# Service difficulty reports: N469AW

A list on [N469AW](https://openairdocs.org/aircraft/N469AW.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 · 206 reports

- [SDR A6WA202609298915](https://openairdocs.org/sdr/A6WA202609298915.md): Indicator · faulted · Sep 29, 2026 · N469AW · Cndair CL6002B19 · Attitude Gyro and Indicating System
  > IN LEVEL FLIGHT STANDBY ATTITUDE INDICATOR SLOWLY CHANGES TO 75 DEGREES NOSE DOWN ATTITUDE, CAGED INDICATOR AND NO CHANGES. AIRCRAFT REMOVED FROM SERVICE. R & R ISI STBY IND OPS CNAD LK CK GOOD AT THIS TIME REF AMM 34-14-01
- [SDR A6WA202409058805](https://openairdocs.org/sdr/A6WA202409058805.md): Strut · faulted · Sep 5, 2024 · N469AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF GOT GEAR DISAGREE, NOSE DOOR OPEN, WOW INPUT, AND STEERING INOP WITH GEAR HANDLE UP. C/W QRH FOR GEAR DISAGREE, PUT GEAR HANDLE DOWN AND GEAR DISAGREE AND NOSE DOOR OPEN WENT OUT. CYCLED NOSE WHEEL STEERING SWITCH PER QRH STEERING INOP LIGHT WEN
- [SDR A6WA202403078722](https://openairdocs.org/sdr/A6WA202403078722.md): Bracket · damaged · Mar 7, 2024 · N469AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > FTER T/O RECEIVED GEAR DISAGREE WARNING, NOSE DOOR OPEN WARNING, NWS INOP, WOW INPUT CAUTION AND STATUS MSG. USED EMER EXT FOR GEAR MSG SHOWED (CONT BLOCK 4) WITHIN A FEW SECONDS OF SELECTING GEAR UP. LANDING WEIGHT. WAS 45,100. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202401038688](https://openairdocs.org/sdr/A6WA202401038688.md): Unknown · unknown · Jan 3, 2024 · N469AW · Cndair CL6002B19 · Navigation System
  > AT 10KFT AHRS 2 FAILED DISPLAYED RED ATT, MAG AND FD FLAGS. AP DISCONNECTED WITH YD 2 INOP MESSAGE. AP WAS IN HEADING MODE. C/W QRH FOUND CBP2-H14 POPPED. (PILOT DECAIRED AN EMERGENCY) AIRCRAFT REMOVED FROM SERVICE. CW OPS CHECK OF AHC IAW AMM 34-21-01. OPS
- [SDR A6WA202302048454](https://openairdocs.org/sdr/A6WA202302048454.md): Not Reported · not reported · Feb 4, 2023 · N469AW · Cndair CL6002B19 · Attitude Gyro and Indicating System
  > ABORTED TAKE-OFF PRIOR TO 80 KNOTS, EFIS COMP MON HEADING. MESSAGE CLEARED AFTER EXITING RUNWAY. BRAKE TEMPS: 3,3,4,5. UNABLE TO CONFIRM WHICH SIDE OFF PRIOR TO RUNWAY EXIT. CAPTAIN'S SIDE 4 DEGREE DRIFT AFTER ONE MINUTE AFTER EXITING RUNWAY. *********AIRCRAF
- [SDR A6WA202211018382](https://openairdocs.org/sdr/A6WA202211018382.md): Floorbeam · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AND CLIP P/N 601R38303-175 AT FS349.0 AND RBL 37 TO 42. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CABIN FLOOR STRUCTURE CROSSBEAM AND CLIP AT FS349.0 AND RBL 37 TO 42. FABRICATED NEW CLIP P/N 601
- [SDR A6WA202211018381](https://openairdocs.org/sdr/A6WA202211018381.md): Door Sill · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR LOWER SILL P/N 601R31132-69 AT FS349.0 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION SERVICE DOOR LOWER SILL AT FS349.0 AND RBL 42. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ
- [SDR A6WA202211018380](https://openairdocs.org/sdr/A6WA202211018380.md): Fitting · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR LOWER SILL DOUBLER P/N 601R38534 AND FITTING 601R38533-9 AT FS 319.0 TO FS349.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR LOWER SILL DOUBLER P/N 601R38534 AND FITTING P/N 601R38533-9 AT FS 319.0
- [SDR A6WA202211018379](https://openairdocs.org/sdr/A6WA202211018379.md): Angle · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AND 601R38303-239 AT FS 319.0 TO FS349.0 AND RBL 43. ************AIRCRAFT REMOVED FROM SERVICE***************** REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AND 601R38303-239
