# Service difficulty reports: N423AW

A list on [N423AW](https://openairdocs.org/aircraft/N423AW.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 · 165 reports

- [SDR A6WA202308238650](https://openairdocs.org/sdr/A6WA202308238650.md): Unknown · unknown · Aug 23, 2023 · N423AW · Cndair CL6002B19 · Passenger/Crew Doors
  > AX DOOR WARNING MSG AT 12,000 FLT LOST PRESSURIZATION IN CABIN AN QRH DESCENDED AND REGAINED PRESSURIZATION IN MANUAL MODE. MSG NEVER CLEARED *********AIRCRAFT REMOVED FROM SERVICE******** ADJUSTED OUTER PAX DOOR HANDLE DETENT IAW AMM 52-11-03. NO OTHER
- [SDR A6WA202305258614](https://openairdocs.org/sdr/A6WA202305258614.md): Unknown · unknown · May 25, 2023 · N423AW · Cndair CL6002B19 · Doors
  > RECEIVED PASSENGER DOOR WARNING MESSAGE IN FLIGHT. FA NOTED LIGHT AIR LEAK WHILE CABIN PRESSURE HELD NORMALLY. AFTER LANDING FA NOTED PASSENGER DOOR HANDLE LIGHTLY UP FROM REGULAR POSITION. FA REPOSITIONED THE HANDLE, MESSAGE DISAPPEARED. *****AIRCRAFT REM
- [SDR A6WA202304248581](https://openairdocs.org/sdr/A6WA202304248581.md): Hinge Arm · corroded · Apr 24, 2023 · N423AW · Cndair CL6002B19 · Aerodynamic Fairings
  > TOILET SERVICE DOOR 196AR LOWER HINGE IS CORRODED AND BONDING JUMPER IS BROKEN. ********AIRCRAFT REMOVED FROM SERVICE*********** INSTALLED 2EA NEW SERVICEABLE HINGE ARMS IAW CRJ-200 SRM 51-41-02 AND 51-42-21. REPLACED JUMPER IAW CRJ 200 AMM 51-80-00-400-802.
- [SDR A6WA202304248582](https://openairdocs.org/sdr/A6WA202304248582.md): Skin · gouged · Apr 24, 2023 · N423AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > A 1" LONG SCRATCH ON THE RH SIDE OF THE NOSE, ABOVE THE OXYGEN SERVICING DOOR. ******AC REMOVED FROM SERVICE*********** INSTALLED RH SKIN PANEL BETWEEN FS 193 TO 210 STRINGER 0 TO 16R IAW CRJ 200 SRM 51-42-06 AND 51-42-13
- [SDR A6WA202304228578](https://openairdocs.org/sdr/A6WA202304228578.md): Intercostal · corroded · Apr 22, 2023 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD6 IS CORRODED ***** AC REMOVED FROM SERVICE ***** REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 P/N 601R318057-1 IAW CRJ 200 SRM 51-42-06 AND 51-42-21
- [SDR A6WA202304158559](https://openairdocs.org/sdr/A6WA202304158559.md): Former · corroded · Apr 15, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR FWD FORMER IS CORRODED IN MULTIPLE AREAS FS 311.75 ******AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED PAX DOOR FWD FORMER P/N601R318031-5 IAW CRJ 200 SRM 51-40-11,51-42-06 AND 52-42-21
- [SDR A6WA202304158556](https://openairdocs.org/sdr/A6WA202304158556.md): Former · corroded · Apr 15, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR AFT FORMER IS CORRODED IN MULTIPLE PLACES. ********AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ 200 STM 51-42-06 AND 51-42-21
- [SDR A6WA202304158554](https://openairdocs.org/sdr/A6WA202304158554.md): Stiffener · cracked · Apr 15, 2023 · N423AW · Cndair CL6002B19 · Standard Practices/Structures
  > PAX DOOR AIR STAIR FWD WEB STIFFENER SECOND DOWN FROM THE TOP IS CRACKED AT THE OUTER END FASTENER HOLE. *******AIRCRAFT REMOVED FROM SERVICE******* REMOVED CRACKED STIFFENER, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STIFFENER PN 601R317742-1 IAW CRJ 200
