1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. 2. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-033 REV 1. 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: 148U2 - [SDR P5CA2026012000002](https://openairdocs.org/sdr/P5CA2026012000002.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-8R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50870 (SRM 53-80-03-2R-2 REV: 47) JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000003](https://openairdocs.org/sdr/P5CA2026012000003.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50869 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000004](https://openairdocs.org/sdr/P5CA2026012000004.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-6R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50868 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000005](https://openairdocs.org/sdr/P5CA2026012000005.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-5L, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50867 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000006](https://openairdocs.org/sdr/P5CA2026012000006.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-2L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50876 (SRM 53-60-03-2R-8 REV: 47) AND EI T2026A53M-087 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000007](https://openairdocs.org/sdr/P5CA2026012000007.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2360. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 50872 (SRM 53-80-03-2R-3 REV 47). INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 47 AND DWG NO: - [SDR P5CA2026012000008](https://openairdocs.org/sdr/P5CA2026012000008.md): String · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S 50877 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR P5CA2026012000009](https://openairdocs.org/sdr/P5CA2026012000009.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-7L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50878 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORMAL.) - [SDR P5CA2026012000010](https://openairdocs.org/sdr/P5CA2026012000010.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-9L, AT STA 930. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 60010 (SRM 53-20-03-2R-1 REV 47) AND EI NO: T2026A53M-050 REV 1. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 - [SDR P5CA2026012000011](https://openairdocs.org/sdr/P5CA2026012000011.md): Stringer Splice · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER AND STRINGER SPLICES S-10R, AT FWD AND FWD SIDE OF STA 2180. REPAIR DAMAGE AREA IAW W/S NO: 50871 (SRM 53-60-03-2R-3 REV: 47) AND EI NO: T2026A53M-076 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR P5CA2026012000012](https://openairdocs.org/sdr/P5CA2026012000012.md): Stringer · cracked · Jan 21, 2026 · N855GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-3L, AT AFT SIDE OF STA 2360.(1. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-034 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
) - [SDR P5CA2026012000013](https://openairdocs.org/sdr/P5CA2026012000013.md): Battery Pack · no test · Jan 21, 2026 · N855GT · Boeing 74787UF · Emergency Lighting > FOUND EXTERIOR EMER LT (L6690) INOP. PERFORM WIRING CONTINUITY CHECK AND SYSTEM TROUBLESHOOTING IAW WDM 33-51-72 REV 35, FOUND M5168 BATTERY FUNCTION FAILED. PERFORM BATTERY REPLACEMENT AT M5168 IAW AMM 33-51-04-900-803 REV 49. CONDITION CHECK NORMAL AND PER - [SDR P5CA2025041600013](https://openairdocs.org/sdr/P5CA2025041600013.md): Shear Tie · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Fuselage Internal Mounting Structure > FUSELAGE SECTION 46 - FUSELAGE SKIN (P/N: 146U3867-5) - PUNCTURE BETWEEN STA 2000 AND S38L TO S39L - CATEGORY B REPAIR.(SHEAR TIE REPLACED AS PER SRM 51-10-02. NEW SHEAR TIE HOLES TRANSFERRED AS PER SRM 51-40-05. NEW SHEAR TIE INSTALLED AS PER SRM 51-40-02. - [SDR P5CA2025041900014](https://openairdocs.org/sdr/P5CA2025041900014.md): Web · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > EMP - RH HORIZONTAL STAB TIP FAIRING I/B CLOSURE WEB, FOUND CRACK.(
CRACK - WEB REPLACED AS PER SRM 51-10-01. NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042100015](https://openairdocs.org/sdr/P5CA2025042100015.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #18 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED
) - [SDR P5CA2025042100016](https://openairdocs.org/sdr/P5CA2025042100016.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #19 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042100017](https://openairdocs.org/sdr/P5CA2025042100017.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #20 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042100018](https://openairdocs.org/sdr/P5CA2025042100018.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #7 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042100019](https://openairdocs.org/sdr/P5CA2025042100019.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #8 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED
) - [SDR P5CA2025042100020](https://openairdocs.org/sdr/P5CA2025042100020.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #9 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED
) - [SDR P5CA2025042200021](https://openairdocs.org/sdr/P5CA2025042200021.md): Beam · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Leading Edge Devices > LHW NO.11 K-FLAP AT WS 569 D-BEAM LWR ATT BOLT AREA, FOUND CRACK.(CRACK AREA REPAIRED AS PER RI NO: RI-57-41-17558 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042200022](https://openairdocs.org/sdr/P5CA2025042200022.md): Channel · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > LH HORIZONTAL STAB TIP T/E FAIRING FWD U CHANNEL CRACK.(U CHANNEL REPLACED AS PER RI NO: RI-55-10-17562 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042300023](https://openairdocs.org/sdr/P5CA2025042300023.md): Seat Track · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach Fittings > M/D STA 1510, 1530, 1550 LBL 11 SEAT TRACK SLOT HOLE ELONGATED.(SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-9 REPAIR 9 FIG 201 AND RI NO: RI-53-65-17570 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042300024](https://openairdocs.org/sdr/P5CA2025042300024.md): Web · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > EMP - RH HORIZONTAL STAB TIP FAIRING CLOSURE WEB LWR CHORD CRACK.(LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042300025](https://openairdocs.org/sdr/P5CA2025042300025.md): Rib · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Horizontal Stabilizer, Spar/Rib > EMP - RH HORIZONTAL STAB TIP FAIRING INTERNAL AREA MOST AFT RIB, FOUND CRACK.(RIB REPLACED AS PER SRM 51-10-02. NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05. NEW RIB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED
) - [SDR P5CA2025042300026](https://openairdocs.org/sdr/P5CA2025042300026.md): Beam · cracked · Apr 30, 2025 · N855GT · Boeing 74787UF · Wing Main, Frame Structure > RHW I/B L/E D-BEAM AT I/B PDU AREA O/B FOUND CRACK ILES 520.(CRACK AREA REPAIRED AS PER RI-57-41-17559 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042300027](https://openairdocs.org/sdr/P5CA2025042300027.md): Support Beam · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Wing Main, Frame Structure > RHW ILE 450 I/B SUPPORT BEAM UPPER FTG FOUND HOLE ELONGATED.(SUPPORT BEAM REPAIRED AS PER SRM 57-41-09-2R-2 REPAIR 2 FIG 203 DETAIL IV AND RI-57-41-17586 REV A. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2025042300028](https://openairdocs.org/sdr/P5CA2025042300028.md): Skin · damaged · Apr 30, 2025 · N855GT · Boeing 74787UF · Trailing Edge Flaps > #21 V/C FLAP LSA LAYER DAMAGED.(PERFORMED REPAIR AT LSA LAYER DAMAGED AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.
) - [SDR P5CA2024110800048](https://openairdocs.org/sdr/P5CA2024110800048.md): Pcb · failed · Nov 8, 2024 · N855GT · Boeing 74787UF · Instrument System Wiring > REJECTED TAKE OFF @ 110 KNOTS MASTER WARING ON EICAS.(REMOVED & REPLACED MAWEA PRINTED CIRCUIT CARD (MASTER MONITORS) AMM 31-51-02/401, HIGH ENERGEY STOP INSPECTION C/W IAW AMM 05-51-10-202-001
) - [SDR P5CA2024072100015](https://openairdocs.org/sdr/P5CA2024072100015.md): Warning Message · false activation · Jul 21, 2024 · N855GT · Boeing 74787UF · Drag Control System > LOW AIRSPEED REJECT DUE TO "CONFIG SPOILER" AT 40 KTS(CMC SHOWED NO EXISTING FAULT. PERFORMED SPOILER TEST AND T/O CONFIG GND TEST, TEST PASSED. NO MAINT MSG IAW 27-61-00/501 AND 31-52-00/501. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER AMM 05-51-10.
) - [SDR P5CA2024061500014](https://openairdocs.org/sdr/P5CA2024061500014.md): Actuator · faulted · Jun 15, 2024 · N855GT · Boeing 74787UF · Drag Control System > SPEED BRAKE HANDLE POPPED UP DURING TAKEOFF ROLL. LOW SPEED. TAKEOFF CONFIG WARNING APPEARED. AUTOSPOILER SYSTEM DEACTIVATED. R & R ACTUATOR IAW AMM 27-62-00, OPS CHECKED GOOD. - [SDR P5CA2023052000027](https://openairdocs.org/sdr/P5CA2023052000027.md): Switch · unknown · May 20, 2023 · N855GT · Boeing 74787UF · Drag Control System > RTO AT APPROXIMATELY 140 KTS DUE TO "CONFIG SPOILERS" WARNING MSG AND SIREN. GROSS T/O WT 442.0(PERFORMED HIGH ENERGY STOP INSPECTION IAW B747 AMM 05-51-10, NO DEFECTS NOTED. SPEEDBRAKE HANDLE SWITCH REPLACED IAW AMM 27-62-10, OPS CHECK GOOD.
