N807AL, cancelled Jul 30, 2008
Service difficulty reports · 104
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 = 'N807AL' AND deregistration_id = 'N807AL-2008-07-30' 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 = 'N807AL' AND deregistration_id = 'N807AL-2008-07-30' 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 TSAA0631102Lever · lack of lubeON TAKEOFF, THE CREW NOTED THE TAKEOFF CONFIGURATION WARNING ALARM AND PERFORMED A LOW SPEED ABORTED TAKEOFF. CREW RECYCLED THE SPEED BRAKE AND THE ALARM CLEARED. CREW PROCEEDED ON TO LIH WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A TAKEOFF WARNING TESSDR TSAA0663089Skin Panel · crackedA .5 INCH CRACK FOUND LT SIDE OF FUSELAGE SKIN AT BS 270 STRINGER 16L. MAINTENANCE REPAIRED WITH APPROXIMATELY 9"X14" EXTERNAL SKIN PTACH FABRICATED DOUBLER AND TRIPPLER PER ECO 3617. FORM 8100 RECEIVED.SDR TSAA0653076Bulkhead · cracked3 CRACKED HOLES COMMON TO BS 178 BULKHEAD WEB BETWEEN WL 240 AND WL 230.5SDR TSAA0653068Door Frame · crackedCRACK NOTED ON FWD CARGO DOOR CUTOUT, AFT LOWER CORNER UNDER DOOR STOP.SDR TSAA0653030Bulkhead · crackedTHREE CRACKS AROUND BS 1016 AFT PRESSURE BULKHEAD GORE WEBS NEAR DOME CAP. WEB SPLICE AND REPAIR DOUBLERS COMPLETED IAW ALOHA'S ECO 3567. HFEC COMPLIED IAW NDT MANUAL PART 5, 51-00-00 FIG 16. FAA FORM 8100-9 RECEIVED.SDR TSAA0653028Skin · crackedAPPROXIMATE 2 INCH SKIN CRACK AT BS 747 +10 STR 24L. REPAIR COMPLETED IAW SRM 53-30-3 FIG 48. REPAIR SIZE APPROX 15 X 11 INCHES. INSURANCE CUT MADE .040 INCH. DOUBLER .032 2024T3; TRIPLER .050 2024T3. HFEC HOLE LAY-OUT IAW NDT MANUAL 51-00-00 PT 6.SDR TSAA0627026Indication Sys · malfunctionedON APPROACH TO KOA, CREW NOTED TRAILING EDGE FLAP INDICATOR SHOWING LEFT SIDE AT 4 DEGREES AND RIGHT SIDE AT 7 DEGREES WITH 5 DEGREES OF FLAPS SELECTED. CREW UNABLE TO EXTEND FLAPS TO 15. CREW DECIDED TO RETURN TO HNL AND DECLARED AN EMERGENCY. WITH ALTERNASDR TSAA0652004Skin · crackedA 4.25 INCH SKIN CRACK ON AFT CARGO DOOR. CRACK LOCATED 18.5 INCHES FROM LOWER FWD CORNER AND 5 INCHES FROM FWD CUTOUT. MAINTENANCE REPAIRED WITH APPROXIMATELY 10 X 7 INCH EXTERNAL SKIN PATCH, FABRICATED DOUBLER (0502024-T3). REPAIR COMPLETED IAW ECO 3550.SDR TSAA0529052Filter · contaminatedNON-ETOPS FLIGHT 278 HNL - KOA, AFTER TAKEOFF, NR 1 ENGINE HYDRAULIC SYSTEM A LOW PRESSURE LIGHT ILLUMINATED. CREW DISENGAGED ENGINE DRIVEN HYDRAULIC PUMP AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CHANGED HYDRAULIC SYSTEM A CASESDR TSAA0529051Hose · leakingNON-ETOPS FLIGHT 88 LIH-HNL - AFTER GEAR UP, HYD PRESSURE INDICATOR SHOWED ZERO. LEFT MAIN LANDING GEAR INDICATOR LIGHTS SHOWED BOTH RED AND GREEN (UNSAFE). WHEN EXTENDING FLAPS AND GEAR, HYD SYSTEM A PRESSURE FLUCTUATED AND A SYSTEM LOW PRESSURE CAUTION LIGSDR TSAA0532032Circuit Breaker · failedFLT 71 OGG-HNL, AFTER DEPARTURE, CREW WAS UNABLE TO MOVE LANDING GEAR LEVER TO THE UP POSITION. CREW FOUND CIRCUIT BREAKER POPPED OUT AND THEN RESET IT. GEAR HANDLE WAS THEN MOVED TO THE UP POSITION. THE FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. MASDR TSAA0532028Landing Gear · malfunctionedGEAR WOULD NOT RETRACT ON T/O FROM KONA. ISOLATION VALVE LIGHT CAME ON AND GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION. WITH GEAR HANDLE DOWN, WE HAD NO GEAR LIGHTS. VISUALLY CHECKED GEAR DOWN AND LANDED AT KONA. INSPECTED LANDING GEAR SYSTEM ANDSDR TSAA0526026Element · failedDURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CHECK LISTS AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AFTER DISCHARGING THE BOTTLES, THESDR TSAA0526025Connector · dirtyON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPLETED AND LIGHT WAS EXTINGUISHED. ENGINE WAS NOT SHUTDOWN, EMERGENCY DECLARED, AND THE AIRCRAFT RETSDR TSAA0425082Slide · deployedDURING GROUND MAINTENANCE, GROUND CREW INADVERTENTLY DEPLOYED THE FORWARD SERVICE DOOR ESCAPE SLIDE. NO INJURIES. REMOVED AND REPLACED THE FORWARD SERVICE DOOR SLIDE IN ACCORDANCE WITH MM 25-61-200.SDR TSAA0477063Transmitter · inoperativeON TAKE-OFF ROLL THE NR 1 ENGINE ONLY INDICATED 1.76 EPR; THE THROTTLES WERE ADVANCED WITH NO RESPONSE FROM ANY INSTRUMENTS. REJECTED TAKE-OFF AND RETURNED TO GATE. REPLACED THE NR 1 ENGINE EPR TRANSMITTER AND CLEARED THE PT2 INLET PROBE OF DEBRIS. RAN NR 1 SDR TSAA0479046Bearing · failedNON-ETOPS FLIGHT 206, HNL-OGG: ON DESCENT ONTO OGG THE NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, THE OIL PRESSURE DECREASED TOWARD ZERO AND THE OIL QUANTITY BEGAN DROPPING WITH THE OIL TEMPERATURE IN THE NORMAL RANGE. FOLLOWED QRH AND SHUT DOWN THE NR 2 ENGINE.SDR TSAA0453002Skin · crackedFOUND AN INCH AND A HALF AND A TWO INCH FUSELAGE CRACK AT BS 767 AND BS 792, ON STRINGER 18L. TRIMMED OUT CRACKS AND VERIFIED CUTOUTS USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED STRUCTURAL AND TAPERED FILLERS, DOUBLER, AND TRIPLER FROM CLADSDR TSAA0375198Duct · failedFLT 240 - HNL-OGG - ENGINE NR 1 OVERHEAT LIGHT CAME ON JUST AFTER TAKEOFF. PULLED THROTTLE BACK AND THE LIGHT WENT OUT. EGT IN GREEN THE ENTIRE TIME. REMOVED AND REPLACED NR 1 COWL ANTI-ICE UPPER DUCTING. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0329180Hose · failedAFTER GEAR RETRACTION LOST ENTIRE 'A'SYSTEM HYD QTY. MAINTENANCE REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PRESSURE RETURN HOSE ASSEMBLY. (M)SDR TSAA0333126Battery Pack · inoperativeREPLACED NR 4 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0357059Skin · dentedGAINED ACCESS TO DENTED AREA. CUTOUT DAMAGE BY SLICING THE LEADING EDGE SKIN PER FIGURE 1. INSTALLED A SPLICE REPAIR AT SS205.46 AND SS 238.71. REPAIR COMPLETED IAW SRM 57-50-3, FIGURE 7 AND ECO 3354. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0352053Guide · misalignedAFTER TAKEOFF, THE CABIN HAD AN EXCESSIVE RATE OF CLIMB, (2,500 FPM). AUTO FAILED ON THE PRESSURIZATION SYSTEM. LANDED HNL WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD SERVICE DOOR WAS IMPROPERLY CLOSED AND LOWER LEFT GUIDE MISALIGNED. MAINTENANSDR TSAA0251181Strap · corrodedKEEL BEAM VERTICAL STRAP CORRODED AT BS 532. BLENDED AND FLAP PEENED REPAIR AREA, FABRICATED TWO FILLER STRAPS, INSTALLED FILLERS AND STRAP.SDR TSAA0251178Stringer · corrodedFOUND CORROSION ON BS 500 AT STRINGER 26R. CUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. FABRICATED REPAIR ANGLES AND DOUBLER IAW SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0251180Stringer · crackedCRACK LOCATED AT BS 767, S-14L. TRIMMED OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND REPAIR ANGLES.SDR TSAA0251177Skin · crackedSKIN CRACK AT BS 380 BETWEEN STRINGER 28L AND 28R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, AIRCRAFT RETURNED TO SERVICE.SDR TSAA0251179Stringer · crackedCRACKS BS 739, S-18R AND BS 745, S-19R. REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL USING HFEC METHOD, FABRICATED AND INSTALLED REPAIR DOUBLER.SDR TSAA0253038Skin · crackedREPAIRED 2.5 INCH LONG SKIN CRACK AT FUSELAGE BS 937 STRINGER 26R. CONFIRMED 