This N-number isn't registered right now. Below is its last known registration, canceled Feb 11, 2020.
Safety record in brief:1 NTSB accident (substantial damage, Aug 2019)No ADs since 1998 matched11 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The pilot's failure to maintain an adequate glidepath during the approach, which resulted in the airplane impacting rocks and dirt at the runway threshold, a separation of the right main landing gear, and a loss of directional control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC19LA045)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
No ADs published since 1998 matched this airframe or engine model.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
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.
From FAA Service Difficulty Reports; matched by N-number and serial number.EXCESSIVE VIBRATION ON #4 ENGINE NO OTHER INDICATION PRECAUTIONARY SHUTDOWN #4 ENGINE/ TWO BLADES WENT TO FEATHER THIRD BLADE STAYED IN LOW PITCH CONDITION
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.COMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANK
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 11 reports.