N438AW

Service difficulty reports · 217

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 = 'N438AW' 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 A6WA201441427Seat Track · corrodedCABIN FLOOR SEAT TRACK AT FS 559+91 & LBL 9 IS CORRODED. REMOVED CORRODED SEAT TRACK & REPLACED WITH NEW SERVICEABLE SECTION IAW AMM 53-01-11 & SRM 51-50-11.Apr 15, 2014 · N438AW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR A6WA201441438Bracket · crackedRIGHT WW HAS BRAKE TRANSDUCER LINE BRACKET CRACKED. R & R CRACKED BRACKET WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06 & 51-40-11.Apr 14, 2014 · N438AW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR A6WA201441437Channel · crackedLEFT TAIL PIPE FAIRING FIRE LOOP CHANNEL IS CRACKED. R & R CRACKED CHANNEL WITH NEW SERVICEABLE CHANNEL IAW CMM 78-11-00-440-001-A01.Apr 12, 2014 · N438AW · Cndair CL6002B19 · Engine Collector/Tailpipe/NozzleSDR A6WA201441123Apu · fireAPU FIRE, PILOTS NOTICED HIGH EGT BUT NO RPM. EMERGENCY CREWS WERE ALERTED. COMPLIED WITH QRH, BOTTLE NEVER DISCHARGED. FIRE WENT OUT ON ITS OWN AFTER SHUTTING DOWN APU. INSPECTED APU & SURROUNDING AREA, NO FIRE DAMAGE NOTED. IAW 25643 4 FOR MEL. VERIFIEFeb 12, 2014 · N438AW · Cndair CL6002B19 · APU Core EngineSDR 2012F00249Warning Message · illuminatedON TAKEOFF ROLL, RECEIVED ANTI-SKID OTBD CAUTION MESSAGE. ABORTED TAKEOFF BELOW 60 KTS.Nov 14, 2012 · N438AW · Cndair CL6002B19 · Brake Anti-Skid SectionSDR A6WA201240416Floorbeam · corrodedFLOORBEAM AT FS 605 AND LBL 27 HAS CORROSION AROUND NUTPLATE. REMOVED CORROSION ON LBL 27 FLOORBEAM CAP AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FLOORBEAM IAW REO 601R-53-21-3778.Apr 12, 2012 · N438AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201240501Vane · dentedRT OTBD FLAP VANE HAS A DENT INBD ON VANE AT WS 162.49. REPAIRED RT OTBD FLAP VANE IAW REO 601R-57-53-041, REV B.Apr 4, 2012 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201240500Angle · crackedFS 621, FWD FACE LBL JUST BELOW W/L 120 ANGLE CRACKED. R & R ANGLE FS 621, LBL 36, W/L 120, SRM 51-40-11, 51-42-21.Apr 4, 2012 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240502Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513, REV A.Apr 3, 2012 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201240499Bulkhead · chafedRT AFT FS 280 BULKHEAD CHAFED FROM GALLEY DOOR. REPAIRED DAMAGE IAW REO 601R-53-11-1727, REV E.Apr 3, 2012 · N438AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA201240417Striker · damagedPAX DOOR CUT OUT FWD SEAL STRIKER DAMAGED FS 310.00. REPAIRED DAMAGE IAW REO 601R-53-22-033, REV C.Apr 3, 2012 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201240272Warning Light · false activationSPOILERONS CAUTION MESSAGE TEMP DISPLAYED IN FLT ( 5 SEC`S) EXTINGUISHED ON ITS OWN. LATER ON APPROACH GEAR DOWN FLAPS 30 RECEIVED (GLD). INTEROGATED SECU NR 1, NR 2 FOR FAULTS ON FLT LEGS NO FAULTS NOTED PERFORM FIM RESET PROCEDURE, NO FURTHER DEFECTS NOTEDFeb 20, 2012 · N438AW · Cndair CL6002B19 · Central WarningSDR A6WA201240141Throttle · malfunctionedCONFIGUATION SPOILER WARNING MESSAGE AT 20 KTS ON TO ROLL. R & R THROTTLE QUADRANT IAW AMM 76-11-01, OPS AND RIGGING CHECKED GOOD.Jan 27, 2012 · N438AW · Cndair CL6002B19 · Power LeverSDR A6WA201140797Computer · failedAHRS NR 1 FAILED IN FLIGHT. COMPLIED WITH QRH SWITCHED TO AHRS NR 2. R & R NR1 AHRS IAW AMM 34-21-01. OPS CHECK GOOD.Sep 4, 2011 · N438AW · Cndair CL6002B19 · Attitude Gyro and Indicating SystemSDR A6WA201140611Transfer Valve · malfunctionedIN FLT, RECEIVED FUEL IMBALANCE CAS MESSAGE. FUEL WAS IMBALANCED UP TO 1100 LBS. ESTIMATED T/O FUEL WAS 4500 LBS EACH WING AND 2500 LBS IN CENTER TANK. DURING QRH, IMBALANCE WAS 3570 LBS LT WING, 1370 LBS CENTER TANK, AND 4390 RT WING. IMBALANCED INCREASEDJul 20, 2011 · N438AW · Cndair CL6002B19 · Aircraft Fuel Distribution SystemSDR