- [SDR A6WA202304158553](https://openairdocs.org/sdr/A6WA202304158553.md): Angle · corroded · Apr 15, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FLOOR SUPPORT ANGLE BETWEEN RBL 18.0 AND RBL 27.0 FS 621.00 CORRODED AROUND OUTBOARD NUTPLATE HOLE *******AIRCRAFT REMOVED FROM SERVICE********* REPAIRED FLOOR SUPPORT ANGLE BETWEEN RBL 18 AND RBL 27 IAW MHIRJ REO 601R-53-61-8004 REV -- DATED 2023-04-13
- [SDR A6WA202304108546](https://openairdocs.org/sdr/A6WA202304108546.md): Angle · cracked · Apr 10, 2023 · N423AW · Cndair CL6002B19 · Doors
  > PAX DOOR AFT STAIR PANEL ANGLE IS CRACKED AT UPPER MID STEP. *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED CRACKED ANGLE. FABRICATED NEW SERVICABLE REPAIR ANGLE WITH 2024-T3.032" PO# W81195 REFERENCING GREO 601R-52-11-702 REV E IAW CRJ 200 SRM 51-24-2
- [SDR A6WA202304048535](https://openairdocs.org/sdr/A6WA202304048535.md): Intercostal · cracked · Apr 4, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FOUND CRACK AT INTERCOSTAL SUPPORT BRACKET BETWEEN FS 621- 625 AT STGR 14L. *****AIRCRAFT REMOVED FROM SERVICE****** REMOVED AND REPLACED ANGLE BRACKET PN 601-35012-51 IAW CRJ-200 SRM 51-42-21.
- [SDR A6WA202303308533](https://openairdocs.org/sdr/A6WA202303308533.md): Intercostal · cracked · Mar 30, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > INTERCOSTAL "U" CHANNEL IS CRACKED BETWEEN FS 621- 625 AT STGR 14L. *******AIRCRAFT REMOVED FROM SERVICE****** INSTALLED NEW INTERCOSTAL "U" CHANNEL BETWEEN FS 621 AND FS 625, STGR 14L IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR A6WA202303308534](https://openairdocs.org/sdr/A6WA202303308534.md): Intercostal · cracked · Mar 30, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > INTERCOSTAL "U" CHANNEL IS CRACKED BETWEEN FS 621 AND FS 625, STGR 13L. *******AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW SERVICEABLE INTERCOSTAL "U" CHANNEL BETWEEN FS 621 AND FS 625, STGR 13L IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR A6WA202303298542](https://openairdocs.org/sdr/A6WA202303298542.md): Angle · corroded · Mar 29, 2023 · N423AW · Cndair CL6002B19 · Fuselage Fixed Partitions
  > PAX DOOR SILL ANGLE HAS SMALL SPOTS OF CORROSION ALL ALONG THE UPPER TRIM ANGLE. AC REMOVED FROM SERVICE. REMOVED AND REPLACED UPPER TRIM ANGLE IAW CRJ200 SRM 51-42-13.
- [SDR A6WA202303268562](https://openairdocs.org/sdr/A6WA202303268562.md): Door Frame · corroded · Mar 26, 2023 · N423AW · Cndair CL6002B19 · Fuselage Structure (General)
  > AVIONICS BAY DOOR CUTOUT LANDING IS CORRODED ******AIRCRAFT REMOVED FROM SERVICE******* COMPLIED WITH MHIRJ REO 601R-53-21-3622 REV -- DATED 2023-04-12
- [SDR A6WA202303258530](https://openairdocs.org/sdr/A6WA202303258530.md): Bonding Plate · corroded · Mar 25, 2023 · N423AW · Cndair CL6002B19 · Nacelle/Pylon Structure
  > L/H PYLON UPPER SURFACE OUTBOARD BONDING PLATE IS CORRODED. *********AIRCRAFT REMOVED FROM SERVICE********* REPLACED PYLON BONDING PLATE IAW TS 15-335 DATED 12/22/2015.
