N470ZW
Service difficulty reports · 157
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 = 'N470ZW' 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 = 'N470ZW' 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 A6WA202501038850Idg · faultedDURING CRUISE AT 30,000FT FOR FLIGHT 6024 CAE-ORD, THE FLIGHT CREW REPORTED A LOSS OF ELECTRICAL POWER. THE FLIGHT CREW DECLARED AN EMERGENCY AND IS RETURNING TO CAE. THIS FLIGHT IS STILL ENROUTE. SHORTLY AFTER LEVEL OFF AT CRUSE RECEIVED GEN 2 FAIL AND AC 2 ASDR A6WA202410128835Bpsu · faultedFLAP FAIL AT ZERO IN CRUISE AIRCRAFT REMOVED FROM SERVICE R+R LH BPSU IAW SUPP 04-048B. OPS CHECK GOOD. REMOVED PLACARD + REMOVED FROM MEL. P/N 855D100-15 S/N OFF 2363 S/N ON 2480 KSGSDR A6WA202410108834Bpsu · failedWHILE EXTENDING FLAP TO 8 DEG ON APPROACH, RCVD "FLAP FAIL" CAUTION MESSAGE. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R LFT BPSU OPS CHECK GOOD AT THISDR A6WA202406068763Electronic Unit · faultedRECEIVED FLAP FAIL CAUTION AT FL 230 IN CRUISE. COMPLETED AND COMPLETED WITH QRH BTMS READ 6,5,4,6 PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLMENT 98-018I BOX 12 FLAPS RESET PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE R & R FECU/ ADJUSTSDR A6WA202406048762Potentiometer · out of adjustUPON DESCENT FROM CRUISE, FLAPS FAIL AT 0 DEGREES C/W QRH. FLAP HANDLE WAS NOT TOUCHED. AIRCRAFT REMOVED FROM SERVICE. ADJUSTED FLAP FECU POTENTIOMETERS IAW AMM 27-51-10 SUBTASK 27-51-10-830/008, REF 353376-3 FOR TS PER AWAC SUPP 98-018I. OPS CK GOOD.SDR A6WA202406048761Flap System · warning messageAT FL240, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS AT 0 DEGREES. BTMS TEMPS 4,3,4 AND 7. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FLAPS PLACED ON MEL AND JOBSDR A6WA202403208726Proximity Sensor · faultedAFTER TAKE OFF RECEIVED NWS CAUTION MSG AND WOW INPUT. MSGS APPEARED APROX 6 SECONDS AFTER GEAR SELECTION. C/W QRH MGS PERSISTED, DURRING APPROCH; WITH GEAR UP AND FLAPS AT 0, MSGS CLEARED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED NLG PROX SENSOR ADJUSTMNESDR A6WA202403087721Rvdt · faulted30 SECONDS AFTER TAKE-OFF, RECEIVED NWS INOP CAUTION MESSAGE. C/W QRH. MESSAGE DID NOT CLEAR. AIRCRAFT REMOVED FROM SERVICE. REF WO 334202 WC #9 FOR CORRECTIVE ACTION. R & R RVTD WO 334202: INSTALLED AND RIGGED LT NWS RVDT PER AMM SUP 15-177A AND RIGGEDSDR A6WA202401208703Proximity Sensor · faultedAFTER T/O RECEIVED HAD NOSE DOOR AND GEAR DISAGREE WARNING MSG RAN QRH ALL GEAR WAS EXTENDED. MSG APPEARED APROX 5 SECONDS OF HANDLE MOVEMENT. LANDING WEIGHT 44,000LBS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NLG CENTERED/EXTENDED BRACKET IAW ASDR A6WA202312288685Engine · unknownDURING