# Service difficulty reports: N455AW A list on [N455AW](https://openairdocs.org/aircraft/N455AW.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 · 202 reports - [SDR A6WA202607178900](https://openairdocs.org/sdr/A6WA202607178900.md): Warning Message · false activation · Jul 17, 2026 · N455AW · Cndair CL6002B19 · Airfoil Anti/De-ice System > DURING CLIMB THROUGH FL210 IN ICE CONDITIONS RECEIVED BLEED AIR DUCT WARNING FOR L FUSELAGE DUCT RAN QRH AND RETURNED TO IWA AIRCRAFT REMOVED FROM SERVICE, INSPECTED LT WING FUSELAGE A-ICE DUCTS AND LOOPS IN LT WHEEL WELL AND AFT EQUIPMENT BAY NO DEFECTS NOTE - [SDR A6WA202606058892](https://openairdocs.org/sdr/A6WA202606058892.md): Ballast · odor · Jun 5, 2026 · N455AW · Cndair CL6002B19 · Passenger Compartment Lighting > INTERMITTENT SMELL OF HOT WIRING BETWEEN ROWS 8-12 ON THE GRD. AIRCRAFT REMOVED FROM SERVICE. R & R LIGHT BALLAST AT ROW 10AB IAW AMM 33-21-04 AND UNUSUAL ODOR. OPS CHKD GOOD. - [SDR A6WA202503278864](https://openairdocs.org/sdr/A6WA202503278864.md): Sensor · malfunctioned · Mar 27, 2025 · N455AW · Cndair CL6002B19 · Landing Gear Position and Warning > NOSE GEAR WOULD NOT RETRACT, ASSOCIATED GEAR DISAGREE AND DOOR WARNING MSGS. HAPPENED ON CLIMB OUT WHEN SELECTING GEAR TO RETRACT AFTER 6 SECONDS. HYD PUMPS IN AUTO. UNDER 150 KNOTS. LANDING WEIGHTS 46,800 IBS. AIRCRAFT REMOVED FROM SERVICE, INSTALLED DOWN L - [SDR A6WA202502018856](https://openairdocs.org/sdr/A6WA202502018856.md): Escape Rope · bound · Feb 1, 2025 · N455AW · Cndair CL6002B19 · Emergency Equipment > 6041 - EMER ESCAPE ROPE IMPROPERLY ZIP TIED. UNABLE FOR USE. EMER EGRESS ROPE WAS ZIPTIED TO IT'S SELF. THE ROPE WOULD NOT BE ABLE TO DEPLOY IN AN EMERG. AIRCRAFT REMOVED FROM SERVICE. CUT ZIP TIED AND RE-STOWED LH AND RH EMERGENCY STOW LINE IAW AWA SUPP - [SDR A6WA202501098852](https://openairdocs.org/sdr/A6WA202501098852.md): Pcu · faulted · Jan 9, 2025 · N455AW · Cndair CL6002B19 · Flight Control System > AIRCRAFT FLUTTERS AT AIRSPEED ABOVE 280KIAS. EXPERIENCED FLUTTER IN AIRFRAME ON CLIMB THROUGH 10000FT. FLUTTER DISAPPEARED AFTER LEVELING OFF AND SLOWING BELOW 250KIAS AT 14,000FT. NO FLUTTER ON DECENT OR APPROACH. AIRCRAFT REMOVED FROM SERVICE. R & R ELE - [SDR A6WA202408288799](https://openairdocs.org/sdr/A6WA202408288799.md): Priority Valve · faulted · Aug 28, 2024 · N455AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > 455 ORD-AZO EXPERIENCED A GEAR DISAGREE WHILE DEPARTING ORD. THE CREW RAN THE QRH AND ELECTED TO RETURN TO ORD. AN EMERGENCY WAS DECLARED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF NOSE DOOR IAW AMM 32-22-01 OPS CHECK GOOD. RETRIEVED PSUE CODES F - [SDR A6WA202407248780](https://openairdocs.org/sdr/A6WA202407248780.md): Control Unit · malfunctioned · Jul 24, 2024 · N455AW · Cndair CL6002B19 · Electrical Power System > AFTER ROTATION, LOUD BUZZING NOISE. ADG DEPLOYED ON ITS OWN. LANDING NOT OVERWEIGHT,, AIR-RETURN TO MKE. AIRCRAFT REMOVED FROM SERVICE. R/R ADG AUTO DEPLOY CONTROL PANEL IAW AMM 24-23-15. OPS CHECK GOOD AT THIS TIME. - [SDR A6WA202406128764](https://openairdocs.org/sdr/A6WA202406128764.md): Oil