- [SDR A6WA202206098190](https://openairdocs.org/sdr/A6WA202206098190.md): Proximity Sensor · warning message · Jun 9, 2022 · N423AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER TAKEOFF RECEIVED GEAR DISAGREE WARNING WHEN SELECTING GEAR UP. APPROX 6 SECONDS AFTER GEAR SELECTION. ALSO RECEIVED NOSE DOOR WARNING MESSAGE. AFTER OPERATING MANUAL RELEASE, RECEIVED A/SKID IB AND PARKING BRAKE SOV. NO ICING, TURBULENCE OR EXCESSIVE
- [SDR A6WA202201058049](https://openairdocs.org/sdr/A6WA202201058049.md): None · none · Jan 1, 2022 · N423AW · Cndair CL6002B19 · Landing Gear Door Retract Section
  > GEAR DISAGREE IN FLIGHT DURING CRUISE WHILE LANDING LEVER WAS UP, PER QRH PULLED MANUAL LEVER AND MESSAGES DISAPPEARED. MESSAGE LASTED FOR ABOUT 15SEC, THE NOSE GEAR SHOWED A RED BOX, HYD PRESSURES AND QUANTITY WAS ALL IN GREEN, THERE WERE NO OTHER ASSOCIATED
- [SDR A6WA202110187905](https://openairdocs.org/sdr/A6WA202110187905.md): None · none · Oct 16, 2021 · N423AW · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) System
  > CREW REPORTS SMOKE/HAZE IN CABIN ON TAXI-OUT, ALSO RECEIVED APU OIL PRESS AND APU OIL TEMP CAUTION MESSAGES, ACCOMPANIED BY APU SHUT DOWN. OIL FOUND ON BELLY AND IN ENCLOSURE UPON GATE RETURN. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS *****SUPPLEM
- [SDR A6WA202106187804](https://openairdocs.org/sdr/A6WA202106187804.md): Control Unit · failed · Jun 15, 2021 · N423AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING APPROACH WHEN SELECTING FLAPS TO 30 DEGREES, RECEIVED A FLAPS FAIL CAUTION MESSAGE. LH FLAP SHOWS 22 DEGREES, RH SHOWS 23 DEGREES. C/W SUPP 98-018I, FLAPS DID NOT RESET ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 305693 MX WC #6-11 FOR ALL WORK PERFO
- [SDR A6WA202104167744](https://openairdocs.org/sdr/A6WA202104167744.md): Seat Track · corroded · Apr 15, 2021 · N423AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LAV FS559+80 RBL9 CORRODED. REQUIRES REPLACEMENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK AT FS559+80, RBL 9 IAW REO 601R-53-00-764
- [SDR A6WA2020021947186](https://openairdocs.org/sdr/A6WA2020021947186.md): Bracket · damaged · Feb 17, 2020 · N423AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > DURING T/O SELECTED GEAR UP, GEAR DISAGREE W/ NLG DOOR EICAS MSG, OCCURED DURING BANK, MANUAL RELEASE USED. HYP PUMP AUTO-ON-AUTO- AUTO, APPROX 160 KTS, NORMAL LANDING 45,500 LBS. AIRCRAFT REMOVED FROM SERVICE R/R PROX SENSOR BRACKET BEHIN
- [SDR A6WA2019090546837](https://openairdocs.org/sdr/A6WA2019090546837.md): Warning System · activated · Aug 19, 2019 · N423AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > AFTER DEPARTING RIC THE CREW EXPERIENCED A FLAP FAIL CAUTION MESSAGE. THEY ADVISED DISPATCH, DECLARED AN EMERGENCY WITH ATC AND DECIDED TO CONTINUE TO ORD. THEY ADVISED THE FLIGHT ATTENDANT OF THE SITUATION. APPROACH AND LANDING ON 10L WAS NORMAL, ARFF FOLLOWE
- [SDR A6WA2019082046794](https://openairdocs.org/sdr/A6WA2019082046794.md): Warning Message · illuminated · Aug 18, 2019 · N423AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > "RECIEVED FLAP FAIL CAUTION MESSAGE DURING INTIAL CLIMB. FLAPS WERE SET AND INDICATED ZERO" CREW DID NOT DECLARE AN EMERGENCY. AIRCRAFT LANDING WENT WELL THE BTMS WAS READING A LITTLE HIGH. THE BTMS WAS READING "NORMAL" AT 6-8.
- [SDR A6WA2019071046693](https://openairdocs.org/sdr/A6WA2019071046693.md): Floorbeam · corroded · Jul 9, 2019 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL27 FLOORBEAM CAP IS CORRODED BETWEEN FS 589 TO FS 605.
