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 CALA2014101692458Stringer · corrodedCORROSION ON AFT CARGO FLOOR STRINGER BS 1460 STRINGER 26L. FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 1 01 DETAIL II. REPAIRED STRINGER 27L BS 1433 TO 1460 IAW SRM 53-00-03 FIG 201 REPAIR 1.SDR CALA2014101692436Frame · corrodedCORROSION AFT CARGO COMPARTMENT FRAME AT BS 1400 BETWEEN STRINGER 27L & 29L. R & R LOWER FRAME SECTION AT BS 1400 BETWEEN STRINGER 25L & 28R IAW SRM 51-40-02 PARA 4 & 7 FIG 3 & 12.SDR CALA2014101692439Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED TOP FLANGE BS 700 LBL 24.75 & LBL 46.5. REPAIRED MAIN CABIN FLOORBEAM TOP FLANGE AT BS 700 LBL 24.75 & LBL 46.5 IAW ECRA 5310-06274. THIS IS A CATEGORY A REPAIR.SDR CALA2014101692441Floorbeam · corrodedCORROSION MAIN CABIN FLOORBEAM UPPER SURFACE BS 365 RBL 4. REPAIRED MAIN CABIN FLOORBEAM UPPER CHORD AT BS 365 RBL 10 TO LBL 70 IAW ECRA 5310-05536, ECRA 5100-01844 & ECRA 5310 -06277. THIS IS A CATEGORY A REPAIR.SDR CALA2014101692433Frame · corrodedCORROSION AFT CARGO COMPARTMENT FRAME AT BS 1420 BETWEEN STRINGER 27L & 29L. R & R IAW SRM 51-40-02 PARA 4 & 7 FIG 3 & 12. FABRICATED LOWER FRAME SECTION IAW SRM 51-30-01 PARA & FIG 7 & DWG 146N1028.SDR CALA2014101392392Structure · dentedDENT AT STATION 1705 BETWEEN STRINGER 17L & 18L. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 3.SDR CALA2014101392393Structure · dentedRE INSPECTION IAW SRM 53-00-01 TABLE V USING LOW FREQ METHOD IAW NDT PART 6 51-00-06. RAMP REPORTED A DENT AT STATION 1680 APPROX 3 FEET BEHIND DOOR 4L. ALL RE INSPECTION COVERED ON CF9067. VERIFIED DENT IS FREE OF CRACKS USING HFEC. DENT LOCATED AT STATIONSDR CALA2014102192527Skin · dentedDENT AT STATION 1705 BETWEEN STRINGER 17L & 18L. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 3.SDR CALA2014100292354Crease Beam · corrodedCORROSION MULTI AREAS AS MARKED. MAIN CABIN CREASE BEAM BS 1000 - 1040. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02 PAR 4 FIG 3 PAR 7 FIG 12 & PAR 5 FIG 9 I.SDR CALA2014092992338Intercostal · corrodedMAIN DECK FLOOR INTERCOSTAL STATION 1795 LBL 12 - RBL 8 FOUND CORRODED. CORRODED INTERCOSTAL REPLACED IAW DWG 146U5620 SHT 10 REV A & SRM 51-40-02.SDR CALA2014092992331Light · inoperativeSEAT 50KJH EMER EXIT LIGHT INOPERATIVE. REPLACED, CHECKED GOOD IAW MM33-51-12.SDR CALA2014092992332Light · inoperativeSEAT 38ABC EMER EXIT LIGHT INOPERATIVE. REPLACED, CHECKED GOOD IAW MM 33-51-12.SDR CALA2014092992333Light · inoperativeRIGHT SIDE OVER WING EMER EXIT LIGHT 3RD AFT INOPERATIVE. REPLACED, CHECKED GOOD IAW MM 33-51-03.SDR CALA2014092992337Light · inoperativeLEFT SIDE OVER WING EMER EXIT LIGHT FWD & AFT INOPERATIVE. REPLACED LT FWD OVERWING LIGHT ASSEMBLY. OPERATIONS CHECKED OK.SDR CALA2014092992322Line · chafedRIGHT OFF WING SLIDE PRESS LINE FOUND CHAFING WHERE IT PENETRATES FUSELAGE THROUGH CLOTH BRAID ON LINE. REPAIRED PRESS LINE GNMM 1-0-0-006.SDR CALA2014092292253Battery · dischargedEMERGENCY EXIT LIGHT SECTION BETWEEN SEAT ROW 21ABC & 27ABC INOPERATIVE. REPLACED BATTERY & CHARGER IAW MM 33-51-07 AT ROW 23. EMERGENCY EXIT LIGHT OPERATIONS NORMAL.SDR CALA2014090992104Mount · gougedNUMBER 2 ENG FWD MOUNT INBD AFT ATTACH