# N851GT: 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: 37565 - Year built: 2012 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 24, 2012 - Certificate issued: July 24, 2012 - Expires: July 31, 2028 - Mode S code: ABABB7 - 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=851GT - Page: https://openairdocs.org/aircraft/N851GT 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 N851GT. ## FAA accident and incident reports None matched to N851GT. ## Service difficulty reports (79, 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 UIEA2026091400877](https://openairdocs.org/sdr/UIEA2026091400877), Sep 14, 2026: OUTFLOW VALVE. FAULTED. AFTER LEVEL OFF AT 340, SLOWLY LOST CABIN PRESSURISATION TO APPROX 10,900. BOTH OUTFLOW VALVES VERIFIED CLOSED. DESCENDED AND RETURNED TO VCP. TRANSFER TO DMI 2 - [SDR UIEA2026082300786](https://openairdocs.org/sdr/UIEA2026082300786), Aug 22, 2026: TRANSCEIVER. INOPERATIVE. RIGHT HF INOPERATIVE. NO HF CAPABILITY, LT & RT UNABLE TO TRANSMIT. R & R HF ANTENNA COUPLER IAW AMM 23-11-03. R & R RT AND LT HF TRANSCIEVER IAW AMM 23-11-05/4 - [SDR UIEA2026052600351](https://openairdocs.org/sdr/UIEA2026052600351), May 23, 2026: SKIN. DAMAGED. LIGHTING STRIKE - SKIN, NOSE CARGO EXTERNAL SKIN NEAR STA 200, S-36R ~ S-39R. ACCOMPLISHED WORK SHEET NO 60306 (SRM 53-00-01-2R-9 REV 48) AND EI NO T2026A52M-96 - [SDR UIEA2026052600352](https://openairdocs.org/sdr/UIEA2026052600352), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 2180 S-10L FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60308 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK - [SDR UIEA2026052600353](https://openairdocs.org/sdr/UIEA2026052600353), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 2180 S-11L FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60309 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK - [SDR UIEA2026052600354](https://openairdocs.org/sdr/UIEA2026052600354), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR BS 2360 S-7R FWD SIDE. PERFORMED REPAIR IAW W/S 60302 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026052600355](https://openairdocs.org/sdr/UIEA2026052600355), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 1960 S-12R FWD AND AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60310 (SRM 53-60-03-2R-4 REV 48). JOB COMPLETED AND CONDITION - [SDR UIEA2026052600356](https://openairdocs.org/sdr/UIEA2026052600356), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR BS 2180 S-10R AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60294 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION CHECK NOR - [SDR UIEA2026052600357](https://openairdocs.org/sdr/UIEA2026052600357), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR BS 2180 S-12R FWD AND AFT SIDE. REPAIRED DAMAGE AREA IAW W/S #60307 (SRM 53-60-03-2R-3 REV 48). JOB COMPLETED AND CONDITION C - [SDR UIEA2026052600358](https://openairdocs.org/sdr/UIEA2026052600358), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 940 AND STA 960, S-9R. REPAIRED DAMAGE AREA IAW W/S 60297 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48. JOB COMPLETED AND C - [SDR UIEA2026052600359](https://openairdocs.org/sdr/UIEA2026052600359), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 980 +160 ~ 1000 S-11L. REPAIRED DAMAGE AREA IAW W/S 60298 AND SRM 53-20-03-2R-1 ALTERNATIVE 1 REV 48 AND EI #T2026A53M-97 - [SDR UIEA2026052600360](https://openairdocs.org/sdr/UIEA2026052600360), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 920 S-11R. REPAIRED DAMAGE AREA IAW W/S #60299 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48 AND EI #T2026A53M-973 REV 2. JO - [SDR UIEA2026052600361](https://openairdocs.org/sdr/UIEA2026052600361), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 980+160 ~ 1000 S-11R. REPAIRED DAMAGE AREA IAW W/S 60301 AND SRM 53-20-03-2R-1 ALTERNATIVE 2 REV 48 AND EI T2026A53M-973 - [SDR UIEA2026052600362](https://openairdocs.org/sdr/UIEA2026052600362), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 850 S-10L. REPAIRED DAMAGE AREA IAW W/S 60359 (SRM 53-20-03-2R-1 REV 48) AND EI T2026A53M-968 REV 1. JOB COMPLETED AND CO - [SDR UIEA2026052600363](https://openairdocs.org/sdr/UIEA2026052600363), May 23, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER NEAR STA 870 S-8L REPAIRED DAMAGE AREA IAW W/S 60356 (SRM 53-20-03-2R-1 REV 48) AND EI T2026A53M-971 REV 1. JOB COMPLETED AND COND - [SDR UIEA2026010600004](https://openairdocs.org/sdr/UIEA2026010600004), Jan 6, 2026: VALVE. DEFECTIVE. CABIN TEMP EXCESSIVE (38C) FOUND MAINT MSG 21304, FLIGHT DECK TRIM AIR VALVE DEFECTIVE. R & R F/D TRIM AIR VALVE AND OPS CHECK OK IAW AMM 21-61-10-401, AIPC 21- - [SDR UIEA2025031300281](https://openairdocs.org/sdr/UIEA2025031300281), Mar 13, 2025: PDU. FAULTED. FLAPS DRIVE CAUTION MSG.(

