# Service difficulty reports: N428AW

A list on [N428AW](https://openairdocs.org/aircraft/N428AW.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 · 209 reports

- [SDR A6WA202407048773](https://openairdocs.org/sdr/A6WA202407048773.md): Switch · faulted · Jul 4, 2024 · N428AW · Cndair CL6002B19 · Engine Thrust Reverser
  > REVERSE UNLOCKED AT 11000FT C/W IAC & QRH PRESSED EMER STOW. REV REMAINED UNLK. SHUT DWN RH ENG. TR APPEARED STOWED ON GND. AIRCRAFT REMOVED FROM SERVICE. C/W M ACTION FOR MEL 78-30-01. R THRUST REVERSER DEACTIVATED PER AWA SUP15-046D. THE T/R WAS FOUND NO
- [SDR A6WA202312218687](https://openairdocs.org/sdr/A6WA202312218687.md): Skin · dented · Dec 21, 2023 · N428AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 4 DENTS ON EXTERIOR LOWER SKIN AT FS 672.20 AND STRINGER 27. CUST W/O: 332319 JOB CARD: 453-900-501 EXTERIOR LOWER SKIN AT FS559.0 +112 - S755.0 AIRCRAFT REMOVED FROM SERVICE. PERFORMED HAND DRESS ON 4 EA DENTED AREAS (P1 TO P4) TO REFORM SKIN TO ORIGI
- [SDR A6WA202209258310](https://openairdocs.org/sdr/A6WA202209258310.md): Tire · flat · Sep 27, 2022 · N428AW · Cndair CL6002B19 · Tire
  > AFTER TO FROM KIND FELT A VIBRATION AND NOTICED #3 BTMS SHOWED LINES AND NO DIGITS. IND REPORTED TIRE DEBRIS ON RUNWAY. #4 BTMS READ 2. LANDED WITH OUT INCIDENT. CFR REPORTS #3 TIRE FLAT #4 TIRE SUPPORTING THE AC. TAXIED TO GATE WITHOUT INCIDENT ***AIRCRAFT
- [SDR A6WA202011247426](https://openairdocs.org/sdr/A6WA202011247426.md): Anti-Ice Valve · malfunctioned · Nov 22, 2020 · N428AW · Cndair CL6002B19 · Engine Anti-Icing System
  > RT ENGINE ANTI ICE CAUTION MESSAGE IN FLIGHT WITH SYSTEM OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT ENGINE COWL ANTI-ICE SHUT OFF VALVE, IAW AWAC SUP 10-094. OPERATIONS AND LEAK CHECK GOOD.
- [SDR A6WA2020013147138](https://openairdocs.org/sdr/A6WA2020013147138.md): Skin · dented · Jan 29, 2020 · N428AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > REF ROUTINE 1018039-1000-0062. 4DMI21302. REPAIR FS589-FS621, STR22L -STR23L, 601R-53-61-6304B. AIRCRAFT REMOVED FROM SERVICE REPAIRED LOWER FUSELAGE SKIN FS589-FS621, STR 21L - STR25R IAW BOMBARDIER REO 601R-53-61-7269 REV.-- DATED 1/28/2020
- [SDR A6WA2020012847137](https://openairdocs.org/sdr/A6WA2020012847137.md): Stiffener · cracked · Jan 28, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK LOCATED AT 409+128 18R ON LOWER END OF STRUT AIRCRAFT REMOVED FROM SERVICE REPAIRED POST AT FS 409+128 RBL 18 IAW REO 601R-53-41-889 REV D 601R-53-41-056 REV F AND 601R-53-41-2679 REV---.
- [SDR A6WA2020012847135](https://openairdocs.org/sdr/A6WA2020012847135.md): Stiffener · cracked · Jan 28, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CRACK AT 409+128, LBL27, INBOARD SIDE AT BOTTOM FASTENER HOLES. AIRCRAFT REMOVED FROM SERVICE REPAIRED CRACKED STIFFENER IAW REO 601R-53-41-056 REV. F.
