# Service difficulty reports: N858GT

A list on [N858GT](https://openairdocs.org/aircraft/N858GT.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 · 94 reports

- [SDR P5CA2026042800022](https://openairdocs.org/sdr/P5CA2026042800022.md): Switch · faulted · Apr 28, 2026 · N858GT · Boeing 74787UF · Drag Control System
  > REJECT AT 62 KTS FOR CONFIG WARNING 421.6 KG. SPEED BRAKE ARMED EICAS AND COULD NOT BE RESET AFTER REJECT. VERIFIED INTERNAL SHORT IN SPEED BRAKE ARM SWITCH IAW WDM 32-41-31 & AMM 20-11-00. R & R SPEED BRK ARM SWITCH IAW AMM 27-62-10. OPS CHECK NORMAL. THIS
- [SDR P5CA2026041800019](https://openairdocs.org/sdr/P5CA2026041800019.md): Tire · leaking · Apr 18, 2026 · N858GT · Boeing 74787UF · Tire
  > #8 TIRE PRESSURE ADVISORY MESSAGE - TIRE PRESSURE DECREASING.(<P>FOUND #8 MAIN TIRE PRESSURE LOW. REMOVED AND REPLACED #8 MAIN WHEEL ASSY PER AMM 32-45-01. ALSO, REPLACED #7 MAIN WHEEL ASSY PER AMM 32-45-01. OPS & LK CHK OK</P>)
- [SDR P5CA2025102200094](https://openairdocs.org/sdr/P5CA2025102200094.md): Power Supply · inoperative · Oct 22, 2025 · N858GT · Boeing 74787UF · Landing Gear Position and Warning
  > MULTIPLE GEAR MESSAGES INCLUDING GEAR MONITOR, GEAR DISAGREE, AND GEAR DOOR AND GEAR WOULD NOT RETRACT. R & R PSEU & PERFORMED CMC GND TEST & ZONAL INSPECTION OF NOSE LANDING GEAR & NOSE LANDING GEAR DOOR IAW AMM 32-09-03/401 & AIPC 32-61-01-01, OPS CHK GOOD
- [SDR P5CA2025101800093](https://openairdocs.org/sdr/P5CA2025101800093.md): Outflow Valve · faulted · Oct 18, 2025 · N858GT · Boeing 74787UF · Pressure Regulator/Outflow Valve
  > AT FLT 310, CABIN PRESSURE BECAME UNCONTROLLABLE. OUTFLOW VALVES WERE INDICATING FULLY CLOSED. CABIN ALTITUDE WAS CLIMBING 200 FPM.(<P>COMPLETED THE FOLLOWING CHECKS PER BOEING SR: CABIN SYSTEM CONTROL PRESSURE TEST AMM TASK 21-31-00-735-011 AND EXCESSIVE CABI
- [SDR P5CA2025100300066](https://openairdocs.org/sdr/P5CA2025100300066.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-8R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50668 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300067](https://openairdocs.org/sdr/P5CA2025100300067.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 980+15, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50670 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300068](https://openairdocs.org/sdr/P5CA2025100300068.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 882, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300069](https://openairdocs.org/sdr/P5CA2025100300069.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 892, S-8L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50659 ATTACH WITH T/C: 11454336. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300070](https://openairdocs.org/sdr/P5CA2025100300070.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300071](https://openairdocs.org/sdr/P5CA2025100300071.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 866, S-10R.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50669 ATTACH WITH T/C: 11454311 (098) 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300072](https://openairdocs.org/sdr/P5CA2025100300072.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 840, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300073](https://openairdocs.org/sdr/P5CA2025100300073.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER CRACK ON S-11L STA 885. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300074](https://openairdocs.org/sdr/P5CA2025100300074.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-11L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50664 ATTACHING WITH THE T/C 11454296. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300075](https://openairdocs.org/sdr/P5CA2025100300075.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 1660, S-10R.(<P>1. ACCOMPLISHED EI NO. T2025A53M-1965 REV 1. 2. ACCOMPLISHED EI NO. T2025A53M-1965 REV 2. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
- [SDR P5CA2025100300076](https://openairdocs.org/sdr/P5CA2025100300076.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880 S-10L.(<P>1. REPAIRED THE STRINGER IAW W/S NO. 50671 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300077](https://openairdocs.org/sdr/P5CA2025100300077.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 780 S-10L.(<P>1. PERFORMED EI NO. T2025A53M-1973 REV 1 SEQUENCE A & B. 2. ACCOMPLISHED EI NO. T2025A53M-1973 REV 2 & T2025A53M-1909 REV 1. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300078](https://openairdocs.org/sdr/P5CA2025100300078.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 760 S-8L.(<P>1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. PERFORM EI NO. T2025A53M-1990 REV 1 SEQUENCE B. 3. INSTALL AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46 AND DWG NO. 142U3625 SH 13 R
