# Service difficulty reports: N471ZW

A list on [N471ZW](https://openairdocs.org/aircraft/N471ZW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 179 reports

- [SDR A6WA202602138898](https://openairdocs.org/sdr/A6WA202602138898.md): Floor Support · corroded · Feb 13, 2026 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON THE FWD LOWER END OF THE SERVICE DOOR THRESHOLD/FLOOR SUPPORT BRACKET. UPON CLEANING OF THE CORROSION, FASTENER HOLES WERE ELONGATED AND REMOVED MATERIAL WAS BEYOND SRM LIMITS. BLENDED DISCREPANT AREAS OF CORROSION AND DID HFEC OF THE B
- [SDR A6WA202601198895](https://openairdocs.org/sdr/A6WA202601198895.md): Floor Support · corroded · Jan 19, 2026 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BEAM AT BL 27L, BETWEEN FS 574 AND FS 621. REPAIR INCLUDED BLENDING OF MINOR CORROSION, CUT AWAY OF CORROSION THAT WAS BEYOND LIMITS, HFEC OF REQUIRED AREAS, REPLACEMENT OF CUT OUT AREAS, AND REINFOR
- [SDR A6WA202601058896](https://openairdocs.org/sdr/A6WA202601058896.md): Support · corroded · Jan 5, 2026 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ALONG AFT PRESSURE BULKHEAD FS 621 HAS CORROSION ON UPPER AND LOWER SURFACE AROUND NUTPLATES BETWEEN BL 9L AND 27L. BLENDED CORROSION, INSPECTED, REBUILT WITH EPOXY, INSTALLED DOUBLER, RESTORED SURFACE TREATMENT, APPLIED CIC.
- [SDR A6WA202511028869](https://openairdocs.org/sdr/A6WA202511028869.md): Windshield · cracked · Nov 2, 2025 · N471ZW · Cndair CL6002B19 · Flight Compartment Windows
  > REQUEST INSPECTION FOR F/O'S WINDSHIELD CRACKS. INSPECTED AND FOUND F/O WINDSHIELD TO BE OUT OF LIMITS IAW AWAC SUPP 14-201D REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202504028867](https://openairdocs.org/sdr/A6WA202504028867.md): Adc · faulted · Apr 27, 2025 · N471ZW · Cndair CL6002B19 · Air Data Computer
  > AT 28000 FT DURING DECENT F/O AIRSPEED DECREASING AND EFIS COMP MON IAS CAUTION PRESENT AT 16000 FT F/O AIRSPEED RETURNED TO NORMAL. REMOVED AND REPLACED #2 ADC. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME
- [SDR A6WA202502118859](https://openairdocs.org/sdr/A6WA202502118859.md): Idg · faulted · Feb 11, 2025 · N471ZW · Cndair CL6002B19 · AC Generator-Alternator
  > ON CLIMB OUT REC'V GEN 1 OFF CAUTION MESSAGE. C/W QRH MESSAGE DISAPPEARED. REMAINED EXTINGUISHED REST OF FLIGHT. ***** AIRCRAFT REMOVED FROM SERVICE ***** R/R #1 IDG ASSEMBLY IAW AMM 24-11-01 REF 370816-4 FOR REQ LEAK AND OPS CHECK. SERVICED IDG IAW AMM SUP
- [SDR A6WA202402128713](https://openairdocs.org/sdr/A6WA202402128713.md): Smoke Detector · false activation · Feb 12, 2024 · N471ZW · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAU MSG IN FLT NO FIRE OR SMOKE PRESET IN LAV CAU PERSISTED C/W QRH MSG PERSITED UNTIL LANDING. NO ONE IN LAV WHEN MSG APPEARED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R LAV SMOKE DETECTOR PER AMM 26-16-01 OPS CHECK GOOD AT THIS TIM
- [SDR A6WA202312288684](https://openairdocs.org/sdr/A6WA202312288684.md): Unknown · unknown · Dec 28, 2023 · N471ZW · Cndair CL6002B19 · Electrical Power System
