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 P5CA0401222Skin · corrodedLEFT MAIN LANDING GEAR FWD CUTOUT EXTERNAL PANEL SKIN FROM LBL 21 - LBL 10 HAS CORROSION. REMOVED CORROSION, CORROSION WITHIN LIMITS, PRIMED & TREATED.SDR P5CA0401221Stringer · corrodedAFT CARGO COMPT STRINGER 50L B/W STA 1680-1700 CORRODED. REMOVED LIGHT CORROSION, PRIMED & TREATED.SDR P5CA0401225Skin · crackedLEFT WING UPPER SURFACE O/B NR 2 PYLON L/E AREA 3 PLACES OF CRACKED SKIN. REMOVED SPLICE PLATE CRACK, FABRICATED SPLICE PLATE, TREATED & PRIMED.SDR P5CA0401223Panel · crackedAFT CARGO COMPT WALKWAY PANEL STA 1775-1795 LBL 22-45 HAS CRACKS, & CORROSION. REMOVED CORROSION, BLENDED & CUTOUT CRACK, FABRICATED DOUBLER, TREATED & PRIMED.SDR P5CA0401213Seat Track · corrodedLEFT CENTER SEAT TRACK DIRTY & CORRODED. REMOVED MINOR CORROSION FROM TRACK, TREATED & PRIMED.SDR P5CA0401211Skin · corrodedFUSELAGE SKIN JOINT HAS SURFACE CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401218Skin · corrodedFWD CARGO DOOR/LWR AFT SKIN HAS CORROSION. REMOVED CORROSION, FABRICATED DOUBLER & FILLER.SDR P5CA041224Skin · corrodedEXTERNAL SKIN AT STA 255 STR 32L AT LAP JOINT DELAMINATION. REMOVED BULGE, NO CORROSION FOUND, REMOVED FASTENER, INSTALLED NEW FASTENER, TREATED & PRIMED.SDR P5CA0401216Fitting · corrodedLEFT NOSE WELL BULKHEAD O/B SIDE OF NLG LWR STR FITTING IS CORRODED. REMOVED CORROSION, PRIMED & TREATED.SDR P5CA0401219Floor Panel · crackedBULK CARGO LEFT SIDE FLOOR PANEL BS 2040-2160 DENTED & CRACKED. CUT OUT DAMAGE AREA, FABRICATED & INSTALLED DOUBLER, PRIME & TREATED.SDR P5CA0401226Frame · corrodedCTR CARGO COMPT FRAME TOP OF UPPER CHORD AT STA 1740 RBL 40 IS CORRODED. REMOVED CORROSION FOUND OUT OF LIMITS, INSTALLED NEW CHORD.SDR P5CA0401217Keelbeam · corrodedKEEL BEAM BOX, PANEL SUPPORT STRUCTURE INNER LIP HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401205Fairing · delaminatedWING TO BODY FAIRING 1916L HAS DELAMINATION. CLEANED AREA & REBONDED.SDR P5CA0401215Keelbeam · corrodedKEEL BEAM BOX BOTTOM SURFACE HAS CORROSION LEFT & RIGHT SIDE. REMOVED FASTENER, REMOVED CORROSION & REINSTALLED FASTENER, TREATED & PRIMED.SDR P5CA0401209Floor Panel · corrodedFWD CARGO FLOOR PANEL HAS CORROSION. REMOVED SURFACE CORROSION, TREATED AND PRIMED.SDR P5CA0401207Web · crackedFWD CARGO COMPARTMENT WEB CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED.SDR P5CA0401208Skin · corrodedLT WING MID FLAP ENTIRE CENTER SECTION PANEL HAS SEVERAL CORROSION SPOTS. REMOVED SURFACE CORROSION , PRIMED AND TREATED.SDR P5CA0401206Keelbeam · corrodedKEEL BEAM APPROX STA 1093 HAS BOTTOM SURFACE CORROSION. REMOVED CORROSION, AFTER WORK IT IS 0.061, OK PER SRM 52-10-01.SDR