# N852GT: 2012 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: 37571 - Year built: 2012 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 28, 2012 - Certificate issued: May 5, 2023 - Expires: May 31, 2030 - Mode S code: ABAF6E - Registered owner: [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC) - Location: [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase) - Owner type: Corporation - Owner's area on the map: 41.0382° N, 73.7107° W: Placed by OpenAirDocs at the center of ZIP code 10577, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=852GT - Page: https://openairdocs.org/aircraft/N852GT 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 (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA26WA132](https://openairdocs.org/ntsb/DCA26WA132), Feb 8, 2026: Boeing 747 (N852GT), Sao Paulo, Brazil, incident, no damage - [NTSB DCA17WA166](https://openairdocs.org/ntsb/DCA17WA166), Jul 15, 2017: Boeing 747-87UF (N852GT), Narita, Japan, incident, minor damage ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20240411004189I](https://openairdocs.org/incident/20240411004189I), Apr 11, 2024: Boeing 747-87UF (N852GT), Anchorage, AK, Minor damage. On April 11, 2024, a Boeing 747-8F deflated six (6) main left gear tires after landing in Anchorage, Alaska (anc). The flight was operated by a flight crew of… ## Service difficulty reports (105, 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 UIEA2026101800991](https://openairdocs.org/sdr/UIEA2026101800991), Oct 18, 2026: OUTFLOW VALVE. FAULTED. CRZ FLT FL 380: CABIN ALT WARNING AT 10,800 FT OBSERVED. ELEC QRH C/W. EMERGENCY DESCENT PERFORMED WITH O2 MASKS ON.(

REMOVED AND REPLACED LWR FWD CARGO OVERB - [SDR UIEA2026092100890](https://openairdocs.org/sdr/UIEA2026092100890), Sep 21, 2026: ACTUATOR. NO TEST. 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 G - [SDR UIEA2026092100891](https://openairdocs.org/sdr/UIEA2026092100891), Sep 21, 2026: STRUCTURE. CRACKED. 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 - [SDR UIEA2026092100892](https://openairdocs.org/sdr/UIEA2026092100892), Sep 21, 2026: FAIRING. CRACKED. 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 A - [SDR UIEA2026092100893](https://openairdocs.org/sdr/UIEA2026092100893), Sep 21, 2026: FAIRING. CRACKED. FOUND R/H OUTBD ELEVATOR INBD UPPER FAIRING PANEL CRACK.(

1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0 G-0 REV 49. 2. ACCOMPLISHED EI T2026A55M-1832 RE - [SDR UIEA2026092100894](https://openairdocs.org/sdr/UIEA2026092100894), Sep 21, 2026: STIFFENER. CRACKED. CRACK - FOUND R/H OUTBD ELEVATOR STIFFENER CRACK AT ELEV STA 260.98.(

1. REMOVED DAMAGED PART IAW SRM 51-40-02-0G-0 REV 49. 2. FABRICATED PART IAW EI T2026A55 - [SDR UIEA2026092100895](https://openairdocs.org/sdr/UIEA2026092100895), Sep 21, 2026: WEB. CRACKED. FOUND R/H OUTBD ELEVATOR WEB CRACKED AT ELEV STA 281.8.(

1. ACCOMPLISHED EI T2026A55M-1832 REV 4 AND EI ATTACHED TO WO 12882275. 2. JOB COMPLETED & CONDIT - [SDR UIEA2026092100896](https://openairdocs.org/sdr/UIEA2026092100896), Sep 21, 2026: SUPPORT. CRACKED. 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 ATTACHE - [SDR UIEA2026092100897](https://openairdocs.org/sdr/UIEA2026092100897), Sep 21, 2026: SUPPORT. CRACKED. 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 ATT - [SDR UIEA2026092100898](https://openairdocs.org/sdr/UIEA2026092100898), Sep 21, 2026: STRINGER. CRACKED. 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 CH - [SDR UIEA2026092100899](https://openairdocs.org/sdr/UIEA2026092100899), Sep 21, 2026: STRINGER. CRACKED. 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 - [SDR UIEA2026092100900](https://openairdocs.org/sdr/UIEA2026092100900), Sep 21, 2026: STRINGER. CRACKED. 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 CHE - [SDR UIEA2026092100901](https://openairdocs.org/sdr/UIEA2026092100901), Sep 21, 2026: STRINGER. CRACKED. 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 - [SDR UIEA2026092100902](https://openairdocs.org/sdr/UIEA2026092100902), Sep 21, 2026: STRINGER. CRACKED. 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), Sep 21, 2026: STRINGER. CRACKED. 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), Sep 21, 2026: STRINGER. CRACKED. 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 CO - [SDR UIEA2026092100905](https://openairdocs.org/sdr/UIEA2026092100905), Sep 21, 2026: STRINGER. CRACKED. 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 COM - [SDR UIEA2026092100906](https://openairdocs.org/sdr/UIEA2026092100906), Sep 21, 2026: STRINGER. CRACKED. 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 COMPLET - [SDR UIEA2026032600107](https://openairdocs.org/sdr/UIEA2026032600107), Mar 25, 2026: SKIN. DAMAGED. LEFT HORIZONTAL STAB L/E UPPER SKIN DAMAGE(

PERFORMED CAT B REPAIR PER EO 4855A028. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2025021900152](https://openairdocs.org/sdr/UIEA2025021900152), Feb 16, 2025: STRUCTURE. DAMAGED. TE RUDDER DAMAGE.(

