N417AW

Service difficulty reports · 217

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 = 'N417AW' 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.

SDR A6WA201140342Skin · chafedLT MLG DOOR FWD EDGE CHAFED 2 EA PLACES. FABRICATED FILLER AND DOUBLER INSTALLED IAW REO 601R-52-82-034 AND REO 601R-52-82-102.Apr 4, 2011 · N417AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140277Heat Shield · crackedAPU EXHAUST HEATSHIELD CRACKED AT 6 O`CLOCK POSITION. REPAIRED APU EXHAUST HEATSHIELD IAW REO 601R-49-81-003, REV B.Apr 4, 2011 · N417AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201140272Door · crackedAPU ENCLOSURE DOOR 311B2 CRACK AT WELD TOP OF STIFFENER. REPAIRED APU ENCLOSURE DOOR 311B2 AND IAW REO 601R-49-11-070.Apr 4, 2011 · N417AW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR A6WA201140343Skin · chafedRT MLG DOOR FWD EDGE CHAFED IN 2 EA PLACES PREVIOUS REPAIRS. R & R LOWER FILLER IAW REO 601R-52-82-034.Apr 3, 2011 · N417AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140332Frame · crackedLBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409+128. REPAIRED IAW REO 601R-53-41-056, REV E.Apr 2, 2011 · N417AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201140331Frame · crackedRBL 18.00 POST CRACKED OTBD BOTTOM AT FS 409.00+128. REPAIRED IAW REO 601R-53-41-056, REV E.Apr 2, 2011 · N417AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201140344Intercostal · crackedPAX DOOR INTERCOSTAL UNDER PANEL 832BR IS CRACKED. REMOVED CRACKED INTERCOSTAL THEN INSTALLED NEW SERVICEABLE INTERCOSTAL PN 601R-31902-318 AND IAW SRM 51-41-06.Apr 2, 2011 · N417AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140273Rib · crackedRT BATT RIB IS CRACKED. REPAIRED RT BATT RIB IAW REO 601R-57-51-046, REV B.Apr 1, 2011 · N417AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201140337Seat Track · corrodedSEAT TIE DOWN TRACK CORRODED LBL 9.00, FS 559+112 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM LBL 9.00, FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Mar 31, 2011 · N417AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140335Seat Track · corrodedSEAT TRACK TIE DOWN CORRODED RBL 9.00, FS 669+112 CARGO BAY PARTS. REMOVED UNSERVICEABLE SEAT TRACK FROM RBL 9.00, FS 559+112 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Mar 31, 2011 · N417AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140217Sill · corrodedLT CARGO BAY FLOOR SILL CORRODED AND CRACKED. REMOVED CORROSION AT LT CARGO BAY FLOOR SILL AND CUT OUT CRACK IAW SRM 51-21-06 AND REO 601R-53-61-433, REV B.Mar 31, 2011 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140216Angle · corrodedCORROSION ON ANGLE CLIPS AT FS 320.10 AND FS 338.00. REMOVED CORRODED CLIPS AT FS 320.10 AND FS 338.00 AND INSTALLED NEW SERVICEABLE CLIPS IAW SRM 51-42-06.Mar 31, 2011 · N417AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140275Pressure Blkhd · crackedFWD PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71, LW 69.684 IAW REO 601R-53-11-563.Mar 30, 2011 · N417AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201140339Seat Track · corrodedSEAT TRACK TIE DOWN CORRODED LBL 9.00, FS 621. REMOVED SERVICEABLE SEAT TRACK FROM LBL 9.00, FS 621 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Mar 29, 2011 · N417AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140338Seat Track · corrodedSEAT TRACK CORRODED LBL 9.00, FS 574 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM LBL 9, FS 574 INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Mar 29, 2011 · N417AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140336Seat Track · corrodedSEAT TRACK TIE DOWN CORRODED RBL 9.00, FS 574 CARGO BAY AREA. REMOVED UNSERVICEABLE SEAT TRACK FROM RBL 9, FS 574 AND INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11.Mar 29, 2011 · N417AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140215Panel · gougedLOWER LT AILERON SHROUD PANEL 599BB GOUGED. REPAIRED LOWER LT SHROUD PANEL 599BB IAW REO 601R-57-60-020.Mar 29, 2011 · N417AW · Cndair CL6002B19 · AileronsSDR A6WA201140214Panel · gougedLOWER LT AILERON SHROUD PANELS 599AB AND 599CB CHAFED. REPAIRED LOWER LT AILERON SHROUD PANELS 599AB AND 599CB IAW REO 601R-57-60-020.Mar 29, 2011 · N417AW · Cndair CL6002B19 · AileronsSDR A6WA201140173Trim Panel · malfunctionedFLT 3755, LOG 212249/1, DLY 3594, RUDDER TRIM KNOB STUCK IN FLIGHT MOMENTARILY WITH LT RUDDER TRIM INPUT. TRIM TENDS TO RUN-AWAY WITHOUT CORRECTION. R & R RUDDER/ AILERON TRIM PANEL REF AMM 27-22-00. OPS CKS GOOD.Mar 14, 2011 · N417AW · Cndair CL6002B19 · Rudder Tab Control SystemSDR AW6A201040583Pressure Blkhd · crackedFS 559, RBL 9.0 INBD SIDE CRACKED AT BOTTOM EDGE FROM LOWEST FASTENER INCORPORATED REO 601R-53-41-260 REV D DATED 09/17/09 ALONG WITH REO 601R-53-41-609 REV B DEVIATION E DATED 12/18/09.Aug 9, 2010 · N417AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR AW6A200940238Bulkhead · crackedMWC 135144-2 - AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 LT, LINTEL ASSY AREA. AFT PRESSURE BULKHEAD CRACK AT FS 621.00 LT AT LINTEL ASSY REPAIRED IAW REO 601R-53-61-1230, REV D. (K)Apr 30, 2009 · N417AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940226Inlet · cracked(AT GATE) 199793/1 - EXCESSIVE SMOKE FROM APU INLET AFTER APU SHUTDOWN FOR 3(?) MINUTES FIRE WARNING FOR SPLIT SEC AND THEN SILENCED ITSELF. INSPECTED APU INLET AND EXHAUST, PULLED APU COVER AND INSPECTED AREA NO DEFECTS NOTED. INSPECTED FIRE LOOPS, NO DEFECApr 27, 2009 · N417AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA200940234Intercostal · crackedMWC 134852-187 - FS 484, RBL 27.00 AND RBL 36 CLIP AND INTERCOSTAL FOUND CRACKED. FS 484, RBL 27.00 AND RBL 36 CLIP AND INTERCOSTAL REPAIRED IAW REO 601R-53-41-059, REV "A". (K)Mar 22, 2009 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940235Attach Fitting · crackedMWC 134852-144 - FS 280.00, RBL 9.0, INBD CLIP OF PILOT BULKHEAD FOUND CRACKED. CLIP AT FS 280.00, RBL 9.0 INBD. REMOVED AND REPLACED IAW SRM 51-42-21 AND 51-42-06. (K)Mar 22, 2009 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940236Retainer · corrodedMWC 134852-112 - AVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)Mar 21, 2009 · N417AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200940169Retainer · corrodedAVIONIC DOOR SEAL RETAINERS FOUND CORRODED. SEAL RETAINER REMOVED AND REPLACED IAW SRM 51-42-06. (K)Mar 21, 2009 · N417AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA200840301Proximity Sensor · out of adjustGEAR DISAGREE WARNING MESSAGE ILLUMINATED AFTER RETRACTION. REF WO 122814 ADJUSTED NLG OLEO CENTERED/EXTENDED PROX SENSOR IAW AMM 32-61-05. OPS CHECK GOOD. (K)Apr 7, 2008 · N417AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840206Flap System · malfunctionedFLAP FAILED MESSAGE, FLAP FAILED AT ZERO. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET. OK. (M)Mar 17, 2008 · N417AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840177Warning Light · false activationSTAB AND MACH TRIM CAUTION IN FLIGHT. AUTOPILOT PITCH TRIM MESSAGE IN FLIGHT. PERFORMED OPS CHECK OF STAB SYSTEM, NO FAULTS NOTED. INTERROGATED HSTCU REF 27-41-00, NO FAULTS NOTED. (M)Mar 10, 2008 · N417AW · Cndair CL6002B19 · Central WarningSDR A6WA200840100Rudder · malfunctionedUNCOMMANDED FULL RT RUDDER AT HIGH ALTITUDE CLIMB 280 KNOTS WITH YAW DAMPER ENGAGED, STEPPED ON RUDDER TO CORRECT AND TRIMMED BACK IN POSITION, PROCEEDED NORMALLY. (K)Feb 15, 2008 · N417AW · Cndair CL6002B19 · Rudder Control SystemSDR A6WA200740227Computer · malfunctionedAFTER TAKEOFF, ROLL AND PITCH INDICATION ON CAPTAINS F/O ATTITUDE INDICATOR CAME ON, FOLLOWED QRH AND RETURNED TO MKE CAPTS PITCH PLUS 7 DEGREES OVER FIRST OFFICER BANK 5-10 DEGREE. REPLACED CAPTAINS AHRS COMPUTER IAW CRJ AM 34-21-01. OPS TEST FOUND SATISFACMay 13, 2007 · N417AW · Cndair CL6002B19 · Integrated Flight SystemSDR A6WA200740216Bracket · crackedPAX DOOR ASSIST MOTOR BRACKET (PN 601R317743-7) CRACKED AT BOTTOM END APPROX. 