# N858GT: 2011 Boeing 747-87UF - Status: Valid registration - Airframe: [Boeing 747-87UF](https://openairdocs.org/model/boeing-747-87uf) (registry code 13848GA, 467 seats) - Engine: [GE GENX-2B67B](https://openairdocs.org/engine/ge-genx-2b67b) (registry code 30165) - Data sheets: [TCDS E00078NE](https://openairdocs.org/tcds/E00078NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 37569 - Year built: 2011 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 16, 2014 - Certificate issued: May 2, 2022 - Expires: May 31, 2029 - Mode S code: ABC5B8 - Registered owner: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=858GT - Page: https://openairdocs.org/aircraft/N858GT From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 16 in force ### Matched by airframe (Boeing 747-87UF) None in force. ### Matched by engine (GE GENX-2B67B) - [AD 2026-14-03](https://openairdocs.org/ad/2026-14-03): Engine Fuel Distribution · General Electric Company GE Aerospace GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Aug 21, 2026 - [AD 2026-04-09](https://openairdocs.org/ad/2026-04-09): Turbine Engine Compressor Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 11, 2026 - [AD 2024-25-07](https://openairdocs.org/ad/2024-25-07): Turbine Engine Compressor Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Feb 12, 2025 - [AD 2022-25-20](https://openairdocs.org/ad/2022-25-20): Turbine Engine Compressor Section, Turbine Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Jan 26, 2023 - [AD 2022-20-12](https://openairdocs.org/ad/2022-20-12): Turbine Engine Compressor Section, Turbine Section · General Electric GEnx-1B54/P2, GEnx-1B58/P2, GEnx-1B64/P2 and 13 more. Effective Nov 16, 2022 - [AD 2022-03-16](https://openairdocs.org/ad/2022-03-16): Turbine Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 21, 2022 - [AD 2022-04-07](https://openairdocs.org/ad/2022-04-07): Fuel Controlling System · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 9, 2022 - [AD 2021-21-05](https://openairdocs.org/ad/2021-21-05): Engine Controls · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Dec 28, 2021 - [AD 2021-13-16](https://openairdocs.org/ad/2021-13-16): Engine Fuel Distribution · General Electric GEnx-2B67, GEnx-2B67/P and GEnx-2B67B. Effective Aug 25, 2021 - [AD 2021-11-07](https://openairdocs.org/ad/2021-11-07): Turbine Engine Compressor Section · General Electric Genx-1B76A/P2, GEnx-1B64, GEnx-1B64/P1 and 17 more. Effective Jul 30, 2021 - [AD 2020-13-04](https://openairdocs.org/ad/2020-13-04): Engine Controls · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Jul 24, 2020 - [AD 2019-02-01](https://openairdocs.org/ad/2019-02-01): Turbine section · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Feb 25, 2019 - [AD 2018-21-12](https://openairdocs.org/ad/2018-21-12): Engine Fuel Distribution · General Electric GEnx-2B67, GEnx-2B67/P and GEnx-2B67B. Effective Jan 4, 2019 - [AD 2013-23-14](https://openairdocs.org/ad/2013-23-14): Critical rotating life-limited parts (LLPs) · General Electric GEnx-2B67 and GEnx-2B67B. Effective Jan 7, 2014 - [AD 2013-16-15](https://openairdocs.org/ad/2013-16-15): Booster anti-ice (BAI) air duct · General Electric GEnx-2B67B. Effective Sep 23, 2013 - [AD 2012-19-08](https://openairdocs.org/ad/2012-19-08): Fan mid shafts (FMS) · General Electric GEnx-1B54, GEnx-1B54/P1, GEnx-1B58 and 13 more. Effective Sep 21, 2012 ### Historical (superseded or no longer in force) - [AD 2018-16-07](https://openairdocs.org/ad/2018-16-07) (historical): Turbine Section · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Aug 15, 2018 - [AD 2017-09-06](https://openairdocs.org/ad/2017-09-06) (historical): Engine · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Jun 9, 2017 - [AD 2015-15-03](https://openairdocs.org/ad/2015-15-03) (historical): Power loss in ice crystal icing (ICI) conditions · General Electric GEnx-1B54, GEnx-1B54/P1, GEnx-1B54/P2 and 26 more. Effective Aug 24, 2015 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N858GT. ## FAA accident and incident reports None matched to N858GT. ## Service difficulty reports (94, newest 50) As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR P5CA2026042800022](https://openairdocs.org/sdr/P5CA2026042800022), Apr 28, 2026: SWITCH. FAULTED. 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 - [SDR P5CA2026041800019](https://openairdocs.org/sdr/P5CA2026041800019), Apr 18, 2026: TIRE. LEAKING. #8 TIRE PRESSURE ADVISORY MESSAGE - TIRE PRESSURE DECREASING.(

