N858FT
Service difficulty reports · 515
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 = 'N858FT' 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.
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 = 'N858FT' AND registry_match = 'registration' 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 P5CA9800079Panel · crackedLT WING OUTBD MIDFLAP ASSY COVE LIP PANEL HAS 10 FT CRACK. REMOVED AND REPLACED LT MIDFLAP ASSY COVE LIP PANEL PER MM 27-51-31.SDR P5CA9701820Doubler · crackedCRACKED DOUBLER NR 3 PYLON I/B SIDE AFT OF AFT MOUNT. REPAIRED PER POLAR MA 5430-07:01.SDR P5CA9701819Frame · crackedCRACKED MAIN DECK FUSELAGE CIRCUMFERENTIAL FRAME AT FS 1900 BETWEEN STRINGERS 11 AND 12. REPAIRED PER POLAR AIR MA 5310-23:01.SDR P5CA9701818Rivets · shearedSHEARED RIVETS ON TIE CLIPS, MAIN DECK FUSELAGE CIRCUM FRAME AT FS 1900 STRINGERS 10, 11, 12, 13, AND 14. REPAIRED PER POLAR AIR MA 5310-23:01.SDR P5CA9701817Rivets · shearedSHEARED RIVETS ON TIE CLIPS, MAIN DECK FUSELAGE CIRCUM FRAME AT FS 1920 STRINGERS 11 AND 12. REPAIRED PER POLAR AIR MA 5310-23:01.SDR P5CA9701816Frame · gougeGOUGE ON PRODUCTION SPLICE MAIN DECK FUSELAGE CIRCUMFERENTIAL FRAME AT FS 1920 BETWEEN STRINGERS 11 AND 12. REMOVED AND REPLACED DAMAGED PRODUCTION SPLICE AS PER SRM 51-10-01.SDR P5CA9701828Frame · crackedFRAME AT STA 1900 BETWEEN STR 11R AND 12R FOUND TO BE CRACKED AS A RESULT OF CARGO LOADING. THE CRACK SEVERED THE FRAME JUST ABOVE THE PRODUCTION SPLICE. REPAIRED PER POLAR AIR CARGO MA 5310-23:01.SDR P5CA9701759Panel · crackedCRACKED UPPER WING FIBERGLASS PANEL AT WS 920. REPAIRED PER BOEING SRM 51-40-09 AND 51-10-01.SDR P5CA9701758Panel · crackedCRACKED FIBERGLASS PANEL LEFT WING UPPER SURFACE AT LEADING EDGE WS 1250. REPAIRED PER BOEING SRM 51-40-09 AND 51-10-01.SDR P5CA9701757Skin · buckledBUCKLED SKIN LEFT WING LEADING EDGE WS 920 TOP SIDE OF NOSE BEAM AFT OF NR 8 LEADING EDGE FLAP. REPAIRED PER BOEING SRM 57-20-03 AND 51-10-01.SDR P5CA9701756Skin · buckledBUCKLED SKIN LEFT WING LEADING EDGE WS 1060 TOP SIDE OF NOSE BEAM. REPAIRED PER BOEING SRM 57-20-03 FIG 7, 57-20-03 AND 51-10-01.SDR P5CA9701755Skin · buckledBUCKLED SKIN LEFT WING LEADING EDGE WS 1250 TOP SIDE OF NOSE BEAM AFT OF NR 5 LEADING EDGE FLAP. REPAIRED PER BOEING SRM 57-20-03, 51-40-03, 57-30-04 FIG. 2 AND 51-10-01.SDR P5CA9701596Panel · missingLEFT WING BLOW OUT PANEL FOUND MISSING ON WALK-AROUND INSPECTION. REPLACED PANEL PER BOEING SRM 51-10-01.SDR P5CA9701601Support · brokenBROKEN LEFT WING LEADING