# N854GT: 2013 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: 37566 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 21, 2013 - Certificate issued: May 12, 2023 - Expires: May 31, 2030 - Mode S code: ABB6DC - 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=854GT - Page: https://openairdocs.org/aircraft/N854GT 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 N854GT. ## FAA accident and incident reports None matched to N854GT. ## Service difficulty reports (142, 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 UIEA2026081100741](https://openairdocs.org/sdr/UIEA2026081100741), Aug 20, 2026: CARGO TRACK. DAMAGED. WHILE WORKING MDDR 256255, FWD CARGO STA 500 LATERAL GUIDE AND ENDSTOP FWD - 4 EA BROKEN, NOTICED UNDERLYING STRUCTURE DAMAGED, INCLUDING SEAT TRACK, WEB, & LOW - [SDR UIEA2026031300089](https://openairdocs.org/sdr/UIEA2026031300089), Mar 14, 2026: BATTERY PACK. INOPERATIVE. MDDR 248876 - MAIN DECK CARGO COMPT LIGHT INOP ABOVE L1 DOOR INOP ( MAIN DECK CARGO HANDLING LIGHTS (747-8F) )(

LH EMER LIGHT POWER PACK CHARGER REPLACED, EME - [SDR UIEA2025041600489](https://openairdocs.org/sdr/UIEA2025041600489), May 27, 2025: SKIN. DAMAGED. #9 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025041600490](https://openairdocs.org/sdr/UIEA2025041600490), May 27, 2025: SKIN. DAMAGED. #18 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT #18 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025041600491](https://openairdocs.org/sdr/UIEA2025041600491), May 27, 2025: SKIN. DAMAGED. #19 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT #19 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025041600492](https://openairdocs.org/sdr/UIEA2025041600492), May 27, 2025: SKIN. DAMAGED. #8 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT #8 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025041600493](https://openairdocs.org/sdr/UIEA2025041600493), May 27, 2025: SKIN. DAMAGED. #7 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT #7 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025041600494](https://openairdocs.org/sdr/UIEA2025041600494), May 27, 2025: SKIN. DAMAGED. #6 V/C FLAP LSA LAYER DAMAGED.(

PERFORMED REPAIR AT #6 V/C FLAP LSA LAYER DAMAGED AREA PER CMM 57-55-42 REPAIR 17-1 REV 33. NO FURTHER DEFECTS NOTE - [SDR UIEA2025050200574](https://openairdocs.org/sdr/UIEA2025050200574), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 6R FOUND CRACKS.(

FWD OF BS 2360 STR 6R FOUND CRACKS REPAIRED IAW RI-53-61-17579 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025050200575](https://openairdocs.org/sdr/UIEA2025050200575), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 6L FOUND CRACK.(

FWD OF BS 2360 STR 6L FOUND CRACK REPAIRED IAW RI-53-61-17576 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025050200576](https://openairdocs.org/sdr/UIEA2025050200576), May 27, 2025: STRINGER. CRACKED. FWD OF BS 2360 STR 9R FOUND CRACK.(

FWD OF BS 2360 STR 9R CRACK REPAIRED IAW RI-53-61-17578 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025050500587](https://openairdocs.org/sdr/UIEA2025050500587), May 27, 2025: PANEL. CRACKED. LHW T/E LWR PNL (115U5464-1) FOUND CRACK AND DELAMINATION.(

PERFORMED REPAIR AT CRACK AND DELAMINATION AREA IAW RI-57-20-17583 REV A. NO FURTHER DEFECTS NOTED - [SDR UIEA2025050800589](https://openairdocs.org/sdr/UIEA2025050800589), May 27, 2025: SKIN. CORRODED. # 23 VC FLAP BULLNOSE FOUND EROSION.(

PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025050800590](https://openairdocs.org/sdr/UIEA2025050800590), May 27, 2025: SKIN. CORRODED. #4 VC FLAP BULLNOSE FOUND EROSION.(

PERFORMED REPAIR AT EROSION AREA IAW SRM 51-70-04 REPAIR 5 REV 45. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400606](https://openairdocs.org/sdr/UIEA2025051400606), May 27, 2025: STRINGER. CRACKED. FWD OF BS 2360 STR 10L FOUND CRACK.(

FWD OF BS 2360 STR 10L CRACK REPAIRED IAW RI-53-61-17590 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400607](https://openairdocs.org/sdr/UIEA2025051400607), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2360 S7L FOUND CRACKED.(

AFT OF STA 2360 S7L CRACK REPAIRED IAW RI-53-81-17571 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400608](https://openairdocs.org/sdr/UIEA2025051400608), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2360 S20L FOUND CRACKED.(

AFT OF STA 2360 S20L CRACK REPAIRED IAW RI-53-81-17588 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400609](https://openairdocs.org/sdr/UIEA2025051400609), May 27, 2025: CHANNEL. CRACKED. EMP -RH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL CRACKED.(

