NYC07FA109

NTSB accident investigation · Piper PA38-112 · Odenton, MD · May 4, 2007

Accident · Serious injuriesField investigationFinal report
Date
May 4, 2007, 16:15 local (20:15 UTC)
Place
Odenton, MD
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N2600NPiper PA38-112
Weather
Visual (VMC) · Day
Status
Completed · report August 28, 2008
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20070504014729A
Case key
65706

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 mismanagement of the airplane's fuel supply, which resulted in fuel starvation and a total loss of engine power.

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(total) - nonmechanicalApproach - vfr pattern - downwind
Fluid,fuel - starvation
Fuel management - improperPilot in commandCause
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency descent/landing

Analysis

The pilot stated that the cross-country flight was uneventful until in the vicinity of his planned destination, and that there were no problems with the performance or handling characteristics of the airplane. As the airplane turned from a southerly heading to an easterly heading to align with the destination runway, the pilot switched fuel tanks, and the engine immediately stopped producing power. According to the pilot, "I made a mistake. I should have switched tanks while the wings were level, before I made the maneuver." The pilot again switched tanks, turned on the fuel boost pump, and attempted a restart, but lacked the altitude to accomplish the engine start. He then maneuvered the airplane to a two-lane road that ran parallel to a busy state highway beneath him for the forced landing. Examination of the airplane at the scene revealed that both fuel tanks were voided, but the fuel caps remained secure in their ports. There was no odor of fuel, nor was there evidence of fuel spillage at the scene. The left fuel gauge indicated one-half tank, and the right fuel gauge indicated "Empty." The fuel selector was selected to the right fuel tank position. According to the pilot, "I had plenty of fuel, I just didn't manage it right."

Factual narrative

History of flight

On May 4, 2007, at 1615 eastern daylight time, a Piper PA38-112, N2600N, was substantially damaged when it collided with terrain during a forced landing near Odenton, Maryland. The certificated commercial pilot was seriously injured. Visual meteorological conditions prevailed for the flight that originated at Allentown Queen City Municipal Airport (1N9), Allentown, Pennsylvania, and was destined for Tipton Airport (FME), Odenton, Maryland. An Air Defense Identification Zone (ADIZ) flight plan was filed for the personal flight conducted under the provisions of 14 Code of Federal Regulations Part 91.

The pilot was interviewed by telephone, and he said that the flight to Tipton was uneventful, and that there were no problems with the performance and handling of the airplane. As he turned the airplane from a southerly heading to an easterly heading to align with the destination runway, he switched fuel tanks, and the engine immediately stopped producing power. According to the pilot, "I made a mistake. I should have switched tanks while the wings were level, before I made the maneuver."

The pilot said that he again switched tanks, turned on the fuel boost pump, and attempted a restart, but lacked the altitude to accomplish the engine start. He then maneuvered the airplane to a two-lane road that ran parallel to the busy state highway beneath him.

A review of radar data from the Federal Aviation Administration (FAA) revealed that a target identified as the accident airplane approached the Tipton Airport area from the north. At 1614, the airplane initiated a 90-degree left turn that aligned the radar track toward Tipton Airport. During the turn, the airplane descended from 900 feet to 800 feet, and slowed from 76 knots groundspeed, to 62 knots groundspeed. During the 23 seconds after completion of the turn, the airplane descended to 500 feet, and slowed to 58 knots, before the target went in to coast mode.

Personnel information

The pilot held a commercial pilot certificate with ratings for airplane single engine land, and instrument airplane. He also held a flight instructor certificate with ratings for airplane single engine land, and instrument airplane. His most recent FAA second-class medical certificate was issued on November 6, 2006.

The pilot reported approximately 2,900 total hours of flight experience, 300 hours of which were in make and model.

Aircraft information

According to a maintenance receipt, the airplane's most recent annual inspection was completed March 8, 2007, at 3,885 aircraft hours. The airplane had accrued 3,899 total aircraft hours.

Meteorological information

At 1639, the weather recorded at Tipton Airport included clear skies with 10 miles visibility. The wind was from 210 degrees at 3 knots, the temperature was 22 degrees Celsius, and the dewpoint was 0 degrees Celsius. The altimeter setting was 30.20 inches of mercury.

Wreckage and impact information

The airplane was examined on the evening of the accident at the scene, about one-half mile northwest of Tipton Airport. The runway was oriented 100/280 degrees magnetic. The wreckage path was about 120 feet long, and oriented about 115 degrees magnetic. The initial ground scar was on a paved road. The ground scars and skid marks continued off the pavement where the road curved, onto a grass apron, and down an embankment where the airplane came to rest.

The airplane's engine compartment and cockpit came to rest centered between two trees. Each tree was embedded in the leading edge of its respective wing about three feet outboard of the cabin. The leading edges of both wings were crushed aft in compression, and each displayed multiple tears and dents across their spans. Both fuel tanks were voided, but the fuel caps remained secure in their ports. There was no odor of fuel, nor was there evidence of fuel spillage at the scene.

Control continuity was established from the cockpit to all flight control surfaces. Examination of the cockpit revealed that the throttle was full forward, the mixture was full rich, and the carburetor heat lever was at mid-travel. The left fuel gauge indicated one-half tank, and the right fuel gauge indicated "Empty." The fuel selector was selected to the right fuel tank position.

The tip of one propeller blade was bent, but the leading edges and faces of each blade were undamaged. The spinner showed a slight dent and some scoring on the side that rested on the ground, but the remainder of the spinner was undamaged.

Tests and research

On May 8, 2007, the engine was examined by two FAA aviation safety inspectors. In a written statement, one inspector said that the engine was rotated by hand at the propeller, and that continuity was established through the powertrain to the valvetrain and accessory section. Compression was confirmed using the thumb method. The right magneto did not produce spark but the left magneto produced spark at all terminal leads. There was approximately 2 teaspoons of fuel in the carburetor bowl.

Additional information

Examination of fuel records revealed that the airplane was serviced with 11.5 gallons of fuel on May 2, 2007, but that only the left tank was filled. In a written statement, the line service technician stated that the pilot requested that only the left tank be filled. He further stated, "Afterwards he checked the fuel level of the left tank with a home-made fuel indicator consisting of a wooden ruler with markings."

The pilot reported that the accident flight was the second flight since he had serviced the airplane with fuel. The pilot estimated that there were "16 or 17" gallons of fuel in the left tank and 23 gallons of fuel in the right tank when he departed for Tipton Airport, and that he flew "all the way down [to Tipton] on the left tank."

According to the pilot, "I had plenty of fuel, I just didn't manage it right."

Aircraft

Registration
N2600N
Reported as
Piper PA38-112
Category
Airplane
Serial number
38-79A0936
Airframe hours
3,899
Engine
Lycoming O-235, 112 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert James
Airworthiness certificate
Standard, Normal; Standard, Utility
Last inspection
Annual · March 1, 2007 · 14 hours before
Departed
1N9 · Allentown, PA
Destination
FME · Odenton, MD
Flight plan
VFR
Airport
FME · Tipton Airport, runway 10, 3,000 × 75 ft, asphalt

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
60
Injuries
Serious
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Seat
Left
Flight hours
2,900 total · 300 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
210° at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
72 °F, dew point 32 °F
Altimeter
30.20 inHg
Observed at
FME, 1 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.

Other investigations on N2600N · 1

Matched to the same aircraft by N-number and date.