N857FT, cancelled Aug 30, 2007
Service difficulty reports · 306
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 = 'N857FT' AND deregistration_id = 'N857FT-2007-08-30' 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 = 'N857FT' AND deregistration_id = 'N857FT-2007-08-30' 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 P5CA9900568Panel · delaminatedLEFT WING TOP FIXED T/E PANEL BETWEEN I/B AILERON AND SPOILER NR 5 TOP SURFACE FOUND DELAMINATED. REMOVED OLD REPAIR AND WATER. REPLACED DAMAGED CORE, FILLERS AND OVERLAYS PER SRM 51-40-12.SDR P5CA9900569Panel · delaminatedLEFT WING T/E UPPER FIXED PANEL AT WING STA 1190 LOWER SURFACE FOUND DELAMINATED. SANDED CLEANED AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR, APPLIED PARTS UNDER VACCUUM AND CURED REPAIR PER SRM 51-40-09.SDR P5CA9801619Skin · holeLEFT WING OUTBOARD POSITION FORE FLAP LEADING EDGE HAS HOLE IN PREVIOUS REPAIR. REPAIRED DAMAGED AREA PER SRM 51-40-09.SDR P5CA9801618Spoiler · holeRIGHT WING NR 12 SPOILER HAS SMALL HOLE IN TOP SIDE SURFACE. CLEANED, POTTED DAMAGED AREA AND REPAIRED PER SRM 51-40-06.SDR P5CA9801617Liner · crackedAPU EXHAUST INNER LINER HAD 12 INCH CRACK. REMOVED AND REPLACED EXHAUST LINER PER MM 49-81-03.SDR P5CA9801616Cowl · holeNR 3 ENGINE OUTBOARD CORE COWL HAS HOLE IN SKIN AND TEMPORARY FASTENER INSTALLED. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.SDR P5CA9801615Fairing · damagedNR 4 ENGINE FWD FAIRING HAS A HOLE WORN THRU STRUCTURE. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03.SDR P5CA9801275Longeron · damageSTA 1900 LONGERON 19R TO 26R FRAME HAS SERVERAL GOUGES ON I/B LIP. REPAIRED FRAME IAW SRM 51-40-03.SDR P5CA9801274Frame · crackedRT I/B MIDFLAP INBOARD MOST FRAME CRACKED. STOPPED DRILLED CRACK AND FABRICATED DOUBLER AND TREATED, PRIMED AND INSTALLED IAW SRM 51-40-03.SDR P5CA9801273Stringer · crackedSTA 2330 LONGERON 14R IS CRACKED. REMOVED CRACKED STRINGER AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-10-03 FIG 4 AND 54-30-02.SDR P5CA9801272Longeron · crackedSTA 2330 LONGERON 17R IS CRACKED. REMOVED CRACKED STRINGERS AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STRINGER AND SPLICE IAW SRM 53-30-02 FIG 4 AND 51-30-02.SDR P5CA9801260Frame · damagedFRAME AT STA 2060 HAS SEVERAL GOUGES FROM GILL LINER SUBSTRUCTURE AT LONGERON 14R TO 21R. REPAIRED FRAME IAW SRM 51-10-03. INSTALLED DOUBLER IAW SRM 51-30-02.SDR P5CA9801259Frame · damagedFRAME AT STA 1780 RIGHT SIDE HAS DEEP GOUGE CAUSED FROM GILL LINER SUBSTRUCTURE AT LONGERON 21R. BLENDED GOUGE AT FRAME IAW SRM 51-10-01. INSTALLED DOUBLER REPAIR IAW SRM 51-10-01.SDR P5CA9801258Fairing · damagedNR 3 FLAP CANOE TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS LAY UP OF 3 PLY SKINS IAW SRM 51-40-15.SDR P5CA9801257Skin · puncturedHOLE IN LOWER SURFACE OF LEFT INBOARD AILERON. CLEANED AREA, REMOVED DAMAGED MATERIAL, AND REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-06.SDR P5CA9801264Angle · crackedL