GE GE90-115B

Service difficulty reports · 122

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 = 'GE90115B'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CA120403004Line · leaking(CAN) RETURNED TO GATE DUE TO HYD QTY LOW LT EICAS DURING TAXI OUT. THE LT HYD SYS RESERVOIR WAS CONFIRMED TO BE PHYSICALLY LOW, BUT THERE WAS NO OBVIOUS EXTERNAL HYDRAULIC LEAKAGE SEEN. THE AIRPLANE WAS THEN ROUTED TO THE HANGAR FOR INVESTIGATION. DURING TRMar 31, 2012 · Boeing 777333ER · Hydraulic System, MainSDR CA110815005Oven · odor(CAN) CREW ADVISED FLIGHT DISPATCH AND MOC OF A BURNING ODOR COMING FROM NR 2 GALLEY. ALL OVENS AND CHILLERS WERE SHUTDOWN, ODOR DISSIPATED. ELECTRICAL ODOR FROM GALLEY NR 2 5HRS INTO FLT. OVENS TURNED OFF AND CHILLER OFF ODOR DISSIPATED. LT NR 2 GALLEY SHAug 13, 2011 · Boeing 777333ER · Buffet/GalleysSDR CA110718014Pitch Control · malfunctionedTAKEOFF REJECTED AT 30KTS DUE TO A FLIGHT CONTROL FAULT, FULL NOSE DOWN TRIM ON TAKEOFF ROLL. RETURNED TO GATE. WHEN T/O THRUST APPLIED CONFIG STABILIZER SOUNDED. TRIM WAS VERIFIED TO GREEN BAN AT 3.5 DURING T/O CHECK. FIM TASK 27-41-00-810-809 CARRIED OJul 12, 2011 · Boeing 777333ER · Stabilizer Position IndicatingSDR CA110708008Switch · failedSMOKE COMING FROM SEAT ROW 31 HJ. POWER REMOVED WITH IFE/PAX SWITCH. SMOKE STOPPED AND ELECTRICAL ODOR DECREASED AFTER REMOVAL OF POWER. DISPATCH AND MX ADVISED FOUND QSEB 31J AT FAULT. PART REPLACED SWITCH DOWNLOAD C/O. OPS OK. NO DAMAGE TO WIRING.Jun 27, 2011 · Boeing 777333ER · Equipment/Furnishings WiringSDR CA110615001Charger · failedODOR OF SMOKE IN THE COCKPIT, MAIN BATTERY & BATTERY CHARGER MAIN STAUS MESSAGES APPEARED. RETURNED TO LAND. DUMPED FUEL. FOUND MAIN BATTERY CHARGER AT FAULT MAIN 7 APU BATTERY, MAIN & APU BATTERY CHARGER. APU BATTERY DFD MEL 24-31-01B.Jun 14, 2011 · Boeing 777333ER · Battery/Charger SystemSDR CA110429003Line · leaking(CAN) FLIGHT CREW CALLED STATION TO REPORT THAT THEY LOST HYDRAULIC PRESSURE DURING TAXI TO THE GATE. MAINTENANCE AND TOW CREW CALLED FOR ASSISTANCE. MAINTENANCE HAD TO CAP THE NR 12 LINE AND THE ACFT WAS TOWED TO THE GATE. THE SPILL WAS 2 FT X 2 FT AND Apr 28, 2011 · Boeing 777333ER · Landing Gear Brake SystemSDR CA101224001Electrical Box · burned(CAN) DURING THE FLIGHT, A BRIEF FIRE STARTED UNDER SEAT THE 63E ELEX BOX. TWO (2) HALON BOTTLES WERE USED TO EXTINGUISH THE FIRE. ONCE OUT, A MEMBER OF THE CABIN CREW WAS ABLE TO REACH IN UNDER THE SEAT AND PULL THE WIRING OUT. THERE WAS NIL ADVERSE PASSENGERDec 23, 2010 · Boeing 777333ER · Entertainment SystemSDR CA101214004Window · cracked(CAN) APPROXIMATELY 4 HOURS AFTER DEPARTURE THE CREW REPORTED THE INSIDE PANEL OF THE FIRST OFFICERS WINDOW HAD CRACKED. THERE WAS NO ARCING AND NO PRESSURE LOSS. RT WINDSHIELD REPLACED AS PER AMM 56-11-00-200-801. WINDOW HEAT OPS TEST C/O, NO FAULTS FOUND.Dec 12, 2010 · Boeing 777333ER · Flight Compartment WindowsSDR 2010FA0001211Turbine Blades · missing(B-16709) RT ENGINE HIGH VIBRATION DURING CLIMB AFTER FL210- 4.3 MAX FELT NEAR R4 DOOR AND ADJACENT CABIN, AIR TURN BACK. PERFORM BSI ON NR2 ENGINE FOUND LPT-1, STG-1 BLADE MISSING AND LPT STG-1 TO STG-4 BLADES DAMAGED, R & R NR2 ENGINE.Nov 20, 2010 · N16709 · Boeing 777 · Turbine SectionSDR CA101019013Wire Harness · chafedDURING TROUBLESHOOTING FOR MULTIPLE AUTOTHROTTLE DISCONNECT SNAGS FOUND WIRES W0770-2008B-20, W0770-2008R-20, W0770-2006B-20 AND W0770-2006R-20 CHAFED ON NR 2 ENG FAN CASE AT THE 12 O`CLOCK POSITION. WIRES TEMPORARILY REPAIRED UNDER PRODUCTION PERMIT B777-73-Oct 16, 2010 · Boeing 777333ER · Engine Control System WiringSDR CA100920002Elevator · unknownON DEPARTURE CREW ADVISED PROBLEM WITH LOAD/TRIM ON ROTATION. TAIL HEAVY, REQUIRED CHECK FWD TO STOP RAPID ROTATION. COLUMN FORCE TRANSDUCER TEST OK. ELEVATOR FEEL SYS TEST, OK. CARGO WEIGHT CHECK OK. UNABLE TO LOCATE EARLIER SNAG SERV.Sep 16, 2010 · Boeing 777333ER · Elevator Control SystemSDR Z6WR 004 2010Panel · debondedTHE 314W1510-2 COWL BOND PNL. (CMM 71-11-30, FIG 2 ITEM 585), HAS EXPOSED GRAPHITE PLIES DUE TO MISSING FIBERGLASS AND WIRE MESH. ON THE UPPER SIDE THERE ARE (3) AREAS WITH MATERIAL STILL ATTACHED AS WELL AS THE LWR END, BUT THE EDGES ARE LOOSE AND LIFTING UPAug 6, 2010 · Boeing 777367ER · Engine Air Intake SystemSDR CA091215003Housing · damaged(CAN) DURING ROUTINE MAINTENANCE, IT WAS FOUND THAT BOTH LT AND RT ENGINE LP FUEL FILTER BOWLS HAD ARCHING DAMAGE. A REPLACEMENT HOUSING WAS ROBBED FROM A SERVICEABLE SPARE POWERPLANT BUT WAS FOUND WITH EVEN MORE SEVERE DAMAGE. ALL DAMAGED HOUSING REPLACED WDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA100119003Housing · worn(CAN) NR 1 ENGINE LP FUEL FILTER HSG AND FILTER SHOWING SIGNS OF WEAR. ATTACHED POWER POINT PRESENTATION SHOWS THE DAMAGED FOUND ON ENGINE NR 2. ENGINE NR 2 ALSO SHOWED SIGNS OF ARCHING AND THE PICTURE SHOWS WHAT APPEARS TO BE A BLACK HOLE. THE NR 1 ENGINE DIDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA100119004Housing · worn(CAN) THE DAMAGED FUEL FILTER WAS FOUND ON ALIAS B34/SN 906537. THIS ENGINE IS CURRENTLY INSTALLED ON 731 POSITION NR 1. PRODUCTION PERMIT 777-73-39874 HAS BEEN ISSUED TO COVER THE FRETTING FOUND. THE