PERFORMED FIM TASK 79-21 TASK 819. PERFORMED PROCEDURE E (1A), (1B), (1C) & (1D).
/PERFORMED ENGINE FLUSH PER AMM 12-22-01. REPLACED LH ENG OIL FILTER PER AMM 79-21-07 & IPC 79-21-03-03. PERFORMED ENGINE RUN PER AMM TASK 71- - [SDR P5CA2024060400011](https://openairdocs.org/sdr/P5CA2024060400011.md): Engine · failed · Jun 4, 2024 · N714SA · Boeing 777FZB · Engine (Turbine/Turboprop) > (IFSD) ON TAKEOFF, HEARD A LOUD BANG ON THE RIGHT SIDE. RH ENG N1 ROLLED BACK. CONDUCTED RIGHT ENGINE VISUAL INSPECTION AND SEVERE DAMAGE FOUND. SHUTDOWN RIGHT ENGINE AT 0120Z(
MX IN WORK WHILE IN AOGM FOR #2 ENG FAILURE. REMOVED AND REPLACED RH ENG IAW EA - [SDR KCSA2024042715](https://openairdocs.org/sdr/KCSA2024042715.md): Fire Loop · false indication · Apr 27, 2024 · N774CK · Boeing 777F · Fire Detection > OVERHEAT CIRCUIT 2R. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT MESSAGE. CLEARS, NO DEFECTS NOTED AT THIS TIME. FIRE LOOP 2 ENGINE RIGHT. PERFORMED TROUBLESHOOTING PER KA B777 FIM 26-11 TASK 811. FAULT WAS INTERMITTENT. ME - [SDR KCSA2024042714](https://openairdocs.org/sdr/KCSA2024042714.md): Fire Warning · illuminated · Apr 27, 2024 · N774CK · Boeing 777F · Fire Detection > STATUS MESSAGES: OVERHEAT CIRCUIT R2. TRANSFERRED TO DMI #100122850 IAW B777 MEL REFERENCE 26-11-2. CATEGORY C. DUE 5-7-24. PLACARDS INSTALLED. STATUS MESSAGE: FIRE LOOP 2 ENGINE RIGHT. TRANSFERRED TO DMI #100122851 IAW B777 MEL REFERENCE 26-11-1-1. CATEGORY C - [SDR KCSA2024042513](https://openairdocs.org/sdr/KCSA2024042513.md): Detection Sys · false activation · Apr 25, 2024 · N774CK · Boeing 777F · Fire Detection > OVERHEAT CIRCUIT R2 STATUS MESSAGE. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPERATIONAL TEST IAW B777 AMM 26-11-00. ALL CHECKS GOOD. FIRE LOOP 2 ENGINE RIGHT. NO ACTIVE STATUS OR EXISTING FAULTS. PERFORMED ENGINE FIRE DETECTION OPE - [SDR QEMY20240524001](https://openairdocs.org/sdr/QEMY20240524001.md): Seal · nicked · Mar 19, 2024 · N446L · Boeing 777* · Turbine Section > ON INCOMING INSPECTION, A NICK/SCRATCH HAS BEEN FOUND ON 1 OFF AIR HOLE AFT CHAMFER, MEASURING: CIRCUMFERENTIAL 0.018 RADIAL 0.005 AXIAL (DEPTH) 0.0009. IT WAS NOTED THAT A SHOT PEEN LAYER WAS PRESENT, INDICATING THE CONDITION HAD POTENTIALLY BEEN PREVIOUSLY R - [SDR FDEA202402050138](https://openairdocs.org/sdr/FDEA202402050138.md): Gearbox · damaged · Feb 5, 2024 · N897FD · Boeing 777F · Turbine Engine Oil System > PERFORMED PRECAUTIONARY ENGINE SHUTDOWN WON RT ENGINE IN CRUISE FL280. IN TITAN INDICATION WAS SECONDARY ENG DISPLAY APPEARING