATION FUEL FLOW WAS SLIGHTLY HIGHER - [SDR AALA201908269038](https://openairdocs.org/sdr/AALA201908269038.md): Eec · unreliable · Aug 25, 2019 · N346AN · Boeing 767323 · Fuel Controlling System > AIRCRAFT WAS GROUNDED: PILOT REPORTS ON INITIAL POWER APPLICATION FOR TAKE OFF, THE NUMBER ONE ENGINE WAS SUBSTANTALLY SLOWER TO SPOOL UP THAN THE #1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE #1 ENGINE MAIN ENGINE CONTROL IAW JOB CARD 12L40073001 AND LEAK C - [SDR FDEA201905081016](https://openairdocs.org/sdr/FDEA201905081016.md): Gearbox · malfunctioned · May 8, 2019 · N604FE · Doug MD11F · Fire Detection > INTERMITTENT "FIRE DET 2 FAULT" DISPALYED ON STATUS MAINT PAGE. OBSERVED 3 HRS INTO FLIGHT. REMOVED AND REPLACED THE ENGINE FIRE DETECTOR GEAR BOX, REF AMM 26-11-03-4-1. REMOVED AND REPLACED THE ENGINE FIRE DETECTOR UPPER RT TURBINE, REF AMM 26-11-03-4-1. PER - [SDR FDEA201902130408](https://openairdocs.org/sdr/FDEA201902130408.md): Pressure Switch · failed · Feb 13, 2019 · N108FE · Boeing 7673S2F · Fuel Pressure Sensor > L ENGINE FUEL FILTER EICAS MESSAGE CAME ON DURING CLIMB. EICAS MESSAGE CAME ON AND OFF SEVERAL TIMES AND REMAINED ON THROUGHOUT. MOST OFF THE FLIGHT. LT ENGINE VIBRATED AND VIBRATION INCREASED DURING DESCENT COMPLIED WITH NON-NORMAL AND NORMAL CHECKLISTS DECL - [SDR IPXA2019013038478](https://openairdocs.org/sdr/IPXA2019013038478.md): Engine · failed · Jan 30, 2019 · N252UP · Doug MD11F · Engine (Turbine/Turboprop) > ENG ONE R AND M STALLED AND ROLLED BACK 22-41 EGT RISING PAST 650. DID A PRECAUTIONARY SHUTDOWN. INSPECTED NR 1 ENG PERFORMED BORO INSP AS PER MM 72-00-07 ENG FAILED INSPECTION LIMITS, ENG REQ REPLACEMENT. - [SDR AALA20181007004](https://openairdocs.org/sdr/AALA20181007004.md): Engine · defective · Oct 7, 2018 · N342AN · Boeing 767323 · Turbine Engine Compressor Section > AIRCRAFT WAS GROUNDED. PHL-BUD DIVERTING JFK ACCOUNT COMPRESSOR STALL DUE TO A POSSIBLE BIRD INGESTION. AN EMERGENCY WAS DECLARED AND THEY LANDED OVERWEIGHT. DURING CLIMB THE "LEFT BLEED OVHT" LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AT CRUISE LEVELLING OF - [SDR AALA20180702005](https://openairdocs.org/sdr/AALA20180702005.md): Engine · unknown · Jul 1, 2018 · N343AN · Boeing 767323 · Engine (Turbine/Turboprop) > AIRCRAFT HAD A LOUD BANG AND MOVED TO THE LEFT. PASSENGERS HEARD AND FELT THE NOISE. AFTER 10 MINUTES ALL LEFT ENGINE PARAMETERS SURGED BACK AND FORTH. IAW AMM 79-21-05, LT ENGINE OIL SYSTEM MAGNETIC CHIP DETECTOR CHECK AND SERVICE. ACCOMPLISHED VSV ACTUATIO - [SDR FDEA201804291144](https://openairdocs.org/sdr/FDEA201804291144.md): Helicoil · backed out · Apr 29, 2018 · N585FE · Doug MD11F · Fuel Control/Turbine Engines > ABOUT AN HOUR INTO FLIGHT AT FL370, A LEVEL 2 FUEL QTY/USED CHECK. RAN QRH AND LEAK WAS FROM THE NR 3 ENGINE. DIVERTED AND DECLARED AN EMERGENCY. TOW DRIVER STATED FUEL WAS LEAKING FROM THE NR 3 ENGINE EVEN AFTER SHUTDOWN. PULLED THE FIRE HANDLE AND THE LE - [SDR FDEA201804171036](https://openairdocs.org/sdr/FDEA201804171036.md): Sensor · malfunctioned · Apr 17, 2018 · N685FE · Airbus A300F4605R · Engine RPM Indicating System > AFTER TAKEOFF, THE NR 2 ENGINE BECAME ERRATIC, N1 +/- 8%, FF +/- 1000 LBS. WOULD GO ON FOR SEVERAL MINUTES THEN STOP FOR A MINUTE THEN