DAMAGE FOUND ON THE POWER PLANT WHEN IT WAS OFF WING. (THDec 15, 2009 · Boeing 777333ER · Engine Fuel DistributionSDR CA091022003Software · malfunctioned(CAN) IN CRUISE AT FL380 ENROUTE TO YVR, AIRCRAFT HAD TEMPORARY LOSS OF BOTH PACKS. BOTH PACKS RETURNED WITHIN APPROX 10 SECONDS. P/N FOR ASCPC AND S/W GIVEN ABOVE. OUTFLOW VALVE PART NUMBER IS 2119160-2. PER IPC 21-31-03-01, THIS IS AN UNAPPROVED COMBINATIOct 7, 2009 · Boeing 777333ER · Cabin Pressure Control SystemSDR CA090811001Transmission · failedAFTER TAKE-OFF THE FLIGHT HAD A FLAPS GEAR DRIVE FAILURE WITH THE FLAPS IN A POSITION BETWEEN 5 AND 20. FLIGHT WAS UNABLE TO CONTINUE TO DESTINATION AND RETURNED TO DEPARTURE. THE FLIGHT WAS APPROX 75000K OVERWEIGHT AND CREW CALLED A PAN PAN EMERGENCY FOR LAJul 23, 2009 · Boeing 777333ER · Trailing Edge Flap Control SystemSDR CA090408003Transmission · malfunctioned(CAN) ACFT DEFECT LOG SNAG RAISED FOR FLAP DRIVE FAILURE WHEN RETRACTING FLAPS FROM 20 UNITS TO 5 UNITS. DURING FAULT ISOLATION, FOUND NR 8 TRANSMISSION WITH (TRIPPED) TORQUE INDICATOR. INDICATOR RESET. HIGH LIFT SYS GROUND TEST CARRIED OUT AND TRIP INDICATORApr 6, 2009 · Boeing 777333ER · Trailing Edge Flap Control SystemSDR CA090323003Drain Line · leaking(CAN) DURING WALKAROUND CHECK, FOUND HYDR LEAK COMING FROM CENTER SYS PRESSURE AND CASE DRAIN FILTER MODULE. LEAK WAS IDENTIFIED AS COMING FROM ONE END OF THE CASE DRAIN TUBE. FURTHER EXAMINATION REVEALED THAT THE LEAK WAS BETWEEN THE TUBE AND THE SWAGED END FMar 20, 2009 · Boeing 777333ER · Hydraulic System, MainSDR CA090204002Engine · failedDURING CRUISE AT FL330, THE LT ENGINE FAILED ABRUPTLY. N1 WINDMILLING AND N2 ZERO. NO RELIGHT ATTEMPT. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ANC. TGB SUSPECTED. ENGINE SB 72-0263R03 IS RELATED.Jan 30, 2009 · Boeing 777333ER · Engine (Turbine/Turboprop)SDR 2009FA0000057Disc · crackedDURING DETAIL INSP OF THE HPT ROTOR STAGE 1 DISC, MULTIPLE CRACK INDICATIONS HAVE BEEN NOTED ON AND BETWEEN THE ID BAYONET TAB FEATURES AT 4 OFF LOCATIONS. THE FPI INDICATIONS HAVE BEEN MEASURED UP TO 0.050 INCH IN LENGTH. THIS HAS BEEN CAUSED BY THE MATING Jan 16, 2009 · Boeing 777* · Turbine SectionSDR CA080917005Engine · vibration(CAN) IN CRUISE, THE FLIGHT EXPERIENCED A NR 1 ENGINE VIBRATION. THE ENGINE CONTINUED OPERATING NORMALLY BUT WITH VIBRATION. THE FLIGHT DIVERTED TO FAIRBANKS, ALASKA. AN ENGINE HAS BEEN SCHEDULED AND TOOLS, PARTS AND MANPOWER ARE CURRENTLY BEING SHIPPED TO Sep 10, 2008 · Boeing 777* · Engine (Turbine/Turboprop)
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