) - [SDR P5CA2023041300008](https://openairdocs.org/sdr/P5CA2023041300008.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > RH WING NO.21 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42
) - [SDR P5CA2023041300009](https://openairdocs.org/sdr/P5CA2023041300009.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > RH WING NO.19 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42
) - [SDR P5CA2023041300010](https://openairdocs.org/sdr/P5CA2023041300010.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > RH WING NO.20 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42
) - [SDR P5CA2023041700011](https://openairdocs.org/sdr/P5CA2023041700011.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > SB 747-57-2369, NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(SB 747-57-2369, NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16190 REV A SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(
SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION AREA ACCOMPLISHED IAW RI-57-50-16189 REV.A
) - [SDR P5CA2023041800013](https://openairdocs.org/sdr/P5CA2023041800013.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Fuselage Structure (General) > APU COMPARTMENT LH STA 2664.19 FRAME FOUND CRACKED (AT ELECTRICAL CABLE ATT BRACKET AREA).(APU COMPARTMENT LH STA 2664.19 FRAME WL 305 CRACK AREA REPAIRED IAW RI-53-82-16186 REV.A.
) - [SDR P5CA2023041800014](https://openairdocs.org/sdr/P5CA2023041800014.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Doors > LHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 FOUND WORN.(LHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 WORN AREA TIME-LIMIT REPAIRED IAW RI-52-00-16187 REV.A.
) - [SDR P5CA2023041900015](https://openairdocs.org/sdr/P5CA2023041900015.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > L/H WING I/B L/E CAVITY NO.7 V LINK (COUNT FROM I/B) UPPER BRACKET FOUND ELONGATED.(LHW ILES 442.84 RIB SUPPORT BEAM ATTACHMENT FLANGE FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-57-00-16173 REV.A.
) - [SDR P5CA2023042300017](https://openairdocs.org/sdr/P5CA2023042300017.md): Rod · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > RHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED.(RHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16197 REV.A
) - [SDR P5CA2023042300018](https://openairdocs.org/sdr/P5CA2023042300018.md): Rod · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED(LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49-16199 REV A
) - [SDR P5CA2023042300019](https://openairdocs.org/sdr/P5CA2023042300019.md): Rod · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FOUND ELONGATED.(LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FABRICATED AND REPLACED IAW RI-52-49-16198 REV.A
) - [SDR P5CA2023042400020](https://openairdocs.org/sdr/P5CA2023042400020.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Wing Structure > RH WING NO.18 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42
) - [SDR P5CA2023042400021](https://openairdocs.org/sdr/P5CA2023042400021.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Empennage Structure > RH HORI. STAB. TIP FAIRING AFT WEDGEÂ U CHANNEL FOUND CRACK(U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16183 REV.A
) - [SDR P5CA2023042400022](https://openairdocs.org/sdr/P5CA2023042400022.md): Unknown · unknown · Apr 27, 2023 · N855GT · Boeing 74787UF · Empennage Structure > LH HORI. STAB. TIP FAIRING AFT WEDGE U CHANNEL FOUND CRACK(U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16182 REV.A
) - [SDR P5CA2023032600006](https://openairdocs.org/sdr/P5CA2023032600006.md): Unknown · unknown · Mar 26, 2023 · N855GT · Boeing 74787UF · Fuselage Main, Attach Fittings > LOGPAGE 1669079 ITEM 6, AIRCRAFT WAS STRUCK BY A CARGO CONTAINER @ APPROX STATION STRINGER 44 AFT OF CARGO DOOR(LOGPAGE 1669079 M6: EVALUATING DAMAGE AT STA 2100 TO STA 2120 STR 44 AFT OF BULKHEAD CARGO DOOR; REMOVED "BKND-OUT" GOUGE AT FUSELAGE AND ELEVATE - [SDR P5CA2022051200111](https://openairdocs.org/sdr/P5CA2022051200111.md): Detector · inoperative · May 12, 2022 · N855GT · Boeing 74787UF · Smoke Detection > MAIN CARGO SMOKE DETECTOR MID 11 INOP(PLACED ON MDR 165471 IAW MEL 26-14-01-04A, CAT C.REMOVED AND REPLACED MAIN DECK MID SMOKE DETECTOR #11 IAW AMM 26-14-01/401. OPS CHECK NORMAL. THIS CLEARS MDDR 165471.) Next page: https://openairdocs.org/aircraft/N855GT/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N855GT/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.