# Service difficulty reports: N449AW

A list on [N449AW](https://openairdocs.org/aircraft/N449AW.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 · 195 reports

- [SDR A6WA202101137518](https://openairdocs.org/sdr/A6WA202101137518.md): Pdu · malfunctioned · Jan 7, 2021 · N449AW · Cndair CL6002B19 · Engine Thrust Reverser
  > EN ROUTE, DURING CLIMB, THE FLIGHT EXPERIENCED A LT THRUST REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLIED WITH THE QRH, NOTIFIED DISPATCH, AND DIVERTED TO KSYR. AIRCRAFT REMOVED FROM SERVICE. PDU LOCK WILL NOT FULLY STOW R & R PDU, IAW AMM 78-30. OPE
- [SDR A6WA202102127628](https://openairdocs.org/sdr/A6WA202102127628.md): Bulkhead Web · cracked · Oct 31, 2020 · N449AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 1" CRACK DETECTED ON FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50. 36" ABOVE FLOOR LEVEL ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED CRACK OF FWD FACE OF AFT PRESSURE BULKHEAD AT LBL 27.50 36 INCHES ABOVE FLOOR LEVEL IAW BOMBARDIER REO 601R-53-61-1285
- [SDR A6WA202011027378](https://openairdocs.org/sdr/A6WA202011027378.md): Structure · corroded · Oct 30, 2020 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL 27 AT FS 559 +80 TO FS 559+120 T CAP EXTRUSION HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP EXTRUSION, LBL 27 AT FS 559 +80 TO FS 559+120, IAW DRAWING 601R35031 AND CRJ 200 SRM 51-42-20.
- [SDR A6WA202011027379](https://openairdocs.org/sdr/A6WA202011027379.md): Seat Track · corroded · Oct 30, 2020 · N449AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 AT FS 559+65 TO FS 559+81 SEAT TRACK HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT LBL 27 AT FS 559+65 TO FS 559+81, IAW REO 601R-53-00-764 AND CRJ 200 SRM 51-42-20.
- [SDR A6WA202011027377](https://openairdocs.org/sdr/A6WA202011027377.md): Beam · corroded · Oct 30, 2020 · N449AW · Cndair CL6002B19 · Fuselage Main, Structure
  > LBL 27 AT FS 559+20 TO FS 605 T CAP EXTRUSION HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T CAP AT LBL 27 FS 559=20 TO FS 605, IAW DRAWING 601R35031.
- [SDR A6WA2019100846907](https://openairdocs.org/sdr/A6WA2019100846907.md): Warning Message · illuminated · Oct 5, 2019 · N449AW · Cndair CL6002B19 · Pneumatic Distribution System
  > ON INITIAL CLIMB L 14TH DUCT WARNING MESSAGE DISPLAYED. WARNING DID NOT EXTINGUISH, PER THE QRH THE FLIGHT RETURNED TO EVV WITH NO FURTHER ISSUES.
- [SDR A6WA2019021146391](https://openairdocs.org/sdr/A6WA2019021146391.md): Warning System · activated · Feb 9, 2019 · N449AW · Cndair CL6002B19 · Engine Thrust Reverser
  > IN CRUISE, RECEIVED L REV UNLOCKED CAUTION MESSAGE. PERFORMED IAC AND QRH, MESSAGE REMAINED. COMPLETED THE QRH, COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY WITH ATC AND LANDED AT NEAREST AIRPORT PER QRH. REVERSER APPEARED TO BE IN STOWED POSITION. N1 REV
- [SDR A6WA2018120946216](https://openairdocs.org/sdr/A6WA2018120946216.md): Unknown · odor · Dec 6, 2018 · N449AW · Cndair CL6002B19 · Air Distribution System
  > FOLLOWING A FAILED START ATTEMPT OF THE APU IN FLIGHT AND A 2 MINUTE COOL DOWN AND A SUCCESSFUL START. THERE WAS A VERY STRONG ODOR OF FUEL IN THE COCKPIT AND CABIN. SHUT DOWN THE APU AND ODOR DISSIPATED. CW OPERATIONAL CHECK OF APU IAW AMM 49-10-00. OPS CHECK
- [SDR A6WA2018072445946](https://openairdocs.org/sdr/A6WA2018072445946.md): Skin · damaged · Jul 23, 2018 · N449AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP, LOWER SKIN DINGED AND PTTED. REMOVED AND REPLACED RT IB FLAP IB LOWER SKIN IAW SRM 51-42-13.
