MIA08CA178

NTSB accident investigation · Dehavilland DH82A · Sevierville, TN · August 30, 2008

Accident · No injuriesData collectionFinal report
Date
August 30, 2008, 16:20 local (20:20 UTC)
Place
Sevierville, TN
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N80660Dehavilland DH82A
Defining event
Initial climb: Powerplant sys/comp malf/fail
Weather
Visual (VMC) · Day
Status
Completed · report January 22, 2009
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20080830848089A
Case key
68838

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

On this page

Probable cause

The failure of the wooden propeller.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Propeller system: propeller blade sectionAircraft › Aircraft propeller/rotor · FailureDehavilland DH82A: 1 caseAll aircraft: 51 casesProbable cause
Terrain: rough terrainEnvironmental issues › Physical environment · Contributed to outcomeDehavilland DH82A: 1 caseAll aircraft: 442 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

During takeoff, at about 100 feet in the air, near the end of the runway, the pilot heard a loud bang and immediately felt an increasing vibration. He reduced engine power and maneuvered to return to the runway. As he lined up for the runway, the engine was producing power but he felt no thrust. The airplane lost altitude and the pilot landed in a rough pasture short of the runway. The landing gear separated and the left wing buckled before coming to a stop. Post-accident examination of the airplane by a Federal Aviation Administration inspector revealed the brass tip separated from the wooden propeller and the blades separated to the hub section. The missing pieces of propeller were not located.

Factual narrative

The pilot of the DeHavilland DH-82A stated that shortly after takeoff he heard a loud bang over the engine noise and through the headset, followed immediately by severe vibration which increased until he reduced the power from take off to low cruise. The airplane was about 100 feet in the air and very near the end of the runway when the trouble started. The pilot elected to try to continue the climb and return to the field as quickly as possible. He was able to maintain sufficient airspeed while he turned around and lined up with the runway. Before he made the runway, the engine, though still running, felt like it stopped providing any thrust. The airplane was no longer able to maintain altitude and touched down in a pasture just before the runway. What appeared from the air to be a relatively smooth pasture; however, the terrain was rough and the impact sheared the landing gear. The left wing buckled as it settled to the ground. The pilot estimated that the total time from lift off to touchdown was approximate 2 to 3 minutes. The responding FAA inspector stated that examination of the engine revealed no discrepancies with it and its components. The wooden propeller was destroyed, split to the hub section. The propeller brass tip cap separated which started the initial vibration and tearing the propeller apart; consistent with the pilot’s account of having engine power but no thrust. The missing sections of the propeller were never located.

Aircraft

Registration
N80660
Reported as
Dehavilland DH82A
Category
Airplane
Serial number
82473
Airframe hours
24
Engine
Dehav ENG GIPSY MAJOR, 140 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · April 25, 2008 · 24 hours before
Departed
TN20 · Sevierville, TN
Destination
TN98 · Knoxville, TN
Flight plan
Unknown
Airport
TN20 · Seymour Air Park

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
55
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
January 30, 2008
Seat
Rear
Flight hours
2,000 total · 15 in this make and model · 13 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
6 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 63 °F
Altimeter
30.04 inHg
Observed at
KTYS, 11 nm away

FAA reports on this event · 1

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