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 IPXA2019041214957Shutoff Valve · failedDIVERSION - L ENG BLEED OFF ILLUMINATED AFTER EAI WAS SELECTED ON DURING FLIGHT AT CRUISE FL 300. L ENG WAS FOLLOWED BY R ENG. L AND R PACK OFF. ACCOMPLISHED CHECKLIST AND DESCENDED TO 10,000 AFTER LOSS OF PRESSURE.REPLACED LT ENG HI PRESS SHUTOFF VALVE REF 36SDR DALA2018101005994Compressor Blade · damagedATB DUE TO RIGHT ENGINE COMPRESSOR STALL DURING CLIMB. MTC INSPECTED ENGINE AND FOUND COMPRESSOR BLADE DAMAGE DURING BOROSCOPE, REMOVED AND REPLACED ENGINE.SDR DALA2018091905658Engine · failedATO/SMKE/FIRE- ON TAKEOFF AT APPROX 140 KNOTS THE LEFT ENGINE FAILED ACCOMPANIED BY SMOKE IN THE FLIGHT DECK. AFTER STOPPING ON RUNWAY THE TOWER REPORTED AN ENGINE FIRE, DISCHARGED TWO FIRE BOTTLE AND WAS GIVEN AN ALL CLEAR BY AIRPORT RESCUE. MAINTENANCE FOUNDSDR DALA2018081004983Gearbox · crackedLEFT ENGINE WAS SHUTDOWN DUE TO OIL PRESSURE LIGHT ILLUMINATED IAW QRH. MAINTENANCE FOUND THE MAIN GEARBOX CRACKED. GEARBOX REPLACED.SDR IPXA2017121224473Engine · failedINSPECTION TYPE:N/ALEFT ENGINE FAILURE ENROUTE FL200 PERFORMED ENGINE FAILURE/SHUTDOWN CHECK LIST ENGINE WAS WITHIN PARAMETERS FOR INFLIGHT START. STARTED NORMALLY AND OPERATED NORMALLY FOR REMAINDER OF FLIGHT.PER FIM 710-05-00-815-806 T/S PER AMM 73-11-10 CHESDR CALA2017092203264Fcu · malfunctionedEICAS MESSAGE FOR CENTER RT FUEL PUMP, RT ENGINE SHUTDOWN. REMOVED AND REPLACED THE FUEL CONTROL UNIT ON THE RIGHT ENGINE IAW AMM 7 3-21-01, OPS CHECKED GOOD . LEAK CHECKED GOODSDR CALA2017031300589Relay · faultySTARTED LEFT ENGINE ALL NORMAL. STARTED RT ENGINE, ALL NORMAL LEFT ENG ROLLED BACK, SHUTDOWN, VISUALLY INSPECTED THE NR 1 ENG INLET AND EXHAUST, INTERROGATED EPCS AND EICAS, NO FAULTS OR DEFECTS NOTED. PERFORMED FIM TASK 73-21-00-815-802-P00, PERFORMED FUELSDR FDEA201609143216Warning Light · illuminatedLEFT OIL FILTER EICAS MESSAGE ILLUMINATED. COMPLIED WITH THE CHECK LIST, INFLIGHT ENGINE SHUTDOWN. DRAINED AND FLUSHED LT ENGINE MAIN OIL TANK, 3RD TIME & REPLACED MAIN ENGINE OIL FILTER IAW 79-21-05-4, 3RD TIME. R & R LT ENGINE LUBRICATION AND SCAVENGE OILSDR IPXA2016081006844Warning Message · illuminatedDURING CRUISE, FL 330 WITH ENG ANTI-ICE ON, RECEIVED A RT ENGINE BLEED VALVE CAUTION AND LIGHT. SECURED THE RT ENGINE BLEED VALVE IAW QRH PROCEDURES. APPROX 5 MINUTES LATER, RECEIVED A LT ENGINE BLEED VALVE CAUTION AND LIGHT AGAIN. COMPLIED WITH QRH PROCEDUSDR FDEA201606292194Stringer · corrodedFWD