Pratt & Whitney PW2040
Service difficulty reports · 2,201
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 = 'PW2040' 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 = 'PW2040' 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 CALA2014021790381Module · faultyK CTR RESERVOIR LOW PRESS LIGHT IS ILLUMINATED AFTER HYD RESERVOIR DRAINED TO SERVICEABLE INDICATION. REPLACED RESERVOIR PRESSURIZATION MODULE IAW MM 29-11-16. CHECKED NORMAL, SECOND PRESS SWITCH CHANGED ON CTR RESERVOIR.SDR CALA2014021790390Recorder · faultyFLT RECORDER OFF, LIGHT ILLUMINATED WITH LT ENG RUNNING & SWITCH IN NORMAL. REPLACED FDR IAW MM 31-3 1-01-401.SDR CALA2014021790392Pan · gougedNR 4 LT PAX DOOR PAN GOUGED .025 AT DEEPEST POINT & IS .5 AWAY FROM CLOSEST RIVET. BLENDED AFFECTED AREA, AFTER BLEND THE DEEPEST POINT MEASURES .027, OK TO CONTINUE IN SERVICE FOR 50HRS OR 25 CYCLES IAW SRM 52-10-01 ALLOWABLE DAMAGE 2 PG 101-102.SDR CALA2014021790393Pan · gougedFOUND BUTTERFLY HANDLE PAN ASSEMBLY GOUGED ABOVE & BELOW HANDLE. NEEDS PAN ASSEMBLY PCN170-5402 IPC 52-11-01-007 ITEM 465.SDR CALA2014021790394Light · inoperativeLT AFT OVERWING DOOR BLUE EXIT LIGHT INOPERATIVE. REPLACED LIGHT IAW MM 33-51-10.SDR CALA2014021790396Light · inoperativeEMERGENCY EXIT LIGHT STRIP FROM ROW 30 TO 32 ILLUMINATION INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP & POWER INVERTER, OPERATIONS CHECKED OK.SDR CALA2014021790391Rivet · damagedSTATIC DISCHARGE DURING DESCENT. LT SIDE OF AIRCRAFT ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW MM 05-51-19. FOUND 61 RIVETS, LT OTBD ELEVATOR & CTR VHF WITH LIGHTENING DAMAGE, ALL DAMAGE DOCUMENTED.SDR CALA2014021790395Unknown · malfunctionedUNCOMMANDED YAW LT & RT ON CLIMB.SDR CALA2014021290364Cooling Fan · defectiveSULFUR OZONE LIKE ODOR IN CABIN. CREW HAS RUN QRH CHECKLIST WITH NO EFFECT, AT THIS POINT FLIGHT IS CONTINUING ON & CREW WILL MONITOR. PERFORMED SMOKE FUMES IN CABIN CHECK IAW AMM 05-51-56 & FOUND PRIMARY EQUIPMENT COOLING FAN BLADES RUBBING IN CASING WITH SSDR CALA2014021390373Frame · damagedDAMAGE TO FAIRING FRAME ASSEMBLY AT BS 900. ACCOMPLISHED RII REQUIREMENT OF SMC15, CHECK ACCOMPLISHED.SDR CALA2014021290365Acoustic Panel · delaminatedNR 2 ENG RT THRUST REVERSER ACOUSTIC PANEL AT 12:00 POSITION DELAMINATED IN CTR. INSTALLED REPAIR DOUBLERS TO THE UPPER BIFURCATION PANEL IAW AMM 78-31-93.SDR CALA2014021290366Seal · out of positionVIBRATION AFTER TAKEOFF. CREW FELT AIRFRAME VIBRATION