- [SDR A6WA2018072445947](https://openairdocs.org/sdr/A6WA2018072445947.md): Skin · dented · Jul 23, 2018 · N449AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT AT FS 589 BELOW CARGO DOOR REPAIRED. REPAIR DENT AT FS 589 BELOW CARGO DOOR IAW EA AWAC-CRJ253-00991 REV A DATE 07/11/2018.
- [SDR A6WA2018072445945](https://openairdocs.org/sdr/A6WA2018072445945.md): Skin · damaged · Jul 23, 2018 · N449AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP LOWER IB SKIN DINGED AND PITTED. REMOVED AND REPLACED LH IB FLAP IB LOWER SKIN IAW SRM 51-42-13.
- [SDR A6WA2018072445944](https://openairdocs.org/sdr/A6WA2018072445944.md): Skin · chafed · Jul 22, 2018 · N449AW · Cndair CL6002B19 · Ailerons
  > RT AILERON UPPER SKIN LEADING EDGE HAS SEVERAL CHAFED SPOTS. REMOVED AND REPLACED RT AILERON UPPER SKIN IAW SRM 51-42-22.
- [SDR A6WA2018072445942](https://openairdocs.org/sdr/A6WA2018072445942.md): Bracket · cracked · Jul 21, 2018 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLIGHT COMPARTMENT CENTER WINDSHIELD POST LT LOWER BRACKET CRACKED FROM LOWER RIVET TO EDGE OF BRACKET. REMOVED AND REPLACED CENTER POST LT LOWER BRACKET IAW SRM 51-42-21 AND 51-25-06.
- [SDR A6WA2018072445943](https://openairdocs.org/sdr/A6WA2018072445943.md): Skin · chafed · Jul 19, 2018 · N449AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT I/B FLAP VANE LEADING EDGE CHAFED AT WS 56.00. REPLACED RIGHT WING I/B FLAP VANE LEADING EDGE IAW SRM 51-42-13.
- [SDR A6WA2018102246118](https://openairdocs.org/sdr/A6WA2018102246118.md): Bulkhead · dented · Jul 17, 2018 · N449AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SIDE HAS A DENT AT LBL22. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-53-61-6635 REV-A.
- [SDR A6WA2018102246119](https://openairdocs.org/sdr/A6WA2018102246119.md): Bulkhead · dented · Jul 17, 2018 · N449AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD FWD SIDE HAS DENT AT LBL31. REPAIRED AFT PRESSURE BULKHEAD IAW REO601R-61-6635 REV-A.
- [SDR A6WA2018072445941](https://openairdocs.org/sdr/A6WA2018072445941.md): Seat Track · corroded · Jul 17, 2018 · N449AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDEWALL SEAT TRACK NR 6 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.
- [SDR A6WA2018072445940](https://openairdocs.org/sdr/A6WA2018072445940.md): Retainer · cracked · Jul 16, 2018 · N449AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON PNL 412DB HAS CRACKED SEAL RETAINER. REPAIRED SEAL RETAINER IAW SUPP 16-363.
- [SDR A6WA2018071845939](https://openairdocs.org/sdr/A6WA2018071845939.md): Skin · chafed · Jul 16, 2018 · N449AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT I/B FLAP VANE LEADING EDGE SKIN CHAFED. REPLACED RIGHT I/B FLAP VANE LEADING EDGE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018071845938](https://openairdocs.org/sdr/A6WA2018071845938.md): Retainer · cracked · Jul 15, 2018 · N449AW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT PYLON PNL 422BT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 54-63-01, 51-42-06, 51-40-11.
- [SDR A6WA2018020545609](https://openairdocs.org/sdr/A6WA2018020545609.md): Bulkhead Web · cracked · Feb 1, 2018 · N449AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING A BULKHEAD INSPECTION, NDT REVEALED A ONE INCH CRACK BS 621, LBL 27.5, WL 132.