CARGO PIT, STR 22L CORRODED BETWEEN FRAME BS 700-720. REMOVED CORROSION IAW SRM-51-10-02-0G, NO ALLOWABLE DAMAGE IAW SRM. FABRICATED AND INSTALLED STRINGER FILLER AND HAT SECTION REPAIR, STA 660-STA 752, S22L IAW-SRM-53-00-03-2R, REPAIR 2, CAT-A, REPAIR.SDR CALA2016061795461Slide · unwanted deployDURING OPERATION OF DOOR, 1R SLIDE INADVERTENTLY DEPLOYED. R & R DOOR 1R ESCAPE SLIDE UP TO STEP 3, E 13, REF AMM 25-66-01.SDR FDEA201606031793Engine · malfunctionedRIGHT ENGINE FAILED AT 4000 FT. COMPLIED WITH QRH, SHUTDOWN ENGINE. OIL PRESSURE WAS 25 PSI AT SHUTDOWN. EGT INCREASED BUT WAS NOT IN THE RED. NR 1 ENGINE OPERATED NORMALLY, NO EXCEEDANCE. RUMBLING NOISE FROM RT ENGINE. RT ENGINE PARAMETERS BEGAN TO ROLLSDR IPXA2016062405015Skin Panel · brokenINSPECTION TYPE:SEG 1, LEFT WING LOWER SURFACE SKIN ABOVE PYLON PANEL 435BR IS CHAFED. REPAIRED WINGS, LOWER SKIN PANEL REPAIR BETWEEN WSTA 285.65 AND WSTA 313.50 AT STR 8 IAW EA 757-5724-27-A222 AND EO NR B757-5730-61103-A.SDR I5PA2016050275701Window · crackedON DESCENT INBOUND, AIRCRAFT EXPERIENCED R1 WINDOW OUTER PANE HAD CRACKED. EMERGENCY PROCEDURES WERE FOLLOWED AND ACFT LANDED IN THE NEAREST SUITABLE AIRPORT, SAFTELY.SDR CALA2015102794722Battery Pack · dischargedEMERGENCY LIGHTS BATTERY POWER SUPPLY, M00730, FAILED. R & R BATTERY PACK & POWER SUPPLY AT M00730. PERFORMED OPERATIONS TEST CHECK FOUND NORMAL IAW AMM 33-51-07 & AMM 33-51-00.SDR FDEA201510203281Oil System · overservicedAFTER TAKEOFF, SMOKE IN COCKPIT & COURIER AREA & MAIN CARGO FIRE EICAS MESSAGE. TURNED BACK, MAIN CARGO FIRE ALERT WENT AWAY & SMOKE CLEARED. ENGINE OIL QUANTITIES 1120Z ARE 23 LT & 22 RT. NO ODORS OR SMOKE AT THIS TIME. RAN NR 1 ENGINE IAW JRH. NOTED OPESDR FDEA201510203290Oil System · overservicedON TAKEOFF HAD SMOKE IN COCKPIT, COURIER AREA & MAIN CARGO, FIRE EICAS MSG, TURNED BACK. MAIN CARGO FIRE ALERT WENT AWAY & SMOKE CLEARED BY THE TIME WE WERE ON THE GND. NR 1 ENG, FOUND ENG OIL TO BE OVER SERVICED, NOTED OIL SPILLING OUT OF SCUPPER WHEN OIL CSDR IPXA2015081192256Intercostal · corrodedINSPECTION TYPE:C, AFT CARGO, BS 1400-1420, LBL 2.9 INTERCOSTAL CORRODED. R & R INTERCOASTAL, PN:146N5425U19 WITH BACR15FV6, BATCH 0001771118, BACR15FT6, BATCH 0002699949 AND BACB130MY6, BATCH 0002779208 IAW DWG 146N145399 AND 146N3300 AND IAW SRM 51-40-02.SDR IPXA2015072891654Eec · malfunctionedFLAMES SHOOTING OUT OF LT ENGINE DURING START REPORTED BY A MECHANIC. CREW REPORTED NO ABNORMAL INDICATIONS DURING ENGINE START. R & R LT