N857GT
Service difficulty reports · 97
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 = 'N857GT' 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 = 'N857GT' 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 P5CA2026082100029Tire · warning messageIN CRUISE FLIGHT, TIRE PRESSURE EICAS MSG. GAUGE SYNOPTIC INDICATED TIRE 14 WAS AT 180 PSI AND CONTINUED TO DROP. R & R NR 14 MWA IAW AMM 32-45-01. VERIFIED SPACER INSTALLED. OPS & LK CHKD OK.SDR P5CA2026070600024Sensor · faultedFLAPS DRIVE MSG IMMEDIATELY AFTER ROTATION BELOW 300 FT. REMOVED AND REPLACED FLAP SKEW SENSOR AND RE-SECURED CONNECTOR D25635J. OPS CHECK GOOD IAW AMM 27-51-01, AIRCRAFT OK FOR SERVICE.SDR P5CA2025080500033Stringer · crackedFOUND STRINGER CRACKED AT BS 884, S7L.. ACCOMPLISHED WORK SHEET 50507 IAW SRM 53-20-03-2R-1, REV 46 TO REPAIR DAMAGED STRINGER. CONDITION CHECKED NORMAL AND JOB COMPLETED.SDR P5CA2025080500034Stringer · crackedFOUND STRINGER CRACKED AT BS 977, S10L. REPAIRED THE STRINGER CRACK IAW W/S 50514, AND SRM 53-20-03-2R-1 REV 46. CONDITION CHECKED NORMAL AND JOB COMPLETED.SDR P5CA2025080500035Stringer · crackedFOUND STRINGER CRACKED AT BS 957, S10L. REPAIRED THE STRINGER CRACK IAW W/S 50536, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080500036Stringer · crackedFOUND STRINGER CRACKED AT BS 957, S8L. REPAIRED THE STRINGER CRACK IAW W/S 50513, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080500037Stringer · crackedFOUND STRINGER CRACKED AT BS 877, S8R. ACCOMPLISHED WORK SHEET 50502, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080500038Stringer · crackedFOUND STRINGER CRACKED AT BS 841, S7R. ACCOMPLISHED WORK SHEET 50499, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080500039Stringer · crackedFOUND STRINGER CRACKED AT BS 798, S13R. PERFORMED EI T2025A53M-1533, REV 0. ACCOMPLISHED EI T2025A53M-1533, REV 1. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080500040Stringer · crackedFOUND STRINGER CRACKED AT BS 2180-2188, S11R. REPAIR SPLICE FOR CRACKED STRINGER IAW W/S 50498, AND SRM 53-60-03-2R-3 REV 46, TR 53-154. CONDITION CHECKED NORMAL AND JOB COMPLETED.SDR P5CA2025080500041Stringer · crackedFOUND STRINGER CRACKED AT BS 922, S9L. ACCOMPLISHED WORK SHEET 50511, AND SRM 53-20-03-2R-1, REV 46, AND WORK SHEET ATTACHED TO W/O 11244309. JOB COMPLETED, AND CONDITION CHECKED NORMAL.SDR P5CA2025080600042Stringer · crackedFOUND STRINGER CRACKED AT BS 884, S9L. ACCOMPLISHED WORK SHEET 50509, AND SRM 53-20-03-2R-1, REV 46, AND WORK SHEET ATTACHED TO W/O 11244332. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600043Stringer · crackedFOUND STRINGER CRACKED AT BS 878, S9L. ACCOMPLISHED WORK SHEET 50509, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600044Stringer · crackedFOUND STRINGER CRACKED AT BS 938, S9L. ACCOMPLISHED WORK SHEET 50512, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600045Stringer · crackedFOUND STRINGER CRACKED AT BS 903, S9L. ACCOMPLISHED WORK SHEET 50510, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600046Stringer · crackedFOUND STRINGER CRACKED AT BS 914 - 917, S9L. ACCOMPLISHED WORK SHEET 50511, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600047Stringer · crackedFOUND STRINGER CRACKED AT BS 878, S10R. ACCOMPLISHED WORK SHEET 50503, AND SRM 53-20-03-2R-1, REV 46. CONDITION CHECKED NORMAL AND JOB COMPLETED.SDR P5CA2025080600048Stringer · crackedFOUND STRINGER CRACKED AT BS 876, S10L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50526, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600049Stringer · crackedFOUND STRINGER CRACKED AT BS 865, S10L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50525, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR P5CA2025080600050Stringer · crackedFOUND STRINGER CRACKED AT BS 882-888, S8L. REPAIR THE STRINGER CRACK IAW W/S 50508, AND SRM 53-20-03-2R-1 REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600051Stringer · crackedFOUND STRINGER CRACKED AT BS 894-897, S8L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50524 AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600052Stringer · crackedFOUND STRINGER CRACKED AT BS 941, S8R. ACCOMPLISHED WORK SHEET W/S 50505 IAW SRM 53-20-03-2R-1, REV 46. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR P5CA2025080600053Stringer · crackedFOUND STRINGER CRACKED AT BS 878, S7R. ACCOMPLISH WORK SHEET 50500 AND SRM 53-20-03-2R-1, REV 46. WORK SHEET ATTACHED TO W/O #11244355. NO FURTHER DEFECTS NOTED.SDR P5CA2025080600054Stringer · crackedFOUND STRINGER CRACKED AT BS 883, S7R. ACCOMPLISH WORK SHEET 50500 AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600055Stringer · crackedFOUND STRINGER CRACKED AT BS 970, S7R. REPAIRED THE STRINGER IAW WORK SHEET 50515, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600056Stringer · crackedFOUND STRINGER CRACKED AT BS 918, S10R. ACCOMPLISHED EI T2025A53M-1577, SEQUENCE A, REV 0 IAW SRM 53-20-03, REPAIR 1, REV 46. ACCOMPLISHED EI T2025A53M-1392, REV 0. ACCOMPLISHED EI #T2025A53M-1577 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600057Stringer · crackedFOUND STRINGER CRACK AT BS 958, S7L. ACCOMPLISHED EI #T2025A53M-1566, SEQUENCE A, REV 0. ACCOMPLISHED EI T2025A53M-1566 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600058Stringer · crackedFOUND STRINGER CRACKED AT BS 963, S7L. ACCOMPLISHED EI T2025A53M-1566, SEQUENCE A, REV 1, AND EI ATTACHED TO W/O 11234472. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600059Stringer · crackedFOUND STRINGER CRACK AT STA 957, S-7R. ACCOMPLISHED EI T2025A53M-1569, SEQUENCE A, REV 0, IAW SRM 53-20-03 REPAIR 1, REV 46. ACCOMPLISHED EI #T2025A53M-1569, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600060Stringer · crackedFOUND STRINGER CRACK AT BS 944, S7R. ACCOMPLISHED EI T2025A53M-1569, SEQUENCE A, REV 1, AND EI ATTACHED TO W/O #11244350. 2. JOB COMPLETED AND CONDITION CHECK NORMALSDR P5CA2025080600061Stringer · crackedFOUND STRINGER CRACKED AT BS 763, S8L. REPAIR THE DAMAGE AREA IAW EI T2025A53M-1575, REV 0, AND SRM 53-20-03, REPAIR 1, REV 46. ACCOMPLISHED EI T2025A53M-1575, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR P5CA2025080600062Skin · dentedPERMANENT REPAIR OF SCRATCH AND DENT ON FUSELAGE SECTION 46 SKIN COMMON TO LAP AND BUTT SPLICE AT STA 1740 AND S-46L REQUIRED PER PART 3 OF EO 4853A132 BEFORE 10000 FC. ACCOMPLISHED EI #T2025A53M-1615, REV 1 FOR UPGRADE FUSELAGE SKIN TIME-LIMITED REPAIR. ASDR P5CA2025080600063Battery · no testFOUND M5168 EMERGENCY POWER COULD NOT STAY MORE THAN 15 MINS IAW AMM 33-51-04-900-803, REV 47. REPLACED POWER SUPPLY BATTERY (M5168) AT UPPER DECK, THE CONDITION CHECK NORMAL IAW AMM 33-51-04-900-803 REV 47. PERFORMED INSTALLATION TEST OF (M5168) POWER SUPSDR P5CA2025080600064Battery Pack · no testFOUND M5170 EMERGENCY POWER FUNCTION. IAW AMM 33-51-04-000-803 & 33-51-04-900-803 & 33-51-04-400-803 REV 48. REPLACED BATTERY ASSY (M5170) AT UPPER DECK AREA, THE CONDITION CHECK NORMAL IAW AMM 33-51-04-900-803 & 33-51-04-400-803 REV 48. PERFORMED INSTALLATSDR P5CA2025010200001Panel · puncturedFUSELAGE - SEC 46 LOWER AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED NEAR STA 1540 TO 1560.