REMOVE & REPLACE #4 PDU FEEDBACK SWITCH ASSY PER AMM 27-88-01. REMOVED AND REPLACED #4L PDU PER AMM 27-81-03 APC 27-81-03-51. OP - [SDR UIEA2025011800085](https://openairdocs.org/sdr/UIEA2025011800085), Jan 18, 2025: OUTFLOW VALVE. FAILED. DURING CLIMB ON, THE CABIN WOULD NOT PRESSURIZE, STOPPED CLIMB AT 10,000, CAB ALT WAS 10300. DELTA P WAS 0.1 COULD NOT CONTROL THE CABIN PRESSURE IN MANUAL OR A - [SDR UIEA2024120601168](https://openairdocs.org/sdr/UIEA2024120601168), Dec 6, 2024: LINE. LOOSE. #1 ADP FAILED, LOSS OF HYDRAULIC FLUID. #1 EDP ON DEFERRAL PRIOR TO FLIGHT.(

R/R EDP PER AMM 29-11-05 & IPC 29-11-05-05, RETURN LINE FOUND LOOSE, LEADING - [SDR UIEA2024071800685](https://openairdocs.org/sdr/UIEA2024071800685), Jul 18, 2024: OUTFLOW VALVE. FAULTED. AIR TURN BACK UNABLE CRUISE ALTITUDE DUE TO PRESSURIZATION(

MIA MX PERFORMED INSPECTION OF EXTERIOR AND INTERIOR OF THE A/C, DOOR SEALS, A/C MANIFOLD DUCTING, - [SDR UIEA2024041300272](https://openairdocs.org/sdr/UIEA2024041300272), Apr 24, 2024: LAMP. INOPERATIVE. RH FUS EMER SLIDE LT L6690 FOUND NOT ILLUMINATED(

R/H FUS EMER SLIDE LT L6690 LAMP REPLACED AND TEST IS NORMAL AS PER AMM 33-51-00 REV 44 15 MAR 2024.

) - [SDR UIEA2024041700277](https://openairdocs.org/sdr/UIEA2024041700277), Apr 24, 2024: LAMP. INOPERATIVE. EMERGENCY LIGHT ON THE TOP OF STAIRWAY FOUND INOP.(

LAMP OF EMERGENCY LIGHT ON THE TOP OF STAIRWAY REPLACED AND OPERATIONAL TEST NORMAL IAW AMM 33-51-07 REV 4 - [SDR UIEA2024041700278](https://openairdocs.org/sdr/UIEA2024041700278), Apr 24, 2024: CURTAIN. TORN. AFT CARGO COMPT STA 2160 END WALL CURTAIN FOUND TORN.(