REPAIRED IAW SRM 51-70-05 AND EA 1955A028. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024111501093](https://openairdocs.org/sdr/UIEA2024111501093), Nov 15, 2024: RAM AIR TURB. ACTIVATED. RAT BUTTON INADVERTANTLY DEPRESSED(

RAM AIR TURBINE DEPLOYED AND OPERATED NORMALLY. RESTOWED RAT AS PER AMM TASK 29-21-00-960-802, ALL FUNCTIONS NORMAL

) - [SDR UIEA2024083000879](https://openairdocs.org/sdr/UIEA2024083000879), Aug 27, 2024: SEAT TRACK. CORRODED. M/D STA 1835-1852 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(

M/D STA 1835-1852 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROT - [SDR UIEA2024083000878](https://openairdocs.org/sdr/UIEA2024083000878), Aug 27, 2024: SEAT TRACK. CORRODED. M/D - STA 1815-1835 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(

M/D STA 1815-1835 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPR - [SDR UIEA2024083000877](https://openairdocs.org/sdr/UIEA2024083000877), Aug 27, 2024: SEAT TRACK. CORRODED. M/D STA 1795-1815 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(

M/D STA 1795-1815 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED - [SDR UIEA2024083000876](https://openairdocs.org/sdr/UIEA2024083000876), Aug 27, 2024: STRUCTURE. TORN. LHW #7 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000875](https://openairdocs.org/sdr/UIEA2024083000875), Aug 27, 2024: STRUCTURE. TORN. LHW #8 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000874](https://openairdocs.org/sdr/UIEA2024083000874), Aug 27, 2024: STRUCTURE. TORN. LHW #9 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000873](https://openairdocs.org/sdr/UIEA2024083000873), Aug 27, 2024: STRUCTURE. TORN. RHW #18 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000872](https://openairdocs.org/sdr/UIEA2024083000872), Aug 27, 2024: STRUCTURE. TORN. RHW #19 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000871](https://openairdocs.org/sdr/UIEA2024083000871), Aug 27, 2024: STRUCTURE. TORN. RHW #20 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000870](https://openairdocs.org/sdr/UIEA2024083000870), Aug 27, 2024: STRUCTURE. TORN. RHW #21 V/C FLAP LSA FOUND TORN.(

PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000869](https://openairdocs.org/sdr/UIEA2024083000869), Aug 27, 2024: PANEL. DAMAGED. LHW I/B MAIN FLAP MOST O/B SEAL PAN PANEL SCREW HOLE FOUND ELONGATED.(

PERFORMED PERMANENT REPAIR AS PER SRM 51-70-05 REPAIR 7. NO FURTHER DEFECTS NOTED - [SDR UIEA2024083000868](https://openairdocs.org/sdr/UIEA2024083000868), Aug 27, 2024: CHANNEL. CRACKED. R/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(

PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17038 REV.A .NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000867](https://openairdocs.org/sdr/UIEA2024083000867), Aug 27, 2024: CHANNEL. CRACKED. L/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(

PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17039 REV.A .NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000866](https://openairdocs.org/sdr/UIEA2024083000866), Aug 27, 2024: BEAM. CRACKED. RHW L/E - ILES 567 D BEAM WEB CRACKED.(

RHW L/E - ILES 567 D BEAM WEB REPAIRED IAW RI-57-41-17036 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000865](https://openairdocs.org/sdr/UIEA2024083000865), Aug 27, 2024: SKIN. DAMAGED. RHW - L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM AREA AS MARKED.(

RHW L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM SKIN PANE - [SDR UIEA2024083000864](https://openairdocs.org/sdr/UIEA2024083000864), Aug 27, 2024: STRINGER. CRACKED. AFT OF STA 2598 BULKHEAD, S-42R STRINGER FOUND CRACKED.(

AFT OF STA 2598 BULKHEAD, S-42R STRINGER REPAIRED IAW RI-53-80-17040 REV.A. NO FURTHER DEFECTS - [SDR UIEA2024083000863](https://openairdocs.org/sdr/UIEA2024083000863), Aug 27, 2024: BEAM. CRACKED. LHW L/E - ILES 567 D-BEAM WEB CRACKED.(

LHW L/E - ILES 567 D-BEAM WEB REPAIRED IAW RI-57-41-17037 REV.A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2024083000862](https://openairdocs.org/sdr/UIEA2024083000862), Aug 27, 2024: STRINGER. CRACKED. AFT OF 2598 BULKHEAD, S-4R STRINGER CRACKED.(

AFT OF 2598 BULKHEAD, S-4R STRINGER REPAIRED IAW RI-53-80-17041 REV.A. NO FURTHER DEFECTS NOTED.

RH #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN FABRICATED IAW RI-57-00-17048 R - [SDR UIEA2024083000860](https://openairdocs.org/sdr/UIEA2024083000860), Aug 27, 2024: SUPPORT CHANNEL. CRACKED. LHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA FOUND CRACKED.(

LHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA REPAIRED IAW RI-57-00-17045 REV A . NO F - [SDR P5CA2022071900149](https://openairdocs.org/sdr/P5CA2022071900149), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: FLAP. PEELING. 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), Aug 4, 2022: SKIN. DELAMINATED. LH W - O/B T/E FLAP AFT EDGE AREA FOUND DELAMINATION ON UPPER SKIN(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR1) All 105: https://openairdocs.org/aircraft/N852GT/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.