EDGE SUPPORT ROD AFT OF NR 6 LEADING EDGE FLAP. REPLACED SUPPORT ROD PER BAC MM 57-21-00.SDR P5CA9701600Floorbeam · crackedCRACK ON UPPER CAP ON FLOORBEAM AT STA 1860, BL 58. FABRICATED AND INSTALLED UPPER CAP PER BAC SRM 51-30-00.SDR P5CA9701599Flange · crackedCRACK ON NR 3 ENGINE TURBINE EXHAUST CASE R-FLANGE (RAIL) AT 6 O'CLOCK. WELDED AND STRESS RELIEVED CRACK PER PWA ENGINE MANUAL 72-53-01.SDR P5CA9701598Flange · crackedCRACK ON NR 2 ENGINE TURBINE EXHAUST CASE S-FLANGE (RAIL) AT 2 O'CLOCK. WELDED AND STRESS RELIEVED CRACK PER PWA ENGINE MANUAL 72-53-01.SDR P5CA9701597Clips · crackedCRACKED SUPPORT CLIPS ON FORWARD AND AFT INNER WEB ON NR 1 PYLON. FABRICATED AND INSTALLED REPLACEMENT CLIPS PER BAC SRM 51-30-01 AND 51-30-03.SDR P5CA9701436Lock Linkage · out of trackUNABLE TO OPEN CREW OVERHEAD EMERGENCY ESCAPE HATCH. FOUND LOCK LINKAGE OUT OF TRACK. REINSTALLED PROPERLY AND DOOR OPEN AND CLOSED OK. LATCH PIN REINSTALLED IAW OVERHAUL MANUAL 52-22-11 AND M/M 52-21-01.SDR P5CA9701433Warning Light · illuminatedSECOND INCIDENT, WARNING LIGHT FOR LOWER AFT CARGO DOOR ILLUMINATED AFTER TAKEOFF DURING FLAP RETRACTION. DUMPED FUEL AND RETURNED TO DEPARTURE STATION. WHEN FLAPS EXTENDED TO 20 UNITS LIGHT WENT OUT THEN BACK ON. LIGHT EXTINGUISHED DURING LANDING GEAR EXTESDR P5CA9701432Warning Light · illuminatedWARNING LIGHT FOR LOWER AFT CARGO DOOR ILLUMINATED AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO DEPARTURE STATION WITH LIGHT EXTINGUISHING WHEN LANDING GEAR EXTENDED. INSPECTED DOOR WITH NO DEFECTS NOTED. CHECKED AND ADJUSTED DOOR SWITCHES PER BAC MM 52-71-0SDR P5CA9701431Altimeter · malfunctionedFLUCTUATION ON CAPTAINS ALTIMETER FROM 25,000 FT TO NEGATIVE 800 FT. REPLACED CAPTAINS ALTIMETER PER BAC MM 34-13-04 AND OPERATIONAL CHECK OK.SDR P5CA9701302Tire Tread · missingON POST FLIGHT INSPECTION, FOUND NR 4 TIRE WITH TREAD MISSING, TIRE DID NOT DEFLATE. TREAD HAD DAMAGED LEFT INBOARD FLAP. REPLACED TIRE ASSEMBLY PER M/M 32-45-01. REPAIRED FLAP PER BOEING SRM 51-40-09, 51-40-06 AND POLAR MA 5750-06:01.SDR P5CA9701216Wire · brokenRIGHT WING OVERHEAT LIGHT ON. ISOLATED RIGHT WING IAW CHECKLIST LIGHT DID NOT GO OUT WITH EITHER NR 3 OR NR 4 ENGINE AT IDLE. WITH NR 3 ENGINE OF AND NR 4 ENGINE AT IDLE LIGHT WENT STEADY ON. FOUND WIRES TO AFT OVERHEAT SENSOR IN NR 4 PYLON BROKEN FROM SENSSDR P5CA9701215Duct · damagedRIGHT WING OVERHEAT LIGHT ON AFTER TAKEOFF. FOUND FLEXIBLE PNEUMATIC DUCT LEAKING DUE TO INTERNAL DAMAGE. REPLACED DUCT LEAK, CHECKED PER