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December 27, 1995 · Stinson ST-108-2 · N135C

Lake Dallas, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 27, 1995
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Lake Dallas, TX
Aircraft
Stinson ST-108-2
Tail Number
N135C
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
FTW96LA077

The pilot reported that after takeoff, while climbing through 500 feet AGL, the engine 'experienced a dramatic and immediate power loss (70-80%) and began surging, all in the low RPM range.' During the emergency descent, he decided to 'ditch under control' in a lake to avoid descending into a residential area. Both occupants exited the airplane after the water landing, and swam to shore. The airplane subsequently submerged. During an engine teardown by the owner, it was discovered that the #6 connecting rod had 'failed.'

NTSB Probable Cause

the failure of the #6 connecting rod assembly. A factor was the lack of suitable terrain for a forced landing which resulted in a water landing.

Full Narrative

On December 27, 1995, approximately 0952 central standard time, a Stinson ST-108-2, N135C, registered to, and operated by the student pilot under instruction, as a Title 14 CFR Part 91 instructional flight, was destroyed during a forced landing to water following a loss of power after takeoff from a private airstrip, near Lake Dallas, Texas. Visual meteorological conditions prevailed and no flight plan was filed. The pilot-in-command, a certified flight instructor (CFI), received minor injuries and the student pilot was not injured. After practicing takeoffs and landings, the flight departed the airstrip about 2 minutes prior to the accident, and was en route to Addison Airport, Dallas, Texas. The CFI reported the following information: After takeoff, while climbing through 500 feet above ground level, the engine "experienced a dramatic and immediate power loss (70-80%) and began surging, all in the low RPM range." The airplane could not sustain level flight. The student pilot was at the controls when the engine started to run rough; however, the CFI assumed control of the airplane during the emergency descent/landing. He attempted to return to the airstrip, however; "although the engine was still running, it was not developing any appreciable thrust." During the descent, he decided to "ditch under control" in a lake to avoid descending into a residential area. Both occupants exited the airplane after the water landing, and swam to shore. The airplane subsequently submerged. During an engine teardown by the owner, it was discovered that the #6 connecting rod had "failed."

Flight

Event TypeAccident
Event Time09:52 CST
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftStinson ST-108-2
Tail NumberN135C
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsFranklin · GA4-165-133 · Reciprocating · 165

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 28 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind10° @ 5 kt
Visibility13 sm
CeilingNone
Temperature / Dew Point39 C / 30 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data