- [SDR P5CA2025100300079](https://openairdocs.org/sdr/P5CA2025100300079.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK BETWEEN STA 2177 AND STA 2185 S-8R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50672 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300080](https://openairdocs.org/sdr/P5CA2025100300080.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER CRACK FRAME FWD SIDE BETWEEN STA 1957 AND STA 1966 S-9R.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50674 AND SRM 53-60-03-2R-4 REV 46/ TR: 53-155. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300081](https://openairdocs.org/sdr/P5CA2025100300081.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 2180, S-11R.(<P>1. PERFORMED STRINGER REPAIR IAW W/S NO. 50658 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300082](https://openairdocs.org/sdr/P5CA2025100300082.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-6R.(<P>1. REMOVED FASTERNERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW W/S NO. 50660 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300083](https://openairdocs.org/sdr/P5CA2025100300083.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-8L.(<P>1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW SRM 51-40-02-0G-0 REV 46 & W/S NO. 50661 AND SRM 53-80-03-2R-2 REV 46/ TR:53-152. 3. CONDITION CHECK NORMAL AND JOB COMPLETE
- [SDR P5CA2025100300084](https://openairdocs.org/sdr/P5CA2025100300084.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER CRACK BETWEEN STA 2177 AND STA 2185 S-10R.(<P>1. PERFORM STRINGER REPAIR IAW W/S NO. 50673 AND SRM 53-60-03-2R-3 REV 46/ TR:53-154. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300085](https://openairdocs.org/sdr/P5CA2025100300085.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > FOUND CROWN STRINGER HAVE CRACK AT STA 920, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300086](https://openairdocs.org/sdr/P5CA2025100300086.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > FOUND CROWN STRINGER HAVE CRACK AT STA 905, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50666 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50666 ATTACH WITH T/C:11454301 (095). 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300087](https://openairdocs.org/sdr/P5CA2025100300087.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND FUSELAGE CROWN STRINGER HAVE CRACK AT STA 780, S-12R.(<P>1. REPAIR STRINGER AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300088](https://openairdocs.org/sdr/P5CA2025100300088.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 793, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300089](https://openairdocs.org/sdr/P5CA2025100300089.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 746, S-12R.(<P>1. REPAIR STRINGER CRACK AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. W/S NO. 50663 ATTACH WITH T/C:11454292. 3. JOB COMPLETED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2025100300090](https://openairdocs.org/sdr/P5CA2025100300090.md): Stringer · cracked · Oct 3, 2025 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-9L.(<P>1. REPAIR THE STRINGER IAW W/S NO. 50667 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)
- [SDR P5CA2025100300091](https://openairdocs.org/sdr/P5CA2025100300091.md): Actuator · malfunctioned · Oct 3, 2025 · N858GT · Boeing 74787UF · Landing Gear Actuator
  > FOUND RH WLG ALTERNATE EXTENSION ACTUATOR FUNCTION ABNORMAL.(<P>1. REPLACED RH WLG ALTERNATE EXTENSION ACTUATOR IAW AMM 32-36-01-004-001 REV 48A AND AMM 32-36-01-404-009 REV 48A. 2. PERFORMED R/H WLG ALTERNATE EXTENSION TEST IAW AMM 32-36-00-705-009 REV 48A, T
- [SDR P5CA2025100300092](https://openairdocs.org/sdr/P5CA2025100300092.md): Power Supply · no test · Oct 3, 2025 · N858GT · Boeing 74787UF · Emergency Lighting
  > FOUND EMERGENCY LIGHT BATTERY (M5169) FUNCTION FAIL AND CAN NOT RE-CHARGE.(<P>REPLACED POWER SUPPLY ASSY AND PERFORM POWER SUPPLY INSTALLATION TEST IAW AMM 33-51-04-000-803, AMM 33-51-04-400-803 AND AMM 33-51-04-900-803 REV 48A. THE RESULT WAS SATISFACTORY.</P
- [SDR P5CA2025040200010](https://openairdocs.org/sdr/P5CA2025040200010.md): Valve · malfunctioned · Apr 2, 2025 · N858GT · Boeing 74787UF · Pressure Regulator/Outflow Valve
  > AIR TURNBACK DUE TO LOSS OF CABIN PRESSURE.(<P>R+R SMOKE OVERIDE VALVE PER AMM 21-58-06, OPS CHECK GOOD.</P>)
- [SDR P5CA2024051200008](https://openairdocs.org/sdr/P5CA2024051200008.md): Hydraulic Line · ruptured · May 12, 2024 · N858GT · Boeing 74787UF · Hydraulic System, Main
  > HYD PRESS SYS 4 EICAS. #4 HYD QTY 40%(<P>INSPECTION FOUND #4 HYDRAULIC RETURN FLEX LINE IN THE R/H HORIZONTAL STABILIZER, CLOSE TO THE R/H INBOARD ELEVATOR PCU HAD RUPTURED. REMOVED THE DAMAGED LINE. INSTALLED TEMPORARY FLEX LINE, WITH RE-INSPECTION DUE EVERY
