# Service difficulty reports: N410AW

A list on [N410AW](https://openairdocs.org/aircraft/N410AW.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 6 · 295 reports

- [SDR A6WA202607128899](https://openairdocs.org/sdr/A6WA202607128899.md): Warning Light · illuminated · Jul 12, 2026 · N410AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > DURING CLIMB RECEIVED FLAPS FAIL CAUTION OCCURRED AT FL220. FLAPS WERE NOT SELECTED FLAPS FAILED AT 0. NO IMPROPER FLAP HANDLE MOVEMENT SUSPECTED. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202502128862](https://openairdocs.org/sdr/A6WA202502128862.md): Smoke Detector · false activation · Feb 12, 2025 · N410AW · Cndair CL6002B19 · Smoke Detection
  > SMOKE TOILET CAUTION MESSAGE DISPLAYED WHILE PARKED AT GATE. C/W QRH MESSAGE REMAINED. C/B 2C5 2D14 2D15 2S2 2U2 PULLED. AIRCRAFT REMOVED FROM SERVICE. R&R LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD AT THIS TIME. CLOSED C/B 2C5, 2D14, 2D15, 2S2,
- [SDR A6WA202405288755](https://openairdocs.org/sdr/A6WA202405288755.md): Winglet · damaged · May 28, 2024 · N410AW · Cndair CL6002B19 · Wing, Plate/Skin
  > REPAIR TO RIGHT WINGLET TIP STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FOLLOWING ITEMS REF CRJ200 SRM 51-42-13, 51-40-11, 51-41-00, 51-42-06, 51-42-20, 51-42-13 REV.39. TIP FAIRING PN 600-15110-4; LEADING EDGE PN 600-15111-4; AFT F
- [SDR A6WA202405138748](https://openairdocs.org/sdr/A6WA202405138748.md): Support Bracket · cracked · May 13, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK FOUND ON POWER RECEPTACLE SUPPORT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET SUPPORT MEMBER P/N 600-33-83-33 ON POWER RECEPTACLE IAW SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 20031, TT: 47,227:03 TC: 4
- [SDR A6WA202405118746](https://openairdocs.org/sdr/A6WA202405118746.md): Fitting · cracked · May 11, 2024 · N410AW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > CRACKED FITTING ON UPPER TRANSLATING COWLING DOOR. ACFT REMOVED FROM SERVICE. REMOVED & REPLACED FITTING INTERLOCK RH ON UPPER TRANSLATING COWLING DOOR, IAW SRM 51-42-28 REV. 39 DATE 2024-05-08. ALL WORK PERFORMED UNDER WORK ORDER 004309. NO. 20124,
- [SDR A6WA202405108744](https://openairdocs.org/sdr/A6WA202405108744.md): Seat Track · damaged · May 10, 2024 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT REMOVED FROM SERVICE. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C.
- [SDR A6WA202405108745](https://openairdocs.org/sdr/A6WA202405108745.md): Seat Track · damaged · May 10, 2024 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR ON FLOOR PANEL & ANGLE AT LBL 12 BETWEEN BS 250 TO 265 IAW MHI RJ REO 601R-53-11-3927 REV. -. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 50008
- [SDR A6WA202405048740](https://openairdocs.org/sdr/A6WA202405048740.md): Channel · corroded · May 4, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FWD GALLEY COMPARTMENT 112 LOWER STRIP HAS SIGNS OF CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED LOWER STRIP ON FWD GALLEY COMPARTMENT 112 REF. C&D ZODIAC CMM 25-33-39 REV. 2
- [SDR A6WA202405028739](https://openairdocs.org/sdr/A6WA202405028739.md): Doubler · corroded · May 2, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FWD GALLEY HARD POINT MOUNT CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED RIGHT FORWARD GALLEY HARD MOUNT POINT REF. C&D ZODIAC CMM 25-31-56 REV. 8
- [SDR A6WA202404308737](https://openairdocs.org/sdr/A6WA202404308737.md): Bracket · corroded · Apr 29, 2024 · N410AW · Cndair CL6002B19 · Service Doors
  > CORROSION FOUND ON SERVICE DOOR BASE STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET LOWER FRAM ON SERVICE DOOR BASE STRUCTURE IAW CRJ200SRM 51-42-20 REV39
- [SDR A6WA202404268738](https://openairdocs.org/sdr/A6WA202404268738.md): Bracket · corroded · Apr 26, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON PASSENGER DOOR CUTOUT STRUCTURE IN 4 PLACES. FS319.7 TO FS349. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 2 EA BRACKET ASSYS P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS310+5 AND FS 333+10 LBL 42 AND REMOVED AND
- [SDR A6WA202404306732](https://openairdocs.org/sdr/A6WA202404306732.md): Blanking Plate · cracked · Apr 26, 2024 · N410AW · Cndair CL6002B19 · Fuselage Main, Structure
  > BLANKING PLATE IN LEFT AND RIGHT WHEEL WELL FOUND CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED LH AND RH BRACKETS FROM WHEEL WELLS IAW CRJ200 SRM 51-42-06 REV 39.
