# Service difficulty reports: N420AW

A list on [N420AW](https://openairdocs.org/aircraft/N420AW.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 · 222 reports

- [SDR A6WA202609028910](https://openairdocs.org/sdr/A6WA202609028910.md): Heat Exchanger · faulted · Sep 2, 2026 · N420AW · Cndair CL6002B19 · Engine Oil Cooler
  > DURING CLIMB NR 2 ENG OIL TEMP REACHED 150'C. C/W QRH -PULLED PWR BACK AND REDUCED PWR. ENG OIL TEMP RETURNED TO NORMAL OPERATING RANGE. NR 2 ENG OIL TEMP CONSTANTLY 20' HOTTER THAN NR 1. MC- ON GRD @ IDLE READS 10-15' HOTTER THAN NR 1. AIRCRAFT REMOVED FROM
- [SDR A6WA202607298904](https://openairdocs.org/sdr/A6WA202607298904.md): Seat Track · gouged · Jul 29, 2026 · N420AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PAX CABIN SEAT RAIL RT SIDE DEEP GOUGE AT FS559 APROX. REMOVED RT SEAT TRACK LOCATED, DRILLED, AND INSTALLED IAW SRM 51-41-00, 51-40-11 AND AMM 53-01-11.
- [SDR A6WA202607288903](https://openairdocs.org/sdr/A6WA202607288903.md): Seat Track · corroded · Jul 28, 2026 · N420AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > PAX CABIN LT SEAT TRACK BS 559 - 559+32) DEEP GOUGE DAMAGE AREA/CORRODED REMOVED LT SEAT TRACK LOCATED, DRILLED AND INSTALLED IAW SRM 51-41-00, 51-40-11 AND AMM 53-01-11.
- [SDR A6WA202411058841](https://openairdocs.org/sdr/A6WA202411058841.md): Elec Connector · loose · Nov 4, 2024 · N420AW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER ADDING TAKEOFF THRUST AND RELEASING BRAKES AIRCRAFT PULLED VERY HARD TO THE LEFT, ABORTED TAKE OFF. TAXIED OFF RUNWAY NO ISSUES AT NORMAL TAXI SPEED. BRAKE TEMPS NORMAL NO ABNORMAL MESSAGES AND NWS OPERATED NORMALLY. ALL OTHER INDICATIONS NORMAL. AIRC
- [SDR A6WA202410268838](https://openairdocs.org/sdr/A6WA202410268838.md): Control Lever · faulted · Oct 26, 2024 · N420AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION MSG AT 20* FLAPS ON APPROACH. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. ACARS: A/C FLT DEP DST TIME ALT N420AW 6068 LEX PHL 1642Z 1756 STATE MINS IAS OAT FLAPS FAIL
- [SDR A6WA202408278795](https://openairdocs.org/sdr/A6WA202408278795.md): Rudder Control · faulted · Aug 23, 2024 · N420AW · Cndair CL6002B19 · Rudder Control System
  > ABORTED TAKE OF DUE TO LACK OF RUDDER RESPONSE LESS THAN 60 KTS FO'S LEG. PRESSURIZED ALL 3 HYD SYSTEMS, VISUALLY VERIFIED FULL DEFLECTION OF RUDDER TRAVEL FROM BOTH CA AND FO RUDDER PEDALS. EICAS INDICATION AGREES. AIRCRAFT REMOVED FROM SERVICE. PERFORME
- [SDR A6WA202401158699](https://openairdocs.org/sdr/A6WA202401158699.md): Bracket · damaged · Jan 15, 2024 · N420AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGRE ON WARNING NLG DOWN MLG UP C/W QRH MANUAL EXT GEAR DOWN ALL AND LOCKED NORMAL LANDING. 6 SEC AND MANUL RELEASE WAS USED. HYD WAS IN AUTO. EMERGENCY DECLARED, 180 KNTS SPEED. NO OVERWEIGHT LDG. AIRCRAFT REMOVED FROM SERVICE. R/R NOSE LANDING GEAR
- [SDR A6WA202310198659](https://openairdocs.org/sdr/A6WA202310198659.md): Bpsu · unknown · Oct 18, 2023 · N420AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > IN CRUISE, RECEIVED FLAPS FAIL CAUTION. BTMS INDICATIONS DID NOT EXCEED 10. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUP 98-018I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. FLAPS FAILED AGAIN APPROX 5 MINUTES AFTER RESET. AIRCRAFT REMOVED FROM SERVICE.
