ATL95LA132

NTSB accident investigation · Cessna 310 · Ridgeland, SC · July 12, 1995

Accident · No injuriesLimited investigationFinal report
Date
July 12, 1995, 14:55 local (18:55 UTC)
Place
Ridgeland, SC
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N3083DCessna 310
Weather
Visual (VMC) · Day
Status
Completed · report October 26, 1995
Report
Approved by Office Director
FAA report
19950712040299A
Case key
3592

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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Probable cause

The pilot's failure to assure that the airplane's alternators were on which led to a complete loss of electrical power, and his failure to attempt to lower the landing gear by emergency procedures.

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.

Airframe/component/system failure/malfunctionCruise - normal
Electrical system,battery - dischargedCause
Alternator - not usedPilot in commandCause
In-flight planning/decision - improperPilot in commandCause
Wheels up landingLanding - flare/touchdown
Precautionary landing - performedPilot in command
Emergency procedure - not performedPilot in commandCause
Gear extension - not performedPilot in commandCause
Wheels up landing - performedPilot in command

Analysis

En route, the pilot was informed that his mode c encoder was not being received. The airplane slowly began losing electrical power, with eventual failure of all communication and navigation equipment (including a hand-held GPS that uses power from the aircraft's batteries.) The pilot continued the flight using pilotage. The pilot reported that when the fuel gages were indicating 10 gals in each tank, he decided to make an off-airport landing on an interstate highway. The pilot attempted to lower the gear, but was unsuccessful. An attempt to manually pump the gear down was not made. Traffic on the interstate forced the pilot to initiate a gear up landing on a service road adjacent to the interstate. The pilot stated that the engine maintained full power during the entire sequence. After the accident, the batteries were recharged and replaced in the aircraft. Both alternators and alternator switches operated normally. No evidenace of charging circuit malfunction or failure was noted.

Factual narrative

On July 12, 1995, about 1455 eastern daylight time, a Cessna 310, N3083D, collided with the terrain during an intentional gear up landing near Ridgeland, South Carolina. The airplane was operated by the owner/pilot under the provisions of 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed. A flight plan was not filed for the personal flight. There were no injuries to the private pilot nor his commercially rated pilot passenger. The airplane was substantially damaged. Origination of the flight was Titusville, Florida, about 1250 eastern daylight time, on the same day.

According to the pilot, the flight was normal until Daytona Beach Approach Control advised him that the mode "C" portion of the transponder was not being received. Approximately 50 minutes into the flight, the pilot realized that he had a failure of all of his communication and navigation equipment,including a hand held GPS that received power from the aircraft's battery. At this time the pilot also noticed that the fuel gauges were indicating a rapid loss of fuel.

The aircraft was approaching Savannah International Airport at an altitude of 8,500 feet, when the pilot made the decision to locate an uncontrolled field where he could make a safe landing. The pilot and his passenger then attempted to use pilotage to locate Ridgeland County Airport, in Ridgeland, South Carolina, which should have been a 15 minute flight.

The pilot stated that they were unsuccessful in locating the airport, and the fuel gauges continued to indicate an abnormal fuel burn. The pilot elected to land on an interstate highway, and a pre-landing checklist was completed. However, an attempt to lower the landing gear was unsuccessful. The pilot did not attempt to use the emergency extension system.

Traffic on the interstate forced the pilot to attempt a gear up landing on an adjacent service road. During the landing sequence, the airplane collided with trees, and was substantially damaged. The pilot stated that the engines never lost power.

A post crash examination of the aircraft was completed by the Federal Aviation Administration. The aircraft landing gear was raised and extended without any problem. Both alternators and regulators were secured, and the drive belts were installed. All electrical connections were tight. All circuit breakers were in.

The fuel quantity was checked in each tank, except the left tip tank which had been compromised in the landing. Both inboard tanks had fuel to a level four inches below the filler neck. The right tip tank had fuel to a level 11.5 inches below the filler neck.

The batteries were recharged and replaced in the aircraft. The damaged propellers were removed,and the engines were run with a test propeller. Both of the alternators and alternator switches operated normally. No evidence of malfunction or failure was noted.

Aircraft

Registration
N3083D
Reported as
Cessna 310
Category
Airplane
Serial number
35283
Engine
Continental O-470M, 240 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Allen M. Prohaska
Airworthiness certificate
Standard, Normal
Departed
X21 · Titusville, FL
Destination
BKW · Beckly, WV

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
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
292 total · 55 in this make and model · 130 as pilot in command · 22 in the last 90 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 9 knots
Visibility
6 statute miles
Lowest ceiling
None
Temperature
91 °F, dew point 70 °F
Altimeter
30.00 inHg
Observed at
SAV, 25 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.