# Service difficulty reports: N451AW

A list on [N451AW](https://openairdocs.org/aircraft/N451AW.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 · 161 reports

- [SDR A6WA202312198682](https://openairdocs.org/sdr/A6WA202312198682.md): Unknown · unknown · Oct 19, 2023 · N451AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > WHEN SELECTING GEAR UP, GEAR DISAGREE. COMPLIED WITH QRH, MESSAGE CLEARED. NORMAL LANDING. NOSE STEERING NORMAL. NOSE GEAR INDICATED DOWN AFTER SELECTING UP, NOSE REMAINED GREEN. AIRCRAFT REMOVED FROM SERVICE. R&R NLG OLEO CENTERED/EXTENDED PROX SENSOR BRACK
- [SDR A6WA202305068591](https://openairdocs.org/sdr/A6WA202305068591.md): Unknown · unknown · May 6, 2023 · N451AW · Cndair CL6002B19 · Window/Windshield System
  > RH WINDOW SHATTERED IN FLIGHT AT FL280 PRESSURIZATION IS NORMAL CW CRH REQ INSP **********AIRCRAFT REMOVED FROM SERVICE********* IN WORK
- [SDR A6WA202211168383](https://openairdocs.org/sdr/A6WA202211168383.md): Wire Harness · failed · Nov 16, 2022 · N451AW · Cndair CL6002B19 · Landing Gear System Wiring
  > RECEIVED STEERING INOP, WOW INPUT, AND WOW OUTPUT FAIL MESSAGES DURING INITIAL CLIMB OUT. GEAR WAS UP AND LOCKED. CW QRH. STEERING SELECTED OFF VIA QRH AND WOW MESSAGES REMAINED. WOW MESSAGES CLEARED WHEN SELECTING GEAR DOWN ON APPROACH. AFTER LANDING RENEGAG
- [SDR A6WA202210228356](https://openairdocs.org/sdr/A6WA202210228356.md): Relay · failed · Oct 22, 2022 · N451AW · Cndair CL6002B19 · APU Engine Fuel and Control
  > APU SOV STATUS PRESENT IN-FLIGHT WITH APU OFF. MESSAGE CLEARED AFTER ENGINE SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. R&R FUEL CONTROL RELAY IAW 20-22-00. OPS CHECK GOOD.
- [SDR A6WA202206288198](https://openairdocs.org/sdr/A6WA202206288198.md): Nut Plate · elongated · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TEMPORARY REPAIR TO THE ELONGATED NUT PLATE HOLE IN FUSELAGE STRUCTURE AT STRINGER 19R BETWEEN FS409+80 - FS409+96. ****AIRCRAFT REMOVED FROM SERVICE *** REPAIRED FUSELAGE SKIN NUT PLATE HOLE AT STRINGER 19R BETWEEN FS409+80 TO FS409+96 REF REO 601R-53-31-128
- [SDR A6WA202206288199](https://openairdocs.org/sdr/A6WA202206288199.md): Support Angle · corroded · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > WIRE SUPPORT ANGLE CORRODED AT THE AFT LAV SERVICE POINT. ***AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED BRACKET.
- [SDR A6WA202206288203](https://openairdocs.org/sdr/A6WA202206288203.md): Intercostal · cracked · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT FS654 TO FS672.20 FOUND CRACKED. ***AIRCRAFT REMOVED FROM SERVICE **** REPAIRED INTERCOSTAL IAW AWAC SUPPLEMENT 13-085B DATE ISSUED 2/03/2014 AND REO 601R-53-62-225 REV. DATED 2013-09-19.
- [SDR A6WA202206288201](https://openairdocs.org/sdr/A6WA202206288201.md): Panel · dented · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS700.00+13 STRINGER 20L+5 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE ***** DRESSED BACK DENT IAW DISPOSITION INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.
- [SDR A6WA202206288196](https://openairdocs.org/sdr/A6WA202206288196.md): Panel · dented · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS 654.50 TO FS 654.50 + 9 STRINGER 22R +5 2 EA. OUTWARD DENTS C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE ***** REPAIRED FS654.50 TO FS654.50+9 STRINGER 22R DENT REF REO 601R-53-61-7835 REV. DATED 2022-05-24.