- [SDR A6WA202211018373](https://openairdocs.org/sdr/A6WA202211018373.md): Fairing · gouged · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT HAND WINGLET AT WS400 TRAILING EDGE FAIRING PANEL 572KL P/N 600-15109 HAS GOUGE DAMAGE. ***********AIRCRAFT REMOVED FROM SERVICE********** REPAIRED COMPOSITE OF LEFT HAND WINGLET AT WS400 TRAILING EDGE FAIRING PANEL 572KL. DAMAGE MEASUREMENTS L= 2.0Ï¿½
- [SDR A6WA202211018371](https://openairdocs.org/sdr/A6WA202211018371.md): Floor Support · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CABIN AFT FLOOR SUPPORT BEAM FITTING BETWEEN FS 574.0 AND FS 621.0 AND LBL 27 HAS CORROSION. MEASUREMENTS ARE L= 3.0Ï¿½ X W=1.0Ï¿½ X D= 0.043Ï¿½. ************AIRCRAFT REMOVED FROM SERVICE**************************** BLENDED CORROSION ON PREVIOUS REPAIR OF FLO
- [SDR A6WA202211018372](https://openairdocs.org/sdr/A6WA202211018372.md): Seat Track · corroded · Nov 1, 2022 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR SEAT TRACK FS 364.0 TO FS 394.0 AND RBL 9 HAS CORROSION. SEAT TRACK P/N 20276-288-0-0. **********AIRCRAFT REMOVED FROM THE SERVICE*********************** REPLACED WITH A NEW SEAT TRACK PN 20276-288-0-0 AT FS 364.0 TO FS 394.0 AND RBL 9. ALL WORK
- [SDR A6WA202105187782](https://openairdocs.org/sdr/A6WA202105187782.md): Floor Support · corroded · May 7, 2021 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HAND PRESSURE FLOOR SILL CORRODED AROUND FASTENER HOLE AT FS449.85+2 AND RBL36 ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AROUND RIGHT HAND PRESSURE FLOOR SILL FASTENER HOLE AT FS449.85+2 AND RBL36, BLENDED AREA 1.1Ï¿½L X 1.0Ï¿½W X 0.002Ï¿½
- [SDR A6WA202105147781](https://openairdocs.org/sdr/A6WA202105147781.md): Floor Support · corroded · May 7, 2021 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT HAND PRESSURE FLOOR SILL CORROSION AROUND FASTENER HOLE AT FS449.85 + 2Ï¿½ RBL 36. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AROUND FASTENER HOLE AT FS449.85 + 2Ï¿½ RBL36. 1.100Ï¿½ L X 1.0Ï¿½W X 0.002Ï¿½ D. HFEC PERFORMED WITH NO INDICAT
- [SDR A6WA202105197783](https://openairdocs.org/sdr/A6WA202105197783.md): Skin · corroded · May 6, 2021 · N469AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > CORROSION ON UPPER FUSELAGE SKIN AT ADF ANTENNA FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON UPPER SKIN FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ORIGINAL
- [SDR A6WA202105147780](https://openairdocs.org/sdr/A6WA202105147780.md): Skin · dented · May 5, 2021 · N469AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTS BETWEEN FS621-FS640, S 24 + 3L -S 24 + 5L. NOTED AS D3, D4, D5. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT D3) AT FS 621 + 3.5Ï¿½ AND S24 + 5Ï¿½L, 6.500Ï¿½L X 0.900Ï¿½W X 0.002Ï¿½D, D4) FS 625.00 + 1Ï¿½ AND S24 + 5Ï¿½, 2.850Ï
- [SDR A6WA202105147778](https://openairdocs.org/sdr/A6WA202105147778.md): Skin · dented · May 5, 2021 · N469AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ ***AIRCRAFT REMOVED FROM SERVICE*** CUT OUT DAMAGE BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ MEASURING 8.2Ï¿½L X 4.1Ï¿½W, HFEC PERFORMED WIT
- [SDR A6WA202105147779](https://openairdocs.org/sdr/A6WA202105147779.md): Skin · chafed · May 5, 2021 · N469AW · Cndair CL6002B19 · Ailerons
  > RIGHT HAND AILERON LOWER LEFT END BETWEEN HINGE POINTS D1 AND D2, OUTBOARD OF OUTBOARD HINGE POINT SKIN IS WORN. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE AT D1) A/STA 370.031 TO A/STA 375.857 4.50Ï¿½L X 0.80Ï¿½W 0.009Ï¿½D D2) A/STA 323.843 TO A/
- [SDR A6WA202105127777](https://openairdocs.org/sdr/A6WA202105127777.md): Skin · dented · May 5, 2021 · N469AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENT AT FS 654.50+2.5" S26L+3.4" ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 654.50+2.5" S26L+3.4" TO ORIGINAL CONTOUR, HFEC PERFORMED WITH NO INDICATIONS, REF ASAP EA# AWAC-CRJ253-01631 REV IR DATED 5/7/2021.