- [SDR A6WA202404298735](https://openairdocs.org/sdr/A6WA202404298735.md): Line · cracked · Apr 25, 2024 · N410AW · Cndair CL6002B19 · Hydraulic System, Main
  > RH MLG HYDRAULIC LINE ANGLE SUPPORT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1EA BRACKET ASSY P/N 601R75262-153 ON RH MLG PANEL RACK AT FS 523.67 BETWEEN RBL18 AND RBL27 IAW CRJ200SRM 51-42-06 REV 39.
- [SDR A6WA202404308731](https://openairdocs.org/sdr/A6WA202404308731.md): Support · cracked · Apr 23, 2024 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR CROSSBEAM SUPPORT CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE P/N 601R35050-109 AT BAGGAGE DOOR ON AFT CARGO SURROUND STRUCTURE IAW CRJ200 SRM 51-42-21 REV 39.
- [SDR A6WA202202218116](https://openairdocs.org/sdr/A6WA202202218116.md): None · none · Feb 18, 2022 · N410AW · Cndair CL6002B19 · Landing Gear System
  > AFTER T/O RECEIVED STEERING INOP CAUTION MSG. WT OFF WHEEL INOP CAUTION MSG. WT OFF WHEEL OUTPUT FAIL STATUS MSG. C/W QRH MSG PERSISTED. ***AIRCRAFT REMOVED FROM SERVICE*** R&R NLG RH WOW HARNESS PER CRJ 200 AMM 32-61-05 OPOS CK AND NLG STEERING GOOD
- [SDR A6WA202110087896](https://openairdocs.org/sdr/A6WA202110087896.md): None · none · Oct 7, 2021 · N410AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > BOTH RIGHT MAIN LANDING GEAR TIRES WERE FLAT TAXING INTO GATE. ***AIRCRAFT REMOVED FROM SERVICE*** REF 343164/3, 343164/4, 343165/1, 343165/2, FOR THE CORRECTIVE ACTIONS, REPLACING #3 AND 4 MAIN TIRES
- [SDR A6WA202102087621](https://openairdocs.org/sdr/A6WA202102087621.md): Pdu · malfunctioned · Feb 6, 2021 · N410AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION AFTER TAKE-OFF, FLAPS REMAINED AT 8 DEGREES WHEN SELECTING ZERO DEGREES (FLAPS FAILED AT 8 DEGREES), BRAKE TEMPS NORMAL ON LANDING. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUP. 98-18I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. A
- [SDR A6WA2020031347227](https://openairdocs.org/sdr/A6WA2020031347227.md): Nut · loose · Mar 12, 2020 · N410AW · Cndair CL6002B19 · Hydraulic System, Main
  > HYD 1 LO PRESS ON CLIMB-OUT, COMPLIED WITH QRH, RECEIVED HYD EDP 1A CAUTION. HYD 1B SELECTED ON APPROX. 1 MIN. SELECTED OFF PER QRH, HYD 1 LO PRESS RETURNED. NO OBSERVED TEMPERATURE CHANGE IN SYSTEM. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND LOOSE
- [SDR A6WA2020031247224](https://openairdocs.org/sdr/A6WA2020031247224.md): Pseu · malfunctioned · Mar 10, 2020 · N410AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > SHORTLY AFTER DEPARTURE OUT OF OKC, THE CREW RECEIVED A NOSE WHEELS STEERING INOP MESSAGE. THERE WAS A STEERING AND WOW INPUT CAUTION AT THE SAME TIME. THE FLIGHT AIR RETURNED TO OKC. NO OVERWEIGHT LANDING AND NO EMERGENCY WAS DECLARED "AIRCRAFT REMOVED FROM
- [SDR A6WA2020031047222](https://openairdocs.org/sdr/A6WA2020031047222.md): Stringer · corroded · Mar 10, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > SUPPLEMENTAL, STRINGER 26R CORRODED BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE: BLENDED TO REMOVE CORROSION. ORIGINAL MATERIAL THICKNESS -.080 MATERIAL LOSS -.080 REMAINING THICKNESS - 0.00 ALLOWABLE LIMITS -.008 REPAIRED STRINGER 26R IAW EA AW
- [SDR A6WA2020030947219](https://openairdocs.org/sdr/A6WA2020030947219.md): Intercostal · corroded · Mar 7, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SUPPLEMENTAL, INTERCOSTAL JUST TO THE LEFT OF STRINGER 27 HAS CORROSION BETWEEN FS349 AND FS364. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS -.080 MATERIAL LOSS -.010 REMAINING MATERIAL -.070 ALLOWABLE LIMITS -.008 REMOV
- [SDR A6WA2020030947218](https://openairdocs.org/sdr/A6WA2020030947218.md): Stringer · corroded · Mar 7, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > SUPPLEMENTAL, STRINGER 26L HAS CORROSION BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS -.063 MATERIAL LOSS -.030 REMAINING THICKNESS -.033 REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-42-06 AND
- [SDR A6WA2020030647217](https://openairdocs.org/sdr/A6WA2020030647217.md): Stringer · cracked · Mar 6, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3 IS CRACKED AT FS379.00. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED STRINGER IAW CRJ200 SRM 51-42-06 & 51-42-21.
