N429QX
Service difficulty reports · 217
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N429QX' AND registry_match = 'registration' 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 n_number = 'N429QX' AND registry_match = 'registration' 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 QXEA2014022600161Doubler · corrodedCORROSION ON LAVATORY SERVICE PORT INTERNAL DOUBLER. REMOVED CORROSION DAMAGE AT AFT LOWER CORNER OF LAVATORY SERVICE PORT INTERNAL DOUBLER REF SRM 52-42-10. REPAIR-1, PROCEDURE 7-B, 1. NDT REPAIR CUTOUT FOR CRACKS. C/W ET INSPECTION ON REWORKED AREA REF NDSDR QXEA2014022600154Beam · corrodedAFT SERVICE DOOR EDGE BEAM, AND THRESHOLD HAVE EVIDENCE OF CORROSION. REMOVED EDGE BEAM AT AFT RT SERVICE DOOR, IAW SRM 51-42-05.
INSTALLED EDGE BEAM IAW SRM 51-42-05.SDR QXEA2014022400145Seat Track · corrodedSEAT TRACK NR 8 CORRODED BEYOND LIMITS. REMOVED SEAT TRACK IAW SRM 51-42-05, STEP 4E (2-8) AND SRM 51-41-00. INSTALLED NEW SEAT TRACK IAW SRM 51-42-05, STEP 4D AND SRM 51-41-00 AND SRM 51-40-15, STEP 6.SDR QXEA2014021900136Seat Track · corrodedSEAT TRACK NR 1 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-05, REPAIR -01 AND SRM 51-40-15 REPAIR -01. LOCATED AND DRILLED IAW SRM 51-40-07, REPAIR -01.SDR QXEA2014021900135Seat Track · corrodedSEAT TRACK 20 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-05 AND SRM 51-40-15, STEP 6.SDR QXEA201402240014Skin · damagedLIGHTNING STRIKE ON SKIN, REPAIRED IAW SRM 51-42-45/53-00-00. FINISH RESTORED TO REWORK AREA IAW SRM 53-00-00.SDR QXEA2014012700065Seal · lack of lubeAFT SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DOOR SEAL, OPS CHECKED GOOD. RETURNED TO SERVICE.SDR QXEA2013071501173Stop · draggingF/A REPORTS UNABLE TO OPEN THE MAIN CABIN DOOR HANDLE. ACFT FERRIED FOR REPAIRS. INSPECTED AND FOUND AFT NR 4 AND NR 5 MAIN CABIN DOOR PRESSURE STOPS DRAGGING AGAINST STOP FITTING WHEN OPENING AND CLOSING. ADJUSTED MAIN CABIN DOOR SHELL IAW MM TASK NR 52-11-SDR QXEA2013042300817Roller · lack of lubeFORWARD MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED AND LUBED ROLLER MECHANISMS. NO DEFECTS NOTED. RETURNED TO SERVICE.SDR QXEA2013041100781Door · lack of lubeMAIN CABIN DOOR DIFFICULT TO OPEN FROM THE LOCKED POSITION. CLEANED AND LUBED ATTACHEMENTS FITTINGS OF MAIN CABIN DOOR INCLUDING TRACK. INSPECTED MCD FOR ANY DEFECTS, NONE NOTED AT THIS TIME. OPERATED MCD SEVERAL TIMES WITH CREW PRESENT. DOOR OPERATES NORMASDR QXEA2013040200727Door · unknownMAIN CABIN DOOR IS DIFFICULT TO OPEN. MAIN CABIN DOOR OPENS AND CLOSES SMOOTHLY. PERFORMED OPS TEST SEVERAL TIMES IAW AMM 52-11-00-710-802. OPS TEST GOOD. PERFORMED FUNCTIONAL TEST OF AIRSTAIR DOOR IAW AMM 52-11-00-720-802. FUNCTIONAL TEST GOOD. NO DEFECSDR QXEA2013021100312Handle · damagedEMERGENCY EXIT LOWER DOOR HANDLE DAMAGED AND SHOCK MOUNT HAS A BROKEN SCREW. REPLACED THE DOOR HANDLE AND THE SHOCK MOUNT IAW SRM 51-42-00.SDR QXEA2013021100311Angle · corrodedFORWARD EMERGENCY DOOR SILL PLATE HAS EVIDENCE OF CORROSION AROUND ALL THE ATTACH SCREWS AND BOTH STOP FITTINGS. REPLACED SILL PLATE ANGLE IAW SRM 51-42-05 AND 51-42-15.SDR QXEA2013021100313Latch · out of adjustRT FORWARD LOWER EMERGENCY EXIT FAILED PIN EXTENSION CHECK LENGTH MEASUREMENT AMM 52-23-00-720-801. ADJUSTED