2.5 INCH REMOVED USING HFEC METHOD. THE REPAIR CONSISTED OF CUTTING OUT THE SKIN CRACK AND FABRICATING A DOUBLER IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133182Battery Pack · dischargedREPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0153149Skin · crackedFOUND FUSELAGE CRACKED AT BS 767, S19L. TRIM OUT CRACK COMPLETED AND VERIFIED CUT OUT USING HFEC METHOD, NO DEFECTS NOTED. FABRICATED AND INSTALLED REPAIR DOUBLER. CLEANED AND TREATED ALL EXPOSED SURFACES IAW SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVSDR TSAA0133145Battery Pack · dischargedREPLACED NR 3 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133023Light · inoperativeREPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0157009Spar · corrodedIDENTIFIED CORROSION AT RT WING FRONT SPAR LOWER CHORD FSS 475. REPAIRED CONSISTS OF REMOVING DAMAGED AREA AT HORIZONTAL FLANGE AND INSTALLING A TAPERED FILLER, HFEC COMPLETED ON ALL FASTENER HOLES AND REWORKED AREA. NO DEFECTS NOTED. CLEAN AND TREATED ALL SDR TSAA0053255Keel · corrodedIDENTIFIED CORROSION AT THE VERTICAL LEG OF THE KEEL BEAM AT BS 535 APPROXIMATELY LBL 6.30. REPAIRED BY REMOVING CORROSION, BLEND OUT COMPLETED, CLEANED AND TREATED AFFECTED AREA. REPAIR COMPLETED ON 12/26/00, IAW SRM 51-10-6. (M)SDR TSAA0053253Skin · crackedIDENTIFIED 3.7 INCH CRACK AT BS 747, STRINGER 18L. CONFIRMED USING HFEC METHOD. (M)SDR TSAA0057142Beam · gougedREPAIRED LT MLG BEAM AT THE OUTBOARD STABILIZER ATTACH POINT. REPAIR CONSISTS OF BLENDING OUT GOUGE AND REAMING OUT FASTENER HOLES AND INSTALLATIONS OF BUSHINGS IAW ECO 3146. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0053141Skin · crackedREPAIRED FUSELAGE SKIN 3 INCH CRACK AT BS 886 STRINGER 24 IAW SRM 53-30-3 FIG 1. VERIFIED BY HFEC METHOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033117Battery Pack · inoperativeREPLACED NR 1 FLOOR LIGHT ASSEMBLY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033116Light · inoperativeREPLACED NR 1 POSITION FLOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0053098Skin · crackedREPAIRED 1.5 INCH CRACK ON FUSELAGE SKIN AT BS 744, STRINGER 19L IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033073Battery Pack · inoperativeREPLACED THE AFT SERVICE DOOR EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033072Battery Pack · inoperativeREPLACED THE FORWARD ENTRY EXIT IDENTIFIER POWER PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA200033061Battery Pack · inoperativeREPLACED NR 3 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9933499Battery Pack · inoperativeREPLACED NR 6 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)SDR TSAA9933470Battery Pack · dischargedREPLACED NR 2 FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9933469Light · inoperativeREPLACED NR 2 FLOOR LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9972466Bleed Valve · failedFLT 263 - HNL-LIH - COMPRESSOR STALL NR 2 ENGINE THROTTLE UP OFF OF IDLE. ABORTED TAKEOFF. RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE PRESSURE BLEED CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD PER MM 75-31-11. AIRCRAFT RETURNED TO SERVICE.SDR TSAA9933452Light · inoperativeREPLACED FORWARD ENTRY EMERGENCY IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA9953404Skin · crackedFOUND 4.125 INCH CRACK 2 INCH FORWARD OF BS 947 AT STRINGER 24L. SKIN REPAIR IAW SRM 53-30-3 FIGURE 6 SHEET 4 PAGE 12B. AIRCRAFT RETURNED TO SERVICE. (M)
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