# N855GT: 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: 37567 - Year built: 2013 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 2, 2013 - Certificate issued: May 16, 2013 - Expires: May 31, 2029 - Mode S code: ABBA93 - 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=855GT - Page: https://openairdocs.org/aircraft/N855GT 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 N855GT. ## FAA accident and incident reports None matched to N855GT. ## Service difficulty reports (125, 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 P5CA2026042000020](https://openairdocs.org/sdr/P5CA2026042000020), Apr 12, 2026: TIRE. WARNING MESSAGE. TIRE PRESSURE EICAS & STS MSG OCCURRED AFTER T/O. PERFORMED CONDITIONAL INSPECTION ON MLG 11 & 12 AXLE IAW AMM 05-51-25 (1-8) & AMM 32-45-04-206-011, NO DAMAGE - [SDR P5CA2026012300014](https://openairdocs.org/sdr/P5CA2026012300014), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-5L, AT AFT SIDE OF STA 2360.(

1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. 2. REPAIR DAMAGE AREA I - [SDR P5CA2026012000002](https://openairdocs.org/sdr/P5CA2026012000002), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-8R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50870 (SRM 53-80-03-2R-2 REV: 47) JOB COMPLETED AND CONDITION CHECK N - [SDR P5CA2026012000003](https://openairdocs.org/sdr/P5CA2026012000003), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50869 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK - [SDR P5CA2026012000004](https://openairdocs.org/sdr/P5CA2026012000004), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-6R, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50868 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK - [SDR P5CA2026012000005](https://openairdocs.org/sdr/P5CA2026012000005), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-5L, AT FWD SIDE OF STA 2598. REPAIR DAMAGE AREA IAW W/S NO: 50867 (SRM 53-80-03-2R-2 REV: 47). JOB COMPLETED AND CONDITION CHECK - [SDR P5CA2026012000006](https://openairdocs.org/sdr/P5CA2026012000006), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-2L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50876 (SRM 53-60-03-2R-8 REV: 47) AND EI T2026A53M-087 REV 1. JOB COM - [SDR P5CA2026012000007](https://openairdocs.org/sdr/P5CA2026012000007), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-20R, AT AFT SIDE OF STA 2360. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S N - [SDR P5CA2026012000008](https://openairdocs.org/sdr/P5CA2026012000008), Jan 21, 2026: STRING. CRACKED. CRACK DAMAGE ON THE STRINGER S-7R, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S 50877 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK NORM - [SDR P5CA2026012000009](https://openairdocs.org/sdr/P5CA2026012000009), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-7L, AT FWD SIDE OF STA 2360. REPAIR DAMAGE AREA IAW W/S NO: 50878 (SRM 53-60-03-2R-8 REV: 47). JOB COMPLETED AND CONDITION CHECK - [SDR P5CA2026012000010](https://openairdocs.org/sdr/P5CA2026012000010), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-9L, AT STA 930. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 47. REPAIR DAMAGE AREA IAW W/S NO: 60010 (SRM - [SDR P5CA2026012000011](https://openairdocs.org/sdr/P5CA2026012000011), Jan 21, 2026: STRINGER SPLICE. CRACKED. CRACK DAMAGE ON THE STRINGER AND STRINGER SPLICES S-10R, AT FWD AND FWD SIDE OF STA 2180. REPAIR DAMAGE AREA IAW W/S NO: 50871 (SRM 53-60-03-2R-3 REV: 47) AND E - [SDR P5CA2026012000012](https://openairdocs.org/sdr/P5CA2026012000012), Jan 21, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-3L, AT AFT SIDE OF STA 2360.(

1. REPAIR DAMAGE AREA IAW EI NO: T2026A53M-034 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL - [SDR P5CA2026012000013](https://openairdocs.org/sdr/P5CA2026012000013), Jan 21, 2026: BATTERY PACK. NO TEST. FOUND EXTERIOR EMER LT (L6690) INOP. PERFORM WIRING CONTINUITY CHECK AND SYSTEM TROUBLESHOOTING IAW WDM 33-51-72 REV 35, FOUND M5168 BATTERY FUNCTION FAILED. PE - [SDR P5CA2025041600013](https://openairdocs.org/sdr/P5CA2025041600013), Apr 30, 2025: SHEAR TIE. DAMAGED. FUSELAGE SECTION 46 - FUSELAGE SKIN (P/N: 146U3867-5) - PUNCTURE BETWEEN STA 2000 AND S38L TO S39L - CATEGORY B REPAIR.(

SHEAR TIE REPLACED AS PER SRM 51-10-0 - [SDR P5CA2025041900014](https://openairdocs.org/sdr/P5CA2025041900014), Apr 30, 2025: WEB. CRACKED. EMP - RH HORIZONTAL STAB TIP FAIRING I/B CLOSURE WEB, FOUND CRACK.(