FOUND #8 MAIN TIRE PRESSURE LOW. REMOVED AND REPLACED #8 MAIN WHEEL ASSY PER AMM 32-45-01. ALSO - [SDR P5CA2025102200094](https://openairdocs.org/sdr/P5CA2025102200094), Oct 22, 2025: POWER SUPPLY. INOPERATIVE. 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 O - [SDR P5CA2025101800093](https://openairdocs.org/sdr/P5CA2025101800093), Oct 18, 2025: OUTFLOW VALVE. FAULTED. AT FLT 310, CABIN PRESSURE BECAME UNCONTROLLABLE. OUTFLOW VALVES WERE INDICATING FULLY CLOSED. CABIN ALTITUDE WAS CLIMBING 200 FPM.(

COMPLETED THE FOLLOWING C - [SDR P5CA2025100300066](https://openairdocs.org/sdr/P5CA2025100300066), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-8R.(

1. REPAIRED THE STRINGER IAW W/S NO. 50668 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHE - [SDR P5CA2025100300067](https://openairdocs.org/sdr/P5CA2025100300067), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 980+15, S-8L.(

1. REPAIRED THE STRINGER IAW W/S NO. 50670 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION - [SDR P5CA2025100300068](https://openairdocs.org/sdr/P5CA2025100300068), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 882, S-8L.(

1. REPAIRED THE STRINGER IAW W/S NO. 50659 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHE - [SDR P5CA2025100300069](https://openairdocs.org/sdr/P5CA2025100300069), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 892, S-8L.(

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 - [SDR P5CA2025100300070](https://openairdocs.org/sdr/P5CA2025100300070), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880, S-10R.(

1. REPAIRED THE STRINGER IAW W/S NO. 50669 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CH - [SDR P5CA2025100300071](https://openairdocs.org/sdr/P5CA2025100300071), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 866, S-10R.(

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. 5066 - [SDR P5CA2025100300072](https://openairdocs.org/sdr/P5CA2025100300072), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 840, S-11L.(

1. REPAIRED THE STRINGER IAW W/S NO. 50664 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB COMPLETE - [SDR P5CA2025100300073](https://openairdocs.org/sdr/P5CA2025100300073), Oct 3, 2025: STRINGER. CRACKED. 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 114 - [SDR P5CA2025100300074](https://openairdocs.org/sdr/P5CA2025100300074), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-11L.(

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. 5066 - [SDR P5CA2025100300075](https://openairdocs.org/sdr/P5CA2025100300075), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 1660, S-10R.(

1. ACCOMPLISHED EI NO. T2025A53M-1965 REV 1. 2. ACCOMPLISHED EI NO. T2025A53M-1965 REV 2. 3. - [SDR P5CA2025100300076](https://openairdocs.org/sdr/P5CA2025100300076), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 880 S-10L.(

1. REPAIRED THE STRINGER IAW W/S NO. 50671 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHE - [SDR P5CA2025100300077](https://openairdocs.org/sdr/P5CA2025100300077), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 780 S-10L.(

1. PERFORMED EI NO. T2025A53M-1973 REV 1 SEQUENCE A & B. 2. ACCOMPLISHED EI NO. T2025A53M-1973 RE - [SDR P5CA2025100300078](https://openairdocs.org/sdr/P5CA2025100300078), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 760 S-8L.(

1. REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. PERFORM EI NO. T2025A53M-1990 REV 1 - [SDR P5CA2025100300079](https://openairdocs.org/sdr/P5CA2025100300079), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK BETWEEN STA 2177 AND STA 2185 S-8R.(

1. PERFORM STRINGER REPAIR IAW W/S NO. 50672 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-1 - [SDR P5CA2025100300080](https://openairdocs.org/sdr/P5CA2025100300080), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER CRACK FRAME FWD SIDE BETWEEN STA 1957 AND STA 1966 S-9R.(

1. REPAIR THE STRINGER IAW W/S NO. 50674 AND SRM 53-60-03-2R-4 REV 46/ TR - [SDR P5CA2025100300081](https://openairdocs.org/sdr/P5CA2025100300081), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT AFT OF STA 2180, S-11R.(

