N425AW

Service difficulty reports · 210

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 = 'N425AW' 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 A6WA200940604Attach Fitting · crackedCRACK FOUND ON INTERCOSTAL CLIP AT FS 484.00, RBL 27.00 AND RBL 36.00 (CRACK ARE NR1 .50", NR2 .50") CLIP AT FS 484.00, RBL 36.00 REPLACED IAW SRM 51-42-06 AND 51-42-21, REMAINING CLIP TO BE REPLACED AT FS 484.00, RBL 27.00, TRANSFERRED MWC 140147-225. (K)Sep 22, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940609Skin · gougedLT MLG DOOR GOUGED AT FWD LOWER CORNER .500" X 2" .040 DEEP REPAIR PERFORMED ON LT MLG DOOR SKIN IAW REO 601R52-82-034 NC. (K)Sep 21, 2009 · N425AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA200940684Drag Angle · crackedPAX DOOR, AFT DRAG ANGLE CRACKED. PAX DOOR AFT DRAG ANGLE REPLACED IAW 601R-52-11-513, REV A. (K)Sep 19, 2009 · N425AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940599Support Bracket · crackedCRACK FOUND ON RT HYD MANIFOLD SUPPORT BRACKET AT FS 718. RT HYD MANIFOLD SUPPORT BRACKET AT FS 718, REPAIRED IAW REO 53-62-031 REV A. (K)Sep 18, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200940620Skin · crackedNLG SKIN CUT-OUT CRACK REPAIRED IAW REO 601R-53-11-048, REV C AT FS 235, RBL 6.0. REPAIRED IAW REO 601-53-11-048 REV C FS 235, RBL 6.0. (K)Sep 17, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200940622Fitting · wornLT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND ROLLER WEAR DAMAGE LT WING OTBD FLAP ALIGNMENT FITTING 601R10156. REPAIRED IAW REO 601R-57-51-143, REV NC. (K)Sep 17, 2009 · N425AW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR A6WA200940603Sill · crackedCARGO DOOR CUTOUT, LWR SILL CRACKED AT STOW FLAP BRAKET LOCATION (LENGTH .500"). REPAIRED IAW REO 53-61-174, REV NC AT CARGO DOOR SILL AT STOW FLAP BRACKET. (K)Sep 17, 2009 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940632Floor Support · corrodedCORROSION FOUND ON FLOOR STRUCTURE BTWN FS 605.00 AND 621.00, RBL 45.00 ON FLOOR STRUCTURE BTWN FS 605.00 AND FS 621.00 AT RBL 45.00 CORROSION REPAIRED IAW SRM 51-21-06. (K)Sep 17, 2009 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940612Skin · gougedLT WING LWR SKIN GOUGED AFT OF FUEL PANEL 540EB. LT WING LWR SKIN GOUGE BLENDED IAW SRM 51-12-00. NDT C/OUT - NO CRACK FOUND. (K)Sep 17, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940623Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650CB CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650CB IAW REO 601R-57-21-030, REV G. (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940614Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650BB. CORRODION ON FUEL ACCESS DOOR CUT-OUT 650BB REPAIRED IAW REO 601R-57-21-030, REV G AND EO E06/012/457 REV "A". (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940615Skin · corrodedCORRODION FOUND ON FUEL TANK ACCESS DOOR CUT-OUT 510AB. ON FUEL TANK ACCESS DOOR CUT-OUT 510AB CORROSION REPAIRED IAW REO 601R-57-21-030 REV G AND EO E06/021/457, REV "A". (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940624Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650DB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A".Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940625Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640BB ON FUEL TANK ACCESS DOOR CUT-OUT 640BB CORROSION REPAIRED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940616Skin · corrodedLT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT OUT 540EB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 540EB CORROSION REPAIRED IAW REO 601R57-21-030, REV G. (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940617Skin · corrodedLT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550GB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 550GB CORROSION REPAIRED IAW REO 601R-57-21-030, REV G. (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940605Fitting · crackedCRACK FOUND ON FLOORBEAM FITTING FS 461, RBL 9.00 OTBD. FLOORBEAM FITTING AT FS 461.00, RBL 9.00 OTBD REPLACED IAW SRM 