- [SDR A6WA2020030347215](https://openairdocs.org/sdr/A6WA2020030347215.md): Attach Angle · cracked · Mar 3, 2020 · N410AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LATCH COVER FWD ATTACH ANGLE IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.
- [SDR A6WA2020030247213](https://openairdocs.org/sdr/A6WA2020030247213.md): Angle · corroded · Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2020030247212](https://openairdocs.org/sdr/A6WA2020030247212.md): Angle · corroded · Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2020030247211](https://openairdocs.org/sdr/A6WA2020030247211.md): Seat Track · corroded · Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RH #2 SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS -.110 MATERIAL LOSS -.025 REMAINING THICKNESS.085 ALLOWABLE LOSS.020 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 53-01-11.
- [SDR A6WA2020030247214](https://openairdocs.org/sdr/A6WA2020030247214.md): Splice Angle · cracked · Feb 29, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SPLICE ANGLE AT FS 409+96 STRINGER 20 RIGHT IS CRACKED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED CRACKED REINFORCING SPLICE ANGLE IAW CRJ 200 SRM 51-42-06 AND REO 601R-53-31-1092
- [SDR A6WA2020022847209](https://openairdocs.org/sdr/A6WA2020022847209.md): Seat Track · corroded · Feb 28, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT HAND #4 FLOOR SEAT TRACK CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS -.110 MATERIAL REMOVED -.022 REMAINING MATERIAL -.088 ALLOWABLE LOSS -.011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11
- [SDR A6WA2020022747206](https://openairdocs.org/sdr/A6WA2020022747206.md): Seat Track · corroded · Feb 27, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH #3 FLOOR SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS -.110 MATERIAL LOSS -.022 REMAINING THICKNESS -.088 ALLOWABLE MATERIAL LOSS -.011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.
- [SDR A6WA2020022547200](https://openairdocs.org/sdr/A6WA2020022547200.md): Bulkhead Web · cracked · Feb 25, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > COMPLY WITH AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING GREO 601R-53-61-1240 REV. D. "AIRCRAFT REMOVED FROM SERVICE" MODIFIED REAR PRESSURE BULKHEAD FS621 IAW GREO 601R-53-61-1240 REV. D.
- [SDR A6WA202002247197](https://openairdocs.org/sdr/A6WA202002247197.md): Support · cracked · Feb 23, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE, INBOARD END LEADING EDGE PANEL 584DT SUPPORT IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SUPPORT IAW CRJ200 SRM 51-42-13
- [SDR A6WA202002247195](https://openairdocs.org/sdr/A6WA202002247195.md): Attach Angle · cracked · Feb 23, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LOWER ATTACH ANGLE ON AFT END OF BEAM IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-42-21.
- [SDR A6WA202002247196](https://openairdocs.org/sdr/A6WA202002247196.md): Skin · chafed · Feb 23, 2020 · N410AW · Cndair CL6002B19 · Ailerons
  > RH AILERON UPPER LEADING EDGE SKIN IS CHAFFED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED LEADING EDGE SKIN IAW CRJ200 SRM 51-42-06 AND AWAC SUPPLEMENT 13-055B.
- [SDR A6WA202002247198](https://openairdocs.org/sdr/A6WA202002247198.md): Floor Support · corroded · Feb 23, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM IS CORRODED AT FS559+48 TO 559+80, RBL 9. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED FLOOR BEAM IAW CRJ200 SRM 53-00-43, FIG. 203. BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL -.050 MATERIAL LOSS -.024 REMAINING MATERIAL -.026 ALLOWABLE LOSS -.
- [SDR A6WA202002247191](https://openairdocs.org/sdr/A6WA202002247191.md): Support Angle · cracked · Feb 21, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER LATCH CLOSE PLATE HAS A CRACKED SUPPORT ANGLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.
- [SDR A6WA202022147190](https://openairdocs.org/sdr/A6WA202022147190.md): Angle · cracked · Feb 21, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS625 TO INTERCOSTAL CLIP CRACKED AT STRINGER 14L. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-21.
