Pratt & Whitney PW2037
Service difficulty reports · 12,809
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 = 'PW2037' 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.
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 = 'PW2037' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA2018122103587Stator · burnedCLIMBING THROUGH FL390, RIGHT ENGINE FAILED. SHUTDOWN RIGHT ENGINE PER QRH. BEFORE ACCOMPLISHING PROCEDURE CAPTAIN NOTED LACK OF OIL PRESSURE AND FUEL FLOW SHOWED 0 , 0. REPLACED RH ENGINE EEC ALTERNATOR (N2 TRANSDUCER) ROTOR AND STATOR PER AMM 73-21-05-4SDR DALA2018121007115Fuel Control · malfunctionedSHIP 695 - ATO - DUE TO LEFT ENGINE DID NOT REACH T/O POWER. CORRECTIVE ACTION: MTC REPLACED FUEL PUMP AND FUEL CONTROL. PERFORMED REQUIRED ENGINE RUNS. AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA2018120657074Pump · making metal(AIRCRAFT 669, L/P 5098942) EICAS MESSAGE L HYD PUMP QRH PROCEDURE FOLLOWED. T/S PER B757 AMM 29-11-00. FOUND METAL IN PRESSURE AND CASE DRAIN LINES, ALSO FOUND METAL IN FILTER MODULE. INSPECTED PTU FILTER MODULE, NO CONTAMINATION FOUND. REMOVED EDP PER B757 ASDR DALA2018111436624Converter · contaminated(AIRCRAFT 6801, L/P 3751740) VERY STRONG WET SOCK SMELL FROM AIR CONDITIONING SYSTEM ON APPROACH. PERFORMED BSI OF THE 2.5 BLEED PORT FINDINGS TURNED OVER TO LEAK AND MCC. FOUND EVIDENCE OF OIL CONTAMINATION IN 2.5 BLEED PORT AREA R/R LT PACK OZON CONVERTER PESDR DALA2018102006261Engine · odorTHERE WAS A RATHER STRONG DIRTY SOCK SMELL IN THE COCKPIT RIGHT AFTER TAKE OFF AND LASTED FOR ABOUT 15 MINS ATL MCC RM 1917Z. SMELL CAME BACK ON DESCENT AND CONTINUED DURING TAXI IN. PERFORMED BOROSCOPE INSPECTION NR 1 AND NR 2 ENG PLUG ON NR 1 ENG 927773 C/W SDR DALA2018101606089Actuator · inoperativeSHIP 6709 - FIRE - ON TAXI OUT WITH BOTH ENGINES RUNNING, LEFT ENGINE STATOR EICAS MESSAGE AND RECEIVED INDICATION THAT THE LEFT ENGINE SHUT DOWN. TOWER NOTIFIED FLIGHT CREW THAT THEY SAW A VISIBLE FIRE FROM LEFT ENGINE, ONE FIRE BOTTLE WAS DISCHARGED. CORRECTSDR DALA2018092705778Engine · odor(AIRCRAFT 6810, L/P 4723748) FA'S REPORTED STRONG " DIRTY SOCK" SMELL ON DESCENT. STRONGER TOWARD THE REAR OF THE AIRCRAFT. SEE LOG PAGE # 4723736. REFERENCE LP 0758072 - REPLACED NBR 2 ENGINE. PERFORMED SECTION II PERMANENT REPAIR PER ERA 571856-14 REV. ORIGISDR DALA2018091005520Engine · seizedDUE TO NR 2 ENGINE FOUND SEIZED FROM IFSD. PERFORM PYLON INSPECTION PER AMM 05-51-10-212-001. NO FURTHER DAMAGE FOUND.SDR DALA2018091005529Engine · failedRT SIDE OF A/C REQUIRES A VISUAL INSP DUE TO NR 2 ENG UNCONTAINED FAILURE. PERFORMED