N864GT
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
23 reports on file, 2025-06-07 – 2026-08-12.
Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 35,411 hrs · 6,203 cycles
CPTS FLASHLIGHT INOPERATIVE. TRANSFER TO DMI 257381 PER MEL 25-60-03-01 CAT C DUE DATE 22AUG26.
Part: SKIN — CRACKED (ZONE 300) · airframe 34,501 hrs · 6,074 cycles
FOUND OTBD ELEVATOR FRONT SPAR LE SKIN CRACKED AT RT L/E HSS 260. ACCOMPLISHED EO 1955A064 REV 1.& 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: SPAR — DAMAGED (ZONE 300) · airframe 34,501 hrs · 6,074 cycles
FOUND OTBD ELEVATOR FRONT SPAR INNER CHORD DAMAGE AT RT LE HSS 314 AND WEB ORIGINAL REPAIR.. ACCOMPLISHED EO 1955A064 REV 1 & 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: SPAR — DAMAGED (ZONE 300) · airframe 34,501 hrs · 6,074 cycles
FOUND OTBD ELEVATOR FRONT SPAR INNER CHORD DAMAGE AT LT LE HSS 231. ACCOMPLISHED EO 1955A065 PART 1 REV 0 AND DWG 65B05731 SH 8 REV A, SH 9 REV A AND EI T2026A55M-1044 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 34,501 hrs · 6,074 cycles
CRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP. REPAIRED CRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP IAW EGAT EI T2026A57M-1011 REV 1. 2. CONDITION CHECK IS SATISFACTORY.
Part: STRINGER — CRACKED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-25R BS 2598 AFT SIDE. REPAIRED IAW EI T2026A53M-1037 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGE ON THE STRINGER S-42L STA 2598 AFT SIDE. PERFORMED REPAIR IAW W/S 60361 (SRM 53-80-03-2R-1 REV 48) AND EI T2026A53M-1093 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: SKIN — DENTED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
DENT ON FUSELAGE AT BS 640, STRINGER 43R - 44R WITHIN SRM LIMITS, ACCOMPLISHED EI T2026A53M-1074 REV 1 AND SRM 53-00-01-2R-10 REPAIR 10 REV 48. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGE ON THE STRINGER S-16R STA 2360 FWD SIDE. PERFORMED REPAIR IAW EI T2026A53M-1042 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGE ON THE STRINGER S-44L STA 2360 FWD SIDE. REPAIRED DAMAGED AREA IAW W/S 60395 (SRM 53-60-03-2R-8 REV 48) AND EI T2026A53M-1112 REV 0. JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGE ON THE STRINGER S-38L STA 2360 FWD SIDE. PERFORMED REPAIR IAW W/S 60394 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-1R STA 2360 FWD SIDE.(<P>1. PERFORMED REPAIR IAW W/S 60391 (SRM 53-60-03-2R-8 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-10R STA 2180 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60416 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-9R STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60418 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-12L STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60417 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-10R STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60419 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-7R STA 2360 FWD SIDE. PERFORMED REPAIR IAW W/S 60392 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-12L STA 2180 FWD AND AFT SIDE AND SPLICE CRACK. PERFORMED REPAIR IAW W/S 60370 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-12R STA 2180 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60371 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-20L STA 2360 AFT SIDE.(<P>1. PERFORMED REPAIR IAW W/S 60374 (SRM 53-80-03-2R-3 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: STRINGER — CRACKED (ZONE 200) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-21R STA 2360 AFT SIDE.(<P>1. PERFORMED REPAIR IAW W/S 60375 (SRM 53-80-03-2R-3 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Part: STRINGER — CRACKED (ZONE 100) · airframe 34,501 hrs · 6,074 cycles
CRACK DAMAGED ON THE STRINGER S-46R STA 2360 FWD SIDE.(<P>1. PERFORMED REPAIR IAW W/S 60393 (SRM 53-60-03-2R-8 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)
Earlier reports · 2025 · 1 report
2025
Part: ENGINE — FAILED (NR 3) · airframe 30,419 hrs · 5,489 cycles
ENGINE 3 FAILURE ON TAKEOFF ROLL AT 110 KNOTS REJECTED TAKEOFF AND CLEARED RUNWAY. NR 3 ENG BORESCOPE INSPECTION PERFORMED IAW AMM 72-00-00-290-801-G00, FOUND HPC STAGE 7 & 8, 9 WHOLE STAGE SERIOUS DAMAGE, BORE PLUG INSTALLED IAW AMM 72-00-00/601. FOUND DAMAGE OUT OF LIMITS. ENGINE 3 N2 LOCKED OUT FOR FERRY FLIGHT AS PER AMM 70-00-30/201. LP 1977855 - M13-M15 - ICN - 20JUN25: REPLACED NO.3 ENGINE AND OPERATION TEST AND LEAK CHECK NORMAL WORK CARD B-72-099-00-01 IPC 71-00-10-01 ITEM 5. ACCOMP PAR-C2092 REMOVED N1, N2 ROTOR LOCKING TOOL AND INSTALLED ALL FAN BLADES SET AND SPINNER CONE AND RE-INSTALLED THE BORESCOPE DRIVE PAD COVER AS PER AMM 71-00-30, 72-22-02, 72-22-01, 72-00-00. ENG SER NR 959440