- [SDR A6WA2020012847136](https://openairdocs.org/sdr/A6WA2020012847136.md): Drag Angle · misinstalled · Jan 27, 2020 · N428AW · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT WEB AND DRAG ANGLE HAS IMPROPERLY INSTALLED FASTENERS PN PAX DOOR AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT WEB AND DRAG ANGLE IAW SRM 51-42-13 AND SRM 51-42-06
- [SDR A6WA2020012247122](https://openairdocs.org/sdr/A6WA2020012247122.md): Post · cracked · Jan 21, 2020 · N428AW · Cndair CL6002B19 · Fuselage Main, Structure
  > FOUND A CRACK LOCATED AT 409+128, LBL 18, ON THE LOWER END OF STRUT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE POST STRUT IAW REO 601R-53-41, 56, REV E.
- [SDR A6WA2020012047113](https://openairdocs.org/sdr/A6WA2020012047113.md): Intercostal · corroded · Jan 17, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL JUST TO THE LEFT OF STRINGER 27 HAS CORROSION SPOTS BETWEEN FRAMES 364 AND 349, IN FWD E&E BAY. ORIGINAL MATERIAL.080, MATERIAL LOSS.009,.071 REMAINING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-4
- [SDR A6WA2020012047114](https://openairdocs.org/sdr/A6WA2020012047114.md): Skin · chafed · Jan 17, 2020 · N428AW · Cndair CL6002B19 · Ailerons
  > LEFT WING AILERON LOWER AND UPPER SURFACE LEADING EDGES ARE CHAFED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON UPPER LEADING EDGE IAW SRM 51-40-11, TR51-42, 51-42-06 AND SUPPLEMENT 13-055B. BLENDED LOWER LE AND FOUND TO BE WITHIN LIMIT
- [SDR A6WA2020012247119](https://openairdocs.org/sdr/A6WA2020012247119.md): Attach Bracket · cracked · Jan 16, 2020 · N428AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > CARGO DOOR AFT SPRING BOX ATTACH BRACKET WAS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR AFT SPRING BOX ATTACH BRACKET IAW CRJ 200 SRM 51-42-06
- [SDR A6WA2020011647112](https://openairdocs.org/sdr/A6WA2020011647112.md): Floor Support · corroded · Jan 16, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FS589 BETWEEN RIGHT FLOOR SILL AND RBL27 HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SUPPORT CAP STRIP IAW SRM 51-42-06 AND 51-42-15.
- [SDR A6WA2020011647111](https://openairdocs.org/sdr/A6WA2020011647111.md): Angle · cracked · Jan 16, 2020 · N428AW · Cndair CL6002B19 · Wing Miscellaneous Structure
  > O/B ANGLE P/N 600-12045-12, ON RIGHT WING AT PANEL 620ML, IS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW SRM 51-41-02.
- [SDR A6WA2020011647108](https://openairdocs.org/sdr/A6WA2020011647108.md): Spar · cracked · Jan 15, 2020 · N428AW · Cndair CL6002B19 · Elevator, Spar/Rib
  > LEFT ELEVATOR LOWER SURFACE 334DB ACCESS PANEL LANDING SPAR FLANGE CRACKED. AIRCRAFT REMOVED FROM SERVICE. REPAIRED LEFT ELEVATOR LOWER SPAR FLANGE IAW REO 601R-55-21-529 REV --.
- [SDR A6WA2020011647109](https://openairdocs.org/sdr/A6WA2020011647109.md): Floor Support · corroded · Jan 15, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE IS CORRODED AT FS559+64-559+80, RBL9. AIRCRAFT REMOVED FROM SERVICE REPAIRED FLOOR STRUCTURE IAW SRM 53-00-43.
- [SDR A6WA2020011647107](https://openairdocs.org/sdr/A6WA2020011647107.md): Skin · dented · Jan 14, 2020 · N428AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP, OUTBOARD END HAS DENT. (OUTBOARD AND BELOW OF THE OUTBOARD FLAP ARM) AIRCRAFT REMOVED FROM SERVICE REPAIRED LEFT WING INBOARD FLAP OUTBOARD END LOWER SKIN IAW REO 601R-57-52-1544.
