# N857GT: 2011 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: 37568
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 27, 2014
- Certificate issued: October 27, 2021
- Expires: October 31, 2028
- Mode S code: ABC201
- 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=857GT
- Page: https://openairdocs.org/aircraft/N857GT

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 N857GT.

## FAA accident and incident reports

None matched to N857GT.

## Service difficulty reports (97, 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 P5CA2026082100029](https://openairdocs.org/sdr/P5CA2026082100029), Aug 21, 2026: TIRE. WARNING MESSAGE. IN CRUISE FLIGHT, TIRE PRESSURE EICAS MSG. GAUGE SYNOPTIC INDICATED TIRE 14 WAS AT 180 PSI AND CONTINUED TO DROP. R & R NR 14 MWA IAW AMM 32-45-01. VERIFIED SPA
- [SDR P5CA2026070600024](https://openairdocs.org/sdr/P5CA2026070600024), Jul 4, 2026: SENSOR. FAULTED. FLAPS DRIVE MSG IMMEDIATELY AFTER ROTATION BELOW 300 FT. REMOVED AND REPLACED FLAP SKEW SENSOR AND RE-SECURED CONNECTOR D25635J. OPS CHECK GOOD IAW AMM 27-51-01
- [SDR P5CA2025080500033](https://openairdocs.org/sdr/P5CA2025080500033), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 884, S7L.. ACCOMPLISHED WORK SHEET 50507 IAW SRM 53-20-03-2R-1, REV 46 TO REPAIR DAMAGED STRINGER. CONDITION CHECKED NORMAL AND JOB
- [SDR P5CA2025080500034](https://openairdocs.org/sdr/P5CA2025080500034), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 977, S10L. REPAIRED THE STRINGER CRACK IAW W/S 50514, AND SRM 53-20-03-2R-1 REV 46. CONDITION CHECKED NORMAL AND JOB COMPLETED.
- [SDR P5CA2025080500035](https://openairdocs.org/sdr/P5CA2025080500035), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 957, S10L. REPAIRED THE STRINGER CRACK IAW W/S 50536, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080500036](https://openairdocs.org/sdr/P5CA2025080500036), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 957, S8L. REPAIRED THE STRINGER CRACK IAW W/S 50513, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080500037](https://openairdocs.org/sdr/P5CA2025080500037), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 877, S8R. ACCOMPLISHED WORK SHEET 50502, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080500038](https://openairdocs.org/sdr/P5CA2025080500038), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 841, S7R. ACCOMPLISHED WORK SHEET 50499, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080500039](https://openairdocs.org/sdr/P5CA2025080500039), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 798, S13R. PERFORMED EI T2025A53M-1533, REV 0. ACCOMPLISHED EI T2025A53M-1533, REV 1. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080500040](https://openairdocs.org/sdr/P5CA2025080500040), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 2180-2188, S11R. REPAIR SPLICE FOR CRACKED STRINGER IAW W/S 50498, AND SRM 53-60-03-2R-3 REV 46, TR 53-154. CONDITION CHECKED NORMA
- [SDR P5CA2025080500041](https://openairdocs.org/sdr/P5CA2025080500041), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 922, S9L. ACCOMPLISHED WORK SHEET 50511, AND SRM 53-20-03-2R-1, REV 46, AND WORK SHEET ATTACHED TO W/O 11244309. JOB COMPLETED, AND
- [SDR P5CA2025080600042](https://openairdocs.org/sdr/P5CA2025080600042), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 884, S9L. ACCOMPLISHED WORK SHEET 50509, AND SRM 53-20-03-2R-1, REV 46, AND WORK SHEET ATTACHED TO W/O 11244332. JOB COMPLETED AND 
- [SDR P5CA2025080600043](https://openairdocs.org/sdr/P5CA2025080600043), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 878, S9L. ACCOMPLISHED WORK SHEET 50509, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080600044](https://openairdocs.org/sdr/P5CA2025080600044), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 938, S9L. ACCOMPLISHED WORK SHEET 50512, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080600045](https://openairdocs.org/sdr/P5CA2025080600045), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 903, S9L. ACCOMPLISHED WORK SHEET 50510, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600046](https://openairdocs.org/sdr/P5CA2025080600046), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 914 - 917, S9L. ACCOMPLISHED WORK SHEET 50511, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMAL.
