# N853GT: 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: 37572 - Year built: 2012 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 3, 2012 - Certificate issued: June 22, 2023 - Expires: June 30, 2030 - Mode S code: ABB325 - 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=853GT - Page: https://openairdocs.org/aircraft/N853GT 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 N853GT. ## FAA accident and incident reports None matched to N853GT. ## Service difficulty reports (110, 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 UIEA2026042100229](https://openairdocs.org/sdr/UIEA2026042100229), Apr 21, 2026: OIL CAP. UNSECURE. ENG 3 OIL SYS STATUS MSG IN FLIGHT. OIL PRESSURE 24 PSI IN CRUISE. NR 3 ENG OIL FILL CAP FOUND OPEN. CLOSED CAP REF AMM 12-13-03. PERFORMED IDLE ENG RUN, OIL PR - [SDR P5CA2024111900049](https://openairdocs.org/sdr/P5CA2024111900049), Nov 19, 2024: ENGINE. UNKNOWN. DURING TAKEOFF WHILE POWER PUSHED UP TO STABILIZATION, THRUST ON ENG #3 AND #4 LAGGED AT 25-30% WHILE ENGINES #1 AND #2 CAME UP NORMALLY TO APPROXIMATELY 45% N1 - [SDR P5CA2024092900046](https://openairdocs.org/sdr/P5CA2024092900046), Oct 2, 2024: STRINGER. CRACKED. APU COMPT STA 2598 RH STRG 42R AFT BULKHEAD FOUND CRACK(

APU COMPT STA 2598 AFT BULKHEAD RH STGR 42R STRINGER REPLACEMENT IAW EO 4853A157 PART 2 STEP 2 AE AND - [SDR P5CA2024092800045](https://openairdocs.org/sdr/P5CA2024092800045), Oct 2, 2024: SUPPORT ROD. CRACKED. RHW L/E CAVITY #7 'A' SUPPORT ROD UPPER L/E RIB TAB CRACKED(

RHW L/E CAVITY #7 'A' SUPPORT ROD UPPER L/E RIB TAB REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2 AND R - [SDR P5CA2024092800044](https://openairdocs.org/sdr/P5CA2024092800044), Oct 2, 2024: SUPPORT. CRACKED. RHW L/E CAVITY #4 "A" UPR SUPPORT ROD ATT TAB (COUNT FROM I/B) FOUND CRACKED(

RHW L/E CAVITY #4 "A" UPR SUPPORT ROD ATT TAB (COUNT FROM I/B) REPAIRED IAW SRM - [SDR P5CA2024092800043](https://openairdocs.org/sdr/P5CA2024092800043), Oct 2, 2024: DOOR. CHAFED. APU - LH COMPT DOOR FWD EDGE CHAFING WORN(

 APU - LH COMPT DOOR FWD EDGE REPAIRED IAW SRM 52-40-01-2R-6 REV 43 DATE 20 JUN 2024. NO FURTHER DEFECTS NOTED - [SDR P5CA2024092800042](https://openairdocs.org/sdr/P5CA2024092800042), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 2R AFT OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 2R AFT OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-80-17141 REV.A. NO FURTHER - [SDR P5CA2024092800041](https://openairdocs.org/sdr/P5CA2024092800041), Oct 2, 2024: SKIN. DELAMINATED. #22 V/C FLAP BULLNOSE FOUND DELAMINATION(

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

) - [SDR P5CA2024092700040](https://openairdocs.org/sdr/P5CA2024092700040), Oct 2, 2024: CHANNEL. CRACKED. LH HORI. STAB. T/E TIP FAIRING U CHANNEL FOUND CRACK(

REPLACED U CHANNEL IAW RI 55-10-17081 REV A. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2024092700039](https://openairdocs.org/sdr/P5CA2024092700039), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 6R FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 6R FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17133 REV.A. NO FURTHER - [SDR P5CA2024092700038](https://openairdocs.org/sdr/P5CA2024092700038), Oct 2, 2024: STRINGER. CRACKED. BS 2360 FWD OF THE PRESSURE BULKHEAD STR 6L FOUND CRACK(