1. PERFORMED STRINGER REPAIR IAW W/S NO. 50658 AND SRM 53-60-03-2R-3 REV 46/ TR: 53-154. 2. - [SDR P5CA2025100300082](https://openairdocs.org/sdr/P5CA2025100300082), Oct 3, 2025: STRINGER. CRACKED. CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-6R.(

1. REMOVED FASTERNERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW W/S NO. 50660 AND SRM 5 - [SDR P5CA2025100300083](https://openairdocs.org/sdr/P5CA2025100300083), Oct 3, 2025: STRINGER. CRACKED. CRACK - FOUND STRINGER HAVE CRACK AT FWD OF STA 2598 S-8L.(

1. REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 46. 2. REPAIR STRINGER IAW SRM 51-40-02-0G-0 REV 46 - [SDR P5CA2025100300084](https://openairdocs.org/sdr/P5CA2025100300084), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER CRACK BETWEEN STA 2177 AND STA 2185 S-10R.(

1. PERFORM STRINGER REPAIR IAW W/S NO. 50673 AND SRM 53-60-03-2R-3 REV 46/ TR:53-154. 2 - [SDR P5CA2025100300085](https://openairdocs.org/sdr/P5CA2025100300085), Oct 3, 2025: STRINGER. CRACKED. FOUND CROWN STRINGER HAVE CRACK AT STA 920, S-9L.(

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 FUR - [SDR P5CA2025100300086](https://openairdocs.org/sdr/P5CA2025100300086), Oct 3, 2025: STRINGER. CRACKED. FOUND CROWN STRINGER HAVE CRACK AT STA 905, S-9L.(

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 - [SDR P5CA2025100300087](https://openairdocs.org/sdr/P5CA2025100300087), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND FUSELAGE CROWN STRINGER HAVE CRACK AT STA 780, S-12R.(

1. REPAIR STRINGER AREA IAW W/S NO. 50663 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. JOB - [SDR P5CA2025100300088](https://openairdocs.org/sdr/P5CA2025100300088), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 793, S-12R.(

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. - [SDR P5CA2025100300089](https://openairdocs.org/sdr/P5CA2025100300089), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 746, S-12R.(

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. - [SDR P5CA2025100300090](https://openairdocs.org/sdr/P5CA2025100300090), Oct 3, 2025: STRINGER. CRACKED. CRACK - FND CROWN STRINGER HAVE CRACK AT STA 860, S-9L.(

1. REPAIR THE STRINGER IAW W/S NO. 50667 AND SRM 53-20-03-2R-1 REV 46/ TR: 53-159. 2. CONDITION CHECK - [SDR P5CA2025100300091](https://openairdocs.org/sdr/P5CA2025100300091), Oct 3, 2025: ACTUATOR. MALFUNCTIONED. FOUND RH WLG ALTERNATE EXTENSION ACTUATOR FUNCTION ABNORMAL.(

1. REPLACED RH WLG ALTERNATE EXTENSION ACTUATOR IAW AMM 32-36-01-004-001 REV 48A AND AMM 32-36-0 - [SDR P5CA2025100300092](https://openairdocs.org/sdr/P5CA2025100300092), Oct 3, 2025: POWER SUPPLY. NO TEST. FOUND EMERGENCY LIGHT BATTERY (M5169) FUNCTION FAIL AND CAN NOT RE-CHARGE.(

REPLACED POWER SUPPLY ASSY AND PERFORM POWER SUPPLY INSTALLATION TEST IAW AMM 33-5 - [SDR P5CA2025040200010](https://openairdocs.org/sdr/P5CA2025040200010), Apr 2, 2025: VALVE. MALFUNCTIONED. AIR TURNBACK DUE TO LOSS OF CABIN PRESSURE.(

R+R SMOKE OVERIDE VALVE PER AMM 21-58-06, OPS CHECK GOOD.

) - [SDR P5CA2024051200008](https://openairdocs.org/sdr/P5CA2024051200008), May 12, 2024: HYDRAULIC LINE. RUPTURED. HYD PRESS SYS 4 EICAS. #4 HYD QTY 40%(

INSPECTION FOUND #4 HYDRAULIC RETURN FLEX LINE IN THE R/H HORIZONTAL STABILIZER, CLOSE TO THE R/H INBOARD ELEVATOR PCU - [SDR P5CA2023091400105](https://openairdocs.org/sdr/P5CA2023091400105), Sep 22, 2023: UNKNOWN. UNKNOWN. LWR RUDDER - FX, L/H AFT SEAL TORN(

