GE GE90-94B

Service difficulty reports · 77

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 = 'GE9094B'
  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 QEMY201812140001Disk · crackedAT THE FPI & INSPECTION PROCESS THE LPT STAGE 6 DISK HAS BEEN FOUND CRACKED AND HAS TO BE REMOVED FROM SERVICE EARLY. PART IS AN LLP. CUSTOMER AND OEM NOTIFIED, AWAITING CONFIRMATION FOR RETURN FOR INVESTIGATION.Dec 14, 2018 · N466L · Boeing 777* · Turbine SectionSDR QEMY201807270001Seal · crackedTHE FWD SEAL EXHIBITS A THROUGH CRACK FROM THE OUTER EDGE OF THE STAGE 1 BLADE RETAINER RADIALLY THROUGH TO THE INNER DIAMETER BAYONET. THE CRACK HAS DISTORTED BOTH HALVES OF THE FORWARD SEAL AND IS VISIBLE WITHOUT ANY MAGNIFICATION AIDS.Jul 24, 2018 · Engine (Turbine/Turboprop)SDR ASMF201611015Carbon Seal · leakingCAPTAIN REPORTED THAT DURING APPROACH, THE LEFT ENGINE OIL QUANTITY DECREASED TO 3 QTS WITH ENGINE PARAMETERS NORMAL. THE AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL PERFORMED LEFT ENGINE LEAK CHECK IAW AMM 71-00-00-700-823, AMM 79-00-00-200-800,Sep 25, 2016 · N776AM · Boeing 7772Q8 · Engine Oil CoolerSDR CALA2016081200527Engine · overtempACFT RETURNED TO DEPARTURE, DUE TO NR 1 ENGINE EGT OVERTEMP. NR 1 ENGINE REMOVED AND REPLACED. OPS AND LEAK CHECKED GOOD.Aug 12, 2016 · N76010 · Boeing 777224 · Engine (Turbine/Turboprop)SDR ASMF201606003Brake Assy · overheatedAIRCRAFT REJECTED TAKEOFF AT 100 KNOTS DUE TO AN EVENT OF 1023 DEGREES CELSIUS OF EGTS EXCEEDANCE IN THE FELT ENGINE AND BY NOTIFICATION OF THE AIR TRAFFIC CONTROL OF FIRE EVIDENCE IN THE RT MLG. THE ACFT WAS SENT TO HANGAR AND MAINTENANCE PERSONNEL PERFORMEDApr 17, 2016 · N774AM · Boeing 7772Q8 · BrakeSDR CALA2016010800041Compressor Blade · bulgedCOMPRESSOR STALL ON TAKEOFF LOW SPEED. INLET & EXHAUST INSPECTION OK. ACCOMPLISHED HPC BORESCOPE INSPECTION ON ENG NR 2 STAGE 1 IAW AMM 72-00-00-290-812-G00. FOUND ONE BULGED BLADE, 55% DEFLECTION UPPER LE PORTION. ENGINEERING CALL FOR ENG CHANGE.Jan 8, 2016 · N78005 · Boeing 777224 · Turbine Engine Compressor SectionSDR ASMF201511008Actuator Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE RT ENG FAIL LIGHT TURNED ON WITHOUT ABNORMAL INDICATIONS & DURING THE RT ENG SHUTDOWN, THE EGT EXCEEDANCE WAS SHOWN. PERFORMED FIM 73-11 TASK 815 & FIM 73-22 TASK 815 & 820 PROCEDURES & IDLE POWER OPERATNov 11, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel DistributionSDR ASMF201507018Wire · damagedAIRCRAFT RETURNED TO PLATFORM, DURING LT ENG START, THE FAILURE CODE 73 21 52 51 & 732 152 51 WERE SHOWED & LT ENG NOT STARTED BY TWO ATTEMPTS. PERFORMED REVISION TO LT ENG, DETECTING LT HIGH PRESS FUEL SOV POSITION IN DISAGREE WITH COMMAND POSITION. THE FIMJun 29, 2015 · N776AM · Boeing 7772Q8 · Engine Fuel System WiringSDR CA140911002Slat · failed(CAN) SLAT PRIMARY FAILED ON DOWNWIND LEG. NORMAL APPROACH/LANDING. ASR TO FOLLOW. RESOLUTION PRIMARY SYSTEM TEST FOR FSEU NR 2 CARRIED OUT AS PER MTCE MESSAGE. TEST PASS. FLAP SLAT OPERATION