STRONG ON TO THRU 5500 FEET WHEN IT DISSIPATED. CABIN CREW ALSO FELT THE SAME VIBRATION ON FINAL APPROACH, VIBRATION RETURNED IN THE AFT CABIN. FOUND SEAL AT PANEL 191DL NOT FLUSH WITH WING UPPER SURFACESDR CALA2014021090345Light · brokenEMERGENCY ESCAPE PATH LIGHTING STRIP 32C BROKEN. REPLACED POWER FEED CABLE AT SEAT 34 ABC. REPLACED CLEAR COVER FROM SEAT 31 AFT TO END OF EMERGENCY EXIT LIGHT TRACK. REPLACED ONE LIGHT AT SEAT 34, OPERATIONS CHECKED NORMAL.SDR CALA2014021090347Wire · damagedRT WING FUELING PANEL DOOR INBD LIGHT INOPERATIVE. WIRING PULLED OUT OF LIGHT HOUSING. EXPOSED CONDUCTOR WIRE TOWARDS WING AREA, THIS EXPOSED WIRING WAS AN UNAPPROVED REPAIR BY TWISTING THE WIRES TOGETHER WITH BLACK ELECTRICAL TAPE AS THE INSULATOR. REMOVEDSDR CALA2014021090343Attach Bolt · damagedNR 2 ENG STRUT UPPER LINK FITTINGS TO BE REMOVED FOR INSPECTION. REMOVED NR 2 ENG STRUT UPPER LINK ATTACH BOLT & FUSE PIN & REPLACED WITH NEW PARTS IAW AMM54-51-02SDR CALA2014021090344Case · damagedREPLACE NR 2 ENG DUE TO IMPACT DAMAGE TO FWD FAN CASE FLANGE. REMOVED NR 2 ENG IAW MM71-00-02 CONT OF AMIS ITEM 8146002, INSTALLED NR 2 ENG IAW AMM71-00-02.SDR CALA2014020690308Light · inoperativeOFF WING ESCAPE SLIDE LIGHT INOPERATIVE LT SIDE FWD. R & R LIGHT BULB, OPERATIONS CHECKED GOOD IAW AMM 33-51-06.SDR CALA2014020690323Engine · oil consumptionNR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMITS. ACFT TO BE REMOVED FROM ETOPS OPERATION UNTIL A POSITIVE FIX IS FOUND & OIL CONSUMPTION RETURNS TO NORMAL LIMITS.SDR CALA2014020390295Charger · inoperativeEMERGENCY EXIT LIGHT JUST FWD OF RT AFT GALLEY DOOR INOPERATIVE. REPLACED CHARGER M108 18 IAW MM 33-51-09, OPERATIONS CHECKED NORMAL.SDR CALA2014020690310Girt Bar · out of adjustRT AFT ENTRY DOOR INDICATED ON EICAS. CLEANED & ADJUSTED GIRT BAR.SDR IPXA2014021481914Frame · dentedDURING INSPECTION 4C16, AFT CARGO BAY, FRAME BS 1340 ABOVE S26R DENTED. ACCOMPLISHED FRAME REPAIR IAW SRM 53-00-07, REPAIR 5, DETAIL-1.SDR CALA2014013190270Battery Pack · dischargedDOOR EMERGENCY EXIT MARKERS AT DOOR 1 RT & LT & FLOOR STRIP BY FWD CLOSET INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-07, OPERATIONS CHECKED OK.SDR CALA2014012990265Apu · shutdownWHILE STARTING THE NR 2 ENG, THE APU AUTO-SHUT DOWN. CREW DISCONTINUED NR 2 ENG START ATTEMPT. WITH THE ASSISTANCE OF THE CREW, THEY RESTARTED THE APU, ACP SECOND START ATTEMPT USING THE APU AIR SOURCE, SECOND NR 2 ENG START ATTEMPT WAS