- [SDR A6WA2017101145336](https://openairdocs.org/sdr/A6WA2017101145336.md): Duct · detached · Oct 4, 2017 · N449AW · Cndair CL6002B19 · Air Distribution System
  > TOILET SMOKE CAUTION MESSAGE ON PUSH BACK, APU ON 10TH STAGE BLEEDS CLOSED, ENGS OFF, F/A REPORTED SMOKE IN THE CABIN. FIRE BOTTLES ARMED. INSPECTED ACFT ELECTRICAL SYSTEMS AND PNEUMATIC SYSTEMS, NO SMOKE OR ODORS PRESENT. FOUND THE LEFT PACK DUCT BLOWN, RE
- [SDR A6WA2017051644997](https://openairdocs.org/sdr/A6WA2017051644997.md): Pump · failed · May 12, 2017 · N449AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > AFTER TAKEOFF WITH GEAR SELECTOR UP, FOR MORE THAN 30 SECONDS RECEIVED GEAR DISAGREE WARNING MESSAGE. MAIN LANDING GEAR SHOWED WHITE HASH MARKS. NOSE GEAR SHOWED RED HASH MARKS. MESSAGE PERSISTED FOR MORE THAN 20 SECONDS. COMPLIED WITH QRH. TURNED ON HYD PUM
- [SDR A6WA2017042844945](https://openairdocs.org/sdr/A6WA2017042844945.md): Switch · failed · Apr 22, 2017 · N449AW · Cndair CL6002B19 · Fuel System Wiring
  > ACRID ODOR IN COCKPIT, (FAINT ELECTRICAL PLASTIC ODOR) APPROX. 10 MIN INTO FLIGHT, NOT NOTICEABLE OUTSIDE COCKPIT, NO ABNORMAL EICAS MESSAGES. DURING TROUBLESHOOTING, FOUND GROUND FAN INTERNAL WIRING HAD FRAYED AND MISSING SHIELDING ON INTERNAL WIRING. R & R
- [SDR A6WA201744943](https://openairdocs.org/sdr/A6WA201744943.md): Switch · not seated · Apr 21, 2017 · N449AW · Bombdr CL6002D15 · Aircraft Fuel Distribution System
  > AFTER ROTATION EXPERIENCED FAINT ELECTRICAL, BURNT / OVERHEATED BRAKE ODOR. WENT AWAY, RETURNED AFTER 5-6 MIN AND AGAIN 20 MIN INTO FLIGHT. EACH TIME A LITTLE STRONGER ODOR. NO INOP FANS, LIGHTS OR ASSOCIATED MESSAGES. ODOR MAINLY IN COCKPIT. 2 TIMES ON APU BL
- [SDR A6WA201744895](https://openairdocs.org/sdr/A6WA201744895.md): B-Nut · loose · Mar 26, 2017 · N449AW · Bombdr CL6002D15 · APU Engine Fuel and Control
  > STRONG FUEL & EXHAUST ODOR COMING FROM BLEED AIR SYSTEM. STRONGER ODOR IN FLT DECK AND DURING FLT. THIS HAPPENS ON ENGINE AIR AS WELL AS ON APU AIR ONLY. FOUND THE MAIN FEED MANIFOLD CRACKED. FOUND BOTTOM B-NUT OF APU SOLENOID SHUTOFF VALVE LOOSE. SECURED
- [SDR A6WA201744886](https://openairdocs.org/sdr/A6WA201744886.md): Coalescer Bag · odor · Mar 24, 2017 · N449AW · Bombdr CL6002D15 · Humidity Control System
  > STRONG EXHAUST PETROLEUM ODOR COMING FROM BLEED AIR SYSTEM. STRONGER ON FLIGHT DECK. NO NOTICEABLE DIFFERENCE BETWEEN GATE AND CRUISE. R & R THE LT & RT COALESCER SOCKS ON AIR-CONDITIONING WATER SEPARATORS IAW SUP 14-192. OPS AIR-CONDITIONING SYSTEM. NO ODOR
- [SDR A6WA201744865](https://openairdocs.org/sdr/A6WA201744865.md): Apu · malfunctioned · Mar 18, 2017 · N449AW · Bombdr CL6002D15 · APU Core Engine
  > APU FIRE MESSAGE, FOLLOWED BY APU AUTO SHUTDOWN. REMOVED AND REPLACED THE APU IAW TASK CARD, SUP 13-005 AND AMM 49-10. OPS AND LEAK CHECKED GOOD.
