# Service difficulty reports: N851GT A list on [N851GT](https://openairdocs.org/aircraft/N851GT.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 79 reports - [SDR UIEA2026091400877](https://openairdocs.org/sdr/UIEA2026091400877.md): Outflow Valve · faulted · Sep 14, 2026 · N851GT · Boeing 74787UF · Pressure Regulator/Outflow Valve > AFTER LEVEL OFF AT 340, SLOWLY LOST CABIN PRESSURISATION TO APPROX 10,900. BOTH OUTFLOW VALVES VERIFIED CLOSED. DESCENDED AND RETURNED TO VCP. TRANSFER TO DMI 259214 PER MEL 21-31-02A CAT C. R & R LWR FWD CARGO OVERBOARD EXHAUST VALVE IAW AMM 21-26-17-000-8 - [SDR UIEA2026082300786](https://openairdocs.org/sdr/UIEA2026082300786.md): Transceiver · inoperative · Aug 22, 2026 · N851GT · Boeing 74787UF · UHF Communications System > RIGHT HF INOPERATIVE. NO HF CAPABILITY, LT & RT UNABLE TO TRANSMIT. R & R HF ANTENNA COUPLER IAW AMM 23-11-03. R & R RT AND LT HF TRANSCIEVER IAW AMM 23-11-05/401 AND LT & RT HF SYS OPS CHECKS GOOD. - [SDR UIEA2026052600351](https://openairdocs.org/sdr/UIEA2026052600351.md): Skin · damaged · May 23, 2026 · N851GT · Boeing 74787UF · Cargo/Baggage Doors > LIGHTING STRIKE - SKIN, NOSE CARGO EXTERNAL SKIN NEAR STA 200, S-36R ~ S-39R. ACCOMPLISHED WORK SHEET NO 60306 (SRM 53-00-01-2R-9 REV 48) AND EI NO T2026A52M-969 REV 0 AND REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600352](https://openairdocs.org/sdr/UIEA2026052600352.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 2180 S-10L FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60308 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600353](https://openairdocs.org/sdr/UIEA2026052600353.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 2180 S-11L FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60309 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600354](https://openairdocs.org/sdr/UIEA2026052600354.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR BS 2360 S-7R FWD SIDE. PERFORMED REPAIR IAW W/S 60302 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600355](https://openairdocs.org/sdr/UIEA2026052600355.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 1960 S-12R FWD AND AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60310 (SRM 53-60-03-2R-4 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600356](https://openairdocs.org/sdr/UIEA2026052600356.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR BS 2180 S-10R AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60294 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600357](https://openairdocs.org/sdr/UIEA2026052600357.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR BS 2180 S-12R FWD AND AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60307 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600358](https://openairdocs.org/sdr/UIEA2026052600358.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 940 AND STA 960, S-9R. REPAIRED DAMAGE AREA IAW W/S 60297 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600359](https://openairdocs.org/sdr/UIEA2026052600359.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 980 +160 ~ 1000 S-11L. REPAIRED DAMAGE AREA IAW W/S 60298 AND SRM 53-20-03-2R-1 ALTERNATIVE 1 REV 48 AND EI #T2026A53M-972 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600360](https://openairdocs.org/sdr/UIEA2026052600360.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 920 S-11R. REPAIRED DAMAGE AREA IAW W/S #60299 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48 AND EI #T2026A53M-973 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600361](https://openairdocs.org/sdr/UIEA2026052600361.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 980+160 ~ 1000 S-11R. REPAIRED DAMAGE AREA IAW W/S 60301 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48 AND EI T2026A53M-973 REV 2. EI ATTACHED TO W/O 12388193 (064). 3. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600362](https://openairdocs.org/sdr/UIEA2026052600362.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 850 S-10L. REPAIRED DAMAGE AREA IAW W/S 60359 (SRM 53-20-03-2R-1 REV 48) AND EI T2026A53M-968 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600363](https://openairdocs.org/sdr/UIEA2026052600363.md): Stringer · cracked · May 23, 2026 · N851GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGED ON THE STRINGER NEAR STA 870 S-8L REPAIRED DAMAGE AREA IAW W/S 60356 (SRM 53-20-03-2R-1 REV 48) AND EI T2026A53M-971 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026010600004](https://openairdocs.org/sdr/UIEA2026010600004.md): Valve · defective · Jan 6, 2026 · N851GT · Boeing 74787UF · Air Distribution System > CABIN TEMP EXCESSIVE (38C) FOUND MAINT MSG 21304, FLIGHT DECK TRIM AIR VALVE DEFECTIVE. R & R F/D TRIM AIR VALVE AND OPS CHECK OK IAW AMM 21-61-10-401, AIPC 21-61-10-08 & FIM TASK 21-61-01-810-819. - [SDR UIEA2025031300281](https://openairdocs.org/sdr/UIEA2025031300281.md): Pdu · faulted · Mar 13, 2025 · N851GT · Boeing 74787UF · Trailing Edge Flap Control System > FLAPS DRIVE CAUTION MSG.(

