# Service difficulty reports: N443AW

A list on [N443AW](https://openairdocs.org/aircraft/N443AW.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 · 182 reports

- [SDR A6WA202206098191](https://openairdocs.org/sdr/A6WA202206098191.md): Steering Sys · warning message · Jun 9, 2022 · N443AW · Cndair CL6002B19 · Steering Unit
  > STEERING INOP CAUT MSG ABOUT 15 MIN AFTER TO. C/W QRH MSG RETURNED AFTER STEERING SWITCH RESET. ATTEMPTED MULTIPLE CYCLES OF STEERING SWITCH NO FIX. AFTER CONFIGURING A/C FOR LANDING CYCLED STEERING SWITCH TO ON CAUT MSG REMAINED CLEARED LANDED WITH NORMAL STE
- [SDR A6WA202205178182](https://openairdocs.org/sdr/A6WA202205178182.md): Bonding Plate · corroded · May 17, 2022 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/Skin
  > RH ENGINE PYLON, TOP SIDE, OUTBOARD BONDING PLATE HAS CORROSION. REMOVE AND REPLACED BONDING PLATE ON RH AFT PYLON TOPSIDE, BONDING CHECK GOOD. PRIMED AND TOP COAT. IAW CRJ-200 SRM 51-45-15, AMM 51-80-00-760-803, SRM 51-25-06, AND 51-25-16 SUPP 15-335 ***AIRC
- [SDR A6WA202205178183](https://openairdocs.org/sdr/A6WA202205178183.md): Frame · corroded · May 17, 2022 · N443AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS605.00 AFT SIDE OF FRAME FROM STR27 TO 23R HAS EVIDENCE OF CORROSION FURTHER CLEANING AND EVALUATION IS REQUIRED CLEANED AND REMOVED FRAME PN 601R36026-27S AT FS605, REPLACED FRAME AT FS605 IAW CRJ-200 SRM 51-26-00, 51-42-21, 51-42-06, AND 51-40-11 ****AIRCR
- [SDR A6WA202203188133](https://openairdocs.org/sdr/A6WA202203188133.md): None · none · Mar 18, 2022 · N443AW · Cndair CL6002B19 · Flight Control System
  > LOST RUDDER TRIM IN FLIGHT. RUDDER TRIM FULL DEFLECTION NL. RUDDER TRIM SWITCH WILL NOT MOVE NR. A/C CONTROLLABLE WITH RH RUDDER INPUT. DIVERTED TO BUF, SMOOTH LANDING AT 47,100LBS ***AIRCRAFT REMOVED FROM SERVICE*** R&R AILERON/RDR TRIM PANEL IAW AMM 27
- [SDR A6WA202107287843](https://openairdocs.org/sdr/A6WA202107287843.md): Power Supply · inoperative · Jul 28, 2021 · N443AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAPS FAIL AT ZERO DEGREES ON APROACH WHEN SELECTED FROM 0 TO 8, FLAPS DID NOT MOVE. LANDING WEIGHT APROX 45000 LBS, SMOOTH UNEVENTFUL LANDING, MAX BTMS 7556. AIRCRAFT REMOVED FROM SERVICE. REF WO 307503 MX WC 2-19 FOR TBS AND CORRECTIVES (LH AND RH B
- [SDR A6WA202107277840](https://openairdocs.org/sdr/A6WA202107277840.md): Flap System · failed · Jul 25, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > REF 347659-2 AFTER TAKEOFF, REC FLAP FAIL CAUTION MSG DURING FLAP RETRACTION FROM FLAPS 8 TO FLAPS 0. CW AWA SUP 98-018I RESET FAILED WHEN MOVING HANDLE FROM 8 TO 0 TO BEGIN 5 FLAP CYCLES ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS
- [SDR A6WA202107207831](https://openairdocs.org/sdr/A6WA202107207831.md): Flap System · malfunctioned · Jul 17, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING APPROACH AND FLAPS SET TO ZERO, RECIEVED A FLAPS FAIL CAUTION. 44 PASSENGERS, FO WAS FLYING, NO OBSERVERS. CAPTAIN STATED DURING DEBRIEF THAT IT WAS A NORMAL ILS APPROACH AT 10 CENTER AND 210 KIAS. LOWERED GEAR AT 200 KIAS. CAPTURED GLIDESLOPE AT 17
