- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 67147
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 26, 2022
- Certificate issued
- May 27, 2022
- Expires
- May 31, 2029
- Mode S code
- ABCF7F
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 56
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1990 | 1 |
|---|---|
| 2013 | 4 |
| 2014 | 4 |
| 2015 | 5 |
| 2016 | 2 |
| 2017 | 3 |
| 2018 | 3 |
| 2019 | 4 |
| 2020 | 5 |
| 2021 | 5 |
| 2022 | 7 |
| 2023 | 9 |
| 2024 | 1 |
| 2025 | 6 |
| 2026 | 5 |
See all 64 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Boeing 747-8F
SAIB NM-20-07Navigation - Glideslope SystemSAIB NM-18-33Engine Fuel and ControlSAIB NM-17-10Maintenance PracticesSAIB NM-15-03Flight ControlsSAIB NM-15-02Cabin Equipment/FurnishingsSAIB NM-14-20Equipment/Furnishings: Cargo CompartmentsSAIB NM-13-02Air Conditioning: Air Distribution SystemNTSB investigations
No NTSB investigations matched to N860GTMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Boeing 747-8F aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR UIEA2026041700203Skin · damagedLEFT WING #6 L/E V/C FLAP EXTERIOR SURFACE LSA SEVERAL AREAS FOUND CHIPPED. LT WING #6 L/E V/C FLAP LSA DAMAGED AREAS REPAIRED IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026041700204Skin · damagedLEFT WING #7 L/E V/C FLAP EXTERIOR SURFACE LSA SEVERAL AREAS FOUND CHIPPED. LT WING #7 L/E V/C FLAP LSA DAMAGED AREAS REPAIRED IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026041700205Skin · damagedLEFT WING #9 L/E V/C FLAP EXTERIOR SURFACE LSA SEVERAL AREAS FOUND CHIPPED. LT WING #9 L/E V/C FLAP LSA DAMAGED AREAS REPAIRED IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026041700206Skin · damagedRIGHT WING 19 L/E V/C FLAP EXTERIOR SURFACE LSA SEVERAL AREAS FOUND CHIPPED. RT WING #19 L/E V/C FLAP LSA DAMAGED AREAS REPAIRED IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026041700207Skin · damagedRIGHT WING NR 21 L/E V/C FLAP EXTERIOR SURFACE LSA SEVERAL AREAS FOUND CHIPPED. RT WING #21 L/E V/C FLAP LSA DAMAGED AREAS REPAIRED IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.SDR UIEA2026041800213Rib · crackedRIGHT INBD ELEVATOR MOST INBD UPPER SUPPORT BRACKET CRACK FOUND. HSS 56.59 & 55.813. RT INBD ELEVATOR MOST INBD UPPER SUPPORT BRACKET (PN 65B05842-10) AND STIFFENER (PN 65B05701-56) REPLACED IAW SRM 51-10-02, REV 48 & SRM 51-40-02, REV 48. NO FURTHER DEFECTSSDR UIEA2026041800215Rib · crackedLEFT INBD ELEVATOR MOST INBD UPPER SUPPORT BRACKET CRACK FOUND. LT INBD ELEVATOR MOST INBD UPPER SUPPORT BRACKET (PN 65B05842-9). REPLACED IAW SRM 51-10-02 REV 48 & SRM 51-40-02 REV 48. NO FURTHER DEFECTS NOTED.SDR UIEA2026042100227Channel · crackedRIGHT HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT WEDGE U-CHANNEL FOUND CRACK. RT HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT WEDGE U-CHANNEL REPLACED IAW RI-55-10-18247 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026042100228Channel · crackedEMP - L/H HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT WEDGE U-CHANNEL FOUND CRACK.(<P>EMP - L/H HORIZONTAL STABILIZER TIP FAIRING AFT SUPPORT WEDGE U-CHANNEL REPLACED IAW RI-55-10-18248 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042100231Web · chafedRIGHT HORIZONTAL STABILIZER T/E MOST I/B WEB AFT FACE FOUND CHAFING. R/H HORIZONTAL STABILIZER T/E MOST I/B WEB AFT FACE. CHAFING AREA REPAIRED IAW RI-55-10-18255 REV.A. NO FURTHER DEFECTS NOTED.SDR UIEA2024100600966A/C Pack · warning messageIN FLIGHT AT FL 360 RECEIVED A PACK 3 CAUTION MSG. RESET PACK PER CHECKLIST AFTER 90 SECONDS RECEIVED PACK 3 MSG AGAIN.(<P>CMC MSG - 21962 33 PACK INOP. RESET PACK 2 IAW AMM 21-51-00-740-802, OPS CHECK GOOD. TRANSFER PACK 3 TO DMI 218252 IAW MEL 21-51-01-01-SDR UIEA2024052800461Skin · debondedDISBOND-SKIN, L/H WING #13 KRUEGER FLAP EXTERNAL SURFACE, WS 353 TO WS 382 AREA.(<P>1. PERFORM PERMANEN REPAIR AT L/H WING #13 KRUEGER FLAP EXTERNAL SURFACE. PLEASE REFER TO THE JOB CARD ATTACHING SHEET #0430722 FOR DETAILED REWORK INFORMATION AND REFER TO EGASDR UIEA2024052800462Skin · damagedLIGHTNING STRIKE - SKIN, NOSE CARGO DOOR FREIGHTER L/H EXTERNAL SKIN, STA 140~ STA 160, WL 205 2 EA, STA 179 S-24AL 1 EA(<P>1. PERFORMED EI T2024A52M-1254 SEQUENCE A. REV 0, W/S 40409 (SRM 53-00-01-2R-9 REV 42) AND DWG 65B20288 SH 1 REV A 2. ACCOMPLISHED EI T2SDR UIEA2023011200016Tcas System · failedDUAL TCAS SYSTEM FAILURE AT CRUISE. CAN'T ENTER CHINESE AIRSPACE WITHOUT TCAS. AIR RETURN TO ICN. R & R RT CMC & OPS & SYS TEST OK IAW AMM 45-10-00/501. PERFORMED TCAS OPS & TCAS INTERFACE TEST, TEST OK IAW AMM 34-45-00/501.
STCs that may be installed · 113
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.