N408AW

Service difficulty reports · 202

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 = 'N408AW' 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 A6WA2013073141114Mount Bracket · bentNR 2 HYD ECO BOTTLE MOUNT IS BENT AND CRACKED ON UPPER FWD R/B CORNER. REMOVE, DUPLICATE AND INSTALL MOUNT WEB BRACKET.Jul 17, 2013 · N408AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2013073141113Angle · crackedRT ANGLE IS CRACKED, R & R.Jul 17, 2013 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013073141112Angle · crackedLT ANGLE IS CRACKED. R & R.Jul 17, 2013 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013073141102Seat Track · corrodedCORROSION ON LT SEAT TRACK FS 409+48. R & R SEAT TRACK IAW 51-41-02.Jul 17, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141120Vane · chafedRIGHT INBD FLAP VANE L/E HAS CHAFE DAMAGE AT R/B, OTBD AND MID OTBD EDGES. R & R MID OTBD AND R/B L/E BLENDED OTBD L/E TO SMOOTH CONTOUR.Jul 16, 2013 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2013073141103Cargo Track · corrodedCARGO TRACK IS CORRODED AT RBL9 AND BS 559+112 TO 574. R & R WITH SERVICEABLE CARGO TRACK.Jul 16, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141101Seat Track · corrodedEXFOILATION CORROSION ON SEAT TRACK AT FS 559+40 .025 DEEP. REPLACED SEAT TRACK.Jul 16, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141100Seat Track · corrodedCORROSION ON RT SEAT TRACK AT BS 506. REPLACED SEAT TRACK FROM 409+128 - 559.Jul 16, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013407311097Cargo Track · corrodedCARGO TRACK, CORRODED AT RBL 9 AND BS 559+86 TO 559+96. REPLACED UNSERVICEABLE CARGO TRACK WITH SERVICEABLE CARGO TRACK.Jul 16, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141125Support · crackedPAX DOOR ASSIST MOTOR SUPPORT CRACKED. R & R CRACKED SUPPORT WITH PN 601R317745-7 IAW SRM 51-42-06.Jul 15, 2013 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013073141116Stiffener · crackedRT JETPIPE 1ST STIFFENER CRACKED AT 9 O`CLOCK POSITION. REPAIRED IAW AMM 78-11-00, REPAIR SRS 042.Jul 15, 2013 · N408AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA2013073141108Angle · crackedRT INBD ANGLE IS CRACKED AT 484 LBL 27. R & R IAW SRM AND REO.Jul 15, 2013 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013073141099Cargo Track · corrodedCARGO TRACK HAS CORROSION AT LBL9 AND BS 559+112 TO 574, REMOVED AND REPLACED CARGO TRACK.Jul 15, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141110Bracket · crackedANGLE BRACKET IS CRACKED UNDER LT FLOOR SUPPORT AT FS 589. R & R.Jul 14, 2013 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2013073141106Tie Down · corrodedCARGO TIE DOWN CORRODED AT LBL 9 AND BS 584 - 600. REMOVED AND REPLACED TIE DOWN IAW SRM 51-21-06, 53-61-49, 51-41-02 AND AMM 20-21-00.Jul 14, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141105Cargo Track · corrodedCARGO TRACK CORRODED AT LBL 27 AND FS 559+104, 559+112 AND FS 568. REMOVED AND REPLACED CARGO TRACK IAW SRN 51-21-06, 53-51-49, 51-41-02, 53-61-49 AND AMM 20-21-00.Jul 14, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2013073141104Seat Track · corrodedCARGO TRACK IS CORRODED AT LBL 9 AND BS 611 TO 616. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-21-06, 53-61-49, 51-41-02 AND AMM 20-21-00.Jul 14, 2013 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201240356Structure · damagedCLIMBING THRU FL140, LT ENG OBSERVED MOMENTARY OVERSPEED OF N1. NORM ENG INDICATIONS OBSERVED. UPON DECENT LEFT ENGINE THRUST LEVER STUCK AND UNABLE TO REDUCE N1 BELOW 81 PERCENT. COMPLIED WITH QRH, THRUST LEVER JAM PROCEDURE AND SHUTDOWN LEFT ENGINE INFLIMar 17, 2012 · N408AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201240457Link · shearedLEFT ELEVATOR PCU LINK TO PCU ROD END, SHEARED LOWER PIN. CONDITION FOUND DURING "A" CHECK FOUND 2 PCU`S WITH SAME PROBLEM. NR 10K, NR 2 FAILED, NR 3 ON (INBD) HEAD SHEARED, BUT PCU STILL FUNCTION HAD NOT FAILED COMPLETELY.Mar 15, 2012 · N408AW · Cndair CL6002B19 · Elevator Tab Control SystemSDR A6WA201140793Shutoff Valve · malfunctionedAFTER LEVELING OFF, NOTICED INCREASING FUEL IMBALANCE BETWEEN LT AND RT WINGS. RT TRANSFER SOV HAD FAILED TO OPEN, LT TRANSFER SOV WAS OPERATING. AUTO TRANSFLOW ATTEMPTED TO REFILL RT WING FROM LT WING, BUT COULDN`T ELIMINATE IMBALANCE SYNOPTIC PAGE SHOWS RTAug 30, 2011 · N408AW · Cndair CL6002B19 · Fuel Transfer ValveSDR A6WA201140849Vane · chafedRT INBD FLAP VANE ON TOP INBD SIDE AT T/E IS CHAFED. BLENDED CHAFE IAW REO 601R-57-52-1768. DID NOT EXCEED MAXIMUM ALLOWABLE DEPTH TOOL USED AAR 1743 CAL DATE 04/20/12.Aug 27, 2011 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140846Bushing · corrodedLEFT HORIZONTAL STABILIZER BUSHING CORRODED. R & R HORIZONTAL STAB BUSHING IAW SB 601R-55-007.Aug 26, 2011 · N408AW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR A6WA201140855Threshold · corrodedSERVICE DOOR THRESHOLD CORRODED ON BOTTOM SIDE AROUND SCREWS LOCATED AND DRILLED SERVICEABLE THRESHOLD P/N 601R-38957-19 IAW SRM 51-40-11 INSTALLED IAW CMM 25-33-01.Aug 26, 2011 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140791Stringer · chafedLT STRINGER NEX TO LT OIL REPLENISH TUBE CHAFED. REPAIRED LT STRINGER 12 NEXT TO LT OIL REPLENISH TUBE BY INCORPORATING SRM STRINGER. REPAIR CHAPTER 53-00-03, FIG 202, SHEET G.Aug 25, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR A6WA201140845Cleat · erodedPAX DOOR FWD AND AFT CLEATS CORRODED. REPAIRED PAX DOOR AFT CLEAT BY DUPLICATING AND INSTALLING REPAIRED PAX DOOR FWD CLEAT AND INSTALLED IAW SRM 53-00-00 & SRM 51-42-06.Aug 24, 2011 · N408AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140785Torque Box · damagedRT THRUST REVERSER TORQUE BOX HAS NUMEROUS DAMAGED AREAS, REO 78-30-4072.Aug 24, 2011 · N408AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201140789Floorbeam · crackedCLIP AT FS 280 FLOORBEAM APPROX RBL 9 IS CRACKED. R & R CLIPS (INBD & OTBD) IAW REO 601R-53-11-171, REV D.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140790Floorbeam · corrodedTOP ON FLOORBEAM AT FS280 HAS HEAVY CORROSION ACROSS UPPER SURFACE AT FLT DECK ENTRY WAY. R & R FWD FLOORBEAM ANGLE IAW SRM 51-42-06.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140788Floorbeam · crackedCLIP AT FS 280 FLOORBEAM APPROX LBL 9 IS CRACKED. R & R LBL9 CLIPS ( INBD AND OTBD) IAW REO 601R-53-11-171, REV D.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140787Floorbeam · crackedFS 280 FLOORBEAM CRACKED AT APPROX LBL12 BY MLG AFT RELEASE CABLES PULLEY SUPPORT ATTACH BOLT. REPAIR IAW REO 601R-53-11-136, REV A.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140786Floorbeam · crackedFS 280 FLOORBEAM CRACKED APPROX RBL 12. REPAIRED FLOORBEAM IAW REO 601R-53-11-171, REV D.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140777Bracket · crackedNR 2 HYD MANIFOLD BRACKET CRACKED. REPAIRED IAW REO 601R-53-62-031, REV A.