N429AW
Service difficulty reports · 190
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 = 'N429AW' 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 = 'N429AW' 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 A6WA202501318856Warning Light · illuminatedAFTER SELECTING THE GEAR UP WITH THE FLAPS AT 0 DEGREES. RECEIVED MOMENTARY GEAR DISAGREE WARNING. MESSAGE CLEARED ON ITS OWN AND QRH REVIEWED. GEAR EXTENDED NORMALLY FOR LANDING. AIRCRAFT REMOVED FROM SERVICE. OPEN.SDR A6WA202411158843Strut · underservicedAFTER SELECTING GEAR LEVER UP NOSE GEAR REMAINED DOWN RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WRINGING MSGS C/W QRH ALL GEAR DOWN AND NORMAL LANDING. SMOOTH LANDING, LAND WEIGHT WAS 46,700. GEAR MESSAGES APPEARED, APPROX 10 SECONDS AFTER SELECTION. MANUAL RESDR A6WA202410158837Engine · faultedIN CLIMB RIGHT ENGINE HAD SPIKE IN ITT AND REDUCTION IN N1 AND N2 AND WAS UNRESPONSIVE FOR 10-20 SECONDS. THEN RETURNED TO NORMAL. ON APPROACH RIGHT ENGINE AGAIN HAD SAME INDICATION AND AIRCRAFT HAD VIBRATIONS. DURING BOTH EVENTS THRUST WAS BEING REDUCED BY PISDR A6WA202401148697Bracket · bentGEAR DISAGREE WARNING AFTER SELECTING GEAR UP DEPARTING ORD. NLG NEVER MOVED & ALSO RECEIVED NLG DOOR OPEN WARING AFTER MLG DISAGREE WARING ACFT REMOVED FROM SERVICE. INTERROGATED PSEU & FOUND CODES: NG0EXT FAR S23, S35 NEAR NGDLK2, S21 NGDLK01, S22 FAR NGUSDR A6WA202209208308Bushing · wrong partELONGATED HOLE DUE TO WRONG BUSHING INSTALLED. WRONG BUSHING OUTSIDE DIAMETER .750, INSIDE DIAMETER .627 / AILERON HOLE .815" OUTSIDE DIAMETER, .611" INSIDE DIAMETER. ***AIRCRAFT REMOVED FROM SERVICE ***** RH AILERON PN: CC670-13000-2 SN: 7711 UPWARD PCU IB SISDR A6WA202206088192Oil System · warning message****SUPPLEMENTAL INFORMATION ******AT CRUISE NOTICED LH ENG OIL PRES FLUCTURATE BETWEEN 25-53 PSI NO MSG PRESENT. NORMAL DESCENT. ON SHORT FINAL RCVD LH ENG OIL PRES WARNING MSG INTERMIATELY. RAN QRH SHUTDOWN LH ENG. LANDED SAFELY. SDR A6WA202202218115None · noneRECEIVED STALL FAIL CAUTION AT 500'. C/W QRH. DIVERTED TO DAY. ON GROUND PERFORMED GPWS TEST, GPWS FAIL STATUS MSG POSTED. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED GPWS TEST TO CLEAR GPWS FAIL MESSAGE. IAW AWA SUP 20-137. ALSO PERFORMED TEST OF SDR A6WA202201108056Trim Switch · faultedRECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES AT CRUISE. QRH DIRECTED FLAPS 20 LANDING, WHICH WAS SUCCESSFUL WITH NO ISSUES. ATTEMPTED TO REENGAGE MULTIPLE TIMES WITHOUT SUCCESS. AIRCRAFT REMOVED FROM SERVICE. ACARS EMAILS REPORT FO STAB TRIM DISCONNESDR A6WA202201048048Warning Message · illuminatedSTAB TRIM CAUTION MSG IN FLT COULD NOT ENGAGE CHANNEL 1 OR 2 AT FLT LEVEL 340. CW QRH L.5 HRS LATER AT 6000 FT BOTH CHANNELS REENGAGED AND STAYED ENGAGED THE REMAINDER OF THE FLT. NORMAL LANDING FLAPS 20. AIRCRAFT REMOVED FROM SERVICE. PERFORMED SUP 05-0SDR A6WA202111297997None · noneWHILE ENROUTE TO PWM THE CREW REPORTED RECEIVING A STAB TRIM AND MACH TRIM CAUTION. THEY DECLARED AND EMERGENCY AND WILL CONTINUE TO PWM. AT FL310 RECEIVED STAB & MACH TRIM CAUTIONS. C/W QRH, TRIM WOULD NOT RE-ENGAGE. ***AIRCRAFT REMOVED FROM SERVICE*** SDR A6WA202107227838Skin · dentedLEFT HAND WING INBOARD LEADING EDGE HAS 3 DENTS AT WS96.134-WS101.00, WS101.00 Ï¿½ WS108.70 AND WS124.10 - 131.80. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DRESS BACK OF DENTS #1 AND #3 TO ORIGINAL CONTOUR PER GREO 601R-57-41-436 REV A DATED 2013-06-19.SDR A6WA202107207828Rib · corrodedRH WING RIB CHANNEL IS PITTING CORROSION AT WS53.60 AND WHEEL WELL HYDRAULIC GUARD ACCESS PANEL AREA. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND RIB CHANNEL CORROSION TO BE OUT OF LIMITS CREATING A HOLE THROUGH RIB CHANNEL THICKNESS OF 0.050Ï¿½. REMOVED ASDR A6WA202107087816Skin · corrodedCORROSION ON SKIN AT UPPER TCAS ANTENNA AT TWO LOCATIONS BETWEEN FS295 TO FS310. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON SKIN AT UPPER TCAS ANTENNA LOCATION FS295 + 4Ï¿½, RH STR 0 + 2Ï¿½, DIMENSION L = 3.00Ï¿½ X W = 2.00Ï¿½ SDR A6WA202107027809Skin · scratchedSCRATCH ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED SRM 57-52-00 INBOARD FLAP REPAIR NO. 2 ON LH INBOARD FLAP UPPER SKIN AT INBOARD TRAILING EDGE. CUTOUT DAMAGED SECTION OF UPPER SKIN INBOARD TRAILINSDR A6WA202107207830Frame · gougedFUSELAGE FRAME AT FS718 HAS TWO GOUGES; 1 AT STR26L AND ANOTHER AT STR25R. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE AT FS718 AND STR26L MEASURING .280"L X .200"W X .011"D AND GOUGE AT FS718 AND STR25R MEASURING .600"L X .200"W X .013"D IAW CRJ200 SDR A6WA202107097819Bulkhead Web · damagedTHREE SCRATCH DAMAGES ON FORWARD FACE OF FS621 BULKHEAD WEB P/N 601R36008. #1 RBL23.875 TO RBL24.25 AT WL135.50 TO WL136.00, MEASURES L = 0.700Ï¿½ X W = 0.200Ï¿½ X D = 0.003Ï¿½ #2 RBL22.125 TO RBL22.325 AT WL134.25, MEASURES L = 0.400Ï¿½ X W = 0.200Ï¿½ X D = 0SDR A6WA202107207829Skin · damagedELONGATED FASTENER HOLE AND TOOLING DAMAGE LH AFT FUSELAGE SKIN AT FS559.00 + 64 Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A REPAIR AT LH AFT FUSELAGE SKIN AT FS559.00 + 64Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ELONGATSDR A6WA202107087817Plate · corrodedCORROSION ON DOOR SILL PANEL ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SERVICE DOOR SILL PANEL P/N 601R38957-31 AND SHIM P/N 601R38695-19 AT FS319 TO FS349. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-40-1SDR A6WA202107067811Angle · dentedCARGO DOOR FWD: TRACK FRAME HAS 4 EACH DENTS ON FLANGE AND THE UPPER/LOWER SUPPORT CHANNELS HAVE DENTS AND ARE BENT. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED/REPLACED FWD CARGO DOOR CAM TRACK ANGLE P/N: 601R35050-15 (NSN) AT FS 574 FROM STR 8LH TO STR 17LSDR A6WA202106177826Door · chafedRH BUTTE DOOR (694PB) HAS CHAFFING CONDITION ON LOWER SURFACE AT WS242. ****AIRCRAFT REMOVED FROM SERVICE****** BLENDED CHAFFING CONDITION ON RH BUTTE DOOR (694PB) LOWER SURFACE AT WS242. ORIGINAL MATERIAL THICKNESS 0.040Ï¿½, MATERIAL LOSS 0.006Ï¿½ WITH RSDR A6WA202107097822Frame · dentedDENTS AND GOUGES ON FUSELAGE AFT FRAME FS682.00Ï¿½ STR S26L TO S27. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE DAMAGE AND HAND DRESSED DENTS TO FUSELAGE FRAME AT FS682.00 STR S26L TO S27. DENT DAMAGE MEASURES L = 7.250Ï¿½ X W = 0.500Ï¿½ X D = 0.070Ï¿½SDR A6WA202107097820Frame · dentedAFT FUSELAGE FRAME DENT FS672.20Ï¿½ STR26R-S27. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED FRAME AT AFT FUSELAGE FS672.20Ï¿½ STR26R-S27. DAMAGE MEASURES L = 1.300Ï¿½ X W = 0.700Ï¿½ X D = 0.048Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTSDR A6WA202106307806Channel · dentedAFT EQUIPMENT COMPARTMENT FUSELAGE FRAME CHANNEL FROM FS 689.5 TO FS 694.00 STR 24 LH HAS MULTIPLE DENTS. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED DAMAGED FRAME CHANNEL AND REPLACED WITH FABRICATED FRAME CHANNEL AT FS 689.5 TO FS 694.00 STR 24 LH. NEW CHASDR A6WA202107097823Skin · dentedAFT FUSELAGE SKIN DENT FS625.30 + 13.5Ï¿½ S24R AND S25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON SKIN AT FS625.30 + 13.5Ï¿½ AND S24R AND S25R. MEASURES L = 0.650Ï¿½ X W = 0.500Ï¿½ X D = 0.005Ï¿½. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SSDR A6WA202107227837Bushing · excess playREFERENCE 347219/1 HORIZONTAL STABILIZER EXCESSIVE PLAY. HORIZONTAL STABILIZER PIVOT BUSHING DIAMETER HOLES IN THE AIRCRAFT STRUCTURE ARE BELOW THE REQUIREMENTS AWA MAINTENANCE TASK CARD SUPPLEMENT NUMBER 19-154 REV B, DATED 07/16/2019. ***AIRCRAFT REMOVESDR A6WA202107097821Skin · dentedAFT EQUIPMENT BAY DOOR PERMANENT REPAIR FS712.00Ï¿½ STR 24R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A PERMANENT REPAIR TO AFT EQUIPMENT BAY DOOR OUTER SKIN FS712.00 AND STR 24R. DAMAGE MEASURES L = 1.200Ï¿½ X W = 0.500Ï¿½ X D = 0.024Ï¿½. PERFORMED HFSDR A6WA202101057513Oil System · overheatedDURING CLIMB THROUGH FL220, NOTICED RT ENGINE OIL TEMP CLIMBING AND INDICATING IN THE RED AT 166. CW QRH FOR HIGH OIL TEMP. POWER LEVER ADJUSTMENTS DID NOT PREVENT OIL TEMP FROM CLIMBING. PERFORMED INFLIGHT ENGINE SHUTDOWN, AFTER SHUTDOWN, NEVER RECEIVED LOSDR A6WA202002247192Cable · damagedL/H VERTICAL STABILIZER AUTO PILOT SERVO HAS RUST ON CABLE AT DRUM. FOUND AUTO PILOT SERVO SERVO CABLE P/N S 601R900200-79 AND 601R90020-131 WITH MULTIPLE BROKEN CABLE STRANDS. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED DAMAGED CABLES P/N S 601R900SDR A6WA202002247193Fairing · damagedL/H T/R DIFFICULT TO OPEN & HAD L/H REV UNLOCK CAUTION AFTER CLEARING RUNWAY AMBER ICON REV ICON ON N1 GAUGE LEVER WAS DIFFICULT TO MOVE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED UPPER STANG FAIRING THAT WAS FOUND TO BE DAMAGED. NO FURTHER DAMAGESDR A6WA2019121047047Wire Harness · faultySUPPLEMENTAL INFORMATION, WOW INPUT CAUTION MSG RECEIVED INTERMITTENTLY SEVERAL TIMES AFTER T/O AND EARLY CLIMB. GEAR WAS STOWED IN UP POSITION WHEN MSG RECEIVED, MSG CLEARED WITHIN 10 MIN OF FLIGHT. AIRCRAFT REMOVED FROM SERVICE HISTORY OF A S02 CODE STOREDSDR A6WA2019062846683A/C Pack · failedAT APPROXIMATELY FL190, THE FLIGHT CREW NOTED THE FAILURE OF THE LEFT PACK, REDUCED AIRFLOW IN THE COCKPIT AND A CLIMBING CABIN PRESSURE. THE CREW INITIATED A DESCENT TO 10,000', DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. LOSS SDR A6WA2018032245697Bulkhead · crackedFWD SIDE OF APB IS CRACKED ABOVE AFT CARGO DOOR TRACK AT ITS END. FOUND ON HFEC INSP.SDR A6WA2018031345693Frame · crackedBS 333 FRAME ABOVE UPPER PAX DOOR SILL WAS FOUND CRACKED. REPLACED.SDR A6WA2018031345692Frame · crackedFRAME BS 605 IS CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.SDR A6WA2018031345691Bracket · crackedRT FUSELAGE BRACKET AT BS 461 FOUND CRACKED. REPLACED THE BRACKET.SDR A6WA2018031345688Drag Angle · crackedPAX DOOR AFT RISER DRAG ANGLE BY THE ASSIST MOTOR YOKE WAS CRACKED. REPLACED THE DRAG ANGLE.SDR A6WA2018031345689Bracket · crackedLEFT FUSELAGE BRACKET AT BS 461 WAS FOUND CRACKED. REPLACEDSDR A6WA2018031345686Bracket · crackedLEFT FUSELAGE BRACKET AT BS 473 WAS FOUND CRACKED. REPLACED THE BRACKET.SDR A6WA2018031345685Angle · crackedBEAM AT BS 280 UPPER ANGLE IS CRACKED JUST OTBD OF THE MLG ALTERNATE CABLE EXTENSION PULLEY BRACKET, OTBD OF LBL 9.SDR A6WA2018031345687Bracket · crackedRIGHT FUSELAGE BRACKET AT BS 473 FOUND CRACKED. REPLACED THE BRAKCET.SDR A6WA2018031345680Skin · damagedRIGHT INBD FLAP LOWER SKIN DENTED, 6 LOCATIONS AND PITTING IN TWO AREAS. REPLACED THE FLAP SKINSDR A6WA2018031345681Mount Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET FOUND CRACKED. REPLACED THE MOUNT.SDR A6WA2018031345682Skin · crackedLEFT FWD FUSELAGE SKIN IS CRACKED AT BS 202 BY FWD EQUIPMENT BAY AFT LATCH. REPLACED THE SKIN.SDR A6WA2018031345684Angle · crackedCARGO DOOR BEAM AFT LOWER ANGLE AT BS 621 BULKHEAD IS CRACKED. REPLACED THE BEAM.SDR A6WA2018031345683Beam · gougedBEAM INBD OF CARGO DOOR, BS 618 - 621 HAS SEVERAL GOUGES. REPLACED THE BEAM.SDR A6WA2018031345696Riser · crackedPAX DOOR LOWER STEP RISER IS CRACKED. REPAIRED IAW AWAC 13-134.SDR A6WA2018031345695Stringer · crackedSTRINGER 3L AFT OF BS 364, PAX DOOR UPPER SILL IS CRACKED. REPAIRED THE STRINGER IAW SRM 53-00-03.SDR A6WA2018031345694Bracket · crackedLEFT LOWER NOSE HYDRAULIC COMPARTMENT BRACKET ABOVE ACCUMULATOR IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.SDR A6WA2018030845666Fitting · crackedBATHTUB FITTING CRACKED AT FS 461, LBL9. REPLACED FITTING IAW SRM 51-42-06., 51-42-21.SDR A6WA2018030845669Floorbeam · corrodedFLOORBEAM CAP CORRODED AT FS574.00, RBL9 TO RBL27. REPLACED BEAM CAP IAW SRM5142-06, 53-00-00, 51-21-00, 51-41-11, 51-24-36.
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