N460AW

Service difficulty reports · 250

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 = 'N460AW' 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 A6WA201140398Access Panel · corrodedFUEL CELL ACCESS HOLE AT PANEL 550GB PITTED WHERE GASKET MEETS WING SURFACE. REPAIRED FUEL CELL ACCESS PANEL 550AD IAW EO E06/021/457.May 8, 2011 · N460AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201140404Skin · chafedLT INBD FLAP IN L/E CHAFED. EVALUATED, BLENDED, PRIMED, ALODINED AND TOP COATED IAW REO 601R-57-52-004.May 8, 2011 · N460AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140403Skin · chafedRT AILERON UPPER AND LOWER L/E (FIXED) HAS CHAFE DAMAGE BLENDED UPPER AND LOWER FIXED LEADING EDGE ALODINED, PRIMED, AND TOP COATED IAW REO 601R-57-60-13 AND REO 601R-57-60-020.May 8, 2011 · N460AW · Cndair CL6002B19 · AileronsSDR A6WA201140405Skin · chafedLT AILERON UPPER AND LOWER SURFACE CHAFED. BLENDED CHAFED AREA ALODINED, PRIMED, AND TOP COATED IAW REO 601R-57-60-013 AND REO 601R-57-60-020.May 8, 2011 · N460AW · Cndair CL6002B19 · AileronsSDR A6WA201140396Access Panel · corrodedFUEL CELL ACCESS HOLE AT PANEL 510AB PITTED WHERE GASKET MEETS WING SURFACE. REPAIRED FUEL CELL ACCESS PANEL 510AB IAW EO E06/021/457.May 8, 2011 · N460AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201140397Skin · corrodedFUEL CELL ACCESS HOLE AT PANEL 550BB PITTED WHERE GASKET MEETS WING SURFACE. REPAIRED FUEL CELL ACCESS PANEL 660BB IAW EO E06/021/457.May 8, 2011 · N460AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201140474Fitting · crackedPAX DOOR FWD COUNTER BALANCE PIVOT FITTING CRACKED AND SHIMS ARE CORRODED AT FS 310. R & R WITH SERVICEABLE COUNTER BALANCE ANCHOR FITTINGS PN 601R380142-3 AND SHIMS PN 600-38061-111.May 7, 2011 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140483Drag Angle · crackedPAX DOOR DRAG ANGLE CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION, THEN FABRICATED NEW SECTION AND INSTALLED IAW B/A REO 601R-52-11-513, REV A. May 7, 2011 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140477Bracket · chafedLT INBD FLAP INBD HINGE BOX HAS CHAFING TOP BRACKET INBD SIDE. R & R LT INBD FLAP INBD HINGE BOX INBD SIDE BRACKET IAW SRM 51-42-13.May 5, 2011 · N460AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140350Stiffener · crackedVERTICAL STIFFENER FS 409+128 LBL 18 OTBD CRACKED AT BOTTOM END. REPAIRED VERTICAL STIFFENER FS 409+128 ON LBL 18 OTBD IAW REO 601R-53-41-056, REV E.May 5, 2011 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140406Angle · crackedLT OBLIQUE ANGLE IS CRACKED ON AEB AT FS 625. R & R WITH SERVICEABLE OBLIQUE ANGLE ON LT AEB AT FS 625, STR 14.May 5, 2011 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140482Hinge · corrodedPAX DOOR STEP HINGE CORRODED. R & R PAX DOOR FOLDING STEP HINGE IAW SRM 51-42-06.May 4, 2011 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140476Skin · corrodedLT LOWER 9 OF VERTICAL L/E HAS MINOR CORROSION AT THE MATING SURFACE BLENDED OUT MINOR CORROSION TO A SMOOTH FINISH IAW SRM 51-12-00.May 4, 2011 · N460AW · Cndair CL6002B19 · Vertical Stabilizer, Plate/SkinSDR A6WA201140473Stiffener · crackedVERTICAL STIFFENER FS 609.00+128, LBL 27 INBD CRACKED AT BOTTOM END. REPAIRED VERTICAL