BS 2360 FWD OF THE PRESSURE BULKHEAD STR 6L STRINGER REPAIRED IAW RI-53-60-17132 REV.A. NO FURTHER DE - [SDR P5CA2024092700037](https://openairdocs.org/sdr/P5CA2024092700037), Oct 2, 2024: STRINGER. CRACKED. BS 2360 FWD OF THE PRESSURE BULKHEAD STR 9R FOUND CRACK(

BS 2360 FWD OF THE PRESSURE BULKHEAD STR 9R REPAIRED IAW RI-53-60-17135 REV A. NO FURTHER DEFECTS NOT - [SDR P5CA2024092700036](https://openairdocs.org/sdr/P5CA2024092700036), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 1L AFT OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 1L AFT OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17138 REV.A. NO FURTHER - [SDR P5CA2024092600035](https://openairdocs.org/sdr/P5CA2024092600035), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 7R FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 7R FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17086 REV.A. NO FURTHER - [SDR P5CA2024092600034](https://openairdocs.org/sdr/P5CA2024092600034), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 7L FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 7L FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17087 REV.A. NO FURTHER - [SDR P5CA2024092600033](https://openairdocs.org/sdr/P5CA2024092600033), Oct 2, 2024: STRINGER. CRACKED. STA 2360, AFT OF PRESSURE BULKHEAD, S22L CRACKED(

STA 2360, AFT OF PRESSURE BULKHEAD S-22L REPAIRED IAW RI-53-80-17089 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2024092600032](https://openairdocs.org/sdr/P5CA2024092600032), Oct 2, 2024: STRINGER. CRACKED. FX - STA 2360 BULKHEAD STRG 22R AFT FOUND CRACK(

FX STA 2360 BULKHEAD STRG 22R AFT REPAIRED IAW RI-53-80-17090 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2024092600031](https://openairdocs.org/sdr/P5CA2024092600031), Oct 2, 2024: STRINGER. CRACKED. STA 2598 BULKHEAD AFT STGR 25R FOUND CRACK(

STA 2598 BULKHEAD AFT STRG 25R REPAIR IAW RI-53-80-17126 REV.A. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2024092600030](https://openairdocs.org/sdr/P5CA2024092600030), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 1L FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 1L FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17134 REV.A. NO FURTHER - [SDR P5CA2024092600029](https://openairdocs.org/sdr/P5CA2024092600029), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 2R FWD OF PRESSURE BULKHEAD STINGER FOUND CRACK(

STA 2360 STR 2R FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-60-17131 REV.A. NO FURTHER - [SDR P5CA2024092600028](https://openairdocs.org/sdr/P5CA2024092600028), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 2L FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 2L FWD OF PRESSURE BULKHEAD STINGER REPAIRED IAW RI-53-60-17130 REV.A. NO FURTHER - [SDR P5CA2024092600027](https://openairdocs.org/sdr/P5CA2024092600027), Oct 2, 2024: STRINGER. CRACKED. STA 2360 STR 1R FWD OF PRESSURE BULKHEAD STRINGER FOUND CRACK(

STA 2360 STR 1R FWD OF PRESSURE BULKHEAD STRINGER REPAIRED IAW RI-53-80-17125 REV.A. NO FURTHER - [SDR P5CA2024092100026](https://openairdocs.org/sdr/P5CA2024092100026), Oct 2, 2024: SKIN. DELAMINATED. #9 V/C FLAP BULLNOSE FOUND DELAMINATION(

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

) - [SDR P5CA2024092100025](https://openairdocs.org/sdr/P5CA2024092100025), Oct 2, 2024: SKIN. DELAMINATED. #23 V/C FLAP BULLNOSE FOUND DELAMINATION(

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

) - [SDR P5CA2024092100024](https://openairdocs.org/sdr/P5CA2024092100024), Oct 2, 2024: SKIN. DELAMINATED. #23 V/C FLAP BULLNOSE FOUND DELAMINATION(

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

) - [SDR P5CA2024092000023](https://openairdocs.org/sdr/P5CA2024092000023), Oct 2, 2024: LAMP. INOPERATIVE. R/H NLG STRUT DOOR UPPER - EMERGENCY INERTIA REEL LIGHT (L6690) INOP(