AFT CARGO COMPT STA 2160 ENDWALL CURTAIN REPAIRED AS PER RI-25-52-16836 REV A. NO FURTHER DEFECTS NOTED - [SDR UIEA2024041900279](https://openairdocs.org/sdr/UIEA2024041900279), Apr 24, 2024: CHANNEL. CRACKED. RH HORIZONTAL STAB T/E ASSY CHANNEL FOUND CRACK(

BONDED NEW CHANNEL AS PER RI-55-10-16833 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024041900280](https://openairdocs.org/sdr/UIEA2024041900280), Apr 24, 2024: SKIN. WORN. #9 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900281](https://openairdocs.org/sdr/UIEA2024041900281), Apr 24, 2024: SKIN. WORN. #7 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900282](https://openairdocs.org/sdr/UIEA2024041900282), Apr 24, 2024: SKIN. WORN. #8 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900283](https://openairdocs.org/sdr/UIEA2024041900283), Apr 24, 2024: SKIN. WORN. #18 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900284](https://openairdocs.org/sdr/UIEA2024041900284), Apr 24, 2024: SKIN. WORN. #20 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900285](https://openairdocs.org/sdr/UIEA2024041900285), Apr 24, 2024: SKIN. WORN. #19 V/C FLAP LSA FOUND WORN(

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

) - [SDR UIEA2024041900286](https://openairdocs.org/sdr/UIEA2024041900286), Apr 24, 2024: NUT. UNKNOWN. REFER JOB CARD SEQ 1.725 #1 CANOE AFT FRAME MOD FIG 6 INSTALLATION AFTER ROW HAS 5EA FASTENER HOLE LOCATION CAN NOT USE BACC30AC6 DUE HOLES TOO CLOSE TO ART INT - [SDR UIEA2024042000302](https://openairdocs.org/sdr/UIEA2024042000302), Apr 24, 2024: SKIN. ERODED. #10 V/C FLAP UPR EDGE FOUND EROSION(

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

) - [SDR UIEA2024042200303](https://openairdocs.org/sdr/UIEA2024042200303), Apr 24, 2024: BEAM. CRACKED. RHW L/E ILES 560 D BEAM WEB CRACKED(

RHW L/E ILES 560 D BEAM WEB REPAIRED AS PER RI-57-41-16827 REV A. NO FURTHER DEFECTS NOTED

) - [SDR UIEA2024042200304](https://openairdocs.org/sdr/UIEA2024042200304), Apr 24, 2024: INTERCOSTAL. DEFORMED. FUSELAGE - SECT 46 - WTB FAIRING INTERCOSTAL, P/N: 65B07241-1 BETWEEN STA 1480 +60 TO STA 1520 LBL 45. DEFORMATION DAMAGE - TEMPORARY REPAIR REFER EA-4853A0088( - [SDR P5CA2023070200034](https://openairdocs.org/sdr/P5CA2023070200034), Jun 30, 2023: BRACKET. UNKNOWN. FOUND THE GROUND PNEUMATIC DOOR GROUND SERVICE MISSING ON WALKAROUND(

FABRICATED THE BRACKET AS PER SERVICE REQUEST 270823140 AND DWG 69B11807 AND INSTALLED B - [SDR P5CA2023062900033](https://openairdocs.org/sdr/P5CA2023062900033), Jun 29, 2023: BRACKET. UNKNOWN. ENGINE START PNEUMATIC GROUND SERVICE DOOR MISSING.(

PERFORMED TIME LIMITED REPAIR PER EA-4852A0005 PART 1 (REV 0). FOLLOW UP REPAIR DUE NEXT F/C. PLACARD INS - [SDR P5CA2022032700106](https://openairdocs.org/sdr/P5CA2022032700106), Apr 1, 2022: NONE. NONE. L/H BLG I/B TRUNNION SUPPORT FITTING AND LOWER CAP FOUND CORROSION(