MAINTENANCE MANUAL 36-11-00.SDR P5CA9701190Clamp · looseRIGHT WING OVERHEAT LIGHT ON CLIMBOUT. PER MAINTENANCE MANUAL 36-11-00 ACCOMPLISHED DUCT LEAK CHECK AND PNEUMATIC DECAY CHECK. NOTED DUCT LEAK AT AFT CLAMP TO PYLON VALVE. REMOVED CLAMP AND INSPECTED DUCT, VALVE AND CLAMP, NO DEFECTS NOTED. REINSTALLED CLASDR P5CA9701169O-Ring · pinchedNR 4 ENGINE OIL QUANTITY DECREASED TO ZERO IN FLIGHT, RATE OF DECREASE 1.5 GALLONS PER HOUR. LOW OIL PRESSURE LIGHT ILLUMINATED WITH LOW OIL PRESSURE INDICATED ENGINE SHUT DOWN. REPLACED PINCHED O-RING ON MAIN OIL FILTER HOUSING PER MAINTENANCE MANUAL 72-61-SDR P5CA9701125Brace · damagedNR 3 ENG PYLON DIAGONAL BRACE DAMAGED AND CHAFING ON O/B SAIL PLANE DOOR AT LOWER O/B SIDE. BLENDED OUT CHAFED AREA IAW BOEING SRM 54-40-01 FIG 5 MATERIAL WITHIN LIMITS.SDR P5CA9701124Brace · damagedNR 4 ENG PYLON DIAGONAL BRACE DAMAGED AND CHAFING ON O/B SAIL PLANE DOOR LOWER O/B SIDE. BLENDED OUT CHAFED AREA IAW BOEING SRM 54-40-01 FIG 5 MATERIAL WITHIN LIMITS.SDR P5CA9701123Intercostal · corrodedLEVEL 2, INTERCOSTAL IN KEEL BEAM AREA HAS SEVERE CORROSION AT APPX BS 1460. REMOVED AND REPLACED INTERCOSTAL IAW BOEING SRM 51-30-02.SDR P5CA9701122Panel · delaminatedKEEL BEAM FUSELAGE PANEL BETWEEN WING GEAR INBD DOORS BULGED. REMOVED PANEL AND FABRICATED NEW PANEL, WORK DONE ON TRAVELER NR 78603.SDR P5CA9701121Battery Pack · dischargedUPPER DECK EMERGENCY LIGHT INOPERABLE. REMOVED AND CHARGED BATTERY PACK PER OHM 33-50-02 AND REINSTALLED BATTERY PACK PER MM 33-51-00.SDR P5CA9701116Web · crackedLOWER RUDDER JUST BELOW ACTUATOR, CRACK IN WEB. REPLACED/INSTALLED IAW SRM 51-30-02 AND 51-10-01.SDR P5CA9701120Heat Exchanger · crackedNR 3 A/C PACK HEAT EXCHANGER IS CRACKED. REINSTALLED NR 3 HEAT EXCHANGER IAW MM 21-51-03, WELDED CRACKED AREA IAW BAC5975.SDR P5CA9701119Cowl Skin · dentedNR 3 ENG OT/BD CORE COWL SKIN DENTED. CUT OUT DAMAGED AREA AND REPAIRED IAW BOEING SRM 54-30-02.SDR P5CA9701118Cowl · crackedNR 1 ENGINE IN/BD CORE COWL SKIN CRACKED AT AFT LWR EDGE. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER FILLERS AND INSTALLED AND TREATED IAW BOEING SRM 54-30-03 AND 51-30-02.SDR P5CA9701117Cowl · damagedNR 1 ENG OT/BD CORE COWL FWD UPPER EDGE DAMAGED. REMOVED DAMAGED AREA IAW BOEING SRM 54-10-02 AND REPAIRED IAW BOEING SRM 54-20-02.SDR P5CA9701115Cowl Skin · crackedNR 3 ENG OUT/BD CORE COWL SKIN CRACKED/PUNCTURED. REPAIRED IAW BOEING SRM 54-30-02.SDR P5CA9700553Insert · strippedNR 4 ENGINE SHUT DOWN DUE TO LOW OIL QUANTITY AND LOW