N448AW

Service difficulty reports · 184

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 = 'N448AW' 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 A6WA200940077Floorbeam · crackedPREVIOUSLY REPAIRED ANGLE AND CLIP CRACKED AT F/S 484, RBL 27 AND RBL 36.0 (REF REO 53-41-059 REV A) FABRICATED ANGLE AND CLIP AND INSTALLED. (K)Feb 18, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940076Structure · crackedPAX DOOR EDGE MEMBER FWD CORNER CRACK, CRACK LENGTH .400 CUT OUT PERFORMED ON PAX DOOR EDGE MEMBER IAW REO 601R-52-11-279. EDDY CURRENT PERFORMED ON CUT-OUT IAW REO 601R-52-11-279. REPAIR PERFORMED ON PAX DOOR EDGE MEMBER FWD CORNER IAW REO 52-11-279. (K)Feb 18, 2009 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940075Sill · crackedLT FLOOR SILL CRACKED AT FS 574.00 UNDER STOP BRACKET. LT FLOOR SILL CRACK AT FS 574 UNDER STOP BRACKET REPAIR IAW REO 601R-53-61-1741. (K)Feb 18, 2009 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940084Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED, CRACK LENGTH .800, REPAIR TO PAX DOOR AFT DRAG ANGLE CARRIED OUT IAW REO 601R-52-11-513, REV A. (K)Feb 17, 2009 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200940083Floorbeam · crackedAFT FLOOR ANGLE AT RBL 9.0, FS 280.00. FOUND CRACKED AFT FLOOR ANGLE AT RBL 9.0, FS 280.0. REPAIRED IAW REO 601R 53-11-136, REV A. (K) Feb 15, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940081Floorbeam · crackedINBD CLIP FOUND CRACKED, FS 280, RBL 9.0. INBD CLIP REPLACED AT FS 280.0, RBL 9.0 IAW SRM 51-42. (K)Feb 15, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200840584Element · malfunctionedLT 14TH DUCT WARNING MESSAGE EN ROUTE. COMPLIED WITH QRH. R&R LT PYLON 14TH STAGE SENSE ELEMENT IAW 36-21-00. OPS CHECK GOOD.Aug 28, 2008 · N448AW · Cndair CL6002B19 · Overheat DetectionSDR A6WA200840563Bpsu · malfunctionedFLAP FAIL ON TAXI OUT AFTER SHORT TURN. ATTEMPT TO RESET PER FIM DID NOT CLEAR MESSAGE. FLAPS AT ZERO. LT BPSU REPLACED IAW AMM 27-51-10-400-801. RIGGING CARRIED OUT AND OPS CHECK CARRIED OUT IAW 27-51-10-220-802. OPS CHECK GOOD. OK FOR SERVICE.Aug 11, 2008 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840561Pdu · failedFLAPS FAIL AT 20 DEGREES ON APPROACH. R&R FLAP PDU PER AMM 27-53-01, OPS CHECK GOOD.Aug 10, 2008 · N448AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840559Flap · malfunctionedFLAPS FAIL AT 30 DEGREES ON APPROACH REF PREVIOUS WRITE UP. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RESET OK.Aug 6, 2008 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840558Flap System · failedFLAPS FAIL AT ZERO DURING APPROACH. FOUND REPEAT LT BPSU, FECU, WIRING FAULT CODES. CONTINUITY RESISTANCE & MEGGER CHECKED LT BPSU WIRING. NO FAULTS FOUND. REPLACED FECU PER AMM CH 27-50. OPS CHECK AND RIG CHECKS GOOD.Aug 4, 2008 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840552Sensor · failedFLAPS FAIL MESSAGE FROM 30 TO 45 ON LANDING. FLAPS FAILED AT 30 DEGREES. REMOVED AND REPLACED LT BRAKE POSITION SENSOR UNIT PER AMM 27-54-01, OPS AND RIG CHECK GOOD. (S)Jul 25, 2008 · N448AW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR A6WA200840549Flap System · failedFLAPS FAILED AT ZERO AFTER TAKEOFF. DID NOT LAND OVERWEIGHT. CORRECTIVE ACTION IN PROGRESS. (A)Jul 23, 2008 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840548Flap System · failedFLAP FAIL CAS MESSAGE ILLUMINATED AT 100FT AGL WITH FLAPS AT 45 DEGREES, MESSAGE ILLUMINATED APPROXIMATELY 1 MINUTE AFTER FLAPS INDICATED AT 45 DEGREES. C/W AWAC SUPP 98-018B RESET C/B`S INTERROGATED FECU, RAN FLAP SYS NO DEFECTS NOTED AT THIS TIME.Jul 22, 2008 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200840235Windshield · crackedON DESCENT CAPTAINS WINDSHIELD CRACKED. COMPLIED WITH QRH, CYCLED HEAT `OFF`, THEN `ON` THEN BACK `OFF`, AFTER RECEIVING LT WINDSHIELD HEAT CAS MESSAGE. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW AMM 56-11-01. (M)Mar 24, 2008 · N448AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200840056Warning System · activatedIDG NR 1 CAUTION MESSAGE ON TAKEOFF, TAKEOFF ABORTED AT LESS THAN 80 KNOTS. (K)Jan 30, 2008 · N448AW · Cndair CL6002B19 · AC Indicating SystemSDR A6WA200740200Flap System · malfunctionedFLAPS FAIL IN FLIGHT WHEN FLAPS 8 DEGREES SELECTED, FLAPS FAILED AT 0 DEGREES. VISUALLY INSPECTED EACH OB FLAP NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATION NOTED. OB FLAP POSITION INDICATION ARE NOT OUTSIDE GO RANGE. FLAP FAIL MESSAGE NOT ILLUMIApr 17, 2007 · N448AW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200740090Relay · damagedON AC SYNOPTIC PAGE, ADG BUSS DISPLAYED IN WHITE. AC1 AND AC2 BUSS SHOW WHITE LINES TO ESS BUSS, ESS BUSS IS GREEN. REMOVED AND REPLACED ADG ESSENTIAL TRANSFER CONTACTOR (KX2D). PERFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 24-51-31. (K)Mar 2, 2007 · N448AW · Cndair CL6002B19 · Alternator-Generator DriveSDR A6WA200740072Spar · misdrilledWHILE PERFORMING E03/062/457 MODIFICATION LT AND RT WING REAR SPARS, A FASTENER HOLE WAS MISDRILLED. HOLE DIAMETER .213 INCH AT TRAILING EDGE WS 129, 2 INCHES IB OF JACKING PAD POINT ON RT WING. (M) MAINTENANCE REAMED HOLE TO ACCOMMODATE .25 INCH HOLE TO BE Feb 24, 2007 · N448AW · Cndair CL6002B19 · Wing SparSDR A6WA200740071Structure · damagedFOUND NR 15 HOLE AT WS 148 LHS IS ELONGATED TO .230 INCH. (M) MAINTENANCE REPAIRED BY CLEANING UP HOLE AND INSTALLING FREEZE PLUG IAW EO 601R57-10925A. (K)Feb 22, 2007 · N448AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA200740070Angle · crackedFOUND FS 484 ANGLE IS CRACKED AT RBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)Feb 21, 2007 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740069Angle · crackedFOUND FS 484 ANGLE IS CRACKED AT LBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)Feb 21, 2007 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740066Angle · crackedLT AND RT FS 625.00 OBLIQUE ANGLES ARE CRACKED .5 INCH LONG ON AFT RADIUS. (K) MAINTENANCE DRILLED OFF, REMOVED CRACKED OBLIQUE ANGLES LT AND RT FS 625 DRILLED UP, ALODINED AND INSTALLED ANGLES PN 601-35012-51 (LT AND 601-35012-529 (RT). OBLIQUE ANGLES INSTFeb 17, 2007 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740065Fitting · crackedFS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB RBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF RBL 9 MFG STANDARD REPAIR NR 601R-53-0057A, STEPS 1 THRU 4. (K)Feb 17, 2007 · N448AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740064Fitting · crackedFS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB OF LBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF LBL 9 IAW MFG STANDARD REPAIR NR 601R-53-0057A STEPS 1 THRU 4. (K)Feb 17, 2007 · N448AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200740063Bracket · crackedHYDRAULIC TRANSDUCER HAT CHANNEL CRACKED APPROX .1 INCH LONG LT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)Feb 16, 2007 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200740062Bracket · crackedHYDRAULIC TRANSDUCER HAT CHANNEL APPROX .1 INCH LONG RT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)Feb 16, 2007 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640366Skin · dentedINBOARD LEFT FLAP LOWER SKIN HAS DENT WITH GOUGE LOCATED 3.75 INCH FROM INBOARD EDGE AND 8.5 INCH FORWARD OF T/E MEASURES 2 INCHES BY 2 INCHES BY .098 INCH DEEP. REPAIRED LEFT INBOARD FLAP LOWER SKIN BY INSTALLING EXTERNAL DOUBLER IAW BSC EO 601R-57-9969. (MOct 3, 2006 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA200540071Bushing · migratedLEFT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .050 INCH AT WS 66. (M)Feb 17, 2005 · N448AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540072Bushing · migratedRIGHT AFT MAIN LANDING GEAR TRUNNION BUSHING IS MIGRATED .041 INCH, AT WS 66. (M)Feb 17, 2005 · N448AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540073Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621, LBL 36, WL 73 IS CRACKED, APPROXIMATELY .25 INCH. (M)Feb 17, 2005 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540069Angle · crackedRT FS 621 ANGLE HAS A .5 INCH CRACK ON OUTBOARD RADIUS. S/D - REPAIRED CRACKED RT FS 621 ANGLE BY CUTTING AWAY DAMAGED AREA AND INSTALLING REPAIR ANGLE AND STRAP IAW BOMBARDIER REO 601R-53-61-117 REV C. (M)Feb 16, 2005 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440009Windshield · failedCAPTAINS FORWARD WINDSHIELD SHATTERED IN FLIGHT. REMOVED AND REPLACED WINDSHIELD. (M)Jan 18, 2004 · N448AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA200340136Controller · intermittentINTERMITTENT RT ENGINE FIRE FAIL CAS INDICATION INFLIGHT AT ONE TIME FOR 3 SECONDS ENGINE FIRE CAS MESSAGE. REMOVED AND REPLACED FIRE DETECTION CONTROLLER. (M)Sep 11, 2003 · N448AW · Cndair CL6002B19 · Fire Detection
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