P5CA0401204Seat Track · corrodedMAIN DECK CARGO COMPT SEAT TRACK HAS CORROSION. REMOVED CORROSION, PRIMED & TREATED.SDR P5CA0401203Frame · corrodedBULK CARGO COMPT FUSELAGE FRAME, UPPER CHORD TOP & BOTTOM HAS SURFACE CORROSION. REMOVE CORROSION, ORIGINAL MATERIAL IS 0.085, AFTER REWORK 0.083 WITHIN LIMITS.SDR P5CA0401202Seat Track · corrodedCABIN LEFT SEAT TRACK HAS CORROSION SPOTS. REMOVED CORROSION .020 MATERIAL WITHIN LIMITS.SDR P5CA0401201Frame · corrodedCENTER CARGO COMPT FRAME UPPER CHORD HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401200Skin · corrodedLEFT WING UPPER SKIN 24 INCHES FWD OF SPAN WISE BEAM NR 2 HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401199Skin · corrodedAFT FUSELAGE HAS SKIN CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401198Bulkhead · corrodedAFT BULKHEAD UNDER FLOOR & WEB CORRODED. REMOVED STIFFENER & WEB FROM FLOORBEAM, INSTALLED NEW ONE.SDR P5CA0401197Floor Support · crackedBULK CARGO COMPT LONGITUDINAL FLOOR SUPPORT CRACKED. REMOVED AND REPLACED DAMAGE AREA.SDR P5CA0401196Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION ALONG FWD OF MID SPAR. BLENDED OUT CORROSION, TREATED & PRIMED.SDR P5CA0401195Floorbeam · crackedBULK CARGO COMPT FLOORBEAM CRACKED. REMOVED & REPLACED DAMAGED AREA.SDR P5CA0401194Stringer · corrodedAFT CARGO COMPT STRINGER 51R HAS CORROSION. REMOVED LITE CORROSION MATERIAL, TREATED & PRIMED.SDR P5CA0401193Skin · corrodedRIGHT WING UPPER SKIN HAS SURFACE CORROSION. REMOVED LITE CORROSION, TREATED & PRIMED.SDR P5CA0100610Web · crackedNOSE WHEEL WELL - BS 300, RIGHT VERTICAL BEAM WEB, 1" LONG CRACK AT 3RD INSULATION HOLE FROM FLOOR BEAM CHORD. REPAIRED BY REMOVING EXISTING FASTENERS & BRACKETS, CUTTING OUT DAMAGED SECTION, INSTALLING DOUBLERS & (2) EA. "T" SECTIONS IAW BOEING TELEX PAO-LGBSDR P5CA0100609Web · crackedNOSE WHEEL WELL - BS320, RIGHT VERTICAL BEAM WEB, 2" LONG CRACK AT 2ND INSULATION HOLE FROM FLOOR BEAM CHORD. REPAIRED BY REMOVING EXISTING FASTENERS, CUTTING OUT DAMAGE, INSTALLING DOUBLER, SPLICE FILLER, SHIM & (2) EA. "T" SECTIONS IAW BOEING TELEX PAO-LGB-SDR P5CA0100608Web · crackedNOSE WHEEL WELL - BS300, LEFT VERTICAL BEAM WEB, 1/8" LONG CRACK AT 3RD INSULATION HOLE FROM FLOOR BEAM CHORD. OPENED HOLE TO 9/16". H.F.E.C. NO INDICATIONS. INSTALLED REPAIR DOUBLERS AS PER BOEING TELEX PAO-LGB-01-00155H & MA #A5310-33-10.SDR P5CA0100607Web · crackedNOSE WHEEL WELL - BS320, LEFT VERTICAL BEAM WEB - (3) CRACKS 1/8" LONG EA. LOCATED AT 2ND, 3RD & 5TH INSULATION HOLES FROM FLOOR BEAM CHORD. OPENED HOLE TO 9/16". H.F.E.C. NO INDICATIONS. INSTALLED REPAIR DOUBLERS AS PER BOEING TELEX PAO-LGB-01-00155H & MA SDR P5CA0100595Aileron · hung upWITH FLAPS UP, AILERON