CORROSION AREA REPAIRED AS PER SRM 53-40-90-2R-1 REPAIR 1 AND HAECO RI NO. RI-53-40-15465 - [SDR P5CA2022032100093](https://openairdocs.org/sdr/P5CA2022032100093), Apr 1, 2022: NONE. NONE. LHW L/E #6 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100094](https://openairdocs.org/sdr/P5CA2022032100094), Apr 1, 2022: NONE. NONE. LHW L/E #7 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100095](https://openairdocs.org/sdr/P5CA2022032100095), Apr 1, 2022: NONE. NONE. LHW L/E #8 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032100096](https://openairdocs.org/sdr/P5CA2022032100096), Apr 1, 2022: NONE. NONE. LHW L/E #9 VC FLAP EXTERIOR LSA FOUND POOR CONDITION(

LSA DAMAGED AREA PERFORMED REPAIR

) - [SDR P5CA2022032300097](https://openairdocs.org/sdr/P5CA2022032300097), Apr 1, 2022: NONE. NONE. R/H H-STAB STA BL 421.5 LOWER CHORD CRACKED(

LOWER CHORD CRACK AREA REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12,FIG.201,DETAIL VII

) - [SDR P5CA2022032400098](https://openairdocs.org/sdr/P5CA2022032400098), Apr 1, 2022: NONE. NONE. #2 V/C FLAP BULLNOSE EDGE FOUND EROSION(

PERFORMED REPAIR AT ERODED AREA

) - [SDR P5CA2022032500099](https://openairdocs.org/sdr/P5CA2022032500099), Apr 1, 2022: NONE. NONE. VERTICAL FIN FWD L/E FAIRING #321B FOUND DENT MARK(

DENT AREA REPAIRED AS PER SRM 55-30-01-2R-4 REPAIR 4 FIG.201

) - [SDR P5CA2022032600100](https://openairdocs.org/sdr/P5CA2022032600100), Apr 1, 2022: NONE. NONE. LH H.STAB REAR WEB AT STA BL 391.9 ANGLE CRACKED.(

CRACK ANGLE LOCAL FABRICATED AS PER RI NO. RI-55-00-15458 REV A AND NEW ANLGE INSTALLED AS PER SRM 51-40-02 - [SDR P5CA2022032600101](https://openairdocs.org/sdr/P5CA2022032600101), Apr 1, 2022: NONE. NONE. R/H H.STAB BL 421.5 UPPER CHORD CRACKED.(

R/H H.STAB BL 421.5 UPPER CHORD REPLACED ACCOMPLISHED IAW SRM 51-40-02 AND SRM 51-40-05 REV 36, 20 FEB 2022 

CRACK WEB REPLACED AS PER SRM 51-10-02 AND NEW WEB INSTALLED AS PER SRM 51-40-02

) - [SDR P5CA2022032600103](https://openairdocs.org/sdr/P5CA2022032600103), Apr 1, 2022: NONE. NONE. L/H STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(

LH STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U11 WAS REPLACED AS PER RI NO. RI-55-10-15472 REV A AND INSTA - [SDR P5CA2022032600104](https://openairdocs.org/sdr/P5CA2022032600104), Apr 1, 2022: NONE. NONE. RH H.STAB TIP FAIRING ATTACH U-CHANNEL CRACKED.(

RH H.STAB TIP FAIRING ATTACH U-CHANNEL P/N 65B03822U12 WAS REPLACED AS PER RI NO. RI-55-10-15473 REV A AND IN - [SDR P5CA2022032700105](https://openairdocs.org/sdr/P5CA2022032700105), Apr 1, 2022: NONE. NONE. LHW I/B T/E LWR PNL AT WS 129.86 TO 228.05 FWD SUPPORT BEAM O/B BRACKET CRACKED(

SUPPORT BEAM FITTING P/N : 115U2252-19 FASBRICATED AS PER RI NO.RI-57-00-1547 All 79: https://openairdocs.org/aircraft/N851GT/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.