N428AW
Service difficulty reports · 209
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 = 'N428AW' 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 = 'N428AW' 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 A6WA200840069Frame · dentedFRAME DENTED OVER LIMITS AT FS 700.00 BTW STR 22L TO STR 23L. FRAME SELECTOR REPLACED AT FS 700.00 BTW STR 22L TO 23L SRM 51-42-06. (K)SDR AA6WA200840030Separator · damagedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 412DB. QTY (1) SEPARATOR REPLACED ON LT PYLON ACCESS PANEL 412DB IAW SRM 51-42-06. (K)SDR A6WA200840030Separator · corrodedQTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 421DB. (K)SDR A6WA20084018ABracket · unknownRT ENGINE UPPER CORE COWL STA ROD PIN AND BRACKET (SPRING CLIP) FOUND. RT ENGINE UPPER CORE COWL STAY ROD PIN REPLACED AND BRACKET (SPRING CLIP) REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840032Frame · dentedDENT EXIST ON SKIN FS 700 STR L 22 TO L 23. REMOVED FRAME IAW REO 601R-53-61-2482. NEW FRAME INSTALLED IAW SRM 51-42-06. (K)SDR A6WA200840041Structure · crackedCRACK FOUND ON FLOOR STRUCTURE ON FS 280, LBL 9. DAMAGE ON FLOOR STRUCTURE AT FS 280, LBL 9 REPAIRED IAW REO 601R-53-11-171. (K)SDR A6WA200840044Bracket · gougedPAX DOOR SURROUND STRUCTURE ROLLER BRACKET GOUGED ON FS 349, STR 6L. SURROUND STRUCTURE NEW ROLLER BRACKET INSTALLED ON PAX DOOR AT FS 349, STR 6 IAW SRM 51-41-04. (K)SDR A6WA200840039Fitting · gougedPAX DOOR SURROUND STRUCTURE CAM FITTING GOUGE ON FS 349, STR 5L. REPLACED IWA SRM 51-42-21. (K)SDR A6WA200840031Support Angle · crackedANGLE CRACK ON RT HEAT EXCHANGE SUPPORT STRUCTURE BTW FS 700 AND FS 718. ANGLE REPLACED ON RT HEAT EXCHANGER SUPPORT STRUCTURE BTW BS 700 AND BS 718 IAW SRM 51-24-16 AND SRM 51-42-06. (K)SDR A6WA200840018Bulkhead · gougedGOUGE FOUND ON AFT OF FLIGHT COMPARTMENT BULKHEAD RBL9, WL 97.50 (.250 X 300). (K)SDR A6WA200840042Angle · crackedONE ANGLE IS CRACKED ON LT PYLON ACCESS PANEL 412BT. ANGLE ON LT PYLON ACCESS PANEL 412BT, REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840040Floor Support · crackedCRACK ON FLOOR SUPPORT STRUCTURE FS 280, RBL 9. REPAIRED IAW REO 61R-53-11-171, REV D. (K)SDR A6WA200840028Bulkhead · corrodedFRETTING FOUND ON AFT OF FLIGHT COMPARTMENT OF BULKHEAD RBL 9, WL 97.50 (250 X 300) .002 DEEP. FRETTING REMOVED IAW SRM 51-12-00. SURFACE FINISH APPLY IAW SRM 51-25-16. (K)SDR A6WA200840027Attach Fitting · crackedFS621.0 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE JUNCTION, ONE CLIP CRACKED. LT FS 621.00 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE INTERCOSTAL QTY (1) ONE CLIP REPLACED IAW SRM 51-24-16 AND SRM 51-42-21. (K)SDR A6WA200840024Intercostal · crackedCRACK EXIST ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. BRACKET REPLACED ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. (K)SDR A6WA200840023Floor Support · crackedCRACK EXIST ON FLOOR SUPPORT STRUCTURE FS621, LBL 41. CRACK REMOVED ON FLOOR SUPPORT STRUCTURE FS 621, LBL 41 IAW REO 601R-53-61-117. (K)SDR A6WA200840022Intercostal · crackedCRACK EXIST ON INTERCOSTAL RBL 27, FS 484. BRACKET ON INTERCOSTAL RBL 27, FS 484, REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840021Floorbeam · crackedANGLE CRACK ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9. NEW ANGLE