- [SDR A6WA202306168631](https://openairdocs.org/sdr/A6WA202306168631.md): Unknown · unknown · Jun 16, 2023 · N420AW · Cndair CL6002B19 · Landing Gear System
  > ON DEPARTURE RECIEVED STEERING INOP CAUTION FOLLOWED BY WOW INPUT CAUTION AND WOW OUT PUT FAIL STATUS MSGS. RAN QRH. CYCLED NWS, MSG PERSISTED. WHEN EXTENDING GEAR ALL MSGS CLEARED. AIRCRAFT REMOVED FROM SERVICE. C/W FAULT ISOLATION OF STERING INOP MSG REF C
- [SDR A6WA202304298588](https://openairdocs.org/sdr/A6WA202304298588.md): Frame · damaged · Apr 29, 2023 · N420AW · Cndair CL6002B19 · Fuselage Main, Frame
  > SKIN DIMPLED AROUND 4 RIVETS ON FRAME FS379.00 BETWEEN STGR23LL AND STGR22L ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME AT FS 379 BETWEEN STRG23L AND STRG22L REF REO 601R-53-21-3628 REV -- DATED 2023-04-21
- [SDR A6WA2023005019589](https://openairdocs.org/sdr/A6WA2023005019589.md): Former · corroded · Apr 29, 2023 · N420AW · Cndair CL6002B19 · Emergency Exits
  > CORROSION FOUND ON PAX DOOR FORMER AT FS320.00 FROM DD5-UPPER FORMER AT HINGE. ***** AC REMOVED FROM SERVICE ***** INSTALL FORMER AT FS 320.00 BETWEEN DD5 DATUM AND UPPER FORMER AT HINGE REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV: -N
- [SDR A6WA202304288586](https://openairdocs.org/sdr/A6WA202304288586.md): Floor Support · corroded · Apr 28, 2023 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION. ***** AC HAS BEEN REMOVED FROM SERVICE ***** REPAIRED L/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS 559 REF REO 601R-53-41-666 REV -- DATED 27-MAY-2008 AND REO 601R-5
- [SDR A6WA202304288587](https://openairdocs.org/sdr/A6WA202304288587.md): Frame · corroded · Apr 28, 2023 · N420AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 319 HAS CORROSION REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R32003 REV P ***** AC REMOVED FROM SERVICE ***** REPLACE FRAME AT FS 319 REF
- [SDR A6WA202304278585](https://openairdocs.org/sdr/A6WA202304278585.md): Intercostal · corroded · Apr 27, 2023 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR21L BETWEEN FS349-FS333 HAS CORROSION ***** AC REMOVED FROM SERVICE ***** INSTALLED NEW INTERCOSTAL FROM STGR 21 LH BETWEEN FS 333.00 AND FS 349.0 REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31527 REV AM
- [SDR A6WA202304228579](https://openairdocs.org/sdr/A6WA202304228579.md): Pressure Deck · corroded · Apr 22, 2023 · N420AW · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H PRESSURE FLOOR SILL PANEL FROM FS409+128 TO FS559 HAS MULTIPLE AREAS OF CORROSION ***** AC REMOVED FROM SERVICE ***** REPAIRE R/H PRESSURE FLOOR SILL REF REO 601R-53-41-3149 REV A DATED 2023-04-14
- [SDR A6WA202304218577](https://openairdocs.org/sdr/A6WA202304218577.md): Frame · damaged · Apr 21, 2023 · N420AW · Cndair CL6002B19 · Fuselage Main, Frame
  > REMOVE EXISTING REPAIR TO COMPLY WITH PERMANENT REPAIR AT THE REQUEST OF THE CUSTOMER ***** AC REMOVED FROM SERVICE ***** REPAIRED FRAME SECTION AT FS276 REF REO 601R-53-11-3859 REV -- DATED 2023-04-19
- [SDR A6WA202304208575](https://openairdocs.org/sdr/A6WA202304208575.md): Frame · corroded · Apr 20, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION ON FRAME FS364.00 AND STRG23L ***** AC REMOVED FROM SERVICE ***** REPLACED FRAME SECTION REF REO 601R-53-21-3626 REV -- DATED 2023-04-19