CLIMB OUT RT ENG ITT SPIKED TO 980 PLUS DEGREES SOUND (BANG) AND VIBRATION HEARD, RT FUEL LOW PRESSURE CAUTION MSG RECEIVED C/W QRH RH ENGINE UNRESPONSIVE. CONT LOG PAGE 363235/1 SELECTED IDLE, INDICATIONS AS FOLLOWS, N1 28 %, ITT 750 DEG C, N2 57 %, ASDR A6WA202309058652Unknown · unknownAT 12K FT RECEIVED MLG BAY OVERHEAT MESSAGE. C/W QRH MESSAGE REMAINED. BTMS READ 1'S. GEAR WAS DOWN. ALL TEMP INDICATIONS NORMAL. *******AIRCRAFT REMOVED FROM SERVICE*********** REF 352283-1 FOR CORRECTIVE ACTION R+R WHEEL BINS. R+R BOTH WHEEL BINS, OPS CHECSDR A6WA202307088637Unknown · unknown9883 - OXY LO PRESS AT 1180 PSI NEED REPLENISHED. AIRCRAFT REMOVED FROM SERVICE. SERVICED CREW O2 TO 1820 PSI. IAW AWAC SUP 09-053ESDR A6WA202305178608Doubler · unknownTOOLING MARKS ON LH FS424.00 ****AIRCRAFT REMOVED FROM SERVICE******* BLENDED TOOL MARKINGS ON LH SKIRT DOUBLER PN 601R31145 -323 AT FS424.00 UNDER ACCESS PANEL WING TO FUSELAGE FRAME ATTACHMENT FWD 161CL. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTISDR A6WA202304018627Floor Support · corrodedCORROSION ON LH FLOOR SILL P/N: 601R31133-47 AND P/N: 601R31133-77 AT FS 574.00+ 12 TO FS 605+12 AND LBL42. CRACK 0.300Ï¿½L X 0.010Ï¿½W ON L/H FLOOR LANDING PLATE P/N: 601R35001-63 AT FS 605.00 AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ATSDR A6WA202304018626Angle · corrodedCORROSION ON FLOOR SILL STRAP P/N 601R31025-29 AT FS280.00 AND LBL 9 TO RBL9. ***** AC REMOVED FROM SERVICE ***** BLENDED CORROSION ON 3 AREAS AT FS280.00 RBL9 TO LBL9. P1-L=2.5IN X W=1.5IN X D=0.036 P2-L=4IN X W=1IN X D=0.037 P3-L=3ININ X W=1.5 X D=0.037 REPSDR A6WA202304018625Seat Track · corrodedSEAT TRACK PN 20276-288-0-0 AT FS349.00Ï¿½ FS599.00+112 LHS HAS CORROSION AT NUMEROUS LOCATIONS. ***** AC REMOVED FROM SERVICE ***** BLENDED CORROSION ON SEAT TRACK PN 20276-288-0-0 AT FS349.00 Ï¿½ FS599.00+112 LH PN 20276-144-0-0. DIMENSIONS P1 L= 63IN X WSDR A6WA202304018623Bushing · unknownHORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. ******AIRCRAFT REMOVED FROM SERVICE****** HORIZONTAL AND VERTICAL STAB PIVOT BUSHINGS ARE WORN BEYOND LIMITS. P1A- L=2.00IN X W 0.1968IN X D=0.001IN P1B- L=2.00IN X W 0.3543IN X D=0.002IN. SDR A6WA202304018624Floor Support · corrodedCORROSION ON FLOOR SILL P/N 601R31145 AT FS449.85 TO FS461.50 AND LBL41-LBL42 ******AIRCRAFT REMOVED FROM SERVICE******* CORROSION ON FLOOR SILL P/N 601R31145 AT FS449.85 TO FS461.50 AND LBL41-LBL42 P11-L=1.300IN X W=1.200IN X D=0.002 P12-L=1.00IN X W=0.700INSDR A6WA202304018621Floor Support · corrodedCORROSION ON CABIN FLOOR SILL RH AT FS484.00+2 TO FS484.00 +5 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON FLOOR SILL RH AT FS484.00+2 TO FS484.00+9 AND RBL 42. P10-L=1.200IN X W=0.800IN X D=0.003 P11-L=2.00IN X W=1.00IN X D=SDR A6WA202304018619Floor Support · corrodedCORROSION ON CABIN FLOOR SILL LH AT FS461.50+6 TO FS473.15+5 AND LBL36. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT FS513.00 TO FS529.00 AND LBL 36-38. P14-L=1.100IN X W=0.600IN X D=0.002 P15-L=1.200IN X W=0.700IN X D=0SDR A6WA202304018618Floor Support · corrodedCORROSION ON CABIN FLOOR SILL LH AT FS513.00 TO FS529.00 AND LBL36-38. AIRCRAFT REMOVED FROM SERVICE. BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT FS513.00 TO FS529.00 AND LBL 36-38. P24-L=0.600IN X W=0.400IN X D=0.002 P25-L=1.700IN X W=0.700IN X D=0.0SDR A6WA202304018620Flange · unknownTWO FLANGES UNDERFLOOR PANEL 271ALF AT FS559.00+16 BLO 0 ARE NOT INSTALLED. AIRCRAFT REMOVED FROM SERVICE. DURING EVALUATION FOUND 13 OVERSIZED HOLE EFFECTING RBL 9 BL 0 AND LBL 9 ON FLOOR BEAM FLANGES AND INSTALLED NEW FLANGES PN 6010R31025-23 AND PN 601SDR A6WA202304018617Floor Support · corrodedCORROSION ON CABIN FLOOR SILL LH AT FS424.00 TO FS424.00+4 AND LBL35-38. *****AIRCRAFT REMOVED FROM SERVICE********* BLENDED 4 AREAS OF CORROSION ON LH FLOOR SILL AT F424.00 TO FS424.00+4 AND LBL 35-38. P2-L=1.800IN X W=1.400IN X D=0.002 P3-L=0.700IN X W=0.50SDR A6WA202304018616Floor Support · corrodedCORROSION ON CABIN FLOOR SILL LH AT FS473.15 AND LBL36. *******AIRCRAFT REMOVED FROM SERVICE******* REMOVED CORROSION ON LH FLOOR SILL AT F473.15AND LBL 36. P16-L=3.500IN X W=1.700IN X D=.002 ORIGINAL THICKNESS 00.80 REMAINING THICKNESS .078 MATERIAL LOSS .SDR A6WA202304018613Bracket · corrodedCORROSION ON PASSENGER DOOR LOWER SILL BRACKETS P/N 601R31527-217 STG17L. ***** AC REMOVED FROM SERVICE ***** EVALUATED BLENDED AREA AT PASSENGER DOOR LOWER SILL BRACKETS P/N 601R31527-217 AT FS310.00+4 TO FS333+9 STG17L FOUND TO BE OUT OF LIMITS. REPLACED TWSDR A6WA202304018610Strap · corrodedCORROSION ON RH FLOOR SILL STRAP PN# 601R3113-102 AT FS559. +112 TO FS621.00 RBL 42. ***** AC REMOVED FROM SERVICE ***** REPLACED FLOOR SILL WITH A NEW SILL P/N601R31133-102 AT FS559.00+80 TO FS559.00_112.RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WASDR A6WA202304018611Floor Support · corrodedCORROSION ON FLOOR SILL PN601R31132-58 AT FS409.00+80 TO FS 409.00+112 AND RBL42. ***** AC REMOVED FROM SERVICE ***** P1 - L= 3.40IN X W= 0.600IN X D= 0.003IN FS409.00+96 P2 - L= 0.700IN X W= 0.700INX D= 0.002IN FS409.00+98 P3 - L= 1.900IN X W= 1.200IN X D= 0SDR A6WA202303058480Module · noneCLIMBING THROUGH FL210, RECEIVED CABIN ALT CAUTION MESSAGE. BEGAN QRH, RECEIVED CABIN ALT WARNING MESSAGE. CW IAC/QRH, DIVERTED TO FWA. CABIN ALT INDICATION WAS RISING WHEN CATION MESSAGE WAS DISPLAYED. *****AIRCRAFT REMOVED FROM SERVICE******* DUE