CRACK - WEB REPLACED AS PER SRM 51-10-01. NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05. N - [SDR P5CA2025042100015](https://openairdocs.org/sdr/P5CA2025042100015), Apr 30, 2025: SKIN. DAMAGED. #18 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042100016](https://openairdocs.org/sdr/P5CA2025042100016), Apr 30, 2025: SKIN. DAMAGED. #19 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042100017](https://openairdocs.org/sdr/P5CA2025042100017), Apr 30, 2025: SKIN. DAMAGED. #20 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042100018](https://openairdocs.org/sdr/P5CA2025042100018), Apr 30, 2025: SKIN. DAMAGED. #7 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042100019](https://openairdocs.org/sdr/P5CA2025042100019), Apr 30, 2025: SKIN. DAMAGED. #8 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042100020](https://openairdocs.org/sdr/P5CA2025042100020), Apr 30, 2025: SKIN. DAMAGED. #9 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2025042200021](https://openairdocs.org/sdr/P5CA2025042200021), Apr 30, 2025: BEAM. CRACKED. LHW NO.11 K-FLAP AT WS 569 D-BEAM LWR ATT BOLT AREA, FOUND CRACK.(

CRACK AREA REPAIRED AS PER RI NO: RI-57-41-17558 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2025042200022](https://openairdocs.org/sdr/P5CA2025042200022), Apr 30, 2025: CHANNEL. CRACKED. LH HORIZONTAL STAB TIP T/E FAIRING FWD U CHANNEL CRACK.(

U CHANNEL REPLACED AS PER RI NO: RI-55-10-17562 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2025042300023](https://openairdocs.org/sdr/P5CA2025042300023), Apr 30, 2025: SEAT TRACK. DAMAGED. M/D STA 1510, 1530, 1550 LBL 11 SEAT TRACK SLOT HOLE ELONGATED.(

SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-9 REPAIR 9 FIG 201 AND RI NO: RI-53-65-17570 REV A - [SDR P5CA2025042300024](https://openairdocs.org/sdr/P5CA2025042300024), Apr 30, 2025: WEB. CRACKED. EMP - RH HORIZONTAL STAB TIP FAIRING CLOSURE WEB LWR CHORD CRACK.(

LWR CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201. NO FURTHER DEFECTS NOTED.RIB REPLACED AS PER SRM 51-10-02. NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05 - [SDR P5CA2025042300026](https://openairdocs.org/sdr/P5CA2025042300026), Apr 30, 2025: BEAM. CRACKED. RHW I/B L/E D-BEAM AT I/B PDU AREA O/B FOUND CRACK ILES 520.(

CRACK AREA REPAIRED AS PER RI-57-41-17559 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2025042300027](https://openairdocs.org/sdr/P5CA2025042300027), Apr 30, 2025: SUPPORT BEAM. DAMAGED. RHW ILE 450 I/B SUPPORT BEAM UPPER FTG FOUND HOLE ELONGATED.(

SUPPORT BEAM REPAIRED AS PER SRM 57-41-09-2R-2 REPAIR 2 FIG 203 DETAIL IV AND RI-57-41-17586 REV - [SDR P5CA2025042300028](https://openairdocs.org/sdr/P5CA2025042300028), Apr 30, 2025: SKIN. DAMAGED. #21 V/C FLAP LSA LAYER DAMAGED.(

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

) - [SDR P5CA2024110800048](https://openairdocs.org/sdr/P5CA2024110800048), Nov 8, 2024: PCB. FAILED. REJECTED TAKE OFF @ 110 KNOTS MASTER WARING ON EICAS.(

REMOVED & REPLACED MAWEA PRINTED CIRCUIT CARD (MASTER MONITORS) AMM 31-51-02/401, HIGH ENERGEY STOP - [SDR P5CA2024072100015](https://openairdocs.org/sdr/P5CA2024072100015), Jul 21, 2024: WARNING MESSAGE. FALSE ACTIVATION. LOW AIRSPEED REJECT DUE TO "CONFIG SPOILER" AT 40 KTS(

CMC SHOWED NO EXISTING FAULT. PERFORMED SPOILER TEST AND T/O CONFIG GND TEST, TEST PASSED. NO MAINT MSG - [SDR P5CA2024061500014](https://openairdocs.org/sdr/P5CA2024061500014), Jun 15, 2024: ACTUATOR. FAULTED. SPEED BRAKE HANDLE POPPED UP DURING TAKEOFF ROLL. LOW SPEED. TAKEOFF CONFIG WARNING APPEARED. AUTOSPOILER SYSTEM DEACTIVATED. R & R ACTUATOR IAW AMM 27-62-00, O - [SDR P5CA2023052000027](https://openairdocs.org/sdr/P5CA2023052000027), May 20, 2023: SWITCH. UNKNOWN. RTO AT APPROXIMATELY 140 KTS DUE TO "CONFIG SPOILERS" WARNING MSG AND SIREN. GROSS T/O WT 442.0(

PERFORMED HIGH ENERGY STOP INSPECTION IAW B747 AMM 05-51-10, - [SDR P5CA2023041300008](https://openairdocs.org/sdr/P5CA2023041300008), Apr 27, 2023: UNKNOWN. UNKNOWN. RH WING NO.21 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(

REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42

) - [SDR P5CA2023041300009](https://openairdocs.org/sdr/P5CA2023041300009), Apr 27, 2023: UNKNOWN. UNKNOWN. RH WING NO.19 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(

REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42

) - [SDR P5CA2023041300010](https://openairdocs.org/sdr/P5CA2023041300010), Apr 27, 2023: UNKNOWN. UNKNOWN. RH WING NO.20 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(

REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42

) - [SDR P5CA2023041700011](https://openairdocs.org/sdr/P5CA2023041700011), Apr 27, 2023: UNKNOWN. UNKNOWN. SB 747-57-2369, NO.8 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(

SB 747-57-2369, NO.8 FLAP TRACK FAIRI - [SDR P5CA2023041700012](https://openairdocs.org/sdr/P5CA2023041700012), Apr 27, 2023: UNKNOWN. UNKNOWN. SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICATION EXISTING REPAIR DEVIATION.(

SB 747-57-2369 NO.1 FLAP TRACK FAIRING ACTUATOR FRAME MODIFICAT - [SDR P5CA2023041800013](https://openairdocs.org/sdr/P5CA2023041800013), Apr 27, 2023: UNKNOWN. UNKNOWN. APU COMPARTMENT LH STA 2664.19 FRAME FOUND CRACKED (AT ELECTRICAL CABLE ATT BRACKET AREA).(

APU COMPARTMENT LH STA 2664.19 FRAME WL 305 CRACK AREA REPAIRED IA - [SDR P5CA2023041800014](https://openairdocs.org/sdr/P5CA2023041800014), Apr 27, 2023: UNKNOWN. UNKNOWN. LHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 FOUND WORN.(

LHW O/B REFUEL PNL 521CB FWD HINGE P/N: 116U4152-5 WORN AREA TIME-LIMIT REPAIRED - [SDR P5CA2023041900015](https://openairdocs.org/sdr/P5CA2023041900015), Apr 27, 2023: UNKNOWN. UNKNOWN. L/H WING I/B L/E CAVITY NO.7 V LINK (COUNT FROM I/B) UPPER BRACKET FOUND ELONGATED.(

LHW ILES 442.84 RIB SUPPORT BEAM ATTACHMENT FLANGE FASTENER HOLE ELONGATI - [SDR P5CA2023042300017](https://openairdocs.org/sdr/P5CA2023042300017), Apr 27, 2023: ROD. UNKNOWN. RHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED.(

RHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49 - [SDR P5CA2023042300018](https://openairdocs.org/sdr/P5CA2023042300018), Apr 27, 2023: ROD. UNKNOWN. LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FOUND ELONGATED(

LHW REFUEL PANEL O/B ROD CLEVIS PN: 116U4252-157 FABRICATED AND REPLACED IAW RI-52-49- - [SDR P5CA2023042300019](https://openairdocs.org/sdr/P5CA2023042300019), Apr 27, 2023: ROD. UNKNOWN. LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FOUND ELONGATED.(

LHW REFUEL PANEL I/B ROD CLEVIS PN: 116U4252-159 FABRICATED AND REPLACED IAW RI-52-49-16198 - [SDR P5CA2023042400020](https://openairdocs.org/sdr/P5CA2023042400020), Apr 27, 2023: UNKNOWN. UNKNOWN. RH WING NO.18 V/C FLAP LSA LAYER FOUND IN POOR CONDITION(

REPAIRED WITH ADHESIVE PASTE AS PER CMM 57-55-42

) - [SDR P5CA2023042400021](https://openairdocs.org/sdr/P5CA2023042400021), Apr 27, 2023: UNKNOWN. UNKNOWN. RH HORI. STAB. TIP FAIRING AFT WEDGEÂ U CHANNEL FOUND CRACK(

U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16183 REV.A

) - [SDR P5CA2023042400022](https://openairdocs.org/sdr/P5CA2023042400022), Apr 27, 2023: UNKNOWN. UNKNOWN. LH HORI. STAB. TIP FAIRING AFT WEDGE U CHANNEL FOUND CRACK(

U-CHANNEL REPLACED AS PER RI NO. RI-55-10-16182 REV.A

) - [SDR P5CA2023032600006](https://openairdocs.org/sdr/P5CA2023032600006), Mar 26, 2023: UNKNOWN. UNKNOWN. LOGPAGE 1669079 ITEM 6, AIRCRAFT WAS STRUCK BY A CARGO CONTAINER @ APPROX STATION STRINGER 44 AFT OF CARGO DOOR(

LOGPAGE 1669079 M6: EVALUATING DAMAGE AT STA - [SDR P5CA2022051200111](https://openairdocs.org/sdr/P5CA2022051200111), May 12, 2022: DETECTOR. INOPERATIVE. MAIN CARGO SMOKE DETECTOR MID 11 INOP(PLACED ON MDR 165471 IAW MEL 26-14-01-04A, CAT C.REMOVED AND REPLACED MAIN DECK MID SMOKE DETECTOR #11 IAW AMM 26-14-01/40 All 125: https://openairdocs.org/aircraft/N855GT/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.