ENGINE ELECTRONIC ENGINE CONTROL MM 73-21-04-024-609-P00, TEST NR 7 AND NR 3 BOTH CHECK GOOD. REF MM 71-00-00, IPC 73-2SDR IPXA2015081192271Floor Panel · corrodedINSPECTION TYPE:C, FWD CARGO FLOOR PANEL 121BF HAS CHAFE MARKS/CORROSION ALSO INCLUDING UNDER AND AROUND THE MBA SYSTEM. BLENDED CHAFE MARKS AND CORROSION ON FWD CARGO FLOOR PANEL 121BF, ORG MAT=0.071, MAT REMOVED=0.011 MAT REM=0.0606 USING TR17809. FOUND TOSDR IPXA2015070190734Engine · overtempRT ENGINE OVERTEMP ON DEPARTURE. THE EGT REACHED 655 DEGREES C. REDUCED THRUST LEVER TO NORMAL RANGE. DECLARED EMERGENCY. RETURNED. ACCOMPLISHED OVERTEMP VISUAL INSPECTION ON RT ENGINE MAX TEMP 654, DEGREES C. DURATION 9 SEC STEADY STATE. EPCS MSG EGT REDSDR IPXA2015061590225Duct · damagedINSPECTION TYPE: C, LT ENGINE OTBD T/R INNER BARREL OUTER SURFACE AFT EDGE SKIN HAS CHIPPED AND BENT. BLENDED, DAMAGE IAW SRM 51-10-02-0G.SDR CALA2015050793679Doubler · crackedEXISTING DOUBLER ON L2 DOOR UPPER HINGE CUT OUT CRACKED. REMOVED EXISTING DOUBLER ON L2 DOOR UPPER HINGE CUT OUT AREA. REPAIRED AREA IAW AMM 52-11-00 FIG 801.SDR IPXA2015041087947Egt Indication · fluctuatesMACHINED RT ENGINE EPR/EGT INDICATION BEGAN TO FLUXUATE. SEVERITY AND FREQUENCY BECAME MORE SEVERE RAPIDLY. ENGINE RETARDED TO IDLE EPR/EGT IND STABILIZED IN NORMAL RANGE. ENGINE NOT SHUTDOWN AND REMAINED IDLE WITH NORMAL IND'S FOR REMAINDER OF FLT. R & R SDR CALA2015032093446Actuator · faultyCREW REPORTS GEAR DISAGREE MSG. LOWERED GEAR & DID NOT GET NOSE GEAR GREEN. ACCOMPLISHED ALT GEAR EXTENSION STILL NO GREEN. ALSO FLIGHT ATTENDANT REPORTED LOUD GRINDING AT INITIAL GEAR RETRACTION. R & R GEAR DOOR ACTUATOR, LOCK ACTUATOR & SEQUENCE VLV. ACCSDR CALA2015021293147Smoke Detector · defectiveAFT CABIN AFT LAVATORY SMOKE DETECTOR GREEN LIGHT IS OFF. REPLACED AFT LAVATORY SMOKE DETECTOR ASSEMBLY. OPERATIONS CHECKED NORMAL.SDR CALA2015012393005Skin · dentedDENT IN EXTERIOR SKIN AT STATION 1695, ABOVE STRINGER 15R. CUT OUT DAMAGED AREA, INSTALLED REPAIR DOUBLER IAW ECRA 5330-04717. NEED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 24 MONTHS.SDR CALA2015011993000Floorbeam · crackedBS 700 FLOORBEAM CRACKED IN UPPER RADIUS AT LBL 45 ON FWD & AFT SIDE. REPAIR BS 700 FLOORBEAM FROM LBL 10 TO LBL 70 IAW ECRA 5310-06386 REV REPAIR IS A CAT A.SDR CALA2015011992997Floorbeam · crackedBS 660 FLOORBEAM CRACK AT LBL 45 IN THE UPPER RADIUS ON THE AFT SIDE. REPAIRED BS 660 FLOORBEAM IAW ECRA 5310-06384. PERMANENT REPAIR.SDR CALA2015011992998Girt