System · leaking · Jun 12, 2024 · N455AW · Cndair CL6002B19 · Turbine Engine Oil System > IN CLIMB, NOTICED L ENG OIL PRESSURE FLUCTUATING. RECEIVED L OIL PRESS WARN MSG. C/W QRH. DID NOT REQ ENG SHUT DOWN. MSG CLEARED AT IDLE. OIL PRESSURE WAS FLUCTUATING BETWEEN 27-32 AT IDLE AND WARNING CLEARED. OIL TEMP NORMAL ENTIRE TIME. DURING WALK AROUND F - [SDR A6WA202404118730](https://openairdocs.org/sdr/A6WA202404118730.md): Yoke · unknown · Apr 11, 2024 · N455AW · Cndair CL6002B19 · Control Column Section > YOKE HAS SLACK IN THE NEUTRAL POSITION WHEN BANKING IN FLT, USING BOTH YOKES, MORE PRONOUNCED IN LEFT BANK, HAPPENS WITH FLAPS IN ANY POSITION. FEELS NORMAL ON THE GRD. NO BINDING FELT. AIRCRAFT REMOVED FROM SERVICE. OPEN - [SDR A6WA202306098628](https://openairdocs.org/sdr/A6WA202306098628.md): Unknown · unknown · Jun 9, 2023 · N455AW · Cndair CL6002B19 · Landing Gear Retraction/Extension System > AFTER SELECTING GEAR UP, RECEIVED NOSE DOOR OPEN WARNING AND GEAR DISAG WARNING. CW QRH MESSAGES CLEARED. NLG SHOWED GREEN DURING EVENT. MANUAL RELEASE NOT USED. *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED NOSEWHEEL CENTERING PROX SENS - [SDR A6WA2023013038427](https://openairdocs.org/sdr/A6WA2023013038427.md): Skin · gouged · Jan 3, 2023 · N455AW · Cndair CL6002B19 · Cargo/Baggage Doors > DURING OVERNIGHT RON MX, INSPECTION DISCOVERED DAMAGE TO THE CARGO DOOR OUTER SKIN UPPER EDGE FROM INCORRECT SCREWS INSTALLED IN THE CARGO BAY LINERS. AIRCRAFT REMOVED FROM SERVICE. PERMANENT REPAIR PERFORMED PER REO 601R-52-31-396. INCORRECT SCREWS REMOVED - [SDR A6WA202211128376](https://openairdocs.org/sdr/A6WA202211128376.md): Stringer · cracked · Nov 12, 2022 · N455AW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > STRINGER 4L AT FS379.00 CRACKED. AIRCRAFT REMOVED FROM SERVICE, REPAIRED PER EA AWACCRJ253-10905 - [SDR A6WA202211128378](https://openairdocs.org/sdr/A6WA202211128378.md): Floorbeam · corroded · Nov 12, 2022 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FLOOR BEAM IS CORRODED AT FS559.0, RBL 27. AIRCRAFT REMOVED FROM SERVICE, BLENDED AND REMOVED CORROSION. REPAIRED PER EA AWAC253-01907 - [SDR A6WA202211098374](https://openairdocs.org/sdr/A6WA202211098374.md): Tip Cap · damaged · Nov 9, 2022 · N455AW · Cndair CL6002B19 · Horizontal Stabilizer Structure > LH HORIZONTAL STAB TIP STRUCTURE HAS (5 TOTAL) ELONGATED SCREW HOLES. AIRCRAFT REMOVED FROM SERVICE, REPAIRED PER EA 105-2022-010 - [SDR A6WA202211088370](https://openairdocs.org/sdr/A6WA202211088370.md): Angle · cracked · Nov 8, 2022 · N455AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings > ANGLE STRUCTURE CRACKED AT RH MLG BAY WEB, FORWARD, OUTBOARD SIDE. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED ANGLE - [SDR A6WA202211078377](https://openairdocs.org/sdr/A6WA202211078377.md): Access Panel · corroded · Nov 7, 2022 · N455AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > PITTING CORROSION ON LH FORWARD TRUNNION ACCESS PANEL. AIRCRAFT REMOVED FROM SERVICE. REPLACED - [SDR A6WA202211068375](https://openairdocs.org/sdr/A6WA202211068375.md): Frame · corroded · Nov 6, 2022 · N455AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR INTERNAL FRAME STRUCTURE AT FS 327.763 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE, REPLACED PAX DOOR INTERNAL FRAME. - [SDR A6WA202201268081](https://openairdocs.org/sdr/A6WA202201268081.md): None · none · Jan 22, 2022 · N455AW · Cndair CL6002B19 · Fuel Transfer Valve > DURING CRUISE @ 15000', NOTICED APU SOV OPEN AND ECU FAIL STATUS MESSAGES ON ED 2. AIR RETURN TO IAD. ***AIRCRAFT REMOVED FROM SERVICE*** INTEROGATED APU ECU FOUND NO LRU FALURES AND PREV CODES INDICATE DOOR ISSUES ONLY. CLEARED CODES AND CW OPERATIONAL CH - [SDR A6WA202201048047](https://openairdocs.org/sdr/A6WA202201048047.md): None · none · Dec 31, 2021 · N455AW · Cndair CL6002B19 · Air Conditioning System > DISPLAY COOL MESSAGE IN FLIGHT. C/W QRH MESSAGE REMAINS. ***AIRCRAFT REMOVED FROM SERVICE*** FOUND DISPLAY COOLING DUCT DETACHED FROM PLENUM UNDER PILOTS DISPLAYS. RE SECURED DUCT IAW AMM 21-24-22 OPERATIONAL TEST IS GOOD. - [SDR A6WA202112208030](https://openairdocs.org/sdr/A6WA202112208030.md): None · none · Dec 18, 2021 · N455AW · Cndair CL6002B19 · Engine (Turbine/Turboprop) > DURING DECENT RIGHT ENGINE BECAME UNRESPONSIVE AT LOW TO MID POWER SETTING. WAS ABLE TO SHUT DOWN ENGINE WITH THROTTLE QUADRENT. NO EICAS MSGS PRESENT. ***AIRCRAFT REMOVED FROM SERVICE*** R/R #2 ENGINE IAW MAINTENANCE TASK CARD 000-71-400-002AW TASK CARD 00 - [SDR A6WA202107067812](https://openairdocs.org/sdr/A6WA202107067812.md): Warning Message · illuminated · Jul 5, 2021 · N455AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > RECEVED FLAP FAIL CAUTION AT ZERO DEGREES. DECLARED EMERG. SMOOTH UNEVENTFUL LANDING MAX BTMS 7. PERFORMED FLAP RESET PROCEEDURE IAW AWAC SUP 98-018I BOX 12. FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REPLACED RH BPSU REF AMM 27-51-10 FECU ABORTS BPSU TEST - [SDR A6WA202107067815](https://openairdocs.org/sdr/A6WA202107067815.md): Warning Message · illuminated · Jul 5, 2021 · N455AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > RECEIVED FLAP FAIL CAUTION ON CLIMB OUT OF ORD WITH FLAPS AT ZERO RETURNED TO ORD FOR UNEVENTFUL LANDING AFTER C/W QRH. NOTE FLAPS WERE ON MEL AT THE TIME. AIRCRAFT REMOVED FROM SERVICE. REPLACED RH BPSU REF AMM 27-51-10 FECU ABORTS BPSU TEST. - [SDR A6WA202104027733](https://openairdocs.org/sdr/A6WA202104027733.md): Bpsu · faulted · Mar 27, 2021 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAPS FAIL MESSAGE AT 30 THOUSAND FT.CREW REPORTED AFTER ENCOUNTERING MODERATE TURBULENCE OVER MUSCLE SHOALS VOR WHILE IN CRUISE FLIGHT, A FLAPS FAILURE OCCURRED AT 0 DEGREES. CAPTAIN STATED HE WILL DECLARE AN EMERGENCY WHILE ON ARRIVAL TO ORD. FLIGHT IS CONTI - [SDR A6WA202103307733](https://openairdocs.org/sdr/A6WA202103307733.md): Flap System · failed · Mar 27, 2021 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAPS FAIL MESSAGE AT 30 THOUSAND FT.CREW REPORTED AFTER ENCOUNTERING MODERATE TURBULENCE OVER MUSCLE SHOALS VOR WHILE IN CRUISE FLIGHT, A FLAPS FAILURE OCCURRED AT 0 DEGREES. CAPTAIN STATED HE