- [SDR P5CA2025080600047](https://openairdocs.org/sdr/P5CA2025080600047), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 878, S10R. ACCOMPLISHED WORK SHEET 50503, AND SRM 53-20-03-2R-1, REV 46. CONDITION CHECKED NORMAL AND JOB COMPLETED.
- [SDR P5CA2025080600048](https://openairdocs.org/sdr/P5CA2025080600048), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 876, S10L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50526, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMA
- [SDR P5CA2025080600049](https://openairdocs.org/sdr/P5CA2025080600049), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 865, S10L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50525, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECKED NORMA
- [SDR P5CA2025080600050](https://openairdocs.org/sdr/P5CA2025080600050), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 882-888, S8L. REPAIR THE STRINGER CRACK IAW W/S 50508, AND SRM 53-20-03-2R-1 REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600051](https://openairdocs.org/sdr/P5CA2025080600051), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 894-897, S8L. REPAIR THE STRINGER CRACK IAW WORK SHEET 50524 AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMA
- [SDR P5CA2025080600052](https://openairdocs.org/sdr/P5CA2025080600052), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 941, S8R. ACCOMPLISHED WORK SHEET W/S 50505 IAW SRM 53-20-03-2R-1, REV 46. CONDITION CHECK NORMAL AND JOB COMPLETED.
- [SDR P5CA2025080600053](https://openairdocs.org/sdr/P5CA2025080600053), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 878, S7R. ACCOMPLISH WORK SHEET 50500 AND SRM 53-20-03-2R-1, REV 46. WORK SHEET ATTACHED TO W/O #11244355. NO FURTHER DEFECTS NOTED
- [SDR P5CA2025080600054](https://openairdocs.org/sdr/P5CA2025080600054), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 883, S7R. ACCOMPLISH WORK SHEET 50500 AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600055](https://openairdocs.org/sdr/P5CA2025080600055), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 970, S7R. REPAIRED THE STRINGER IAW WORK SHEET 50515, AND SRM 53-20-03-2R-1, REV 46. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600056](https://openairdocs.org/sdr/P5CA2025080600056), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 918, S10R. ACCOMPLISHED EI T2025A53M-1577, SEQUENCE A, REV 0 IAW SRM 53-20-03, REPAIR 1, REV 46. ACCOMPLISHED EI T2025A53M-1392, RE
- [SDR P5CA2025080600057](https://openairdocs.org/sdr/P5CA2025080600057), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACK AT BS 958, S7L. ACCOMPLISHED EI #T2025A53M-1566, SEQUENCE A, REV 0. ACCOMPLISHED EI T2025A53M-1566 REV 1. JOB COMPLETED AND CONDITION CHECK
- [SDR P5CA2025080600058](https://openairdocs.org/sdr/P5CA2025080600058), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 963, S7L. ACCOMPLISHED EI T2025A53M-1566, SEQUENCE A, REV 1, AND EI ATTACHED TO W/O 11234472. JOB COMPLETED AND CONDITION CHECK NOR
