N810AL, cancelled Jan 26, 2009

Service difficulty reports · 76

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 = 'N810AL' AND deregistration_id = 'N810AL-2009-01-26'
  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 TSAA0732043Module · failedNON-ETOPS FLIGHT 221 OGG - HNL. WHEN THE CREW SELECTED THE LANDING GEAR TO UP, THE LT MAIN GEAR DOWN LIGHT TOOK A FEW SECONDS LONGER TO EXTINGUISH THAN THE OTHER GEAR INDICATIONS. AFTER THE GEAR LEVER WAS SELECTED TO OFF, THE LT MAIN GEAR EXTENDED UNCOMMANDEJul 31, 2007 · N810AL · Boeing 7372Y5 · Landing Gear Retraction/Extension SystemSDR TSAA0729040Hose · failedFLIGHT 26 HNL-OGG - AFTER TAKEOFF FROM HNL, CREW NOTED LOSS OF SYSTEM A HYDRAULIC PRESSURE. CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE TOWED THE AIRCRAFT TO THE GATE AND REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR HYDRAULIC SURGE RELIEF LJul 7, 2007 · N810AL · Boeing 7372Y5 · Hydraulic System, MainSDR TSAA0726029Fire Detector · failedFLIGHT 93 HNL-LIH - AFTER STARTING THE NR 1 ENGINE, THE CREW NOTED THE NR 1 ENGINE FIRE INDICATION LIGHT ILLUMINATED. CREW FOLLOWED THE QRH PROCEDURES: SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AIRCRAFT WAS TOWED BACK TO THEMay 31, 2007 · N810AL · Boeing 7372Y5 · Fire DetectionSDR TSAA0632057Wheel · separatedON LANDING, CREW HEARD AN UNUSUAL (BUMP) NOISE WITH NORMAL LANDING. TAXI TO GATE WITHOUT FURTHER INCIDENT. CREW FOUND NR 1 MAIN LANDING GEAR WHEEL ASSEMBLY HAD SEPARATED FROM THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE NR 1 MLG BRAKE ASSEMBLY AND THEJul 24, 2006 · N810AL · Boeing 7372Y5 · Wheel/Ski/FloatSDR TSAA0651040Spar · corrodedHORIZONTAL STABILIZER RT REAR SPAR UPPER CHORD CORROSION (3 AREAS).May 24, 2006 · N810AL · Boeing 7372Y5 · Horizontal Stabilizer, Spar/RibSDR TSAA0651039Spar · corrodedVERTICAL STABILIZER RIGHT T/E REAR SPAR CORROSION (3 AREAS).May 24, 2006 · N810AL · Boeing 7372Y5 · Vertical Stabilizer, Spar/RibSDR TSAA0653018Skin Panel · crackedA 2 INCH SKIN CRACK AT BS 929 STR 24L. A .04 INSURANCE MADE IAW SRM 53-30-3. RIVET PATTERN LAID OUT AND DRILLED AND MANUFACTURED REPAIR DOUBLER, TRIPLER, AND 2 FILLERS PER SRM 53-30-3 FIG 48 DET XIX. HFEC RIVET HOLES IAW BOEING NDT MANUAL 51-00-00 PT 6. REMar 17, 2006 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0653017Spar · corrodedCORROSION ON UPPER & LOWER SURFACE OF FRONT SPAR LOWER CORD BETWEEN FSS 297 & FSS-306 AT SLAT NR 4. BLENDED INBOARD - OUTBOARD DIRECTION 10:1 DEPTH TO BLEND RATION. SHOT/FLAP PEEN BLENDED ARE PER SRM. FABRICATED SOLID FILLERS TO REPLACE REMOVED MATERIAL. FMar 11, 2006 · N810AL · Boeing 7372Y5 · Leading Edge DevicesSDR TSAA0621007Fan · defectiveON APPROACH THE PILOT SMELLED SMOKE AND AFTER LANDING THE SMELL GREW STRONGER. AIRPLANE TAXIED BACK TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD, NO HELP. THE CABIN AUGMENTATION FAN WAS FOUND TO BE INOP. REMOVED AND REPLACJan 27, 2006 · N810AL · Boeing 7372Y5 · Air Distribution FanSDR TSAA0653006Skin · crackedA 4 INCH FUSELAGE SKIN CRACK BS 937 AT STRINGER 21L. MAINTENANCE REPAIRED WITH APPROXIMATELY 24 X 20 INCH SKIN PATCH, FABRICATED DOUBLER, TRIPLER, AND STRUCTURAL FILLER NR 5 AND 6 PER SRM 53-30-3, FIG 48, DET XII.Jan 24, 2006 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0575031Bleed Valve · defectiveON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. LJul 20, 2005 · N810AL · Boeing 7372Y5 · Compressor Bleed ValveSDR TSAA0575029Bleed Valve · defectiveRUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH ANJul 12, 2005 · N810AL · Boeing 7372Y5 · Compressor Bleed ValveSDR TSAA0479019Engine · leakingFLT 224 - LIH-HNL - LOW OIL PRESSURE ILGHT ON NR 1 ENGINE ILLUMINATED. OIL