- [SDR A6WA202107207832](https://openairdocs.org/sdr/A6WA202107207832.md): Flap System · malfunctioned · Jul 17, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT 0, FLAPS ALREADY ON MEL, FN 3917 EMERGENCY DECLARED BY CREW. AS THEY TURNED ONTO AN EXTENDED FINAL INTO ORD, FO FLYING, WENT UNDER 180, SELECTED FLAPS TO 8 & RECEIVED A FLAP MASTER CAUTION, FLAPS NEVER MOVED OUT OF 0. RAN QRH & DECLARED EMERGENC
- [SDR A6WA202107157827](https://openairdocs.org/sdr/A6WA202107157827.md): Control Unit · malfunctioned · Jul 15, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING THE APPROACH TO KORD, THE FLIGHT CREW EXPERIENCED A FLAP FAILURE AND DISCONTINUED THE APPROACH. THE CREW COMPLETED REQUIRED CHECKLISTS, DECLARED AN EMERGENCY WITH ATC, COMMUNICATED WITH THE FLIGHT ATTENDANT, PASSENGERS AND DISPATCH THEN RETURNED AND LAN
- [SDR A6WA202106077798](https://openairdocs.org/sdr/A6WA202106077798.md): Flap System · stuck · Jun 6, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AFTER SELECTING FLAPS ZERO AFTER TAKEOFF, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS STUCK AT 3 DEG LEFT & 4 DEG RIGHT. IAS AT TIME OF FLAP FAIL WAS 200 KTS, OAT OF 27 DEG C, & TIME NOTED IN AIR WAS 1 MINUTE. (BLOCK 2) PERFORMED FLAP RESET PROCEDURE IAW SUPP 9
- [SDR A6WA202106047794](https://openairdocs.org/sdr/A6WA202106047794.md): Bpsu · failed · Jun 4, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AT FL 300 AND MACH. FLAPS FAILED AT ZERO. AIRCRAFT REMOVED FROM SERVICE. LEFT BPSU REPLACED, OPS CHECK GOOD.
- [SDR A6WA202106047793](https://openairdocs.org/sdr/A6WA202106047793.md): Bpsu · failed · Jun 3, 2021 · N443AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FL 240 RECEIVED FLAPS FAIL CAUTION MSG C/W QRH FLAPS FAILED AT 0 DEGREES. DECLARED AN EMERGENCY AND LANDED WITH NO ISSUES IN IAD. C/W FIM RESET IAW AWAC SUP 98-18I BOX 12 FLAP RESET, AND PLACED ON MEL AIRCRAFT REMOVED FROM SERVICE. R&R LFT BPSU IAW AM
- [SDR A6WA2020032647244](https://openairdocs.org/sdr/A6WA2020032647244.md): Skin · dented · Mar 14, 2020 · N443AW · Cndair CL6002B19 · Wing, Plate/Skin
  > PERFORM PERMANENT REPAIR TO R/H L/E BETWEEN WS 226 TO WS 242 THAT MEASURES 2.0"L X 2.5" W X.037"D. "AIRCRAFT REMOVED FROM SERVICE" DENT AT WS 242 REFORMED TO ORIGINAL CONTOUR AND HFEC WITH NO CRACK INDICATIONS. REF ASAP EA# AWAC-CRJ257-01476 REV IR DTD 03/
- [SDR A6WA2020032547237](https://openairdocs.org/sdr/A6WA2020032547237.md): Doubler · corroded · Mar 6, 2020 · N443AW · Cndair CL6002B19 · Passenger Compartment Equipment
  > SUPPLEMENTAL, CLOSET ASSY HAS CORROSION ON LWR SILL BY MOUNT POINT. AIRCRAFT REMOVED FROM SERVICE. MANUFACTURED PART ITEMS 55 & 75 AND REPLACED ITEMS 35 AND 65. REF ASAP EA AWAC-CRJ225-01480 REV IR DTD 3/21/20.