AREA HAS GOUGE APPROX 250 INCHES FROM BOLT HOLE FLANGE. STRUT FITTING, UPPER MOUNT, HAND BLENDED GOUGE IAW SRM 54-51-09. EDDY CURRENT BY INSPECTION WITH NO DEFECTS FOUND. ROTO PEENED IAW GPM 1-0-01-076. NOTE ORIGINAL SDR CALA201409039258Light · looseEMERGENCY EXIT LIGHT STRIP LOOSE NEAR ROW 11. SECURED THE LIGHT AND OPS CHECKED NORMAL.SDR CALA2014082892035Floorbeam · crackedMAIN CABIN FLOORBEAM UPPER CHORD HAS A CRACK AT THE RADIUS, BS 660 LBL 46. REPAIRED MAIN CABIN FLOORBEAM UPPER CHORD IAW ECRA 5310-06181.SDR CALA2014082692024Skin · crackedLOWER EXT FUSELAGE SKIN BS 760 LBL 12, SKIN CRACKED 2 PLACES. REMOVED DAMAGE, FABRICATED & INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 3.SDR CALA2014082692022Frame · corrodedAFT PIT BS 1480 STRINGER 27R CORROSION ON FRAME. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-30-01.SDR CALA2014082592011Shear Tie · damagedBS 1420 BETWEEN STRINGER 28R & 29R SHEAR TIE HAS DAMAGED HOLE. FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-30-01 & 51-40-05.SDR CALA2014082592012Frame · crackedAFT PIT BS 1440 FRAME INBD CHORD CRACKED AT RBL 11. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5360-01389.SDR CALA2014082592013Stringer · corrodedAFT PIT BS 1406 STRINGER 29R IS CORRODED. R & R STRINGER 29R FROM BS 1406 TO 1452 IAW SRM 51-40-02 & SRM 51-40-05.SDR CALA2014082592015Frame · dentedAFT PIT BS 1600 STRINGER 26L DENT ON UPPER SURFACE OF FRAME. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 5.SDR CALA2014082192003Light · disconnectedEXIT LINE STRIP BY SEAT 20ABC NEEDS TO BE RECONNECTED, PIECES IN THE COCKPIT. REPLACED LIGHT STRIP & CLEAR TRACK COVER SECTION. LIGHT STRIP CHECKED GOOD.SDR CALA2014081391977Shear Tie · corrodedAFT PIT BS 1380 RBL 3 FRAME SHEAR TIE CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02.SDR CALA2014081391978Repair · gougedNUMBER 1 PYLON AFT FAIRING FRAME AT OTBD END, PREVIOUS REPAIR GOUGED. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-70-11.SDR CALA2014081391971Unknown · malfunctionedCABIN DECOMPRESS AT 33K. CABIN CLIMBED TO 11K & WOULD NOT DESCEND. EICAS MSG CABIN ALTITUDE. ACFT WAS DESCENDED BELOW 10K IAW QRH & CABIN PRESS FOLLOWED DESCENT. PERFORMED SEVERAL TASKS INCLUDING AMM 5-51-98 CABIN PRESSURIZATION INSPECTIONS. SEE AMIS HISSDR CALA2014081391974Cover · looseEMERGENCY LIGHTING STRIP BY 8BAC - 9ABC IS LOOSE. SECURED EMER PATH LIGHTING CLEAR COVER FROM 8ABC TO 9ABC.SDR CALA2014081191924Frame · damagedFUSE FRAME REPAIRS AT BS 1600, STRINGER 26L & BS 1320, STRINGER 28L WERE ACP.SDR CALA2014081191925Skin · dentedMAJOR REPAIR, REF INBD CF9048. SKIN DENT AT STATION 520 STRINGER 24 - 25R. DENT IS OUT OF LIMITS.SDR CALA2014081191926Structure · crackedDOOR 2R UPPER DOOR HINGE CUT OUT CRACKED, MAJOR REPAIR. INSTALLED DOUBLER REPAIR IAW SRM 52-10-02 REPAIR NR 1. THIS IS A CATEGORY B REPAIR. THE REPAIR ANGLE WAS MADE IAW PARA 4G IAW PARA 5 TABLE 202.SDR CALA2014081391966Crease Beam · corrodedRIGHT CABIN CREASE BEAM INBD CHORD CORROSION. REMOVED DAMAGE, FABRICATED & INSTALLED REPAIR PARTS IAW SRM 51-40-05.SDR CALA2014081391972Apu · faultyAPU HAD SHUTDOWN, FAULT LIGHT ILLUMINATED & EICAS MSG APU FAULT DISPLAYED. ADDED 6 QTS OIL, RAN APU, HAD AUTO SHUTDOWN WITHIN 4 MINUTES WITH HEAVY WHITE SMOKE COMING OUT OF THE TAIL PIPE. OIL TANK WAS EMPTY WHEN CHECKED AFTER SHUTDOWN. OIL DRIPPING FROM BOTSDR CALA2014081191935Skin · dentedEXT FUSE SKIN BS 430 STRINGER 15L, DENT. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW SRM 53-00-01.SDR CALA2014081191936Frame Splice · gougedBS 1520 FRAME SPLICE ABOVE STRINGER 23R, MULTIPLE GOUGES. FABRICATED & INSTALLED NEW SPLICE IAW DWG 146N1042 & SRM 51-30-01.SDR CALA2014081191937Fairing · crackedRIGHT EMPENNAGE BS 1787 STRINGER 17R - 19R. FIXED FAIRING PANEL CRACKED. FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 5387-01001.SDR CALA2014081191938Stringer · corrodedAFT PIT BS 1472 STRINGER 29R CORROSION. FABRICATED & INSTALLED NEW STRINGER 29R FROM BS 1460 TO 1488 IAW SRM 53-00-03.SDR CALA2014081191940Idg · lowLEFT GEN DRIVE ON UPPER EICAS ON TAKEOFF ROLL, ABORTED AT 85 KNTS. SERVICED LT IDG TO FULL, RAN LT ENG, NO LEAKS NOTED, CHECKED OK.SDR CALA2014081391962Idg · lowLEFT GEN DRIVE ON UPPER EICAS ON TAKEOFF ROLL, TAKEOFF ABORTED. SERVICED LT IDG TO FULL, RAN LT ENG NO LEAKS NOTED, LFT GEN CHECKED OK. RE-CHECK IDG FLUID AFTER 25 FLIGHT HOURS. DPI CHECKED OK, BPCU SHOWED NEED OIL & CLEARED AFTER.SDR UFHR20140825001Control Valve · failedTHE CONTROL VALVE BODY WAS SUBJECTED TO NDT WHICH REVEALED AN INDICATION AND WAS REJECTED FOR RETURN TO SERVICE.SDR CALA2014080691743Irs · malfunctionedIRS RT OUT OF LIMITS 19 KNOTS LT 2 KTS CTR 3 KTS WITHIN LIMITS. TO BE RECHECKED AFTER NEXT FLIGHT.SDR CALA2014080691744Eec · malfunctionedRIGHT ENG PRI CONT STATUS MSG. REPLACED EEC ON ENG NR 2 IAW AMM 73-21-04-401. ENG RUN ACCOMPLISHED OK.SDR CALA2014080691745Compressor · stalledRT ENG SN 726726 HAD AUDIBLE COMPRESSOR STALL DURING ENG START AT STARTER CUT OUT AT APPROXIMATELY 47 -48%. VISUALLY INSPECTED NR 2 ENG CHIP DETECTORS & PERFORMED BORE INSPECTION OF ENG VIA PLUGS AP 2 & AP 8. NO ABNORMALITIES FOUND BY INSPECTION.SDR CALA2014080691746Engine · overtempRIGHT ENG SN 726726, DURING ENG START EGT EXCEEDED START LIMITS, MAX EGT FROM EXCEEDANCE PAGE REPORTED TO BE 552 FOR ONE SECOND IAW JRH 2-5-62 FIG 1. EXCEEDANCE IS IN AREA A WHICH REQUIRES VISUAL INSPECTION IAW AMM 72-00-00 PAGE 686U PARA 16. PERFORMED VISUASDR CALA2014072891555Light · unsecureFLOOR LIGHTING STRIP IN FRONT OF FIRST CLASS CLOSET IS PULLED UP. INSTALLED NEW BASE STRIP & INSTALLED EEL LAMP IAW MM 33-51-00. OPERATIONS CHECKED GOOD.SDR CALA2014072591517Crease Beam · corrodedCABIN FLOOR STRUCTURE BS 940 - 960 STRINGER 17L LT CREASE BEAM INTERCOSTAL UPPER SURFACE CORRODED. R & R CREASE BEAM.SDR CALA2014072591518Skin · dentedSKIN DENTS CLOSE TO DOUBLER AT STATION 580 & STRINGER 29R. REMOVED DOUBLER, CUT OUT SKIN DAMAGE, FABRICATED & INSTALLED ALL REPAIR PARTS. ACCOMPLISH PERM REPAIR AT 24 MONTHS. PLANNING TO CONTACT ENGINEERING AFTER 22 MONTHS, BUT BEFORE 23 MONTHS FOR INSTRUCTSDR CALA2014072591519Skin · dentedSKIN DENTS AT STATION 611 & STRINGER 29R NEAR ANTENNAS. REMOVED DAMAGED SKIN, FABRICATED & INSTALLED ALL REPAIR PARTS. ACCOMPLISH PERMANENT REPAIR BEFORE 24 MONTHS. PLANNING TO CONTACT ENGINEERING AFTER 22 MONTHS, BUT BEFORE 23 MONTHS FOR INSTRUCTIONS WITH
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