- [SDR A6WA2020011347101](https://openairdocs.org/sdr/A6WA2020011347101.md): Stiffener · cracked · Jan 11, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STIFFENER P/N 601R36008-51 ON AFT SIDE OF 621 BULKHEAD, LBL 40, IS CRACKED. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED STIFFENER IAW CRJ SRM 51-42-06.
- [SDR A6WA2020011347100](https://openairdocs.org/sdr/A6WA2020011347100.md): Threshold · corroded · Jan 11, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR THRESHOLD HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE LOCATED, DRILLED AND REPLACED THRESHOLD IAW CRJ SRM 51-42-06 & TR51-4.
- [SDR A6WA2020011347102](https://openairdocs.org/sdr/A6WA2020011347102.md): Angle · cracked · Jan 11, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REAR PRESSURE BULKHEAD STGR 14 OBLIQUE ANGLE IS CRACKED. REMOVED FROM SERVICE REMOVED AND REPLACED REAR PRESURE BULKHEAD STGR 14 OBLIQUE ANGLE IAW CRJ-200 SRM 51-42-21
- [SDR A6WA2020011347103](https://openairdocs.org/sdr/A6WA2020011347103.md): Angle · cracked · Jan 11, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RPB AT FS 621 STRG 14 OBLIQUE ANGLE IS CRACKED AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RPB OBLIQUE ANGLE AT FS 621 BSTRG 14
- [SDR A6WA2020011347099](https://openairdocs.org/sdr/A6WA2020011347099.md): Support Bracket · cracked · Jan 10, 2020 · N428AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET CRACKED AT FS530, LH MLG WHEEL WELL. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER SUPPORT BRACKET AT FS530 IAW CRJ200 SRM 51-42-06
- [SDR A6WA2020011347104](https://openairdocs.org/sdr/A6WA2020011347104.md): Support · corroded · Jan 10, 2020 · N428AW · Cndair CL6002B19 · Landing Gear Doors
  > L/H MLG AFT LUG INTERIOR CORRODED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED DAMAGED SUPPORT ON LH MLG DOOR IAW CRJ-200 SRM 51-42-28
- [SDR A6WA2020011047097](https://openairdocs.org/sdr/A6WA2020011047097.md): Attach Angle · cracked · Jan 6, 2020 · N428AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > AFT LOWER CARGO DOOR BEAM ATTACH ANGLE CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CRACKED ANGLE IAW 51-42-21
- [SDR A6WA2020011047098](https://openairdocs.org/sdr/A6WA2020011047098.md): Attach Angle · cracked · Jan 6, 2020 · N428AW · Cndair CL6002B19 · Cargo/Baggage Doors
  > FWD LOWER CARGO DOOR BEAM ATTACH ANGLE CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED CRACKED ANGLE IAW CRJ 200 SRM 51-42-21
- [SDR A6WA2020010747095](https://openairdocs.org/sdr/A6WA2020010747095.md): Fitting · cracked · Jan 5, 2020 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H LOWER WINDSHIELD SIDE POST JOINT TO SILL FITTING CRACKED ON AFT SIDE AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED R/H LOWER WINDSHIELD SIDE POST JOINT TO SILL FITTING IAW CRJ-200 SRM 51-42-21
- [SDR A6WA2019123047084](https://openairdocs.org/sdr/A6WA2019123047084.md): Bracket · cracked · Dec 29, 2019 · N428AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > BRAKE PRESURE TRANSDUCER BRACKET IN R/H MLG WHEEL WELL AT FS529 IS CRACKED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRAKE PRESSURE TRANSDUCER BRACKET IAW CRJ200 SRM 51-42-06
- [SDR A6WA2018091446053](https://openairdocs.org/sdr/A6WA2018091446053.md): Light · broken · Sep 3, 2018 · N428AW · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY FLOODLIGHT BROKEN AT THE PAX DOOR. R&R FLOODLIGHT, OPS CHECK GOOD IAW 33-51-19.