ANGLE BELOW SPLICE FITTING AT RIGHT BODY GEAR WHEEL WELL STA 1480 CRACKED. REMOVED AND REPLACED L ANGLE IAW SRM 51-10-01 AND 51-30-02.SDR P5CA9801263Fitting · damagedRT I/B MIDFLAP AFT SUPPORT FITTING GOUGED. REMOVED AND REPLACED RT O/B MIDFLAP AFT SUPPORT FITTING IAW SB 747-27-2280.SDR P5CA9801262Skin · corrosionLEVEL 1 CORROSION, FOUND UNDER BOTH ATC ANTENNAS. REMOVED CORROSION IAW SRM 51-10-06.SDR P5CA9801261Skin · damagedRT I/B MIDFLAP HAS DEEP GOUGE AT LEADING EDGE I/B CARRIAGE CUT OUT. REWORKED GOUGES IAW SRM 57-50-01. TREATED AND PRIMED IAW SRM 51-10-02.SDR P5CA9801271Pin · corrodedRIGHT WING NR 7 SPINDLE AFT BOGIE O/B SUPPORT PIN CORRODED. REPLACED O/B SUPPORT PIN ON NR 7 SPINDLE AFT BOGIE IAW 747 OHM 27-51-75.SDR P5CA9801270Skin · delaminatedRIGHT FLYING DOOR LOWER SECTION HAS SPOTS OF DELAMINATION ON ITS INNER SURFACE AT DENT LOCATION. SANDED AND REMOVED DAMAGED AREA AND REPAIRED IAW SRM 51-40-09.SDR P5CA9801269Cowling · damagedNR 4 ENG INBOARD T/R TRAILING EDGE AT 8 O'CLOCK POSITION SKIN DAMAGED AND PEELING IN THREE AREAS. REPAIRED SKIN ROUTED SMALL CRACK AND REBONDED SKIN IAW 51-40-05.SDR P5CA9801268Skin · damagedNR 2 LEFT AFT FLAP TRAILING EDGE DAMAGED. REPAIRED DAMAGE AT AFT T/E FLAP IAW SRM 51-40-09.SDR P5CA9801267Fairing · damagedNR 2 FLAP FAIRING CANOE HAS HOLE DAMAGE INSIDE. APPLIED FIBERGLASS OVERLAYS AND REPAIRED IAW SRM 51-40-15.SDR P5CA9801266Skin · damagedLEFT INBOARD MIDFLAP HAS HOLE IN UPPER SURFACE JUST AFT OF INBOARD CARRIAGE. REMOVED DAMAGED SKIN AND REPAIRED WITH FIBERGLASS DOUBLERS IAW SRM 51-40-09.SDR P5CA9801265Antenna · corrosionNR 1 AND NR 2 ATC ANTENNAS HAVE SURFACE CORROSION. REPLACED BOTH NR 1 AND NR 2 ATC ANTENNAS. OPS CHECKED GOOD IAW 3450-01-01.SDR P5CA9801250Door · corrodedLEVEL 1 CORROSION LEFT FLYING DOOR LOWER SECTION ALONG LOWER EDGE OF ITS INNER SURFACE AROUND BOLD HEADS. REMOVED AND REPLACED FASTENERS AND CLEANED AREAS IAW SRM 51-30-02.SDR P5CA9801249Skin · crackedNR 3 ENG O/B FAN COWL CRACK ON UPPER FWD AND AFT HINGE CUTOUT. BLENDED OUT CRACKED AREA AROUND FORWARD HINGE. CRACK WITHIN SRM LIMITS PER SRM 51-40-06 FIG 2. REPAIRED PER SRM 51-40-06.SDR P5CA9801248Floorbeam · corrodedLEVEL 1 CORROSION FOUND ON BOTTOM OF FLOORBEAM BS 600. REMOVED SURFACE CORROSION IAW SRM 51-10-01.SDR P5CA9801247Support · corrodedLEVEL 1 CORROSION FOUND UNDER F/E SEAT FLOOR PANEL SUPPORT BEAM. REMOVED SURFACE CORROSION ON SUPPORT BEAM AND TREATED IAW SRM 51-10-06.SDR P5CA9801246Support · corrodedLEVEL 1 CORROSION AT SUPPORT CHANNEL FOR DRAIN PAN AT BS 340. CORROSION REMOVED FROM SUPPORT CHANNEL AT STA 340 IAW SRM 51-10-01.SDR P5CA9801222Skin · corrosionRT BODY MLG BOTH INBOARD AND OUTBOARD STRUT DOOR ASSEMBLIES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02.SDR P5CA9801215Skin · corrosionLEFT BODY MLG INBD AND OTBD STRUT DOOR ASSEMBILES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02.SDR P5CA9800776Cowl · dentedNUMBER 2 ENGINE NOSE COWL SKIN DENTED AT 0630 POSITION. REPAIRED