A6WA201140501Unknown · odorAPU AUTOSHUTDOWN AT GATE WITH STRONG FUEL ODOR. INSPECTED APU FOUND NO EVIDENCE OF FUEL LEAKS.Jun 20, 2011 · N438AW · Cndair CL6002B19 · Air Distribution SystemSDR AW6A201140438Strut · binding"WOW INPUT" CAUTION, "STEERING INOP" CAUTION, AND "WOW OUTPUT FAIL "STATUS, NORMALLY EXTENDED GEAR. RECEIVED 3 GREEN GEAR DISAGREE MESSAGE EXTINGUISHED. REARMED NWS. STEERING RE-ENGAGED. "WOW INPUT" AND "WOW OUTPUT FAIL" MESSAGE CLEARED DURING TAXI. FOUNDMay 30, 2011 · N438AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA201140044Relay · malfunctionedWHILE HOLDING AT 16,000 FT RECEIVED CABIN ALTITUDE MESSAGE IMMEDIATELY FOLLOWED BY CABIN ALTITUDE WARNING MESSAGE COMPLIED WITH IAL AND QRH. R & R RELAYS K1GA & K2GA IAW ESPM REF W/C NR 2 FOR OPS CK OF JB11.Jan 21, 2011 · N438AW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR A6WA201040573Cam · wornRT OTBD FLAP, FLAP VANES CAMS WORN MEASURED RT OTBD FLAP VANE CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.Jun 23, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040464Cam · wornLT OTBD FLAP CAMS ARE WORN. MEASURED LT OOTBD FLAP CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.Jun 23, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040569Panel · crackedRT T/R CRACKED AT 6 O`CLOCK POSITION BELOW SAM PANEL. REPAIRED RT T/R IAW REO 601R-78-30-3998.Jun 18, 2010 · N438AW · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA201040459Mount · crackedAFT PAX DOOR COUNTER BALANCE SPRING MOUNT CRACKED. R & R AFT PAX DOOR COUNTER BALANCE SPRING MOUNT WITH NEW IAW SRM 51-42-06, 51-42-43.Jun 18, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040458Skin · chafedLT AILERON L/E SKIN CHAFED FROM OTBD CTR HINGE BUT COTTER KEY. REPAIRED LT AILERON L/E SKIN FROM OTBD CTR HINGE NUT COTTER KEY IAW B/A REO 601R-57-60-078, REV A.Jun 17, 2010 · N438AW · Cndair CL6002B19 · AileronsSDR A6WA201040562Step · crackedPAX DOOR AFT UPPER CORNER ON STAIR STEPS CRACKED. REPAIRED IAW REO 601R-52-11-279.Jun 16, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040572Seal · crackedSEAL ON OTBD SIDE OF LT FLIGHT SPOILER ATTACHED TO WING HAS A 5" CRACK. R & R WITH NEW SERVICEABLE SEAL IAW SRM 51-42-06 AND SRM 51-41-02.Jun 16, 2010 · N438AW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR A6WA201040457Skid · chafedAPU SKID ASSY CHAFED BY DRAIN LINE, REPOSITIONED DRAIN LINE. REPAIRED SKID IAW REO 601R-49-12-008.Jun 16, 2010 · N438AW · Cndair CL6002B19 · APU Cowling/ContainmentSDR A6WA201040434Fitting · chafedLT OTBD FLAP GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.Jun 16, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040436Fitting · chafedRT OTBD FLAP, GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.Jun 16, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040456Frame · corrodedCORROSION ON FRAME FS 333.00 BETWEEN STR 26L AND STR 26R. REMOVED CORROSION (LEVEL 1) BETWEEN STR 27 AND STR 26L IAW SRM 51-21-06 AND REPAIR FRAME AS 333.00 BETWEEN STR 27 AND 26R IAW REO 601R-53-21-149, REV ORIGINAL.Jun 15, 2010 · N438AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA201040433Fairing · chafedLT FUSELAGE UNDER LT INBD FLAP STUB FAIRING AND FWD OF FAIRING CHAFED. REPAIRED CHAFE DAMAGE ON LT FUSELAGE UNDER INBD FLAP STUB FAIRING FWD IAW MFG REV ORIG REO 601R-53-41-1233.Jun 15, 2010 · N438AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201040432Strip · chafedLT ENGINE LOWER NOSE COWL AFT EDGE STRIP IS CHAFED. R & R UNSERVICEABLE LT ENGINE LOWER NOSE COWL AFT EDGE STRIP AND INSTALLED SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-10.Jun 15, 2010 · N438AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040438Intercostal · crackedINTERCOSTAL CRACKED BETWEEN FS 338.0 AND 347.25 WL 147 INTERNAL PAX DOOR STRUCTURE. REPLACED IAW SRM.Jun 15, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040431Stiffener · chafedVERTICAL