N451CE
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Tatonduk Outfitters, Ltd. (FXGA) | Operator | on 2019-08-01 | Operator named in NTSB report |
Accident & incident history
Operated by Tatonduk Outfitters Limited (per NTSB report)
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.
11 reports on file, 2015-06-05 – 2019-03-14.
Part: FRAME — CRACKED (FUSELAGE)
FUSELAGE FRAME REPAIR REPLACEMENT AT F/STA -29 LT SIDE. TO REPAIR CRACK ON FRAME REPAIR AT F/STA -29 ABOVE FWD DOOR HINGE. REMOVE AND REPLACE EXISTING REPAIR PER OVERHAUL MANUAL 11-4-8 AND 11-4-9.
Part: PROPELLER — SHEARED (NR 4) · airframe 41,732 hrs
EXCESSIVE VIBRATION ON #4 ENGINE NO OTHER INDICATION PRECAUTIONARY SHUTDOWN #4 ENGINE/ TWO BLADES WENT TO FEATHER THIRD BLADE STAYED IN LOW PITCH CONDITION
Part: SKIN — CRACKED (FUSELAGE)
CRACKED FUSELAGE SKIN UNDER COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. CRACKED FUSELAGE SKIN UNDER NR 2 COMM ANTENNA AT F/STA 348 BETWEEN STRINGER 1L AND 1R. PERFORM SKIN REPAIR PER DC-6 A&B OHM FIGURE 12-22.
Part: CARBURETOR — LEAKING (ENGINE) · airframe 41,170 hrs
COMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANK
Part: SKIN — CORRODED (BS 380)
CORRODED SKIN LAP JOINT AT BS 380 BETWEEN STRINGER 20R AND 21R. CORRODED SKIN LAP JOINT. CUT-OUT DAMAGE AND INSTALL REPAIR DOUBLER PER THE INSTRUCTIONS CONTAINED IN EAC EO 0502.
Part: CAP — CRACKED (WING)
WING STRINGER CAP 21, CRACKED AT STATION 238R. REMOVE STRINGER CAP FROM STATION 230.5 TO 252.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
Part: CAP — CRACKED (WING)
WING STRINGER CAP 18, CRACKED AT STATION 238L. REMOVED STRINGER CAP FROM STATION 232L TO 250L. MANUFACTURE & INSTALL STRINGER CAP & SPLICES IAW REPAIR SKETCH 891212002.
Part: CAP — CRACKED (WING)
WING STRINGER CAP 21, CRACKED AT STATION 242L. REMOVE STRINGER CAP FROM STATION 230.0 TO 250.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
Part: CAP — CRACKED (WING)
NUMBER 2 MAIN TANK, OTBD LANDING DOUBLER CRACKED. REMOVE STRINGER CAP FROM STATION 230.0 TO 250.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
Part: CAP — CRACKED (WING)
WING STRINGER CAP 19, CRACKED AT STATION 238R & 244R. REMOVE STRINGER CAP FROM STATION 230.5 TO 252.0. MANUFACTURE & INSTALL CAP STRINGER SPLICES IAW REPAIR SKETCH 891212002.
Part: SPAR CAP — CORRODED (WING)
FORWARD UPPER WING SPAR CAP CORRODED AT WS 350L. REMOVE CORROSION & INSTALL REPAIR PARTS IAW SORM INC REPORT SI-43712WR100. THIS REPAIR IS BASED ON A REPAIR PERFORMED ON N747CE SN 44661, APPROVED WITH FORM 8110-3 DATED SEPT 17 2008.