- [SDR A6WA2019062646679](https://openairdocs.org/sdr/A6WA2019062646679.md): Beam · gouged · Jun 26, 2019 · N423AW · Cndair CL6002B19 · Fuselage Main, Structure
  > DAMAGE FOUND ON FWD LOWER PORTION OF CARGO DOOR BEAM THAT REQUIRES FURTHER INSPECTION. CABLE GOUGED INTO BEAM IN TWO PLACES.
- [SDR A6WA2019070346684](https://openairdocs.org/sdr/A6WA2019070346684.md): Door Sill · corroded · Jun 18, 2019 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL IS CORRODED BETWEEN F.S.559+80 TO F.S.559+96.
- [SDR A6WA2019062046670](https://openairdocs.org/sdr/A6WA2019062046670.md): Angle · cracked · Jun 16, 2019 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.S.625 R/H OBLIQUE ANGLE IS CRACKED
- [SDR A6WA2019062146673](https://openairdocs.org/sdr/A6WA2019062146673.md): Bracket · cracked · Jun 13, 2019 · N423AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PRESSURE TRANSDUCER BRACKETG IN LH WHEEL WELL PRESSURE FLOOR AT F.S.529 LBL 22 IS CRACKED.
- [SDR A6WA2019062146672](https://openairdocs.org/sdr/A6WA2019062146672.md): Bracket · cracked · Jun 13, 2019 · N423AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > HYDRAULIC LINE BRACKET IN RH WHEEL WELL PRESSURE FLOOR AT F.S.524 RBL 22 IS CRACKED.
- [SDR A6WA2019070846690](https://openairdocs.org/sdr/A6WA2019070846690.md): Post · cracked · Jun 10, 2019 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATIONS ON FS 409+128 VERTICAL POSTS, BL 0.0, LT & RT AFT FLANGE RADIUS APPROX. 0.50" LONG, 70% & 80% FSH, FAILS NDT.
- [SDR A6WA2019070846689](https://openairdocs.org/sdr/A6WA2019070846689.md): Post · cracked · Jun 10, 2019 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATIONS ON FS 409+128 INBD & OTBD POSTS AT RBL18 AFT FLANGE APPROX. 0.50" LONG, 50% FSH, FAILS NDT.
- [SDR A6WA2019070846688](https://openairdocs.org/sdr/A6WA2019070846688.md): Post · cracked · Jun 10, 2019 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND INDICATION ON FS 409+128 LBL 18 VERTICAL POSTS INBD & OTBD SIDES AFT FLANGE RADIUS APPROX. 0.50" LONG 50% FSH FAILS NDT.
- [SDR A6WA2019062146671](https://openairdocs.org/sdr/A6WA2019062146671.md): Pulley Bracket · cracked · Jun 10, 2019 · N423AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SUPPORT WHEEL PULLEY BRACKET IS CRACKED.
- [SDR A6WA2019060446645](https://openairdocs.org/sdr/A6WA2019060446645.md): Warning System · false activation · May 22, 2019 · N423AW · Cndair CL6002B19 · Engine Oil Indicating System
  > ON INITIAL CLIMB RCVD MULTIPLE INTERMITTENT L ENG OIL PRESS WARNING MSGS. OIL PRESS AND OIL TEMP INDICATONS APPEARED NORMAL. PERFORMED AIR RETURN TO DAY.
- [SDR A6WA2017101145335](https://openairdocs.org/sdr/A6WA2017101145335.md): Generator · failed · Oct 3, 2017 · N423AW · Cndair CL6002B19 · AC Generator-Alternator
  > APU GENERATOR FAILED IN FLIGHT DURING CLIMBOUT, COMPLIED WITH QRH, THE APU GEN WOULD NOT RESET, RETURNED TO DEPARTURE. R & R THE APU GENERATOR IAW AMM 24-22-01, OPS AND LEAK CHECKED GOOD.
- [SDR A6WA201745097](https://openairdocs.org/sdr/A6WA201745097.md): Warning System · activated · Jul 12, 2017 · N423AW · Cndair CL6002B19 · Hydraulic Pressure Indicator
  > RECEIVED HYD 1 LO PRESS CAUTION MSG IN FLIGHT. AC PUMP ON, PRESSURE CONTINUED TO FALL. TURNED OFF ACMP AFTER 1 MINUTE OF OPERATION. DIVERTED TO CLT. EDP OPERATED 1 HOUR. QTY SHOWED DASHES. REPLACED EDP1, HYD LINE AND FITTING, SERVICED AND BLED NR 1 HYD SYS OP
- [SDR A6WA2017060545039](https://openairdocs.org/sdr/A6WA2017060545039.md): Frame · corroded · Jun 3, 2017 · N423AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 349 HAS CORROSION SPOTS ON FWD AND AFT SIDES BETWEEN STRINGERS 26L AND 23R.