NORMAL, APU FUNCTION SDR CALA2014013190274Unknown · malfunctionedFUEL ENTERS CTR FUEL TANK WITH FUEL VLVS IN SHUTOFF DURING FUELING.SDR CALA2014013190275Warning System · faultyRT HYD SYS PRESS LIGHT INTERMITTENT WITH HYD PUMPS OFF.SDR CALA2014012790239Cover · looseEMERGENCY FLOOR LIGHTING STRIP AT ROW 20 LOOSE. CLEAR PLASTIC COVER STRIP IS OFF. INSTALLED COVER STRIP EMERGENCY EXIT LIGHT.SDR CALA2014012890247Angle · damagedAFT CARGO COMPARTMENT DOOR LOWER SILL LT ANGLE HAS FOUR EACH DENTS & GOUGE BS 1403- 1394 RBL 22. REPAIRED AFT CARGO DOOR LOWER SILL FROM BS 1392 TO BS 1428 IAW UAL ECRA 5360-01359.SDR CALA2014012890248Floorbeam · crackedMAIN CABIN FLOOR BEAM BS 660 LBL 45 CRACKED IN RADIUS. REPAIRED MAIN CABIN FLOOR BEAM AT BS 660 LBL 38 TO LBL 60 IAW UAL ECRA 5300-01829.SDR CALA2014012890249Warning Light · false activationLT AFT ENTRY DOOR LIGHT AT 90 KTS TAKEOFF ABORTED, NO AUTO BRAKES. VERIFIED DOOR IS CLOSED. ACCOMPLISHED HIGH ENERGY STOP IAW 05-51-14MM INSPECTION.SDR CALA2014012890254Vsi · failedVERTICAL SPEED INDICATOR SHOWS OFF FLAG AT ALTITUDE, STOPPED WORKING.SDR CALA2014012790240Lens · unsecureEXIT LIGHT STRIP RIPPED FROM FLOOR IN LAST ROW. SECURED EMERGENCY EXIT LIGHT LENS.SDR CALA2014012790241Radio Altimeter · malfunctionedCTR RADAR ALTIMETER FLAG CYCLES INOPERATIVE. RESET CTR RADIO ALTIMETER, OPERATION TESTED OK IAW MM 34-33-00.SDR CALA2014012790246Unknown · malfunctionedFLIGHT DIVERTING TO SFO DUE TO A CTR HYD SYS QTY AT ZERO.SDR CALA2014012790236Wire · damagedCABIN CHIMES INOPERATIVE WHEN CALLING FROM HANDSETS. CALL LIGHTS DO ILLUMINATE, POSITION 1 01 FWD, 03 MID, 05 AFT & 08 ALL. REPAIRED WITH SOLDER BLACK WIRE POSITION 3 & BLUE WIRE POSITION 2 AT L1 DOOR HANDSET CONNECTOR, ACCOUNT PA & INTERPHONE ALSO INOPERATISDR CALA2014012790237O-Ring · damagedRT MAIN TANK TRANSFERRED INTO CTR TANK. WHEN MAINS DROPPED TO ABOUT 10.0, FUEL BEGAN DRAINING FROM THE RT TO CTR TANK. FOUND LEAKING COUPLING IN FUEL FEED LINE OTBD OF RT CTR OVERRIDE BOOST PUMP, REPLACED O RINGS IN COUPLING, SYS CHECKED NORMALSDR CALA2014012790238Indicator · inaccurateFUEL QUANTITY INDICATIONS ON UNDER WING PANEL ARE INACCURATE, COCKPIT GAUGES OK.SDR CALA2014012490218Light · brokenEMERGENCY EXIT LIGHT STRIP BROKEN AT DOOR, FWD AFT LAVATORY. PERMANENT REPAIR SPLICE INSTALLED ICW AMM 33-51-96, OPERATIONS OK.SDR CALA2014012490221Floorbeam · crackedMAIN CABIN FLOOR BEAM BS 700, LBL45 CRACKED IN RADIUS. REPAIRED MAIN CABIN FLOOR BEAM AT BS 700 