(<P>FUSELAGE - SEC 46 STA 1540-1560 RBL 45" TO RBL 55" LOWER AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED AREA REPAIRED IAW RI-53-12-17630 REV.A </P>)SDR P5CA2024121600050Pcb · faultedMASTER WARNING LIGHTS (RED) AND BELL WERE ACTIVATING EVERY 90 SECONDS WITH NO EICAS OR OTHER RED LIGHTS ILLUMINATING.(<P>REMOVED AND REPLACED MASTER MONITOR A & MAWEA PCC IAW B747 AMM 31-51-02. OPS CHECK GOOD. PART EFFECTIVITY VERIFIED PER IPC 31-51-02-01.</P>SDR P5CA2024093000047Seat · malfunctionedCAPTAIN SEAT, UNABLE TO LOCK IN ANY FWD/AFT DETENT (SEE 1857990)(<P>CAPT SEAT FWD & AFT MANUAL CONTROL CABLE BROKEN. R/R CAPT SEAT ASSY & OPS TEST GOOD IAW AMM 25-11-01/401 & IPC 25-11-01-10</P>)SDR P5CA2024032300006Actuator · brokenBODY GEAR STEERING EICAS MESSAGE. RTO AT LOW SPEED(<P>PERFORMED DVI OF R/H BODY GEAR AND FOUND R/H BODY GEAR, R/H ACTUATOR BROKEN. PERFORMED CONDITIONAL INSPECTION PER AMM 05-41-07. NO FURTHER DAMAGE NOTED. </P>)SDR P5CA2023072200037Unknown · unknownREFER EO 1957A593 PART 1 SB 747-57-2369 REV 1 NO.1 FLAP TRACK ACTUATOR FRAME EXISTING REPAIR MODIFICATION(<P>ACTUATOR FRAME MODIFICATION CARRIED OUT AS PER ATLAS AIR EO 1957A593 REV 3 PART 1 AND REPAIRED AS PER RI NO: RI-57-50-16381 REV A</P>)SDR P5CA2023072200038Unknown · unknownLHW NO. 1E VC FLAP FWD BULKHEAD FOUND DEFORMED ( FWD L/E D BEAM AFT B/HEAD WEB STIFFENER DEFORMED )(<P>B/HEAD STIFFENER DEFORM AREA REPAIRED AS PER RI NO. RI-57-41-16375 REV A</P>)SDR P5CA2023072200039Unknown · unknownRHW FIXED L/E D BEAM AFT B/HEAD FOUND BROKEN(<P>B/HEAD BROKEN AREA REPAIRED AS PER RI NO : RI-57-41-16382 REV A</P>)SDR P5CA2023072200040Stiffener · unknownRHW WING FRONT SPAR ILES 487 ( AFT OF 14 K / FLAP ) STIFFENER FOUND CRACK(<P>CRACK STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( REV 40 DATE 2 JUN 2023 )</P>)SDR P5CA2023072200041Stiffener · unknownLHW L/E FRONT SPAR ILES 470 ( AFT OF 12 K/FLAP ) STIFFENER LWR FOUND BROKEN.(<P>BROKEN STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023 )</SDR P5CA2023072200042Unknown · unknownLHW L/E CAVITY ILES 540 D BEAM AFT BULKHEAD FOUND CRACK(<P>B/HEAD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-16383 REV A</P>)SDR P5CA2023072200043Unknown · unknownLHW WING TIP I/B UPPER AFT EDGE STRAP FOUND BURN MARK(<P>BURN MARK AREA REPAIRED AS PER RI NO: RI-57-30-16423 REV A</P>)SDR P5CA2023072200044Unknown · unknownLHW I/B L/E ILES 410 'V' SUPPORT ROD UPPER ATT. BRACKET FOUND ELONGATED ( NO.5 AND 6 ).(<P>NO.6 BRACE UPPER (2EA) FASTENER HOLES AND UPPER ATT BRACKET O/B (2EA) FASTENER HOLES REPAIRED AS PER RI NO : RI-57-41-16380 REV A</P>)SDR P5CA2023072200045Unknown · unknownLHW FIXED L/E OLES 530 'D' BEAM FOUND CRACK(<P>D BEAM B/HEAD CRACK AREA REPAIRED AS PER RI NO: RI-57-41-16369 REV A</P>)SDR P5CA2023072200046Unknown · unknownLHW L/E D BEAM FWD EXTERNAL SKIN FOUND DENT ( AFT OF NO.6 V/C FLAP )(<P>SKIN DENT ARAE REPAIRED AS PER RI NO : RI-57-41-16394 REV A</P>)SDR P5CA2023072200047Support Web · unknownLH HORI STAB ACCESS PANEL 334QB O/B SUPPORT WED FOUND CRACK(<P>SUPPORT WEB REPLACEMENT AS PER SRM 51-10-02, NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW WEB INSTALLED AS PER SRM 51-40-02 ( SRM REV 40, DATE 20 JUN 2023 )</P>)SDR P5CA2023072200048Unknown · unknownLH HORI STAB ACCESS PANEL 334QB O/B SUPPORT RIB LWR CHORD FOUND CRACK(<P>LOWER CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201 REV 40 DATE 20 JUN 2023</P>)
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