- [SDR P5CA2025080600059](https://openairdocs.org/sdr/P5CA2025080600059), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACK AT STA 957, S-7R. ACCOMPLISHED EI T2025A53M-1569, SEQUENCE A, REV 0, IAW SRM 53-20-03 REPAIR 1, REV 46. ACCOMPLISHED EI #T2025A53M-1569, RE
- [SDR P5CA2025080600060](https://openairdocs.org/sdr/P5CA2025080600060), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACK AT BS 944, S7R. ACCOMPLISHED EI T2025A53M-1569, SEQUENCE A, REV 1, AND EI ATTACHED TO W/O #11244350. 2. JOB COMPLETED AND CONDITION CHECK N
- [SDR P5CA2025080600061](https://openairdocs.org/sdr/P5CA2025080600061), Aug 7, 2025: STRINGER. CRACKED. FOUND STRINGER CRACKED AT BS 763, S8L. REPAIR THE DAMAGE AREA IAW EI T2025A53M-1575, REV 0, AND SRM 53-20-03, REPAIR 1, REV 46. ACCOMPLISHED EI T2025A53M-1575, 
- [SDR P5CA2025080600062](https://openairdocs.org/sdr/P5CA2025080600062), Aug 7, 2025: SKIN. DENTED. PERMANENT REPAIR OF SCRATCH AND DENT ON FUSELAGE SECTION 46 SKIN COMMON TO LAP AND BUTT SPLICE AT STA 1740 AND S-46L REQUIRED PER PART 3 OF EO 4853A132 BEFORE 1
- [SDR P5CA2025080600063](https://openairdocs.org/sdr/P5CA2025080600063), Aug 7, 2025: BATTERY. NO TEST. FOUND M5168 EMERGENCY POWER COULD NOT STAY MORE THAN 15 MINS IAW AMM 33-51-04-900-803, REV 47. REPLACED POWER SUPPLY BATTERY (M5168) AT UPPER DECK, THE CONDITIO
- [SDR P5CA2025080600064](https://openairdocs.org/sdr/P5CA2025080600064), Aug 7, 2025: BATTERY PACK. NO TEST. FOUND M5170 EMERGENCY POWER FUNCTION. IAW AMM 33-51-04-000-803 & 33-51-04-900-803 & 33-51-04-400-803 REV 48. REPLACED BATTERY ASSY (M5170) AT UPPER DECK AREA, T
- [SDR P5CA2025010200001](https://openairdocs.org/sdr/P5CA2025010200001), Jan 3, 2025: PANEL. PUNCTURED. FUSELAGE - SEC 46 LOWER AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED NEAR STA 1540 TO 1560.(<P>FUSELAGE - SEC 46 STA 1540-1560 RBL 45" TO RBL 55" LOWER 
- [SDR P5CA2024121600050](https://openairdocs.org/sdr/P5CA2024121600050), Dec 16, 2024: PCB. FAULTED. MASTER WARNING LIGHTS (RED) AND BELL WERE ACTIVATING EVERY 90 SECONDS WITH NO EICAS OR OTHER RED LIGHTS ILLUMINATING.(<P>REMOVED AND REPLACED MASTER MONITOR A &
- [SDR P5CA2024093000047](https://openairdocs.org/sdr/P5CA2024093000047), Sep 30, 2024: SEAT. MALFUNCTIONED. CAPTAIN SEAT, UNABLE TO LOCK IN ANY FWD/AFT DETENT (SEE 1857990)(<P>CAPT SEAT FWD &AMP; AFT MANUAL CONTROL CABLE BROKEN. R/R CAPT SEAT ASSY &AMP; OPS TEST GOOD 
- [SDR P5CA2024032300006](https://openairdocs.org/sdr/P5CA2024032300006), Mar 21, 2024: ACTUATOR. BROKEN. BODY GEAR STEERING EICAS MESSAGE. RTO AT LOW SPEED(<P>PERFORMED DVI OF R/H BODY GEAR AND FOUND R/H BODY GEAR, R/H ACTUATOR BROKEN. PERFORMED CONDITIONAL INSPECT
- [SDR P5CA2023072200037](https://openairdocs.org/sdr/P5CA2023072200037), Aug 18, 2023: UNKNOWN. UNKNOWN. REFER EO 1957A593 PART 1 SB 747-57-2369 REV 1 NO.1 FLAP TRACK ACTUATOR FRAME EXISTING REPAIR MODIFICATION(<P>ACTUATOR FRAME MODIFICATION CARRIED OUT AS PER ATLA