- [SDR A6WA2020032547240](https://openairdocs.org/sdr/A6WA2020032547240.md): Cable · frayed · Mar 6, 2020 · N443AW · Cndair CL6002B19 · Passenger/Crew Doors
  > L1 DOOR MAIN PAX DOOR POWER ASSIST CABLE IS FRAYED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED L1 MAIN PAX DOOR POWER ASSIST CABLE REF CRJ-200 AMM 52-11-00
- [SDR A6WA2020032647242](https://openairdocs.org/sdr/A6WA2020032647242.md): Vane · cracked · Mar 4, 2020 · N443AW · Cndair CL6002B19 · Engine Thrust Reverser
  > #2 ENGINE THRUST REVERSER CASCADE AT 12 O'CLOCK POSITION HAS A CRACKED VANE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED 12 O'CLOCK POS CASCADE ON #2 ENG REF CRJ 299 AMM 78-33-01. REV 60
- [SDR A6WA2020032647243](https://openairdocs.org/sdr/A6WA2020032647243.md): Skin · dented · Mar 4, 2020 · N443AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > PERFORM REPAIR TO L/H FUSELAGE SKIN BETWEEN FRAMES FS 544 TO FS 559 & S9L TO S10L FOR 1-OFF DENT THAT MEASURES 2.4"L X.5"W X.128"D. "AIRCRAFT REMOVED FROM SERVICE" CUTOUT DAMAGED AREA. HFEC PERFORMED AROUND CUTOUT. REPAIR DOUBLER FABRICATED FROM 2024-T3
- [SDR A6WA202002147179](https://openairdocs.org/sdr/A6WA202002147179.md): Bracket · damaged · Feb 13, 2020 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > AFTER T/O SELECTED GEAR UP GOT GEAR DISAGREE AND NOSE DOOR OPEN (W) MS GS AND NOSE GEAR WOULD NOT RETRACT. RAN QRH FOR NOSE DOOR OPEN ALL (W) MSGS DISAPPEARED AIRCRAFT REMOVED FROM SERVICE INSPECTED NLG DOORS, NO DEFECTS NOTED,
- [SDR A6WA2019112147021](https://openairdocs.org/sdr/A6WA2019112147021.md): Bpsu · malfunctioned · Nov 16, 2019 · N443AW · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > SHORTLY AFTER DEPARTURE, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO KORD WITHOUT FURTHER INCIDENT. FLAPS FAIL CAS MSG MOVING FLAP LEVERS FROM 8 TO 0 AFTER TAKE OFF PERFROMED FLAP FAIL RESET PROCEDURES I
- [SDR A6WA2019110546972](https://openairdocs.org/sdr/A6WA2019110546972.md): Pitot Line · contaminated · Nov 2, 2019 · N443AW · Cndair CL6002B19 · Pitot/Static System
  > DURING CLIMB OUT IN MODERATE ICING RECEIVED IAS AND ALT YELLOW BOX MSG"S ON BOTH PFD'S AND OTHER ASSOCIATED MSG'S. NO PITOT OR STATIC HEAT FAILURES. COULD NOT ISOLATE EITHER ADC, BOTH APPEARED INOP. RECEIVED ADC TEMP DISAGREE CAUTION AFTER 10 MIN. ALL MSG'S CL
- [SDR A6WA2019020846371](https://openairdocs.org/sdr/A6WA2019020846371.md): Windshield · cracked · Feb 6, 2019 · N443AW · Cndair CL6002B19 · Flight Compartment Windows
  > LEFT WINDSHIELD ARCED AT FL 280 CW QRH. APPEARS TO BE CRACKED. LH WINDSCREEN MIDDLE PANE IS CRACKED ALMOST FULL WIDTH
- [SDR A6WA2018101246109](https://openairdocs.org/sdr/A6WA2018101246109.md): Warning System · activated · Oct 10, 2018 · N443AW · Cndair CL6002B19 · Hydraulic Pressure Indicator
  > OUT OF 15,000FT IN DECENT RECEIVED DYD 1 LO PRESS CAUTION C/W QRH PROBLEM DID NOT RESOLVE. PRESSURE WENT FROM 1800PSI TO 500PSI IN 2 MINUTES. TURNED ACMP OFF, PUMP RAN FOR APPROX 3 MINUTES. EDP RAN FOR APPROX 15 MINUTES AT LO PRESS.
- [SDR A6WA201846019](https://openairdocs.org/sdr/A6WA201846019.md): Warning Message · illuminated · Aug 30, 2018 · N443AW · Cndair CL6002B19 · Cabin Cooling System
  > 4826 WHILE TRANSFERING BLEEDS TO THE ENGINES AFTER T/O CHECKLIST RECEIV ED LH PACK HI PRESSURE CAUTION MSG. CW QRH PROCEEDURE. MSG REMAINED. ON CLIMB WITH LG ENGINE AT BELOW 60% N1 RECEIVED LH PACK OVERPRESSURERE DUCED LH ENGINE TO 57% N1 AND CYCLED PACK SW.
- [SDR A6WA2018042445778](https://openairdocs.org/sdr/A6WA2018042445778.md): Latch · cracked · Apr 18, 2018 · N443AW · Cndair CL6002B19 · Doors
  > LEFT LRU DOOR AFT LATCH STRUCTURE IS CRACKED.