STIFFENER ON REAR FACE OF 621 BULKHEAD CHAFED APPROX 6" DOWN FROM TOP. REPAIRED VERTICAL STIFFENER ON REAR FACE OF 621 BULKHEAD APPROX 6" DOWN FROM TOP IAW B/A REP NR 601R-53-61-1523, REV ORIGINAL.Jun 14, 2010 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040437Skin · unserviceableRT AILERON BOTTOM L/E INBD SKIN PN CC670-13052-2. R & R NEW SERVICEABLE SKIN.Jun 14, 2010 · N438AW · Cndair CL6002B19 · AileronsSDR A6WA201040435Fairing · chafedRT FUSELAGE UNDER FLAP STUB FAIRING HAS CHAFING DAMAGE AND FWD OF FAIRING. REPAIRED CHAFE DAMAGE ON RT FUSELAGE UNDER FLAP STUB FAIRING FWD, IAW REV ORIG REO 601R-53-41-1233.Jun 14, 2010 · N438AW · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA201040561Floorbeam · corrodedFWD FLOOR ANGLE FS 280.00, WL 73.10 HAS CORROSION. R & R FWD FLOOR ANGLE IAW SRM 51-42-06.Jun 12, 2010 · N438AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA201040429Attach Fitting · corrodedAFT ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER END AT FS 338.00. R & R WITH NEW IAW SRM 51-42-06.Jun 10, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040419Panel · chafedLT INBD FLAP STUB PANEL HAS CHAFING. REMOVED UNSERVICEABLE FLAP STUB FROM LT INBD FLAP AND INSTALLED SERVICEABLE FLAP STUB.Jun 10, 2010 · N438AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA201040418Structure · chafedRT UPPER NOSE COWL AFT EDGE STRIP IS CHAFED. REPAIR CHAFED DAMAGE ON RT UPPER NOSE COWL AFT AND EDGES STRIP IAW CMM 71-14-01.Jun 10, 2010 · N438AW · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR A6WA201040414Plate · damagedCARGO STEP PLATE DAMAGED (2EA) GOUGES (1) FWD AND (1) AFT REMOVED STEP PLATE UNSERVICEABLE AND REPLACED SERVICEABLE CARGO STEP PLATE PN 601R35205-65 IAW SRM 51-42-06.Jun 10, 2010 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040413Hinge · damagedDAMAGED SCREW HOLES IN CARGO STEP PLATE HINGE ASSY. REMOVED UNSERVICEABLE HINGES (3 EA) AND REPLACED W/NEW HINGES (3 EA) PN 601R35205-06, 601R35205-71, AND 601R3520567 IAW SRM 51-42-06.Jun 10, 2010 · N438AW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR A6WA201040423Panel · chafedRT AILERON L/E PANEL 699BB HAS MINOR CHAFE DAMAGE BLENDED IAW SRM 57-60-00 WITH .002" MATERIAL LOSS.Jun 9, 2010 · N438AW · Cndair CL6002B19 · AileronsSDR A6WA201040422Panel · chafedRT AILERON L/E 699CB HAS MINOR CHAFE DAMAGE. REPAIRED IAW 200-57-60-06 WITH 0.0003 MATERIAL LOSS.Jun 9, 2010 · N438AW · Cndair CL6002B19 · AileronsSDR A6WA201040424Panel · chafedRT AILERON PANEL 699AB HAS MINOR CHAFE DAMAGE. REAPIRE IAW REO 601R-57-60-020 WITHIN .013 MATERIAL LOSS.Jun 9, 2010 · N438AW · Cndair CL6002B19 · AileronsSDR A6WA201040417Intercostal · crackedRT INTERCOSTAL LOCATED BETWEEN FS 621 AND FS 625.30 IS CRACKED. REMOVED AND FABRICATED NEW INTERCOSTAL AND INSTALLED IAW REO 601R-53-61-100, REV A AND REO 601R-53-61-422.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040416Intercostal · crackedLT INTERCOSTAL LOCATED BETWEEN FS 621 AND 625.30 IS CRACKED. R & R WITH NEW FABRICATED INTERCOSTAL IAW REO 601R-53-61-100 REV A AND REO 601R-53-61-422.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040427Channel · crackedCARGO DOOR FWD ROLLER GUIDE "C" CHANNEL CRACKED. GOING FROM UNDER RIVET HEAD. REPLACE IAW SRM 51-42-06 AND 51-31-06.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA201040426Rib · crackedRT MLG BATT RIB IS CRACKED, REO 601R-57-51-046.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA201040430Attach Fitting · corrodedFWD ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER EOP AT FS 320.10. R & R WITH NEW SRM 51-42-06.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA201040428Attach Fitting · corrodedAFT ATTACH CLIP IS CORRODED ON PAX DOOR INNER FRAME UPPER EOP AT FS 320. R & R SRM 51-42-06.Jun 7, 2010 · N438AW · Cndair CL6002B19 · Passenger/Crew Doors
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