- [SDR P5CA2023072200038](https://openairdocs.org/sdr/P5CA2023072200038), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW NO. 1E VC FLAP FWD BULKHEAD FOUND DEFORMED ( FWD L/E D BEAM AFT B/HEAD WEB STIFFENER DEFORMED )(<P>B/HEAD STIFFENER DEFORM AREA REPAIRED AS PER RI NO. RI-57
- [SDR P5CA2023072200039](https://openairdocs.org/sdr/P5CA2023072200039), Aug 18, 2023: UNKNOWN. UNKNOWN. RHW FIXED L/E D BEAM AFT B/HEAD FOUND BROKEN(<P>B/HEAD BROKEN AREA REPAIRED AS PER RI NO : RI-57-41-16382 REV A</P>)
- [SDR P5CA2023072200040](https://openairdocs.org/sdr/P5CA2023072200040), Aug 18, 2023: STIFFENER. UNKNOWN. RHW WING FRONT SPAR ILES 487 ( AFT OF 14 K / FLAP ) STIFFENER FOUND CRACK(<P>CRACK STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED AS PE
- [SDR P5CA2023072200041](https://openairdocs.org/sdr/P5CA2023072200041), Aug 18, 2023: STIFFENER. UNKNOWN. LHW L/E FRONT SPAR ILES 470 ( AFT OF 12 K/FLAP ) STIFFENER LWR FOUND BROKEN.(<P>BROKEN STIFFENER REPLACED AS PER SRM 51-10-02, NEW STIFFENER HOLES TRANSFERRED A
- [SDR P5CA2023072200042](https://openairdocs.org/sdr/P5CA2023072200042), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW L/E CAVITY ILES 540 D BEAM AFT BULKHEAD FOUND CRACK(<P>B/HEAD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-16383 REV A</P>)
- [SDR P5CA2023072200043](https://openairdocs.org/sdr/P5CA2023072200043), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW WING TIP I/B UPPER AFT EDGE STRAP FOUND BURN MARK(<P>BURN MARK AREA REPAIRED AS PER RI NO: RI-57-30-16423 REV A</P>)
- [SDR P5CA2023072200044](https://openairdocs.org/sdr/P5CA2023072200044), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW I/B L/E ILES 410 'V' SUPPORT ROD UPPER ATT. BRACKET FOUND ELONGATED ( NO.5 AND 6 ).(<P>NO.6 BRACE UPPER (2EA) FASTENER HOLES AND UPPER ATT BRACKET O/B (2EA)
- [SDR P5CA2023072200045](https://openairdocs.org/sdr/P5CA2023072200045), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW FIXED L/E OLES 530 'D' BEAM FOUND CRACK(<P>D BEAM B/HEAD CRACK AREA REPAIRED AS PER RI NO: RI-57-41-16369 REV A</P>)
- [SDR P5CA2023072200046](https://openairdocs.org/sdr/P5CA2023072200046), Aug 18, 2023: UNKNOWN. UNKNOWN. LHW L/E D BEAM FWD EXTERNAL SKIN FOUND DENT ( AFT OF NO.6 V/C FLAP )(<P>SKIN DENT ARAE REPAIRED AS PER RI NO : RI-57-41-16394 REV A</P>)
- [SDR P5CA2023072200047](https://openairdocs.org/sdr/P5CA2023072200047), Aug 18, 2023: SUPPORT WEB. UNKNOWN. LH HORI STAB ACCESS PANEL 334QB O/B SUPPORT WED FOUND CRACK(<P>SUPPORT WEB REPLACEMENT AS PER SRM 51-10-02, NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NE
- [SDR P5CA2023072200048](https://openairdocs.org/sdr/P5CA2023072200048), Aug 18, 2023: UNKNOWN. UNKNOWN. LH HORI STAB ACCESS PANEL 334QB O/B SUPPORT RIB LWR CHORD FOUND CRACK(<P>LOWER CHORD REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 FIG 201 REV 40 DATE 20 JUN 202

All 97: https://openairdocs.org/aircraft/N857GT/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

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