WILL DECLARE AN EMERGENCY WHILE ON ARRIVAL TO ORD. FLIGHT IS CONTI - [SDR A6WA202012117459](https://openairdocs.org/sdr/A6WA202012117459.md): Flap System · out of tolerance · Dec 11, 2020 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAPS FAIL CAUTION AT 0 DEG DURING CRUISE AT FL340. AFTER NORMAL LANDING, BTMS TEMP NR 3 BRAKE - 2. PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPP 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. FOUND FLAP BPSU LEFT - [SDR A6WA202011307434](https://openairdocs.org/sdr/A6WA202011307434.md): Ecu · malfunctioned · Nov 28, 2020 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > DURING CLIMB OUT AT FLAP RETRACTION ALTITUDE FLAP FAILED AT 6 DEGREES. LAST GOOD POSITION 8 DEGREES, RETRACTING FROM 8 TO ZERO AND NO OTHER INDICATIONS. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT, IAW FIM 27-50-00. DURING TSING FECU FAILED SELF TEST. REMO - [SDR A6WA202012017436](https://openairdocs.org/sdr/A6WA202012017436.md): Pdu · fault message · Nov 25, 2020 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Actuator > ON FINAL FLAPS FAILED AT 8 DEGREES. WE WENT AROUND, CLIMBED TO 10,000' COMPLIED WITH QRH AND RETURNED FOR LANDING. NO BRACE OR EMERGENCY DECLARED. AIRCRAFT REMOVED FROM SERVICE. INTERRROGATED THE FECU, IAW FIM 27-50. FOUND NUMEROUS FAULT CODES FOR THE PDU - [SDR A6WA202011117406](https://openairdocs.org/sdr/A6WA202011117406.md): Bpsu · failed · Nov 8, 2020 · N455AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > CREW RECEIVED FLAP FAIL ON APPROACH INTO ORD AT 0. CREW BROKE OFF APPROACH AND ARE NOW GETTING READY GET BACK ON FINAL. FLAPS FAIL CAUTION MESSAGE WHEN FLAPS WERE SELECTED ZERO TO 8 DEG IN FLIGHT. FLAPS FAILED AT ZERO DEGREES PEAK BTMS 6,4,9,7. QRH WAS C/W - [SDR A6WA202010267363](https://openairdocs.org/sdr/A6WA202010267363.md): Flap System · malfunctioned · Oct 26, 2020 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAP FAIL CAUTION MESSAGE WITH FLAPS ZERO AT FINAL APPROACH. PERFORMED FLAP RESET PROCEDURE, IAW AWAC SUPPLEMENT 98-18I BOX 11, FLAPS RESET. PLACARDED AND PLACED FLAPS ON MEL. AIRCRAFT REMOVED FROM SERVICE. INTERROGATED FECU, TROUBLESHOOT PER FIM 27-50-00, - [SDR A6WA202009297299](https://openairdocs.org/sdr/A6WA202009297299.md): Seat Track · corroded · Sep 27, 2020 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > CLEANED LT & RT SEAT TRACKS FS 424 & FS 559. RT HAND SEAT TRACK RBL 9 CORRODED AND FOUND TO BE OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK, IAW REO 601R-53-00-764. - [SDR A6WA202009297298](https://openairdocs.org/sdr/A6WA202009297298.md): Floorbeam · corroded · Sep 27, 2020 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > REMOVED NUTPLATE AND FOUND AREA HAD CORROSION OUT OF LIMITS ON FLOOR BEAM AT RBL 9 STA FS 572, IAW SRM53-61-13. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR BEAM, IAW DRAWING 601R35031. - [SDR A6WA202009177286](https://openairdocs.org/sdr/A6WA202009177286.md): Proximity Sensor · out of adjust · Sep 15, 2020 · N455AW · Cndair CL6002B19 · Landing Gear Position and Warning > GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING RT MAIN DID NOT RETRACT SELECTING 3B AND 2B ON. RECEIVED 3 GREEN AFTER SELECTING MANUAL RELEASE. MSG APPEARED WITH IN 6 SECOND OF SELECTING GEAR UP WITH LT MAIN AND NOSE AMBER AND RT MAIN RED. AIRCRAFT REMOVED - [SDR A6WA2020031647230](https://openairdocs.org/sdr/A6WA2020031647230.md): Pump · malfunctioned · Mar 14, 2020 · N455AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main > RH MLG DISAGREE ON CLIMB AFTER GEAR SELECTED UP. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED #3A HYD PUMP PER AMM 29-12-03 OPS/LEAK CHECK GOOD PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION PER AMM 32-30-00 OPS CHECK GOOD. NO DEF - [SDR A6WA2019012146292](https://openairdocs.org/sdr/A6WA2019012146292.md): Warning System · false activation · Jan 17, 2019 · N455AW · Cndair CL6002B19 · Engine Thrust Reverser > LEFT THRUST REVERSER UNLOCK MESSAGE INFLIGHT. THRUST REVERSER DID NOT DEPLOY. CW QRH. - [SDR A6WA2018112546169](https://openairdocs.org/sdr/A6WA2018112546169.md): Bulkhead · cracked · Nov 20, 2018 · N455AW · Cndair CL6002B19 · Fuselage Main, Bulkhead > INDICATION NOTED AT FS 621.00 REAR PRESSURE BULKHEAD FWD FACE AT LBL36.0, WL 79.30 - 80.30 1" LONG AND 100% FULL SCREEN HEIGHT, FAILING NDT. REPAIRED FS 621.00 REAR PREASURE BULKHEAD IAW REO 601R-53-61-1240 REV D AND 601R-53-61-6775 REV-. - [SDR A6WA2018112146168](https://openairdocs.org/sdr/A6WA2018112146168.md): Skin · dented · Nov 20, 2018 · N455AW · Cndair CL6002B19 · Trailing Edge Flaps > L/H INBOARD FLAP HAS APPROX. 1" X 1" DENT BETWEEN W.S.47.61 AND W.S.56.30 (LOWER SIDE). REPAIRED L/H INBD FLAP LOWER SKIN IAW EA# AWAC-CRJ257-01096. - [SDR A6WA2018111946166](https://openairdocs.org/sdr/A6WA2018111946166.md): Channel · cracked · Nov 18, 2018 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CHANNEL BETWEEN F.S.621.00 AND F.S.625.30 AT STGR 13L OUTBD OF LBL36.2 IS CRACKED. - [SDR A6WA2018111446157](https://openairdocs.org/sdr/A6WA2018111446157.md): Seat Track · corroded · Nov 9, 2018 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > L/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S.559+64 TO F.S.559+80. REMOVED SIDE SEAT RAIL, FABRICATED NEW SERVICABLE SIDE SEAT RAIL AND INSTALLED IAW BOMBARDIER REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR A6WA2018111246157](https://openairdocs.org/sdr/A6WA2018111246157.md): Seat Track · corroded · Nov 9, 2018 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LT SIDE SEAT RAIL IS CORRODED BETWEEN FS 559+64 TO FS 559+80. REMOVED SIDE SEAT RAIL, FABRICATED NEW SERVICEABLE SIDE SEAT RAIL AND INSTALLED IAW REO 601R-53-00-055 REV C DATED 2017-03-21. - [SDR A6WA2018111446158](https://openairdocs.org/sdr/A6WA2018111446158.md): Seat Track · corroded · Nov 8, 2018 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LBL9 SEAT RAIL IS CORRODED BETWEEN F.S.364 TO F.S.379. REMOVED CORRODED SEAT RAIL AND INSTALLED NEW SERVICABLE SEAT RAIL IAW CRJ 200 AMM 53-01-11-400-802. - [SDR A6WA2018111246158](https://openairdocs.org/sdr/A6WA2018111246158.md): Seat Track · corroded · Nov 8, 2018 