STIFFENER AT FS 409.00, LBL 27 INBD IAW REO 601R-53-41-056, REV E.May 4, 2011 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140346Seat Track · corrodedNR 1 SEAT TRACK FLOOR LBL9 HAS CORROSION ON FWD END. R & R NR 1 SEAT TRACK LBL9 IAW SRM 51-21-01.May 2, 2011 · N460AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140345Seat Track · corrodedNR 1 SEAT TRACK RBL9 HAS CORROSION ON FWD END BLENDED OUT CORROSION ON SERVICEABLE SEAT TRACK P/N 126-2075 IAW SRM 53-21-49 TO A SMOOTH FINISH ALODINED IAW SRM 51-21-11.May 2, 2011 · N460AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140347Bulkhead · chafedRT AFT 280 BULKHEAD CHAFED BY GALLEY DOOR. FABRICATED FILLER AND DOUBLER TO PLACE IN CUT OUT DAMAGED AREA IAW REO 601R-53-11-1727, REV E.May 2, 2011 · N460AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201140478Skin · chafedPANEL 599CB HAS CHAFE DAMAGE BLENDED PANEL 599CB IAW SRM 51-12-00.May 1, 2011 · N460AW · Cndair CL6002B19 · AileronsSDR A6WA201140171Elevator System · stiffABNORMALLY HEAVY FLIGHT CONTROL FEEL WHEN DOING ELEVATOR CHECKS ( FLAPS AT -0- DEGREES OR 20 DEGREES. PERFORMED OPS TEST AND FREEDOM OF MOVEMENT OF ELEVATORS REF AMM 27-31-00. OPS CHECKED GOOD. PERFORMED FUNCTIONAL TEST OF PITCH SIMUALTOR UNITS IAW AMM 27-3Mar 7, 2011 · N460AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA201040338Clutch · lack of lubeDURING FLT PITCH FLIGHT CONTROLS FELT UNUSUALLY HEAVY REGARDLESS OF FLAP POS OCCURS ON GROUND ALSO. C/W LUBE OF ELEVATOR SERVO CLUTCH IAW AMM TASK 12-20-22-640-802 IAW SL. OPS CK GOOD.Apr 29, 2010 · N460AW · Cndair CL6002B19 · Elevator Control SystemSDR A6WA200940292Attach Bracket · crackedCLIP ON INTERCOSTAL AT FS 484.00, RBL 27.00, WL 72.00 IS CRACKED. CLIP ON INTERCOSTAL AT FS 484.00, RBL 27.00, WL 72.00. REPLACED IAW 51-42-06 AND 51-42-21. (K)Jun 1, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940293Attach Angle · crackedCLIP ON INTERCOSTAL AT FS 484.00, LBL 27.00, WL 72.00 IS CRACKED. CLIP ON INTERCOSTAL AT FS 484.00, LBL 27.00, WL 72.00. REPLACED IAW SRM 51-42-06 AND 51-42-21. (K)Jun 1, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940294Sill · crackedCRACK FOUND ON CARGO BAY FLOOR SILL FS 574. CARGO BAY FLOOR SILL FS 574 REPAIRED IAW REO 601R-53-61-1741. (K)May 29, 2009 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940295Sill · crackedCRACK FOUND ON CARGO LOWER SILL FS 589 AND FS 605. CARGO LOWER SILL FS 589.00 AND FS 605.00. REPAIRED IAW REO 601R-53-61-433.May 29, 2009 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6AW200940297Floorbeam · crackedQTY (2) FLOORBEAM ANGLES AT FS 280.00, LBL 9.00, WL 72.00 ARE CRACKED. QTY (2) FLOORBEAM ANGLES AT FS 280.00, LBL 9.0, WL 72.00 REPLACED IAW SRM 51-42-21- AND 51-42-06. (K)May 28, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200940297Floorbeam · crackedQTY (2) FLOOR SUPPORT ANGLES AT FS 280.00, LBL 9.0, WL 72.00 ARE CRACKED. QTY (2) FLOOR SUPPORT ANGLES AT FS 280.00, LBL 9.0, WL 72.00 REPLACED IAW SRM 51-42-21. (K)May 28, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940298Floorbeam · crackedQTY (2) FLOORBEAM ANGLES AT FS 280.00, RBL 9.00, WL 72 ARE CRACKED. QTY (2) FLOORBEAM ANGLES AT FS 280.00, RBL 9.000, WL 72.00 REPLACED IAW SRM 51-21-42. (K)May 28, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940299Floorbeam · crackedUPPER AFT FLOORBEAM ANGLE AT FS 280.00, WL 72.00 IS CRACKED AT RBL 9.00 AND LBL 9.00. UPPER AFT FLOORBEAM ANGLE AT FS 280.00, LW 72.00, AT RBL 9.0 AND LBL 9.0 REPAIRED IAW REO 601R-53-11-136, REV. A. (K)May 28, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940290Latch · corrodedCREW ESCAPE HATCH, UNABLE TO EJECT OUT HANDLE DUE TO CORROSION BETWEEN OUT HANDLE AND HOUSING. OUTER HANDLE ASSY REPLACED IAW CMM 52-22-01. (K)May 27, 2009 · N460AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200940296Bulkhead Web · crackedMWC 136515-39 - AFT PRESSURE BULKHEAD WEB AT THE LINTEL LOCATION IS CRACKED. AFT PRESSURE BLKHD WEB AT THE LINTEL LOCATION REPAIRED IAW REO 601R-53-61-1230 REV D. (K)May 27, 2009 · N460AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940264Drive Unit · malfunctioned180710/3 -FLAPS FAIL AT 8 DEGREES UPON RETRACTION TO ZERO DEGREES. UPON LANDING BRAKE TEMPS WERE NORMAL (4,4,4,4) LANDED AT 46,100. COMPLIED WITH RESET IAW AWAC SUPP 98-018C. RESET AND PLACED ON MEL. INTEROGATED FECU FOUND PDU DIFF FAULTED. IAW FIM 27-50-May 21, 2009 · N460AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840061Warning System · activatedON NORMAL TAKEOFF, SELECTED GEAR UP AND RECEIVED NLG DOOR OPEN AND GEAR DISAGREE WARNINGS AND WOW INPUT AND NWS INOP CAS MESSAGES. COMPLIED WITH QRH FOR ALL MESSAGES, ALL CLEARED, ALL 3 GEARDOWN AND LOCKED. RETURNED TO DEPARTURE FOR NORMAL LANDING. (K)Feb 3, 2008 · N460AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200840054Handle · looseSERVICE DOOR HOLD OPEN LATCH HANDLE LOOSE. (K) REMOVED AND REPLACED HOLD OPEN LATCH HANDLE ROLL PINS (2). OPS CHECK GOOD IAW AMM 52-41-00. (S)Jan 27, 2008 · N460AW · Cndair CL6002B19 · Service DoorsSDR A6WA20080046Unknown · malfunctionedHIGHER THAN NORMAL BACK PRESSURE NEEDED DURING LANDING WITH YOKE. (K)Jan 23, 2008 · N460AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA200740644Unknown · unknownDURING APPROACH TO MHT, NOSE UP TRIM OF 9.2 UNITS REQUIRED TO MAINTAIN NORMAL GLIDE PATH. FLIGHT CONTROLS HEAVIER THAN NORMAL, ESPECIALLY ELEVATOR. AILERONS FEEL HEAVY ALSO. NO UNUSUAL WEATHER CONDITIONS. ALL HYDRAULIC NORMAL. ELEVATOR TRIM ON GO AROUND ONov 14, 2007 · N460AW · Cndair CL6002B19 · Flight Control SystemSDR A6WA200740327Skin · crackedAFTER REMOVING PAX DOOR TOP STEP 832DT FOR ACCESS FWD PAX DOOR FWD SIDE SKIN CRACKED APPROX .750 INCH L LOWER CORNER OF NR 2 STEP IN RADIUS. MAINTENANCE CUT AWAY DAMAGE FABBED REPAIR PARTS AND INSTALLED IAW REO 601R52-11-702, STEPS 1 THRU 12. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740326Drag Angle · crackedPAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX .5 INCH LONG AT LOWER CORNER OF NR 2 STEP. MAINT REPAIRED IAW REO 601R-52-11-702. REV A STEPS 1 THRU 12. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740325Drag Angle · crackedPAX DOOR AFT DRAG ANGLE HAS A CRACK APPROX 1 INCH LONG AT UPPER EDGE OF CABLE PULLEY BRACKET. [07-31-07] MAINTENANCE REPAIRED IAW REO 601R-52-11-513, STEPS 1-10. (K)Jun 19, 2007 · N460AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200740320Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS 621, WL 73, LBL 27 - 45 IS CRACKED .5 INCHES LONG. MAINTENANCE REPAIRED FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)Jun 18, 2007 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740319Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS 621, WL 73, RBL 27 - 45 IS CRACKED .5 INCH LONG. MAINTENANCE REPAIRED FS 621 ANGLE IAW REO 601R-53-61-117, REV C. (K)Jun 18, 2007 · N460AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200740331Channel · crackedCARGO DOOR FWD TRACK LOWER CHANNEL CRACKED. MAINTENANCE REMOVED AND REPLACED CHANNEL IAW CRJ 200 SRM 51-40-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740330Intercostal · crackedLT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1..5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601-35012-51 IAW CRJ SRM 51-42-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740329Intercostal · crackedRT FS 621 TO FS 625 UPPER INTERCOSTAL (OBLIQUE) ANGLE IS CRACKED 1.5 INCH LONG. MAINTENANCE REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE (PN 601-35012-52 IAW SRM 51-42-06. (K)Jun 17, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740328Intercostal · crackedUNDERFLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE AT IB SIDE OF LBL 36, FS 484, WL 72.5. MAINTENANCE CUT OFF CRACKED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R53-41-059. (K)Jun 14, 2007 · N460AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740111Relay · failedON AC ELECTRICAL SYNOPTIC PAGE ADG BUS DISPLAYED IN WHITE. AC1 AND AC2 BUS SHOW WHITE LINES TO ESS BUS, ESS BUS IS GREEN. REMOVED AND REPLACED K2XD RELAY IAW AMM 24-51-31. OPS CHECK GOOD. (K)Mar 2, 2007 · N460AW · Cndair CL6002B19 · AC Power Distribution SystemSDR A6WA200740026Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE, ZERO DEGREE FLAP LANDING. TOUCHDOWN SPEED 173, MAX BRAKE TEMP WAS 4, 45,000 LBS LANDING WEIGHT. DID NOT LAND OVERWEIGHT OR MAKE OR HARD LANDING. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING IAW AWAC SUPPLEMENT 98-018A. REJan 15, 2007 · N460AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740023Bpsu · maladjustmentFLAP FAIL YELLOW CAUTION ILLUMINATED INFLIGHT WITH FLAP A ZERO. INSPECTED FLAPS, NO EVIDENCE OF TWISTING OR SKEWING PER AWAC AMM SUPPLEMENT 98-018A, RESET CIRCUIT BREAKERS, FLAPS OPERATE NORMALLY PER AMM 27-50. PLACED ON 72 HOUR FLAP WATCH. REMOVED AND REPLAJan 9, 2007 · N460AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200640268Cap · leakingFOUND FUEL LEAKING FROM CENTER WING CAP COVER. REMOVED AND REPLACED CAMLOCK FASTENER. (M)Jun 27, 2006 · N460AW · Cndair CL6002B19 · Fuel StorageSDR A6WA200540211Panel · damagedATTACHMENT HOLE ENLARGED ON OUTBOARD SIDE OF PANEL 684BB, DAMAGED WHILE REMOVING SCREW HOLE DIA WAS .193 NOW .265. INSTALLED FABRICATED 100 COUNTERSINK FREEZE PLUG IAW BRAS EO NR 601-57-6666. (M)Apr 17, 2005 · N460AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200440013Control Lever · failedON DEPARTURE OUT OF IND, FLAP FAIL CAS MESSAGE, ED1 AND FLIGHT CONTROL PAGE SHOWS FLAP FAIL AT 8 DEGREES, RAN QRH DIVERTED TO MKE. REPLACED FLAP CONTROL LEVER AND RIGGED LEFT PBSU PER AMM 27. OPS CHECK NORMAL. (M)May 5, 2004 · N460AW · Cndair CL6002B19 · Trailing Edge Flap Control System
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