INSTALLED ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9, SRM 51-42-20. (K)SDR A6WA200840038Stringer Clip · crackedBTW FS 621.00 AT RT STR 14 STRINGER CLIP CRACKED. NEW STRINGER CLIP INSTALLED IAW SRM 51-42-20. (K)SDR A6WA200840037Bulkhead · crackedCRACK SUSPECTED ON LT FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE FITTING CUTOUT. REPAIR PERFORMED ON FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE CUTOUT IAW REO 601R-53-11-563. (K)SDR A6WA200840036Nose Cowl · wornLT ENGINE LOWER NOSE COWL (432AB) AFT CORNER WORN THIN.. (K)SDR A6WA200840034Nose Cowl · wornLT ENGINE UPPER NOSE COWL (432AT) AFT CORNER WORN THIN. REPLACED ON LT ENG UPPER NOSE COWL (432AT) AFT CORNER IAW CMM 71-14-01-300-814-A01. (K)SDR A6WA200840033Bracket · gougedBRACKET ASSY FWD AND AFT OF CARGO STEP PLATE FOUND GOUGED. BRACKET ASSY FWD AND AFT ON CARGO STEP PLATE REPLACED IAW SRM 51-42-21. (K)SDR A6WA200840029Hinge · damagedPASSENGER DOOR VERTICAL FOLDING STEP HINGE REPLACED IAW SRM 51-42-06. (K)SDR A6WA200840045Handle · crackedHANDLE ASSY CRACKED ON AVIONIC BAY DOOR. HANDLE ASSY REPLACED ON AVIONIC BAY ACCESS DOOR IAW SRM 51-42-06 IAW AMM 52-41-03-400-801. (K)SDR A6WA200840043Support Fitting · damagedLT HANDRAIL SUPPORT FITTING CHAFED AND BENT ON PAX DOOR. REPLACED LT HANDRAIL SUPPORT FITTING ON PAX DOOR. (K)SDR A6WA200840035Support Bracket · crackedMLG BAY LT HYDRAULIC SUPPORT BRACKET FOUND CRACKED. MLG BAY LT NEW HYDRAULIC SUPPORT BRACKET INSTALLED IAW SRM 51-42-06. (K)SDR A6WA200740544Adc · malfunctionedAIR RETURN, AFTER TAKEOFF RECEIVED AIRSPEED, ALTITUDE, HEADING MESSAGES ON PFD2, COMPLIED WITH QRH FOR EACH AS WELL AS ADC FAILURE. REPLACED NR 2 ADC USING AMM 34-13-01. PERFORMED OPS CHECK OF ADC NR 2 USING AMM 34-13-01-710-801 CHECK GOOD. PERFORMED FUNCTISDR A6WA200740092Connector · defectiveCIRCUIT BREAKER PANEL 1, K3 POPPED (WEATHER RADAR RT). REMOVED AND REPLACED RADAR ANTENNA ELEC CONNECTOR AND WEATHER RADAR ANTENNA IAW AMM 34-41-01. REMOVED AND REPLACED WEATHER RADAR CONTROL PANEL IAW 34-41-04, RAN OPS CHECK OF WEATHER RADAR IAW AMM 34-41-0SDR A6WA200740041Sensor · malfunctionedFLAP FAIL CAUTION MESSAGE INFLIGHT, FAILED AT ZERO. PERFORMED EXTERNAL VISUAL INSPECTION OF EACH OUTBOARD FLAP, NO EVIDENCE OF TWISTING, SQUEEZING OR ABNORMAL DEFORMATIONS, RESET. UPON INSPECTION OF THE FECU FOUND LEFT BPSU SENSOR FAULT ERROR CODES. REMOVEDSDR A6WA200640400Unknown · unknownCLIMBING OUT AT 5000 FT FLAPS AT ZERO, FLAP FAIL AMBER CAUTION CAS MESSAGE, CW QRH. PERFORMED ZERO FLAP LANDING, APPLIED BRAKES AT 80 KNOTS, MAX BTMS READING WAS 3. NORMAL LANDING WEIGHT. PERFORMED INSPECTION IAW AWAC SUPPLEMENT 98-18, NO EVIDENCE OF TWISTISDR A6WA200640382Pitot Tube · fodSMOKE ODOR IN COCKPIT AFTER ENGINE SHUTDOWN AND LEAVING AIRCRAFT CHECKLIST WITH BATTERY MASTER ON. INSPECTED PITOT SYS FOUND FOD IN RT PITOT TUBE REMOVED AND REPLACED RT PITOT TUBE RUN PITOT STATIC LEAK CHECK, NO LEAKS FOUND, SYSTEM CHECKS NORMAL. (K)SDR A6WA200640379Window · failedF/O WINDOW SHATTERED. REMOVED AND REPLACED F/O SIDE WINDOW IAW AMM. OPS CHECK AND LEAK CHECK GOOD. (K)SDR A6WA200640264Skin · gougedFOUND GOUGED DENT AT FS 643 APPROX 6 INCHES LONG BETWEEN STRINGER 23 AND STRINGER 24. (M)SDR A6WA200640262Skin · ground damageFOUND FUSELAGE DAMAGED BY BELT LOADER UNDER CARGO DOOR BETWEEN