N855GT
Service difficulty reports · 125
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 = 'N855GT' 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 = 'N855GT' 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 P5CA2021042100147Stringer · crackedCRACK DAMAGE ON THE STRINGERS S-9R, AT AFT SIDE OF STA 2180(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-934 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U3481 SH63 REV -, 146U3922 SH 21 REV - AND 146U2200 SH 120 REV C. CONDITION CHK NORMSDR P5CA2021042100148Stringer · crackedCRACK DAMAGE ON THE STRINGER S-22R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-924 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1323 SH 105 REV -, AND 146U1961 SH 615, 614 - . CONDITION CHECK NORMAL AND JOB COMPLESDR P5CA2021042100149Stringer · damagedCRACK ADAMAGE ON THE STRINGER S-12R, AT FWD SIDE OF STA 1960(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-922 REV 1. REINSTALL FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U1961 SHEET 465 REV B AND 146U1312 SH 123 REV -. CONDITION CHECK NORMAL AND JOB COMPLSDR P5CA2021042100150Stringer · damagedCRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2180(<P>REPAIRED DAMAGED AREA IAW EI NO T2021A53M-935 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2181 SH 392 REV A AND 146U2200 SH 164 REV -. CONDITION CHECK NORMAL AND JOB COMPLETSDR P5CA2021042100151Wire · damagedFOUND WIRE WS95-328-20R / W895-329-20B / WS95-330-20Y AND W895-334-20R / W895-335-20B / W895-336-20Y WIRE TOUCH WITH STRUCTURE AND DAMAGE NEAR CONNECTOR DV 744 #2 RAM AIR INLET ACTUATOR(<P>IAW SMM 21-622-03-00-801 / 21-62-03-400-801 REV 35, WDM 21-62-21 REV 23SDR P5CA2021010200001None · noneBIRD STRIKE HALFWAY DOWN RW 27 JUST PRIOR TO ROTATE. MCC DIRECTED TO RETURN TO CVG FOR MX INSPECTION. BIRD STRIKE AREA IS NOSE/CARGO DOOR (RT SIDE) STA 200/RWL 250 AND RWL 312. AFFECTED AREA HAS BEEN CLEANED AND INSPECTED, NO DAMAGE FOUND. ENGINES AND AIRCRAFTSDR P5CA2020110400371Engine · malfunctionedFLIGHT CREW REPORTED TO HKG MX THAT NR 3 ENGINE DID NOT SPOOL UP ON TAKE OFF, BUT SECOND TRY WAS NORMAL. DISCUSSED WITH PPE, AND DOWNLOADED QAR DATA FOR REVIEW.SDR P5CA2020042000145Compressor · stalledREPEAT WRITEUP - REF LOG PAGE 1127088. DURING TAKEOFF ROLL AND ENGINES ACCELERATING TO TAKEOFF THRUST, COMPRESSOR STALL EITHER #1 OR #2 AT A LOW SPEED 30 KNOTS. A FLASH OF LIGHT WAS VISABLE ALSO.(<P>ENGINE 1 REMOVED AND REPLACED IAW GE 8130 FORM 20398. OPS CHESDR P5CA2020041400144Unknown · malfunctionedDURING TAKE OFF ROLL AND ENGINE ACCELERATING TO THRUST, SUSPECT COMPRESSOR STALL ON EITHER 1 OR 2.(<P ><SPAN>C/W ECM #2020P-176 AND / 2020P-174. NO DEFECTS NOTED.</SPAN></P>)SDR P5CA2019041600054Support · damagedLHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 398, UPPER BEAM.(<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 398 - 404.55 RIB FASTENER HOLES ELONGATION AREAS REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2019041600055Support · damagedLHW L/E CAVITY SUPPORT STRUT UPPER MOUNTING HOLE FOUND ELONGATE AT ILES 440, UPPER BEAM. (<P>LHW L/E CAVITY SUPPORT STRUT AT ILES 440 - 442.84 RIB FASTENER HOLES ELONGATION AREA REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2019041600056Spar · crackedNO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA. (<P>NO.2 PYLON CAVITY REAR SPAR BOTTOM AREA WING FIXED LEADING EDGE VAPOR BARRIER CRACK AT I/B NACELLE AREA REPAIRED IAW SRM 57-41-01-2R-6 REPAIR 6, TEMPORSDR P5CA2019041600057Support Bracket · crackedAPU COMPARTMENT R/H STA 2696 CONDUIT SUPPORT BRACKET MOUNTED FRAME CRACKED.