- [SDR A6WA2016122844700](https://openairdocs.org/sdr/A6WA2016122844700.md): Handle · unsecure · Dec 26, 2016 · N449AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR HANDLE DOES NOT POP OUT FROM OUTSIDE.
- [SDR A6WA2016121644663](https://openairdocs.org/sdr/A6WA2016121644663.md): Light · inoperative · Dec 13, 2016 · N449AW · Cndair CL6002B19 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY LIGHTS DOES NOT ILLUMINATE FROM ROW 7 TO AFT OF ACFT.
- [SDR A6WA2016112144593](https://openairdocs.org/sdr/A6WA2016112144593.md): Flap System · failed · Nov 20, 2016 · N449AW · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED ON GO AROUND AT 20 DEGREES. COMING UP FROM 45 DEGREES. OVERSPEED CLACKER OCCURRED NEAR THE SAME TIME, AIR SPEED WAS 180 KIAS. COMPLIED WITH AWAC SUPP 98-018G TO STEP 12 A1. FLAPS FAILED ON CIRCUIT BREAKER RESET (CBP1-F4 AND CBP2-F4)
- [SDR A6WA201644538](https://openairdocs.org/sdr/A6WA201644538.md): Apu · leaking · Oct 31, 2016 · N449AW · Cndair CL6002B19 · APU Oil System
  > SMOKE APPEARED IN THE FLIGHT DECK FROM AIR CONDITIONING VENTS, APU SHUTDOWN SHORTLY AFTERWARDS. LARGE PUDDLE OF OIL DRIPPING FROM AFT EQUIPMENT BAY.
- [SDR A6WA201644535](https://openairdocs.org/sdr/A6WA201644535.md): Light · inoperative · Oct 30, 2016 · N449AW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS FROM ROW 8 AFT DO NOT TURN ON.
- [SDR A6WA201644365](https://openairdocs.org/sdr/A6WA201644365.md): Unknown · odor · Sep 23, 2016 · N449AW · Cndair CL6002B19 · Air Distribution System
  > SMOKE APPEARANCE AND ELECTRICAL ODOR ROW 10 D/F AND 11 D/F AT CEILING LIGHTS WITH LIGHTS ON.
- [SDR A6WA201644278](https://openairdocs.org/sdr/A6WA201644278.md): Yaw Damper · defective · Aug 29, 2016 · N449AW · Cndair CL6002B19 · Autopilot System
  > WHILE IN CRUISE, ACFT HAD UNCOMMANDED YAW TO LEFT. YAW DAMPERS REMAINED ENGAGED AT ALL TIMES. UNCOMMANDED YAW WAS INTERMITENT AND RANDOM IN NATURE. REQUEST INSPECTION. REMOVED AND INSTALLED NEW LINER ACUATOR YAW DAMPER IAW 22-22-01. OPS CHECKED GOOD IAW
- [SDR A6WA201644157](https://openairdocs.org/sdr/A6WA201644157.md): Unknown · malfunctioned · Jul 26, 2016 · N449AW · Cndair CL6002B19 · Autopilot System
  > INTERMITTENT UNCOMMANDED YAW DURING CRUISE AND DECENT. YD2 DISENGAGED PRIOR TO APPROACH RE-ENGAGED ALTHOUGH YAW MOTION CONTINUED.
- [SDR A6WA201644054](https://openairdocs.org/sdr/A6WA201644054.md): Light · inoperative · Jun 30, 2016 · N449AW · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED THAT THE FLOOR LEVEL EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROW 8 AFT. FOUND DURING THE FIRST FLIGHT OF THE DAY ACCEPTANCE INSPECTION.
- [SDR A6WA201644033](https://openairdocs.org/sdr/A6WA201644033.md): Stringer · corroded · Jun 24, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF THE SPADE DOOR UPPER BUSHINGS, FOUND CORROSION UNDER LT SPADE DOOR FITTING.