ON MFD & OIL QUANTITY 3. OIL TEMP & PRESSURE INDICATED NORMAL. AFTER APPROX 5 MINS, OIL PRESSURE SLOWLY BEGAN DECREASING OVER 30-40 - [SDR FDEA202301200148](https://openairdocs.org/sdr/FDEA202301200148.md): Actuator · failed · Jan 20, 2023 · N889FD · Boeing 777FS2 · Powerplant System > L/H ENGINE I/B FAN COWL OPEN ACTUATOR UPPER ROD END BROKEN. REMOVED L/H ENGINE INBOARD FAN COWL ACTUATOR REF AMM 71-12-01-4 R/I. INSTALLED NEW FAN COWL OPENING ACTUATOR ON #1 ENGINE, RH (INBOARD) SIDE REFERENCE BOEING 777 AMM 71-12-01-4. OPERATIONAL CH - [SDR P5CA2022111700204](https://openairdocs.org/sdr/P5CA2022111700204.md): Exciter · faulted · Nov 17, 2022 · N643GT · Boeing 7673JHF · Exciter > SINGLE IGNITOR FAIL, NO LIGHT. R/ #2 ENGINE(
CONTINUE OPS PER MEL 74-00-01A TRANSFER TO MDDR 175362. CAT A DUE 18NOV22.
/LOG PAGE 1584511 M6: R/R RH ENGINE #2 EXCITER IAW AMM 74-11-01. PERFORMED AUDIBLE OPS CHECK IAW AMM 74-00-00. OPS CHECK NORMAL ON - [SDR NM1Y2021080300001](https://openairdocs.org/sdr/NM1Y2021080300001.md): Shaft · abnormal · Aug 3, 2021 · Boeing 777 · Turbine Engine Compressor Section > DURING THE HPC CONE SHAFT FPI INSPECTION DURING AN HPC MODULE SHOP VISIT, SAFRAN AIRCRAFT ENGINES DISCOVERED AN UNUSUAL 8 MM LONG CRACK IN THE SLOT AREA. THE TC HOLDER HAS BEEN INFORMED AND INVESTIGATIONS ARE ON-GOING. - [SDR FDEA202012303220](https://openairdocs.org/sdr/FDEA202012303220.md): Heat Shield · cracked · Dec 30, 2020 · N878FD · Boeing 777FS2 · Nacelle/Pylon, Main Frame > ON CHECK FOUND NR 1 ENGINE AFT FAIRING HEATSHIELD WITH 2 SEPARATE CRACKS. ATTACHED PICTURES WITH DIMENSIONS. COMPLIED WITH E.A. #: G-5450-T0358849 PT 2. NR 1 ENGINE AFT FAIRING HEATSHIED CRACKED INTERIM REPAIR. - [SDR Q2SA20201129442](https://openairdocs.org/sdr/Q2SA20201129442.md): Smoke Warning · false activation · Nov 29, 2020 · N774SA · Boeing 777FZB · Smoke Detection > AIRCRAFT GROUNDED. DURING APPROACH, LAV SMOKE ALARM SOUNDED. NEGATIVE FIRE FOUND, RESET ALARM. ICN MX RESET THE SELF TEST SWITCH AND THEN OPERATIONS CHECKED NORMAL, AS PER AMM 26-13-00/501. - [SDR Q2SA20200914435](https://openairdocs.org/sdr/Q2SA20200914435.md): Outflow Valve · inoperative · Sep 14, 2020 · N777SA · Boeing 777FZB · Pressure Regulator/Outflow Valve > AIRCRAFT GROUNDED, UNABLE TO CONTROL CABIN ALTITUDE PRESSURIZATION. CABIN PRESSURE OUTFLOW VALVE ASSEMBLY REPLACED, IAW AMM 21-31-03-000-812-002/21-31-03-400-811-002. TEST PASSED AND STATUS CLEARED. - [SDR Q2SA202001132424](https://openairdocs.org/sdr/Q2SA202001132424.md): Light · inoperative · Jan 12, 2020 · N702GT · Boeing 777F16 · Emergency Lighting > AIRCRAFT GROUNDED. EXTERNAL EMER LIGHTS NOT WORKING AT DOORS 1R AND 1L. EXTERNAL EMERGENCY LIGHT BULBS REPLACED AND TEST OK IAW AMM 33-51-04-960-801. - [SDR CA190730008](https://openairdocs.org/sdr/CA190730008.md): Axle · sheared · Jul 27, 2019 · Boeing 777233LR · Main Landing Gear Strut/Axle/Truck > (CAN) DURING REPLACEMENT OF #6 M/W FOUND MLG AXLE SLEEVE RETAINER PIN SHEARED AND SLEEVE MIGRATION OF APPROX 0.400` AFT AND 0.300` INBD. RESOLUTION L/H MAIN LANDING GEAR CENTER AXLE REPLACED AS PER AMM 32-11-26. (TC# 20190730008) - [SDR DALA2020012973598](https://openairdocs.org/sdr/DALA2020012973598.md): Tube · damaged · Jun 16, 2019 · N708DN · Boeing 777232LR · Turbine Engine Oil System > DUE TO OIL QUANTITY FELL TO L01 ON LEFT ENGINE. PRESSURE AND TEMP NORMAL. PRECAUTIONARY DIVERSION. FOUND THE NR 4 AND 5 BEARING SUPPLY OIL TUBE DAMAGE. REMOVED AND REPLACED THE OIL TUBE IAW AMM 70-00-01-400-804-H01. LEAK CHECKED GOOD. - [SDR Q2SA20180528392](https://openairdocs.org/sdr/Q2SA20180528392.md): Hmu · unknown · May 28, 2018 · N777SA · Boeing 777FZB · Fuel Controlling System > RT ENGINE INLFIGHT SHUTDOWN, STARTED NORMALLY. IAW FIM 73-22 THE HMU WAS REPLACED. THE AIRCRAFT GROUNDED. FDE RECEIVED MAINT MSG 73-34802. FOLLOWED FIM 73-22 TASK 849 ITEM C (1) TO (7) ACCOMPLISHED AND FOUND GOOD. NO FAULT NOTED IAW FIM 73-22 TASK 849. R - [SDR CALA2018040901137](https://openairdocs.org/sdr/CALA2018040901137.md): Warning Message · false activation · Apr 9, 2018 · N26967 · Boeing 7879 · Turbine Engine Oil System > ENGINE OIL FILTER RT STATUS MESSAGE DURING DESCENT. FLT CREW FOLLOWED CHECKLIST AND SHUTDOWN THE ENGINE. INSPECTED OF DEBRIS MONITORING SYSTEM SENSOR AND REPLACED THE RT ENGINE OIL FILTER, NO DEBRIS FOUND AND LEAK CHECKED OK. ACCOMPLISHED AN IN-FLIGHT WINDMIL - [SDR DALA2018040902303](https://openairdocs.org/sdr/DALA2018040902303.md): Packing · leaking · Apr 7, 2018 · N704DK · Boeing 777232LR · Turbine Engine Oil System > DIVERTED, DUE TO THE RIGHT ENGINE OIL QUANTITY INDICATED 7 QUARTS AND WAS DECREASING. MAINTENANCE FOUND THE RIGHT ENGINE STARTER LEAKING AT GEARBOX SPLIT LINE. REPLACED THE STARTER PACKINGS AND COMPLIED WITH HIGH POWER RUN, NO LEAKS NOTED. AIRCRAFT RETURNED - [SDR DALA2017091800002](https://openairdocs.org/sdr/DALA2017091800002.md): Oil System · leaking · Sep 17, 2017 · N703DN · Boeing 777232 · Turbine Engine Oil System > RETURNED TO DEPARTURE DUE TO THE LEFT ENGINE OIL QUANTITY WAS DECREASING. REPLACED THE ENGINE. - [SDR