  > DURING TAKE-OFF ROLL, RECEIVED IDG 2 DISC CAUTION FOLLOWED BY YD 2 INOP STATUS MESSAGE AND CONFIG SPLRS WARNING MESSAGE FOLLOWED BY GEN 2 OFF CAUTION MESSAGE. ABORTED TAKE-OFF AT 56 KNOTS. ALL BRAKE TEMPS BELOW 5, BTMS REMAINED GREEN. *******AIRCRAFT REMOVED
- [SDR A6WA20231218681](https://openairdocs.org/sdr/A6WA20231218681.md): Unknown · unknown · Dec 14, 2023 · N471ZW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > AFTER GEAR RETRACTION RECIEVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSGS. C/W QRH MSGS CLEARED. ****AIRCRAFT REMOVED FROM SERVICE*********** INSP AND FOUND NLG PROX SW DMG'ED. PULLED CODE S23 NGOEXT. OPS CHECKED NLG DOOR IAW AMM 32-22-01. OPS CK GOOD. C
- [SDR A6WA202311218677](https://openairdocs.org/sdr/A6WA202311218677.md): Bracket · corroded · Nov 21, 2023 · N471ZW · Cndair CL6002B19 · Wing, Attach Fittings
  > 471 20123 457-900-342 10HOURS ***** AIRCRAFT REMOVED FROM SERVICE ***** RH WING LEADING EDGE AT ANTI ICE STUB DUCT INBOARD BRACKET FOUND WITH CORROSION. REMOVED AND REPLACED 1EA BRACKET P/N 601R120371-245 AT RH FORWARD SPAR AT WS139.54 TO WS149.58. IAW CRJ
- [SDR A6WA202311188674](https://openairdocs.org/sdr/A6WA202311188674.md): Angle · corroded · Nov 18, 2023 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 471 20081 330500 MFG 453-900-500 41.3 HRS RH FLOOR DOOR SILL STRUCTURE HAS 4 SPOTS OF EXFOLIATION FS295-FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION ON ANGLE P/N 601R38303-239 TO SERVICE DOOR SILL BETWEEN FS319.7 TO FS349 AND EVALUATED ORIG
- [SDR A6WA202311178676](https://openairdocs.org/sdr/A6WA202311178676.md): Bracket · corroded · Nov 17, 2023 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > 471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PAS
- [SDR A6WA202311178675](https://openairdocs.org/sdr/A6WA202311178675.md): Cleat · corroded · Nov 17, 2023 · N471ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > 471 20103 330500 MFG 427-680-100 3 HRS LH UPPER FLOOR SKIN AND SILL HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS339-FS259. ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED 1EA CLEAT P/N 601R31527-176, 1EA BRACKET ASSY P/N 601R31527-217 ON PAS
- [SDR A6WA202310108669](https://openairdocs.org/sdr/A6WA202310108669.md): Skin · dented · Oct 10, 2023 · N471ZW · Cndair CL6002B19 · Trailing Edge Flaps
  > DENT ON THE R/H INBD UPPER SURFACE INBD END. DENT ON R/H INBD FLAP UPPER SKIN WS 50.489+13. L=5.200Ï¿½ X W=0.400Ï¿½ X D=0.008Ï¿½ FOUND TO BE OUT OF LIMITS IAW SRM 57-52-00 REV 39. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC WITH NO INDICATIONS. VERIFIED N
- [SDR A6WA202212098402](https://openairdocs.org/sdr/A6WA202212098402.md): Trim System · faulted · Dec 9, 2022 · N471ZW · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB AND MACH TRIM DROPPED OFFLINE. AIRCRAFT REMOVED FROM SERVICE. OPS CHECKED GOOD, COULD NOT DUPLICATE. R & R HSTCU IAW AMM 27-41-01, PREVENTIVE. OPS CHECKED GOOD.
