N416AW
Service difficulty reports · 183
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N416AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N416AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR A6WA202512038873Actuator · malfunctionedRECEIVED FLAPS FAIL WHEN SELECTING FLAPS FROM 8 TO 20. IT FAILED AT 8. C/W QRH. AIRSPEED 180 KNOTS WHEN FAILED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 98-018I BOX 12. FLAPS RESET. REF 357078-1 FOR MEL REF 357077-4 PERFORMED FLAP FAIL RESET PROCEDURE. PSDR A6WA202409058806Control Unit · faultedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. AIRCRAFT REMOVED FROM SERVICE R&R THE FECU IAW AMM 27-51-05. OPS CHECK GOOD. REMOVED PLACARD AND REMOVED FROM MEL. SDR A6WA202409058804Control Unit · failedFLAPS FAIL CAUT MESSAGE FLAPS FAILED AT 16K FT 250 KNOTS FAILED IN THE ZERO DEGREE POSITION. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18I BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** R&R THE FECU IAW SDR A6WA202401198702Landing Gear · warning messageAFTER T/O RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE. RAN QRH PROCEDURE MSG'S WENT AWAY. LANDING WIGHT 44, 600LBS, SMOOTH NORMAL LANDING. MSG APPEARED AFTER 2 SECONDS SELECTING GEAR. AIRCRAFT REMOVED FROM SERVICE PERFORMED GEAR SWING IAW AMM 32-30-00 OPS CHSDR A6WA202310208661Sensor · unknownPERSISTENT ANTI-ICE DUCT WARNING MESSAGE. RH FUSELAGE SHOWED RED ON THE SYNOPTIC PAGE. C/W QRH AND RETURNED TO YUL. *********AIRCRAFT REMOVED FROM SERVICE********* T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.SDR A6WA202310208660Sensor · unknownANTI ICE DUCT WARN MSG ******AIRCRAFT REMOVED FROM SERVICE******** T/S PER MTCM 19-149. REPLACED LOOP A46WK PER AMM 36-21-04. OPS CHECK GOOD.SDR A6WA202212138409Strap · out of positionPREVIOUS REPAIR ON PASSENGER DOOR FRAME 310 .0 DAMAGE FROM INPROPER DOOR CLOSING. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW REPAIR STRAP 601R-53-22-033-1 IAW REO 601R-53-22-033 REV -D DATE 2014/02/17 REPAIR TYPE 1 FOR FASTENER CALL OUTSDR A6WA202212138410Skin · noneTEMPORARY REPAIR TO FUSELAGE SKIN AT BS 257.75, S15L. DENT MEASURES 0.55" X 0.4" X 0.004" DEPTH - HAS BEEN COMPLIED WITH IAW EA AWAC-CRJ253-01543. PERFORMED PERMANENT REPAIR AS REQUIRED ****AIRCRAFT REMOVED FROM SERVICE**** COMPLIED WITH REO 601R-53-11-3811 SDR A6WA202212098403Floor Support · corrodedR/H PRESSURE FLOOR SILL HAS CORROSION FROM FS 513 TO FS 559. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PRESSURE FLOOR SILL REF REO 601R-53-41-3104 REV -.SDR A6WA202212088398Floor Support · corrodedL/H PRESSURE FLOOR SILL CORRODED FROM FS 439 TO 529. AIRCRAFT REMOVED FROM SERVICE. REPAIRED CORRODED AREA IAW REO 601R-53-41-3103 REV -.SDR A6WA202212078397Skin · dentedFUSELAGE DENTED AT BS 605 S21L-22L. AIRCRAFT REMOVED FROM SERVICE. REPAIRED THE SKIN IAW REO 601R-53-61-7913, REV -.SDR A6WA202212068396Rib · crackedUPON REMOVAL OF THE INBOARD FLAP SEAL ON THE L/H INBOARD FLAP, A CRACK WAS FOUND ON THE FWD CHERRYMAX HOLE.
