N444CE
Registered owner: EVERTS AIR FUEL INC, AK (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.
3 reports on file, 2006-02-23 – 2015-06-25.
Part: STRINGER — CRACKED (RT WING)
CRACKED WING STRINGER 21 AT WS 179R. TO REPAIR WING STRINGER, REMOVE EXISTING REPAIR MADE IAW SRM IO 1C-118A-3-1 AROUND FUEL TANK ACCESS PANEL CUT, STRINGER 21 CAP AT WS 194.5R. CUT STRINGER 21 AT WS 190.75R. MANUFACTURE SKIN DOUBLER IAW DWG 1525-01. MANUFACTURE STRINGER SPLICE & STRINGER CAP SPLICE IAW REPAIR SKETCH 891212002. INSTALL PARTS WET IAW DWG 1525-01 & REPAIR SKETCH 891212002.
Part: DOUBLER — CORRODED (LT WING)
REPLACEMENT OF CORRODED DOUBLER OTBD OF NR 2 NACELLE BETWEEN CTR & AFT SPARS. REPLACE AN EXISTING CORRODED DOUBLER WITH A NEW ONE IAW SRM TO 1C-188A-3-1. MANUFACTURE A NEW ONE FROM 2024-T3 0.071 IAW DWG 1526-01 & SRM TO 1C-118A-3-1.L TRIM OUT CRACK AT THE AFT SPAR AT WS 176.5L & MAKE FILLER FROM 7075-T6 0.063. INSTALL DOUBLER IAW DWG 1526-01.
Part: CYLINDER — CRACKED (NR 2 ENGINE) · airframe 31,924 hrs
NR 2 ENGINE SHUT DOWN DUE ROUGH RUNNING