- [SDR A6WA202206288202](https://openairdocs.org/sdr/A6WA202206288202.md): Panel · dented · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS625.30+12 STRINGER 22R+4 OUTWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ****AIRCRAFT REMOVED FROM SERVICE **** REPAIRED DENT DAMAGE TO FUSELAGE LOWER SKIN BETWEEN FS625.00 - FS640.00 AND STR 22R - STR 23R REF REO 601R-53-61-7836 REV. DATED 2022-05-25
- [SDR A6WA202206288197](https://openairdocs.org/sdr/A6WA202206288197.md): Panel · dented · Jun 28, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FS605.00+1 STRINGER 23L+3 INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL. ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829 REV DATED 2022-05-17.
- [SDR A6WA202206278194](https://openairdocs.org/sdr/A6WA202206278194.md): Skin Panel · dented · Jun 27, 2022 · N451AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > F/S 605.00+1, STRINGER 23L+3; INWARD DENT C/T EXTERIOR SIDE OF SKIN PANEL ***AIRCRAFT REMOVED FROM SERVICE **** DRESSED BACK DENT AS PER INSTRUCTIONS OUTLINED IN REO 601R-53-61-7829, REV--, DATED 2022-05-17 AND REO 601R-51-00-309 REV. -A DATED 2017-08-23. GE
- [SDR A6WA202108167856](https://openairdocs.org/sdr/A6WA202108167856.md): Seal · mismanufactured · Aug 15, 2021 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > REF. 342366/4 AND 342667/1- LOUD SQUEAL AT 4,000 FT 250 KNOTS. ABNORMAL CLIMB RATE AT CABIN ALT. AT 10,000 FT, CABIN ALT REMAINED AT 5,000 FT. CABIN ALT INCREASED WITH DECREASED POWER. ON FINAL APPROACH ABNORMALLY HIGH RATE OF DECENT OF CABIN ALT. LANDING W
- [SDR A6WA202108177857](https://openairdocs.org/sdr/A6WA202108177857.md): Seal · leaking · Aug 14, 2021 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > 3930 DURING CLIMBOUT AROUND 13K FEET HEARD LOUD HISSING SOUND COMING FROM BEHIND THE FLIGHT DECK. FA CALLED AND SAID IT WAS FROM THE MAIN CABIN DOOR. AROUND 19K FEET HISSING GOT LOUDER AND CABIN RATE RAPIDLY INCREASED. CABIN ALTITUDE NEVER EXCEEDED 6K FEET.
- [SDR A6WA202010267364](https://openairdocs.org/sdr/A6WA202010267364.md): Windshield · cracked · Oct 26, 2020 · N451AW · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN OUTER SINDSCREEN (WINDSHIELD) CRACKED WHILE ASCENDING THROUGH 19,000FT. C/W QRH AND RETURNED TO DAY. AIRCRAFT REMOVED FROM SERVICE. R & R LT WINDSHIELD, IAW AMM 56-11-01 REF WO 300890 MX WORK CARD NR 3 FOR OPERATIONS AND LEAK CHECK.
- [SDR A6WA202010067312](https://openairdocs.org/sdr/A6WA202010067312.md): Skin · damaged · Oct 6, 2020 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > NUT PLATE HOLE IN FUSELAGE SKIN AND UNDERLINING DOUBLER AT STR 19R AND FS 409+93 OBLONG/ELONGATED TO 0.297W X 0.294. AIRCRAFT REMOVED FROM SERVICE. OPENED HOLE IN STR 19R TO 0.2055, REF REO 601R-53-31-1145 DATED 2020-10-05. OPENED ELONGATED HOLE IN FUSELAGE