- [SDR A6WA2018042445779](https://openairdocs.org/sdr/A6WA2018042445779.md): Bulkhead · cracked · Apr 18, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR TRACK AT UPPER END IS CRACKED.
- [SDR A6WA201845775](https://openairdocs.org/sdr/A6WA201845775.md): Fitting · cracked · Apr 16, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BATH TUB FITTING AT BS 461, OTBD SIDE OF LBL 9 IS CRACKED.
- [SDR A6WA201845774](https://openairdocs.org/sdr/A6WA201845774.md): Hinge · cracked · Apr 14, 2018 · N443AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER FOLDING STEP HINGE CRACKED.
- [SDR A6WA2018041645773](https://openairdocs.org/sdr/A6WA2018041645773.md): Drag Angle · cracked · Apr 14, 2018 · N443AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAD A CRACKED AFT DRAG ANGLE.
- [SDR A6WA2018041645770](https://openairdocs.org/sdr/A6WA2018041645770.md): Skin · dented · Apr 13, 2018 · N443AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP LOWER SKIN DENTED AT FLAP STATION 54.5 APPROXIMATELY 4 INCHES FROM TRAILING EDGE.
- [SDR A6WA2018041645769](https://openairdocs.org/sdr/A6WA2018041645769.md): Bracket · cracked · Apr 11, 2018 · N443AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MLG WHEEL WELL PRESSURE TRANSDUCER BRACKET IS CRACKED. REPLACED THE BRACKET IAW SRM 51-42-06.
- [SDR A6WA2018041645771](https://openairdocs.org/sdr/A6WA2018041645771.md): Retainer · cracked · Apr 10, 2018 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > L/H PYLON PANEL 412BT SEAL RETAINER CRACKED. REPAIRED THE SEAL RETAINER IAW SUPP 16-363.
- [SDR A6WA2018041645772](https://openairdocs.org/sdr/A6WA2018041645772.md): Retainer · cracked · Apr 10, 2018 · N443AW · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > LEFT LOWER PYLON PANEL 412DB SEAL RETAINER IS CRACKED. REPAIRED THE SEAL RETAINER IAW 16-363.
- [SDR A6WA2018042445777](https://openairdocs.org/sdr/A6WA2018042445777.md): Angle · damaged · Apr 3, 2018 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ANGLE DAMAGED AT BS 280 TO 295, STRINGERS 2L TO 4L, REPAIRED IAW REO 601R31522.
- [SDR A6WA2018012545575](https://openairdocs.org/sdr/A6WA2018012545575.md): Anti-Ice Valve · defective · Jan 16, 2018 · N443AW · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CLIMBOUT RECEIVED LEFT COWL ANTI-ICE CAUTION MESSAGE WITH COWL ANTI-ICE SELECTED OFF. C/W QRH MESSAGE CLEARED AT 84% N2. RETURNED FOR A NORMAL LANDING UNDER LANDING WEIGHT.
- [SDR A6WA2017103045366](https://openairdocs.org/sdr/A6WA2017103045366.md): Actuator · malfunctioned · Oct 21, 2017 · N443AW · Cndair CL6002B19 · Autopilot System
  > UNCOMMANDED YAW, ONCE DURING CLIMB AND ONCE IN CRUISE. SLIGHT YAW AND NO CROSSWIND OR TAILWIND NOTICED. NO MESSAGE POSTED, AUTOPILOT ENGAGED. REMOVED AND REPLACED LEFT YAW DAMPER LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECKED GOOD.
- [SDR A6WA2017022244801](https://openairdocs.org/sdr/A6WA2017022244801.md): B-Nut · leaking · Feb 16, 2017 · N443AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > DURING DESCENT WITH APU OFF AND BOTH PACKS SELECTED TO AUTO, CREW REPORTED STRONG FUEL ODOR IN CABIN AND COCKPIT. PERFORMED VISUAL INSPECTION OF AFT EQUIPMENT BAY AIR CONDITIONING DUCTS, NO DEFECTS NOTED. FOUND A B-NUT FITTING ON APU FUEL CONTROL UNIT LEAKING
- [SDR A6WA201744756](https://openairdocs.org/sdr/A6WA201744756.md): Unknown · odor · Jan 16, 2017 · N443AW · Cndair CL6002B19 · Air Distribution System
  > EXHAUST SMELL AND SMOKE IN CABIN WITH BOTH PACKS ON AND APU RUNNING.