PRESSURE DROPPED TO 20 PSI. FOLLOWED QRH AND SHUTDOWN THE NR 1 ENGINE. DECLARED EMERGENCY AND HAD UNEVENTFUL LANDING. REMOVED AND REPLACED THE NR 1 ENGINE PER FORMS M-211 THROUGH M-Jan 16, 2004 · N810AL · Boeing 7372Y5 · Turbine Engine Oil SystemSDR TSAA0429001Line · failedFLT 240 - HNL-OGG - ON GEAR RETRACTION 'A' SYSTEM HYDRAULIC ANNUNCIATOR LIGHT CAME ON. SYSTEM QUANTITY AT 1.5 GALLONS. RETURNED TO HNL. FOUND RIGHT MAIN GEAR UPLOCK ACTUATOR FLEX-LINE RUPTURED. REMOVED AND REPLACED FLEX-LINE. LEAK CHECK OK. SERVICED HYDRADec 30, 2003 · N810AL · Boeing 7372Y5 · Hydraulic System, MainSDR TSAA0333205Battery Pack · inoperativeREPLACED AFT ENTRY DOOR IDENT EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 29, 2003 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0353037Skin · crackedNINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES CRACK FREE. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAFeb 9, 2003 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0233228Battery Pack · dischargedREPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0233229Light · inoperativeREPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0253201Structure · gougedCUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE.Oct 2, 2002 · N810AL · Boeing 7372Y5 · Cargo/Baggage DoorsSDR TSAA0253183Frame · corrodedAUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE.Jun 29, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, FrameSDR TSAA0253152Skin · crackedFOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.Jun 17, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0253142Skin · corrodedFOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PER SRM. ULTRASOUND INSPECTED TO ENSURE NO REMAINING CORROSION. HFEC AFFECTED FASTENER HOLE BORE FOMay 15, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253141Skin · wornFOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED THE REPAIR PARTS WITH FASTENERS. APPLIED BMS 5-95 SEALANT TO THE MATINGMay 13, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253134Pressure Panel · corrodedFOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.May 13, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0251133Skin · gougedFOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0251132Bracket · chafedFOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Trailing Edge FlapsSDR TSAA0251130Slat · corrodedFOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Leading Edge DevicesSDR TSAA0253146Skin · wornRIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER, SPLICE PLATE AND DOUBLER. AIRCRAFT RETURNED TO SERVICE.Apr 25, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253125Spar · corrodedFOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETEDApr 25, 2002 · N810AL · Boeing 7372Y5 · Wing SparSDR TSAA0253127Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART.Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0253126Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNED TO SERVICE.Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0253128Stringer · dentedFOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERApr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Longeron/StringerSDR TSAA0253131Floorbeam · crackedFOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLETED INSTALLATION OF RApr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR TSAA0253006Frame · corrodedREMOVED CORROSION DAMAGE ON STRINGER 5R UPPER CHORD AT BS 1093. REMOVED FORWARD PORTION OF DAMAGED CHORD. FABRICATED REPLACEMENT CHORD AND SPLICE ANGLES AND INSTALLED REPAIR PARTS PER FIGURE 1 IAW ECO 3259. AIRCRAFT RETURNED TO SERVICE. (M)Jan 1, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, FrameSDR