DETAILED VISUAL INSP OF RT SIDE OF A/C PER AMM 05-41.SDR DALA2018080404891Engine · making metalDURING CRUISE A LEFT ENGINE OIL FILTER MESSAGE ILLUMINATED, COMPLIED WITH QRH. LEFT ENGINE SHUTDOWN. DIVERTED. MAINTENANCE FOUND METAL ON CHIP DETECTORS AND OIL FILTER. REMOVED AND REPLACED THE NR 1 ENGINE.SDR DALA2018073104798Fcu · malfunctionedGROUND NOTIFIED LEFT ENGINE WAS SMOKING AFTER SHUTDOWN ALL ENG. GAUGES WERE NORMAL. ENG CONTINUED TO SMOKE UNTIL WE REACHED THE GATE. FOUND FU HIGH PRESS VALVE REMAING OPEN AT ENG SHUTDOWN. R&R FU PER AMM 73-21.SDR DALA2018071304518Fcu · malfunctionedRIGHT ENG REPORT OF FLAME AND SMOKE ON SHUTDOWN. R&R FUEL CTL MM 73-21 NEED LEAK/HIGH PWR RUN. FOUND NO OTHER EVIDENCE OF LEAKAGE.SDR DALA2018071604499Engine · malfunctionedTOXIC FUMES IN COCKPIT COPILOT FELT DIZZY AND HAD TO GO ON O2. DIVERTED INTO MCO. REPLACED NR 1 ENG ON W/C 7100-9902E-01.SDR DALA2018070904429Blade · damagedDURING BORESCOPE INSPECTION OF ESN 16445, FOUND ONE 3RD STAGE LPT BLADE WITH SULFIDATION, APPARENT LOSS OF MATERIAL AND CORROSION GROWTH THROUGH THE BLADE. PER AMM 72-00-00-803-POO. THIS CONDITION REQUIRES THE ENGINE TO BE CHANGED. THE NR 1 ENGINE S/N 16445 HASDR DALA2018062904288Engine · malfunctionedIFSD & DIV - DUE TO STATUS MESSAGES RT ENGINE SEC CONT AND RT ENGINE PRI CONT CAME ON AT FL370. DURING CLIMB TO FL390 THRUST LEVERS ADVANCED ALL ENGINE PARAMETERS RED LINED AND ENGINE UNRESPONSIVE TO THROTTLE COMMANDS A LOUD BANG AND YAW WAS EXPERIENCED, FOLLSDR DALA2018070304357Fuel Control · faultyNR 1 ENGINE SMOKING EXCESSIVELY AT SHUTDOWN. FUEL SMELL REPORTED BY GROUND CREW AND PASSENGERS. REMOVED & REPLACED NR 1 ENGINE FUEL CONTROL PER AMM 7321. RAN ENGINE TO PWR INCLUDING ACCEL CHECKS. NO SMELL OR ODORS IN CABIN. ENGINE CHECKS NORMAL PER AMM 71-00.SDR I5PA201806250002Igniter · malfunctionedRT ENG WILL NOT IGNITE USING NR 1 IGNITER. LT ENG IGNITES NORMALLY USING NR 1 IGNITER.SDR DALA2018051753363Shutoff Valve · faultedABORTED TAKEOFF BELOW 80 KNOTS DUE TO THE CREW REPORTING THAT THEY LOST THE RT BLEED SYS. ALSO REPORTED THAT DURING ENGINE START ON BOTH ENGINES, THE BLEED LIGHTS FLICKERED. DURING ADVANCING THE THROTTLES, BOTH BLEED LIGHTS REMAINED OUT AND THE BLEEDS STABILISDR DALA2018050102975Transmitter · separatedDURING TAKEOFF RIGHT ENGINE ROLLED BACK TO SUB IDLE. THE TAKEOFF WAS ABORTED AT 70 KNOTS. R & R THE NR 2 ENGINE FUEL CONTROL, FUEL PUMP, AND EEC. REMOVED AND REINSTALLED THE ORIGINAL PT2/TT2 PROBE IAW AMM 73-21. MTC FOUND FUEL FLOW TRANSMITTER HOUSING SEPARSDR DALA2018041502576Generator · failedLEFT GENERATOR FAILURE WITH ASSOCIATED EICAS AMBER MESSAGE. FOLLOWED QRH PROCEDURES. RESET ONCE, NO LUCK, STARTED APU & CONTINUED ON TO DESTINATION. R & R THE C901 LEFT GEN CIRCUIT BREAKER IAW AMM 24-22. 