N824AL, cancelled Oct 29, 2013
Service difficulty reports · 78
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 = 'N824AL' AND deregistration_id = 'N824AL-2013-10-29' 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.
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 = 'N824AL' AND deregistration_id = 'N824AL-2013-10-29' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR TSAA0821016Fan · failedFLIGHT 93 OGG - HNL - THE CREW NOTED AN UNPLEASANT BURNING ODOR IN THE CABIN DURING FLIGHT WITH NO SMOKE PRESENT. THE ODOR DECREASED WITH ENGINES AT LOWER THROTTLE SETTINGS. THE AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACSDR TSAA0853003Bulkhead · crackedWHILE PERFORMING ECO 1822 PART I (REFERENCE AD 93-08-08 AND AD 90-06-02) A CRACK WAS DISCOVERED ON THE LT BULKHEAD BS 1156 ALONG THE LAST ROW OF RIVETS APPROX WL 272-275. REPAIRED CRACK IN ACCORDANCE WITH ECO 1822 PART II (S/B 737-53-1-86 R3).SDR TSAA0721046Sensor · failedNON-ETOPS FLIGHT 63 HNL-LIH, DURING CLIMB, THE CREW NOTED LOUD NOISE AND ICE EMANATING FROM THE AIR CONDITIONING SYSTEM. THE CREW ATTEMPTED TO CONTROL THE NOISE AND ICE BY SELECTING A WARMER TEMPERATURE WITH NO CHANGE IN CONDITION. THE NOISE WAS DISRUPTIVE TSDR TSAA0675112Control Valve · failedFLT 206 HNL-OGG: DURING TAKEOFF ROLL, NR 1 ENGINE EPR WOULD NOT INCREASE ABOVE 1.53 WITH MORE THAN A TWO THROTTLE KNOB WIDTH SPLIT AND EGT RISING TO 580 DEGREES. NR 2 ENGINE STABILIZED AT 1.89 EPR AND EGT AROUND 530 DEGREES. TAKEOFF WAS ABORTED AROUND 80 KNOSDR TSAA0632094Uplock · dirtyAFTER TAKEOFF, THE RT MLG DID NOT RETRACT. CREW CYCLED THE LANDING GEAR LEVER AND WAS ABLE TO RETRACT THE GEAR. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE RT MLG UPLOCK SENSOR AND PERFORMED THE MAIN LANDING GEAR EXTENSION AND RETRSDR TSAA0672088Nose Bullet · looseNON-ETOPS FLT 281: CLIMBING THRU 16,000 FEET WITH THE ENGINE ANTI-ICE ON, THE CREW HEARD A LOUD BANGING SOUND COMING FROM THE LT SIDE OF THE AIRCRAFT. ENGINE INDICATIONS WERE NORMAL. THE CREW RETARDED THE NR 1 ENGINE THRUST LEVER AND THE BANGING STOPPED. TSDR TSAA0629060Hose · failedNON-ETOPS FLT 77 ITO-HNL: DURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED SYSTEM ‘A’ HYDRAULIC FAILURE. THE CREW BROUGHT THE AIRCRAFT TO A STOP, NOTIFIED TOWER, AND PERFORMED THEIR QRH CHECK LIST. THE AIRCRAFT WAS TOWED BY MAINTENANCE TO THE GATE. R & R NOSDR TSAA0652044Slide · out of positionNON-ETOPS: FLT 206 HNL - OGG: ON THE GROUND, FWD SVC DOOR EMERGENCY SLIDE ACCIDENTALLY DISLODGED FROM THE DOOR BUT DID NOT INFLATE. REMOVED AND REPLACED FORWARD SERVICE DOOR SLIDE CHUTE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0653002Skin Panel · crackedFUSELAGE SKIN CRACK LOWER BL-0, BETWEEN S-28L AND R AT BS 370. TWO 1/2 INCH FUSELAGE SKIN CRACKS LOWER BL-0, BETWEEN S-28L AND R AT BS370 AND BS380. MAINTENANCE REPAIRED WITH APPROXIMATELY 40" X 