# Service difficulty reports: N427ZW

A list on [N427ZW](https://openairdocs.org/aircraft/N427ZW.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 5 · 203 reports

- [SDR A6WA202302128463](https://openairdocs.org/sdr/A6WA202302128463.md): Unknown · unknown · Feb 12, 2023 · N427ZW · Cndair CL6002B19 · Flight Management Computing Hardware System
  > SHORTLY 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, S
- [SDR A6WA202205168188](https://openairdocs.org/sdr/A6WA202205168188.md): Structure · damaged · May 16, 2022 · N427ZW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > MULTIPLE 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.2
- [SDR A6WA202203138129](https://openairdocs.org/sdr/A6WA202203138129.md): Cowling · damaged · Mar 13, 2022 · N427ZW · Cndair CL6002B19 · Engine Cowling System
  > REF 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 A6WA202111307998](https://openairdocs.org/sdr/A6WA202111307998.md): Switch · failed · Nov 29, 2021 · N427ZW · Cndair CL6002B19 · Door Warning System
  > AFTER 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 SERVIC
- [SDR A6WA202111157970](https://openairdocs.org/sdr/A6WA202111157970.md): None · corroded · Sep 21, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > R/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"W
- [SDR A6WA202111087953](https://openairdocs.org/sdr/A6WA202111087953.md): Seat Track · corroded · Sep 3, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > CORROSION 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 LH
- [SDR A6WA202109167879](https://openairdocs.org/sdr/A6WA202109167879.md): Strap · corroded · Aug 30, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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 A6WA202109087874](https://openairdocs.org/sdr/A6WA202109087874.md): Skin · damaged · Aug 26, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SCRIBE 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 + 128
- [SDR A6WA202110017892](https://openairdocs.org/sdr/A6WA202110017892.md): Skin · dented · Aug 25, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT 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 A6WA202109087868](https://openairdocs.org/sdr/A6WA202109087868.md): Floor Support · corroded · Aug 25, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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¿½
- [SDR A6WA202109087867](https://openairdocs.org/sdr/A6WA202109087867.md): Floor Support · corroded · Aug 25, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION 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. CORROSIO
- [SDR A6WA202109087869](https://openairdocs.org/sdr/A6WA202109087869.md): Pressure Deck · corroded · Aug 25, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Structure
  > CORROSION 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 A6WA202108247939](https://openairdocs.org/sdr/A6WA202108247939.md): None · dented · Aug 24, 2021 · N427ZW · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > RIGHT 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 = 1
- [SDR A6WA202109287891](https://openairdocs.org/sdr/A6WA202109287891.md): None · corroded · Aug 19, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION 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= 2.60
- [SDR A6WA202108187936](https://openairdocs.org/sdr/A6WA202108187936.md): Plate · corroded · Aug 18, 2021 · N427ZW · Cndair CL6002B19 · Doors
  > SERVICE 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 UNDER
- [SDR A6WA202110217919](https://openairdocs.org/sdr/A6WA202110217919.md): Seat Track · corroded · Aug 17, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION 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 A6WA202110217917](https://openairdocs.org/sdr/A6WA202110217917.md): Seat Track · corroded · Aug 17, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION 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, FS43
- [SDR A6WA202110217918](https://openairdocs.org/sdr/A6WA202110217918.md): Seat Track · corroded · Aug 17, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > CORROSION 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 A6WA202109087870](https://openairdocs.org/sdr/A6WA202109087870.md): Skin · gouged · Aug 16, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SCRIBE 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 + 128
- [SDR A6WA202108157938](https://openairdocs.org/sdr/A6WA202108157938.md): Cowl Door · gouged · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Engine Air Baffle Section
  > RH 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 = 0
- [SDR A6WA202109087871](https://openairdocs.org/sdr/A6WA202109087871.md): Skin · damaged · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > NUMBER 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 228-50162-4
- [SDR A6WA202109087872](https://openairdocs.org/sdr/A6WA202109087872.md): Skin · dented · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT 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 = 0.8
- [SDR A6WA202109087873](https://openairdocs.org/sdr/A6WA202109087873.md): Skin · dented · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT 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 = 0.450Ï
- [SDR A6WA202108307864](https://openairdocs.org/sdr/A6WA202108307864.md): Skin · dented · Aug 15, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT 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. F
- [SDR A6WA202110017893](https://openairdocs.org/sdr/A6WA202110017893.md): Skin · dented · Aug 14, 2021 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > DENT 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 A6WA202109177881](https://openairdocs.org/sdr/A6WA202109177881.md): Panel · damaged · Aug 14, 2021 · N427ZW · Cndair CL6002B19 · Wing, Plate/Skin
  > BLENDED 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 FINIS
- [SDR A6WA202111087954](https://openairdocs.org/sdr/A6WA202111087954.md): None · cracked · Aug 13, 2021 · N427ZW · Cndair CL6002B19 · Doors
  > CRACK 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 MID
- [SDR A6WA201904296590](https://openairdocs.org/sdr/A6WA201904296590.md): Structure · punctured · Apr 25, 2019 · N427ZW · Cndair CL6002B19 · Fuselage Structure (General)
  > PUNCTURE 1.25" LONG AT FS 625.30 STR 18R
- [SDR A6WA2018020645612](https://openairdocs.org/sdr/A6WA2018020645612.md): Smoke Detector · faulty · Feb 4, 2018 · N427ZW · Cndair CL6002B19 · Smoke Detection
  > SMOKE 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 A6WA201845542](https://openairdocs.org/sdr/A6WA201845542.md): Frame · corroded · Jan 4, 2018 · N427ZW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 605 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26L IN THE CARGO BAY.
