# Service difficulty reports: N417AW A list on [N417AW](https://openairdocs.org/aircraft/N417AW.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 · 217 reports - [SDR A6WA202502118861](https://openairdocs.org/sdr/A6WA202502118861.md): Anti-Ice Valve · faulted · Feb 11, 2025 · N417AW · Cndair CL6002B19 · Engine Anti-Icing System > L COWL ANTI ICE CAUTION LIGHT IN FLIGHT. DIVERTED TO PIA. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE PER AWA AMM SUPP 10-094.OPS CHECK GOOD. PERFORMED OPERATIONAL TEST OF THE ENGINE COWL AND ANTI-ICE SYSTEM PER A - [SDR A6WA202412288848](https://openairdocs.org/sdr/A6WA202412288848.md): Warning Message · false indication · Dec 28, 2024 · N417AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > 6030 - FLAPS FAIL CAUTION MESSAGE SHOWING 0 DEGREES AT CRUISE. FLAP HANDLE POSTION WAS AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED TROUB - [SDR A6WA202310138658](https://openairdocs.org/sdr/A6WA202310138658.md): Unknown · cracked · Oct 13, 2023 · N417AW · Cndair CL6002B19 · Wing, Plate/Skin > RH DETAILED INSPECTION OF LOWER WING PLANK SPLICE JOINTS AT BL45.0 WS65.75 AND WS148.0 CONFIRMED 2ND LAYER DEFECT INDICATIONS IN FWD 2 FASTENER LOCATIONS PROCEEDING TOWARD AFT ROW OF FASTENERS. APPROXIMATELY.250". *****AIRCRAFT REMOVED FROM SERVICE******** HA - [SDR A6WA202301278450](https://openairdocs.org/sdr/A6WA202301278450.md): Floor Support · corroded · Jan 27, 2023 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > PAX DOOR AFT LOWER SILL IS CORRODE ***** AC REMOVED FROM SERVICE ***** REPAIRED PAX DOOR AFT LOWER SILL REF REO 601R-53-21-3596 REV -- DATED 2023-01-19 - [SDR A6WA202301278451](https://openairdocs.org/sdr/A6WA202301278451.md): Drain · cracked · Jan 27, 2023 · N417AW · Cndair CL6002B19 · Wing Miscellaneous Structure > L/H AFT WING DRAIN BY BOOST PUMP ATTACHMENT HOLES ARE CRACKED INSIDE HOLES **** AC REMOVED FROM SERVICE ***** REPAIRED L/H AFT WING DRAIN BY BOOST PUMP ATTACHMENT HOLES REF REO 601R-57-21-3679 REV-- 2023-01-13 - [SDR A6WA202301278449](https://openairdocs.org/sdr/A6WA202301278449.md): Frame Splice · corroded · Jan 27, 2023 · N417AW · Cndair CL6002B19 · Fuselage Main, Frame > FRAME SPLICE LOCATED AT FS 394 BETWEEN STRG 22R AND STRG 23R IS CORRODED. ****AIRCRAFT REMOVED FROM SERVICE******* REPAIRED FRAME SPLICE LOCATED AT FS 394 BETWEEN STRG 22R AND STRG 23R - [SDR A6WA2023012318439](https://openairdocs.org/sdr/A6WA2023012318439.md): Floor Support · corroded · Jan 21, 2023 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > L/H FLOOR SILL HAS CORROSION BETWEEN FS 559+80 TO FS621. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE FLOOR SILL - [SDR A6WA202301208435](https://openairdocs.org/sdr/A6WA202301208435.md): Floorbeam · corroded · Jan 20, 2023 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > LBL 27 FLOOR BEAM HAS SPOTS OF CORROSION APPROX. LOCATION FS605-FS589 *************AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED NEW FLOOR BEAM CAP FROM SUPPORT STRUCTURE AT LBL27.00 BETWEEN FS559.00+112 - FS621.00 PER CRJ-200 SRM 51-42-21, CRJ- - [SDR A6WA202301208434](https://openairdocs.org/sdr/A6WA202301208434.md): Floorbeam · corroded · Jan 20, 2023 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > RBL 27 FLOOR BEAM HAS SPOTS OF CORROSION APPROX. LOCATION FS559+80 ********AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED FLOOR BEAM SECTION RBL27 FS559-FS574 REF CRJ-200-SRM 51-42-21, CRJ-200-SRM 51-42-06, DWG 601R 31026 REV F, AND COMPLIED WITH - [SDR A6WA202301188432](https://openairdocs.org/sdr/A6WA202301188432.md): Floor Skin · corroded · Jan 18, 2023 