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October 8, 1998 · Piper PA-31-350 · N3543A

Ravenna, OH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 8, 1998
Injury Outcomes
No injuries (1 uninjured)
Location
Ravenna, OH
Aircraft
Piper PA-31-350
Tail Number
N3543A
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
NYC99LA005

The pilot departed on a night multiple-leg flight series with full tanks. On approach for the second landing, the green landing gear lights extinguished. The pilot discovered that if the landing gear was extended the circuit breaker would stay in and if the landing gear was retracted the circuit breaker would pop. The circuit breaker controlled the landing gear lights, the engine oil pressure, and both fuel quantity gauges. The pilot continued on four additional flights in that condition. The fourth flight terminated 5 miles from the runway with a double power loss. Examination revealed the fuel tanks were empty. The pilot had flown the airplane 4.3 hours including 6 takeoffs, one missed approach, and a 20 minute ground run prior to departure with both engines running on the final flight.

NTSB Probable Cause

The pilot's improper decision to continue to operate the airplane with inoperative equipment which resulted in fuel exhaustion. Factors were the inoperative fuel quantity gauges, and the night conditions.

Full Narrative

On October 8, 1998, about 0255 eastern daylight time, a Piper PA-31-350, N3543A, operated by Castle Aviation, was destroyed during a forced landing near Ravenna, Ohio. The certificated commercial pilot was not injured. Night visual meteorological conditions prevailed for the positioning flight, which had departed from Detroit, Michigan (DTW). The flight was operated on an instrument flight rules (IFR) flight plan under 14 CFR Part 91. Interviews with an inspector from the Federal Aviation Administration (FAA) disclosed that the flight had originated earlier in the evening from Portage County Airport (29G), Ravenna, with full fuel tanks (182 gallons of useable fuel). The pilot operated the airplane on a series of positioning flights under 14 CFR Part 91, and when cargo was carried, the flights were operated under 14 CFR Part 135. The pilot told the FAA Inspectors that on the second leg of the flight, while on final approach, the green "landing gear down and locked" lights failed to illuminate. The pilot performed a missed approach and while being vectored for the ILS a second time, noticed that a circuit breaker had popped, and reset it. The pilot also reported that the circuit breaker would not stay reset as long as the landing gear was retracted. However, when the landing gear was extended, the circuit breaker would stay reset. After landing, the pilot departed on the next leg of his flight series, and continued to operate the airplane in this condition for four additional flights. At the completion of the last cargo flight which terminated in DTW, the pilot was asked by company personnel if he had sufficient fuel for the return flight to 29G, and replied that he did. The pilot reported that en route to 29G, he used the remaining fuel in the auxiliary tanks and then switched to the main tanks. While on a descent, about 2,600 feet mean sea level (MSL), and maneuvering for a visual approach, the engines started surging and subsequently lost power. The pilot then performed a forced landing in a wooded area about 5 miles east of the airport. Examination of the airplane by FAA Inspectors revealed that all fuel tanks were empty, and the airplane had flown 4.3 hours since being refueled. During that time, the pilot performed six takeoffs, two approaches with higher than normal speeds at the request of approach control, and one missed approach to a second ILS approach. The pilot also incurred a 20 minute ground delay with both engines operating prior to his final departure. The pilot also told the FAA Inspectors that the fuel gauges indicated between 1/4 and 1/2 on the main fuel tanks prior to departure from DTW. Examination by FAA Inspectors revealed that with no electrical power on the fuel quantity measuring system, the left fuel tank gauge read 1/4 and the right fuel tank gauge read 1/3. Examination of electrical wiring diagram for the Piper PA-31-350 revealed that the circuit breaker that had popped when the landing gear was retracted, controlled the landing gear lights, the oil pressure indications for both engines, and both fuel quantity gauges. The toxicological testing report from the Ohio State Highway Crime Lab, Columbus, Ohio, was negative for drugs and alcohol for the pilot.

Flight

Event TypeAccident
Event Time02:55 EDT
Nearest AirportPortage County Airport (5nm E)
Runway27
Runway Length3500 ft
Runway Width75 ft
Flight Plan FiledIFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-31-350
Tail NumberN3543A
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · TIO-540-J2BD · Reciprocating · 350
Seats3

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 40 · Second Class

Conditions

ConditionsVMC
LightDark Night
WindCalm
Visibility3 sm
CeilingBroken clouds 800 ft
Temperature / Dew Point55 / 55
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data