- [SDR A6WA202105127776](https://openairdocs.org/sdr/A6WA202105127776.md): Cap · corroded · May 5, 2021 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BEAM CAP CORRODED FS 589.0+7.5 LBL 27. BLENDED CORROSION AT FS 589.0+7.5 LBL 27, OUT OF LIMITS PER CRJ200 SRM 53-00-0 REV 38. REMOVED AND REPLACED FLOOR BEAM CAP AT FS 589.0+7.5 TO FS 606.0 LBL 27 IAW SRM51-42-21 REV 38.
- [SDR A6WA202102197662](https://openairdocs.org/sdr/A6WA202102197662.md): Relay · failed · Feb 18, 2021 · N469AW · Cndair CL6002B19 · Air Distribution System
  > WEIGHT OFF WHEELS, FAN CUT OFF, RECEIVED DISPLAY COOL CAUTION MESSAGE, CONTINUED CLIMB TO 7000 MESSAGE PERSISTED MX ADVISED RETURN TO MKE. A FEW MINUTES LATER F/O'S PFD RECEIVED A DISPLAY TEMP MESSAGE, FOLLOWED BY CAPTAINS PFD DISPLAY TEMP MESSAGE, F/O'S MFD
- [SDR A6WA202102037573](https://openairdocs.org/sdr/A6WA202102037573.md): Strut · collapsed · Feb 1, 2021 · N469AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > RECEIVED GEAR DISAGREE MASTER WARNING SHORTLY AFTER TAKE-OFF AT APPROXIMATELY 300 FT AFE ALONG WITH WOW INPUT CAUTION, STEERING INOP CAUTION, WOW OUTPUT FAIL STATUS MESSAGE. COMPLIED WITH QRH. OCCURRED SHORTLY AFTER SELECTING GEAR UP. ON TAXI-IN AT IAD HYD 3 H
- [SDR A6WA202101267567](https://openairdocs.org/sdr/A6WA202101267567.md): Strut · collapsed · Jan 24, 2021 · N469AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING MSG NOSE GEAR WOULD NOT RETRACT CW QRH, WARNING OCCURED WITHIN 10 SECONDS OF HANDLE SELECTION. SMOOTH NORMAL LANDING BTMS MAX 3. LDG WEIGHT 41700. WOW INPUT CAUTION AND STEERING INOP AFTER THE GEAR DISAGREE AND NOSE
- [SDR A6WA2019061246656](https://openairdocs.org/sdr/A6WA2019061246656.md): Warning Message · false activation · Jun 11, 2019 · N469AW · Cndair CL6002B19 · Brake Anti-Skid Section
  > ON APPROACH AND WHILE SELECTING THE GEAR DOWN, THE FLIGHT CREW RECEIVED AN ANTI-SKID CAUTION MESSAGE. THE FLIGHT CREW CONSULTED THE QRH, CONFERRED WITH DISPATCH, CONTACTED ATC AND DECLARED AN EMERGENCY. CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INC
- [SDR A6WA201904176563](https://openairdocs.org/sdr/A6WA201904176563.md): Bulkhead · cracked · Apr 16, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATION NOTE AT F.S. 621 REAR PRESSURE BULKHEAD AT LBL 9.50, WL 75 100% F.S.H. AND APPOX 1.4 LONG FAILING NDT.