- [SDR A6WA202304158560](https://openairdocs.org/sdr/A6WA202304158560.md): Intercostal · corroded · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD4 BETWEEN FS 338.00 FS349.00 *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED A NEW PAX DOOR INTERCOSTAL FS338.00-FS349.00. REF DWG 601R31702 REV-N AND CRJ 200 SRM 51-42-06
- [SDR A6WA202304158558](https://openairdocs.org/sdr/A6WA202304158558.md): Cleat · corroded · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION FOUND ON PAX DOOR CLEAT AT FS313.56 DD4. *****AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW CLEAT AT FS 313.56 DD4 REF CRJ-200-SRM 51-42-06 AND DRAWING 601R31702 REV N
- [SDR A6WA202304158561](https://openairdocs.org/sdr/A6WA202304158561.md): Former · corroded · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > PAX DOOR FWD FORMER HAS CORROSION BETWEEN DD6-DD5 *********AIRCRAFT REMOVED FROM SERVICE******* REPLACED NEW PAX DOOR FWD FORMER REF DRAWING 601R31702 REV N
- [SDR A6WA202304158552](https://openairdocs.org/sdr/A6WA202304158552.md): Flap · damaged · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Trailing Edge Flaps
  > PERFORM PERMANENT REPAIR FOR LH INBOARD FLAP INNER DOUBLER. ********AIRCRAFT REMOVED FROM SERVICE******* REPAIRED L/H INBOARD FLAP UPPER SKIN REF REO 601R-57-52-2482 REV -- DATED 2023-04-12
- [SDR A6WA202304158555](https://openairdocs.org/sdr/A6WA202304158555.md): Frame · corroded · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FRAME AT FS 333 HAS CORROSION STGR23L-25R ********AIRCRAFT REMOVED FROM SERVICE******** REPLACED FRAME AT FS333 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21, AND DRAWING 601R32004 REV M
- [SDR A6WA202304158557](https://openairdocs.org/sdr/A6WA202304158557.md): Cleat · corroded · Apr 15, 2023 · N420AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON PAX DOOR CLEAT AT FS338.00 AND UPPER FORMER AT HINGE *********AIRCRAFT REMOVED FROM SERVICE******* INSTALLED NEW PAX DOOR CLEAT AT FS338.00 REF DWG 601R31702 REV-N CRJ 200 SRM 51-42-10
- [SDR A6WA202304128547](https://openairdocs.org/sdr/A6WA202304128547.md): Floor Skin · dented · Apr 12, 2023 · N420AW · Cndair CL6002B19 · Fuselage, Door Hinge
  > PRESSURE FLOOR SKIN HAS 2EA DENTS BETWEEN LBL 9-BL0 FS499 *******AIRCRAFT REMOVED FROM SERVICE***** REPAIRED PRESSURE FLOOR SKIN REF REO 601R-53-41-3147 REV -- DATED 2023-04-07
- [SDR A6WA202304088545](https://openairdocs.org/sdr/A6WA202304088545.md): Former · corroded · Apr 8, 2023 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR AFT FORMER HAS CORROSION BETWEEN DD6-DD5 ***** AC REMOVED FROM SERVICE ***** REPLACED AFT PAX DOOR FORMER REF DWG 601R31702 REV N
- [SDR A6WA202304088544](https://openairdocs.org/sdr/A6WA202304088544.md): Hinge · unknown · Apr 8, 2023 · N420AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > "Ï¿½PASSENGER DOOR HINGE ON FUSELAGE LUGS FAILED THE CHECK WITH THE NO/GO GAUGE ***** AC REMOVED FROM SERVICE ***** REPLACED PAX DOOR HINGE,BOMBARDIER DWG 601R31527 REV AM AND REO 601R-53-21-656 REV A DATED 2017/03/06"
- [SDR A6WA202304078541](https://openairdocs.org/sdr/A6WA202304078541.md): Frame · corroded · Apr 7, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FRAME AT FS 310 HAS CORROSION STRG26L-26R. AC REMOVED FROM SERVICE. INSTALLED NEW LOWER FRAME SECTOR TO THE LOWER SKIN @ FS310 REF CRJ-200 SRM 51-42-06 AND DWG 601R32002 REV.AC.