REMOVE & REPLACE #4 PDU FEEDBACK SWITCH ASSY PER AMM 27-88-01. REMOVED AND REPLACED #4L PDU PER AMM 27-81-03 APC 27-81-03-51. OPS CHECK GOOD. NO MESSAGES OR FAULTS NOTED.

) - [SDR UIEA2025011800085](https://openairdocs.org/sdr/UIEA2025011800085.md): Outflow Valve · failed · Jan 18, 2025 · N851GT · Boeing 74787UF · Pressure Regulator/Outflow Valve > DURING CLIMB ON, THE CABIN WOULD NOT PRESSURIZE, STOPPED CLIMB AT 10,000, CAB ALT WAS 10300. DELTA P WAS 0.1 COULD NOT CONTROL THE CABIN PRESSURE IN MANUAL OR AUTO.(

REMOVED AND REPLACED R/H OUTFLOW VALVE IAW B747 AMM 21-31-01 UP TO SUBTASK 21-31-01-430-016. - [SDR UIEA2024120601168](https://openairdocs.org/sdr/UIEA2024120601168.md): Line · loose · Dec 6, 2024 · N851GT · Boeing 74787UF · Hydraulic System, Main > #1 ADP FAILED, LOSS OF HYDRAULIC FLUID. #1 EDP ON DEFERRAL PRIOR TO FLIGHT.(

R/R EDP PER AMM 29-11-05 & IPC 29-11-05-05, RETURN LINE FOUND LOOSE, LEADING TO FLUID LOSS. SCAVENGE FILTER CHECKED FOR DEBRIS, NONE FOUND. R/R RETURN MOD FILTER PER MCC REQUEST. FI - [SDR UIEA2024071800685](https://openairdocs.org/sdr/UIEA2024071800685.md): Outflow Valve · faulted · Jul 18, 2024 · N851GT · Boeing 74787UF · Pressure Regulator/Outflow Valve > AIR TURN BACK UNABLE CRUISE ALTITUDE DUE TO PRESSURIZATION(

MIA MX PERFORMED INSPECTION OF EXTERIOR AND INTERIOR OF THE A/C, DOOR SEALS, A/C MANIFOLD DUCTING, NO ISSUES FOUND. R/R E/E FAN, R/R OVBD SOV, R/R X2 RELAYS FOR FWD CGO OVBD VALVE OPEN & CLOSE, & R/ - [SDR UIEA2024041300272](https://openairdocs.org/sdr/UIEA2024041300272.md): Lamp · inoperative · Apr 24, 2024 · N851GT · Boeing 74787UF · Emergency Lighting > RH FUS EMER SLIDE LT L6690 FOUND NOT ILLUMINATED(

R/H FUS EMER SLIDE LT L6690 LAMP REPLACED AND TEST IS NORMAL AS PER AMM 33-51-00 REV 44 15 MAR 2024.

