# Service difficulty reports: N850GT A list on [N850GT](https://openairdocs.org/aircraft/N850GT.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 · 116 reports - [SDR UIEA2026083000825](https://openairdocs.org/sdr/UIEA2026083000825.md): Landing Gear · malfunctioned · Aug 30, 2026 · N850GT · Boeing 74787UF · Nose/Tail Landing Gear > AFTER LINING UP ON RWY 08R, ENGS STABILIZED AT 45 % WHEN ADVANCING THROTTLES, ACFT VEERED RIGHT. TOWER NOTICED SMOKE FROM NOSE TIRES, TAKEOFF REJECTED AT 10KTS. RETURN TO BLOCKS FOR TIRE INSPECTION. REMOVED NOSE TIRES, INSPECTED NLG AXLE IAW AMM 32-45-02. NO - [SDR UIEA2026042300239](https://openairdocs.org/sdr/UIEA2026042300239.md): Stringer · cracked · Apr 23, 2026 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK - FOUND M/D STRINGER CRACK AT STA 1960 FWD SIDE S-9R.(

1. REPAIRED DAMAGED AREA IAW W/S 60224 & SRM 53-60-03-2R-4 REV 48. 2. JOB COMPLETED.

) - [SDR UIEA2026042300240](https://openairdocs.org/sdr/UIEA2026042300240.md): Stringer · cracked · Apr 23, 2026 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK - FOUND M/D STRINGER CRACK AT STA 1960 FWD SIDE S-11R.(

1. REPAIRED DAMAGED AREA IAW W/S 60225 & SRM 53-60-03-2R-4 REV 48. 2. JOB COMPLETED.

) - [SDR UIEA2026042300241](https://openairdocs.org/sdr/UIEA2026042300241.md): Stringer · cracked · Apr 23, 2026 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK - FOUND M/D STRINGER CRACK AT STA 1960 FWD SIDE S-12R.(

1. REPAIRED DAMAGED AREA IAW W/S 60226 & SRM 53-60-03-2R-4 REV 48. 2. JOB COMPLETED.

) - [SDR UIEA2026042300242](https://openairdocs.org/sdr/UIEA2026042300242.md): Stringer · cracked · Apr 23, 2026 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360.(

1. REPAIRED DAMAGED AREA IAW W/S 60229 & SRM 53-60-03-2R-8 REV 48. 2. JOB COMPLETED.

) - [SDR UIEA2026042300243](https://openairdocs.org/sdr/UIEA2026042300243.md): Stringer · cracked · Apr 23, 2026 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > CRACK DAMAGE ON THE STRINGER S-15L, AT STA 1140 FWD STRINGER.(

1. REMOVE THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 48. 2. ACCOMPLISHED EI T2026A53M-699 REV 1. 3. INSTALL FASTENER IAW SRM 51-40-02-0G-0 REV 48 AND DWG 144U3635 SH18 REV - & DWG 144U7702 S - [SDR UIEA2025022000153](https://openairdocs.org/sdr/UIEA2025022000153.md): Warning Message · false activation · Feb 20, 2025 · N850GT · Boeing 74787UF · Stabilizer Position Indicating > BLOCK TURN BACK. LOW SPEED REJECT T/O DUE TO T/O WARNING STAB TRIM. MCC NOTIFIED, NO EICAS MESSAGE, NO CURRENT FAULT, NO EXISTING FAULT, HORIZONTAL STABILIZER TRIM CONTROL SYSTEM AND ADJUSTMENT TEST IAW AMM 27-41-00/501. - [SDR UIEA2024061900555](https://openairdocs.org/sdr/UIEA2024061900555.md): Switch · failed · Jun 19, 2024 · N850GT · Boeing 74787UF · Fire Protection System > REJECTED TAKE OFF AT 30/40 KNOTS DUE TO BLEED DUCT LEAK R LOOP A FAIL, APU DUCT LEAK AND WARNING MESSAGE SPOILER CONFIGURATION(