- [SDR A6WA202108247862](https://openairdocs.org/sdr/A6WA202108247862.md): Flap System · faulted · Aug 23, 2021 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***AIRCRAFT REMOVED FROM SERVICE*** FLAP FAILURE CAUTION. FLAPS FAILED AT 8 DEGREES. PERFORMED FLAP RESET PR
- [SDR A6WA202101267522](https://openairdocs.org/sdr/A6WA202101267522.md): Actuator · failed · Jan 10, 2021 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRCR
- [SDR A6WA202101137522](https://openairdocs.org/sdr/A6WA202101137522.md): Flap System · malfunctioned · Jan 10, 2021 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER THE CREW SELECTED FLAPS OUT OF ZERO THEY RECEIVED FLAP FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH THEIR QRH AND PERFORMED A FLAP ZERO LANDING. THE CREW STATED THEY HAD A SMOOTH LANDING. MESSAGE WAS RESET AND A/C WAS FERRIED TO MKE FOR REPAIR. AIRC
- [SDR A6WA202101137517](https://openairdocs.org/sdr/A6WA202101137517.md): Bpsu · malfunctioned · Jan 6, 2021 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION ON APPROACH, FLAPS FAILED AT 20 DEGREES. CREW PREFORMED GO-AROUND AND COMPLIED WITH THE QRH. ONCE ON THE GROUND AND AT THE GATE FLAP RESET PROCEDURE WAS FOLLOWED, IAW AWAC SUPPLEMENT 98- 18I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SER
- [SDR A6WA202012297500](https://openairdocs.org/sdr/A6WA202012297500.md): Power Supply · no test · Dec 24, 2020 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 ON APROACH CW QRH LANDED UNEVENTFULLY. FLAP FAIL OCCURED WHEN SELECING FROM 20 TO 30 DEG. PERFOREMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. T/S RT BPSU
- [SDR A6WA2020030247210](https://openairdocs.org/sdr/A6WA2020030247210.md): Apu · making metal · Feb 28, 2020 · N471ZW · Cndair CL6002B19 · APU Core Engine
  > ***SUPPLEMENTAL**** ODOR OF FUEL IN COCKPIT AFTER APU START IN FLT. ODOR DISSIPATED AS SOON AS BLEED WHERE TURN OFF. AIRCRAFT REMOVED FROM SERVICE THE APU WAS PLACED ON MEL,48-10-01-01 AND MX C/W SUP 09-037C FOR UNUSUAL ODORS OF CONTAMINATION FROM THE APU OR
- [SDR A6WA2020022847208](https://openairdocs.org/sdr/A6WA2020022847208.md): Igniter · failed · Feb 27, 2020 · N471ZW · Cndair CL6002B19 · APU Start/Ignition System
  > STRONG FUEL SMELL IN COCKPIT& CABIN AFTER STARTING APU. R&R EXCITER PER AMM 49-41-01-000-801, OPS CHECK GOOD. R&R BOTH APU IGNITORS PER AMM 49-41-05-000-801, OPS CHECK GOOD. SN OFF:1366J SN ON:J11060014
- [SDR A6WA2020022847203](https://openairdocs.org/sdr/A6WA2020022847203.md): Fuel Line · loose · Feb 26, 2020 · N471ZW · Cndair CL6002B19 · APU Engine Fuel and Control
  > FUEL SMELL IN COCKPIT AND CABIN IN FLIGHT IMMEDIATELY AFTER APU START FOUND BOTH FUEL FEED AND FUEL RETURN LINES @ APU FUEL CONTROL LOOSE TIGHTENED AS REQUIRED.OPS CHECK GOOD IAW, A
- [SDR A6WA202002147180](https://openairdocs.org/sdr/A6WA202002147180.md): Wire Harness · damaged · Feb 13, 2020 · N471ZW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKEOFF, RECEIVED GEAR DISAGREE WARNING, NLG BOX WAS RED & NOSE DOOR WARNING MESSAGE. OCCURED IN ICING. MESSAGE CLEARED ON ITS OWN. THEN DURING APPROACH, RECEIVED GEAR DISAGREE AGAIN WITH RED NLG BOX & NOSE DOOR WARNING. CYCLED GEAR AND PUT HYD 2B &
- [SDR A6WA2019121847065](https://openairdocs.org/sdr/A6WA2019121847065.md): Warning Message · false activation · Dec 16, 2019 · N471ZW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > LEFT WING A/ICE (C) MSG CAME ON IN FLT. C/W QRH. MSG PERSISTS. WERE IN ICING CONDITIONS. CLIMBED TO HIGHER ALTITUDE TO LEAE ICING CONDITIONS. LEFT FUSELAGE AND WING SHOWED IN AMBER. AFTER CLIMBING ABOVE ICING CONDITIONS RCVD L WINGA/ICE, R WING A/ICE + ICE (C)
- [SDR A6WA2019121847061](https://openairdocs.org/sdr/A6WA2019121847061.md): Warning Message · false activation · Dec 15, 2019 · N471ZW · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT TR UNLOCK CAUTION MESSAGE DISPLAYED DURING FLIGHT C/W QRH EMER STOW MESSAGE REMAINED. CREW LANDED NEAREST SUITABLE AIRPORT (IND) PER QRH. AIRCRAFT REMOVED FROM SERVICE LUBRICATED RT TR IAW AMM 12-20 OPS CHECK GOOD AT THIS TIME REMOVED PLACARD REMOVED F