TSAA0133092Battery Pack · dischargedREPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 20, 2001 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0132070Downlock Sensor · failedINBOUND TO HNL FROM LIH - REPORTED TO MAINTENANCE CONTROL OF THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ON IN-FLIGHT. CAPTAIN PERFORMED FLYBY FOR TOWER TO CHECK GEARS DOWN WHILE F/O ALSO CHECKED BY GOING TO BACK OF AIRCRAFT. GEARS RECYCLED ONCE AND LIGHT STILLJun 13, 2001 · N810AL · Boeing 7372Y5 · Landing Gear Position and WarningSDR TSAA0033216Battery · inoperativeREPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)Oct 16, 2000 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0053198Skin · dentedREPAIRED A DENT AT LEFT FUSELAGE BS 360-380 STRINGER 17L, AFT OF FORWARD ENTRY DOOR. CUT OUT DAMAGED AREA PERFORMED HFEC INSPECTION. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)Jul 30, 2000 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0033182Battery · inoperativeREPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 30, 2000 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0073139Fcu · failedFLT 71 - OGG-HNL - THE NR 1 ENGINE RPM GAGE IMMEDIATELY DECREASED TO ZERO THE MOMENT THE AIRCRAFT LIFTED OFF THE RUNWAY. DID NOT ATTEMPT A RESTART, ACCOMPLISHED NORMAL SINGLE ENGINE LANDING WITH NO FURTHER PROBLEMS NOTED. REMOVED AND REPLACED NR 1 ENGINE FUEMay 29, 2000 · N810AL · Boeing 7372Y5 · Fuel Controlling SystemSDR TSAA9933479Battery · dischargedREPLACED NR 3, 4, 5, AND 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 9, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR 99ZZZM807Sensor · intermittentFLT 101 - OGG-HNL - LEFT MAIN GEAR RED UNSAFE GEAR LIGHT COMES ON INTERMITTENTLY DURING FLIGHT. REMOVED AND REPLACED UPLOCK SENSOR LEFT GEAR PER MM 32-61-21 AND ALSO CHECKED UPLOCK MECHANISM PER MM 32-32-31. ALL OK, OPS OK ON GEAR SWING. AIRCRAFT RETURNED TOct 26, 1999 · N810AL · Boeing 7372Y5 · Landing Gear Position and WarningSDR TSAA9933408Battery Pack · dischargedREPLACED NR 3 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Aug 21, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA9933368Battery Pack · dischargedREPLACED NR 5 EMERGENCY FLOOR BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 31, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA9933362Battery Pack · dischargedREPLACED NR 4 EMERGENCY FLOOR BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA9921300Relief Valve · failedHNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED, BUT DIDN'T CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTRJul 6, 1999 · N810AL · Boeing 7372Y5 · Cabin Pressure Control SystemSDR TSAA9921292Controller · failedHNL/ITO - FLT 248 - PRESSURIZATION FAILURE AT FL 230. LOST AUTO, STANDBY, AND A/C MANUAL SHOWED VALVE CLOSED BUT DID NOT CONTROL CABIN. LATER, MANUAL AND STANDBY WORKED. DIVERTED TO OGG AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CABIN PRESSURE CONTRJul 6, 1999 · N810AL · Boeing 7372Y5 · Cabin Pressure ControllerSDR TSAA9933285Battery · dischargedREPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jun 8, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA9933246Battery · dischargedREPLACED NR 6 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK FOR LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M)May 31, 1999 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA9933223Battery · dischargedREPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT POWER SUPPLY DUE TO BEING INOPERATIVE. AIRCRAFT RETURNED TO SERVICE. (M)Apr 19, 1999 · N810AL · Boeing 7372Y5 · Emergency Lighting
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