- [SDR A6WA202304078538](https://openairdocs.org/sdr/A6WA202304078538.md): Intercostal · corroded · Apr 7, 2023 · N420AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD6 BETWEEN FS 320-FS 338.00 *******AIRCRAFT REMOVED FROM SERVICE******** REPLACE INTERCOSTAL ON PAX DOOR DD6 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21
- [SDR A6WA202304078537](https://openairdocs.org/sdr/A6WA202304078537.md): Bracket · cracked · Apr 7, 2023 · N420AW · Cndair CL6002B19 · Doors
  > FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE CRACKED. *******AIRCRAFT REMOVED FROM SERVICE****** REPLACED FWD CARGO DOOR BOX SPRING FRAME SUPPORT STRUCTURE BRACKET REF SRM 51-42-06
- [SDR A6WA202304068536](https://openairdocs.org/sdr/A6WA202304068536.md): Intercostal · corroded · Apr 6, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 ******AIRCRAFT REMOVED FROM SERVICE******** REPLACED PAX DOOR INTERCOSTAL AT DD5 BETWEEN FS 338.00 TO FS 349.00 REF DWG 601R31702 REV-N
- [SDR A6WA202304018529](https://openairdocs.org/sdr/A6WA202304018529.md): Unknown · cracked · Apr 1, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FS484.00 BETWEEN RBL 27-36, FLIGHT CONTROL CABLE ROLLER GUIDE ASSY, INBOARD ATTACH ANGLE CRACKED(MARKED) *****AIRCRAFT REMOVED FROM SERVICE*********** REPLACED CLIP REF SRM51-42-21 AND DWRG 601R31171 REV - E
- [SDR A6WA202304018528](https://openairdocs.org/sdr/A6WA202304018528.md): Unknown · cracked · Apr 1, 2023 · N420AW · Cndair CL6002B19 · Fuselage Structure (General)
  > FS 484.00 BETWEEN LBL 27-36 FLIGHT CONTROL CABLE ROLLER GUIDE ASSY,INBOARD ATTACH ANGLE ********AIRCRAFT REMOVED FROM SERVICE******* REPLACE CLIP 484 CLIP REF DRAWING 601R31171 REV E, AND CRJ-200 SRM 51-42-21
- [SDR 2022FA0000081](https://openairdocs.org/sdr/2022FA0000081.md): Fms · abnormal · Feb 10, 2022 · N420AW · Cndair CL6002B19 · Navigation System
  > COLLINS 4200 FMS. KEYS ON KEYBOARD ARE WORE OUT AND WHEN YOU TYPE THE KEYS REPEATS THE SAME NUMBER OR LETTER, 2 TO 3 TIMES. COMPANY REFUSES TO FIX THEM. IMO THIS IS A SAFETY OF FLIGHT ISSUE. ALL AIRCRAFT IN FLEET HAVE THIS PROBLEM. 405-471AW
- [SDR A6WA202112017999](https://openairdocs.org/sdr/A6WA202112017999.md): None · none · Nov 30, 2021 · N420AW · Cndair CL6002B19 · Engine Oil Cooler
  > ON TAKE-OFF REC'D RT ENG OIL WARNING MESSAGE. MESSAGE WAS INTERMITTENT. OIL PSI FLUCTUATED BETWEEN 25 AND 35 PSI. OIL TEMP WAS NORMAL. MESSAGE WAS LESS INTERMITTENT WITH REDUCED POWER. EVENT DESCRIPTION: EN ROUTE, THE #2 ENGINE OIL PRESSURE BEGAN TO