- [SDR A6WA2019121247054](https://openairdocs.org/sdr/A6WA2019121247054.md): Control Cable · failed · Dec 11, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH. EICAS INDICATES FLAPS @ 30 DEGREES. COMPLIED WITH QRH, EMERGENCY DECLARED. FLAPS SUCCESSFULLY RESET IAW AWAC SUPP. 98-018G AIRCRAFT REMOVED FROM SERVICE COULD NOT DUPLICATE FLAP FAIL CAUTION MSG. I
- [SDR A6WA2019112747031](https://openairdocs.org/sdr/A6WA2019112747031.md): Floor Support · corroded · Nov 21, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL FS 409+96 TO 409+112 HAS CORROSION. REPAIRED AIRCRAFT REMOVED FROM SERVICE REPAIRED RH FLOOR SILL FS 409+96 TO 409+112 IAW ASAP EA# AWAC-CRJ253-01375
- [SDR A6WA2019112647030](https://openairdocs.org/sdr/A6WA2019112647030.md): Floor Support · corroded · Nov 21, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL FS 559+80 TO FS574 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SILL FS 559+80 TO FS574 IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019112047025](https://openairdocs.org/sdr/A6WA2019112047025.md): Retainer · corroded · Nov 18, 2019 · N471ZW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR SEAL RETAINER AT BOTTOM CENTER OF DOOR HAS CORROSION AROUND FASTENERS AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED SEAL RETAINER ON SERVICE DOOR IAW AWAC SUPPLEMENT 19-310
- [SDR A6WA2019112047016](https://openairdocs.org/sdr/A6WA2019112047016.md): Skin · cracked · Nov 15, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NOSE LANDING GEAR SPADE DOOR CUT OUT RH AND LH AFT CORNERS CRACKED AIRCRAFT REMOVED FROM SERVICE REPAIRED NOSE LANDING GEAR SPADE DOOR CUTOUT SKIN RH AND LH CORNERS IAW BOMBARDIER REO 601R-53-11-010
- [SDR A6WA2019112047019](https://openairdocs.org/sdr/A6WA2019112047019.md): Vane · chafed · Nov 14, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE HAS 3 CHAFES ON LEADING EDGE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FLAP VANE LEADING EDGE SKIN IAW CRJ200 SRM 51-42-13
- [SDR A6WA2019111547008](https://openairdocs.org/sdr/A6WA2019111547008.md): Striker · gouged · Nov 14, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR SEAL STRIKER IS GOUGED AT PREVIOUS REPAIR NEAR TOP, AFT, LATCH PIN FITTING AIRCRAFT REMOVED FROM SERVICE REPLACED DAMAGED STRIKER REPAIR IAW B/A REO 601R-53-22-033
- [SDR A6WA201911147000](https://openairdocs.org/sdr/A6WA201911147000.md): Seat Track · corroded · Nov 12, 2019 · N471ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE REPLACED LH FLOOR SEAT RAIL FROM FS 409+128 TO FS 559 IAW AWAC SUPP 19-254A
- [SDR A6WA201911147006](https://openairdocs.org/sdr/A6WA201911147006.md): Seat Track · corroded · Nov 11, 2019 · N471ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 HAS CORROSION. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED RH FLOOR SEAT RAIL FROM FS 409+128 TO 559 IAW CRJ 200 AMM 53-01-11
- [SDR A6WA2019112047018](https://openairdocs.org/sdr/A6WA2019112047018.md): Skin · chafed · Nov 9, 2019 · N471ZW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON LEADING EDGE HAS CHAFFING MARKS ALONG UPPER SIDE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H L/E OF AILERON IAW CRJ200 SRM 51-42-06 AND AWAC SUP. 14-270
- [SDR A6WA2019111146994](https://openairdocs.org/sdr/A6WA2019111146994.md): Angle · cracked · Nov 9, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 409+128 VERTICAL POST AT BL0 ANGLE CRACKED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED FS 409+128 VERTICAL POST AT BL0 ANGLE IAW REO 601R-53-41-889 REV D
- [SDR A6WA2019111146992](https://openairdocs.org/sdr/A6WA2019111146992.md): Doubler · corroded · Nov 9, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON REMOVAL OF FLOOR SILL FS559+80 TO FS 574 FOUND LOWER DOUBLER CORRODED. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED LOWER DOUBLER IAW CRJ 200 SRM 53-51-43
- [SDR A6WA2019111847001](https://openairdocs.org/sdr/A6WA2019111847001.md): Seat Track · corroded · Nov 7, 2019 · N471ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SUPPLEMENTAL INFORMATION, NR 1 FLOOR SEAT TRACK ON RBL 9 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED NR 1 FLOOR SEAT TRACK ON RBL 9 IAW AMM 53-01-11.
