The fatigue failure of the forward pressure bulkhead canted web that originated from stress corrosion cracking areas. Contributing to the failure were inspection procedures and intervals inadequate to identify the crack.
N401LC
1975 LOCKHEED 382G-44K-30
Fixed wing multi engine · Turbo-prop · Restricted
3 NTSB records
for this tail number, including substantial damage. See the full record below.
Registration
Airframe
Powerplant
Live Flight Status
Checking live traffic…
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Transponder & Tracking
The hex code is the aircraft's ICAO 24-bit address, broadcast by its ADS-B transponder. It is the key used to match live position reports to this registration.
NTSB Accident & Incident Record
Feb 12, 2016
Accident
Substantial Iliamna, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 121
Probable Cause
NTSB DCA16LA096
Jul 19, 2007
Accident
Substantial McGrath, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause
The pilot's excessive rotation of the airplane during takeoff, which resulted in dragging the tail on the runway and substantial damage.
NTSB ANC07LA067
Jul 2, 2001
Accident
Substantial Lake Minchumina, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 121
Probable Cause
The flight crew's improper recovery from a bounced landing. Factors associated with the accident were the selection of an unsuitable landing area, and a rough/uneven landing surface.
NTSB ANC01LA081