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 A6WA201240723Angle · corrodedPAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 & FS 349.00 AT WL 73 CORRODED. R & R PAX DOOR LOWER SURROUND STRUCTURE ANGLE BETWEEN FS 310.00 AND FS 349.00 AT WL 73 IAW SRM 51-42-06 & 51-42-21.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240718Hinge Fitting · gougedRIGHT OTBD FLAP, OTBD FORWARD HINGE BOX HAS A GOUGE BEHIND THE FORWARD INBD FLAP HINGE BOX FAIRING ATTACH POINT. BLENDED AND ROTO PEENED RT OTBD FLAP, OTBD FWD HINGE BOX IAW REO 601R-57-21-1715 SRM 51-40-11, 51-12-00, 51-28-11, 51-25-06, 51-25-16, 51-24-11.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240717Hinge Fitting · gougedLT OTBD FLAP, OTBD HINGE BOX IS GOUGED BY FAIRING ATTACHMENT FASTENER INBD FWD LT OTBD FLAP OTBD HINGE BOX BLENDED AND SHOT PEENED IAW REO 601R-57-21-1715, SRM 51-25-16, 51-12-00, 51-40-11, 51-24-11, 51-21-11, 51-25-06.Jul 21, 2012 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240719Retainer · damagedCARGO DOOR SEAL RETAINER DAMAGED. REMOVED DAMAGED CARGO DOOR SEAL RETAINER AND REPLACED WITH NEW SERVICEABLE IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240715Support Bracket · crackedCARGO DOOR LOWER FWD SUPPORT BRACKET IS CRACKED. REMOVED CRACKED CARGO DOOR LOWER FWD SUPPORT BRACKET INSTALLED NEW SERVICEABLE CARGO DOOR LOWER FORWARD BRACKET IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240721Mount Bracket · crackedPAX DOOR POWER ASSIST MOTOR MOUNTING BRACKET IS CRACKED. REMOVED CRACKED MOUNTING BRACKET THEN INSTALLED NEW SERVICEABLE BRACKET PN 601R317745-7 IAW SRM 51-42-06.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240716Support Bracket · crackedRT JETPIPE UPPER CORE COWL STANG ROD SUPPORT BRACKET ASSY MISSING RIVET AND STIFFENER AT XN214 CRACKED. R & R STIFFENER IAW CMM 78-11-00, SRS 042.Jul 20, 2012 · N448AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201240722Handle · crackedPAX DOOR EXTERIOR OPEN HANDLE IS CRACKED. REMOVED CRACKED OUTER HANDLE FROM PAX DOOR AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW AMM 52-11-03.Jul 19, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240704Handle · crackedCARGO DOOR HANDLE CRACKED ON FLANGE. REMOVED DAMAGED HANDLE ASSY AND REPLACED WITH NEW SERVICEABLE HANDLE ASSY, PN H3415-31 IAW SRM 51-42-01, 51-42-21 AND AMM 52-31-03.Jul 19, 2012 · N448AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201240714Hinge · damagedPAX DOOR FUSELAGE HINGE HALF HAS DAMAGE FROM ROLL PIN COMPLIED WITH REO 601R-52-11-1347.Jul 18, 2012 · N448AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201240712Attach Angle · crackedPAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IS CRACKED. R & R PAX DOOR LATCH CAM COVER PLATE AFT ATTACH ANGLE IAW SRM 51-41-02.Jul 18, 2012 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240713Hinge · chafedPAX DOOR HINGE HAS CHAFED LUGS. COMPLIED WITH REO 601R-52-11-1347.Jul 18, 2012 · N448AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201240766Trunnion · damagedFOUND OVERSIZE HOLE IN LT MLG LOWER TRUNNION FLANGE AFT MOST HOLE IN DOUBLER WHILE PERFORMING COLD WORKING. REPAIRED 1 EA DISCREPANT HOLE IN LT LOWER MLG TRUNNION FLANGE IAW REO 601R-57-21-1714, REV 2012 7/14.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA201240710Attach Bracket · crackedHYDRAULIC NR 3 BRAKE ACCUMULATOR BRACKET FWD CRACKED. R & R 3 ATTACH BRACKET IAW SRM 51-42-21.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240711Seat Track · corrodedCORROSION FOUND ON CARGO TRACKS AT LBL 9 & RBL 9 AT FS 568-559+110. R & R CARGO TRACKS WITH SERVICEABLE IAW AMM 53-01-11.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240708Door · chafedAPU ENCLOSURE DOOR HAS CHAFE ON INSIDE. REMOVED CHAFE DAMAGE ON APU ENCLOSURE DOOR IAW REO 601R-49-11-070, REV B.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR A6WA201240709Door · crackedAPU ENCLOSURE DOOR HAS MULTIPLE CRACKS. REPAIRED CRACKS ON APU DOOR, 3 EA, IAW REO 601R-49-11-070, REV B.