LOCALLY FABRICATE REPAIR IAW RI #RI-53-00-16472 REV A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090600103](https://openairdocs.org/sdr/P5CA2023090600103), Sep 22, 2023: UNKNOWN. UNKNOWN. #9 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER  CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090600102](https://openairdocs.org/sdr/P5CA2023090600102), Sep 22, 2023: UNKNOWN. UNKNOWN. #8 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER  CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090600101](https://openairdocs.org/sdr/P5CA2023090600101), Sep 22, 2023: UNKNOWN. UNKNOWN. #19 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER  CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090600100](https://openairdocs.org/sdr/P5CA2023090600100), Sep 22, 2023: UNKNOWN. UNKNOWN. #21 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090600099](https://openairdocs.org/sdr/P5CA2023090600099), Sep 22, 2023: CHANNEL. UNKNOWN. LHÂ HORIZONTAL STAB O/B T/E WEDGE FWD ATTACH U-CHANNEL CRACK(

U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16446 REV A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090500098](https://openairdocs.org/sdr/P5CA2023090500098), Sep 22, 2023: UNKNOWN. UNKNOWN. #7 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090500097](https://openairdocs.org/sdr/P5CA2023090500097), Sep 22, 2023: UNKNOWN. UNKNOWN. #6 VC FLAP LSA FOUND TORN(

PERFORMED LSA REPAIR AS PER CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2023090400096](https://openairdocs.org/sdr/P5CA2023090400096), Sep 22, 2023: UNKNOWN. UNKNOWN. RHW L/E #3 PYLON TO WING CAVITY VAPOUR BARRIER FOUND CRACK(

VAPOUR BARRIER PANEL CRACK AREA REPAIRED AS PER SRM 57-41-01-2R-6 REPAIR 6 FIG 201 TO FIG 204 REV - [SDR P5CA2023090400095](https://openairdocs.org/sdr/P5CA2023090400095), Sep 22, 2023: UNKNOWN. UNKNOWN. #9 VC FLAP BULL NOSE O/B EDGE FOUND DELAM MARKED(

PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 5. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023090300094](https://openairdocs.org/sdr/P5CA2023090300094), Sep 22, 2023: UNKNOWN. UNKNOWN. RH I/B ELEVATOR I/B AFT UPPER SURFACE FOUND DENT MARK(

PERFORMED COMPOSITE WET LAYUP REPAIR AS PER SRM 51-70-04 REPAIR 1. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023083000092](https://openairdocs.org/sdr/P5CA2023083000092), Sep 22, 2023: UNKNOWN. UNKNOWN. APU COMPT STA 2664 WL 310 R//H FRAME FOUND CRACK(

FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 REV 40 DATE 20 JUN 2023. NO FURTHER DEFE - [SDR P5CA2023083000091](https://openairdocs.org/sdr/P5CA2023083000091), Sep 22, 2023: UNKNOWN. UNKNOWN. APU BATTERY COMPT STA 2598 - STA 2618 STR 42R FOUND CRACK(

CRACK STRINGER REPLACED AS PER RI #RI-53-80-16468 REV A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023083000090](https://openairdocs.org/sdr/P5CA2023083000090), Sep 22, 2023: UNKNOWN. UNKNOWN. APU COMPARTMENT LH FRAME STA 2664 CRACKED(

 FRAME CRACK AREA REPAIRED AS PER RI #RI-53-80-16456 REV A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023083000089](https://openairdocs.org/sdr/P5CA2023083000089), Sep 22, 2023: UNKNOWN. UNKNOWN. APU COMPT LH FRAME STA 2685 CRACKED(

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

- [SDR P5CA2023083000088](https://openairdocs.org/sdr/P5CA2023083000088), Sep 22, 2023: UNKNOWN. UNKNOWN. M/D STA 1480 +20 - 1480 +40 RBL 75" HAT SECTION FOUND CRACK(

HAT SECTION CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-10 REPAIR 10 FIG 201 REV 40, DATE 20 JUN 2 - [SDR P5CA2023082800087](https://openairdocs.org/sdr/P5CA2023082800087), Sep 22, 2023: FITTING. UNKNOWN. LH WLG I/B STRUT DOOR FWD EDGE LOWER FITTING WORN(

WORN FTG REPLACED AS PER SRM 51-10-02 AND NEW FTG HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FTG INSTALL All 94: https://openairdocs.org/aircraft/N858GT/reports.md ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 747-87UF aircraft: https://openairdocs.org/model/boeing-747-87uf/aircraft.md - The GE GENX-2B67B engine: https://openairdocs.org/engine/ge-genx-2b67b.md --- 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.