927856. PERFORMED IDG ADJUSTMENT TEST IAW AMM 24-11-0SDR DALA2018041602508Engine · bird ingestionAIR TURNBACK AT APPROXIMATELY 1000 FT AGL AFTER TAKEOFF, HEARD A LOUD BANG FOLLOWED BY AN ODOR OF SMOKE AND MOMENTARY FLUCTUATION ON THE RIGHT ENGINE. RAN QRH AND RETURNED TO DEPARTURE. MAINTENANCE FOUND EVIDENCE OF BIRD STRIKE. REPLACED 1ST STAGE BLADE SET SDR DALA2018040902300Line · leakingDURING CRUISE, OIL QUANTITY ZERO, OIL PRESSURE DROPPED INTO RED AND LT ENGINE OIL LIGHT ON. EICAS MESSAGE FOR THE LT ENGINE OIL PRESSURE LOW. DIVERTED. ENGINE WAS NOT SHUT DOWN. THE LT ENGINE CHIP DETECTOR AND OIL FILTER CHECKED CLEAN. SERVICED AND RAN ENGINESDR DALA2018022201111Throttle · unresponsiveCREW PERFORMED AN AIR TURNBACK DUE TO THE LEFT ENGINE THROTTLE UNRESPONSIVE. TAKEOFF POWER WAS NORMAL. REPLACED THE EEC, FCU, AND FUEL PUMP. BURNER PRESSURE MOISTURE TRAPS AND MANIFOLD LINE INSPECTED FOR CONTAMINATION. IDLE RUNS COMPLETE, HIGH POWER RUNS REQUSDR DALA2018020100602Engine · vibrationNR 2 ENGINE VIBRATION DURING CLIMB OUT, N1 1.5 AS POWER INCREASED, VIBRATION INCREASED. R & R TCC AIR VALVE IAW AMM 75-24. R & R THE ENGINE OIL FILTER AND CHECKED CHIP DETECTORS, NO METAL. PERFORMED LPC BOROSCOPE 6 THRU 17 STAGE. HPT 1-3 STAGE; LPT 3RD STSDR DALA2017122608896Pma · failedDIVERTED DUE TO LEFT ENGINE HAD AN IN FLIGHT SHUTDOWN. FOUND THE LEFT ENGINE PMA FAILED. PMA REPLACED, AND RUN-OUT INSPECTIONS COMPLETED. HIGH POWER RUNS COMPLETED AND NO LEAKS.SDR DALA2017101807716Engine · smokePERFORMED AN AIR TURN BACK TO DEPARTURE, DUE TO SMOKE IN THE MAIN CABIN. PERFORMED A HIGH POWER ENGINE RUN AND CONFIRMED SMOKE CAUSED BY THE NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE.SDR DALA2017101307501Engine · failedREJECTED TAKEOFF AT APPROXIMATELY 70 KNOTS, THE RIGHT ENGINE COMPRESSOR STALL. FIRE CREWS CONFIRMED NO FIRE. TAXI BACK TO GATE WAS UNEVENTFUL. FOUND METAL IN THE TAIL PIPE AND THE FAN SEIZED. REMOVED AND REPLACED THE NR 2 ENGINE. OPS AND LEAK CHECKED GOOD.SDR DALA2017100607321Fuel Control · malfunctionedREACHING FL390, AFTER LEVEL OFF, LEFT ENGINE EXPERIENCED TWO SEPARATE THRUST REDUCTIONS WITH ACCOMPANYING AIRCRAFT VIBRATIONS. AFTER EACH SEPARATE REDUCTION & VIBRATION, THE ENGINE RECOVERED NORMAL OPS. NO LIMIT EXCEEDED AND MC NOTIFIED. COMPLETED QRH PROCESDR DALA2017090700001Engine · fireLEFT ENGINE FIRE AFTER TAKEOFF, RETURNED TO DEPARTURE. REPLACED THE LEFT ENGINE IAW AMDS 7100-9902E.SDR DALA2017083006447Unknown · odorAT FL390 ANTI-ICE SELECTED ON, STRONG DIRTY GYM SOCK ODOR FOR 15 MINUTES. OPENED LT AND RT ENGINE COWLS IAW AMM 71-11 FOR BOROSCOPE. NO LEAKS FOUND. R & R THE LT AND RT RECIRCULATION FAN FILTERS IAW AMM 21-25. COMPLIED WITH NO GO ODI CHECKLIST, NO FAULTS NOTESDR DALA2017073105889Circuit Breaker · failedLT ENGINE ANTI ICE CIRCUIT BREAKER TRIPPED. FOUND HIGH STAGE PILOT REGULATOR DAMAGED. REMOVED AND REPLACED THE HIGH STAGE PILOT IAW AMM 36-11. REMOVED AND REPLACED THE CIRCUIT BREAKER C-27 IAW BSWPM CHAPTER 20. HIGH STAGE PILOT REGULATOR CHECKED GOOD IAW ASDR DALA2017072505675Hydraulic Line · leakingFLT 1149 DTW-LAX, LOSS THE LEFT HYD SYSTEM QUANTITY REQUIRING THE MLG TO BE EXTENDED ALTERNATELY. FOUND LEAK FROM PRESSURE FLEX HOSE MPN AS115-06-0172 AT NLG DOOR ACTUATOR . REPLACED HOSE NO LEAKS, REPLACED PTU, EDP AND ALL FILTERS OK FOR SVC.SDR DALA2017090600003Mount · damagedDURING THE ACCOMPLISHMENT OF CMM 71-21-15, REPAIR 1-2, THE SHAFT END JOURNAL OF THE SUBJECT FORWARD ENGINE MOUNT BEAM REQUIRED MACHINING BELOW THE REPAIRABLE LIMIT IN ORDER TO COMPLETELY REMOVE PREVIOUS CHROME PLATING. THE SHAFT END JOURNAL IS BELOW THE MINIMUSDR DALA2017060504509Engine · making metalATB, IFSD, OPERATING ON FLIGHT 889, ATL TO RDU, CLIMBING THROUGH 13K FEET, HAD AN UNCOMMANDED LEFT ENGINE SHUT DOWN WITH A LOUD BANG. EGT AND OIL TEMPS WERE IN THE RED. THE LEFT FIRE HANDLE WAS PULLED. MTC FOUND METAL IN THE TAIL PIPE REQUIRING ENGINE CHANGE. SDR DALA2017053004363Eec · malfunctionedDIVERTED DUE TO A RT ENGINE ROLL BACK WITH SMALL COMPRESSOR STALLS. ENGINE WAS NOT SHUT DOWN. FOUND NUMEROUS EPCS MESSAGES RELATED TO THE EEC. ENGINE INSPECTIONS PERFORMED. BORESCOPE INSPECTION PERFORMED. ALL CHECKED GOOD. EEC AND THE 14TH STAGE BLEED CONVSDR CALA2017052401557Engine · fireDURING TAXI FLAMES WERE REPORTED TO BE EMANATING FROM THE NR 2 ENGINE TAILPIPE.. THE ENGINE WAS SHUTDOWN. EMERGENCY WAS DECLARED. PERFORMED STEP 6 & 7 FROM NTSB. PERFORMED GVI OF NR 2 ENGINE AND SURROUNDING AREA FOR EVIDENCE OF FIRE DAMAGE. FOUND NO EVIDSDR DALA2017052504286Sensor · malfunctionedAFTER SELECTING ENGINE ANTI-ICE, LEFT ENGINE BLEED OFF EICAS MESSAGE. WITH OFF LIGHT, FOLLOWED QRH AND IT REOCCURRED WITH FUMES THROUGHOUT CABIN. TURNED ENGINE ANTI-ICE OFF AND RESET WORKED. R & R 450 DEG TEMP SENSOR, AND THE FAN AIR TEMP SENSOR, ALSO THE FASDR DALA2017041503164Inlet · damagedFAN INLET DAMAGED AT THE 5 AND 7 O`CLOCK POSITIONS. INSTALLED A REPAIR IAW ERA 480335-14MA, REV B, SECTION 1.SDR DALA2017041503165Acoustic Liner · damagedNOSE COWL ACOUSTICAL LINER DAMAGED IN 6 PLACES. INSTALLED PERMANENT REPAIR