# Service difficulty reports: N857GT

A list on [N857GT](https://openairdocs.org/aircraft/N857GT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 97 reports

- [SDR P5CA2026082100029](https://openairdocs.org/sdr/P5CA2026082100029.md): Tire · warning message · Aug 21, 2026 · N857GT · Boeing 74787UF · Tire
  > 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 SPACER INSTALLED. OPS & LK CHKD OK.
- [SDR P5CA2026070600024](https://openairdocs.org/sdr/P5CA2026070600024.md): Sensor · faulted · Jul 4, 2026 · N857GT · Boeing 74787UF · Trailing Flap Position Indicating System
  > 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, AIRCRAFT OK FOR SERVICE.
- [SDR P5CA2025080500033](https://openairdocs.org/sdr/P5CA2025080500033.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 COMPLETED.
- [SDR P5CA2025080500034](https://openairdocs.org/sdr/P5CA2025080500034.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL AND JOB COMPLETED.
- [SDR P5CA2025080500041](https://openairdocs.org/sdr/P5CA2025080500041.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 CONDITION CHECKED NORMAL.
- [SDR P5CA2025080600042](https://openairdocs.org/sdr/P5CA2025080600042.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 CONDITION CHECKED NORMAL.
- [SDR P5CA2025080600043](https://openairdocs.org/sdr/P5CA2025080600043.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL.
- [SDR P5CA2025080600049](https://openairdocs.org/sdr/P5CA2025080600049.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL.
- [SDR P5CA2025080600050](https://openairdocs.org/sdr/P5CA2025080600050.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL.
- [SDR P5CA2025080600052](https://openairdocs.org/sdr/P5CA2025080600052.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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, REV 0. ACCOMPLISHED EI #T2025A53M-1577 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600057](https://openairdocs.org/sdr/P5CA2025080600057.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL.
- [SDR P5CA2025080600058](https://openairdocs.org/sdr/P5CA2025080600058.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL.
- [SDR P5CA2025080600059](https://openairdocs.org/sdr/P5CA2025080600059.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600060](https://openairdocs.org/sdr/P5CA2025080600060.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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 NORMAL
- [SDR P5CA2025080600061](https://openairdocs.org/sdr/P5CA2025080600061.md): Stringer · cracked · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Longeron/Stringer
  > 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, REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR P5CA2025080600062](https://openairdocs.org/sdr/P5CA2025080600062.md): Skin · dented · Aug 7, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Plate/Skin
  > 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 10000 FC. ACCOMPLISHED EI #T2025A53M-1615, REV 1 FOR UPGRADE FUSELAGE SKIN TIME-LIMITED REPAIR. A
- [SDR P5CA2025080600063](https://openairdocs.org/sdr/P5CA2025080600063.md): Battery · no test · Aug 7, 2025 · N857GT · Boeing 74787UF · Emergency Lighting
  > 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 CONDITION CHECK NORMAL IAW AMM 33-51-04-900-803 REV 47. PERFORMED INSTALLATION TEST OF (M5168) POWER SUP
- [SDR P5CA2025080600064](https://openairdocs.org/sdr/P5CA2025080600064.md): Battery Pack · no test · Aug 7, 2025 · N857GT · Boeing 74787UF · Emergency Lighting
  > 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, THE CONDITION CHECK NORMAL IAW AMM 33-51-04-900-803 & 33-51-04-400-803 REV 48. PERFORMED INSTALLAT
- [SDR P5CA2025010200001](https://openairdocs.org/sdr/P5CA2025010200001.md): Panel · punctured · Jan 3, 2025 · N857GT · Boeing 74787UF · Fuselage Main, Bulkhead
  > 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 AFT CARGO COMPARTMENT FLOOR PANEL PUNCTURE - DAMAGED AREA REPAIRED IAW RI-53-12-17630 REV.A </P>)
- [SDR P5CA2024121600050](https://openairdocs.org/sdr/P5CA2024121600050.md): Pcb · faulted · Dec 16, 2024 · N857GT · Boeing 74787UF · Fire Detection
  > 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 & MAWEA PCC IAW B747 AMM 31-51-02. OPS CHECK GOOD. PART EFFECTIVITY VERIFIED PER IPC 31-51-02-01.</P>
- [SDR P5CA2024093000047](https://openairdocs.org/sdr/P5CA2024093000047.md): Seat · malfunctioned · Sep 30, 2024 · N857GT · Boeing 74787UF · Flight Compartment Equipment
  > CAPTAIN SEAT, UNABLE TO LOCK IN ANY FWD/AFT DETENT (SEE 1857990)(<P>CAPT SEAT FWD & AFT MANUAL CONTROL CABLE BROKEN. R/R CAPT SEAT ASSY & OPS TEST GOOD IAW AMM 25-11-01/401 & IPC 25-11-01-10</P>)
- [SDR P5CA2024032300006](https://openairdocs.org/sdr/P5CA2024032300006.md): Actuator · broken · Mar 21, 2024 · N857GT · Boeing 74787UF · Landing Gear Steering System
  > 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 INSPECTION PER AMM 05-41-07. NO FURTHER DAMAGE NOTED. </P>)
- [SDR P5CA2023072200037](https://openairdocs.org/sdr/P5CA2023072200037.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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 ATLAS AIR EO 1957A593 REV 3 PART 1 AND REPAIRED AS PER RI NO: RI-57-50-16381 REV A</P>)
- [SDR P5CA2023072200038](https://openairdocs.org/sdr/P5CA2023072200038.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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-57-41-16375 REV A</P>)
- [SDR P5CA2023072200039](https://openairdocs.org/sdr/P5CA2023072200039.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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.md): Stiffener · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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 PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( REV 40 DATE 2 JUN 2023)</P>)
- [SDR P5CA2023072200041](https://openairdocs.org/sdr/P5CA2023072200041.md): Stiffener · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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 AS PER SRM 51-40-05 AND NEW STIFFENER INSTALLED AS PER SRM 51-40-02 ( SRM REV 40 DATE 20 JUN 2023)</
- [SDR P5CA2023072200042](https://openairdocs.org/sdr/P5CA2023072200042.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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) FASTENER HOLES REPAIRED AS PER RI NO: RI-57-41-16380 REV A</P>)
- [SDR P5CA2023072200045](https://openairdocs.org/sdr/P5CA2023072200045.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Wing Structure
  > 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.md): Support Web · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure
  > 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 NEW WEB INSTALLED AS PER SRM 51-40-02 ( SRM REV 40, DATE 20 JUN 2023)</P>)
- [SDR P5CA2023072200048](https://openairdocs.org/sdr/P5CA2023072200048.md): Unknown · unknown · Aug 18, 2023 · N857GT · Boeing 74787UF · Horizontal Stabilizer Miscellaneous Structure
  > 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 2023</P>)

Next page: https://openairdocs.org/aircraft/N857GT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N857GT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N857GT/reports

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