- [SDR A6WA201644035](https://openairdocs.org/sdr/A6WA201644035.md): Striker · bent · Jun 24, 2016 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR CUTOUT FWD EDGE AT UPPER LOCK LUG, LIP, SEAL STRIKER BENT.
- [SDR A6WA201644036](https://openairdocs.org/sdr/A6WA201644036.md): Stringer · corroded · Jun 24, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF THE SPADE DOOR UPPER BUSHINGS, FOUND CORROSION UNDER RT SPADE DOOR FITTING.
- [SDR A6WA201644034](https://openairdocs.org/sdr/A6WA201644034.md): Frame · cracked · Jun 24, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED, FS 333 AND STR 1L.
- [SDR A6WA201644037](https://openairdocs.org/sdr/A6WA201644037.md): Pan · corroded · Jun 24, 2016 · N449AW · Cndair CL6002B19 · Service Doors
  > SERVICE DOOR AFT LOWER PAN SEGMENT HAS CORROSION ON LOWER AND UPPER SURFACES. COMPLIED WITH TEMPORARY DISPOSITION FOR CORROSION DAMAGE ON LOWER AFT PAN OF SERVICE DOOR IAW REO 601R-52-41-238, REV DATED 06-21-2016.
- [SDR A6WA201644030](https://openairdocs.org/sdr/A6WA201644030.md): Skin · cracked · Jun 22, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > SKIN CRACKED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R. REPAIRED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R IAW GREO 601R-53-11-048, REV-D, DATED 06/10/2015.
- [SDR A6WA201644027](https://openairdocs.org/sdr/A6WA201644027.md): Floorbeam · corroded · Jun 22, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CARGO PIT FLOOR AFT FITTING INBD FLANGE IS CORRODED AT FS 612.00, LBL9. REPAIRED CORROSION ON INBD AND OTBD FLANGES ON LBL9 CARGO BEAM AT FS 612, FS 615 IAW EA AWAC-CRJ253-00409, REV-A.
- [SDR A6WA201644025](https://openairdocs.org/sdr/A6WA201644025.md): Frame · corroded · Jun 21, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 319.7, FWD SIDE JUST OTBD OT THE STR 23R INTERCOSTAL CORRODED, REPAIRED.
- [SDR A6WA201644020](https://openairdocs.org/sdr/A6WA201644020.md): Frame · corroded · Jun 18, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333, ON THE FWD SIDE BETWEEN STR 23R AND 20R HAS CORROSION, REPAIRED.
- [SDR A6WA201644007](https://openairdocs.org/sdr/A6WA201644007.md): Floorbeam · corroded · Jun 16, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > AFT FLOORBEAM FITTING AT LBL27 AND FS610.00 TO 621.00 HAS CORROSION ON FLANGE AND UNDER TEFLON CAP STRIP. REPAIRED CORROSION AT FS 610.00 TO 621.00, LBL27 CARGO FLOORBEAM REO 601R-53-61-4530, REV-A.
- [SDR A6WA201644021](https://openairdocs.org/sdr/A6WA201644021.md): Angle · cracked · Jun 16, 2016 · N449AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LEFT OVERWING TO FUSELAGE PANEL ATTACH STRUCTURE AT FS 470.00 IS CRACKED, REPLACED.
- [SDR A6WA201644010](https://openairdocs.org/sdr/A6WA201644010.md): Floor Support · corroded · Jun 16, 2016 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO PIT FLOOR SUPPORT IS CORRODED AT FS 589.00 BETWEEN LBL9 TO 27. REPLACED CARGO FLOOR SUPPORT AT FS 589.00 BETWEEN LBL9 TO 27 IAW SRM 51-40-11, 51-42-06.
- [SDR A6WA201644009](https://openairdocs.org/sdr/A6WA201644009.md): Structure · corroded · Jun 16, 2016 · N449AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR MEMBER BETWEEN RBL 27 TO RT SILL AND FS 589.00 IS CORRODED AROUND SCREW HOLES. REPLACED CARGO FLOOR MEMBER FROM RBL 27 TO RT SILL, FS 589.00 IAW SRM 51-40-11, 51-42-06.

Next page: https://openairdocs.org/aircraft/N449AW/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 = 'N449AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N449AW/reports

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