51-42-21. (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940613Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640AB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 640AB IAW REO 601R-57-21-030, REV G. EO. E06/021/457, REV A. (K)Sep 16, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940601Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD AT FS 280.00, LBL 9.0 (CRACK LENGTH .400). REPAIRED PERFORMED ON PILOT BULKHEAD AT FS 280.00, LBL 9.0 IAW REO 601R-53-11-171 "SCHEME A", REV D.Sep 16, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940683Bulkhead · crackedAFT PRESSURE BULKHEAD AT FS 621.00 CRACK AT LINTEL. AFT PRESSURE BULKHEAD AT LINTEL LOCATION REPAIRD IAW REO 601R-53-61-1230, REV D. (K)Sep 15, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940628Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550CB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550CB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)Sep 15, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940629Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550DB IAW REO 601R-57-21-060, REV G. (K)Sep 15, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940626Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 540DB. CORROSION ON FUEL ACCESS DOOR CUT-OUT 540DB REMOVED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV A. (K)Sep 15, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940627Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 510BB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 510BB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)Sep 15, 2009 · N425AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200940631Structure · crackedREPAIR CRACKS ON PASSENGER DOOR STAIR, TOP AFT CORNER OF EDGE MEMBER. REPAIR PERFORMED ON PASSENGER DOOR STAIR, TOP AFT CORNER OF EDGE MEMBER IAW REO 601R-52-11-27. (K)Sep 14, 2009 · N425AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940611Fitting · wornRT WING OTBD FLAP ALIGNMENT FITTING 601R10156 FOUND WITH ROLLER WEAR DAMAGE. RT WING, OTBD FLAP ALIGNMENT FITTING, REPAIRED IAW REO 601R57-51-149, REV NC. (K)Sep 12, 2009 · N425AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200940600Bulkhead · crackedCRACK FOUND ON PILOT BULKHEAD AT FS 280.00, RBL 9.0 (LENGTH 2.250"). PILOT BULKHEAD AT FS 280.00, RBL 9.00 REPAIRED AND PERFORMED IAW REO 601R-53-11-171, REV "D". (K)Sep 11, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940621Bulkhead · damagedAFT PRESSURE BULKHEAD FS 621, LBL 27.50, LB 130.00 ABOVE CARGO DOOR TRACK REPAIRED IAW REO 601R-53-61-1541, REV B. (K)Sep 10, 2009 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200940602Sill · crackedCARGO DOOR SILL CRACKED AT FS 589.00 AND FS 605.00. CARGO DOOR SILL REPAIRED IAW REO 601R-53-61-433. (K)Sep 9, 2009 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940173Fire Bottle · dischargedCARGO BOTTLE LOW MESSAGE IN FLIGHT. COMPLIED WITH QRH, DIVERTED, MESSAGE OUT ON LANDING. REMOVED AND REPLACED LT CARGO FIRE EXTINGUISHER BOTTLE A2HL IAW AMM 26-25-01. OPS CHECK GOOD AT THIS TIME. (K)Mar 29, 2009 · N425AW · Cndair CL6002B19 · Extinguishing SystemSDR A6WA200840595Warning Light · illuminatedON GEAR EXTENSION AND RETRACTION RECEIVED ANTI-SKID OB CAUTION MESSAGE. COMPLIED WITH QRH. EMERGENCY LANDING DECLARED. BRAKE SYSTEM OPS CHECK GOOD IAW 32-43-00710-801. (K)Sep 26, 2008 · N425AW · Cndair CL6002B19 · Central WarningSDR A6WA200840458Flap System · malfunctionedFLAPS FAILED AT ZERO IN FLIGHT. BRAKE TEMPS WERE IN NORMAL RANGE AT LANDING. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEM RESET OK. AIRCRAFT RELEASED FOR SERVICE. (A)Jun 9, 2008 · N425AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840099Fuel Line · leakingFUEL LEAKING FROM DRAIN UNDER AFT FUSELAGE. REMOVED AND REPLACED FUEL LINE ASSY IAW 28-20-01. (K)Feb 14, 2008 · N425AW · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA200840006Selector Valve · failedON DEPARTURE, SELECTED GEAR LEVER UP. RECEIVED TRIPLE CHIME AND DISAGREE AURAL MESSAGE. GOT GEAR DISAGREE NOSE GEAR DOOR WARN MESSAGES AND WOW INPUT AND NWS INOPERATIVE CAUTION MESSAGES. EXECUTED QRH IN THAT ORDER, HAD 3 GEAR DOWN LOCKED INDICATIONS. REMOVEJan 4, 2008 · N425AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR A6WA200740545Wire Harness · damagedON TAKEOFF ROLL, THRUST LEVER ADVANCEMENT GOT LEFT JET OVERHEAT FAIL CAS MESSAGE. ABORTED TAKEOFF AT 10 KNOTS, MAX BTMS READING IS 4, TAKEOFF WEIGHT 44,300 LBS. REMOVED AND REPLACED ENGINE NR 1 FIRE DETECTION HARNESS PER AMM 26-11-07. OPS CHECK GOOD. (M)Sep 24, 2007 · N425AW · Cndair CL6002B19 · Fire Protection System WiringSDR ATWA200740511Panel · damagedFOUND RIGHT KIDNEY PANEL CUTOUT AT FORWARD FUSELAGE HAS ONE ELONGATED HOLE. (M)Sep 15, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200740511Skin · damagedRT KIDNEY PANEL CUTOUT AT FWD FUSELAGE HAS ONE ELONGATED HOLE. MAINTENANCE REPAIRED IAW REO 601R-53-11-162. (M)Sep 15, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200740510Angle · crackedFOUND FS 559 LBL 9 VERTICAL POST AT OUTBOARD LEG IS CRACKED AT BOTTOM RIVET. SUP - MAINTENANCE REPAIRED POST OUTBOARD LEG AT LBL 9, FS 559 IAW REO 601R-53-41-057 REV A. (M)Sep 7, 2007 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740509Attach Fitting · crackedFOUND FS 280 LBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M)Sep 7, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740508Attach Fitting · crackedFOUND FS 280 LBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-13, 51-42-21 AND BSC SRM 601R-57-0057A. (M)Sep 7, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740507Attach Fitting · crackedFOUND FS 280 RBL 9 INBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND 51-42-21. (M)Sep 7, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740506Attach Fitting · crackedFOUND FS 280 RBL 9 OUTBOARD CLIP CRACKED. SUP - MAINTENANCE REPLACED CLIP IAW SRM 51-42-06 AND BSC SRM 601R-53-0057A. (M)Sep 7, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740539Channel · crackedCARGO DOOR FORWARD TRACK BOTTOM CHANNEL, P/N 601R35050-25 IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE CHANNEL P/N 601R35050-25 IAW CRJ 200 SRM 51-42-06. (M)Sep 6, 2007 · N425AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA200740540Bracket · crackedBRAKE TRANSDUCER BRACKET IN LT MLG WHEEL WELL IS CRACKED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE BRACKET P/N 601R75262-159 IAW CRJ 200 SRM 51-41-04, AND 51-42-06. (M)Sep 5, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740498Bulkhead · crackedFS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LINE. CRACK IS APPROX 1.3 INCH LONG. (M)Sep 4, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740499Support Bracket · crackedEXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .6 INCHES LONG. (M)Sep 4, 2007 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740496Bulkhead · crackedFS 202.75 FORWARD PRESSURE BULKHEAD IS CRACKED LT SIDE AT WL 65, APPROX LBL 28, FITTING FOR RT INBOARD BRAKE NR 3 HYD LINE. CRACK IS APPROX 1.3 INCHES LONG. SUP - MAINTENANCE REPAIRED CRACK BY TRIMMING OUT DAMAGE AND INSTALLING FILLER AND DOUBLE IAW BSC EO 6Sep 4, 2007 · N425AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200740497Bracket · crackedEXTERNAL POWER RECEPTACLE SUPPORT BRACKET, P/N 600-33283-33, IS CRACKED AT RECEPTACLE FORWARD OUTBOARD ATTACH MEDT BOLT HOLE. CRACK IS APPROX .5 INCHES LONG. SUP - MAINTENANCE REMOVED AND INSTALLED SERVICEABLE SUPPORT BRACKET P/N 600-33283-33 IAW CRJ 200 SRMSep 4, 2007 · N425AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640314Target · looseAFTER TAKEOFF ON GEAR RETRACTION LEFT MLG INDICATED INTRANSIT, LT MLG NEVER SHOWED UP AND LOCKED. GEAR DISAGREE CAS MESSAGE 28 SECONDS. COMPLIED WITH QRH, PULLED EMERGENCY GEAR EXT HANDLE, GEAR CAME DOWN, 3 GREEN ALL DOWN AND LOCKED. FOUND LEFT MLG UPLOCK TAug 8, 2006 · N425AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200540335Control Cable · frayedSPOILERON FAULT, AILERON FEELS ROUGH WHEN TURNED TO THE RIGHT. AC HAS FRAYED AILERON CABLES DUE TO INCORRECT INSTALLATION, REPLACED CABLES.Nov 28, 2005 · N425AW · Cndair CL6002B19 · Aileron Control System
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