- [SDR A6WA202010067311](https://openairdocs.org/sdr/A6WA202010067311.md): Former · cracked · Oct 6, 2020 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER CRACKED. P/N 601R318034-3 AT FS 347.25 THAT MEASURES 2.9'' L. AIRCRAFT REMOVED FROM SERVICE. CUT OUT DAMAGED AREA OF FORMER 3.0" L, REF REO NR: 601R-52-11-2834 DATED 2020-10-05. PERFORMED HFEC INSPECTION OF CUT OUT AREA AND INNER SKIN, I
- [SDR A6WA202010057310](https://openairdocs.org/sdr/A6WA202010057310.md): Access Panel · gouged · Oct 5, 2020 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT FLAP LOWER INBOARD ACCESS PANEL 584AB GOUGED AT UPPER CENTER LEADING EDGE. GOUGE ON LT FLAP LOWER INBOARD ACCESS PANEL 584AB MEASURES 0.6125''L X 0.30''W X0.011''D. BLENDED GOUGE TO A SMOOTH CONTOUR. DEPTH NOT TO EXCEED ORIGINAL DEPTH OF 0.011'', IAW EA
- [SDR A6WA202010057309](https://openairdocs.org/sdr/A6WA202010057309.md): Skin · gouged · Oct 4, 2020 · N451AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 2 EACH MISS-DRILLED SCREWS LT FWD WING TO BODY FAIRING ATTACHED POINT (ON FUSELAGE). HOLE NR 1 LOCATED AT FS 409+71.6 AND STR 21L THAT MEASURES 0.307'' W AND 0.25'' L. HOLE NR2 LOCATED AT FS 409+70.45 AND STR 22L THAT MEASURES 0.249'' W AND 0.208'' L. AIRCR
- [SDR A6WA202010057305](https://openairdocs.org/sdr/A6WA202010057305.md): Skin · cracked · Oct 3, 2020 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL STRUCTURE ENTRY DOOR/STAIRS AFT SIDE FOUND CRACK IN SKIN AT 2ND TO TOP STEP. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PASSENGER DOOR STAIRS AFT SIDE AT 2ND STEP, REF AIR WISCONSIN SUPPLEMENT NO: 14-162 DATE OF ISSUE JULY 21, 2014. REM
- [SDR A6WA2020031147223](https://openairdocs.org/sdr/A6WA2020031147223.md): Landing Gear · malfunctioned · Mar 9, 2020 · N451AW · Cndair CL6002B19 · Nose/Tail Landing Gear
  > AFTER T/OFF ON CLIMB, RECEIVED GEAR DISAGREE AFTER 6 SECS FROM SELECTION. NLG SHOWS DOWN AND NLG DOOR OPEN. BOTH MLG SHOW UP AND LOCKED. ALSO RECEIVED NWS INOP, WOW INPUT CAUTION, WOW OUTPUT FAIL MESSAGES. RAN QRH AND STEERING MESSAGE CLEARED
- [SDR A6WA2020012247121](https://openairdocs.org/sdr/A6WA2020012247121.md): Wire Harness · not reported · Jan 20, 2020 · N451AW · Cndair CL6002B19 · Landing Gear System Wiring
  > AFTER TAKE OFF, RECEIVED A GEAR DISAGREE, NOSE GEAR REMAINED DOWN. COMPLIED WITH QRH. MANUAL GEAR EXTENSION ACCOMPLISHED, RECEIVED 3 GREEN. ON TAXI IN, RECEIVED A HYD 3 HIGH TEMP AND NWS INOPERATIVE CAUTION. COMPLIED WITH QRH. MESSAGES CLEARED. AIRCRA
- [SDR A6WA2019092346882](https://openairdocs.org/sdr/A6WA2019092346882.md): Warning System · activated · Sep 20, 2019 · N451AW · Cndair CL6002B19 · Landing Gear Position and Warning
  > NOSE DOOR OPEN (W) MSG RECEIVED WHEN PUTTING GEAR UP ON DEPARTURE GEAR DISAGREE(W) ALSO RECEIVED. RAN QRH FOR NOSE DOOR OPEN. MSG APPEARED IMMEDIATELY AFTER HANDLE MOVEMENT.
- [SDR A6WA201904106548](https://openairdocs.org/sdr/A6WA201904106548.md): Warning Message · illuminated · Apr 6, 2019 · N451AW · Cndair CL6002B19 · Engine Thrust Reverser
  > DURING CLIMB, AT APPROXIMATELY 15,000 FEET, THE FLIGHT CREW RECEIVED A RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT.