- [SDR A6WA2020022047189](https://openairdocs.org/sdr/A6WA2020022047189.md): Support Bracket · cracked · Feb 19, 2020 · N410AW · Cndair CL6002B19 · Ailerons
  > RIGHT WING AILERON CENTER PANEL SUPPORT BRACKET IS CRACKED. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED SUPPORT BRACKET IAW CRJ200 SRM 51-42-06.
- [SDR A6WA2020021947188](https://openairdocs.org/sdr/A6WA2020021947188.md): Bulkhead Web · cracked · Feb 19, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0 AND WL 111.00. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ 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 U
- [SDR A6WA2020021847183](https://openairdocs.org/sdr/A6WA2020021847183.md): Door Sill · corroded · Feb 14, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL ANGLE IS CORRODED. FULL LENGTH OF PART. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LOWER SILL ANGLE I/A/W CRJ-200 SRM 51-42-06, 51-42-10, 51-42-21
- [SDR A6WA2020021447181](https://openairdocs.org/sdr/A6WA2020021447181.md): Skin · chafed · Feb 14, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN TWO PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED TO SMOOTH CONTOUR FLAP STATION 56.50 MATERIAL LOSS.014 FLAP STATION 105.00 MATERIAL LOSS.026 ORIGINAL THICKNESS.050 REMOVED AND REPLACED LEADING EDGE
- [SDR A6WA202002147175](https://openairdocs.org/sdr/A6WA202002147175.md): Floor Support · corroded · Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SUPPORT CLEATS ARE CORRODED, FWD AND AFT. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL.063 MATERIAL LOSS.018 REMAINING THICKNESS.045 ALLOWABLE LOSS.006 REMOVED AND REPLACED CLEAT AND BRACKET IAW CRJ200 SRM 51
- [SDR A6WA202002147178](https://openairdocs.org/sdr/A6WA202002147178.md): Skin · chafed · Feb 13, 2020 · N410AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT WING IB FLAP VANE SKIN LE CHAFFED IN 3 PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED MID AND INBD AREAS IAW BOMBARDIER REO 601R-57-52-004 REMOVED AND REPLACED LE PANEL AT STA. 141 IAW CRJ200 SRM 51-42-13
- [SDR A6WA202002147177](https://openairdocs.org/sdr/A6WA202002147177.md): Cargo Track · corroded · Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT RBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS.160 MATERIAL LOSS.080 REMAINING THICKNESS.080 ALLOWABLE LOSS.060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00-
- [SDR A6WA202002147176](https://openairdocs.org/sdr/A6WA202002147176.md): Cargo Track · corroded · Feb 13, 2020 · N410AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACK AT LBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS.160 MATERIAL REMOVED.070 REMAINING MATERIAL.090 ALLOWABLE LOSS.060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00
- [SDR A6WA202021247169](https://openairdocs.org/sdr/A6WA202021247169.md): Bulkhead Web · cracked · Feb 12, 2020 · N410AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD IS CRACKED AT CARGO DOOR AFT TRACK, APPROX. LBL27.5 AND WL 130. AIRCRAFT REMOVED FROM SERVICE REPAIR TRANSFERRED TO AAR W.O. 1018176/2000/0019 C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS6
- [SDR A6WA2019052346633](https://openairdocs.org/sdr/A6WA2019052346633.md): Skin · dented · May 22, 2019 · N410AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN IS DENTED BETWEEN FS 700.00 AND 736.00 AND BETWEEN STRINGER 16R AND 17R.
- [SDR A6WA2019051546600](https://openairdocs.org/sdr/A6WA2019051546600.md): Warning System · activated · May 13, 2019 · N410AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AT 600 FT AGL RECEIVED NLG UNSAFE (YELLOW CROSSHATCHED) ACCOMPLISHED G O AROUND AND CW QRH PROCEDURE. CYCLED GEAR AND RECEIVED 3 GREEN (INTER MITTENT) MC THIS INDICATION IS WITH GEAR DOWN ONLY AND INTERMITTENT. *FROM PLOT* - THE PILOT WAS ON APPROACH AND SELE
- [SDR A6WA2018022645659](https://openairdocs.org/sdr/A6WA2018022645659.md): Frame · chafed · Feb 25, 2018 · N410AW · Cndair CL6002B19 · Fuselage Main, Frame
  > REPAIR RT FRAME FS718.
- [SDR A6WA2018022645657](https://openairdocs.org/sdr/A6WA2018022645657.md): Bracket · cracked · Feb 25, 2018 · N410AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR ASSIST MOTOR BRACKET CRACKED.

Next page: https://openairdocs.org/aircraft/N410AW/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 = 'N410AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N410AW/reports

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