DALA2017091806954](https://openairdocs.org/sdr/DALA2017091806954.md): Seal · leaking · Sep 14, 2017 · N703DN · Boeing 777232 · Turbine Engine Oil System > RETURNED TO DEPARTURE DUE TO THE LEFT ENGINE OIL QUANTITY DECREASING. REPLACED THE IDG GEARBOX SEAL. - [SDR FDEA201708222331](https://openairdocs.org/sdr/FDEA201708222331.md): Line · chafed · Aug 22, 2017 · N862FD · Boeing 777FS2 · Turbine Engine Oil System > AT 6 30 INTO FLIGHT, RIGHT ENGINE OIL QTY DROPPED TO 4 AND STATUS ALERT. OIL CONTINUED TO DROP TO ZERO AND THEN OIL PRESSURE STARTED TO FLUCTUATE AND DROP. ALERTED GOC AND COORDINATED DIVERT TO PACD. SHUT DOWN RIGHT ENGINE WHEN "ENG OIL PRESS R" CAME ON AT - [SDR DALA2017041202957](https://openairdocs.org/sdr/DALA2017041202957.md): Blade · torn · Apr 11, 2017 · N702DN · Boeing 777232 · Turbine Engine Compressor Section > DURING BORESCOPE INSPECTION, FOUND A TEAR IN THE 5TH STAGE HPC BLADE. - [SDR DALA2017041703128](https://openairdocs.org/sdr/DALA2017041703128.md): Blade · damaged · Apr 1, 2017 · N702DN · Boeing 777232LR · Turbine Engine Compressor Section > NR 2 ENGINE HAS DAMAGE TO STAGES 3, & 5 HPC BLADES THAT EXCEED AMM 72-00-00-290-803-H01 LIMITS. COMPLIED WITH ERA 557259-14 REV ORIG, SECTION I. - [SDR FDEA201609043116](https://openairdocs.org/sdr/FDEA201609043116.md): Sensor · false indication · Sep 4, 2016 · N863FD · Boeing 777FS2 · Engine Oil Indicating System > ENGINE OIL FILTER SENSOR RT ON STATUS PAGE FOLLOWED BY ENGINE OIL FILTER BYPASS RT, ALERT ON EICAS. PERFORMED CHIP CHECK ANALYSIS AND NO M50 MATERIAL FOUND IN THE DEBRIS. REPLACED OIL FILTER - [SDR Q2SA20150921227](https://openairdocs.org/sdr/Q2SA20150921227.md): Line · leaking · Sep 21, 2015 · N774SA · Boeing 777FZB · Hydraulic System, Main > HYD PRESSURE SYS C, HYD QTY LOW SYS C: FOUND NR 12 BRAKE LINE LEAKING. INSTALLED TEMPORARY FLEX LINE ON NR 12 BRAKE IAW AMM 20-10-10. OPS AND LEAK CHECK GOOD IAW AMM 29-11-00. - [SDR CA150807002](https://openairdocs.org/sdr/CA150807002.md): Radar · failed · Aug 6, 2015 · Boeing 777233LR · Localizer/VOR System > (CAN) 12NM OUT ON LOCALIZER 08L, ACFT STARTED WEAVING. FOUND LT RADAR GAIN AT MAX. RIGHT GAIN AT CAL. RETURNED LEFT TO CAL. RT RADAR SYS TESTED IAW AMM 34-43-00-730-803-002. - [SDR CA150623009](https://openairdocs.org/sdr/CA150623009.md): Idg · failed · Jun 23, 2015 · Boeing 777233LR · AC Generator-Alternator > (CAN) RIGHT GEN DRIVE FAIL, APU REQUIRED FOR REMAINDER OF FLIGHT. RESOLUTION RT ENG DRIVEN GEN REPLACED IAW 24-11-01-401. LEAK CHECK CARRIED OUT NO LEAKS, POWER PLANT TEST CARRIED OUT IAW TASK 