OUT NO FAULTS.Sep 8, 2014 · Boeing 777233LR · Leading Edge Slat Control SystemSDR ASMF201312005Engine · malfunctionedCAPTAIN REPORTED THAT DURING TAKEOFF, THE RT ENG REACHED 1031 CELSIUS DEGREES OF EGT FOR AROUND 2 SECONDS. PERFORMED RT ENG INSPECTION WITH EGT PARAMETERS WITHIN OPERATION LIMITS IAW AMM 71-00-00 & ENG EXCEEDANCE CHECK IAW AMM 71-00-00, TESTED CORRECT.Dec 1, 2013 · N746AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)SDR ASMF201308008Fairing · damagedDURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN RT ENGINE. BIRD STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-18, DETECTING 6 FAIRING DAMAGES AND 2 PANELS WITH 4 IMPACT, BEING WITHIN LIMITS OF OPERATION IAW AMM 71-00-00. PANELS WERE REPAIRED IJul 12, 2013 · N745AM · Boeing 7772Q8 · Wing StructureSDR ASMF201207009Panel · puncturedDURING TRANSIT CHECK, DAMAGE WAS DETECTED IN THE NOSE COWLING SKIN ACOUSTIC PANEL OF THE LT ENGINE, A PUNCTURE 1 X 0.75 INCH BEING OUT OF LIMITS IAW SRM 54-11-01. THE DAMAGE WAS REPAIRED IAW AMX-12-0324-02B, TESTED CORRECT.Jul 31, 2012 · N776AM · Boeing 7772Q8 · Nacelle/Pylon, Main FrameSDR ASMF20110322001Bolt · looseCAPTAIN REPORTED DURING THE DESCENT, THE RT ENGINE VIBRATION REACHED 4.7 OF N2. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK 71-00-00-700-847-G01 DETECTING 6 RT ENGINE FAN WEIGHT BALANCE BOLTS WERE LOOSE AT THE 5, 11, 12, Mar 22, 2011 · N774AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)SDR ASMF201102003Blades · damagedDURING A BORESCOPE INSPECTION OF THE HPC 1ST STAGE BLADES OF RIGHT ENGINE WAS DETECTED FOUR BLADES OF THE HPC 1ST STAGE WITH LEADING EDGE TIP CURLED 45 DEGREES OUT OF LIMITS IAW 72-00-00, PARAGRAPH 5H (8) C (7), PAGE 625; WITH DIMENSIONS OF 1.0 INCHES LENGTH AFeb 14, 2011 · N774AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASMF201012005Sensor · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CRUISE THE ENG OIL FILTER RT LIGHT TURNED ON WITH AN OIL TEMP INDICATION OF 60 CENTIGRADE DEGREES AND OIL PRESSURE INDICATION OF 60 PSI; THE EICAS MESSAGES ENG OIL FILT R AND MX MESSAGES 79-31452, 79-31-31462 AND 7Dec 3, 2010 · N746AM · Boeing 7672Q8 · Engine Oil CoolerSDR ASMF201010007Sensor · damagedACFT PERFORMED AN UNSCHEDULED LANDING, DUE TO DURING CLIMB THE ENG OIL FILTER SENSOR AND ENG OIL FILTER LIGHTS TURNED ON AND DURING CRUISE THE EICAS MESSAGE ENG OIL FILTER WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH 7.20 PROCEDURE, CONFIRMING THE FAILURE. DUROct 20, 2010 · N745AM · Boeing 777222 · Turbine Engine Oil SystemSDR ASMF201008002Pressure Sensor · damagedACFT RETURNED OF FLIGHT DUE TO DURING CLIMB, EICAS MESSAGE AND LIGHT TURNED ON OF ENG OIL FILTER L WAS SHOWN. THE FLIGHT CREW PERFORMED THE QRH ENG OIL FILTER L, R PROCEDURE, CONFIRMING THE FAILURE. MX PERSONNEL REPLACED THE LT OIL DIFFERENTIAL PRESSURE SENSORAug 24, 2010 · N746AM · Boeing 7772Q8 · Engine Oil PressureSDR ASMF201008001Tire · detachedDURING TAKEOFF RUN; A STRONG NOISE WAS HEARD, IECAS MESSAGE OF