Bar · obstructed2L UNABLE TO ARM. REMOVED DEBRIS FROM UNDER GIRT BAR & FROM DOOR FITTING ON SILL. LUBED GIRT BAR & FLOOR FITTING. CYCLED DOOR ARM DISARM LEVER. OPERATIONS CHECKED OK.SDR CALA2015011992994Bear Strap · crackedL1 DOOR CUT OUT 1.3 INCHES SUBSURFACE CRACK IN BEAR STRAP. AD RELATED EA 5330-04213 REV B. REPAIRED IAW EA 5330-04213 OP 2 REV B STEP 24 REQUIRES CF IAW AD 2012-25-11. ACCOMPLISHED NDT INSPECTION OF FUSE SKIN DOUBLER & TRIPLER REPAIR. INSTALLED IAW EA 5330SDR IXXA20150112001Engine · bird ingestionAIR RETURN TO DEPARTURE DUE TO A BIRD STRIKE OF THE NR 1 ENGINE. ENGINE SECURED. IN FLIGHT. ACFT GROUNDED NO OPS. ENGINE BEYOND REPAIR WITH CORE DAMAGE OUT OF LIMITS AT C2 FAN. NR 1 ENGINE R & R.SDR FDEA201412244167Wire Harness · damagedDURING INITIAL CLIMB, NR 1 ENGINE EXCEEDED 1051 DEGREES EGT. NO FIRE INDICATIONS, NO ABNORMAL AIRFRAME MOVEMENTS. RAN QRH SHUTDOWN THE ENGINE. TROUBLESHOT IAW SMP AND FOUND HIGH RESISTANCE DURING HARNESS. SHAKE TEST ON UPPER ENGINE EGT HARNESS , REPLACED USDR IPXA2014121285048Switch · failedDURING TAKEOFF ROLL, BURNING RUBBER ODOR IN COCKPIT. ONCE AIRBOURN ODOR DIMINISHED. BOTH PACKS ON. NO SMOKE AT CRUISE OR CLIMB OUT. HOWEVER DURING DESENT INTO GSP ODOR RETURNED. ON TAXI IN, ODOR SUBSIDED, ALL ENGINE INDICATIONS NORMAL. NO EICAS MSG FOUNDSDR IPXA2014121085041Oil System · overservicedBURNING ODOR OBSERVED ON BOTH T/O AND LANDING AT LOW ALTITUDE. NO SMOKE OBSERVED. CREW REPORTS SUSPECTED SOURCE OF ODOR TO BE THE RT ENG/PACK. OPENED AND INSPECTED RT ENGINE FAN AND CORE. NO HYDRAULIC OR ENGINE OIL LEAKS NOTED. FOUND ENGINE OIL QTY TO BE OSDR CALA2014120892797Warning System · false activation20 MIN AFTER DEPARTURE LE SLAT DISAGREE RETRACTING FLAPS FROM 1 TO 0, DIVERTED. ACCOMPLISHED FAULT ISOLATION FOR, LE SLAT DISAGREE, 27-81 FAULT TREE 803, ACCOMPLISHED LE SLAT ROTARY ACTUATOR INSPECTION CHECK, RESET 3, 5 & 10 RA. FLAP OPERATIONS CHECKED MULTISDR DALA2014120906446Oil System · leakingWHILE OPERATING ON FLIGHT 312, PASSING THRU 14,000 FT, CREW REPORTED FLIGHT DECK AND CABIN BEGAN TO FILL WITH SMOKE. LT ENGINE OIL TEMPERATURE INCREASING AND OIL PRESSURE DROPPING, CREW DIVERTED. ENGINE WAS NOT SHUTDOWN. MAINTENANCE FOUND HIGH SATURATION OF OSDR CALA2014120592796Frame · corrodedAFT PIT, BILGE AREA, FRAME CORROSION STATION 1300, STRINGER 30L. REMOVED DAMAGE & INSTALL REPAIR IAW REO-G18514 REV A & ECRA 5310-06329.SDR CALA2014110492651Light · inoperativeFORWARD LUMINESCENT EXIT LIGHTS DOOR 1L & 1 RIGHT AS