20" SKIN PATCH, FABRICATED DOUBLER )1002024-T3). REPAIR COMPLESDR TSAA0532055Tire · failedDURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE FOUND HOLE IN LT NOSEWHEEL AND BOTH TIRES FLAT. REMOVED AND REPLACED BOTH NOSEWHEEL TIRES, INSPESDR TSAA0532050Anti-Skid Sys · deactivatedON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED.SDR TSAA0552009Warning Light · false indicationFLT 211, OGG-HNL, FORWARD CARGO DOOR LIGHT CAME ON DURING TAKEOFF ROLL. ABORTED TAKEOFF PRIOR TO 80 KTS. RETURNED TO GATE. MAINTENANCE OPENED AND CLOSED THE FORWARD CARGO DOOR AND CHECKED LOCKS FOR SECURITY. OPS CHECK OK AND LIGHTS CHECK GOOD. IN HNL, FWDSDR TSAA0527002Sensor · defectiveFLT 278, HNL-KOA: ON INITIAL TAKEOFF ROLL, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED (NR 4 SLAT) WITH THE CONFIGURATION WARNING HORN. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP EXTEND SENSOR. OPS CHECK OK PERSDR TSAA0434084Indicator · inoperativeFLT 220, HNL-OGG: FIRST OFFICE AIRSPEED INDICATOR INOP. RETURNED TO HNL, UNEVENTFUL LANDING. REMOVED AND REPLACED THE MACH AIR SPEED INDICATOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0436069Bleed Air Sys · malfunctionedFLIGHT 280, HNL-KOA: PASSING THROUGH 8000 FT ON CLIMB-OUT, THE RT DUCT PRESSURE WAS OBSERVED AT ABOUT 40PSIG WITH THE ISOLATION VALVE CLOSED AND THE RT BLEED & RT PACK OFF. THE PRESSURE THEN DECREASED TO 14 PSIG, AND THEN DECREASED FURTHER WHEN POWER WAS REDUCSDR TSAA0353219Skin · corrodedFOUND LT UPPER WING SURFACE CORRODED BETWEEN FRONT & REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 6 AS NR 1 - 19 AT LOCATIONS, NR 1, 2, & 3 AT WBL 227, NR 4 AT WLB 228, NR 5 AT WBL 254, NR 6 AT WBL 264, NR 7 AT WBL 268, NR 8 AT WBL 234, NR 9 AT WBL 236, NR 10 AT SDR TSAA0353218Skin · corrodedFOUND RIGHT UPPER WING SURFACE CORROSION BETWEEN THE FRONT AND REAR SPAR IDENTIFIED ON FIGURES 1 THROUGH 5 AS NR 1 TO NR 15 AT THE FOLLOWING LOCATIONS, NR 1 AT WBL 92.5, NR 2, 3, 4, 5 AND 6 BETWEEN WBL 198.6 AND WBL 227.0, NR 7 AND 8 AT WBL 157, NR 9 AND 10 BESDR TSAA0253267Skin · crackedCLEANED OUTER SKIN AT EACH MOUNTING HOLE. OVER-DRILLED ELONGATED HOLES TO RESTORE HOLES TO CIRCULAR SHAPE. TRIMMED OUT CRACK DAMAGED HOLE LARGE ENOUGH TO REMOVE CRACK TO RECTANGULAR SHAPE. HFEC VERIFIED HOLES CRACK FREE. FABRICATED CIRCULAR AND RECTANGULARSDR TSAA0253249Floorbeam · crackedREMOVED EXISTING FASTENERS, STIFFENERS, ANGLE AND A SECTION OF THE WEB. REMOVED AND DISCARDED REINFORCING ANGLE, DOUBLER AND A SECTION OF THE WEB. DRILL AND COLD WORKED THE HOLES IN THE CHORD. INSTALLED SPLICE ANGLE AND STIFFENERS WITH FASTENERS SHOWN IN SESDR TSAA0253268Lap Joint · damagedTRIMMED BONDED DOUBLER ABOVE EXISTING FASTENER PATTERN LEAVING ED FOR FINAL FASTENER INSTALL. OPENED DISCREPANT COUNTERSINK HOLE TO .75 INCH DIAMETER. VERIFIED CRACK FREE USING HFEC. HOLE OPENED UP TO 1 INCH INSURANCE