N434AW
Service difficulty reports · 281
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 = 'N434AW' 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 = 'N434AW' 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 A6WA202408158792Outflow Valve · failedDURING CLIMB NOTICED CABIN ALTITUDE CLIMBING ABNORMALLY HIGH. RECEIVED CABIN ALT CAUTION MSG. FOLLOWED BY CABIN ALT WARNING. CW IAC AND QRH CMSGS CLEARED IN DECENT. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND OVB EXHAUST SOV NOT FULLY CLOSED. SET TO SDR A6WA202407278782Panel · openAFTER TAKEOFF FROM KCMH & GEAR WERE RETRACTED, CREW HEARD AN UNUSUAL NOISE. NO CAUTION OR WARNING MESSAGE NOTED BY CREW. VOLUME OF NOISE INCREASED ABOVE 250 KNOTS. CREW CONTACTED ATC TO MAKE AWARE OF SITUATION & DECLARED AN EMERGENCY. FLIGHT ATTENDANT & PAX BRSDR A6WA202402068716Skin · dentedCREW REPORTED DENT LOCATED ON UPPER LH WINGSKIN DURING WALKAROUND. WORKING WITH MHI, DENT WAS FOUND TO BE A PREVIOUS BLEND REPAIR WITH UNDERLYING FREEZE PLUG IN THE FWD AND MID WING PLANKS. MHI OR AWA COULD NOT FIND ANY DOCUMENTATION FOR THIS REPAIR. MHI ISSDR A6WA202303288640Spar · damagedFOUND DRILL START DAMAGE ON RH WINGLET REAR SPAR P/N: 600-15104-6 ON THE IB SIDE OF THE REAR SPAR CHANNEL BETWEEN WGLT STA 6.36 - 12.50 MEASURING 0.180"L X 0.180"W X 0.026"D. AIRCRAFT REMOVED FROM SERVICE. BLENDED OUT DRILL START DAMAGE TO A SMOOTH CONTOURSDR A6WA202303288639Skin · dentedFOUND 3 DENTS ON FUSELAGE SKIN AROUND PASSENGER DOOR CUTOUT, FS 310, STR 14L - 15L = 1.2"L X .400"W X .315"D; FS 349 AT STR 14L = 2.8"L X .350"W X .162"D; AND FS 349, STR 15L - 16L = 0.9"L X 0.320"W X 0.145"D. AIRCRAFT REMOVED FROM SERVICE. PERFORMED TRIM OSDR A6WA202205208501Skin · noneLEFT-WING LEADING-EDGE SKIN P/N 601R12074-3 SHOWS EROSION/ROUGHNESS OF 0.005" MULTIPLE SPOTS. ******AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED LEADING EDGE SKIN P/N 601R12074-3.SDR A6WA202205108510Unknown · unknownRIGHT-WING LEADING-EDGE SHOWS SIGNS OF ROUGHNESS ********AIRCRAFT REMOVED FROM SERVICE********* RE-SKIN OTB SECTION OF RH WING OUTB LEADING EDGE AND INSTALLED 1 EA RIB AND 1 EA STRAPSDR A6WA202205098502Skin · noneLH OUTBOARD LEADING EDGE SKIN P/N 601R12074-3 FOUND ERODED BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** REMOVED AND REPLACED SKIN P/N 601R12074-3.SDR A6WA202204118483Angle · crackedFLOOR SUPPORT ANGLE ALONG FS621 BULKHEAD OUTBOARD OF FLOOR BEAM LBL27 IS CRACKED (MARKED) *****AIRCRAFT REMOVED FROM SERVICE***** R&R -1 ANGLE, (EXISTING REPAIR), REF BOMBARDIER REO 601R-53-61-117 REV-D DATED 2017-02-26 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51SDR A6WA202204088484None · noneDENT RH OTBD FLAP UPPER SKIN *****AIRCRAFT REMOVED FROM SERVICE**** REPAIREDSDR A6WA202202218117None · noneUPON FIRST WALK AROUND FO FOUND LH STANG FAIRING MISSING. R&R LH ENG STANG FAIRING IAW AMM 78-34SDR A6WA202106157803Transceiver · faultedWEATHER RDR TURNED ITSELF OFF AND WOULD NOT TURN BACK ON . AIRCRAFT REMOVED FROM SERVICE. R&R WEATHER RADAR RECIEVER/TRANSMITTER ASSY IAW AMM 34-41-01. OPS TEST GOOD. SN REMOVED: 1C6WV SN INSTALLED: 58VUSDR A6WA202104127737Pseu · fault