- [SDR A6WA2018402165625](https://openairdocs.org/sdr/A6WA2018402165625.md): Valve · sticking · Feb 11, 2018 · N428AW · Cndair CL6002B19 · Cabin Pressure Control System
  > CLIMBING TO FL 200, PRESSURIZATION WAS NORMAL. ABOVE FL 220 CABIN ALTITUDE CLIMBED AT AN EXCESSIVE RATE. DURING CRUISE AT FL 290, CABIN ALTITUDE 7300 AND A DELTA P OF 7300 FT. WHEN STARTING DECENT AND REDUCING ENGINE POWER CABIN ALTITUDE CLIMBED AT A RATE OF
- [SDR A6WA201845611](https://openairdocs.org/sdr/A6WA201845611.md): Warning Message · illuminated · Feb 4, 2018 · N428AW · Cndair CL6002B19 · Ice/Rain Protection System
  > RECIEVED AN ANTI-ICE DUCT WARNING MESSAGE IN FLT. LEFT WING LEADING EDGE RED ON SYNOPTIC PAGE. OCCURED ON APPROACH. THROTTLE MID RANGE. INDICATIONS INITIALLY CLEARED WHEN ANTI-ICE SELECTED TO OFF THEN TO STANDBY. MESSAGE INDICATION RECURRED AFTER SEVERAL MIN
- [SDR A6WA201845576](https://openairdocs.org/sdr/A6WA201845576.md): Skin · dented · Jan 17, 2018 · N428AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN DENTED AT BS 589 TO 621, STRINGERS 22 - 23L
- [SDR A6WA2018011745562](https://openairdocs.org/sdr/A6WA2018011745562.md): Angle · cracked · Jan 10, 2018 · N428AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > RT UPPER OBLIQUE ANGLE CRACKED ON AFT PRESSURE BULKHEAD. REPLACED.
- [SDR A6WA2018011745565](https://openairdocs.org/sdr/A6WA2018011745565.md): Bracket · cracked · Jan 9, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT LOWER CENTER WINDSHIELD POST BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-21.
- [SDR A6WA2018011545563](https://openairdocs.org/sdr/A6WA2018011545563.md): Bracket · cracked · Jan 9, 2018 · N428AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LEFT LOWER CENTER WINDSHIELD POST BRACKET CRACKED. REPLACED THE BRACKET.
- [SDR A6WA201845548](https://openairdocs.org/sdr/A6WA201845548.md): Angle · cracked · Jan 7, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT UPPER OBLIQUE ANGLE CRACKED AT FS 621.00, STR 14L. REPLACED ANGLE IAW SRM 51-42-21, 51-40-11.
- [SDR A6WA2018011745566](https://openairdocs.org/sdr/A6WA2018011745566.md): Skin · corroded · Jan 4, 2018 · N428AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT I/B FLAP SKIN CORRODED. REPLACED LT I/B LOWER SKIN IAW SRM 51-42-10, 51-42-13.
- [SDR A6WA2018010945556](https://openairdocs.org/sdr/A6WA2018010945556.md): Doubler · corroded · Jan 4, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT DOUBLER CORRODED AT FS 313.00, LBL20. REPLACED DOUBLER IAW SRM 51-21-06, 51-42-13, 51-24-36, 51-40-11.
- [SDR A6WA2018010945550](https://openairdocs.org/sdr/A6WA2018010945550.md): Guide · cracked · Jan 3, 2018 · N428AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > PANEL 422BT GUIDES ARE CRACKED. REPLACED GUIDES IAW CMM 20-42-06.
- [SDR A6WA2018010945552](https://openairdocs.org/sdr/A6WA2018010945552.md): Angle · cracked · Jan 2, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AT FS280.00, RBL8. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.