- [SDR A6WA202111227984](https://openairdocs.org/sdr/A6WA202111227984.md): None · none · Nov 18, 2021 · N420AW · Cndair CL6002B19 · Ice/Rain Protection System
  > 3885 RT WING A-ICE CAUTION MSG USING STANDBY. EN ROUTE, THE FLIGHT EXPERIENCED A RIGHT WING ANTI ICE CAUTION MESSAGE. IN THE INTEREST OF SAFETY, TO AVOID ICING CONDITIONS, THE CREW AND DISPATCHER HAVE AGREED TO DIVERT TO DAY. NO EMERGENCY DECLARED AND THE FL
- [SDR A6WA202107067813](https://openairdocs.org/sdr/A6WA202107067813.md): Seat Track · corroded · Jul 5, 2021 · N420AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE RAIL BETWEEN FS 449 TO 499 IS OUT OF LIMITS DUE TO HEAVY CORROSION. REMOVED AND REPLACED LH SIDE RAIL
- [SDR A6WA202102127627](https://openairdocs.org/sdr/A6WA202102127627.md): Windshield · cracked · Feb 10, 2021 · N420AW · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT WINDSHIELD CRACKED IN FLIGHT DURING CLIMB OUT. AIR RETURN TO IAD. AIRCRAFT REMOVED FROM SERVICE. R & R CA WINDSHIELD PER AMM 56-11-01 SEE LP 307033/1 FOR SEALANT CURE CHECK AND 307033/2 FOR OPS CHECK/LEAK CHECK OF WINDSHIELD HEAT P/N OFF:NP139321-13,S
- [SDR A6WA202101297571](https://openairdocs.org/sdr/A6WA202101297571.md): Windshield · cracked · Jan 27, 2021 · N420AW · Cndair CL6002B19 · Flight Compartment Windows
  > EVENT DESCRIPTION: CREW REPORTED CRACKED WINDSHIELD EN ROUTE TO MKE. FLIGHT DIVERTED TO DAY AND DECLARED AN EMERGENCY. FLIGHT IS A REPOSITION WITH ZW MECHANICS ON BOARD, REF 307026/4: AT FLT 300 OBSERVED ARCING ON F/O' WINDSCREEN TURNED F/O WINDSHIELD HEAT O
- [SDR A6WA202101257568](https://openairdocs.org/sdr/A6WA202101257568.md): Wire Harness · damaged · Jan 24, 2021 · N420AW · Cndair CL6002B19 · Landing Gear System Wiring
  > STEERING INOPERABLE MESSAGE AT CRUISE FL 290. CW QRH MESSAGE PERSISTED, AFTER SELECTING GEAR DOWN CYCLED STEERING OFF ON MESSAGE RETURNED. EMERGENCY DECLARED. CYCLED SW AGAIN AT 500 FT MESSAGE CLEARED. STEERING APPEARED NORM AFTER LANDING. TAXI TO GATE UN
- [SDR A6WA202101057514](https://openairdocs.org/sdr/A6WA202101057514.md): Warning Message · false activation · Jan 4, 2021 · N420AW · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > RECEIVED R AOA HEAT CAUTION MESSAGE IN-FLIGHT. C/W QRH MESSAGE PERSISTED. AIRCRAFT REMOVED FROM SERVICE. C/W FIM RESET MESSAGE CLEARED.