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > R/H SIDE FLOOR SILL HAS AREAS OF CORROSION FROM FS 559+80 TO FS 621.0 *******AIRCRAFT REMOVED FROM SERVICE******** BLEND AND RESTORE FINISH - [SDR A6WA202201278082](https://openairdocs.org/sdr/A6WA202201278082.md): Anti-Ice System · false indication · Jan 27, 2022 · N417AW · Cndair CL6002B19 · Ice/Rain Protection System > ON CLIMB IN CLEAR CLOUDS RECEIVED WING ANTI-ICE DUCT WARNING MESSAGE. ANTI-ICE WAS OFF WHEN OCCURRED. ANTI-ICE SYNOPTICS SHOWED RED LEADING EDGE OF LEFT WING ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS - [SDR A6WA202102047576](https://openairdocs.org/sdr/A6WA202102047576.md): Skin · dented · Feb 3, 2021 · N417AW · Cndair CL6002B19 · Fuselage Main, Plate/Skin > DENT IN SKIN B/T FS640.0 AND FS672.20, B/T STR 26R AND STR 27R ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED DENT IN SKIN B/T 640.0 AND 672.20, B/T STR 26R AND STR 27R IAW EA#AWAC-CRJ253-01550 - [SDR A6WA202102047579](https://openairdocs.org/sdr/A6WA202102047579.md): Structure · corroded · Feb 3, 2021 · N417AW · Cndair CL6002B19 · Fuselage Main, Structure > CORROSION FOUND ON FS 310 B/T STR 26L AND STR 26R ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FS 310 LOWER SECTION AT FS 310.0 BETWEEN STR 26L AND 26R - [SDR A6WA202102047578](https://openairdocs.org/sdr/A6WA202102047578.md): Floor Support · corroded · Feb 3, 2021 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FLOOR SUPPORT L/H AT FS559.O CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT L/H AT FS559.O - [SDR A6WA202102047577](https://openairdocs.org/sdr/A6WA202102047577.md): Floor Support · corroded · Feb 3, 2021 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS559.00 FLOOR SUPPORT CORRODED BEYOND LIMITS ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED FLOOR SUPPORT AF FS559.00 - [SDR A6WA202009107284](https://openairdocs.org/sdr/A6WA202009107284.md): Windshield · cracked · Sep 8, 2020 · N417AW · Cndair CL6002B19 · Flight Compartment Windows > CAPTAIN`S WINDSHIELD CRACKED AT FL320. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN`S WINDSHIELD, IN REFERENCE TO 56-11-01 & IAW AWAC SUPP 09-047A. - [SDR A6WA2019112047012](https://openairdocs.org/sdr/A6WA2019112047012.md): Pressure Switch · malfunctioned · Nov 14, 2019 · N417AW · Cndair CL6002B19 · Airfoil Anti/De-ice System > SUPPLIMENTAL INFORMATION, AFTER DEPARTURE RECEIVED RIGHT WING ANTI ICE CAUTION MESSAGE WITH STANDBY MODE. RESET ANTI ICE AND RECEIVED CAUTION MESSAGE AFTER 1 MIN 30 SECONDS. AIRCRAFT REMOVED FROM SERVICE. R/R RIGHT HAND ANTI ICE PRESSURE SWITCH IAW AMM 30-10 O - [SDR A6WA2019080246767](https://openairdocs.org/sdr/A6WA2019080246767.md): Warning Message · illuminated · Jul 9, 2019 · N417AW · Cndair CL6002B19 · Trailing Flap Position Indicating System > AFTER TAKE-OFF, THE CREW RECEIVED A FLAP FAIL AT APPROX. 8 DEGREES. FLIGHT CONTINUED AND DECLARED AN EMERGENCY. RECEIVED FLAPS FAIL CAUTION MSG AT APROX 20,000 FEET FLAPS AT ZERO. PERFORMED FLAP RESET PROCEEDURE IAW SUP 98-18G BOX 12. FLAPS RESET. - [SDR A6WA2019022546413](https://openairdocs.org/sdr/A6WA2019022546413.md): Hinge · gouged · Feb 22, 2019 · N417AW · Cndair CL6002B19 · Fuselage, Door Hinge > PASSENGER DOOR HINGE HALF ON FUSELAGE SIDE AFT LUG IS GOUGED. REPLACED HINGE HALF IAW CRJ200 SRM 53-21-23, REO 601R-53-21-656 REV-A. - [SDR A6WA2019022146405](https://openairdocs.org/sdr/A6WA2019022146405.md): Attach Angle · cracked · Feb 20, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > AC POWER CONTROL UNIT LOWER ATTACH ANGLE IS CRACKED. REPLACED - [SDR A6WA2019022146406](https://openairdocs.org/sdr/A6WA2019022146406.md): Mount · cracked · Feb 19, 2019 · N417AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR ASSIST MOTOR OUTBD MOUNT IS CRACKED AT LOWER RADIUS. REPLACED - [SDR A6WA2019022146408](https://openairdocs.org/sdr/A6WA2019022146408.md): Floorbeam · cracked · Feb 19, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FS 280 BEAM AFT ANGLE IS CRACKED AT LBL 9 AND RBL 9. REPAIRED - [SDR A6WA2019022246409](https://openairdocs.org/sdr/A6WA2019022246409.md): Beam · worn · Feb 18, 2019 · N417AW · Cndair CL6002B19 · Cargo/Baggage Doors > CARGO DOOR LOWER O/B BEAM MEMBER 601R35050-64 HAS WEAR FROM ASSIST CABLE. REPLACED CARGO DOOR BEAM MEMBER IAW SRM51-42-06, 51-42-21. - [SDR A6WA2019022146407](https://openairdocs.org/sdr/A6WA2019022146407.md): Frame · cracked · Feb 18, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 333 FRAME STR 3L TO STR 0 IS CRACKED STARTING AT TOOLING HOLE. REPLACED - [SDR A6WA2019021846401](https://openairdocs.org/sdr/A6WA2019021846401.md): Floorbeam · corroded · Feb 15, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FS280.00 BEAM CORRODED FROM LBL9 TO RBL9. REPAIRED BEAM IAW REO 601R-53-11-926 REV-B. - [SDR A6WA2019021846402](https://openairdocs.org/sdr/A6WA2019021846402.md): Floorbeam · cracked · Feb 15, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Floor Beam > FS280.00 BEAM FWD ANGLE CRACKED AT LBL 9 AND RBL9. - [SDR A6WA2019021846403](https://openairdocs.org/sdr/A6WA2019021846403.md): Floor Panel · cracked · Feb 13, 2019 · N417AW · Cndair CL6002B19 · Fuselage Floor Panel > FWD EQUIPMENT COMPARTMENT TRU DECK CRACKED AT FS193.00, LBL30. REPAIRED TRU DECK IAW REO 601R-53-11-081 REV-NC. - [SDR A6WA2019021546394](https://openairdocs.org/sdr/A6WA2019021546394.md): Bracket · cracked · Feb 13, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > CARGO DOOR AFT BALANCE SPRING ASSY MOUNT BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-24-21, 51-42-06. - [SDR A6WA2019021546393](https://openairdocs.org/sdr/A6WA2019021546393.md): Angle · cracked · Feb 12, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > CARGO DOOR BEAM FWD ATTACH ANGLE CRACKED. REPLACED ANGLE IAW CRJ200 SRM 51-42-21, 51-40-11, TR51-42. - [SDR A6WA2019021146390](https://openairdocs.org/sdr/A6WA2019021146390.md): Stiffener · cracked · Feb 9, 2019 · N417AW · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle > RIGHT EXHAUST NOZZLE FAIRING HAS A CRACKED STIFFENER THIRD FROM THE FWD END. REPLACED STIFFENER IAW CMM 21-42-06. - [SDR A6WA2019021146389](https://openairdocs.org/sdr/A6WA2019021146389.md): Bracket · cracked · Feb 9, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > RIGHT MLG WHEEL WELL HYDRAULIC LINE Z BRACKET CRACKED. REPLACE BRACKET IAW SRM 51-42-06. - [SDR A6WA2019021146382](https://openairdocs.org/sdr/A6WA2019021146382.md): Landing · cracked · Feb 6, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LT TRU PANEL LAND CRACKED AT AFT DOOR LATCH CUTOUT. REPAIRED. - [SDR A6WA2019021146385](https://openairdocs.org/sdr/A6WA2019021146385.md): Post · cracked · Feb 6, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Structure > NLG WHEEL WELL FS 202.75 RBL 9 VERTICAL POST UPPER CLIP CRACKED. REPLACED - [SDR A6WA2019021146380](https://openairdocs.org/sdr/A6WA2019021146380.md): Bracket · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR LOWER BRACKET PULLEY MOUNT CRACKED. REPLACED. - [SDR A6WA2019021146379](https://openairdocs.org/sdr/A6WA2019021146379.md): Fitting · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > WINDSHIELD CO-PILOT SIDE POST OUTBD CLIP CRACKED. REPLACED. - [SDR A6WA2019021146381](https://openairdocs.org/sdr/A6WA2019021146381.md): Drag