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Auxiliary Power Unit (APU) DoorsSDR A6WA201240705Bulkhead · damagedRT AFT SIDE OF 280 BULKHEAD HAS DAMAGE ON PREVIOUS REPAIR FROM CONTACT WITH GALLEY STORAGE DOOR. BLENDED OUT MINOR SURFACE DAMAGE AND RESTORED PROTECTIVE FINISH IAW SRM 51-12-00, 51-21-11, 51-25-06, 51-25-16.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240706Mount Bracket · crackedRT MLG WW PRESSURE TRANSDUCER MOUNT BRACKET CRACKED. R & R CRACKED BRACKET IN RT MLG WW PRESSURE TRANSDUCER MOUNT BRACKET WITH NEW SERVICEABLE PN 601R75262-157 IAW SRM 51-42-06, 51-40-11, 51-25-06.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240707Bracket · crackedLT MLG WHEEL WELL PRESSURE TRANSDUCER MOUNT BRACKET CRACKED. R & R CRACKED BRACKET ON LT MLG WW WITH NEW IAW SR 51-42-06 AND 51-40-11.Jul 17, 2012 · N448AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA201240767Post · crackedRBL 27 POST AT FS 409+128 CRACKED ON LOWER END. COMPLIED WITH REO 601R-53-41-056, REV F.Jul 14, 2012 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240720Threshold · corrodedSERVICE DOOR THRESHOLD HAS SEVERAL CORRODED FASTENER HOLES AND CRACKED. REMOVED UNSERVICEABLE SERVICE DOOR THRESHOLD AND REPLACED WITH SERVICEABLE SERVICE DOOR THRESHOLD IAW SRM 51-41-00.Apr 18, 2012 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140211O-Ring · missingLT ENG LOW OIL PRESS INDICATION. OIL PRESSURE AT 37 PSI. CW, QRH, REDUCED TO IDLE. OIL PRESSURE DROPPED TO 35 PSI. OIL PRESSURE 27-31 PSI TIL SHORT FINAL THEN DROPPED TO 25 PSI. JUST PRIOR LDG AND 20 PSI JUST AFTER LDG. SHUTDOWN ENGINE AFTER LANDING. FOMar 28, 2011 · N448AW · Cndair CL6002B19 · AC Generator-AlternatorSDR A6WA201040939Bulkhead · crackedFS 202 BULKHEAD CRACKED AROUND BRAKE PUSH-PULL ROD. REPAIRED BULKHEAD AT FS 202.00 BY FULLY INCORPORATING REO 601R-53-11-2009.Nov 1, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040952Skin · gougedTOP OF RT FLIGHT SPOILER AT CTR T/E IS GOUGED. REPAIRED RT FLIGHT SPOILER UPPER SKIN BETWEEN SPOILER STA 195.3603 AND SPOILER STA 204.3603 IAW REO 601R-57-73-133.Nov 1, 2010 · N448AW · Cndair CL6002B19 · SpoilersSDR A6WA201040947Skin · chafedLT AILERON UPPER L/E IS CHAFED. REPAIRED AREAS AILERON STA 302-304 AILERON 309-321 AND AILERON STA 360-345 IAW REO 601R-57-60-013, NC.Nov 1, 2010 · N448AW · Cndair CL6002B19 · AileronsSDR A6WA201040801Bulkhead · damagedFOUND MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 REPAIR. REPAIRED MISLOCATED FUEL QTY CONNECTOR PLUG HOLE ON RT 559 IAW DEVIATION REO 601R-53-41-1303.Oct 30, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040949Fitting · chafedRT OTBD FLAP INBD ROLLER GUIDE FITTING CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00, EDDY CURRENT INSPECTION IAW NDTM 51-20-06. ROTO PEEN REWORKED AREA SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040951Fitting · chafedRT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER CHAFED. BLENDED OUT CHAFED AREA IAW SRM 51-12-00, EDDY CURRENT INSPECT IAW NDTM 51-20-06, ROTOPEEN IAW SRM 51-24-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040944Fitting · chafedLT OTBD FLAP INBD ROLLER FITTING BENEATH ROLLER IS CHAFED. BLENDED OUT DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00, EDDY CURRENT INSPECTED IAW 51-20-06 SHOT PEEN IAW SRM 51-24-11. RESTORED PROCTINO FINISH IAW SRM 51-21-16.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040943Track · chafedRT THRUST REVERSER UPPER PYLON TRACK CHAFED. BLENDED OUT CHAFE AREA TO SMOOTH CONTOUR IAW SRM 51-12-00, NOT EXCEDING REPORTED DEPTH EDDY CURRENT INSPECTED, RESTORED FINISH IAW CMM 20-21-11.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040954Sidewall Panel · crackedAFT STAIR SIDEWALL CRACKED ABOVE PANEL 832FR. REPAIRED AFT STAIR PANEL SIDEWALL ABOVE 832FR IAW REO 601R-52-11-702, REV C.