messagePROX SYS CHAN CAUTION MSG IN FLIGHT. QRH C/W. MANUALLY EXTENDED LANDING GEAR. INSTALLED GEAR PINS. ***AIRCRAFT REMOVED FROM SERVICE*** INTERROGATED PSEU, FOUND CODES A01-A06 AND RED FAIL LIGHT ILLUMINATED. R&R PSEU IAW AMM 32-61-01. OPS CHECK GOOD. GESDR A6WA202104067735Floorbeam · damagedTOOL MARK COMMON TO FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED TOOL MARK ON FLOOR STRUCTURE WEB AT FS364.00+8 AND LBL28 WITH BLEND DIMENSIONS OF 0.600Ï¿½L X 0.500Ï¿½W X 0.027Ï¿½D WITH A REMAINING THICKNESS OR 0.0SDR A6WA202103247726Seat Track · corrodedSEAT TRACK HAS CORROSION AND GOUGES WITH CORROSION COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL 9. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED SEAT TRACK COMMON TO CENTER OF SEAT TRACK AT FS 379.00+3 TO FS 379.00+11 LBL SDR A6WA202103227720Beam · damagedLIGHTNING HOLE HAS TORN AREAS X2 AT TOP OF HOLE FS 409.00+69+11.5" TO FS409.00+96+13 RBL 8 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 DAMAGED AREAS ON LIGHTNING HOLES AT FS 409.00+69+11.5 TO 409.00+69+13 RBL 8 FOUND WITHIN LIMITS REF ASAP EA# AWAC-CRJ25SDR A6WA202103267730Skin · damagedRT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650BB HAS CRACK INDICATION AT AFT INBOARD ARC APPROX. WS180.00, INDICATION MEASURES APPROX. 0.10. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WING LOWER PLANK ACCESS PANSDR A6WA202103267731Skin · damagedRT WING LOWER PLANK ACCESS PANEL CUTOUT AT 650AB HAS CRACK INDICATION AT OUTBOARD ARC APPROX. WS173.00, INDICATION MEASURES APPROX. 0.10. (INITIATES AWAC EO6/021/457) ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED BLEND AT CRACK INDICATION LOCATION ON R/H WISDR A6WA202103247725Door Frame · crackedPAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AFT ***AIRCRAFT REMOVED FROM SERVICE*** PAX DOOR STRUCTURE O/B PANEL UPPER EDGE INTERIOR SUSPECTED 2'' CRACK O/B OF STEP BULKHD BOTTOM STEP LOOKING AFSDR A6WA202103227721Fairing · gougedSTAB FAIRING 326CR GOUGED FROM STAB MOVEMENT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE ON VERTICAL STABILIZER FAIRING PANEL 326CR. FOUND WITHIN LIMITS REF EA# AWAC-CRJ255-01588 REV A DATED 3/19/2021SDR A6WA202103197719Bulkhead Web · damagedREAR PRESSURE BULKHEAD FORWARD FACE HAS SCRATCHES COMMON TO FORWARD SIDE OF 621.00 BULKHEAD LBL 18 AT TOP OF BULKHEAD AROUND CANNON PLUGS. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED THREE BLENDED AREAS ON REAR PRESSURE BULKHEAD DOUBLER FORWARD FACE OF UPPSDR A6WA202103197718Skin · dentedINWARD DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROXIMATELY WING STATION 106.40. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT COMMON TO EXTERIOR SKIN, LOWER SIDE OF INBOARD RIGHT HAND FLAP AT APPROX. WING STATION 106.40SDR A6WA202103157713Skin · dentedINWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3.75, STR 23L+4.25. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 265.00+3.75, SR 23L+4.25 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED, REF ASAP EA# AWAC-CRJ-253-0158SDR A6WA202103157714Skin · dentedINWARD DENT COMMON TO EXTERIOR SKIN AT FS 235.00-13, STRINGER 24L+4 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 235.00+13, STR 24L+4 TO ORIGINAL CONTOUR, HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# CRJ253-01586 REV IR DTSDR A6WA202103157716Skin · dentedINWARD DENT COMMON TO EXTERIOR SKIN AT FS 265.00+3, STR 23L+1 ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED INWARD DENT AT FS 265.00+3 STR 23L+1 TO ORIGINAL CONTOUR. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF ASAP EA# AWAC - CRJ253-01585 REVSDR A6WA202010257348Bpsu · failedWHILE AT CRUISE FL300, FLAP FAIL CAUTION MESSAGE APPEARED WITH NO INPUT ON FLAP HANDLE. RAN QRH. TOUCHDOWN BELOW MAX LANDING WEIGHT. BRAKE TEMP MAX WERE 5 RT OUTBOARD BRAKE. FLAP FAIL REMAINED DISPLAYED ON TAXI TO GATE. PERFORMED FLAP RESET PROCEDURE, IASDR A6WA2020041347257Circuit Breaker · shortedON TAKE-OFF ROLL, PRIOR TO ROTATION, WE SAW AND HEARD ELECTRICAL FLASHES BEHIND CAPTAIN AND SCREENS FLICKERED, ALSO SMELLED ELECTRICAL SMOKE BRIEFLY. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND RAZOR BLADE MAKING CONTACT WITH CBP1-A2 AND A5 (FORSDR A6WA202002147182Floor Support · corrodedRH FLOOR SILL IN AFT CARGO HAS SPOTS OF CORROSION, FS559.00+80 TO FS559.00+112. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL - .063 MATERIAL LOSS - .063 REMAINING THICKNESS - .000 ALLOWABLE LIMITS - .015 REMOVED AND REPLACED FSDR A6WA2020021347174Floor Support · corrodedFLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM FS409.00+128 TO FS559.00, RBL 9 AIRCRAFT REMOVED FROM SERVICE ORIGINAL MATERIAL .063 MATERIAL REMOVED .026 REMAINING MATERIAL .037 ALLOWABLE LOSS .005 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-01439SDR A6WA2020021347170Bulkhead Web · crackedAFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0, WL 111.00. AIRCRAFT REMOVED FROM SERVICE WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING BOMBARSDR A6WA2020021347172Frame · corrodedFRAME 333 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGERS 25R AND 26L. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS .050 MATERIAL LOSS .012 REMAINING MATERIAL .038 ALLOWABLE LOSS .005 REMOVED AND REPLACED FRAMESDR A6WA2020021247167Floor Support · corrodedFLOOR SUPPORT IS CORRODED IN NUMEROUS LOCATIONS FROM 409+128-559.00, INBD SIDE OF BEAM. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS .063 MATERIAL LOSS .026 REMAINING MATERIAL .037 REPAIRED FLOOR SUPPORT IAW EA AWAC-CRJ253-0SDR A6WA2020021247168Strap · corrodedFLOOR SUPPORT STRAP IS CORRODED AT FS559.00+112, RBL27-RBL45. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL .100 MATERIAL LOSS .013 REMAINING MATERIAL .087 ALLOWABLE LOSS .010 REMOVED AND REPLACED STRAP IAW CRJ200 SRM 51-42-06SDR A6WA2020021247162Floor Support · corrodedFLOOR SUPPORT IS CORRODED FROM FS574.00 TO FS621.