- [SDR P5CA2023091400105](https://openairdocs.org/sdr/P5CA2023091400105.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Rudder Structure
  > LWR RUDDER - FX, L/H AFT SEAL TORN(<P>LOCALLY FABRICATE REPAIR IAW RI #RI-53-00-16472 REV A. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090600103](https://openairdocs.org/sdr/P5CA2023090600103.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #9 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090600102](https://openairdocs.org/sdr/P5CA2023090600102.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #8 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090600101](https://openairdocs.org/sdr/P5CA2023090600101.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #19 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090600100](https://openairdocs.org/sdr/P5CA2023090600100.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #21 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090600099](https://openairdocs.org/sdr/P5CA2023090600099.md): Channel · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Horizontal Stabilizer Structure
  > LHÂ HORIZONTAL STAB O/B T/E WEDGE FWD ATTACH U-CHANNEL CRACK(<P>U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16446 REV A. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090500098](https://openairdocs.org/sdr/P5CA2023090500098.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #7 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090500097](https://openairdocs.org/sdr/P5CA2023090500097.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #6 VC FLAP LSA FOUND TORN(<P>PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</P>)
- [SDR P5CA2023090400096](https://openairdocs.org/sdr/P5CA2023090400096.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Wing Miscellaneous Structure
  > RHW L/E #3 PYLON TO WING CAVITY VAPOUR BARRIER FOUND CRACK(<P>VAPOUR BARRIER PANEL CRACK AREA REPAIRED AS PER SRM 57-41-01-2R-6 REPAIR 6 FIG 201 TO FIG 204 REV 40 DATE: 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090400095](https://openairdocs.org/sdr/P5CA2023090400095.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Trailing Edge Flaps
  > #9 VC FLAP BULL NOSE O/B EDGE FOUND DELAM MARKED(<P>PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023090300094](https://openairdocs.org/sdr/P5CA2023090300094.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Elevator, Plate/Skin
  > RH I/B ELEVATOR I/B AFT UPPER SURFACE FOUND DENT MARK(<P>PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023083000092](https://openairdocs.org/sdr/P5CA2023083000092.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Fuselage Main, Frame
  > APU COMPT STA 2664 WL 310 R//H FRAME FOUND CRACK(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 REV 40 DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023083000091](https://openairdocs.org/sdr/P5CA2023083000091.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > APU BATTERY COMPT STA 2598 - STA 2618 STR 42R FOUND CRACK(<P>CRACK STRINGER REPLACED AS PER RI #RI-53-80-16468 REV A. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023083000090](https://openairdocs.org/sdr/P5CA2023083000090.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Fuselage Main, Frame
  > APU COMPARTMENT LH FRAME STA 2664 CRACKED(<P> FRAME CRACK AREA REPAIRED AS PER RI #RI-53-80-16456 REV A. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023083000089](https://openairdocs.org/sdr/P5CA2023083000089.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Fuselage Main, Frame
  > APU COMPT LH FRAME STA 2685 CRACKED(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 REV 40 DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023083000088](https://openairdocs.org/sdr/P5CA2023083000088.md): Unknown · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Fuselage Miscellaneous Structure
  > M/D STA 1480 +20 - 1480 +40 RBL 75" HAT SECTION FOUND CRACK(<P>HAT SECTION CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-10 REPAIR 10 FIG 201 REV 40, DATE 20 JUN 2023. NO FURTHER DEFECTS NOTED</P>)
- [SDR P5CA2023082800087](https://openairdocs.org/sdr/P5CA2023082800087.md): Fitting · unknown · Sep 22, 2023 · N858GT · Boeing 74787UF · Landing Gear System
  > LH WLG I/B STRUT DOOR FWD EDGE LOWER FITTING WORN(<P>WORN FTG REPLACED AS PER SRM 51-10-02 AND NEW FTG HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FTG INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023). NO FURTHER DEFECTS NOTED</P>)

Next page: https://openairdocs.org/aircraft/N858GT/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 = 'N858GT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N858GT/reports

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