FS 605.00 AND FS 621.00 AND STR 22L TO STR 0 CL. MAINTENANCE PERFORMED MAJOR REPAIR TO FS 605 AND FS 621 AT STRINGER 22L TO STRINGER 25L IAW BOMBARDIER SERVICES CORPORATION EO 601R-53-9415. (M)SDR A6WA200640261Skin · puncturedAIRCRAFT FUSELAGE PUNCTURED BY BELT LOADER AT FS 640.00 BETWEEN STRINGERS 23L AND 24L. (M)SDR A6WA200640139Sensor · failedWHILE RUNNING LT PACK IN AUTO MODE AT FULL COLD DUCT TEMP EXCEEDED 100 C, SMOKE IN COCKPIT, SHUT OFF PACK AND SMOKE CLEARED. CM ACTION C/W PLACARDED AND PLACED ON MEL. REMOVED AND REPLACED LT PACK TEMP SENSOR (RT4HB) OPS CHECK GOOD. REMOVED FROM MEL AND PLASDR A6WA200640126Acm · smokeSMOKE IN COCKPIT AND CABIN ON GROUND AT GATE. REMOVED AND REPLACED LT AIR CYCLE MACHINE, OPS CHECK GOOD IAW AMM, THIS CLEARS MEL, PLACARD REMOVED. (K)SDR A6WA200640045Floor Support · crackedCARGO FLOOR SUPPORT RT SIDE AT FS 621 CRACKED .50 INCH LONG. MAINTENANCE REPAIRED CARGO FLOOR SUPPORT AT FS 621.00 RT SIDE IAW REO. (K)SDR A6WA200640044Intercostal · crackedFS 484 INTERCOSTAL ANGLE AT LBL 36 IS CRACKED. MAINTENANCE REPAIRED FS 484 INTERCOSTAL ANGLE AT LBL36 IAW REO. (K)SDR A6WA200640043Angle · crackedFS 484 INTERCOSTAL ANGLE AT RBL 36 IS CRACKED. MAINTENANCE REPAIRED FS 484 INTERCOSTAL ANGLE AT RBL 36 IAW REO. (K)SDR A6WA200640049Structure · corrodedRT WING PLANK HOLE NR 14 HAS CORROSION AT IB SIDE 8 INCH L X .002 INCH-.003 INCH DEEP AND AT OB SIDE 5 INCH L X .001 INCH-.002 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 274.319 HOLE NR 14 IAW REO. (K)SDR A6WA200640047Skin · corrodedRT WING PLANK HOLE NR 15 HAS CORRODION AT IB AFT SIDE 4 INCHES L X .002 INCH-.003 INCH D AND IB FWD SIDE 1.5 INCH L X .001 INCH - .002 INCH D AND AT OB SIDE 1 INCH L X .002 INCH-.003 INCH D. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLESDR A6WA200640046Skin · corrodedRT WING PLANK HOLE NR 16 HAS CORROSION AROUND ENTIRE OPENING .003 INCH-.005D IN CRITICAL AREA. MAINTENANCE REPAIRED RT WING PLANK ACCESS HOLE AT WS 303.861 HOLE NR 16 IAW REO. (K)SDR A6WA200640051Skin · corrodedFOUND RIGHT WING PLANK HOLE NR 11 HAS CORROSION AT OUTBOARD SIDE 2 INCHES LONG BY .002 INCH - .003 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 209.040 HOLE NR 11 IAW BOMBARDIER REO 601R-57-21-030 REV D. (M)SDR A6WA200640052Skin · corrodedFOUND RIGHT WING HOLE NR 1 HAS CORROSION ON THE INBOARD SIDE 2 INCHES LONG BY .003 INCH - .005 INCH DEEP AND AT OUTBOARD AFT SIDE 1.3 INCH LONG BY .003 INCH - .005 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 54.89SDR A6WA200640050Skin · corrodedFOUND RIGHT WING PLANK HOLE NR 12 HAS CORROSION AT INBOARD SIDE 7 INCHES LONG BY .005 INCH - .005 INCH DEEP AND AT OUTBOARD SIDE 6 INCHES LONG BY .003 INCH - .5 INCH DEEP. NOT IN CRITICAL AREA. MAINTENANCE REPAIRED RIGHT WING PLANK ACCESS HOLE AT WS 230.415 SDR A6WA200640038Clip · crackedFS 280 FLOORBEAM CLIP OB SIDE LBL 9 IS CRACKED NEAR RADIUS APPROX .50 INCH. MAINTENANCE INSTALLED NEW CLIP OB SIDE LBL 9 IAW SRM. (K)SDR A6WA200640042Fitting · wornRT OB FLAP, OB ROLLER GUIDE ON FIXED VANE IS WORN TO MINIMUM LIMITS. MAINTENANCE REMOVED AND REPLACED FLAP FITTING IAW REO. (K)SDR A6WA200640041Clip · crackedFS 280 FLOORBEAM CLIP OB SIDE RBL 9 IS CRACKED REAR RADIUS APPROX .50 INCH. MAINTENANCE REMOVED AND REPLACED BRACKET PN 601R31113-58 IAW SRM. (K)
Back to N428AW