N427ZW
Service difficulty reports · 203
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 = 'N427ZW' 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 = 'N427ZW' 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 A6WA202302128463Unknown · unknownSHORTLY AFTER LEVEL OFF AT FL320, REV'D EFIS COMP MON CAUTION FOR IAS. C/W QRH. AT FL320, CA SIDE INDICATED 270, FO'S SIDE INDICATED 282. AT FL300, CA SIDE INDICATED 240. FO'S SIDE INDICATED 295 KIAS. FO AND STANDBY WERE MATCHED WITH EACH OTHER. IAW QRH, SSDR A6WA202205168188Structure · damagedMULTIPLE DAMAGE TO A/C EXTERNAL POWER RECEPTACLE SURROUNDING STRUCTURE AT FS 193 TO FS 202.75 AND S23R TO S24R. ************AIRCRAFT REMOVED FROM SERVICE************************* CUT AWAY DAMAGED PORTION OF FWD DOOR LANDING DOUBLER P/N: 600-33042-325 WITH .2SDR A6WA202203138129Cowling · damagedREF 334833/1 DAMAGE FOUND ON RH ENG INLET COWL. AIRCRAFT REQUIRES INSPECTION FOR FURTHER DAMAGE. *** AIRCRAFT REMOVED FROM SERVICE *** PERV GVI OF NOSE AREA FOR BIRD STRIKE DAMAGE NO DEFECTS NOTED NO EVDIENCE OF ENG INJSETION IAW AMM 05-51-25-210-801. AC OK SDR A6WA202111307998Switch · failedAFTER TAKEOFF RECEIVED OVERBOARD COOL CAUTION MESSAGE AND IB COOL FAIL STATUS MESSAGE, PRESSURIZATION WAS ABNORMAL. CW QRH, DESCENT TO 10K FEET, WITH EMER DEPRESS SELECTED ON. PAX DOOR VENT FLAP WAS VERIFIED CLOSED ON ARRIVAL. AIRCRAFT REMOVED FROM SERVICSDR A6WA202111157970None · corrodedR/H FLOOR SILL AT FS 559+88, FS 559+101.75, AND FS 600 AT RBL 41 AROUND NUT PLATE HOLES HAVE CORROSION. FAA IDENTIFIED DURING AGING AIRCRAFT INSPECTION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION AT 4 EACH AREAS RBL 41: FS 559+88 (P1)= 1.4"L X 1"WSDR A6WA202111087953Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON LH SIDEWALL SEAT TRACKS AT FS364, FS386, FS394, FS409, FS409+8, FS409+16, FS409+32, FS409+40, FS409+64, FS409+96 AND FS409+128. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED LH SIDEWALL SEAT RAILS AT MULTIPLE LOCATIONS ON LHSDR A6WA202109167879Strap · corrodedCORROSION ON RH FLOOR PRESSURE SILL AND FLOOR STRAP AT FS559 AND RBL41. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON FLOOR STRAP P/N 601R31025-29 AT FS559 AND RBL27 TO RBL41 THAT WAS OUT OF LIMITS AND REPLACED WITH NEW FORMED SHEET ALUMINUM OF SDR A6WA202109087874Skin · damagedSCRIBE MARKS ON RH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128 AND S17R TO S27R ALONG SEALANT LINE OF WING TO BODY FAIRING 192BB. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRIBE MARKS ON RH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128SDR A6WA202110017892Skin · dentedDENT WITH CREASE ON AFT FUSELAGE SKIN AT FS634.00 AND S25L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN AT FS634.00 AND S25L. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.018Ï¿½. CUTOUT DIMENSIONS L= 1.600Ï¿½ SDR A6WA202109087868Floor Support · corrodedCORROSION AT TWO LOCATIONS ON FLOOR SILL LH SIDE AT FS353.00-FS359.00 AND LBL41. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON FLOOR SILL LH SIDE AT FS353.00-FS359.00 AND LBL41. P/N 601R31148. CORROSION DIMENSIONS P1 - L = 1.33Ï¿½SDR A6WA202109087867Floor Support · corrodedCORROSION ON FLOOR SILL RH AT FS353 RBL41, FS359 RBL41 AND FS384 RBL41 AROUND NUTPLATE HOLES. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON RH FLOOR SILL AT FS353 RBL41, FS359 RBL41 AND FS384 RBL41 AROUND NUTPLATE HOLES. P/N 601R31148. CORROSIOSDR A6WA202109087869Pressure Deck · corrodedCORROSION AT TWO LOCATIONS ON FLOOR SKIN PRESSURE PANEL LH BETWEEN FS514.00 Ï¿½ FS529.00 AND LBL41. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON FLOOR SKIN PRESSURE PANEL LH BETWEEN FS514.00 Ï¿½ FS529.0 AND LBL41. P/N 601R31145.SDR A6WA202108247939None · dentedRIGHT HAND WING LEADING EDGE SKIN (DWG: 601R12057, REF) HAS A DENT BETWEEN WS149.580 Ï¿½ WS158.523. PERFORMED DRESS BACK OF DENT ON RIGHT HAND WING LEADING EDGE SKIN (DWG: 601R12057 REF) BETWEEN WS149.580 Ï¿½ WS158.523. DENT DIMENSIONS L = 5.750Ï¿½ X W = 1SDR A6WA202109287891None · corrodedCORROSION ON SERVICE DOOR LOWER SILL AT BETWEEN FS319.00 AND FS349.00. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON SERVICE DOOR LOWER SILL AT BETWEEN FS319.00 AND FS349.00. FLOOR ANGLE P/N 601R338303-167. MEASUREMENTS P1 - L= 4.200Ï¿½ X W= 2.60SDR A6WA202108187936Plate · corrodedSERVICE DOOR PLATE HAS CORROSION AT FS319 TO FS349 RH. REMOVED AND REPLACED WITH A NEW SERVICE DOOR PLATE AT FS319 TO FS349 RH. PN 601R38957-31. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 51-41-02 REV 38. WORK PERFORMED UNDERSDR A6WA202110217919Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON RH SIDEWALL SEAT TRACKS AT FS424, FS439, FS461, FS478, FS484, FS499, FS513, FS559+24 AND FS559+56. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H SIDEWALL SEAT RAILS AT MULTIPLE CORROSION AT FS424, FS439, FS461, FS478, SDR A6WA202110217917Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON L/H SIDEWALL SEAT TRACKS AT FS424, FS439, FS461, FS473.15, FS484, FS499, FS513, FS529, FS544, FS559+8 AND FS559+64. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED L/H SIDEWALL SEAT RAILS AT MULTIPLE CORROSION AT FS 424, FS43SDR A6WA202110217918Seat Track · corrodedCORROSION AT MULTIPLE LOCATIONS ON R/H SIDEWALL SEAT TRACKS AT FS379, FS401, FS409+8, FS409+24, FS409+32, FS409+48, FS409+64, FS409+80, FS409+112 AND FS409+128. ***AIRCRAFT REMOVED FROM SERVICE*** CORROSION AT MULTIPLE LOCATIONS ON R/H SIDEWALL SEAT TRACKS SDR A6WA202109087870Skin · gougedSCRIBE MARKS ON LH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128 AND S17L TO S27L ALONG SEALANT LINE OF WING TO BODY FAIRING 191BB. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SCRIBE MARKS ON LH FORWARD FUSELAGE SKIN FS409.00 + 64 TO FS409.00 + 128SDR A6WA202108157938Cowl Door · gougedRH ENGINE LOWER CORE COWL HAS A GOUGE DAMAGE ON INNER SKIN BETWEEN XN166.00 AND XN168.00. PERFORMED DOUBLER REPAIR TO RH ENGINE LOWER CORE COWL HAS A GOUGE DAMAGE ON INNER SKIN BETWEEN XN166.00 AND XN168.00. P/N 228-50162-418. DAMAGE MEASUREMENTS ARE L = 0SDR A6WA202109087871Skin · damagedNUMBER 2 ENGINE LOWER COWL HAS DAMAGE ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO NUMBER 2 ENGINE LOWER COWL ON THE LOWER EDGE OF CORE BETWEEN XN170.73 AND XN176.5. P/N 228-50162-4SDR A6WA202109087872Skin · dentedDENT ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S18R TO S19R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENTED SKIN TO ORIGINAL CONTOUR ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S18R TO S19R TO ORIGINAL CONTOUR. P/N 601R35005. DENT MEASUREMENT L = 0.8SDR A6WA202109087873Skin · dentedDENT ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S24R TO S25R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENTED SKIN ON FUSELAGE SKIN FS625.00 TO FS640.00 AND S24R TO S25R TO ORIGINAL CONTOUR. P/N 601R35005. DENT MEASUREMENTS L = 0.500Ï¿½ X W = 0.450ÏSDR A6WA202108307864Skin · dentedDENT AFT FUSELAGE SKIN AT FS656 S20R - S21R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO AFT FUSELAGE SKIN AT FS656 S20R - S21R. DENT DIMENSIONS L = 0.900Ï¿½ X W = 0.800Ï¿½ X D = 0.010Ï¿½. CUTOUT DIMENSIONS L=7.50Ï¿½ X W = 4.50Ï¿½. FSDR A6WA202110017893Skin · dentedDENT ON FORWARD FUSELAGE SKIN AT FS280.00 Ï¿½ FS295.0 AND S22R TO S23R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON FORWARD FUSELAGE SKIN AT FS280.00 Ï¿½ FS295.0 AND S22R TO S23R AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSION L = 1.20Ï¿½ X W = SDR A6WA202109177881Panel · damagedBLENDED TOOL MARK DAMAGE ON PANEL 650LB TO A SMOOTH CONTOUR. PERFORMED HFEC WITH NO INDICATIONS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED TOOL MARK DAMAGE ON PANEL 650LB TO A SMOOTH CONTOUR. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISSDR A6WA202111087954None · crackedCRACK INDICATION ON RH WING LOWER PLANK AT WS 65.75 BETWEEN STR 15R AND STR 16R. CRACK DIMENSIONS ARE 2.00"(L) X .001" (W). ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED 2.2" (L) X 1.8" (W) CUTOUT OF LOWER FWD PLANK, 3.9" (L) X 2.35" (W) CUTOUT OF LOWER MIDSDR A6WA201904296590Structure · puncturedPUNCTURE 1.25" LONG AT FS 625.30 STR 18RSDR A6WA2018020645612Smoke Detector · faultySMOKE TOILET CAUTION MESSAGE RECEIVED IN FLIGHT. FLIGHT DIVERTED TO MKE. CREW COMPLIED WITH QRH. MESSAGE PERSISTED FOR ABOUT TWO MINUTES. LAV WAS UNOCCUPIED. PER MX CONTROL REMOVED AND REPLACED LAV SMOKE DETECTOR PER AMM 26-16. OPS CK GOOD.SDR A6WA201845542Frame · corrodedFRAME BS 605 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26L IN THE CARGO BAY.SDR A6WA2017010245533Skin · dentedLEFT INBD FLAP LOWER SKIN DENTED ON T/E CORNER. REPAIRED THE FLAP SKIN IAW SRM 57-52-00.SDR A6WA2017010245516Angle · crackedANGLE CRACKED ON THE INBD SIDE OF FRAME BS 625.3, STRINGER 13R IN THE AFT EQUIPMENT BAY. REPLACED THE ANGLE IAW SRM 51-42-21.SDR A6WA2017010245518Floorbeam · crackedBS 280 FWD FLOORBEAM ANGLE FOUND CRACKED AT RIVET HOLE, RBL 6. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.SDR A6WA2017010245517Frame · crackedFRAME BS 605 IS CRACKED JUST ABOVE AND BELOW STRINGER 9L IN THE CARGO BAY. REPAIRED THE FRAME IAW REO 601R-53-61-5214, REV A.SDR A6WA2017010245501Seat Track · corrodedLT AISLE SEAT TRACK BETWEEN BS 364 AND 409+16 CORRODED. REPLACED THE SEAT TRACK.SDR A6WA2017010245500Floor Support · corrodedRBL 9 FLOOR SUPPORT LANDING BETWEEN BS 559+64 AND 559+80 CORRODED. REPAIRED THE FLOOR SUPPORT.SDR A6WA2017010245515Floorbeam · crackedRIGHT BS 280 FLOORBEAM UPPER CAP ANGLE CRACKED, FWD SIDE OTBD ON RBL 9. REPAIRED THE FLOORBEAM UPPER CAP ANGLE IAW REO 601R-53-11-137, REV-A.SDR A6WA2017010245524Angle · crackedANGLE IS CRACKED AT THE INBD SIDE OF RBL 36, BS 484. REPLACED THE ANGLE IAW SRM 51-42-20, AND 51-42-11.SDR A6WA2017010245522Floorbeam · crackedLBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ANGLE IAW SRM 51-42-21.SDR A6WA2017010245519Attach Angle · crackedLBL 9 FLOORBEAM INBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.SDR A6WA2017010245521Attach Angle · crackedRBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.SDR A6WA2017010245523Angle · crackedANGLE CRACKED AT BS 484, OTBD OF LBL 9. REPLACED THE ANGLE IAW SRM 51-42-20.SDR A6WA2017010245520Floorbeam · crackedRBL 9 FLOORBEAM INBD ATTACH ANGLE IS CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.SDR A6WA2017010245503Seat Track · corrodedLEFT ISLE SEAT TRACK NR 2 CORRODED BETWEEN BS 409+16 TO 409+128, LBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11.SDR A6WA2017010245504Seat Track · corrodedLEFT SEAT TRACK NR 3 CORRODED FROM BS 409+128 TO 559, LBL 9. REPLACED THE SEAT TRACK IAW AMM 53-01-11.SDR A6WA2017091845289Sensor · out of adjustAFTER TAKEOFF, RECEIVED A STEERING INOPERATIVE AND WOW INPUT CAUTION MESSAGES. RETURNED TO DEPARTURE. ADJUSTED THE AFT NLG DOOR AND WOW SENSORS. OK FOR CONTINUED SERVICE.SDR A6WA201745265Actuator · malfunctionedYOKE STUCK ONCE, AUTOPILOT DISCONNECT FOR TWO SECONDS. CAPTAIN PUT AFT FORCE TO FREE YOKE. OCCURRED ON APPROACH WHILE AUTOPILOT IN DESCENT MODE. REMOVED AND REPLACED ELEVATOR SERVO ACTUATOR IAW AMM 22-11, OPS CHECKED GOOD.SDR A6WA201644336Sign · unsecureFLIGHT 3941, EXIT SIGN ABOVE SERVICE DOOR HANGING DOWN BY WIRES. IT WAS PLACED ON THE MEL LIST.SDR A6WA201643783Cooling Fan · vibrationIN LEVEL FLIGHT AT 11,000 FT, AUTOPILOT OFF, EXPERIENCED AN AIRFRAME VIBRATION AT APPROX 240 KTS. VIBRATION WAS FELT IN THE AIRFRAME, NOT & OF THE FLIGHT CONTROLS. FLIGHT CONTROL SYNOPTIC PAGE APPEARED NORMAL. VIBRATION DECREASE & WENT AWAY BELOW 230 KTS. SDR A6WA201643445Cam · obstructedPASSENGER DOOR WILL NOT OPEN OUTSIDE OR INSIDE. REMOVED SCREW UNDER LOCK CAM ASSEMBLY. CLEANED & LUBED PAX DOOR, OPERATIONS CHECKED GOOD.
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