12 INCHES LONG. (K)Apr 27, 2007 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740215Floor Support · corrodedRT FWD FLOOR SUPPORT ANGLE (PN 601R31148-79) BETWEEN FS 310.00 AND FS319.70 CORRODED ON AFT END. REMOVED AND REPLACED SUPPORT (PN 601R31148-79) IAW SRM 51-23-00, SRM 51-42-06 AND DRWG 601R31148. (K)Apr 26, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740214Skin · corrodedRT WING PLANK AT ACCESS HOLE 640DB HAS CORROSION ON LOWER IB SIDE MEASURES APPROX .5 X .25 X .002 IN NON-CRITICAL AREA. REPAIRS ACCOMPLISHED IAW EO E06/021/457. (K)Apr 24, 2007 · N417AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200740208Bracket · corrodedFOUND SERVICE DOOR SURROUND STRUCTURE LOWER SILL JOINT BRACKET (P/N 601R38335-1, CORRODED AT FS 318.70 WL 73 STRINGER 18. (M) REMOVED AND REPLACED BRACKET (PN 601R383355-1) IAW SRM 51-40-11 AND BSC EO 601R53-11628. (K)Apr 19, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740206Bracket · crackedRT HYDRAULIC TRANSDUCER BRACKET (PN 601R75262-157) CRACKED APPROX .2 INCH LONG IN RT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740207Support Bracket · crackedRT HYDRAULIC TRANSDUCER LINE SUPPORT BRACKET, P/N 601R75262-153, CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (M) INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740205Bracket · crackedLT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159) CRACKED APPROX .1 INCH LONG IN LT MLG WHEEL WELL CEILING. (M) MAINTENANCE INSTALLED NEW BRACKET IAW SRM 51-42-06. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA200740204Fitting · crackedOUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .4 INCH LONG. (M) REPAIRED FS 280 CLIP IAW BSC SR 601R530057A. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740203Fitting · crackedINBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9.0 IS CRACKED IN RADIUS APPROX .2 INCH LONG. (M) REPAIRED FS280 CLIP IAW BSC SR 601R530057A. (K)Apr 18, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740202Fitting · crackedOUTBOARD FLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9.0 IS CRACKED IN RADIUS APPROX .1 INCH LONG. (M) REPAIRED FS280 CLIP IAW BSC SR 601R530557A.Apr 18, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740185Pcu · malfunctionedVIBRATION NOTED AT 10,000 FT AIRSPEED 310 KNOTS, SLOWED TO 260 KNOTS, VIBRATION STOPPED. GEAR WAS UP. REMOVED AND REPLACED RT SPOILER PCU REF AMM 27-62-01, OPS CHECK GOOD AT THIS TIME. REMOVED SPOILER PCU SER NO MAL 5041, PN 270007, TSN: 11492 CSN: 10286. Apr 2, 2007 · N417AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200740201Sill · corrodedCARGO DOOR SILL PLATE HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATES FROM FS 574 TO 621. (M) REPAIRED CARGO DOOR SILL PLATE IAW SRM 51-21-01 AND 51-25-01. (K)Mar 13, 2007 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740113Warning System · activatedWHEN SELECTING FLAPS FROM 8 DEGREES TO 20 DEGREES, A FLAP CAUTION MESSAGE OCCURRED IN FLIGHT. (K)Mar 11, 2007 · N417AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640310Microphone · intermittentCAPTAINS OXYGEN MASK MIC INTERMITTENT. REMOVED AND REPLACED CAPTAINS OXYGEN MASK IAW 35-10-00, OPS CHECK GOOD. (M)Aug 8, 2006 · N417AW · Cndair CL6002B19 · Communications SystemSDR A6WA200540324Idg · faultyON TAKEOFF ROLL IDG NR 1 FAULT FOLLOWED GEN NR 1 FAULT ABORTED 40 KNOTS BTMS INDICATION 2,2,22 LIGHT BREAKING. SERVICED IDG NR 1 IAW AMM. COMPLIED WITH ENGINE RUN. OPS CHECK GOOD. NOT LEAKS NOTED IAW AMM. NO HIGH ENERGY STOP INSPECTION REQUIRED. (K)Nov 15, 2005 · N417AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200540161Floor Support · crackedRIGHT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. PERFORMED A MAJOR REPAIR BY REMOVING DAMAGED ANGLE AND INSTALLING A REPAIR ANGLE IAE BOMBARDIER, INC REO 601R-53-61-117 REV C. (M)May 1, 2005 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540232Floor Support · crackedMWC 135 RT FS621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING SECTION OF DAMAGED ANGLE, FABRICATING AND INSTALLING REPAIR ANGES IAW MFG REO. (K)Apr 22, 2005 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540231Floor Support · crackedMWC 134 LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING AND INSTALLING REPAIR ANGLES IAW MFG REO. (K)Apr 22, 2005 · N417AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540160Skin · chafedRIGHT LOWER WING PLANK UNDER PANEL 650HB IS CHAFED IN TWO AREAS. INBOARD AREA CHAFED .050 INCH WIDE 6 INCHES LONG APPROX .002 INCH DEEP. OUTBOARD AREA CHAFED .050 INCH WIDE 4 INCHES LONG APPROX .001 INCH DEEP. FORWARD CENTER IS AT STARTING STAGES OF CORROSIApr 18, 2005 · N417AW · Cndair CL6002B19 · Wing, Plate/Skin
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