- [SDR A6WA2019022546417](https://openairdocs.org/sdr/A6WA2019022546417.md): Adc · malfunctioned · Feb 24, 2019 · N451AW · Cndair CL6002B19 · Air Data Computer
  > DURING APPROACH, THE FLIGHT CREW IDENTIFIED A AIR DATA COMPUTER 2 ISSUE (INDICATED AIRSPEED AND ALTITUDE) AND ABANDONED THE APPROACH. THE CREW COMPLETED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY AND ATTEMPTED AN APPROACH FOR THE SECOND TIME. AFTER RECE
- [SDR A6WA2018080945968](https://openairdocs.org/sdr/A6WA2018080945968.md): Bulkhead Web · cracked · Aug 6, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD ABOVE AFT CARGO DOOR, AFT OF THE TRACK WAS CRACKED. REPAIRED THE BULKHEAD WEB.
- [SDR A6WA2018080645967](https://openairdocs.org/sdr/A6WA2018080645967.md): Skin · dented · Aug 5, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP, LOWER OTBD SKIN PANEL HAD TWO DENTS. REPLACED THE FLAP SKIN PANEL IAW SRM 51-42-13
- [SDR A6WA2018080645966](https://openairdocs.org/sdr/A6WA2018080645966.md): Skin · dented · Aug 5, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP, LOWER INBD SKIN PANEL HAD MULTIPLE AREAS OF DENTS, DINGS, AND PITS. REPLACED THE FLAP SKIN IAW SRM 51-42-13.
- [SDR A6WA2018080645960](https://openairdocs.org/sdr/A6WA2018080645960.md): Beam · cracked · Aug 2, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR BEAM CUT BY BOTH DOOR ASSIST CABLE, LOWER OTBD FLANGE, AT TWO PLACES. REPLACED THE CARGO DOOR BEAM LOWER OTBD FLANGE IAW SRM 51-42-21, AND SRM 51-42-06.
- [SDR A6WA2018080645962](https://openairdocs.org/sdr/A6WA2018080645962.md): Angle · cracked · Aug 2, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM OTBD ANGLE AT LBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE.
- [SDR A6WA2018080645959](https://openairdocs.org/sdr/A6WA2018080645959.md): Strap · corroded · Aug 1, 2018 · N451AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM STRAP AT BS 559 HAD CORROSION BETWEEN RBL 27 AND THE RT FLOOR SUPPORT, IN THE CABIN. REMOVED AND REPLACED THE FLOORBEAM STRAP IAW SRM 51-42-06, 51-40-11, 53-41-43, AND 53-00-00
- [SDR A6WA2018080645958](https://openairdocs.org/sdr/A6WA2018080645958.md): Web · cracked · Aug 1, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF A CRACKED DRAG ANGLE REPAIR, AFT RISER WEB FOUND TO BE CRACKED BY THE ASSIST MOTOR YOKE. REPAIRED PAX DOOR AFT WEB RISER IAW SUPP 15-310
- [SDR A6WA2018080645956](https://openairdocs.org/sdr/A6WA2018080645956.md): Skin · dented · Aug 1, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP LOWER OTBD SKIN PANEL WAS DENTED. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-13.
- [SDR A6WA2018080645957](https://openairdocs.org/sdr/A6WA2018080645957.md): Skin · cracked · Aug 1, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > ON REMOVAL OF THE PAX DOOR AFT RISER DRAG ANGLE, THE INNER SKIN HAD A CRACK UNDER THE DRAG ANGLE SLPICE. REPAIRED PAX DOOR INNER SKIN IAW 18-225.
- [SDR A6WA2018080645964](https://openairdocs.org/sdr/A6WA2018080645964.md): Strap · damaged · Jul 30, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR FWD SEAL STRIKER REPAIR STRAP DAMAGED. REPLACED PAX DOOR FWD SEAL STRIKER REPAIR STRAP IAW SUPP 17-009.
- [SDR A6WA2018073045955](https://openairdocs.org/sdr/A6WA2018073045955.md): Skin Panel · damaged · Jul 29, 2018 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > LT INBD FLAP LOWER INBD SKIN PANEL HAS MULTIPLE AREAS WITH DAMAGE. REPLACED LT INBD FLAP LOWER INBD SKIN PANEL IAW SRM 51-42-13.
- [SDR A6WA2018073045954](https://openairdocs.org/sdr/A6WA2018073045954.md): Fitting · cracked · Jul 28, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLIGHT DECK WINDSHIELD CENTER POST LOWER LEFT FITTING CRACKED. REPLACED FITTING IAW SRM 51-42-21.