(<P>APU COMPARTMENT R/H STA 2696 WL 292, LOWER SUPPORT FRAME CRACK AREA REPAIRED IAW RI-53-82-13469 REV. A. </P>)SDR P5CA2018010800005Line · damagedUPPER DECK PORTABLE ELT ROPE DAMAGED. THE PORTABLE ELT WAS REMOVED AND REPLACED IAW AMM 25-63-03.SDR P5CA2017032800078Support · crackedNR 3 PYLON CAVITY VAPOR BARRIER FWD OTBD SUPPORT, CRACKED. REPAIRED IAW RI-57-41-10697, REV A.SDR P5CA2017032800076Panel · crackedRIGHT WING NR 5 FLAP TRACK, FWD UPPER FIXED PANEL OTBD CHANNEL AFT SIDE FOUND CRACKED. REPAIRED IAW RI-57-22-11773, REV A.SDR UIEA2016082600709Pump · leakingSTATUS HYDRAULIC PRESSURE ENGINE 2 AND EICAS HYDRAULIC QTY LOW 2. REMOVED ENGINE 1 EDP AND INSTALLED ON 2 ENGINE IAW AMM 29-11-05. OPS CHECK
AND LEAK CHECK GOOD, NO DEFECTS NOTED AT THIS TIME.SDR UIEA2016062000433Pump · leakingAFTER TAKEOFF HYDRAULIC QTY LOW 4 EICAS MESSAGE. RAN ECL NR 4, SYSTEM OFF. REF LP 812459, ITEM 11. FOUND NR 4 ADP HYDRAULIC PUMP LEAKING. R & R NR 4 ADP AND OPS AND LEAK CHECKS OK IAW MM 29-11-17.SDR UIEA2016041000238Jumper · openDURING TAKEOFF ROLL RECEIVED AURAL WARNING, MASTER CAUTION LIGHT & EICAS ALERT MSG CONFIG. PERFORMED REJECTED TAKEOFF AT APPROX 145 KNOTS. FOUND CMC MSG 277791. PERFORMED TROUBLESHOOTING IAW AMM 27-00-00 & FOUND JUMPER AT LE PANEL OPEN. R & R JUMPER WERE PSDR UIEA2015092700555Warning System · false activationREJECTED TAKEOFF AT 60KTS DUE TO CONFIG SPOILER EICAS WARNING. CUT OUT INSPECTION OF SPOILERS & CARRIED OUT OPERATIONS CHECK OF SPOILERS IAW AMM 27-61-00-715-001 & ALL SATISFACTORY.SDR UIEA2015052600285Unknown · unknownENGINE NR 1 OIL QTY GRADUALLY WENT DOWN TO ZERO, ALL OTHER INDICATIONS, OIL PRESS & TEMP WERE NORMAL. PERFORMED OPEN & CLOSED COWL INSPECTION IAW AMM 79-00-00, NO LEAKS NOTED AT THIS TIME. PERFORMED ENG DRY MOTOR IAW AMM 71-00-00 TEST 2, NO LEAKS NOTED AT THSDR UIEA2015030300160Skin · dentedDENT ON FUSELAGE SKIN AT STATION 516 BETWEEN STRINGER 35R - 36R. REPAIRED DAMAGE AREA IAW EI NO T2015A53B-390 REV 1. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2015020100060Fan · defectiveNUMBER 1 PACK PRODUCES AN ODD SMELL AS IF THERE IS ELEC BURNING. VISUAL INSPECTION AT PACKS INLET & OUTLET AT PACK 1 BAY, NO ABNORMALITIES NOTED. REF ITEM 3 DETAILED INSPECTION ACCOMPLISHED & FOUND EE SUPPLY FAN AT FAULT. FAN DEACTIVATED & OPERATIONS CHECKSDR UIEA2014102400504Proximity Sensor · faultyGEAR TILT STATUS MSG, GEAR WOULD NOT RETRACT AFTER TAKE TAKEOFF, QRH CHECKLIST ACCOMPLISHED. R & R L/B TRUCK TILT LEVER LOCK PROX SENSOR S2653 IAW AMM 32-61-12. ADJUSTED SENSOR IAW AMM 32-61-12. OPERATIONS NORMAL IAW AMM 32-61-00 & 32-31-00.SDR UIEA2014060200222Engine · power lossINADVERTENT ENCOUNTER WITH ICE CRYSTALS, NR 2 ENG ROLLED BACK. PERFORMED BORESCOPE INSPECTION OF ALL HIGH PRESS COMPRESSOR BLADE AIRFOILS OF THE NR 2 ENG IAW AMM TASK 71-00-00-200-816-G00, AWL 30-099-01 & AD 2013-24-01 PARA J I & SATISFACTORY.
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