EMP - RH HORIZONTAL STABILIZER TIP FAIRING T/E UPPER CLOSURE RIB REPLACED IAW RI-55-10 - [SDR UIEA2025051400610](https://openairdocs.org/sdr/UIEA2025051400610), May 27, 2025: CHANNEL. CRACKED. EMP - LH HORIZONTAL STABILIZER TIP FAIRING T/E WEDGE U CHANNEL CRACK.(

EMP - LH HORIZONTAL STABILIZER TIP FAIRING T/E UPPER CLOSURE RIB REPLACED IAW RI-55-10- - [SDR UIEA2025051400611](https://openairdocs.org/sdr/UIEA2025051400611), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2360 S21L FOUND CRACKED.(

AFT OF STA 2360 S21L CRACK REPAIRED IAW RI-53-81-17565 REV C. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400612](https://openairdocs.org/sdr/UIEA2025051400612), May 27, 2025: STRINGER. CRACKED. FWD OF STA 2598 S7L FOUND CRACKED.(

FWD OF STA 2598 S7L CRACK REPAIRED IAW RI-53-81-17580 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400613](https://openairdocs.org/sdr/UIEA2025051400613), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2360 S24L FOUND CRACKED.(

AFT OF STA 2360 S24L CRACK REPAIRED IAW RI-53-81-17572 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400614](https://openairdocs.org/sdr/UIEA2025051400614), May 27, 2025: STRINGER. CRACKED. FWD OF STA 2598 S7R FOUND CRACKED(

FWD OF STA 2598 S7R CRACK REPAIRED IAW RI-53-81-17568 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051400615](https://openairdocs.org/sdr/UIEA2025051400615), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2598, S4L FOUND CRACKED.(

AFT OF STA 2598, S4L CRACK REPAIRED IAW RI-53-81-17626 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051500616](https://openairdocs.org/sdr/UIEA2025051500616), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2598, S12L FOUND CRACKED.(

AFT OF STA 2598, S12L CRACK REPAIRED IAW RI-53-81-17603 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051500617](https://openairdocs.org/sdr/UIEA2025051500617), May 27, 2025: STRINGER. CRACKED. M/D - STA 2340-2360 S-20R STRINGER FOUND CRACK.(

M/D - STA 2340-2360 S-20R STRINGER CRACK REPAIRED IAW RI-53-61-17604 REV A. NO FURTHER DEFECTS NOT - [SDR UIEA2025051500618](https://openairdocs.org/sdr/UIEA2025051500618), May 27, 2025: STRINGER. CRACKED. FWD OF BS2360 STR 7L FOUND CRACKS.(

FWD OF BS2360 STR 7L CRACKS REPAIRED IAW RI-53-61-17577 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051500619](https://openairdocs.org/sdr/UIEA2025051500619), May 27, 2025: STRINGER. CRACKED. M/D - STA 1940-1960 S-11L STRINGER FOUND CRACK.(

M/D - STA 1940-1960 S-11L STRINGER CRACK REPAIR IAW 747-8F SRM 53-60-03 REPAIR 4 ALTERNATIVE 2 & 747-8F S - [SDR UIEA2025051500622](https://openairdocs.org/sdr/UIEA2025051500622), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2360 S5R FOUND CRACKED.(

AFT OF STA 2360 S5R CRACK REPAIRED IAW RI-53-81-17597 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600623](https://openairdocs.org/sdr/UIEA2025051600623), May 27, 2025: STRINGER. CRACKED. FWD OF BS 2360 STR 10R FOUND CRACK.(

FWD OF BS 2360 STR 10R CRACK REPAIRED IAW RI-53-61-17589 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600624](https://openairdocs.org/sdr/UIEA2025051600624), May 27, 2025: STRINGER. CRACKED. FWD OF BS 2360 STR 7R FOUND CRACKS.(

FWD OF BS 2360 STR 7R CRACKS REPAIRED IAW RI-53-61-17592 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600625](https://openairdocs.org/sdr/UIEA2025051600625), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2598, S5L FOUND CRACKED.(

AFT OF STA 2598, S5L CRACK REPAIRED IAW RI-53-81-17566 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600626](https://openairdocs.org/sdr/UIEA2025051600626), May 27, 2025: STRINGER. CRACKED. FWD OF STA 2598 S6R FOUND CRACKED.(

FWD OF STA 2598 S6R CRACK REPAIRED IAW RI-53-81-17564 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600627](https://openairdocs.org/sdr/UIEA2025051600627), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2598, S7R FOUND CRACKED.(