***AIRCRAFT REMOVED FROM SERVICE *****
REMOVED AND INSTALLED NEW RIB AT L/H INBOARD FLAP AS PER REO 601R-57-52-2472 REV -- DATED 2022-11-29SDR A6WA202212028395Seat Track · corroded9EA LH PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION (MARKED)
****AIRCRAFT REMOVED FROM SERVICE *****
REPLACED PASSENGER SEAT STRUCTURE REF CRJ200 B/E AEROSPACE, 926-DH124A & 926-DH224A SERIES, CMM 25-26-95SDR A6WA202212028394Seat · corrodedRIGHT PASSENGER SEATS THE STRUCTURE HAS EVIDENCE OF CORROSION. AIRCRAFT REMOVED FROM SERVICE. REPLACED THE SEAT STRUCTURE IAW 926-DH124A & 926-DH224A SERIES, CMM 25-26-95.SDR A6WA202211298392Skin · dentedLEFT WING INBD FLAP HAS A DENT INBD BOTTOM SIDE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00, REPAIR -3, AND SRM 51-23-00.SDR A6WA202211268391Vane · chafedRIGHT WING INBOARD FLAP THE FLAP VANE CHAFING ON THE TOP INBOAD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE RT WING INBOARD FLAP VANE REF REO 601R-57-52-2469 REV-.SDR A6WA202211268388Vane · chafedLEFT WING INBOARD FLAP THE FLAP VANE IS CHAFFED ON THE TOP INBOARD TRAILING EDGE. ACFT REMOVED FROM SERVICE. REPAIRED THE LT WING INBOARD FLAP VANE IAW REO 601R-57-52-2469 REV-.SDR A6WA202211258387Strap · corrodedLEFT FLOOR STRAP A BS 559 BETWEEN LBL 47 AND LBL 27 HAD CORROSION. ACFT REMOVED FROM SERVICE. REPLACE THE STRAP.SDR A6WA202201228079Idg · faultedIN FLIGHT RECEIVED GEN 1 CAUTION MESSAGE (APU WAS ON MEL), F/O SMELLED BURNED PLASTIC MOMENTARILY C/W QRH GEN 1 MESSAGE PERSISTED. TURNED GEN 1 TO OFF/RESET. MESSAGES RECEIVED: L WINDSHIELD & L WINDOW CAUTION, CW QRH MESSAGES CLEARED. ***AIRCRAFT REMOVED FRSDR A6WA202103127712Reservoir · malfunctionedOPEN WARNING MESSAGE. CW QRH. ON HYD SYNOPTIC PAGE, #3 SYS SHOWED 300PSI, 70% QUANTITY AND BOTH HYD PUMP OFF. SYS 3 HYD SWITCHES SET FOR TAKEOFF. WITH FLAPS SET TO 8D DEGREES. PUMP CB'S WERE IN. AT GATE, QUANTITY SHOWS 70%. NO OBVIOUS SIGNS OF LEAKS NOTESDR A6WA202101047509Skin · crackedFS 220 RIGHT SIDE EXTERNAL SKIN CRACKED AFT OF NOSE GEAR CUT OUT RADIUS. AIRCRAFT REMOVED FROM SERVICE. REPAIRED FUSELAGE EXTERNAL SKIN FS 220.00 RIGHT SIDE AFT OF NOSE GEAR CUT OUT, IAW MHI RJ AVIATION REO 601R-53-11-3647.SDR A6WA202012237495Structure · corrodedT-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621 IS CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED T-CAP EXTRUSION ON LBL 27, FS 559+118 TO FS 621.SDR A6WA202012187467Seat Track · corrodedRT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACK FROM FS 559 TO FS 559+64.SDR A6WA202012187469Seat Track · corrodedLBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT LBL 9, FS 364 THRU FS 409.SDR A6WA202012187466Seat Track · corrodedSEAT TRACK CORROSION AT RBL 9, FS 559+64. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED SEAT TRACK AT RBL 9, FS 559+64.SDR A6WA202012187468Seat Track · corrodedRBL 9, FLOOR SEAT TRACK FS 364 THRU FS 409 CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL 9, FS 364 THRU FS 409.SDR A6WA20190416562Display · failedON ARRIVAL, BOTH MFD'S FAILED, ONCE SHUTDOWN AT GATE, MFD #2 CAME BACK. (INFLIGHT AT 10000FT FAILURE OCCURRED).SDR A6WA2019030546451Flap · failedRECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH WHILE SELECTING FLAPS 45. FLAPS FAILED AT 33 DEGREES.SDR A6WA2019020246355Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED.SDR A6WA2019013146349Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN F.S.319 AND F.S.349.SDR A6WA2019013146350Structure · gougedR/H INBD FLAP, OUTBD HINGE BOX IS GOUGED ON INBD SIDE OF OUTBD LUG WHERE FLAP ATTACHES TO HINGE BOX.SDR A6WA2019012946342Frame · corrodedFS 319 IS CORRODED AT STR 26R.SDR A6WA2019012846340Frame · corrodedFS 310.00 LOWER FRAME SEGMENT IS CORRODED AT STRINGER 26R.SDR A6WA2019012846329Bulkhead · crackedINDICATIONS NOTED AT FS 621 REAR PRESSURE BULKHEAD FWD FACE AT LBL18 WL131.9 .9" IN LENGTH AND 55% FSH. AT LBL27.5 WL131 2.9" LONG AND 100% FSH. AT LBL 27.5 WL 105 1.25" LONG AND 78% FSH. ALL FAIL NDT.SDR A6WA2019012446325Skin · dentedLEFT WING I/B FLAP LOWER SKIN DENTED WITH CREASE THROUGH DENT WS 70.00 DENT APPROX. .300" X .250" X .025" DEEP.SDR A6WA2019020646370Former · corrodedPAX DOOR FWD FORMER IS CORRODED UNDER PANEL 832HL.SDR A6WA2019012146314Support Angle · crackedLT WINDSHIELD SUPPORT ANGLE IS CRACKED BETWEEN FS 220.00 AND FS 235.00 BETWEEN STGR 11L TO 14L.SDR A6WA2018102546123Bulkhead · crackedDURING SCHEDULED INSP OF AFT PRESS BULKHEAD FS621. FOUR CRACKS WERE DISCOVERED DURING EDDY CURRENT, 8 DAMAGED RIVETS DURING VISUAL, AND 7 TOOLING MARKS DURING VISUAL.SDR A6WA201845541Windshield · crackedFO WINDSHIELD CRACKED AT 21,200'. C/W QRH. RETURNED TO CAE, LANDING OVERWEIGHT AT 48,240 LBS. LANDING WAS SMOOTH.SDR A6WA201745078Apu · shutdown4108 APU AUTO SHUT DOWN ON GROUND WITH ASSOCIATED FUEL SMELL. REPLACED THE APU.SDR A6WA2017010444725Floor Support · corrodedFLOOR SUPPORT HAS LIGHT CORROSION SPOTS ON THE TOP AND BOTTOM SIDE BETWEEN BS 574 - 601.00 IN THE CARGO BAY. REPAIRED IAW EA AWAC-CRJ253-00609 REV-IR.SDR A6WA201744726Doubler · crackedINTERNAL DOUBLER COMMON TO UPPER BEACON LIGHT INSTALLATION IS CRACKEDSDR A6WA2017010444723Pulley Bracket · damagedTWO INBD BOLT HOLES FOR LANDING GEAR ALTERNATE EXTENTION PULLEY BRACKET ARE ELONGATED AT LBL 12 POST BS 280.00. REPAIRED IAW REO 601R-53-11-300- REV --.SDR A6WA2017010344721Floorbeam · corroded1013785-1000-0065 - FLOORBEAM AT FS 280 IS CORRODED BTW RBL 9 AND LBL 9SDR A6WA2017010344720Floor Support · corrodedMAIN CABIN FLOOR SUPPORT CORRODED LBL43 BS 349-408.SDR A6WA2017010344717Fitting · corrodedSERVICE DOOR LOWER SILL FITTING IS CORRODEDSDR A6WA2017010344716Angle · corrodedSERVICE DOOR CUT-OUT SILL HAS AREAS OF CORROSION FROM BS 319 - 349SDR A6WA2016123044712Bulkhead · gougedFORWARD FACE OF THE AFT PRESSURE BULKHEAD HAS SEVEN AREAS THAT ARE GOUGED. REPAIRED THE PRESSURE BULKHEAD IAW GREO 601R-53-61-2155 REV-A AND REO 601R-53-61-5895.SDR A6WA2016010344713Frame · corrodedFRAME BS 605 HAS CORROSION ON THE FWD AND AFT SIDE, BETWEEN STRINGER 20 AND 23L.SDR A6WA2016123044711Skin · dentedLEFT INBOARD FLAP LOWER SKIN HAS MULTIPLE DENTS BELOW INBD LOWER ACCESS PANEL. REPAIRED THE LT WING TE FLAP LOWER SKIN IAW REO 601R-57-52-1544.
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