LATCH IAW AMM 52-23-00-820-801.SDR QXEA2013021100309Support Bracket · corrodedFORWARD EMERGENCY EXIT DOOR HAS CORROSION ALONG THE FORWARD FLANGE OF THE DOOR HANDLE SUPPORT BRACKET. DAMAGE FOUND TO ONLY BE IN PROTECTIVE COATINGS. RESTORED FINISHES IAW SRM 51-25-00.SDR QXEA2013021100310Attach Bolt · corrodedFORWARD EMERGENCY EXIT DOOR HAS A CORRODED WINDOW ATTACH BOLT.SDR QXEA2013011400056Glowstrip · delaminatedPHOTO LUMENESCENT FLOOR STRIP AT ROW 1 IS LOOSE AND DELAMINATED. REPLACED THE FLOOR STRIP IAW AMM 33-51-16-000-801 AND 33-51-16-400-801. RETURNED TO SERVICE.SDR QXEA2012111801387Wire Harness · damagedCLIMBING THROUGH FL240 NOTICED NR 2 ITT READING 276 C, ALL OTHER NR2 ENG PARAMETERS APPEARED NORMAL, NR 1 ENG ITT, 710 C, OAT -30 C. REPLACED THE WIRE HARNESS, OPS CHECKED GOOD. RETURNED TO SERVICE.SDR QXEA2012071900715Light · damagedFLOOR PATH LIGHTING STRIP DISCOLORED AT RT NR 7 SEGMENT, LT NR 1 SEGMENT. REPLACED AS REQUIRED IAW CMM 33-51-01.SDR QXEA2012071100658Glowstrip · damagedPHOTOLUMINESCENT STRIP IN BETWEEN THE LAV AND INTERNAL CARGO DOOR IS MORE THAN 80 PERCENT DAMAGED. REPLACED PHOTOLUMINESCENT STRIP IAW AMM TASK 33-51-16-000-801 AND 33-51-16-400-801, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.SDR QXEA2012062500536Warning Message · false activationDEICE PRESSURE CAUTION ILLUMINATED. BOOT PAIRS APPEARED TO OPERATE NORMALLY. SYS PRESSURE 20 PSI BOTH SIDES. RAN THE EMERGENCY ABNORMAL CHECKLIST, CAUTION EXTINGUISHED AND DID NOT REAPPEAR. COMPLIED WITH GENERAL VISUAL INSPECTION OF AIRFRAME DE-ICE BOOTS IAWSDR QXEA2012061700471Door Seal · failedF/A'S REPORT AFT PASSENGER DOOR IS HARD TO OPEN AND CLOSE. FERRIED FOR REPAIRS. R & R AFT PAX DOOR SEAL. RETURNED TO SERVICE.SDR QXEA2012061200436Light · overheatedPOSSIBLE ELECTRICAL TYPE ODOR IN AFT GALLEY AREA. COMPLIED WITH AIR CONTAMINATION CHECKLIST, WAS ABLE TO DETECT A VERY SLIGHT ELETRICAL ODOR FROM AFT GALLEY UPPER BULKHEAD VENTS. PERFORMED INSPECTION OF AFT CARGO BAY AREA, FOUND ELECTRCAL ODOR COMING FROM ASDR QXEA2012060300417Wire · pinchedEMERGENCY LIGHT ON F/A'S SEAT BULKHEAD NEXT TO MAIN CABIN DOOR INOPERATIVE. FERRIED FOR REPAIRS. INSPECTED WIRING AND FOUND 2 WIRES PINCHED. SPLICED WIRE 1 AND WIRE 2 WITH ENVIRONMENTAL SPLICES. ENSURED PROPER OPERATION OF EMERGENCY LIGHT. LIGHT CHECKED GOSDR QXEA2011112201244Feel Unit · malfunctionedGOING THRU 11,000 FT AFTER SELECTING THE AUTO PILOT OFF AND LEVELING WHILE LEFT TURN AT 10,000 FT THE LEFT RUDDER WAS JAMMED. AFTER APPLYING PRESSURE THE JAM BROKE FREE. RUDDER RESPONDED AND EXCESSIVE LEFT YAW. RUDDER REMIANED NORMAL FOR REMAINDER OF FLIGHT WSDR QXEA2011100600927Fan · odorFROM T/O TO TOUCHDOWN, ODOR OF EXHAUST FILLED THE ACFT, WAS MORE INTENSE WITH APPLICATION OF HEAT AND AT TOP OF DESCENT. C/W FIM TASK FOR SMOKE/OILY ODOR IN CABIN FIM 71-00-00-810-817. GROUND RAN ACFT AT VARIOUS POWER SETTINGS & W/ NR 1 & NR 2 ENG BLEED ISOLSDR QXEA2011100600926Fan · obstructedUPON ENTERING CABIN NOTICED STRONG ACRID ODOR & A HAZE IN THE CABIN THE RECIRC FAN SWITCH WAS ON WITH NO AIRFLOW FROM PASSENGER VENTS. REMOVED RECIRCULATION FAN IAW AMM TASK 21-22-16-000-801. FOUND RED SHOP RAG LODGED IN RECIRC FAN INTAKE. INSPECTED DOWNSTSDR QXEA2011100300919Stanchion · corrodedSTANTION AT FRAME 236 IS CORRODED BY STRINGER 31P. REMOVED STRINGER TO FRAME ANGLE AND BLENDED AWAY CORROSION PER SR, 51-21-00-00-01. REMAINING THICKNESS IS .014, OUT OF LIMITS. INSTALLED NEW STANTION IAW SRM 51-42-05-01-01.SDR QXEA2011100300923Frame · corrodedFRAME X8.000 LOWER FLANGE HAS CORROSION ABOVE STRINGER 25P JUST BELOW FWD LT PAX DOOR. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .043", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-20-SDR QXEA2011100300922Stanchion · corrodedSTANCHION AT FR 236 IS CORRODED BY STR 31P. BLENDED AWAY CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS IS .014", MATERIAL LOSS OUT OF LIMITS. REMOVED STANCHION IAW SRM 51-42-05-02-01. RECEIVED NEW PART AND MATCH DRILLED IAW SRM 51-42-05-02-0SDR QXEA2011100300921Threshold · corrodedFORWARD PAX DOOR THRESHOLD AND THRESHOLD SUPPORT ARE CORRODED. FOUND THRESHOLD TO BE OUT OF LIMITS IAW SRM 53-20-23. REMOVED THRESHOLD AND REMOVED CORROSION ON LOWER SUPPORT IAW SRM 51-42-05-02-01 AND 53-20-23. MEASURED LOWER SUPPORT AND FOUND TO BE OUT OF SDR QXEA2011092900908Doubler · corrodedINTERNAL SKIN DOUBLER FOR LAV VENT IS CORRODED BY STR FR 19.4 TO 32.4. REMOVED CORROSION IAW SRM 51-21-00-00-01. MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00-00-02. FABRICATED NEW DOUBLER IAW TASK CARD 6-53-1022. COMPLIED WITH TASK CARD 6-53-10SDR QXEA2011092900914Coax · chafedADF 1 ANTENNA CABLE CHAFED FWD OF FRAME 32.400. RELEASED CABLE TIES AND CLAMPS. REPAIRED OUTER JACKET OF CABLE WITH SHRINK TUBING IAW WM 20-15-01. ACCOMPLISHED ELECTRICAL TEST OF CABLE IAW AMM 20-30-11-760-801 AND WM 34-52-00. RESECURED CABLE. SYS CHECKED SDR QXEA2011092900913Skin · chafedRT WING OTBD FLAP UPPER SKIN IS CHAFED BETWEEN STA YW245.019 AND YW281.019. BLENDED OUT DAMAGE IAW RD 8/4-57-1594. FOUND TO BE WITHIN LIMITS AND CONFIRMED CRACK FREE AREA IAW NTM 51-00-02-250-801 AND RD 8/4-57-1594. ALODINED, PRIMED AND PAINTED IAW RD 8/4-5SDR QXEA2011092900912Frame · corrodedFRAME 54.0, FLANGES FROM STR 31P TO 29P ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344. CONFIRMED CRACK FREE AREA REF NTM 51-00-02-250-801. FRAME FLANGE FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRM 51-SDR QXEA2011092900911Stringer · corrodedSTRINGER 24S HAS AN AREA OF CORROSION FR 564.5 TO 584.5. REMOVED CORROSION IAW SRM 51-21-00-00-02. REMAINING THICKNESS .058". AREA FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3960. CONFIRMED CRACK FREE REF NTM 51-00-01-250-801. ALODINED, PRIMED AND PAINTED ANSDR QXEA2011092900910Stringer · corrodedSTRINGER 31P IS CORRODED AFT OF FR 176. REMOVED CORROSION IAW SRM 51-21-00-00-02. AREA FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3961. COMFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801. COMPLETED REPAIR IAW RD 8/4-53-3961.SDR QXEA2011092800906Frame · corrodedFRAME 69.4, FLANGES FROM STR 29P TO 32S ARE CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344. BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-01-250-801. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SDR QXEA2011092800905Frame · corrodedFRAME 54.0, FLANGE FROM STR 33 TO 32S IS CORRODED. REMOVED CORROSION IAW RD 8/4-53-2344. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED, PAINTED AND APPLIED CPC IAW SRSDR QXEA2011092800904Flap Track · chafedRT WING INBD FLAP, UPPER INBD NR 1 FLAP TRACK IS CHAFED. BLENDED OUT CHAFE DAMAGE IAW RD 8/4-57-1352. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1352. APPLIED PRIMER AND TOP COAT IAW RD 8/4-57-1352. COMPLETED RD 8/4-57-1352.SDR QXEA2011092800902Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN UNDER LAV DRAIN MAST EXTERNAL DOUBLER. CORROSION REMOVED IAW SRM 51-21-00-00-02. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-02-250-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3970. APPLIED PRIMER, REQUIRED IAW RD 8/4-53SDR QXEA2011092800901Skin · corrodedLONGITUDINAL SKIN STRAP OTBD OF STR 32P IS CORRODED FR 71.2 TO FR 216. REMOVED CORROSION IAW SRM 51-21-00-00-01. BLENDED AREAS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3957. APPLIED ALODINE, PRIMER, PAINT AND CPC AS REQUIRED IAW RD 8/4-53-3957. COMPLIED WITSDR QXEA2011092800900Skin · corrodedLONGITUDINAL SKIN STRAP OTBD OF STR 32P IS CORRODED FR 71.2 TO FR 116. REMOVED CORROSION IAW SRM 51-21-00-00-01. BLENDED AREAS ON STRAP FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3957. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-02-250-801. APPLIED ALODINE,SDR QXEA2011092700899Support · corrodedTHRESHOLD SUPPORT FOR FORWARD RT EMERGENCY EXIT IS CORRODED. REMOVED THRESHOLD SUPPORT IAW SRM 51-42-05-02-01 AND FOUND SUPPORT TO BE OUT OF LIMITS IAW SRM 52-20-21-00-01. REMOVED GUSSETS IAW SRM 51-42-15-02-01. FOUND GUSSETS TO BE CORRODED BEYOND LIMITS. SDR QXEA2011092700903Flap Track · corrodedLT WING INBD FLAP, UPPER INBD NR 1 FLAP TRACK IS CHAFED. REMOVED AND BLENDED DAMAGE IAW RD 8/4-57-1352. DAMAGE EXTENDED 7.1" BEYOND THE ALLOWABLE AREA. MINIMUM REMAINING THICKNESS IN AREA COVERED BY RD 8/4-57-1352 IS .186". MINIMUM REMAINING THICKNESS THE SDR QXEA2011092600895Doubler · corrodedCORROSION FOUND ON LAV VENT EXTERNAL DOUBLER DURING REMOVAL OF LAV VENT. REMOVED DOUBLER FROM ACFT IAW SRM 51-42-05-02-01 FOR ACCESS. REMOVED CORROSION IAW SRM 51-21-00-00-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-00-00-02. FABRICATED NEW DOUBLER IAW TSDR QXEA2011092600894Frame · corrodedFRAME 32.4 UPPER TIE TO INTERCOASTAL 28P IS CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02. MINIMUM REMAINING THICKNESS .037". CONFIRMED AREA CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. FABRICATED PART USING 7075-T6 .040" IAW DWG 85329356SDR QXEA2011092900909Frame · corrodedFRAME 156, FLANGES STR 27P TO 32P ARE CORRODED. REMOVED CORROSION IAW SRM 51-21-00-00-02 AND RD 8/4-53-2344. FOUND CORROSION BEYOND LIMITS ON FRAME FLANGE BETWEEN STR 28P AND 29P. MINIMUM REMAINING THICKNESS .037" CONFIRMED CRACK FREE REF NTM 51-00-02-250-8SDR QXEA2011092600893Intercostal · corrodedINTERCOSTAL INBD OF STR 29P IS CORRODED FR 54.0 TO 69.4. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AREA CRACK FREE REF NTM 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-3959. COMPLETED REPAIR IAW RD 8/4-53-3959.SDR QXEA2011092600892Intercostal · corrodedINTERCOSTAL INBD OF STR 30P IS CORRODED FR 54.0 TO 69.4. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED AREA CRACK FREE REF NTM 51-00-01-250-801. MATERIAL LOSS WITHIN LIMITS OF RD 8/4-53-3958. COMPLETED REPAIR IAW RD 8/4-53-3958.
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