) - [SDR UIEA2024041700277](https://openairdocs.org/sdr/UIEA2024041700277.md): Lamp · inoperative · Apr 24, 2024 · N851GT · Boeing 74787UF · Emergency Lighting > EMERGENCY LIGHT ON THE TOP OF STAIRWAY FOUND INOP.(

LAMP OF EMERGENCY LIGHT ON THE TOP OF STAIRWAY REPLACED AND OPERATIONAL TEST NORMAL IAW AMM 33-51-07 REV 44, 15 MAR 2024

) - [SDR UIEA2024041700278](https://openairdocs.org/sdr/UIEA2024041700278.md): Curtain · torn · Apr 24, 2024 · N851GT · Boeing 74787UF · Cargo Compartments > AFT CARGO COMPT STA 2160 END WALL CURTAIN FOUND TORN.(

AFT CARGO COMPT STA 2160 ENDWALL CURTAIN REPAIRED AS PER RI-25-52-16836 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900279](https://openairdocs.org/sdr/UIEA2024041900279.md): Channel · cracked · Apr 24, 2024 · N851GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > RH HORIZONTAL STAB T/E ASSY CHANNEL FOUND CRACK(

BONDED NEW CHANNEL AS PER RI-55-10-16833 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900280](https://openairdocs.org/sdr/UIEA2024041900280.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #9 V/C FLAP LSA FOUND WORN(

PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900281](https://openairdocs.org/sdr/UIEA2024041900281.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #7 V/C FLAP LSA FOUND WORN(

PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900282](https://openairdocs.org/sdr/UIEA2024041900282.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #8 V/C FLAP LSA FOUND WORN(

PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900283](https://openairdocs.org/sdr/UIEA2024041900283.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #18 V/C FLAP LSA FOUND WORN(

PERFORMED REPIAR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900284](https://openairdocs.org/sdr/UIEA2024041900284.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #20 V/C FLAP LSA FOUND WORN(

PERFORMED REPAIR AT LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900285](https://openairdocs.org/sdr/UIEA2024041900285.md): Skin · worn · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #19 V/C FLAP LSA FOUND WORN(

PERFORMED REPAIR LSA WORN AREA IAW CMM 57-55-42. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900286](https://openairdocs.org/sdr/UIEA2024041900286.md): Nut · unknown · Apr 24, 2024 · N851GT · Boeing 74787UF · Wing Main, Frame Structure > REFER JOB CARD SEQ 1.725 #1 CANOE AFT FRAME MOD FIG 6 INSTALLATION AFTER ROW HAS 5EA FASTENER HOLE LOCATION CAN NOT USE BACC30AC6 DUE HOLES TOO CLOSE TO ART INTERFERENCE COLLAR(

NUTS REPLACED AS PER RI-57-50-16856 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042000302](https://openairdocs.org/sdr/UIEA2024042000302.md): Skin · eroded · Apr 24, 2024 · N851GT · Boeing 74787UF · Leading Edge Devices > #10 V/C FLAP UPR EDGE FOUND EROSION(

PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042200303](https://openairdocs.org/sdr/UIEA2024042200303.md): Beam · cracked · Apr 24, 2024 · N851GT · Boeing 74787UF · Wing Main, Frame Structure > RHW L/E ILES 560 D BEAM WEB CRACKED(

RHW L/E ILES 560 D BEAM WEB REPAIRED AS PER RI-57-41-16827 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042200304](https://openairdocs.org/sdr/UIEA2024042200304.md): Intercostal · deformed · Apr 24, 2024 · N851GT · Boeing 74787UF · Aerodynamic Fairings > FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL, P/N: 65B07241-1 BETWEEN STA 1480 +60 TO STA 1520 LBL 45. DEFORMATION DAMAGE - TEMPORARY REPAIR REFER EA-4853A0088(

FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL REPLACED AS PER SRM 51-10-02, SRM 51-40-02 AND RI-53 - [SDR P5CA2023070200034](https://openairdocs.org/sdr/P5CA2023070200034.md): Bracket · unknown · Jun 30, 2023 · N851GT · Boeing 74787UF · Fuselage Miscellaneous Structure > FOUND THE GROUND PNEUMATIC DOOR GROUND SERVICE MISSING ON WALKAROUND(

FABRICATED THE BRACKET AS PER SERVICE REQUEST 270823140 AND DWG 69B11807 AND INSTALLED BRACKET AT NEW PNEUMATIC DOOR IAW SRM 51-40-02-01

) - [SDR P5CA2023062900033](https://openairdocs.org/sdr/P5CA2023062900033.md): Bracket · unknown · Jun 29, 2023 · N851GT · Boeing 74787UF · Service Doors > ENGINE START PNEUMATIC GROUND SERVICE DOOR MISSING.(

PERFORMED TIME LIMITED REPAIR PER EA-4852A0005 PART 1 (REV 0). FOLLOW UP REPAIR DUE NEXT F/C. PLACARD INSTALLED. TRANSFER TO DMI 188348 NON-MEL DUE DATE 6/30/2023.