CUT. FABBED .032/.036 INCH THICK CIRCULSDR TSAA0255264Skin · gougedCUT AND REMOVED GOUGE AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0255266Skin · gougedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0255265Skin · dentedCUT OUT DAMAGED AREA. FABRICATED REPAIR .063 DOUBLER AND .040 FILLER FROM 2024 T3 CLAD. INSTALLED REPAIR PARTS AND FASTENERS WET WITH MBS 5-95 SEALANT. REPAIR COMPLETED IAW SRM 55-10-1 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0253236Pressure Panel · damagedPERFORMED MODIFICATION TO THE WEB AND DOUBLER OF THE MAIN WHEEL WELL PRESSURE FLOOR TRANSVERSE BEAM BETWEEN BS 650 AND BS 727 AND BETWEEN RT AND LT BBL 45. FABRICATED WEB FILLER AND REPAIR DOUBLER IAW FIGURE 7. REPLACED ANGLE, CHANNEL AND DOUBLER WITH PARTS SDR TSAA0253235Beam · damagedOVERSIZED 4 HOLES IN THE RIGHT MLG LOWER BEAM CHORD FLANGE. FABRICATED FOUR FREEZE PLUGS. FABRICATED FOUR 1 INCH DIAMETER RETAINING WASHERS. INSTALLED FREEZE PLUGS AND OPENED ID HOLES TO THE EXISTING .1875 INCH DIAMETER PANEL ATTACH BOLTS. INSTALLED RETAINSDR TSAA0253232Structure · crackedTRIMMED OUT THE DAMAGE OF THE HOLES TO A RECTANGULAR SHAPE. VERIFIED CRACK REMOVED USING HFEC. FABRICATED CIRCULAR DOUBLERS FOR EACH HOLE. REPAIR COMPLETED IAW ECO 3302. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0253231Fitting · damagedREMOVED DAMAGE FROM THE NR 2 AND NR 7 FLAP TRACK ATTACHMENT FITTING HOLE. FABRICATED A 'NEW' REPLACEMENT TUBE AND BUSHING INCREASING THE OUTSIDE DIAMETER .0015 TO .0020 INCH INTERFERENCE FIT ON THE FINISHED DIAMETER OF THE HOLE. INSTALLED NEW TUBE AND BUSHINSDR TSAA0253234Structure · corrodedBLENDED THE DAMAGE ON THE LUG. SPOTFACED THE INBOARD AND OUTBOARD SURFACES. OVERSIZED THE TAPERED/ELONGATED HOLE OF THE INBOARD LUG ON THE ORIGINAL CENTERLINE TO OBTAIN A ROUND AND TRUE CONDITION. FABRICATED NEW REPAIR SLEEVE BUSHING TO FIT THE OVERSIZED INSDR TSAA0253233Structure · crackedTRIM OUT ALL THREE HOLES IN THE DAMAGED ZONE. HFEC THE EDGE OF THE TRIM. FABRICATED A DOUBLER AND A TRIPLER. INSTALLED DOUBLER AND TRIPLER. REPAIR COMPLETED IAW ECO 3250, FIGURE 24. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0233136Battery Pack · dischargedREPLACED NR 6, EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0233054Battery Pack · dischargedREPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133184Battery Pack · dischargedREPLACED NR 1 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0126181Fire Loop · defectiveFLT 205 - HNL-LIH - EN ROUTE TO LIH, THE APU FIRE WARNING ILLUMINATED THOUGH THE APU WAS PREVIOUSLY MEL'D. THE APU FIRE BOTTLE WAS DISCHARGED AND THE AIRCRAFT RETURNED TO HNL WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS OPERATING UNDER MEL 49-1 FOR A PREVIOUS SDR TSAA0133164Battery Pack · dischargedREPLACED LEFT OVERWING IDENT BATTERY PACKED DUE TO LOW VOLTAGE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0153151Bulkhead · crackedFOUND RIVET HOLES CRACKED AT BS 178 LEFT AND RIGHT LBL 9 WL 234. REMOVED CRACK PER SRM 53-10-11 PAGE 1, PROCEDURE 1. VERIFIED CRACK REMOVED USING HFEC. INSTALLED REPAIR DOUBLER IAW ECO 3138 PART 1. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133096Battery Pack · corrodedFOUND LEFT OVERWING EMERGENCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133095Battery Pack · corrodedAFT ENTRY DOOR EMEREGNCY IDENT LIGHT INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133082Battery Pack · inoperativeREPLACED NR 1 AND NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OP CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0153021Frame · crackedIDENTIFIED A CRACK AT 2 PLACES ON THE RIGHT SIDE OF BS 1156 CHORD BETWEEN WL 281-269. STOP DRILLED ENDS OF CRACKS, REMOVED FASTENERS ON AFFECTED CHORD ASSEMBLY AND INSTALLED REPAIR STIFFENER ANGLE IAW ECO 1822. APPLIED ALODINE AND PRIMER BMS 10-11 TYPE 1 PRISDR TSAA0153019Frame · crackedIDENTIFIED CRACK AT RIGHT UPPER CHORD BS 727, STRINGER 18A AFT HOLE BY UTILIZING HFEC AND ULTRASONIC METHOD. REMOVED AND REPLACED RIGHT UPPER CHORD ASSEMBLY CLEANED AND TREATED ALL EXPOSED AREAS AND APPLIED CORROSION INHIBITING COMPOUND IAW ECO 1785. AIRCRAFSDR TSAA0153020Frame · dentedIDENTIFIED DENT ON FRAME ASSEMBLY 5 INCHES BY 7 INCHES AT BS 360-380 STRINGER 17L. (M)SDR TSAA0033206Battery Pack · inoperativeREPLACED NR 1, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA200033056Battery Pack · inoperativeREPLACED POSITION 1 FLOOR PROXIMITY LIGHT ASSY BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA200032031Valve · inoperativeHNL/ITO - FLT 108 - ON TAKOFF ROLL, PARKING BRAKE LIGHT AND ANTI-SKID INOPERABLE. INBOARD/OUTBAORD LIGHT REMAINED ILLUMINATED. PARKING BRAKE LEVER WAS IN RELEASED POSITION WITH NO BRAKE DRAG FELT. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED SDR TSAA9933518Battery Pack · dischargedREPLACED BATTERY PACK FOR NR 2 EMERGENCY FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9933447Battery Pack · dischargedREPLACED BATTERY PACK FOR CENTER AISLE EMERGENCY LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNE TO SERVICE. (M)SDR TSAA9957416Beam · corrodedLEFT MLG BEAM CORRODED BEYOND LIMITS. REPLACED LEFT MLG BEAM (PERFORMED BY BOEING AOG TEAM). AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9952415Frame · crackedFORWARD ENTRY DOOR FRAME CORRODED AT LWR AFT CORNER ABOVE DOOR SILL. REPAIRED IAW ECO 2992. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9933411Battery · dischargedREPLACED BATTERY PACKS FOR NR 2, NR 4 AND NR 5 EMERGENCY FLOOR LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9933390Battery Pack · dischargedREPLACED BATTERY PACK IN AFT CONTROL MODULE DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)
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