REMOVED AND REPLACED DAMAGED APU BLEED AIR DUCT SEAL AT WING STATION RH 1010 AS PER AMM 36-11-01. OPS AND LEAK CHECK GOOD. REPLACE - [SDR UIEA2024031900158](https://openairdocs.org/sdr/UIEA2024031900158.md): Battery Pack · no test · Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency Lighting > U/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACE BATTERY PACK AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024031900159](https://openairdocs.org/sdr/UIEA2024031900159.md): Battery Pack · no test · Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency Lighting > U/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACE BATTERY PACK AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024031900160](https://openairdocs.org/sdr/UIEA2024031900160.md): Battery · no test · Mar 29, 2024 · N850GT · Boeing 74787UF · Emergency Lighting > U/D EMER LIGHT BATT PACK CAP TEST FAILED. REPLACED BATTERY POWER SUPPLY AND OPERATION TEST NORMAL IAW AMM 33-51-04 REV 44. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100166](https://openairdocs.org/sdr/UIEA2024032100166.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #8 V/C FLAP LSA FOUDN TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100170](https://openairdocs.org/sdr/UIEA2024032100170.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #9 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA AS PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100172](https://openairdocs.org/sdr/UIEA2024032100172.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #6 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100178](https://openairdocs.org/sdr/UIEA2024032100178.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #7 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100180](https://openairdocs.org/sdr/UIEA2024032100180.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #21 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100181](https://openairdocs.org/sdr/UIEA2024032100181.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #20 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100182](https://openairdocs.org/sdr/UIEA2024032100182.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #19 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032100183](https://openairdocs.org/sdr/UIEA2024032100183.md): Skin · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #18 V/C FLAP LSA FOUND TORN. PERFORMED REPAIR AT LSA TORN AREA PER SMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200184](https://openairdocs.org/sdr/UIEA2024032200184.md): Floor Panel · damaged · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Floor Panel > M/D - STA 460 - 480 LBL 30-90 FLOOR PANEL FOUND DEPRESSION. FABRICATED FLOOR PANEL IAW RI-53-00-16779 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200188](https://openairdocs.org/sdr/UIEA2024032200188.md): Skin · dented · Mar 29, 2024 · N850GT · Boeing 74787UF · Landing Gear Doors > 2EA DENTS IN LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 FWD DENT 3.0W X 0.5 DEEP AFT DENT 3.0W X.05 AFT DENT 2.5W X 0.3 DEEP DEEP. LH NLG DOOR AT O/B EDGE CENTERED LENGTH WISE STA 292.82 FWD WITHIN SRM 52-80-01-1A-1 LIMITS REV 42 ( W=3" Y=0.06 - [SDR UIEA2024032200189](https://openairdocs.org/sdr/UIEA2024032200189.md): Repair · torn · Mar 29, 2024 · N850GT · Boeing 74787UF · Trailing Edge Flaps > #10 V/C FLAP EXISTING PATCH FOUND TORN. PERFORMED REPAIR AT EXISTING PATCH TORN AREA PER SRM 51-70-04 REPAIR 7. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200190](https://openairdocs.org/sdr/UIEA2024032200190.md): Skin · dented · Mar 29, 2024 · N850GT · Boeing 74787UF · Landing Gear Doors > 2EA DENTS IN LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 FWD DENT 3.0W X 0.5 DEEP AFT DENT 2.5W X.03 DEEP. LH NLG DOOR AT O/B EDGE CENTERED LENGTHWISE STA 292.82 AFT WITHIN SRM 52-80-01-1A-1 LIMITS REV 42 DATE 20 FEB 2024 ( W=1" Y=0.030" W/Y = 33 - [SDR UIEA2024032200191](https://openairdocs.org/sdr/UIEA2024032200191.md): Skin · dented · Mar 29, 2024 · N850GT · Boeing 74787UF · Cargo/Baggage Doors > DENT AFT CARGO DOOR BS 1850 LENGTH 1.063 X 0.118 X 0.01 WIDTH WITHIN LIMITS PER SRM 53-00-01-14-2 FIG. REF SRM 52-30-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL V111 REV 42 AND NTM PART 6, 51-00-00 PROC 23 REV 176. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200192](https://openairdocs.org/sdr/UIEA2024032200192.md): Door Frame · dented · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Structure > DENT AT FWD EDGE AFT CARGO DOOR FRAME DENT. SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 REV 42. MEASURED LENGTH 1.25" DEPTH 0.100" WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL I LIMIT REV 42. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200193](https://openairdocs.org/sdr/UIEA2024032200193.md): Rib · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer, Spar/Rib > RH HORI STAB CLOSURE RIB UPPER CHORD FOUND CRACKED. UPPER CHORD REPLACED IAW SRM 51-10-02, SRM 51-40-05 AND SRM 51-40-02 ALL IN REV 42. HORI STAB CLOSURE RIB UPPER CHORD AREA. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200194](https://openairdocs.org/sdr/UIEA2024032200194.md): Web · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > RH HORI STAB TIP FAIRING I/B SUPPORT WEB LOWER CHORD CRACKED. LOWER CHORD REPLACED PER SRM 51-10-02, SRM 51-40-05 AND SRM 51-40-02 ALL IN REV 42 DATE 20 FEB 2024 AT EMP - RH HORI STAB TIP FAIRING I/B SUPPORT WEB LOWER CHORD AREA. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200195](https://openairdocs.org/sdr/UIEA2024032200195.md): Skin · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer, Plate/Skin > EMP - RH HORI STAB REAR SPAR STIFFENER FOUND CRACK AT STAB STAB. 560-4. FABRICATE THE STIFFENER P/N 65B03779-66 PER 65B03779 DWG 1, 2 AND PL AS PER FORM 02373R02, SRM 51-10-02, 51-40-05 AND SRM 51-40-02 REV 42. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032200196](https://openairdocs.org/sdr/UIEA2024032200196.md): Skin · damaged · Mar 29, 2024 · N850GT · Boeing 74787UF · Vertical Stabilizer, Plate/Skin > VERT FIN TIP FAIRING UPPER T/E CORNER BURN MARK. BLEND OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED. ALLOWABLE DAMAGE PER SRM 55-30-30-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL XIV ALL IN REV 42. - [SDR UIEA2024032400212](https://openairdocs.org/sdr/UIEA2024032400212.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 920-940 S-7R STRINGER SUSPECT SCRATCH / CRACK AND STA 962 STR 7R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 920-940 AND STA 962 S-7R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16783 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400213](https://openairdocs.org/sdr/UIEA2024032400213.md): Channel · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > L/H HORI. STAB. TIP FAIIRNGÂ U CHANNEL FOUND CRACK. BONDED NEW U CHANNEL PER RI-55-10-16799 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400214](https://openairdocs.org/sdr/UIEA2024032400214.md): Channel · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure > R/H HORI. STAB. TIP FAIIRNGÂ U CHANNEL FOUND CRACK. BONDED NEW U CHANNEL PER RI-55-10-16798 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400215](https://openairdocs.org/sdr/UIEA2024032400215.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 940-960 S-8R STRINGER SUSPECT SCRATCH / CRACK AND STA 982 STR 8R 1 LOC CRACK FROM RIVET TO STRINGER. M/D STA 940-960 AND STA 982 S-8R STRINGER REPAIR AS PER SRM 53-20-03 & RI-53-20-16784 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400216](https://openairdocs.org/sdr/UIEA2024032400216.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 880-900 S-8R STRINGER SUSPECT SCRATCH / CRACKED. M/D - STA 880-900 S-8R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16784 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400217](https://openairdocs.org/sdr/UIEA2024032400217.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D STA 880-900 S-7R STRINGER SUSPECT SCRATCH / CRACK. M/D STA 880-900 S-7R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16783 REV A. NO FURTHER DEFECTS NOTED. P/N 142U7741-14.