Angle · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Passenger/Crew Doors > PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED. - [SDR A6WA2019021146376](https://openairdocs.org/sdr/A6WA2019021146376.md): Bracket · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings > FS 509 LBL 47 FAIRING BRACKET CRACKED. REPLACED. - [SDR A6WA2019021146378](https://openairdocs.org/sdr/A6WA2019021146378.md): Fitting · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > WINDSHIELD PILOT SIDE POST OUTBD FITTING CRACKED. REPLACED. - [SDR A6WA2019021146377](https://openairdocs.org/sdr/A6WA2019021146377.md): Bracket · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > RT MLG WHEEL WELL TRANSDUCER HAT BRACKET CRACKED. REPLACED. - [SDR A6WA2019020846375](https://openairdocs.org/sdr/A6WA2019020846375.md): Fitting · cracked · Feb 5, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > BATHTUB FITTING AT RBL 9 FS 461 IS CRACKED. REPLACED - [SDR A6WA2019020646364](https://openairdocs.org/sdr/A6WA2019020646364.md): Bracket · cracked · Feb 4, 2019 · N417AW · Cndair CL6002B19 · Aerodynamic Fairings > FS449.85, LBL FAIRING BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06. - [SDR A6WA2019021146384](https://openairdocs.org/sdr/A6WA2019021146384.md): Frame · cracked · Feb 4, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Frame > FS 605 FRAME AT STR 9L CRACKED. REPAIRED. - [SDR A6WA2019020646362](https://openairdocs.org/sdr/A6WA2019020646362.md): Bracket · cracked · Feb 4, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > FS 461.5 FAIRING BRACKET AT LBL 47 CRACKED. REPLACED BRACKET IAW SRM 51-42-06. - [SDR A6WA2019020646363](https://openairdocs.org/sdr/A6WA2019020646363.md): Bracket · cracked · Feb 4, 2019 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach Fittings > FS 469, LBL FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW SRM 51-42-06. - [SDR A6WA2019021146383](https://openairdocs.org/sdr/A6WA2019021146383.md): Channel · cracked · Feb 3, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FWD CARGO DOOR TRACK LOWER U-CHANNEL CRACKED. REPLACED. - [SDR A6WA2019020646369](https://openairdocs.org/sdr/A6WA2019020646369.md): Support Bracket · cracked · Feb 3, 2019 · N417AW · Cndair CL6002B19 · Aerodynamic Fairings > FS449.85, RBL 47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06. - [SDR A6WA2019020646367](https://openairdocs.org/sdr/A6WA2019020646367.md): Support Bracket · cracked · Feb 3, 2019 · N417AW · Cndair CL6002B19 · Aerodynamic Fairings > FS477, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ200 SRM 51-42-06. - [SDR A6WA2019020646368](https://openairdocs.org/sdr/A6WA2019020646368.md): Support Bracket · cracked · Feb 3, 2019 · N417AW · Cndair CL6002B19 · Aerodynamic Fairings > FS469, RBL47 FAIRING SUPPORT BRACKET CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-42-06. - [SDR A6WA2019020646366](https://openairdocs.org/sdr/A6WA2019020646366.md): Angle · cracked · Jan 31, 2019 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure > FS280, STR 3L I/B AND O/B CLIPS CRACKED. REPLACED CLIPS IAW CRJ 200 SRM 51-42-06, 51-42-21. - [SDR A6WA2019020646365](https://openairdocs.org/sdr/A6WA2019020646365.md): Attach Bracket · cracked · Jan 30, 2019 · N417AW · Cndair CL6002B19 · Wing, Attach Fittings > RIGHT WING MID L/E I/B ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW CRJ 200 SRM 51-41-02. Next page: https://openairdocs.org/aircraft/N417AW/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 = 'N417AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N417AW/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.