- [SDR A6WA2018073045953](https://openairdocs.org/sdr/A6WA2018073045953.md): Web · cracked · Jul 26, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR UPPER STEP WEB BELOW TOP FOLDING STEP IS CRACKED. REPAIRED IAW REO 601R-52-11-279 REV-NC.
- [SDR A6WA2018080645963](https://openairdocs.org/sdr/A6WA2018080645963.md): Drag Angle · cracked · Jul 23, 2018 · N451AW · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE WAS CRACKED. REPAIRED THE AFT DRAG ANGLE IAW REO 601R-52-11-513 REV B.
- [SDR A6WA2018072445949](https://openairdocs.org/sdr/A6WA2018072445949.md): Bracket · cracked · Jul 22, 2018 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR TRACK, LOWER AFT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
- [SDR A6WA201745241](https://openairdocs.org/sdr/A6WA201745241.md): Connector · unsecure · Aug 29, 2017 · N451AW · Cndair CL6002B19 · Light System Wiring
  > FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE FROM ROWS 9 AFT. SECURED THE EMERGENCY LIGHT CONNECTOR AT ROW 12, OPS CHECKED GOOD IAW AMM 33-51-01.
- [SDR A6WA201745084](https://openairdocs.org/sdr/A6WA201745084.md): Sign · inoperative · Jul 4, 2017 · N451AW · Cndair CL6002B19 · Emergency Lighting
  > EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51-10, OPS CHECKED GOOD.
- [SDR A6WA201644072](https://openairdocs.org/sdr/A6WA201644072.md): Bracket · broken · Jul 6, 2016 · N451AW · Cndair CL6002B19 · Nacelle/Pylon, Attach Fittings
  > LEFT NOSE COWL PDU WIRE HARNESS BRACKET BROKEN. REPLACED BRACKET IAW CMM 20-42-06.
- [SDR A6WA201644071](https://openairdocs.org/sdr/A6WA201644071.md): Stringer Clip · cracked · Jul 6, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > STRINGER CLIP BS 621 STRINGER 13L AFT SIDE IS CRACKED
- [SDR A6WA201644067](https://openairdocs.org/sdr/A6WA201644067.md): Frame · corroded · Jul 5, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 HAS CORROSION ON THE FWD SIDE BETWEEN STRINGERS 22 - 23R IN THE FWD E&E BAY. REMOVED CORROSION AND INSTALLED DOUBLERS AS REQUIRED IAW REO 601R-53-21-2733 REV-A.
- [SDR A6WA201644059](https://openairdocs.org/sdr/A6WA201644059.md): Skin · cracked · Jul 1, 2016 · N451AW · Cndair CL6002B19 · Wing, Plate/Skin
  > RT I/B L/E INNER SKIN IS CRACKED 24 INCHES FROM I/B EDGE. REPAIRED DAMAGE IAW EA AWAC-CRJ257-00423 REV-IR AND AWAC SUPPLEMENT 16-188.
- [SDR A6WA201644061](https://openairdocs.org/sdr/A6WA201644061.md): Lug · chafed · Jul 1, 2016 · N451AW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT O/B FLAP, CENTER HINGE ARM FWD ATTACH POINT, O/B LUG IS CHAFED. REPAIRED IAW REO 601R-57-53-1048 REV.
- [SDR A6WA201644058](https://openairdocs.org/sdr/A6WA201644058.md): Fitting · cracked · Jul 1, 2016 · N451AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BS 621 SEAT TRACK ATTACHMENT LBL 27 HAS CORROSION. REPAIRED ATTACH FITTING IAW EA AWAC-CRJ 253-00421 REV-IR.
- [SDR A6WA201644052](https://openairdocs.org/sdr/A6WA201644052.md): Floor Support · gouged · Jun 29, 2016 · N451AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT BETWEEN BS 559+48 AND 559+64 IS GOUGED BY THE TOILET DUMP FITTING. REPAIRED THE FLOOR SUPPORT IAW EA AWAC-CRJ253-00422 REV- IR.
- [SDR A6WA201644050](https://openairdocs.org/sdr/A6WA201644050.md): Rib · cracked · Jun 28, 2016 · N451AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > JET PIPE FAIRING 446AL FWD RIB IS CRACKED. REPAIRED THE RIB IAW CMM 78-11-00-300-810-A01.

Next page: https://openairdocs.org/aircraft/N451AW/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 = 'N451AW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N451AW/reports

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