- [SDR A6WA201904156561](https://openairdocs.org/sdr/A6WA201904156561.md): Bulkhead Web · cracked · Apr 14, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INDICATION NOTED AT F.S. 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL 18.0, WL 106, APPROX 1.9 LONG, 53% F.S.H. FAILING NDT.
- [SDR A6WA201904156560](https://openairdocs.org/sdr/A6WA201904156560.md): Bulkhead Web · cracked · Apr 14, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > F.S. 621 PRESSURE BULKHEAD FWD FACE HAS AN INDICATION NOTED AT BL 0.00, WL 29.9, 3.2 INCHES LONG, AND 52% FULL SCREEN HEIGHT FAILING NDT.
- [SDR A6WA201904156556](https://openairdocs.org/sdr/A6WA201904156556.md): Vane · chafed · Apr 13, 2019 · N469AW · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H FLAP VANE SKIN LEADING EDGE IS CHAFED AT STOPS.
- [SDR A6WA201904126555](https://openairdocs.org/sdr/A6WA201904126555.md): Seat Track · corroded · Apr 12, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT RAIL IS CORRODED BETWEEN F.S.399.00 TO F.S.409.00+126.
- [SDR A6WA201904126554](https://openairdocs.org/sdr/A6WA201904126554.md): Seat Track · corroded · Apr 12, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.399 TO F.S.409.00+126.
- [SDR A6WA201904126553](https://openairdocs.org/sdr/A6WA201904126553.md): Skin · chafed · Apr 11, 2019 · N469AW · Cndair CL6002B19 · Aileron Tabs
  > L/H INBD FLAP VANE SKIN LEADING EDGE IS CHAFED AT CENTER AND INBD STOP LOCATIONS.
- [SDR A6WA201904086542](https://openairdocs.org/sdr/A6WA201904086542.md): Beam · damaged · Apr 6, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND DAMAGE ON THE CARGO DOOR BEAM IN MULTIPLE AREAS, MARKED WITH RED TAPE.
- [SDR A6WA201904086543](https://openairdocs.org/sdr/A6WA201904086543.md): Intercostal · cracked · Apr 6, 2019 · N469AW · Cndair CL6002B19 · APU Cowling/Containment
  > APU INLET DOOR ACTUATOR AFT MOUNT BRACKET APPEARS TO BE CRACKED AND INTERCOSTAL FWD END APPEARS CRACKED (FS654).
- [SDR A6WA201904086539](https://openairdocs.org/sdr/A6WA201904086539.md): Floorbeam · cracked · Apr 6, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Frame
  > WHILE WORKING R/H F.S.280 BEAM FOUND L/H F.S.280 BEAM CRACKED AT LBL9
- [SDR A6WA201904086538](https://openairdocs.org/sdr/A6WA201904086538.md): Floorbeam · cracked · Apr 6, 2019 · N469AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > R/H F.S.280 BEAM IS CRACKED AT RBL9.
- [SDR A6WA201904056537](https://openairdocs.org/sdr/A6WA201904056537.md): Bracket · cracked · Apr 5, 2019 · N469AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER BRACKET ON CARGO DOOR SUPPORT FRAME IS CRACKED
- [SDR A6WA201904046531](https://openairdocs.org/sdr/A6WA201904046531.md): Seat Track · corroded · Apr 3, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+112 TO F.S.559.00+80.
- [SDR A6WA201904046532](https://openairdocs.org/sdr/A6WA201904046532.md): Seat Track · corroded · Apr 3, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+96 TO F.S.559.00-80.
- [SDR A6WA201904046533](https://openairdocs.org/sdr/A6WA201904046533.md): Seat Track · corroded · Apr 3, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+96 TO F.S.559.00+80.
- [SDR A6WA201904046535](https://openairdocs.org/sdr/A6WA201904046535.md): Seat Track · corroded · Apr 3, 2019 · N469AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK IS CORRODED BETWEEN F.S.559.00+64 TO F.S.559.00+32.