FROM LBL 8 TO LBL 60 IAW UAL ECRA 5300-01823 ON NON-ROUTINE 38346.SDR CALA2014012490222Unknown · faultyDISCONNECTED LAVATORY SMOKE DETECTORS & BREAKER STILL POPS, SMOKE DETECTORS ARE STILL DISCONNECTED, WITH FWD LAVATORY DISCONNECTED, CB STAYS IN. CONNECTOR STILL DISCONNECTED.SDR CALA2014013190279Oil System · overtempHIGH OIL TEMP NR 2 ENG. EMERGENCY DECLARED & EQUIPMENT REQUESTED.SDR CALA2014012490224Slider · lack of lubeDOOR 4R LEVER WILL NOT REACH DISARM POSITION. LUBED GIRT BAR SLIDERS, ARM DISARM HANDLE MOVES FREELY & DOOR ARMS & DISARMS.SDR CALA2014012190201Warning System · false activationMAIN BATTERY CHARGER STATUS MESSAGE. DURING PREFLIGHT & STANDBY POWER CHECK, FLIGHT CREW NOTED STATUS MESSAGE APPEARED, ABLE TO ERASE MESSAGE & ACCOMPLISHED MAIN BATTERY CHARGER CHECK. UNABLE TO DUPLICATE MESSAGE AGAIN AFTER NUMEROUS TRIES. REPLACED RELAY KSDR CALA2014012190202Idg · faultyLT ENG GENERATOR DRIVE LIGHT NOT ILLUMINATED WITH LT ENG SHUT DOWN. FOUND IDG SERVICED PROPERLY. CLEANED CANNON PLUG. STARTED ENG IAW JRH 2-5-1 & CHECKED IDG IAW JRH 2-5-5. SHUT DOWN ENG & DRIVE LIGHT IAW MM 24-11-00. COMPLIED WITH MEL 2411C GEN DRIVE LIGHSDR CALA2014012190203Light · inoperativeSYS FAIL LIGHT FOR FIRE SYSTEM IS NOT ILLUMINATED DURING LIGHT TEST.SDR CALA2014012190204Generator · trippedCREW REPORTS LT GENERATOR TRIPPED OFF & WILL NOT RESET.SDR CALA2014012090188Static Line · unsecureDOOR 1R UNABLE TO ARM, FOUND STATIC LINE EXTENDED IN GIRT MECHANISM. SECURED STATIC LINE IAW SERVICE TIP 25-66-0 1, DOOR ARMS NORMALLY.SDR CALA2014012090189Light · defectiveSLIDE INDICATOR AT DOOR 4R TOO DIM. REPLACED BULBS, OPERATION NORMAL.SDR CALA2014011590155Bpcu · faultyCREW REPORTED THAT 1.5 HRS INTO FLT, FLT ATTD REPORTED NO PWR TO AFT GALLEY. AT 2.0 HRS INTO FLT BOTH LT & RT UTILITY BUSSES TRIPPED OFF. IAW FIM CREW CYCLED UTILITY BUS SWITCHES ALL PWR RESTORED & OPERATIONS NORMAL. REPLACED BPCU IAW MM24-41 -03, SHOOK OUTSDR CALA2014011690164Fire Loop · faultySTATUS MESSAGE ON CLIMB OUT APU FIRE LOOP 2. REPLACED APU UPPER FIRE DETECTOR ELEMENT IAW AMM26-15-02. UNABLE TO DUPLICATE PROBLEM, TESTED OK.SDR CALA2014011490146Housing · leakingENG WAS SHUT DOWN & WIND MILLING APPROXIMATELY 25 MINUTES, OIL PRESS REMAINED ABOVE ZERO & OIL TEMP REMAINED NORMAL, NO VIBRATION NOTED, IAW JRH 2-5-63 FOR WIND MILLING INSPECTION. ACCOMPLISHED WINDMILL INSPECTION IAW AMM 72-00-00 & JRH 2-5-63. FOUND NO DEB
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