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040953Skin · crackedAFT PAX DOOR AIRSTAIR SKIN CRACKED UNDER STEP 832DT. REPAIRED AFT SKIN UNDER STEP 832DT IAW REO 601R-52-11-702, REV C.Oct 29, 2010 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040948Rib · crackedLT WING BATT RIB IS CRACKED. REPAIRED LT WING BATT RIB AT WS 53.60 IAW REO 601R-57-51-046, REV B, REPAIR NR 2.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040946Skin · chafedLT INBD FLAP VANE L/E INBD CTR AND OTBD CHAFED. REPAIR LT INBD FLAP VANE SKIN AT FLAP STA 137.012 AND BETWEEN FLAP STA 98.509 AND 108.135 IAW REO 601R-57-52-004, REV C. R & R LT INBD FLAP VANE INBD L/E SIN IAW SRM 51-42-13.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040955Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED ON PREVIOUS REPAIR. REPAIRED AFT DRAG ANGLE IAW REO 601R-52-11-513, REV A.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040809Skin · chafedRT INBD FLAP, FLAP VANE SKIN L/E CHAFED AT INBD CTR OTBD ENDS BLENDED CTR AND OTBD LOCATIONS ARE WITHIN LIMITS, INBD VANE L/E LOCATION REPLACED L/E SKIN COMPLETING WORK IAW REO 601R-57-52-004, REV C, SRM 51-42-13.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040800Panel · corrodedFUEL C/O FOR PNL 550CB REQUIRE AWAC E06/021/457 CURRENT REV TO BE C/W INDICATION FOUND ON AFT OTBD SIDE. REPAIRED FUEL PANEL C/O PNL 550CB IAW REO 601R-57-21-030 REV H, AT APT OTBD SIDE DETAIL III.Oct 28, 2010 · N448AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA201040941Bulkhead · chafedFS 280, RBL 9 APPROX 18" FROM FLOOR ON BACKSIDE OF BULKHEAD HAS 2 AREAS OF CHAFING. REPAIRED FS 280 BULKHEAD AT RBL 11.0 BETWEEN STR 13A & 14A REO 601R-53-11-1727, REV D.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201040940Fitting · crackedLBL9 INBD CLIP FS 280 CRACKED. R & R CLIP AT FS 280, INBD SIDE OF LBL 9.0 IAW SRM 51-42-21.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040808Angle · crackedRT OBLIQUE ANGLE AT FS 625.00 IS CRACKED. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-100.Oct 27, 2010 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040950Plate · chafedRT INBD FLAP INBD OF LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.Oct 25, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040945Plate · chafedLT INBD FLAP INBD AFT LUG PLATE HAS CHAFE DAMAGE WS 80.50. REPAIRED IAW REO 601R-57-52-1536, TYPE I.Oct 25, 2010 · N448AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040942Bearing · out of toleranceREPLACE MIDDLE (UPPER & LOWER) RUDDER HINGE BEARINGS ON ACFT WITH RUDDER PN 601R22014-1. R & R BEARINGS.Oct 24, 2010 · N448AW · Cndair CL6002B19 · Rudder StructureSDR A6WA200940815Anti-Ice System · warning messageANTI ICE DUCT WARNING ON TAKE OFF SYNOPTIC PAGE INDICATES LEFT FUSELAGE, MESSAGE DID NOT CLEAR WHEN 14TH STAGE AIR SELECTED OFF. C/A IN PROGRESS.Jan 1, 2010 · N448AW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR A6WA200940085Threshold · corrodedSERVICE DOOR THRESHOLD CORRODED. CORROSION REMOVED IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-00-00. SERVICE DOOR THRESHOLD PLATE REPLACED IAW CRJ 200 51-41-02. (K)Feb 21, 2009 · N448AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940082Floorbeam · crackedAFT FLOORBEAM ANGLE AT LBL 9.00, FS 280.00 FOUND CRACKED AFT FLOOR ANGLE AT LBL 9.0, FS 280. REPAIRED IAW REO 601R-53-11-136 REV A. (K)Feb 20, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940080Floorbeam · crackedOTBD CLIP CRACKED AT FS 280.00, LBL 9.0, OTBD CLIP AT FS 280.00 AND LBL 9.00. REPLACED IAW SRM 51-52-21. (K)Feb 20, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200940079Beam · crackedCARGO DOOR UPPER BEAM LOWER ANGLE AT FS 621.00 (PRESSURE BULKHEAD) CRACKED. CARGO DOOR UPPER BEAM LOWER ANGLE AT FS 621 (BULKHEAD PRESSURE) REPLACED IAW SRM 51-42-21. (K)Feb 19, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200940078Floorbeam · crackedPREVIOUS REPAIR, ANGLE AND CLIP CRACKED AT FS 480.00, LBL 27.00 AND LBL 36.00. AND ANGLE AND CLIP ARE REPLACED IAW SRM 51-42-21. (K)Feb 19, 2009 · N448AW · Cndair CL6002B19 · Fuselage Main, Floor Beam
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