- [SDR A6WA20194116550](https://openairdocs.org/sdr/A6WA20194116550.md): Warning Message · illuminated · Mar 16, 2019 · N469AW · Cndair CL6002B19 · Central Warning
  > DISPLAY COOL CAUTION MESSAGE RAN QRH, MESSAGE DID NOT CLEAR. RECIEVED MESSAGE AT 34000 FT
- [SDR A6WA2018121746242](https://openairdocs.org/sdr/A6WA2018121746242.md): Warning Message · false activation · Dec 16, 2018 · N469AW · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > THRU 8500 FEET MASTER WARNING FOR ANTI ICE DUCT IN THE RH FUSELAGE LI E. RAN QRH NO OTHER ACTION REQUIRED. QRH REQUIRES THAT THE WING, COWL AND 14TH STAGE VLVS TO BE CLOSED. THE MSG REMAINED FOR 10 MINUTES AFT R ALL VLVS WERE CLOSED.
- [SDR A6WA201745253](https://openairdocs.org/sdr/A6WA201745253.md): Light · inoperative · Sep 5, 2017 · N469AW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTING INOPERATIVE AT ROW 9 TO BACK. INSPECTED THE LIGHT, NO DEFECTS. NOTED THE AFT RIBBON ASSY HAS NO POWER TO LIGHT.
- [SDR A6WA201745219](https://openairdocs.org/sdr/A6WA201745219.md): Light · inoperative · Aug 22, 2017 · N469AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ROW 6-8 DID NOT OPERATE WHEN INITIALLY TESTED, LIGHTS TURNED ON WHEN LEFT IN ON POSITION FOR EXTENDED PERIOD, APPROXIMATELY 90 SECONDS. R & R THE NR 3 EMERGENCY BATTERY INVERTER IAW AMM 33-51-07, R & R THE NR 4 EMERGENCY BATTERY INVERTER AMM
- [SDR A6WA2017082245217](https://openairdocs.org/sdr/A6WA2017082245217.md): Sign · unreliable · Aug 21, 2017 · N469AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT SYSTEM IS UNRELIABLE. REMOVED AND REPLACED THE RT EMERGENCY EXIT FLOOR LEVEL SIGN IAW AMM 33-51-10-04. SYSTEM OPS CHECKED GOOD.
- [SDR A6WA2017081845205](https://openairdocs.org/sdr/A6WA2017081845205.md): Wire · broken · Aug 16, 2017 · N469AW · Cndair CL6002B19 · Light System Wiring
  > WIRE BROKEN FOR EMERGENCY LIGHTS BETWEEN ROW 6 AND ROW 8. REPAIRED THE WIRE LY22822 IAW ESPM 20-16-00.
- [SDR A6WA201745197](https://openairdocs.org/sdr/A6WA201745197.md): Light · inoperative · Aug 14, 2017 · N469AW · Cndair CL6002B19 · Emergency Lighting
  > EMER EXIT FLOOR LIGHTING FROM ROW 8-5 INOP. RT EMER EXIT LIGHT ON SIDEWALL IS INOP. INSPECTED FLOOR TRACK LIGHTING. NO DAMAGE NOTED. NO DAMAGE TO SIDEWALL LIGHT. NO OTHER LIGHTS INOP. REF 316335/4 FOR MEL.
- [SDR A6WA201745182](https://openairdocs.org/sdr/A6WA201745182.md): Inverter · inoperative · Aug 14, 2017 · N469AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOOR LIGHTING ROW 5-8 AND RT OVERWING EXIT INOPERATIVE. REMOVED AND REPLACED THE NR 3 INVERTER IAW AMM 33-31-07-04, SYSTEM OPS CHECKED GOOD.
- [SDR A6WA201745194](https://openairdocs.org/sdr/A6WA201745194.md): Connector · damaged · Aug 12, 2017 · N469AW · Cndair CL6002B19 · Light System Wiring
  > PER MAINTENANCE CONTROL, REQUEST FLOOR TRACK LIGHT CONNECTOR AT ROW 6 TO 8 NEEDS REPLACED. FOUND BROKEN CONNECTOR PINS BETWEEN SEAT ROW 7-8. R&R ONE SECTION OF FLOOR TRACK LIGHTING IAW SUPP 16-371A. OP CK GOOD.
- [SDR A6WA201745200](https://openairdocs.org/sdr/A6WA201745200.md): Connector · unsecure · Aug 12, 2017 · N469AW · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS ON FLOOR ROW 6-8 NOT WORKING. RESECURED EMERG FLOOR TRACK LIGHT CONNECTORS AT ROW 6-8. OP CK GOOD IAW AMM 33-51-00.

Next page: https://openairdocs.org/aircraft/N469AW/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 = 'N469AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N469AW/reports

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