REOCCURE. RECEIVED A NR 2 FADEC FAULT ON THE ECAM ON LANDING. REMOVED AND REPLACED THE N1 SPEED SENSOR IAW AMM 77-11-01- - [SDR FDEA201712133380](https://openairdocs.org/sdr/FDEA201712133380.md): Switch · failed · Dec 13, 2017 · N659FE · Airbus A300B4605R · Fuel Pressure Sensor > ON CLIMB OUT FROM KFAR GOT FUEL CLOG LIGHT NR 2 ENG PASSING 10,000 FT. COMPLIED WITH ECAM AND REDUCED POWER. FUEL CLOG LIGHT WENT OUT AT A LOW POWER SETTING. ADVANCED POWER AND CLOG LIGHT CAME BACK ON. R&R NR 2 ENG FUEL FILTER IAW MM 73-12-02-04, FILETR R - [SDR UIEA2017120702369](https://openairdocs.org/sdr/UIEA2017120702369.md): Eec · malfunctioned · Dec 6, 2017 · N1361A · Boeing 76731B · Fuel Controlling System > L ENG EEC C1 STATUS MSG. REMOVED AND REPLACED LEFT ENGINE EEC IAW AMM 73-21-51, PERFORMED OPS CHECK IAW 71-00-00 OPS CHECK NORMAL AT THIS TIME. NO STATUS MESSAGE PRESENT. PERFORMED IDLE RUN IAW AMM 71-00-00. OPS CHECK NORMAL. - [SDR FDEA201711283321](https://openairdocs.org/sdr/FDEA201711283321.md): Pressure Switch · failed · Nov 28, 2017 · N654FE · Airbus A300F4605R · Engine Fuel Distribution > DURING T/O ROLL KBNA # 1 FUEL FILTER CLOG LIGHT AND ASSOCIATED ECAM ALERT..REJECTED T/O AND RETURNED TO THE RAMP. REMOVED AND REPLACED #1 ENG. FUEL DIFFERENTIAL PRESS. SWITCH AS PER AMM 73-34-11- 04, OPS CHECK GOOD. - [SDR IPXA2017110823386](https://openairdocs.org/sdr/IPXA2017110823386.md): Compressor · stalled · Nov 8, 2017 · N334UP · Boeing 767300 · Turbine Engine Compressor Section > AFTER TAKEOFF RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. RIGHT EGT STARTED TO FLUCTUATE FOLLOWED BY VIBRATIONS AND POPPING SOUNDS. THE TOWER REPORTED FLAMES FROM RIGHT ENGINE. ENGINE WAS SHUT DOWN, EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. REM - [SDR UIEA2017102502050](https://openairdocs.org/sdr/UIEA2017102502050.md): Clamp · out of position · Oct 25, 2017 · N649GT · Boeing 767375 · Ignition Harness (Distribution) > NR 2 ENGINE LT UPPER IGNITION LEAD CLAMP OUT OF POSITION. POSITIONED THE IGNITION LEAD CLAMP. - [SDR UIEA2017102502048](https://openairdocs.org/sdr/UIEA2017102502048.md): Blade · nicked · Oct 25, 2017 · N649GT · Boeing 767375 · Turbine Engine Air Inlet Section > NR 1 ENGINE FAN BLADE NR 12 HAS A SMALL NICK AT THE TIP. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI THE FAN BLADE IAW AMM 70-11-06-232-010-600. NO CRACKS NOTED. - [SDR UIEA2017102502047](https://openairdocs.org/sdr/UIEA2017102502047.md): Blade · nicked · Oct 25, 2017 · N649GT · Boeing 767375 · Turbine Engine Air Inlet Section > NR 1 ENGINE FAN BLADE NR 3 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI THE FAN BLADE IAW AMM 72-31-02-308-045-H00. NO CRACKS NOTED. - [SDR UIEA2017102502046](https://openairdocs.org/sdr/UIEA2017102502046.md): Blade · nicked · Oct 25, 2017 · N649GT · Boeing 767375 · Turbine Engine Air Inlet Section > NR 1 ENGINE FAN BLADE NR 14 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-405-H00. FPI OF THE BLADE IAW AMM 70-31-06-232-010-045-H00. NO CRACKS NOTED. Next page: https://openairdocs.org/engine/ge-cf6-80-series/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 = 'CF680' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/ge-cf6-80-series/reports --- 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.