TIRE PRESS WAS SHOWN AND TIRE PRESS LIGHT TURNED ON, THE TIRE NR 1 WAS DEFLATED AND THE FLIGHT CONTINUED TO MAD IAW FCT 777 (TM) 8.18 (32-40-72-00 PROCEDURE). MX DETECTED MAIN TIRE NR 1 FLOOR DETAAug 19, 2010 · N745AM · Boeing 7772Q8 · TireSDR ASMF201006002Seal · out of positionACFT RETURNED TO DEPARTURE, DURING CLIMB WAS DETECTED A LOAD COMPARTMENT PRESSURIZATION LEAK NOISE. MX FOUND THE FWD ACCESS ELEC DOOR SEAL, UPSIDE DOWN, THE DOOR SEAL WAS REPOSITIONED IAW MM 52-08-00 AND PRESSURIZATION TEST WAS PERFORMED IAW MM 52-00-05, TESTEJun 8, 2010 · N774AM · Boeing 7772Q8 · Passenger/Crew DoorsSDR ASMF20100405Compressor · damagedDURING A BORESCOPE INSP OF THE HPC AND HPT MODULES OF RT ENGINE WERE DETECTED 41 BLADES OF HPC 8TH STAGE AND 23 BLADES OF 9TH STAGE WITH TEARS, NICKS, BENDS AND MISSING MATERIAL FROM THE LEADING TO THE T/E. OPENApr 28, 2010 · N746AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASMF201004001Blades · damagedDURING A BORESCOPE INSP OF THE HPC 1, 4 AND 9 STAGES BLADES OF THE RT ENGINE WAS DETECTED. 1 BLADE OF THE HPC 1ST STAGE WITH L/E TIP CURLED 90 DEGREES OUT OF LIMITS IAW 72-00-00, PARA 5H (L) (7), PAGE 625; WITH DIMENSIONS OF 3.5 INCHES LENGTH AND 1.25 INCHES WApr 12, 2010 · N776AM · Boeing 777222 · Turbine Engine Compressor SectionSDR ASMF20100321001Blade · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENG WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGINE Mar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASMF201004002Blades · damagedDURING A BOROSCOPIC INSP OF THE HPC 1ST STAGE BLADES, VSV AND IGV SYSTEMS OF LT ENGINE WAS DETECTED THE HPC 1ST STAGE WITH A TIP CURLED BROKEN, CAUSING DAMAGES IN THE 1ST, 2ND, 3RD AND 4TH STAGES IAW AMM 72-00-00, PARAGRAPH 5H. THE FINAL REPAIR DETAILS OR ENGIMar 21, 2010 · N745AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR ASM2008F00001Blade · bentDURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIRST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLAAug 3, 2008 · N776AM · Boeing 7772Q8 · Turbine Engine Compressor SectionSDR 2008FA0000472Engine · failedDURING TRANSIT CHECK, THE RT ENGINE WAS DETECTED WITH DAMAGES. MAINT PERFORMED BOROSCOPIC INSPECTION, DETECTING DAMAGES OUT OF LIMITS, SO RT ENGINE WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. (K)Jun 6, 2008 · N745AM · Boeing 7772Q8 · Engine (Turbine/Turboprop)SDR ASMF200806001Sensor · failedAIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, NO DAMAGES WERE DETECTED IAW MM 71-00-00. RIGHT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED Jun 1, 2008 · N745AM · Boeing 7772Q8 · Fuel Controlling SystemSDR 2008FA0000471Sensor · failedAC RETURNED TO DEPARTURE DUT TO RT ENGINE STALLED. MAINT PERFORMED FIM 75-21 TASK 822 AND STALL INSPECTION IN 1ST, 5TH AND 9TH HPC STAGES. NO DAMAGES WERE DETECTED IAW MM 71-00-00. RT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED CORRECT. THE OVERWEIGHTJun 1, 2008 · N745AM · Boeing 7772Q8 · Engine Indicating System
Back to GE GE90-94B