WELL AS FWD MOST FLOOR EEL INOPERATIVE. REPLACED FWD MOST EEL CABIN ENTRANCE IAW MM33-51-96. ALL LUMINESCENT LIGHTS OPERATIONS CHECKED GOOD.SDR CALA2014102792617Battery · dischargedPER A CHECK, SEAT EEL FROM SEAT 32 TO SEAT 38, INOPERATIVE. REPLACED BATTERY & BATTERY CHARGER IAW MM 33-51-07-0201. OPERATIONS CHECKED OK.SDR FDEA201410243370Fitting · damagedPYLON NR 1 PYLON AFT ENG MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE.SDR FDEA201410243371Fitting · damagedNR 2 PYLON AFT ENGINE MOUNT BULKHEAD FITTING FWD & AFT SHEAR PIN BUSHING HOLES FOUND OUT OF DWG TOLERANCE. REPAIRED IAW EA F-5450-T0311678. REPAIR CLASSIFIED AS MAJOR.SDR CALA2014102492570Brake · lack of lubeRECEIVED TE FLAP DISAGREE MSG WHEN FLAP HANDLE FROM 20 TO 25. FOUND TRANSMISSION OVLD INDICATOR TRIP 1, 5 & 8. RESET TRIP OVLD INDICATOR & LUBED FLAP TRANS TORQUE BRAKE. CYCLED FLAPS, NO FAULTS NOTED.SDR FDEA201410233362Fitting · damagedNR 2 ENGINE AFT MOUNT LOWER HANGER FITTING LT & RT BUSHING LUG HOLES FOUND OVERSIZED AFTER BUSHING REMOVAL. REPAIRED IAW EA F-7120-T0312222. REPAIR CLASSIFIED AS MINOR.SDR CALA2014102492569Light · disconnectedEMERGENCY EXIT LIGHT STRIP AT ROW 30 DISCONNECTED. ATTACHED LIGHT STRIP, LIGHT TESTED OK.SDR CALA2014102192533Skin · puncturedAPU COMPARTMENT INTERNAL FUSE SKIN HAS PUNCTURE THRU THE HONEYCOMB BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON. REPAIR APU COMPARTMENT INTERNAL SKIN AT BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON IAW ECRA 5350-02153.SDR CALA2014102492558Skin · puncturedAPU COMPARTMENT INTERNAL SKIN HAS PUNCTURE THRU THE BS 1926.7 & 18.5 FROM THE RT APU DOOR SUPPORT LONGERON. REPAIR APU COMPARTMENT INTERNAL SKIN IAW ECRA 5350-02153 & MUST BE INSPECTED AT INTERVALS NOT TO EXCEED 500 FLIGHT INSPECTION IAW PART 2 OF ECRA. AT NSDR CALA2014102192528Floorbeam · corrodedCORROSION ON BOTTOM SIDE OF UPPER T CAP AT BS 1681 RBL 47. REPAIRED MAIN CABIN FLOORBEAM UPPER CAP AT BS 1681 RBL 47 IAW SRM 53-60-51 REPAIR 4 FIG 201.SDR CALA2014102192529Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM AFT FACE BS 1681 BL 57RT. REPAIRED MAIN CABIN FLOORBEAM AT BS 1681 RBL 57 IAW ECRA 5310-06284 & ALL REQUIRED NDT.SDR CALA2014101692457Stringer · corrodedCORROSION ON AFT CARGO STRINGER AT BS 1440 STRINGER 27L STRINGER SPLICE. FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 1 01 DETAIL II. REPAIRED STRINGER 27L BS 1433 TO 1460 IAW SRM 53-0 0-03 FIG 201 REPAIR 1.
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