- [SDR A6WA2017010245533](https://openairdocs.org/sdr/A6WA2017010245533.md): Skin · dented · Dec 27, 2017 · N427ZW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN DENTED ON T/E CORNER. REPAIRED THE FLAP SKIN IAW SRM 57-52-00.
- [SDR A6WA2017010245516](https://openairdocs.org/sdr/A6WA2017010245516.md): Angle · cracked · Dec 27, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE 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 A6WA2017010245518](https://openairdocs.org/sdr/A6WA2017010245518.md): Floorbeam · cracked · Dec 22, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FWD FLOORBEAM ANGLE FOUND CRACKED AT RIVET HOLE, RBL 6. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06.
- [SDR A6WA2017010245517](https://openairdocs.org/sdr/A6WA2017010245517.md): Frame · cracked · Dec 22, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 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 A6WA2017010245501](https://openairdocs.org/sdr/A6WA2017010245501.md): Seat Track · corroded · Dec 21, 2017 · N427ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LT AISLE SEAT TRACK BETWEEN BS 364 AND 409+16 CORRODED. REPLACED THE SEAT TRACK.
- [SDR A6WA2017010245500](https://openairdocs.org/sdr/A6WA2017010245500.md): Floor Support · corroded · Dec 21, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT LANDING BETWEEN BS 559+64 AND 559+80 CORRODED. REPAIRED THE FLOOR SUPPORT.
- [SDR A6WA2017010245515](https://openairdocs.org/sdr/A6WA2017010245515.md): Floorbeam · cracked · Dec 19, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RIGHT 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 A6WA2017010245524](https://openairdocs.org/sdr/A6WA2017010245524.md): Angle · cracked · Dec 16, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE IS CRACKED AT THE INBD SIDE OF RBL 36, BS 484. REPLACED THE ANGLE IAW SRM 51-42-20, AND 51-42-11.
- [SDR A6WA2017010245522](https://openairdocs.org/sdr/A6WA2017010245522.md): Floorbeam · cracked · Dec 15, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017010245519](https://openairdocs.org/sdr/A6WA2017010245519.md): Attach Angle · cracked · Dec 15, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOORBEAM INBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017010245521](https://openairdocs.org/sdr/A6WA2017010245521.md): Attach Angle · cracked · Dec 15, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE ATTACH ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017010245523](https://openairdocs.org/sdr/A6WA2017010245523.md): Angle · cracked · Dec 15, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE CRACKED AT BS 484, OTBD OF LBL 9. REPLACED THE ANGLE IAW SRM 51-42-20.
- [SDR A6WA2017010245520](https://openairdocs.org/sdr/A6WA2017010245520.md): Floorbeam · cracked · Dec 15, 2017 · N427ZW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM INBD ATTACH ANGLE IS CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017010245503](https://openairdocs.org/sdr/A6WA2017010245503.md): Seat Track · corroded · Dec 14, 2017 · N427ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT 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 A6WA2017010245504](https://openairdocs.org/sdr/A6WA2017010245504.md): Seat Track · corroded · Dec 14, 2017 · N427ZW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK NR 3 CORRODED FROM BS 409+128 TO 559, LBL 9. REPLACED THE SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2017091845289](https://openairdocs.org/sdr/A6WA2017091845289.md): Sensor · out of adjust · Sep 17, 2017 · N427ZW · Cndair CL6002B19 · Landing Gear Steering System
  > AFTER 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 A6WA201745265](https://openairdocs.org/sdr/A6WA201745265.md): Actuator · malfunctioned · Sep 7, 2017 · N427ZW · Cndair CL6002B19 · Elevator Control System
  > YOKE 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 A6WA201644336](https://openairdocs.org/sdr/A6WA201644336.md): Sign · unsecure · Sep 16, 2016 · N427ZW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 3941, EXIT SIGN ABOVE SERVICE DOOR HANGING DOWN BY WIRES. IT WAS PLACED ON THE MEL LIST.
- [SDR A6WA201643783](https://openairdocs.org/sdr/A6WA201643783.md): Cooling Fan · vibration · Apr 13, 2016 · N427ZW · Cndair CL6002B19 · Hydraulic System, Main
  > IN 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 A6WA201643445](https://openairdocs.org/sdr/A6WA201643445.md): Cam · obstructed · Jan 9, 2016 · N427ZW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT OPEN OUTSIDE OR INSIDE. REMOVED SCREW UNDER LOCK CAM ASSEMBLY. CLEANED & LUBED PAX DOOR, OPERATIONS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N427ZW/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 = 'N427ZW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N427ZW/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.