R/H NLG STRUT DOOR UPPER EMERGENCY INERTIA REEL LIGHT L6690 LAMP REPLACED IAW AMM 33-51- - [SDR P5CA2024092000022](https://openairdocs.org/sdr/P5CA2024092000022), Oct 2, 2024: POWER SUPPLY. FAULTED. EMERGENCY LT L5730, L5731, L5732, L5734, L1382, L6690, M4914, X325 AND X326 WENT OFF IN LESS THAN 15 MINUTES(

EMER PWR SUPPLY M5168 REPLACED AND TEST NORMAL I - [SDR P5CA2024091900021](https://openairdocs.org/sdr/P5CA2024091900021), Oct 2, 2024: FLAP. WORN. #21 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2024091900020](https://openairdocs.org/sdr/P5CA2024091900020), Oct 2, 2024: FLAP. WORN. #20 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2024091900019](https://openairdocs.org/sdr/P5CA2024091900019), Oct 2, 2024: FLAP. WORN. #19 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2024091900018](https://openairdocs.org/sdr/P5CA2024091900018), Oct 2, 2024: FLAP. WORN. #9 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2024091900017](https://openairdocs.org/sdr/P5CA2024091900017), Oct 2, 2024: FLAP. WORN. #8 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2024091900016](https://openairdocs.org/sdr/P5CA2024091900016), Oct 2, 2024: FLAP. WORN. #6 V/C FLAP FOUND LSA WORN(

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

) - [SDR P5CA2023082800080](https://openairdocs.org/sdr/P5CA2023082800080), Aug 28, 2023: UNKNOWN. UNKNOWN. FIRE WARNING ENGINE #2(

R/R #2 ENGINE REF W/O #1177398 WORK CARD B72-099-00-01 UER #2 ENG ESN 959577. NO FURTHER DEFECTS NOTED.