) - [SDR UIEA2024032400218](https://openairdocs.org/sdr/UIEA2024032400218.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 900 STR 10R 1 LOC CRACK FROM RIVET TO STRINGER AND STA 920 STR 10R 5 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 900 AND STA 920 STR 10R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16786 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032400219](https://openairdocs.org/sdr/UIEA2024032400219.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 820 STR 9R 1 LOC CRACK AT STRINGER AND STA 840 STR 9R 1 LOC CRACK AT STRINGER. M/D - STA 820 STR 9R AND STA 840 STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16785 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500220](https://openairdocs.org/sdr/UIEA2024032500220.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 910 STR 12R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 910 STR 12R STRINGER REPAIR AS PER SRM 53-20-03 REPAIR 2, REFER TO HKA-TLS-24-0130. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500221](https://openairdocs.org/sdr/UIEA2024032500221.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 918 - 920 STR 9R 8 LOC CRACK FROM RIVET TO STRINGER AND STA 962 STR 9R 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 918 - 920 AND STA 962 STR 9R STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16785 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500222](https://openairdocs.org/sdr/UIEA2024032500222.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 778 STR 9L 1 LOC CRACK FROM RIVET TO STRINGER AND STA 781 STR 9L 2 LOC CRACK. M/D - STA 778 AND STA 781 STR 9L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16782 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500223](https://openairdocs.org/sdr/UIEA2024032500223.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > M/D - STA 934, 938, 942 STR 9L 3 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 934, 938, 942 STR 9L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16782 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500224](https://openairdocs.org/sdr/UIEA2024032500224.md): Stringer · cracked · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer > BS 943, STR 7L 1 LOC CRACK FROM RIVET TO STRINGER. M/D - STA 943 STR 7L STRINGER REPAIR AS PER SRM 53-20-03 AND RI-53-20-16781 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500225](https://openairdocs.org/sdr/UIEA2024032500225.md): Flap · eroded · Mar 29, 2024 · N850GT · Boeing 74787UF · Leading Edge Devices > #16 K/FLAP BULLNOSEÂ FOUND EROSION. PERFORMED REPAIR AT EROSION AREA PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED. - [SDR UIEA2024032500227](https://openairdocs.org/sdr/UIEA2024032500227.md): Seat Track · damaged · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage, Seat/Cargo Attach Fittings > M/D - STA 1512 AND STA 1552 LBL 11:33 SEAT TRACK HOLES INSPECTION FINDING ARE BUSHING MISSING AS PER EO 4835A085(