PER ERA363449-14MA.SDR DALA2017012600657Engine · icedEXPERIENCED ONE ICE CRYSTAL ICING (ICI) EVENT DURING WHICH AN ENGINE EXPERIENCED AN HPT SEIZURE IN-FLIGHT. COMPLIED WITH SECTION 1 AND 2 OF ERA 554584-14 REV ORIG.SDR DALA2016121309868Engine · making metalPERFORMED AN IN-FLIGHT SHUTDOWN ON THE NR 2 ENGINE DUE TO RIGHT ENGINE OIL FILTER MESSAGE. MAINTENANCE FOUND METAL CHIPS ON THE NR 3 BEARING MCD. ENGINE CHANGED.SDR DALA2017032702457Shaft · undersizeDURING THE ACCOMPLISHMENT OF CMM 310N3020 (71-21-15) REPAIR 1-2, THE SHAFT END JOURNAL OF THE FORWARD ENGINE MOUNT BEAM REQUIRED MACHINING BELOW THE REPAIRABLE LIMIT IN ORDER TO COMPLETELY REMOVE PREVIOUS CHROME PLATING. THE SHAFT END JOURNAL OF THE PART MEASUSDR DALA2016091606714Rotor · cokedWHILE IN CRUISE, CREW REPORTED HEARING LOUD BANG, FOLLOWED BY ENGINE ROLLBACK AND SHUTDOWN. ACFT DIVERTED. CREW DECLARED AN EMERGENCY. MAINTENANCE FOUND PMA ROTOR AND STATOR COKED WITH OIL AND SCORED. PMA STATOR, ROTOR, AND CARBON SEAL WERE REPLACED. TRENSDR DALA2016082306190Engine · power lossPERFORMED RTO DUE TO RIGHT ENGINE ROLL BACK AFTER THROTTLES ADVANCED. REPLACED SVA ACTUATOR, FCU AND FUEL PUMP. INSPECTED WIRING, PMA, PB SENSE LINE AND MANIFOLD. ENGINE TESTS AND HIGH POWER RUNS PERFORMED.SDR DALA2016080505894Engine · smokeDURING TAXI OUT, NOTIFIED OF SMOKE COMING FROM LEFT ENGINE. RETURNED TO GATE. MAINTENANCE FOUND OIL IN THE TAILPIPE. NO EVIDENCE OF FIRE. NR 4 BEARING SUSPECTED. REMOVED AND REPLACED NUMBER 1 ENGINE (2016-00454).SDR CALA2016072995598Frame · corrodedCORROSION ON FRAME BS 1680, BL 0 JUST FWD OF AFT WASTE PAN. R & R THE FRAME IAW DWG 146N1032 AND SRM 51-40-05,PAR.4 FIG.2 AND 51-10-02,PAR.4 & 7, FIG.3,8,12 AND DWG 146N1025SDR DALA2016072705689Compressor · damagedCREW PERFORMED AIR TURN BACK DUE TO RT ENGINE COMPRESSOR STALL. MTC PERFORMED BOROSCOPE AND FOUND 16TH STAGE COMPRESSOR DAMAGE. REMOVED AND REPLACED ENGINE.SDR CALA2016072595586Skin · gougedRIGHT FUSELAGE BS 660 AFT OF FWD CARGO DOOR HAS SMALL GOUGE IN SKIN. REPAIRED IAW ECRA 5330-05753.SDR DALA2016072505509Engine · failedWHILE TAXIING TO THE GATE, WHITE SMOKE WAS OBSERVED FROM BOTTOM OF THE ENGINE AND TAILPIPE FIRE OCCURRED AFTER SHUTDOWN LEFT ENGINE. ON INSPECTION FOUND OIL IN TAIL PIPE. R & R ENGINE.SDR CALA2016072195570Control Module · malfunctionedABORTED TAKEOFF APPROACHING 125 KTS DUE TO SPOILER ALERT MESSAGE. REQUESTED FIRE/RESCUE FOR HOT BRAKES, TOWED TO GATE REPLACED SPOILER CONTROL MODULE 1R IAW MM 27-09-00, ACCOMPLISHED TAKEOFF CONFIG WARNING CARD MODULE TEST, AND LANDING CONFIG WARNING CARD MOD
Back to Pratt & Whitney PW2037