) - [SDR P5CA2022092700182](https://openairdocs.org/sdr/P5CA2022092700182), Oct 16, 2022: SUPPORT RIB. ELONGATED. RHW L/E CAVITY ILES 440 RIB SUPPORT V-LINK FASTENER HOLE ELONGATED(RHW L/E CAVITY ILES 440 RIB SUPPORT V-LINK FASTENER HOLE REWORKED AS PER RI-57-00-15895 REV A - [SDR P5CA2022092700174](https://openairdocs.org/sdr/P5CA2022092700174), Oct 16, 2022: SUPPORT FRAME. CRACKED. EMP - APU COMPT LH STA 2680 SUPPORT FRAME FOUND CRACKED (EMP APU COMPT LH STA 2680 FRAME REPAIRED AS PER SRM 53-80-07-2R-1 AND 51-70-11-2R-0) - [SDR P5CA2022092700175](https://openairdocs.org/sdr/P5CA2022092700175), Oct 16, 2022: SUPPORT FRAME. CRACKED. EMP - APU COMPT LH STA 2690 SUPPORT FRAME FOUND CRACK (EMP APU COMPT L/H STA 2690 FRAME REPAIRED AS PER SRM 53-80-07-2R-1 AND 51-70-11-2R-0) - [SDR P5CA2022092700176](https://openairdocs.org/sdr/P5CA2022092700176), Oct 16, 2022: SKIN. DENTED. EMP - L/H HORI STAB L/E #331BL SKIN FOUND DENT MARK (LH H/STAB L/E ( #331BL ) DENT AREA REWORKED AS PER SRM 55-10-01-1-1A-1 FIG 101) - [SDR P5CA2022092700177](https://openairdocs.org/sdr/P5CA2022092700177), Oct 16, 2022: SKIN. DENTED. EMP - VERT STAB L/E SKIN (321B) FOUND DENT(V/STAB L/E SKIN ( 321B ) DENT AREA ( 2EA ) REWORKED AS PER SRM 53-30-01-1A-1 FIG 101) - [SDR P5CA2022092700178](https://openairdocs.org/sdr/P5CA2022092700178), Oct 16, 2022: SKIN. DENTED. EMP - VERT STAB L/E SKIN (#321G) FOUND DENT (V/STAB L/E SKIN ( #321G ) DENT AREA REWORKED AS PER SRM 53-30-01-1A-1 FIG 101) - [SDR P5CA2022092700179](https://openairdocs.org/sdr/P5CA2022092700179), Oct 16, 2022: WEB. CRACKED. EMP - LH HORI STAB O/B BL 421.5 WEB FOUND CRACK AFTER TIP FAIRING REMOVED (LH H/STAB O/B BL 421.5 WEB REPAIRED AS PER SRM 55-10-09-2R-12 & RI-55-00-15908 RE - [SDR P5CA2022092700180](https://openairdocs.org/sdr/P5CA2022092700180), Oct 16, 2022: SUPPORT FRAME. CRACKED. EMP - APU COMPT LH STA 2685 SUPPORT FRAME FOUND CRACK (EMP APU COMPT LH STA 2685 FRAME REPAIRED AS PER SRM 53-80-07-2R-1 AND 51-70-11-2R-0) - [SDR P5CA2022092700181](https://openairdocs.org/sdr/P5CA2022092700181), Oct 16, 2022: SUPPORT RIB. ELONGATED. RHW L/E CAVITY ILES 530 RIB SUPPORT `V` LINK FASTENER HOLES ELONGATED(RHW LE CAVITY ILES 530 RIB SUPPORT V-LINK FASTENER HOLE REWORKED AS PER RI-57-00-15895 REV - [SDR P5CA2022092700183](https://openairdocs.org/sdr/P5CA2022092700183), Oct 16, 2022: SUPPORT RIB. ELONGATED. RHW LE CAVITY ILES 470 SUPPORT RIB V-LINK FASTENER HOLE ELONGATED(RHW LE CAVITY ILES 470 SUPPORT RIB V-LINK FASTENER HOLE REWORKED AS PER RI-57-00-15895 REV A) - [SDR P5CA2022092700184](https://openairdocs.org/sdr/P5CA2022092700184), Oct 16, 2022: FASTENER. ELONGATED. LHW LE CAVITY ILES 450 RIB SUPPORT V-LINK FASTENER HOLE ELONGATED (LHW L/E CAVITY ILES 450 RIB SUPPORT V-LINK FASTENER HOLE REWORKED AS PER RI-57-00-15894 REV A - [SDR P5CA2022092900185](https://openairdocs.org/sdr/P5CA2022092900185), Oct 16, 2022: STRAP. CRACKED. NO.4 PYLON TORQUE BOX O/B LWR MATEL STRIP FOUND CRACK.(NO.4 PYLON TORQUE BOX O/B LWR MATEL STRIP REPAIRED AS PER RI-54-51-15911 REV A) - [SDR P5CA2022092900186](https://openairdocs.org/sdr/P5CA2022092900186), Oct 16, 2022: STRAP. CRACKED. NO.1 PYLON TORQUE BOX I/B LWR MATAL STRIP FOUND CRACK (NO.1 PYLON TORQUE BOX I/B LOWER METAL STRIP REPAIRED AS PER RI-54-51-15909 REV A) - [SDR P5CA2022092900187](https://openairdocs.org/sdr/P5CA2022092900187), Oct 16, 2022: STRAP. CRACKED. NO.2 PYLON TORQUE BOX I/B LWR METAL STRIP FOUND CRACK (NO.2 PYLON TORQUE BOX I/B LOWER METAL STRIP REPAIRED AS PER RI-54-51-15910 REV B) - [SDR P5CA2022100900189](https://openairdocs.org/sdr/P5CA2022100900189), Oct 16, 2022: CHANNEL. CRACKED. EMP-RH HORI STAB TIP FAIRING ATTACHED U-CHANNEL FOUND CRACKED AFTER FAIRING REMOVED (REPAIRED U-CHANNEL AS PER RI NO.: RI-55 - 10 - 15887 REV.A) - [SDR P5CA2022101000190](https://openairdocs.org/sdr/P5CA2022101000190), Oct 16, 2022: SKIN. DAMAGED. #6 V/C FLAP LSA LAYER IN POOR CONDITION (REPAIRED AS PER CMM 57-55-42 REPAIR 17-1) All 110: https://openairdocs.org/aircraft/N853GT/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.