STA 1512 AND STA 1552 LBL 11:33 SEAT TRACK REPAIRED IAW SRM 53-00-52 REPAIR 9 REV 42 DATE 20 FEB 2024 AND RI-53-00-16801 REV A. NO FURTHER DEFEC - [SDR UIEA2024032600228](https://openairdocs.org/sdr/UIEA2024032600228.md): Skin · dented · Mar 29, 2024 · N850GT · Boeing 74787UF · Fuselage Main, Plate/Skin > RH SIDE SECTION 46 13" AFT MIDWAY UP FROM AFT CARGO DOOR CUTOUT 3" X 3" CIRCULAR BLEND. REPAIR IAW SRM 51-10-02 AND SRM 51-20-01 REV 42 DATE 20 FEB 2024 AND RI-53-60-16802 REV A. NO FURTHER DEFECTS NOTED. - [SDR UIEA2023121540997](https://openairdocs.org/sdr/UIEA2023121540997.md): Unknown · unknown · Nov 11, 2023 · N850GT · Boeing 74787UF · Trailing Edge Flap Control System > FLAPS DRIVE ON APPROACH WHEN SELECTING FLAPS 5 (FROM FLAPS 1). T/E FLAPS STATUS MSG AFTER LANDING. EMERGENCY DECLARED.(

RAN FCC GROUND TEST. ALL PASSED REF AMM 27-51-00. FLAPS OPERATE NORMAL.

) - [SDR UIEA2023073100766](https://openairdocs.org/sdr/UIEA2023073100766.md): Transducer · unknown · Jul 31, 2023 · N850GT · Boeing 74787UF · Drag Control System > REJECTED TAKE-OFF AT 141 KTS DUE TO TAKE-OFF CONFIG SPOILERS.(

R/R SPEEDBRAKE TRANSDUCER IAW AMM 27-08-06. OPS CHECK OK. DMI 190404 CLOSED.

) - [SDR UIEA2022111501189](https://openairdocs.org/sdr/UIEA2022111501189.md): Pressure Switch · faulted · Nov 15, 2022 · N850GT · Boeing 74787UF · Hydraulic System, Main > FLT CONTROL SYS-STATUS MSG REPEAT WRITE-UP PREVIOUS FLIGHT PAGE 1680476. MSG APPEARD DURING CRUISE AT FL320. INFO ONLY HYD #2 QTY 11.4 MSG BLANKED WITH BREAKES SET AFTER BLOCK IN AT ICN.(

COMPLIED WITH FIM 27-09-00-810-878 AND PERFORMED ALL WIRING CHECKS. FO - [SDR UIEA2022021400112](https://openairdocs.org/sdr/UIEA2022021400112.md): Panel · cracked · Feb 23, 2022 · N850GT · Boeing 74787UF · Cargo Compartments > M/D - STA 1780 - 1840 LBL 11-33 CASTER MAT FOUND CRACK.(

PERFORM REPAIR AS PER CMM 25-59-36 REV 2 REPAIR 6.A REPAIR OF A CORNER OF THE PANEL.

) - [SDR UIEA2022021400113](https://openairdocs.org/sdr/UIEA2022021400113.md): Panel · cracked · Feb 23, 2022 · N850GT · Boeing 74787UF · Cargo Compartments > M/D - STA 1700 - 1740 LBL 11 - 33 CASTER MAT FOUND CRACKED.(

PERFORM REPAIR AS PER CMM 25-59-36 REV 2 REPAR 6.A REPAIR OF A CORNER OF THE PANEL.

) Next page: https://openairdocs.org/aircraft/N850GT/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 = 'N850GT' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N850GT/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.