NOSE COWL PANEL AT 0630 POSITION PER SRM 51-40-07.SDR P5CA9800774Transmitter · inoperativeNR 2 ENGINE WOULD NOT MAKE TAKEOFF THRUST. TEMP 912 DEGREES 1:08 EPR. ABORTED TAKEOFF. REMOVED AND REPLACED EPR TRANSMITTER REF MM 77-11-00. REMOVED AND REPLACED T7 LINE AS PRECAUTION REF MM 77-12-00. REQ OPS CHECK. OPS CHECK SATISFACTORY PER MM 77-00-00.SDR 98ZZZX2249Brake · damagedWHILE PARKED ON GATE, NR 9, NR 11, AND NR 15, MAIN WHEELS COLLAPSED DUE TO BRAKE OVERHEAT. ON WHEEL CHANGE, NR 11 AND NR 15 BRAKE UNITS WERE FOUND DAMAGED AND WERE REPLACED.SDR P5CA9800767Fitting · gougedLEFT I/B AILERON I/B PRIMARY HINGE WING FITTING LT SIDE IS GOUGED BY RETAINER BOLT HOLE AREA. BLENDED GOUGE LESS THAN 10 PERCENT MATERIAL LOSS PER SRM 57-50-01.SDR P5CA9800765Engine · malfunctionedVIBRATION ON TAKEOFF. RETARDED AND ADVANCED NR 2 ENG THROTTLE. VIBRATION FOLLOWED THROTTLE MOVEMENT. A/C PACKS WERE OFF. REMOVED AND REPLACED NR 2 ENGINE PER MM 71-00-00. OPS CHECK, LEAK CHECK ALL NORMAL ON ENG RUN-UP PER MM 71-00-00.SDR P5CA9800747Keel Beam · damagedSHEET METAL DAMAGE TO LOWER KEEL BEAM AREA AND LOWER WEB AT STA 1380 RT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING OUT DAMAGE AND FABRICATION FILLERS, DOUBLERS AND TRIPLERS AND REPLACING PER PAC MA NR 5310-24:10.SDR P5CA9800746Accumulator · failedBRAKE ACCUMULATOR LOWER CAP BROKEN OFF COMPLETELY. REMOVED AND REPAIRED BRAKE ACCUMULATOR PER MM 32-41-09. PRECHARGED ACCUMULATOR PER MM 12-15-09. SYSTEM TESTS NORMAL PER MM 32-41-00.SDR P5CA9800745Keel Beam · damagedSHEET METAL DAMAGE TO UPPER KEEL BEAM WEB AT STATION 1380 IN THE RIGHT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUTTING DOUBLERS AND TRIPLERS PER PAC MA 5310-24:01.SDR P5CA9800738Accumulator · rupturedDURING APPROACH, AFTER GEAR DOWN LOST NR 4 HYD SYSTEM, 0 BRAKE PRESSURE ON GUAGE. HYD BRAKE ACCUMULATOR RUPTURED, DAMAGE TRIM AIR DUCT, APU FUEL DRAIN LINE, HYD LINE DAMAGE.SDR P5CA9800572Support · crackedAPU VERTICAL SUPPORT TUBE AT BS 2705 WL 364 HAS CRACK. REPLACED PER SRM 51-10-01.SDR P5CA9800571Flap · corrosionLEVEL 1 CORROSION AT LEADING EDGE FRONT SPAR WS 972 NR 7 FLAP. REPAIRED CORROSION PER SRM 51-10-01.SDR P5CA9800570Stiffener · corrosionLEVEL 1 CORROSION ON RT WING GEAR STA 1350 STIFFENER. REPAIRED CORROSION PER SRM 51-10-01.SDR P5CA9800569Frame · crackedBS 540 S26L FRAME CRACKED. REPAIRED FRAME PER RS53-22-33687 BOEING.SDR P5CA9800567Seat Track · corrosionLEVEL 1 CORROSION ON SEAT TRACK STA 920 RBL 97R. REPAIRED CORROSION PER SRM 53-10-05.SDR P5CA9800734Support · crackedLEVEL 1 CORROSION MAIN DECK FLOOR SUPPORT BL 22 TO 24. REPAIRED CORROSION PER SRM 51-40-04.SDR P5CA9800733Tie Down · corrodedLEVEL 1 CORROSION AT TIE DOWN FITTING SUPPORT FUSELAGE BS 2300 BL 22. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.SDR P5CA9800732Tie Down · corrodedLEVEL 1 CORROSION AT TIE DOWN FUSELAGE BS 2180 BL 30. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02.
Back to N857FT, cancelled Aug 30, 2007