- [SDR A6WA2020082537282](https://openairdocs.org/sdr/A6WA2020082537282.md): Warning Message · illuminated · Aug 23, 2020 · N420AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL CAUTION MESSAGE DURING CRUISE AT 280 KNOTS, C/W QRH. DECLARED EMERGENCY AND SELECTED LONGEST RUNWAY. AIRCRAFT REMOVED FROM SERVICE. RESET AND PLACED ON MEL FOR 10 CYCLES.
- [SDR A6WA2020082537283](https://openairdocs.org/sdr/A6WA2020082537283.md): Bpsu · malfunctioned · Aug 23, 2020 · N420AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP WERE MEL'D AT ORD AND RESET. EN ROUTE TO CID THEY FAILED AGAIN. FLIGHT WILL CONTINUE TO CID. THE CAPTAIN INDICATED THAT DURING DESCENT TO KCID THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, ADVISE
- [SDR A6WA2019090946858](https://openairdocs.org/sdr/A6WA2019090946858.md): Warning System · false activation · Sep 6, 2019 · N420AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > UPON GEAR EXTENSION RECIVED GEAR DISAGREE NOSE SHOWED UNSAFE PERFORMED EMERGENCY GEAR EXTENSION PER QRH. MESSAGE OCCURED 6 SECONDS AFTER SELECTION, NO OTHER ASSOSIATED EICAS MESSAGES.
- [SDR A6WA2019071046694](https://openairdocs.org/sdr/A6WA2019071046694.md): Skin · dented · Jul 9, 2019 · N420AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AIRCRAFT SKIN HAS TWO PROTRUDING DENTS BETWEEN FS 621-640 AND IN BETWEEN STRINGERS 25L AND 26L. REPAIRED SKIN BETWEEN FS 621-640 BETWEEN STRINGER 25L AND 26L IAW EA# AWAC-CRJ253-01271.
- [SDR A6WA2019062846682](https://openairdocs.org/sdr/A6WA2019062846682.md): Skin · cracked · Jun 18, 2019 · N420AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > CORE COWL 435AT UPPER SKIN AFT I/B CORNER CRACKED. REPAIRED CORE COWL IAW CMM71-12-01.
- [SDR A6WA2019062646678](https://openairdocs.org/sdr/A6WA2019062646678.md): Bracket · cracked · Jun 18, 2019 · N420AW · Cndair CL6002B19 · Wing, Attach Fittings
  > BRACKET BETWEEN TH INBD LE AND CENTER LE CRACKED. REPLACED
- [SDR A6WA2019061846666](https://openairdocs.org/sdr/A6WA2019061846666.md): Beam · gouged · Jun 16, 2019 · N420AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR BEAM GROOVED AT AFT END OF BEAM DUE TO CARGO DOOR SPRING CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW CRJ200 SRM 51-42-06, 51-42-21.
- [SDR A6WA2019061846667](https://openairdocs.org/sdr/A6WA2019061846667.md): Cleat · corroded · Jun 16, 2019 · N420AW · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > PAX DOOR AFT LOWER CLEAT CORRODED. REPLACED CLEAT IAW CRJ 200 SRM 51-42-06, 51-42-10, 51-42-12.
- [SDR A6WA2019061846668](https://openairdocs.org/sdr/A6WA2019061846668.md): Cleat · corroded · Jun 16, 2019 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > PAX DOOR LOWER SILL FWD CLEAT CORRODED. REPLACED CLEAT IAW CRJ200 SRM 51-42-06, 51-42-10, 51-42-12.
- [SDR A6WA2019062646677](https://openairdocs.org/sdr/A6WA2019062646677.md): Vane · chafed · Jun 14, 2019 · N420AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP VANE MIDDLE LE CHAFED. REPLACED.

Next page: https://openairdocs.org/aircraft/N420AW/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 = 'N420AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N420AW/reports

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