- [SDR A6WA2019111146990](https://openairdocs.org/sdr/A6WA2019111146990.md): Floor Support · corroded · Nov 7, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE REPAIRED IAW CRJ 200 SRM 51-42-06, REO 601R-53-41-666 REV-C.
- [SDR A6WA2019111146993](https://openairdocs.org/sdr/A6WA2019111146993.md): Beam · damaged · Nov 7, 2019 · N471ZW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM 601R35050-64 CUT BY CABLE ASSIST. REPLACED AIRCRAFT REMOVED FROM SERVICE REPLACED CARGO DOOR BEAM 601R35050-64 IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2019111146988](https://openairdocs.org/sdr/A6WA2019111146988.md): Tab · cracked · Nov 7, 2019 · N471ZW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING HINGE BOX @ WS80-50 HAS BROKEN BONDING WIRE TAB. AIRCRAFT REMOVED FROM SERVICE REPLACED TAB IAW CRJ 200 SRM 51-42-21.
- [SDR A6WA2019111146989](https://openairdocs.org/sdr/A6WA2019111146989.md): Attach Angle · cracked · Nov 6, 2019 · N471ZW · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR BEAM ATTACH ANGLE IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21, 53-61-23, TR51-42.
- [SDR A6WA2019111146987](https://openairdocs.org/sdr/A6WA2019111146987.md): Bracket · cracked · Nov 6, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD COUNTER BALANCE SPRING BOX MOUNT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNT BRACKET IAW CRJ-200 SRM 51-52-06
- [SDR A6WA2019111146986](https://openairdocs.org/sdr/A6WA2019111146986.md): Angle · cracked · Nov 5, 2019 · N471ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 RBL 9 INBOARD CLIP IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-06 AND 51-42-42
- [SDR A6WA2019110546971](https://openairdocs.org/sdr/A6WA2019110546971.md): Bracket · cracked · Nov 1, 2019 · N471ZW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD CARGO DOOR TRACK LOWER ATTACH POINT IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED FWD CARGO TRACK LWR ATTACH POINT BRACKET IAW CRJ 200 SRM 51-42-21 AND 51-41-00
- [SDR A6WA2019031546473](https://openairdocs.org/sdr/A6WA2019031546473.md): Flap · failed · Mar 14, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES. THE CREW COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY AND LANDED IN IAD WITHOUT FURTHER INCIDENT. FLAP RESET ATTEMPT WAS NOT SUCCESSFUL.
- [SDR A6WA2019030446452](https://openairdocs.org/sdr/A6WA2019030446452.md): Flap · failed · Mar 3, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 0 DEGREES AT CRUISE FLIGHT.
- [SDR A6WA2019022546411](https://openairdocs.org/sdr/A6WA2019022546411.md): Warning Message · illuminated · Feb 21, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO DESTINATION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT.
- [SDR A6WA2019020546361](https://openairdocs.org/sdr/A6WA2019020546361.md): Flap System · failed · Jan 29, 2019 · N471ZW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 DEGREES ON APROACH PERFORMED FLAPS RESET PROSEDURE IAW AWAC SUP 98-018G FLAPS RESET PLACARDED AND PLACED ON MEL

Next page: https://openairdocs.org/aircraft/N471ZW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N471ZW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N471ZW/reports

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