71-00-00-800-833-H00. OPERATIONAL TEST FOR RT IDG CARRIED OUT IA - [SDR CA150515005](https://openairdocs.org/sdr/CA150515005.md): Warning System · activated · May 14, 2015 · Boeing 777233LR · Trailing Flap Position Indicating System > (CAN) FLIGHT REPORTED FLAP RUDDER FAIL MSG ON ECAM, NO PAN PAN. DID ORDER ERS TO MONITOR & MEET ACFT ON LANDING. NO FURTHER INFO WAS PROVIDED. TROUBLESHOOTING CARRIED OUT IAW FIM 27-82-00-810-811. CHECKED SERVICEABLE. - [SDR FDEA201504171254](https://openairdocs.org/sdr/FDEA201504171254.md): Eec · inoperative · Apr 17, 2015 · N855FD · Boeing 777FS2 · Fuel Control/Reciprocating Engines > DURING CRUISE THE LT ENGINE FLAMED OUT, WOULD NOT RESTART. LEFT FUEL CONTROL VALVE ILUMINATED SHUTTING DOWN LEFT ENGINE. INFLIGHT START CHECKLIST ACCOMPLISHED LEFT ENGINE WOULD NOT RESTART. INTERROGATED MAT AND FOUND ENG EEC C1 L FAULT LATCHED (FAULT CODE) - [SDR CA150312005](https://openairdocs.org/sdr/CA150312005.md): Fan · failed · Mar 10, 2015 · Boeing 777233LR · Air Distribution Fan > (CAN) AS REPORTED BY CABIN CREW, FREQUENT AND NUMEROUS ODORS DETECTED IN GALLEY, PASSENGER CABIN, AND LAVATORY AREAS DURING FLIGHT. POWER TO IFE SYSTEM, READING LIGHT CONTROL, PASSENGER CALL SYS, ETC WERE TURNED OFF FOR REMAINDER OF FLIGHT. RESOLUTION IFE CO - [SDR FDEA201412174136](https://openairdocs.org/sdr/FDEA201412174136.md): Blade · damaged · Dec 17, 2014 · N853FD · Boeing 777FS2 · Turbine Engine Compressor Section > RIGHT ENG VIBRATION DURING CLIMB PASSING 1000` AGL. ENG SECONDARY VIBRATION MONITOR DISPLAYED 5.0 N1 ON RT ENG. VIBRATION FELT IN YOKE, RUDDER PEDALS & FLOOR. NO OTHER ABNORMAL INDICATIONS. DUMPED FUEL & RETURNED. FOUND NR 2 FAN BLADE TE TIP CAP & TE GUAR - [SDR FDEA201409272823](https://openairdocs.org/sdr/FDEA201409272823.md): Balance Weight · out of position · Sep 27, 2014 · N880FD · Boeing 777F28 · Turbine Engine Compressor Section > AS THE THROTTLES DECREASED AT TOP OF CLIMB THE AIRCRAFT DEVELOPED A SIGNIFICANT VIBRATION THAT COULD BE FELT & HEARD. THE LT ENG N1 VIBRATION WAS 3.2, ALL OTHER PARAMETERS WERE NORMAL ON BOTH ENGS. RETARDING THE THROTTLE 10% N1 IN CRUISE AT FL310 DIMINISHED - [SDR CA140523002](https://openairdocs.org/sdr/CA140523002.md): Oven · overheated · May 22, 2014 · Boeing 777233LR · Buffet/Galleys > (CAN) WHILE EN-ROUTE, FIRE WITH BLACK SMOKE REPORTED BY F/A IN REAR GALLEY OVEN. 2 FIRE EXTINGUISHERS USED TO PUT OUT THE FIRE. F/A OBSERVED SPARKS ABOVE OVEN. ALL ELECTRICAL POWER TURNED OFF TO THE AFT GALLEY OVEN AND NO FURTHER SERVICE WAS CONDUCTED. NO - [SDR