N852GT
Service difficulty reports · 105
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 = 'N852GT' 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 = 'N852GT' 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 UIEA2026101800991Outflow Valve · faultedCRZ FLT FL 380: CABIN ALT WARNING AT 10,800 FT OBSERVED. ELEC QRH C/W. EMERGENCY DESCENT PERFORMED WITH O2 MASKS ON.(<P>REMOVED AND REPLACED LWR FWD CARGO OVERBOARD VALVE PER AMM 21-26-17/401. TEST PASSED. PERFORMED CABIN PRESSURE LEAKAGE TEST PER AMM 05-51-08SDR UIEA2026092100890Actuator · no testRIGHT WING LANDING GEAR ALTN ELEC MOTOR TEST FAILED. REMOVED RT WING LANDING GEAR ACTUATOR MOTOR IAW AMM 32-36-02-004-001 REV 51. 2. INSTALLED RH WING LANDING GEAR ACTUATOR MOTOR IAW AMM 32-36-01-404-009 REV 51 STEP 3 A TO E.(1)(E) 2. 3. WING RH ALTERNATE TESSDR UIEA2026092100891Structure · crackedFOUND R/H OUTBD ELEVATOR UPPER CHORD CRACK AT ELEV STA 2818. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49 AND DWG 65B05731 SHEET 1 REV E, SHEET 2 REV E, SDR UIEA2026092100892Fairing · crackedFOUND R/H OUTBD ELEVATOR UPPER FAIRING PANEL CRACK. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49, DWG 65B05786 SHEET 2 REVSDR UIEA2026092100893Fairing · crackedFOUND R/H OUTBD ELEVATOR INBD UPPER FAIRING PANEL CRACK.(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0 G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FASTENER IAW SRM 51-40-02-0G-0 REV 49, DWG 65B0578SDR UIEA2026092100894Stiffener · crackedCRACK - FOUND R/H OUTBD ELEVATOR STIFFENER CRACK AT ELEV STA 260.98.(<P>1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV SDR UIEA2026092100895Web · crackedFOUND R/H OUTBD ELEVATOR WEB CRACKED AT ELEV STA 281.8.(<P>1. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 2. JOB COMPLETED & CONDITION CHK OK.</P>)SDR UIEA2026092100896Support · crackedRT OTBD ELEVATOR SUPPORT CRACK AT ELEV STA 285. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO W/O 12882275. 3. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHEESDR UIEA2026092100897Support · crackedFOUND RT OUTBD ELEVATOR SUPPORT CRACK AT ELEV STA 277. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. FABRICATED PART IAW EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. INSTALLED FABRICATED PART IAW SRM 51-40-02-0G-0 REV 49 AND DWG 183U3400 SHESDR UIEA2026092100898Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 2360, S-7L FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60689, SRM 53-60-03-2R-8 REV 49 AND EI T2026A53M-1996 REV 0. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100899Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 880, S-8L AFT SIDE. REPAIRED CRACK AREA IAW WS 60691, SRM 53-20-03-2R-1 REV 49 AND EI T2026A53M-1988 REV 0. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100900Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 870, S-7R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60704, SRM 53-20-03-2R-1 REV 49 AND EI T2026A53M-1844 REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100901Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-20R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60683 & SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100902Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-5L FWD SIDE. ACCOMPLISHED EI T2026A53M-1841 REV 2. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100903Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-21R FWD SIDE. ACCOMPLISHED IAW WS 60684 AND SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100904Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2360, S-7R FWD SIDE. REPAIRED DAMAGED AREA IAW WS 60690 AND SRM 53-60-03-2R-8 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100905Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR STA 2180, S-11R AFT SIDE. REPAIRED DAMAGED AREA IAW WS 60686 & SRM 53-60-03-2R-3 REV 49. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026092100906Stringer · crackedCRACK DAMAGE ON THE STRINGER NEAR BS 2180, S-10R AFT SIDE. REPAIRED DAMAGED AREA IAW WS 60687 & SRM 53-60-03-2R-3 REV 49. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR UIEA2026032600107Skin · damagedLEFT HORIZONTAL STAB L/E UPPER SKIN DAMAGE(<P>PERFORMED CAT B REPAIR PER EO 4855A028. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2025021900152Structure · damagedTE RUDDER DAMAGE.(<P>REPAIRED IAW SRM 51-70-05 AND EA 1955A028. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024111501093Ram Air Turb · activatedRAT BUTTON INADVERTANTLY DEPRESSED(<P>RAM AIR TURBINE DEPLOYED AND OPERATED NORMALLY. RESTOWED RAT AS PER AMM TASK 29-21-00-960-802, ALL FUNCTIONS NORMAL</P>)SDR UIEA2024083000879Seat Track · corrodedM/D STA 1835-1852 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P><SPAN>M/D STA 1835-1852 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE SDR UIEA2024083000878Seat Track · corrodedM/D - STA 1815-1835 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P><SPAN>M/D STA 1815-1835 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGSDR UIEA2024083000877Seat Track · corrodedM/D STA 1795-1815 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P>M/D STA 1795-1815 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG SDR UIEA2024083000876Structure · tornLHW #7 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000875Structure · tornLHW #8 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000874Structure · tornLHW #9 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000873Structure · tornRHW #18 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000872Structure · tornRHW #19 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000871Structure · tornRHW #20 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000870Structure · tornRHW #21 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000869Panel · damagedLHW I/B MAIN FLAP MOST O/B SEAL PAN PANEL SCREW HOLE FOUND ELONGATED.(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-05 REPAIR 7. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000868Channel · crackedR/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17038 REV.A .NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000867Channel · crackedL/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(<P>PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17039 REV.A .NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024083000866Beam · crackedRHW L/E - ILES 567 D BEAM WEB CRACKED.(<P><SPAN>RHW L/E - ILES 567 D BEAM WEB REPAIRED IAW RI-57-41-17036 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000865Skin · damagedRHW - L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM AREA AS MARKED.(<P>RHW L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM SKIN PANEL CLOSE UP AS PER RI-57-41-17056 REV.A AND SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024083000864Stringer · crackedAFT OF STA 2598 BULKHEAD, S-42R STRINGER FOUND CRACKED.(<P><SPAN>AFT OF STA 2598 BULKHEAD, S-42R STRINGER REPAIRED IAW RI-53-80-17040 REV.A. NO FURTHER DEFECTS FOUND.</SPAN></P>)SDR UIEA2024083000863Beam · crackedLHW L/E - ILES 567 D-BEAM WEB CRACKED.(<P><SPAN>LHW L/E - ILES 567 D-BEAM WEB REPAIRED IAW RI-57-41-17037 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000862Stringer · crackedAFT OF 2598 BULKHEAD, S-4R STRINGER CRACKED.(<P><SPAN>AFT OF 2598 BULKHEAD, S-4R STRINGER REPAIRED IAW RI-53-80-17041 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024083000861Support Rib · brokenRHW #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN.(<P><SPAN>RH #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN FABRICATED IAW RI-57-00-17048 REV.A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.<SDR UIEA2024083000860Support Channel · crackedLHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA FOUND CRACKED.(<P>LHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA REPAIRED IAW RI-57-00-17045 REV A . NO FURTHER DEFECTS NOTED.</P>)SDR P5CA2022071900149Flap · peelingRH W #20 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000150Flap · peelingRH W - #21 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000151Flap · peelingRH W - #19 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000152Flap · peelingRH W - #18 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000153Flap · peelingLH W - #10 VC-FLAP SURFACE LSA FOUND PEELING OFF(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR7)SDR P5CA2022072000154Flap · peelingLH W - #9 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000155Flap · peelingLHW - #8 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072000156Flap · peelingLH W - #7 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)SDR P5CA2022072100157Skin · delaminatedLH W - O/B T/E FLAP AFT EDGE AREA FOUND DELAMINATION ON UPPER SKIN(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR1)
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