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140778Skin · chafedCHAFING AT LT MLG DOOR L/E CHANGED -3 .100" IAW REO 601R-52-82-016.Aug 23, 2011 · N408AW · Cndair CL6002B19 · Landing Gear DoorsSDR A6WA201140844Fairing · chafedCHAFING DAMAGE ON OTBD ENDS OF FAIRING 193AB ON LOWER SKIN UNDER FAIRING MATING SURFACES. REPAIRED DAMAGE IAW REO 601R-57-21-880, REV C, ZONE A.Aug 22, 2011 · N408AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201140848Vane · chafedLT INBD FLAP VANE ON TOP INBD SKIDE OF T/E CHAFED. REPAIRED IAW REO 601R-57-52-1765.Aug 22, 2011 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201140847Structure · chafedLEFT LWR NOSE COWL T/E STRIP CHAFED. R & R T/E STRIP PN 228-50081-107 IAW CMM 71-14-01.Aug 21, 2011 · N408AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201140850Retainer · corrodedMAIN AVIONICS COMPARTMENT DOOR SEAL RETAINER CORRODED. R & R DOOR SEAL RETAINER IAW SRM 51-42-06.Aug 20, 2011 · N408AW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR A6WA201140767Seat Track · corrodedRT NR1 FLOOR SEAT TRACK CORRODED. R & R RT NR1 FLOOR SEAT TRACK.Aug 19, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140768Seat Track · corrodedLT NR1 FLOOR SEAT TRACK CORRODED. R & R LT NR1 FLOOR SEAT TRACK.Aug 19, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA2011081940770Sill · corrodedSEVERAL; AREAS PF CORROSION, LT FLOOR SILL FROM FS 409+128 TO FS 559.00. REMOVED CORROSION FROM LT FLOOR SILL (7 AREAS) FROM FS 409+128 TO FS 559.00.Aug 19, 2011 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201140769Seat Track · corrodedRT NR 2 SEAT TRACK CORRODED. R & R RT NR 2 SEAT TRACK.Aug 19, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201140851Handle · crackedPAX DOOR ESTERNAL HANDLE IS CRACKED. REMOVED UNSERVICEABLE PAX DOOR EXTERNAL HANDLE AND INSTALLED SERVICEABLE PAX DOOR EXTERNAL HANDLE IAW AMM 52-11-03 AND EO EO08/007/452.Aug 18, 2011 · N408AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201140853Hinge Fitting · chafedAFT HINGE LUG ON PAX DOOR HAS CHAFING DAMAGE FROM HINGE PIN. REPAIRED AFT HINGE LUG ON PAX DOOR IAW SRM 51-12-00 AND REO 601R-52-11-1347.Aug 16, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201140852Hinge Fitting · chafedPAX DOOR AFT HINGE LUG ON FUSELAGE SIDE HAS CHAFING DAMAGE IN 2 PLACES. REPAIRED PAX DOOR AFT HINGE LUG ON FUSELAGE SIDE IAW DOOR SRM 51-12-00 AND REO 601R-53-21-814.Aug 16, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Door HingeSDR A6WA201140854Floorbeam · crackedFLOORBEAM CRACKED AT FS484.0, LBL27.0. R & R FLOORBEAM TEE IAW REO 601R-53-41-059.Aug 15, 2011 · N408AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201140776Bracket · crackedU BRACKET AT FS 574 CRACKED AT LOWER EDGE AROUND RIVET, 2 PLACES. R & R U BRACKET WITH SERVICEABLE PART.Aug 14, 2011 · N408AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201140609Carbon Seal · failedON POST FLT WALK AROUND FOUND SMOKE COMING FROM NR 2 JET PIPE AND STRONG ODOR. R & R OF NR 7 CARBON SEAL. OPS AND LEAK CHECK GOOD. REF EMM 72-00-00, SEP 38.Jul 15, 2011 · N408AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA201040936Pdu · malfunctionedWHILE CLIMBING THRU FLIGHT LEVEL 255. RECEIVED R-REV UNLOCK CAUTION MESSAGE. BOTH REVERSER DISARM AT THE TIME MESSAGE RECEIVED. MESSAGE PERSISTED UNTIL ENGINE SHUTDOWN AT GATE C/W QRH. DIVERTED. R & R RT T/R PDU IAW AMM 78-32-03. OPS CHECKED GOOD, REMOVEDec 8, 2010 · N408AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200940696Angle · crackedPRESSURE BULKHEAD AT FS 559.0, LBL 18.0 CRACK AT CAP ANGLE LOCATION PRESSURE BULKHEAD AT FS 559, LBL 18.0. REPAIRED IAW REO 601R-53-41-260, REV D. (K)Oct 16, 2009 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200940697Angle · crackedPRESSURE BULKHEAD AT FS 559, RBL 18.0 CRACKED AT CAP ANGLE LOCATION. PRESSURE BULKHEAD AT FS 559, RBL 18.0 REPAIRED IAW REO 601R-53-41-260 REV D AND REO 601R-53-41-609, REV A. (K)Oct 16, 2009 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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