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION IAW CRJ200 SRM 53-61-43 & 51-31-59. ORIGINAL THICKNESS .050 ALLOWABLE LOSS .020 ACTUAL MATERIAL LOSS .050 REMAINING THICKNESS .000 REMOVEDSDR A6WA2020021147161Floor Support · corrodedFLOOR SUPPORT IS CORRODED AT FS584.00, RBL 9. AIRCRAFT REMOVED FROM SERVICE REMOVED CORROSION IAW AWAC SUPPLEMENT 19-206. ORIGINAL THICKNESS .050 MATERIAL LOST .029 ALLOWABLE LOSS LIMITS .013 REMAINING THICKNESS .021 REMOVED AND REPLACED FLOOR BEAM IAW BOMBSDR A6WA2020021147159Spar · damagedL/H WING FRONT SPAR HAS DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE. AIRCRAFT REMOVED FROM SERVICE REPAIRED L/H WING FRONT SPAR DOUBLE DRILLED HOLE AT TOP CENTER OF CENTER LEADING EDGE IAW BOMB. REO 601R57-00-116.SDR A6WA2020021147158Floor Support · corrodedFLOOR SUPPORT IS CORRODED AT FS621.00 TO FS574, LBL 9. AIRCRAFT REMOVED FROM SERVICE REPAIRED FLOOR SUPPORT IAW AWAC SUPPLEMENT 20-024.SDR A6WA2020021147157Angle · crackedRIB ON LH PYLON LOWER FLANGE CRACKED FS605. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED IAW AWAC SUPPLEMENT 14-252A.SDR A6WA20200207156Strap · corrodedFLOOR STRAP AT FS559.00, RBL 45 TO RBL 27, IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLOOR STRAP IAW CRJ200 SRM 51-42-06 AND TR 51-42.SDR A6WA20200207155Access Panel · crackedPANEL 630BL HAS CHAFFING ON INNER SURFACE. CRACK INDICATIONS NOTED DURING HFEC INSPECTION OF REPAIRED SURFACE. AIRCRAFT REMOVED FROM SERVICE REPAIRED PANEL 630BL IAW AWAC SUPPLEMENT 19-218A.SDR A6WA2020020547152Bracket · corrodedLEFT WING TRANSITION PICOLLO TUBE BRACKET BETWEEN INBOARD AND CENTER LEADING EDGES IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED PICOLLO TUBE TRANSITION TUBE BRACKET IAW CRJ200 SRM 51-42-06 % 51-41-06.SDR A6WA202002057151Seat Track · corrodedLEFT SIDE SEAT TRACK BETWEEN FS449.85 & FS499.00 HAS CORROSION AND GOUGED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.SDR A6WA202020347146Frame · corrodedFRAME 310 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGER 24L AND 24R, IN THE FWD E&E BAY. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FRAME SEGMENT IAW CRJ200 SRM 51-42-06 AND 51-42-21.SDR A6WA202020347145Floorbeam · corrodedFLOOR SUPPORT IS CORRODED AT FS589.00, LBL 9 TO LBL 27. AIRCRAFT REMOVED FROM SERVICE INSTALLED NEW FABRICATED CAP STRIP AT FLOOR SUPPORT AT FS589.00, LBL 9 TO LBL 27 IAW CRJ200 SRM 51-42-06, 51-24-36 AND TR 51-42.SDR A6WA2020020347147Frame Angle · corrodedFRAME 409 AFT ANGLE SPLICE HAS CORROSION SPOTS BETWEEN STRINGER 26L THRU 26R IN THE FWD E&E BAY AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE AT FRAME 409 AFT ANGLE SPLICE BETWEEN STINGER 26L AND 26R AND INSTALLED NEW ANLGE SPLICE IAW CRJ 200 SRM 51-42-06 ANSDR A6WA2020020347143Seat Track · corrodedCARGO SEAT TRACK AT FS559+112 TO FS574, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-00-49.SDR A6WA202020347144Seat Track · corrodedCARGO SEAT TRACK AT FS559+86 TO FS559+96, RBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.SDR A6WA202020347140Seat Track · corrodedCARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO TRACK IAW CRJ200 AMM 53-00-49.SDR A6WA202020347141Seat Track · corrodedCARGO SEAT TRACK AT FS559+112 TO FS574.00, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.SDR A6WA202020347142Seat Track · corrodedCARGO SEAT TRACK AT FS559+86 TO FS559+96, LBL 9 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CARGO SEAT TRACK IAW CRJ200 AMM 53-00-49.
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