AFT OF STA 2598, S7R CRACK REPAIRED IAW RI-53-81-17569 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600628](https://openairdocs.org/sdr/UIEA2025051600628), May 27, 2025: STRINGER. CRACKED. AFT OF STA 2598 S46R SUSPECT CRACKED.(

AFT OF STA 2598 S46R CRACK REPAIRED IAW RI-53-81-17627 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051600629](https://openairdocs.org/sdr/UIEA2025051600629), May 27, 2025: STRIKER. CRACKED. AFT OF STA 2598 S49L SUSPECT CRACKED.(

AFT OF STA 2598 S49L CRACK REPAIRED IAW RI-53-81-17581 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051800631](https://openairdocs.org/sdr/UIEA2025051800631), May 27, 2025: STRIKER. CRACKED. AFT OF STA 2360 S4L FOUND CRACKED.(

AFT OF STA 2360 S4L CRACKED REPAIRED IAW RI-53-81-17594 REV B. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051800632](https://openairdocs.org/sdr/UIEA2025051800632), May 27, 2025: STRIKER. CRACKED. AFT OF STA 2598, S1L FOUND CRACKED.(

AFT OF STA 2598, S1L CRACK REPAIRED IAW RI-53-81-17587 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051800633](https://openairdocs.org/sdr/UIEA2025051800633), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 2L FOUND CRACKS.(

FWD OF BS 2360 STR 2L CRACKS REPAIRED I.A.W RI-53-61-17633 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051900634](https://openairdocs.org/sdr/UIEA2025051900634), May 27, 2025: STRIKER. CRACKED. FWD OF BS2360 STR 1R FOUND CRACKS.(

FWD OF BS2360 STR 1R CRACKS REPAIRED IAW RI-53-61-17632 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051900635](https://openairdocs.org/sdr/UIEA2025051900635), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 2R FOUND CRACKS.(

FWD OF BS 2360 STR 2R CRACKS REPAIRED IAW RI-53-61-17601 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051900636](https://openairdocs.org/sdr/UIEA2025051900636), May 27, 2025: STRIKER. CRACKED. M/D - STA 1940-1960 S-10L STRINGER FOUND CRACK.(

M/D - STA 1940-1960 S-10L STRINGER CRACK REPAIRED IAW RI-53-61-17629 REV A. NO FURTHER DEFECTS NOT - [SDR UIEA2025051900637](https://openairdocs.org/sdr/UIEA2025051900637), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 1L FOUND CRACKS.(

FWD OF BS 2360 STR 1L CRACKS REPAIRED I.A.W RI-53-61-17598 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051900640](https://openairdocs.org/sdr/UIEA2025051900640), May 27, 2025: STRIKER. CRACKED. FWD OF BS 2360 STR 8R FOUND CRACK.(

FWD OF BS 2360 STR 8R CRACK REPAIRED IAW RI-53-61-17591 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025051900641](https://openairdocs.org/sdr/UIEA2025051900641), May 27, 2025: STRIKER. CRACKED. AFT OF STA 2598, S1R FOUND CRACKED.(

AFT OF STA 2598, S1R CRACK REPAIRED IAW RI-53-81-17585 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025052000642](https://openairdocs.org/sdr/UIEA2025052000642), May 27, 2025: STRINGER. CRACKED. M/D - STA 2340-2360 S-21L STRINGER FOUND CRACK.(

M/D - STA 2340-2360 S-21L STRINGER CRACK REPAIRED IAW RI-53-61-17602 REV A. NO FURTHER DEFECTS NOT - [SDR UIEA2025052000643](https://openairdocs.org/sdr/UIEA2025052000643), May 27, 2025: PANEL. CRACKED. LHW WS740 FIXED T/E PNL RIB FOUND CRACKED.(

LHW WS740 FIXED T/E PNL RIB CRACK REPAIRED IAW RI-57-24-17634 REV A. NO FURTHER DEFECTS NOTED.M/D - STA 2160-2180 S-11R STRINGER CRACK REAPAIR IAW RI-53-61-17643 REV A. NO FURTHER DEFECTS NOTE - [SDR UIEA2025052100664](https://openairdocs.org/sdr/UIEA2025052100664), May 27, 2025: STRINGER. CRACKED. M/D - STA 980+160 - 1000 S-12L STRINGER FOUND CRACK.(

M/D - STA 980+160 - 1000 S-12L STRINGER CRACK REPAIRED IAW RI-53-20-17611 REV A. NO FURTHER D - [SDR UIEA2025052100665](https://openairdocs.org/sdr/UIEA2025052100665), May 27, 2025: STRINGER. CRACKED. M/D - STA 1140-1160 S-16R STRINGER FOUND CRACK.(

M/D - STA 1140-1160 S-16R STRINGER CRACK REPAIRED IAW RI-53-41-17638 REV A. NO FURTHER DEFECTS NOT All 142: https://openairdocs.org/aircraft/N854GT/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.