ANC83FA131

NTSB accident investigation · Cessna U206 · Near Iliamna, AK · July 25, 1983

Accident · No injuriesField investigationFinal report
Date
July 24, 1983, 21:30 local (Jul 25, 1983, 05:30 UTC)
Place
Near Iliamna, AK
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N4661ZCessna U206
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Safety recommendations
Yes
FAA report
19830724037139A
Case key
4042

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(partial) - mech failure/malfTakeoff - initial climb
Induction air control/system - inadequateCause
Aircraft/equipment inadequateManufacturerCause
Induction air control/system - fatigueCause
Induction air control/system - failure,partialCause
Induction air control/system - separationCause
Engine assembly,valve,intake - foreign object damageCause
Forced landingLanding - flare/touchdown
Other gear collapsedLanding - flare/touchdown
Terrain condition - none suitableFactor
Landing gear,float assembly - overloadFactor

Analysis

The eng lost power just after a water takeoff. The acft landed straight ahead in muskeg & tundra collapsing the floats. Eng teardown revealed a metallic 'nugget' in the left intake manifold between the #4 & #6 ports. Numerous marks were found on the inside of both intake manifolds. There was minor denting, scratching & peening on the interior of the 90 deg elbows from both ends of the crossover tube, intake valve ports, seats & valve faces of cyls 4,5 & 6. The nugget was composed of the same material as the airbox ass'y, Cessna p/n 1250705, which contained two holes aprx 2-1/2 square inches each in the airbox wall. The holes were caused by fatigue cracks. The source of loading causing the fatigue crackpropagation was due to membrane &/or bending loads in the airbox wall caused by out-of-plane deformation. These deformation were most likely caused by exciting a natural mode of vibration in the wall. Three duct failures were reported to the FAA in 1983, two of which were in C-210 acft.

Aircraft

Registration
N4661Z
Reported as
Cessna U206
Category
Airplane
Serial number
U20605998
Airframe hours
325
Engine
Continental IO-520-F, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Part 135
Registered owner
Rust'S Flying Service
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · July 13, 1983 · 31 hours before
Destination
Lake Clark, AK
Flight plan
Company VFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Certificate
Commercial
Airplane ratings
Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
5,809 total · 1,869 in this make and model · 5,714 as pilot in command · 233 in the last 90 days · 3 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
80° at 20 knots, gusting 25
Visibility
5 statute miles
Lowest ceiling
1,500 ft overcast
Temperature
55 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.