- [SDR A6WA2018010945549](https://openairdocs.org/sdr/A6WA2018010945549.md): Angle · cracked · Jan 2, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AT FS 280.00, LBL11. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.
- [SDR A6WA2018010945553](https://openairdocs.org/sdr/A6WA2018010945553.md): Angle · cracked · Jan 2, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AT FS280.00, LBL8. REPLACED ANGLE IAW REO601R-53-11-171 REV-D.
- [SDR A6WA2018010945551](https://openairdocs.org/sdr/A6WA2018010945551.md): Angle · cracked · Jan 2, 2018 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE CRACKED AT FS 280.00, RBL11. REPLACED ANGLE IAW REO 601R-53-11-171 REV-D.
- [SDR A6WA2017010445539](https://openairdocs.org/sdr/A6WA2017010445539.md): Floor Support · cracked · Dec 31, 2017 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR OPENING FLOOR SUPPORT HAS CRACK. REPAIRED THE FLOOR SUPPORT.
- [SDR A6WA2017011545557](https://openairdocs.org/sdr/A6WA2017011545557.md): Skin · chafed · Dec 30, 2017 · N428AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE SKIN CHAFED AT WS 56.30. REPLACED SKIN IAW SRM 51-42-13.
- [SDR A6WA2017010945554](https://openairdocs.org/sdr/A6WA2017010945554.md): Doubler · corroded · Dec 30, 2017 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR MOUNT DOUBLER CORRODED FOR GALLEY AT FS317.00. REPLACED DOUBLER IAW SRM 51-24-36, 51-42-06.
- [SDR A6WA2017010945555](https://openairdocs.org/sdr/A6WA2017010945555.md): Doubler · corroded · Dec 30, 2017 · N428AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GALLEY FLOOR SUPPORT DOUBLER CORRODED FROM FS 297.00, RBL5. REPLACED DOUBLER IAW SRM 51-24-36, 51-42-06, 51-42-13.
- [SDR A6WA2017010945557](https://openairdocs.org/sdr/A6WA2017010945557.md): Skin · chafed · Dec 30, 2017 · N428AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBOARD FLAP VANE SKIN CHAFED AT W56.30. REPLACED SKIN IAW SRM 51-42-13.
- [SDR A6WA201745232](https://openairdocs.org/sdr/A6WA201745232.md): Rvdt · failed · Aug 25, 2017 · N428AW · Cndair CL6002B19 · Landing Gear Steering System
  > DURING CRUISE AT FL 320, RECEVED A STEERING INOPERATIVE CAUTION MESSAGE. COMPLIED WITH QRH. MESSAGE PERSISTED. DECLARED EMERGENCY. REPLACED THE LT NWS RVDT IAW 15-177A, CHECKED GOOD AFTER TAXI TEST.
- [SDR A6WA201745220](https://openairdocs.org/sdr/A6WA201745220.md): Wire Harness · damaged · Aug 23, 2017 · N428AW · Cndair CL6002B19 · Landing Gear System Wiring
  > STEERING INOPERATIVE CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE PERSISTS. DECLARED EMERGENCY. R & R NLG ELECTRICAL STEERING HARNESS IAW 12-029D. OPS CHECKED GOOD, NO MESSAGE.
- [SDR A6WA201745096](https://openairdocs.org/sdr/A6WA201745096.md): Target · loose · Jul 12, 2017 · N428AW · Bombdr CL6002D15 · Landing Gear Position and Warning
  > GEAR DISAGREE AFTER TAKEOFF. RT MLG UNSAFE. COMPLIED WITH QRH. MANUALLY EXTENDED GEAR. EMERGENCY DECLARED, AIR RETURN. FOUND ACARS DATA POINTS TO RT MLG UPLOCK. INSPECTED AND FOUND RT MLG UPLOCK PROXIMITY SENSOR PS7GA TARGET LOOSE. TORQUED AND SAFETIED

Next page: https://openairdocs.org/aircraft/N428AW/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 = 'N428AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N428AW/reports

---
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