TO EXTENSSDR A6WA202302188607Seat Track · corrodedFLOOR SEAT RAIL HAS 4 EA AREAS OF CORROSION BETWEEN FS 574 TO FS 615 AND RBL 27. *************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED 4 EA AREAS OF CORROSION IAW CRJ200 SRM 51-21-06 REV 39. EVALUATED BLEND AREAS AND FOUND AREAS P1 TO P3 SDR A6WA202302048455Switch · not reportedSTAB TRIM / MACH TRIM MESSAGE APPROX 7000 - 8000 FEET. APPROX 200 KNOTS. THEY WOULD NOT RE-ENGAGE. MULTIPLE ATTEMPTS. AUTO-PILOT NOT ENGAGED. ******AIRCRAFT REMOVED FROM SERVICE********* R/R FO PITCH TRIM DISCONNECT SWITCH IAW AMM SUP 10-048D. OPS CHECK SDR A6WA202203028119None · noneAILERON TRIM SLIGHTLY OUT OF ZERO R WING DOWN. WILL NOT RESPOND TO L WING DOWN TRIM SWITCH MOVEMENTS. POSITIONED TO ZERO P2-F7 COLLARD C/B P2-F7. PLACARDED AND PLACED ON MEL. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED AILERON/RUDDER TRIM PANELSDR A6WA202111087955Handle · faultedDURING APPROACH, THE CREW RECEIVED A FLAP FAILURE MESSAGE. CREW ELECTED TO GO AROUND, COORDINATE WITH DISPATCH & DECLARED AN EMERGENCY. CREW COMMUNICATED WITH F/A AND PAX, RETURNED & LANDED WITHOUT FURTHER INCIDENT. FLAPS FAILED AT 20 DEG ON APPROACH SDR A6WA2021081087818Sensor · faultedRECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. RIGHT FUSELAGE DUCT INDICATED. C/W QRH, MESSAGE PERSISTS. ***AIRCRAFT REMOVED FROM SERVICE*** R&R AFT EQUIPMENT BAY FUSELAGE AIR BLEED LEAK SENSING ELEMENT A46WK IAW AMM 36-21-04 OPS CHECK GOOD.SDR A6WA2020022847207Solenoid Valve · failedPILOT REPORTS APU FAILED TO START ON DESCENT FAILED TO LIGHT. AFTER 2ND ATTEMPT THERE WAS A STRONG FUEL SMELL IN AIRCRAFT. FUEL SMELL WENT AWAY AFTER THEY SHUT IT DOWN. FOUND COALESCER TO BE CONTAMINATED DUE TO APU START FAILURE. C/W AWAC SUP 09-037C. APU OPSDR A6WA2019122047073Hinge · gougedL1 DOOR HINGE LUGS FROM FWD #2, #9, #19, #30, #32, #36, #39, #46, #50, #52, HAVE GOUGES. AIRCRAFT REMOVED FROM SERVICE BLENDED LUGS #2,#9,#19,#30,#32,#36,#39,#46,#50,#52,IAW SRM 51-12-00, REV.37, AFTER BLENDING REMAINING MATERIAL THICKNESS IS AS FOLLOWS,SDR A6WA2019121847067Vane · gougedL/H I/B FLAP VANE L/E BETWEEN FLAP STA 69.631-FLAP STA 79.257 HAS GOUGE DAMAGE. AIRCRAFT REMOVED FROM SERVICE CUT OUT DAMAGED SKIN ON L/H I/B FLAP VANE AT FLAP STA 77.5 . CUTOUT DIMENSIONS ARE 1.3"W X .7"L . FABRICATED FLAP VANE INSERT AND VANE BUTT STRASDR A6WA2019122047069Fitting · crackedSERVICE DOOR FITTING BELOW HANDLE HAS A CRACK. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SERVICE DOOR FITTING P/N 601R38723-17 REF CRJ 200 AMM 52-41-03 REV 60 AND CRJ 200 SRM 51-42-20 REV 37.SDR A6WA2019080946784Bulkhead Web · crackedCRACK WAS DISCOVERED IN THE AFT PRESSURE BULKHEAD FS621, LB 27.50, 103.50 WL DURING SCHEDULED SDI OF THE AFT PRESSURE BULKHEAD. CRACK WAS REPAIRED PER REO 601R-53-61-1285.SDR A6WA2018071845935Bypass Valve · faultyGEAR DISAGREE WARNING ON APPROACH. RIGHT GEAR UNSAFE. C/W QRH MSG REMAINS. CYCLED GEAR, RT MLG CAME DOWN AND LOCKED. REMOVED AND REPLACED MAIN LANDING GEAR RUN AROUND BYPASS VALVE IAW AMM 32-32-20. COMPLIED WITH FUNCTIONAL TEST OF MAIN LANDING GEAR EXTENSION SDR A6WA2018071345929Battery Pack · dischargedCABIN EMERGENCY LIGHTS 2 AND 4 IN CEILING NOT LIGHTING. REPLACED NR 4 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-04, OPS CHECK OKAY.SDR A6WA2018032945735Tiller · malfunctionedABORTED TAKEOFF BECAUSE A/C WOULD NOT STEER, FULL HARD LEFT. ON TAXI IN TILLER WOULD NOT SELF CENTER, LOW SPEED ABORT BTMS OK REMOVED AND REPLACED THE TILLER IAW AMM 32-51-01. OPS CHECKED GOOD.SDR A6WA2017121945487Floor Support · corrodedLEFT FLOOR SILL CORRODED FROM FS 559+80 TO 621.00, LBL42. REPAIRED SILL IAW REO 601R-53-00-526.SDR A6WA201745452Angle · cracked1015032-1000-0010 - ANGLE AT L/H LONGERON 24 ABOVE CENTER WING FWD OF FS 473.15 IS CRACKED. REMOVED AND REPLACED ANGLE AT L/H LONGERON 24 ABOVE CENTER WING IAW CRJ200 SRM 51-42-06, 51-42-21.SDR A6WA2017120445452Angle · crackedANGLE AT LT LONGERON 24 ABOVE CENTER WING FWD OF FS 473.15 IS CRACKED. REMOVED AND REPLACED ANGLE AT LT LONGERON 24 ABOVE CENTER WING IAW SRM 51-42-06, 51-42-21.SDR A6WA2017120445454Bracket · crackedSYSTEM 1 AC PUMP CASE DRAIN FILTER BRACKET IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.SDR A6WA2017120445453Angle · crackedANGLE AT RT LONGERON 24 ABOVE CENTER WING FWD OF FS473.15 IS CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06, 51-42-21.SDR A6WA2017120445455Support Bracket · crackedSYSTEM 2 HYD CASE DRAIN FILTER FRAME SUPPORT BRACKET HAS A 1" CRACK. REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.SDR A6WA2017102545372Window · arcedRIGHT WINDSHIELD HEAT ARCING, WINDOW CRACKED, INCIDENT OCCURED CLIMBING THRU 20,000 FT. OBSERVED ARCING, NO ODOR. SELECTED OFF. LANDED. R & R THE WINDSHIELD IAW AMM 56-11-01, OPS & LEAK CHECK GOOD.SDR A6WA201644146Ballast · defectiveF/A REPORTS STRONG ELECTRICAL BURNING ODOR IN VICINITY OF ROW 7 AND ROW 8, NO PASSENGERS ON BOARD AT TIME OF DISCOVERY. DID NOT NOTICE ANY
VISIBLE OR AUDIBLE ARCING/SPARKING. INSPECTED AND VERIFIED BALLAST B113 CAUSED FLUORESCENT CEILING LIGHTS AT ROW 5AC TSDR A6WA201644018Unknown · malfunctionedAFTER TAKEOFF AT 7000 FT, NOTICED ACFT WAS NOT PRESSURIZING ON PRESSURE CONTROLLER NR 1. SWITCHED TO PRESSURE CONTROLLER 2, CABIN ALTITUDE CLIMBING AT SAME RATE AS ACFT. SWITCHED TO MANUAL, NO AFFECT. AIR RETURN, LANDED AT 44,000 LBS GROSS.
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