/

LP 1620525 M9: FABRICATED THE BR - [SDR P5CA2022032700106](https://openairdocs.org/sdr/P5CA2022032700106.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Landing Gear System > L/H BLG I/B TRUNNION SUPPORT FITTING AND LOWER CAP FOUND CORROSION(

CORROSION AREA REPAIRED AS PER SRM 53-40-90-2R-1 REPAIR 1 AND HAECO RI NO. RI-53-40-15465 REV.A

) - [SDR P5CA2022032100093](https://openairdocs.org/sdr/P5CA2022032100093.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > LHW L/E #6 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100094](https://openairdocs.org/sdr/P5CA2022032100094.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > LHW L/E #7 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100095](https://openairdocs.org/sdr/P5CA2022032100095.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > LHW L/E #8 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100096](https://openairdocs.org/sdr/P5CA2022032100096.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > LHW L/E #9 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032300097](https://openairdocs.org/sdr/P5CA2022032300097.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > R/H H-STAB STA BL 421.5 LOWER CHORD CRACKED(

LOWER CHORD CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12,FIG.201,DETAIL VII

) - [SDR P5CA2022032400098](https://openairdocs.org/sdr/P5CA2022032400098.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > #2 V/C FLAP BULLNOSE EDGE FOUND EROSION(

PERFORMED REPAIR AT ERODED AREA

) - [SDR P5CA2022032500099](https://openairdocs.org/sdr/P5CA2022032500099.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > VERTICAL FIN FWD L/E FAIRING #321B FOUND DENT MARK(

DENT AREA REPAIRED AS PER SRM 55-30-01-2R-4 REPAIR 4 FIG.201

) - [SDR P5CA2022032600100](https://openairdocs.org/sdr/P5CA2022032600100.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > LH H.STAB REAR WEB AT STA BL 391.9 ANGLE CRACKED.(

CRACK ANGLE LOCAL FABRICATED AS PER RI NO. RI-55-00-15458 REV A AND NEW ANLGE INSTALLED AS PER SRM 51-40-02.

) - [SDR P5CA2022032600101](https://openairdocs.org/sdr/P5CA2022032600101.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > R/H H.STAB BL 421.5 UPPER CHORD CRACKED.(

R/H H.STAB BL 421.5 UPPER CHORD REPLACED ACCOMPLISHED IAW SRM 51-40-02 AND SRM 51-40-05 REV 36, 20 FEB 2022

) - [SDR P5CA2022032600102](https://openairdocs.org/sdr/P5CA2022032600102.md): Web · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > R/H H.STAB, STAB BL 421.5 WEB CRACKED(

CRACK WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB INSTALLED AS PER SRM 51-40-02

) - [SDR P5CA2022032600103](https://openairdocs.org/sdr/P5CA2022032600103.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > L/H STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(

LH STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U11 WAS REPLACED AS PER RI NO. RI-55-10-15472 REV A AND INSTALLED AS PER SRM 51-40-02 REV 36, DATE 20 FEB 2022.

) - [SDR P5CA2022032600104](https://openairdocs.org/sdr/P5CA2022032600104.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Empennage Structure > RH H.STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(

RH H.STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U12 WAS REPLACED AS PER RI NO. RI-55-10-15473 REV A AND INSTALL AS PER SRM 51-40-02 REV 36. DATE 20 FEB 2022.

) - [SDR P5CA2022032700105](https://openairdocs.org/sdr/P5CA2022032700105.md): None · none · Apr 1, 2022 · N851GT · Boeing 74787UF · Wing Structure > LHW I/B T/E LWR PNL AT WS 129.86 TO 228.05 FWD SUPPORT BEAM O/B BRACKET CRACKED(

SUPPORT BEAM FITTING P/N: 115U2252-19 FASBRICATED AS PER RI NO.RI-57-00-15477 REV A AND BOEING DRAWING 115U2252-19PL

) Next page: https://openairdocs.org/aircraft/N851GT/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 = 'N851GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N851GT/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.