# Service difficulty reports: N852GT

A list on [N852GT](https://openairdocs.org/aircraft/N852GT.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 3 · 105 reports

- [SDR UIEA2026101800991](https://openairdocs.org/sdr/UIEA2026101800991.md): Outflow Valve · faulted · Oct 18, 2026 · N852GT · Boeing 74787UF · Pressure Regulator/Outflow Valve
  > CRZ 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 05-51-08
- [SDR UIEA2026092100890](https://openairdocs.org/sdr/UIEA2026092100890.md): Actuator · no test · Sep 21, 2026 · N852GT · Boeing 74787UF · Landing Gear Actuator
  > RIGHT 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 TES
- [SDR UIEA2026092100891](https://openairdocs.org/sdr/UIEA2026092100891.md): Structure · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Structure
  > FOUND 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 UIEA2026092100892](https://openairdocs.org/sdr/UIEA2026092100892.md): Fairing · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > FOUND 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 REV
- [SDR UIEA2026092100893](https://openairdocs.org/sdr/UIEA2026092100893.md): Fairing · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > FOUND 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 65B0578
- [SDR UIEA2026092100894](https://openairdocs.org/sdr/UIEA2026092100894.md): Stiffener · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > CRACK - 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 UIEA2026092100895](https://openairdocs.org/sdr/UIEA2026092100895.md): Web · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > FOUND 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 UIEA2026092100896](https://openairdocs.org/sdr/UIEA2026092100896.md): Support · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > RT 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 SHEE
- [SDR UIEA2026092100897](https://openairdocs.org/sdr/UIEA2026092100897.md): Support · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Elevator Miscellaneous Structure
  > FOUND 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 SHE
- [SDR UIEA2026092100898](https://openairdocs.org/sdr/UIEA2026092100898.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100899](https://openairdocs.org/sdr/UIEA2026092100899.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100900](https://openairdocs.org/sdr/UIEA2026092100900.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100901](https://openairdocs.org/sdr/UIEA2026092100901.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100902](https://openairdocs.org/sdr/UIEA2026092100902.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100903](https://openairdocs.org/sdr/UIEA2026092100903.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100904](https://openairdocs.org/sdr/UIEA2026092100904.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100905](https://openairdocs.org/sdr/UIEA2026092100905.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026092100906](https://openairdocs.org/sdr/UIEA2026092100906.md): Stringer · cracked · Sep 21, 2026 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > CRACK 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 UIEA2026032600107](https://openairdocs.org/sdr/UIEA2026032600107.md): Skin · damaged · Mar 25, 2026 · N852GT · Boeing 74787UF · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB L/E UPPER SKIN DAMAGE(<P>PERFORMED CAT B REPAIR PER EO 4855A028. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2025021900152](https://openairdocs.org/sdr/UIEA2025021900152.md): Structure · damaged · Feb 16, 2025 · N852GT · Boeing 74787UF · Rudder Structure
  > TE RUDDER DAMAGE.(<P>REPAIRED IAW SRM 51-70-05 AND EA 1955A028. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2024111501093](https://openairdocs.org/sdr/UIEA2024111501093.md): Ram Air Turb · activated · Nov 15, 2024 · N852GT · Boeing 747 · Hydraulic Accumulator, Auxiliary
  > RAT 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 UIEA2024083000879](https://openairdocs.org/sdr/UIEA2024083000879.md): Seat Track · corroded · Aug 27, 2024 · N852GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 UIEA2024083000878](https://openairdocs.org/sdr/UIEA2024083000878.md): Seat Track · corroded · Aug 27, 2024 · N852GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 DAMAG
- [SDR UIEA2024083000877](https://openairdocs.org/sdr/UIEA2024083000877.md): Seat Track · corroded · Aug 27, 2024 · N852GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 UIEA2024083000876](https://openairdocs.org/sdr/UIEA2024083000876.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > LHW #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 UIEA2024083000875](https://openairdocs.org/sdr/UIEA2024083000875.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > LHW #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 UIEA2024083000874](https://openairdocs.org/sdr/UIEA2024083000874.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > LHW #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 UIEA2024083000873](https://openairdocs.org/sdr/UIEA2024083000873.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > RHW #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 UIEA2024083000872](https://openairdocs.org/sdr/UIEA2024083000872.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > RHW #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 UIEA2024083000871](https://openairdocs.org/sdr/UIEA2024083000871.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > RHW #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 UIEA2024083000870](https://openairdocs.org/sdr/UIEA2024083000870.md): Structure · torn · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > RHW #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 UIEA2024083000869](https://openairdocs.org/sdr/UIEA2024083000869.md): Panel · damaged · Aug 27, 2024 · N852GT · Boeing 74787UF · Trailing Edge Flaps
  > LHW 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 UIEA2024083000868](https://openairdocs.org/sdr/UIEA2024083000868.md): Channel · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure
  > R/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 UIEA2024083000867](https://openairdocs.org/sdr/UIEA2024083000867.md): Channel · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure
  > L/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 UIEA2024083000866](https://openairdocs.org/sdr/UIEA2024083000866.md): Beam · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Wing Main, Frame Structure
  > RHW 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 UIEA2024083000865](https://openairdocs.org/sdr/UIEA2024083000865.md): Skin · damaged · Aug 27, 2024 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > RHW - 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 UIEA2024083000864](https://openairdocs.org/sdr/UIEA2024083000864.md): Stringer · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > AFT 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 UIEA2024083000863](https://openairdocs.org/sdr/UIEA2024083000863.md): Beam · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Wing Main, Frame Structure
  > LHW 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 UIEA2024083000862](https://openairdocs.org/sdr/UIEA2024083000862.md): Stringer · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > AFT 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 UIEA2024083000861](https://openairdocs.org/sdr/UIEA2024083000861.md): Support Rib · broken · Aug 27, 2024 · N852GT · Boeing 74787UF · Wing, Rib/Bulkhead
  > RHW #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 UIEA2024083000860](https://openairdocs.org/sdr/UIEA2024083000860.md): Support Channel · cracked · Aug 27, 2024 · N852GT · Boeing 74787UF · Wing Miscellaneous Structure
  > LHW 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 P5CA2022071900149](https://openairdocs.org/sdr/P5CA2022071900149.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > RH W #20 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000150](https://openairdocs.org/sdr/P5CA2022072000150.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > RH W - #21 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000151](https://openairdocs.org/sdr/P5CA2022072000151.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > RH W - #19 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000152](https://openairdocs.org/sdr/P5CA2022072000152.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > RH W - #18 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000153](https://openairdocs.org/sdr/P5CA2022072000153.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > LH W - #10 VC-FLAP SURFACE LSA FOUND PEELING OFF(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR7)
- [SDR P5CA2022072000154](https://openairdocs.org/sdr/P5CA2022072000154.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Control Surfaces
  > LH W - #9 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000155](https://openairdocs.org/sdr/P5CA2022072000155.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Control Surfaces
  > LHW - #8 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072000156](https://openairdocs.org/sdr/P5CA2022072000156.md): Flap · peeling · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Control Surfaces
  > LH W - #7 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)
- [SDR P5CA2022072100157](https://openairdocs.org/sdr/P5CA2022072100157.md): Skin · delaminated · Aug 4, 2022 · N852GT · Boeing 74787UF · Wing, Plate/Skin
  > LH W - O/B T/E FLAP AFT EDGE AREA FOUND DELAMINATION ON UPPER SKIN(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR1)

Next page: https://openairdocs.org/aircraft/N852GT/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 = 'N852GT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N852GT/reports

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