CA140404003](https://openairdocs.org/sdr/CA140404003.md): Pump · failed · Apr 2, 2014 · Boeing 777233LR · Hydraulic Pump (Electric/Engine), Main > (CAN) FLIGHT DEPARTED AND ACFT BEHIND WITNESSED VAPOUR COMING FROM RT ENGINE. ONCE IN THE AIR HYDRAULIC PRESSURE IN RT PRIMARY PUMP WENT TO ZERO. MAINTENANCE ADVISED AFTER LANDING, IT WAS A BLOWN SEAL. CREW DECLARED AN EMERGENCY WITH ATC AND AFTER QUICK CONS - [SDR FDEA201306171317](https://openairdocs.org/sdr/FDEA201306171317.md): Scavenge Pump · failed · Jun 17, 2013 · N883FD · Boeing 777FHT · Turbine Engine Oil System > RT ENGINE APPEARED TO BE LOOSING OIL BEFORE START, LEFT 24 QTS, RIGHT 23 QTS. AFTER 3 HOURS OF FLIGHT RT ENG SLOWLY DECREASED TO 14 QTS WHILE LT ENG REMAINED AT 19 QTS. JUST PRIOR TO ENTERING ETOPS, RT ENG REDUCED TO 13 QTS LT AT 19 QTS. DIVERTED. OIL WENT - [SDR Q2SA20130528203](https://openairdocs.org/sdr/Q2SA20130528203.md): Skin · damaged · May 28, 2013 · N714SA · Boeing 777FZB · Leading Edge Devices > LEFT WING L/E OTBD OF ENGINE PANEL, OPEN. DURING INVESTIGATION FOUND APPROX 11 X 7 INCH SECTION OF SKIN DETACHED FROM RIVET ROW ON NR 5 SLAT STA 711.5 ACCOMPLISHED EAM 7727003R0 PART 1. R & R L/E SLAT IAW AMM 27-81-15/401. - [SDR CA130222006](https://openairdocs.org/sdr/CA130222006.md): Compressor · damaged · Feb 15, 2013 · Boeing 777233LR · Turbine Engine Compressor Section > (CAN) STARTING RT ENGINE, FUEL FLOW.3 TO.4 ON START. ENGINE ACCELERATED TOWARDS IDLE, STARTER CUTOUT, FUEL FLOW DID NOT INCREASE AND ENGINE HUNG AND WOUND DOWN. ON RESTART ALL NORMAL. ACFT FLEW 1 LEG, AND THEN MAINTENANCE AT NEXT BS T/S. ENGINE REPLACED - [SDR 2013FA0000078](https://openairdocs.org/sdr/2013FA0000078.md): Bushing · galled · Feb 7, 2013 · N775SA · Boeing 777FZB · Main Landing Gear Attach Section > AFTER VISUAL INSPECTION, RT MLG FOUND HAS A GALLED BUSHING ON RETRACTION TRUNNION SLEEVE. FOUND THE AREA OF THE PITTING ON THE SLEEVE. AREA IS WIDTH APPROX 2 CM AROUND THE SLEEVE. PERFORMED IAW RECOMMEND TO REMOVE THE BRONZE TRANSFER WITH SCOTCHBRITE, THE - [SDR Q2SA20121023198](https://openairdocs.org/sdr/Q2SA20121023198.md): Sign · inoperative · Oct 23, 2012 · N775SA · Boeing 777FZB · Emergency Lighting > LEFT DOOR AFT INTERIOR EMERGENCY EXIT SIGN INOP. TRANSFER TO DI 2789 PER MEL 33-51-01. PLACARD INSTALLED. Next page: https://openairdocs.org/engine/ge-ge90-110b1/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 = 'GE90110B1' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/ge-ge90-110b1/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.