LOCKED UP WHILE TRYING TO MAKE A RIGHT TURN. WITH FLAPS 5 DEGREES, AILERON LOCKED AT LEFT BANK +/- 20 DEGREES (IAS 250 KNOTS). CLEANED LEFT AND RIGHT AILERON PROGRAMMERS AND LUBRICATED PER 12-21-16. FLIGHT CONTROL CHECK OF AILERONS OPSDR P5CA0100593Link · brokenR.H. O/B FORE FLAP, MOST O/B SUPPORT LINK BROKEN. REMOVED & REPLACED LINK ASSY. OPS CHECK O.K.SDR P5A0100592Light · inoperativeEMERGENCY LIGHTS IN UPPER DECK DO NOT TEST. REMOVED AND REPLACED U/D DOME EMERGENCY LIGHT PER MM 33-51-00. ALL OPS OK.SDR P5CA0000208Bushing · crackedRIGHT BODY LANDING GEAR INBOARD TRUNNION BUSHING CRACKED. REPLACED RT BODY LANDING GEAR INBOARD AND OUTBOARD TRUNNION FITTING. BORE REWORKED AND NEW REWORKED BUSHINGS INSTALLED PER SRM 53-10-08 FIG 1 & 2 AND POLAR CARD M3213-001.SDR P5CA0000209Frame · crackedMAIN DECK BS 2231 S-24L AND S-25L DOOR CUTOUT REVEAL CRACKED (DOOR 5L). REPAIRED PER SRM 53-10-04 FIG 91 AND BOEING INSTRUCTION PAO-HKG-00-00023H.SDR P5CA0000200Thrust Reverser · malfunctionedON TAKEOFF ROLL AT APPROX 25 KTS, NR 2 THRUST REVERSER UNLOCKED LIGHT ILLUMINATED. TAKEOFF ABORTED. TRANSFEREDTO MEL 78-2-A CAT C DMI NR 25184 AS PER MX CONTROL AXLE VERIFICATION INSPECTION C/W AS PER DDPG 78-2-A.SDR P5CA0000197Engine · stalledNR 2 ENGINE STALLED LOST POWER AND WAS SHUTDOWN PER IAW POLAR PROCEDURES. LOG PAGE NR 098103. REMOVED AND REPLACED NR 2 ENGINE AS PER POLAR W/C 7100-002, OPS CHECKS GOOD.SDR P5CA9900573Line · crackedFOUND HYDRAULIC LEAK FROM NR 4 SYSTEM RETURN LINE AT TOP OF LOWER AFT CARGO COMPARTMENT NEAR DOOR ACTUATOR. PERMANENT REPAIRED LINE (1 INCH DIAMETER) BY DEUTSCH PERMASWAGE REPAIR KIT. LEAK CHECKED OK. SERVICED NR 4 SYSTEM PER MM 29-11-00.SDR P5CA9900550Floorbeam · damagedFOUND FLOORBEAM AFT CARGO PIT STA 1800R DAMAGED. REPAIRED PER SRM 51-30-02 AND SRM 51-10-02.SDR P5CA9900549Panel · crackedFOUND RIGHT WING FLYING PANEL CRACKED. REPAIRED PER SRM 51-40-03.SDR P5CA9900558Frame · damagedNR 3 INBOARD POWER COWL NR 3 LATCH AREA HAS FRAME/OUTER SKIN DAMAGE. REPAIRED PER SRM 54-30-03.SDR P5CA9900557Doubler · crackedNR 3 OUTBOARD POWER COWL INNER DOUBLER FOUND CRACKED. REPAIRED PER SRM 54-30-03.SDR P5CA9900556Cowl · crackedNR 3 INBD POWER COWL NR 4 LATCH AREA FOUND TEAR. REPAIRED PER SRM 54-30-03.SDR P5CA9900555Frame · crackedAFT CARGO PIT AREA BS 1780 STR 25R T CAP SECTION CRACKED. REPAIRED PER SRM 51-40-03 AND 51-30-02.SDR P5CA9900554Fitting · crackedFOUND NR 1 ENGINE STRINGER ASSY ATTACH FITTING CRACKED. REPAIRED PER SRM 51-10-01 AND MM 78-11-01.SDR P5CA9900553Cowl · damagedFOUND NR 3 INBD POWER COWL FWD END CENTER STIFFENER ATTACH ANGLE BROKEN. REPAIRED PER SRM 51-10-01 AND 51-30-02.
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