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > LBL9 SEAT RAIL IS CORRODED BETWEEN FS 364 TO FS 379. REMOVED CORRODED SEAT RAIL AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW AMM 53-01-11-400-802. - [SDR A6WA2018111246155](https://openairdocs.org/sdr/A6WA2018111246155.md): Seat Track · corroded · Nov 7, 2018 · N455AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings > RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 364 TO FS 409. REMOVED CORRODED SEAT RAIL FROM RBL9 BETWEEN FS 364 TO FS 409 AND INSTALLED NEW SERVICEABLE SEAT RAIL IAW REO 601R-53-00-485 REV C DATED 2017-12-18 AND AMM 53-01-11-400-802. - [SDR A6WA2017110945405](https://openairdocs.org/sdr/A6WA2017110945405.md): Inverter · inoperative · Nov 8, 2017 · N455AW · Cndair CL6002B19 · Emergency Lighting > DURING AN ACCEPTANCE CHECK, CREW REPORTED THE RIGHT OVERWING EXIT EMERGENCY SIGN WAS INOPERATIVE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTS INVERTER IAW AMM 33-51-07, OPS CHECKED GOOD. - [SDR A6WA201745392](https://openairdocs.org/sdr/A6WA201745392.md): Inverter · failed · Nov 2, 2017 · N455AW · Cndair CL6002B19 · Emergency Lighting > FLOOR EMERGENCY EXIT SIGN AT SEAT 8D INOPERATIVE. R & R THE INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD. - [SDR A6WA2017021544790](https://openairdocs.org/sdr/A6WA2017021544790.md): O-Ring · leaking · Feb 10, 2017 · N455AW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main > IN CRUISE FLIGHT RECEIVED HYD 3 LOW PRESS CTN MESSAGE, HYD 3 QUANTITY 5 %, HYD 3 PRESS 2000. COMPLIED WITH QRH, HYD 3 B ACMP TURNED ON. UPON LANDING HYD 3 QUANTITY 5% AND PRESSURE 0. INSPECTED AND FOUND HYD PUMP 3A BALL ATTENUATOR LEAKING. REMOVED AND REPLACE - [SDR A6WA201744770](https://openairdocs.org/sdr/A6WA201744770.md): Flap · malfunctioned · Jan 26, 2017 · N455AW · Cndair CL6002B19 · Trailing Edge Flap Control System > FLAP FAIL CAUTION MESSAGE INFLIGHT FAILED AT ZERO DEGREES. PERFORMED FLAP REST PROCEDURES IAW SUP 98-018G. FLAPS RESET. - [SDR A6WA2016102644521](https://openairdocs.org/sdr/A6WA2016102644521.md): Angle · corroded · Oct 24, 2016 · N455AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > RIGHT WINDSCREEN SUPPORT ANGLE AT BS 349, LBL 27-36 IS CORRODED - [SDR A6WA201644518](https://openairdocs.org/sdr/A6WA201644518.md): Frame · corroded · Oct 23, 2016 · N455AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME 333 HAS CORROSION ON THE FWD SIDE BETWEEN STR 23R AND 22R. - [SDR A6WA201644516](https://openairdocs.org/sdr/A6WA201644516.md): Floorbeam · corroded · Oct 23, 2016 · N455AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > CARGO FLOORBEAM AT FS 559+80 BETWEEN RBL9 AND LBL9 CORRODED. REPAIRED. - [SDR A6WA201644517](https://openairdocs.org/sdr/A6WA201644517.md): Frame · cracked · Oct 22, 2016 · N455AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME FS 333 CRACKED JUST I/B OF STR 1L. Next page: https://openairdocs.org/aircraft/N455AW/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 = 'N455AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N455AW/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.