- [SDR A6WA2016122844686](https://openairdocs.org/sdr/A6WA2016122844686.md): Skin · damaged · Dec 22, 2016 · N443AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AT BS 559+112 TO 574, STRINGERS 14 TO 16R.
- [SDR A6WA2016122844687](https://openairdocs.org/sdr/A6WA2016122844687.md): Stringer · damaged · Dec 22, 2016 · N443AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 15R DAMAGED BETWEEN BS 559+112 AND 574
- [SDR A6WA201644324](https://openairdocs.org/sdr/A6WA201644324.md): Inverter · inoperative · Sep 12, 2016 · N443AW · Bombdr CL6002D15 · Emergency Lighting
  > FLIGHT NUMBER 4041. EMERGENCY LIGHTS BETWEEN ROWS 5D AND 8D, AND EMERGENCY EXIT ROW 8F LOWER GREEN EXIT SIDEWALL SIGN NOT ILLUMINATING. R & R THE NR 3 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.
- [SDR A6WA201644276](https://openairdocs.org/sdr/A6WA201644276.md): Light · inoperative · Aug 29, 2016 · N443AW · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT 3862. LEFT LOWER EXIT LIGHT ROW 8 INOPERATIVE. FLOOR LIGHT ROWS 2-5 INOPERATIVE CYCLED EMERG LIGHT SWITCH. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51
- [SDR A6WA201644143](https://openairdocs.org/sdr/A6WA201644143.md): Heat Exchanger · unserviceable · Jul 24, 2016 · N443AW · Cndair CL6002B19 · Engine Oil Cooler
  > ON CLIMBOUT, RECEIVED HIGH OIL TEMP OF 151, FLASHING YELLOW, CW QRH OIL TEMP AGAIN CLIMBED IN TO CAUTION RANGE, FOLLOWED QRH PROCEDURES, ACCOMPLISHED SINGLE ENGINE PROCEDURES, OIL TEMP AND PRESSURE CLIMBING PRIOR TO ENGINE SHUTDOWN, OIL PRESSURE NEVER EXCEEDE
- [SDR A6WA201643858](https://openairdocs.org/sdr/A6WA201643858.md): Skin · damaged · May 7, 2016 · N443AW · Cndair CL6002B19 · Horizontal Stabilizer, Plate/Skin
  > REPAIR RT HORIZONTAL STAB, LOWER SKIN TEMP REPAIR IAW REO 601R-55-11-520. PERFORM PERMANENT REPAIR AS REQUIRED.
- [SDR A6WA201643857](https://openairdocs.org/sdr/A6WA201643857.md): Support Angle · cracked · May 7, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL 9 IN NLG WW HAS A CRACKED SUPPORT ANGLE TOP OF RBL 9 POST. REPLACED ANGLE AT RBL 9 & FS 202.75 IN NLG BAY IAW SRM 51-42-06.
- [SDR A6WA201643859](https://openairdocs.org/sdr/A6WA201643859.md): Spar · damaged · May 7, 2016 · N443AW · Cndair CL6002B19 · Horizontal Stabilizer, Spar/Rib
  > REPAIR RT HORIZONTAL STAB AT RIB 9. TEMP REPAIR COMPLIED WITH IAW REO 601R-55-11-519. PERFORM PERMANENT REPAIR.
- [SDR A6WA201643852](https://openairdocs.org/sdr/A6WA201643852.md): Skin · chafed · May 6, 2016 · N443AW · Cndair CL6002B19 · Rudder, Plate/Skin
  > BOTH SIDES OF RUDDER LE ARE HEAVILY CHAFED.
- [SDR A6WA201643856](https://openairdocs.org/sdr/A6WA201643856.md): Strap · damaged · May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INSTALLED NEW FUEL PRESS BOX, REQUIRED STRAP REPLACEMENT.
- [SDR A6WA201643853](https://openairdocs.org/sdr/A6WA201643853.md): Seat Track · corroded · May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL LBL 27 OTBD FLANGE HAS CORROSION AFT OF FS 559+112.
- [SDR A6WA201643848](https://openairdocs.org/sdr/A6WA201643848.md): Support Bracket · cracked · May 6, 2016 · N443AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER ENTRY DOOR SUPPORT WHEEL BRACKET CRACKED.
- [SDR A6WA201643849](https://openairdocs.org/sdr/A6WA201643849.md): Angle · cracked · May 6, 2016 · N443AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT WINDSHIELD SIDE POST LOWER OTBD ANGLE CLIP IS CRACKED IN FLIGHT DECK.

Next page: https://openairdocs.org/aircraft/N443AW/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 = 'N443AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N443AW/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.