- [SDR A6WA2017060545037](https://openairdocs.org/sdr/A6WA2017060545037.md): Skin · corroded · Jun 2, 2017 · N423AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER INBD SKIN SURFACE CORRODED.
- [SDR A6WA2017060145033](https://openairdocs.org/sdr/A6WA2017060145033.md): Floor Support · corroded · May 21, 2017 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT CORRODED BS 310 - 303, RBL 41. REPAIRED IAW SRM 51-21-06, 53-21-43, 51-42-10, 51-42-21.
- [SDR A6WA2017060145031](https://openairdocs.org/sdr/A6WA2017060145031.md): Skin · chafed · May 20, 2017 · N423AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBD FLAP VANE L/E CHAFED ON INBD SIDE. REPLACED THE FLAP VANE IAW SRM 51-42-13.
- [SDR A6WA2017060145032](https://openairdocs.org/sdr/A6WA2017060145032.md): Skin · chafed · May 20, 2017 · N423AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE LEADING EDGE CHAFED AT CENTER. REPLACED THE FLAP VANE IAW SRM 51-42-13.
- [SDR A6WA2017052445023](https://openairdocs.org/sdr/A6WA2017052445023.md): Floorbeam · cracked · May 20, 2017 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM OTBD ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017052445024](https://openairdocs.org/sdr/A6WA2017052445024.md): Floorbeam · cracked · May 20, 2017 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL9 FLOORBEAM ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017052445025](https://openairdocs.org/sdr/A6WA2017052445025.md): Floorbeam · cracked · May 20, 2017 · N423AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > LBL 9 FLOORBEAM OTBD ATTACH ANGLE CRACKED AT BS 280. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21.
- [SDR A6WA2017060745045](https://openairdocs.org/sdr/A6WA2017060745045.md): Intercostal · corroded · May 18, 2017 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED BETWEEN BS 349 TO 364, STRINGER 25R. REPLACED THE INTERCOSTAL IAW EA CRJ253-00687 REV-IR.
- [SDR A6WA2017060745038](https://openairdocs.org/sdr/A6WA2017060745038.md): Floor Support · corroded · May 18, 2017 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED FROM BS 589 TO 621, LBL 27. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-21 AND REO 601R-53-61-3778 REV-A.
- [SDR A6WA201744914](https://openairdocs.org/sdr/A6WA201744914.md): Strut · discharged · Apr 9, 2017 · N423AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > NOSE WHEEL STEERING INOPERATUVE CAUTION MESSAGE INFLIGHT. COMPLIED WITH QRH, MESSAGE REMAINED. DURING CLIMB AT APROX FL 21, NWS WAS ARMED MESSAGE CAME ON AFTER SELECTING OFF MESSAGE WENT OUT. R & R THE TILLER IAW AMM 32-51-01, NO FIX, SERVICED NLG SHOCK S
- [SDR A6WA201644414](https://openairdocs.org/sdr/A6WA201644414.md): Warning Message · false activation · Oct 8, 2016 · N423AW · Cndair CL6002B19 · Overheat Detection
  > ENROUTE, RECIEVED MLG BAY OVERHEAT WARNING MESSAGE, COMPLIED WITH THE QRH. BTMS INDICATIONS WERE ALL AT 1. LANDED WITHOUT INCIDENT
- [SDR A6WA201644349](https://openairdocs.org/sdr/A6WA201644349.md): Service Door · sticks · Sep 20, 2016 · N423AW · Cndair CL6002B19 · Passenger/Crew Doors
  > SERVICE DOOR IS HARD TO OPEN FROM INSIDE AND OUTSIDE. HANDLE OPERATES NORMALLY, DOOR HARD TO PULL FROM AIRFRAME.

Next page: https://openairdocs.org/aircraft/N423AW/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 = 'N423AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N423AW/reports

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