OIL PRESSURE. ENGINE WINDMILLED WITH N1 30 PERCENT, N2 2 PERCENT, OIL PRESSURE 10 PSI, OIL TEM 50 DEGREES. FOUND ANGLE GEAR BOX COVER LOOSE REPLACED MOUNT BOLT BUSHING PER M/M 72-61-00. PERFORMED GEAR BOSDR P5CA9700524O-Ring · leakingNR 4 ENGINE OIL QUANTITY DROPPED TO 0 AND OIL PRESSURE LIGHT CAME ON. SHUT DOWN ENGINE, WINDMILL TIME 22 MINUTES WITH ZERO OIL PRESSURE AND QUANTITY. FOUND PACKING LEAKING AT BOTTOM OF TOWER SHAFT REPLACED PACKING PER M/M 72-61-00 PAGE 1, COMPLIED WITH WINDMSDR P5CA9700510Skin · damaged#3 PYLON TO RIGHT WING LEADING EDGE PULLED RIVETS ON REPAIR. REPLACED FASTENERS PER BOEING SRM 51-30-02.SDR P5CA9700507Union · distortedNR 4 HYDRAULIC SYSTEM WENT FROM 8.5 GALLONS TO 2.5 GALLONS, AS PER ALTERNATE PROCEDURES DEPRESSURIZED EDP AND ADP QUANTITY STABILIZED AT 2.5 GALLONS. RETURNED TO MIA. FOUND NR 4 EDP PRESSURE LINE BULKHEAD FITTING AT VERTICAL FIREWALL DISTORTED. REMOVED AND SDR P5CA9700428Module · failedAUTO BRAKE LIGHT ON IN FLIGHT, AUTO BRAKE WILL NOT ENGAGE. ON ROLL OUT, 3 TIRES BLOWN. CONFIRMED AUTO BRAKE FAILED IN OPEN DEFERRED PER MEL 32-23, TESTED ANTI-SKID. FOUND THAT BRAKES 9, 11, 12, AND 13 FAILED CHECK PER MAINTENANCE MANUAL 32-42-00. REPLACED SDR P5CA9700387Fuel Qty Ind · frozeIN CRUISE, NR 3 MAIN FUEL QTY INDICATOR FROZE AT 61,000 LBS, 5 HOURS INTO FLIGHT, NR 3 FORWARD BOOST PUMP LOW PRESSURE LIGHT CAME ON. DUE TO WEATHER IN JFK, DIVERTED TO ORD. TRANSFERED TO DMI PER MEL 28-11. INDICATOR CHANGED AT JFK, CALIBRATED PER MAINTENANSDR P5CA9700301Skin · delaminatedRIGHT WING INBOARD MID FLAP LEADING EDGE OUTBOARD END DELAMINATED. REPAIRED PER BOEING SRM 51-40-09, PAINTED PER 51-24-11.SDR P5CA9700297Door · crackedLEFT WING LANDING GEAR AFT LOWER CORNER OF FLYING DOOR CRACKED. REMOVED AND REPLACED LEFT W/L/G INBD DOOR I/A/W M.M. 32-12-06.SDR P5CA9700285Tr Sleeve · damagedNR 3 ENGINE EXTERIOR SKIN ON T/R SLEEVE IS DAMAGED (SCRATCHES AND GOUGES) RT SIDE AT 4:30 AND 5 O'CLOCK POSITION. SANDED AND CLEANED OUT SCRATCHES ABD GOUGES I/A/W SRM 54-00-02.SDR P5CA9700284Rub Strip · gougedRIGHT INBOARD AFT FLAP RUB STRIP GOUGED. BLENDED OUT GOUGE AND FILLED I/A/W SRM 51-41-01.SDR P5CA9700283Skin · damageNR 3 SAILBOAT INBOARD DOOR INTERNAL SKIN PUNCTURED. ROUTED OUT AND SMOOTHED PUNCTURED AREA, FABRICATED FILLER AND DOUBLER, AND BONDED REPAIR MEMBERS I/A/W SRM 51-10-06.SDR P5CA9700282Flange · brokenNR 2 PYLON DUCT ATTACH FLANGE BROKEN. REPAIRED BY WELDING FLANGE I/A/W WD 85SFT9701A.
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