ANC99LA060

NTSB accident investigation · Aeronca 15AC · Pedro Bay, AK · May 8, 1999

Accident · Serious injuriesLimited investigationFinal report
Date
May 7, 1999, 18:25 local (May 8, 1999, 02:25 UTC)
Place
Pedro Bay, AK
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1315HAeronca 15AC
Weather
Visual (VMC) · Day
Status
Completed · report June 22, 2000
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19990507004739A
Case key
46274

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

A separation of the number 3 engine cylinder head assembly, and a burned through fuel line.

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(partial) - mech failure/malfClimb - to cruise
Engine assembly,cylinder - separationCause
FireEmergency descent/landing
Fuel system,line - burnedCause
DitchingEmergency landing
Terrain condition - water

Analysis

The certificated commercial pilot reported that while climbing through 7,000 feet msl, he smelled smoke in the airplane, followed by a rough running engine. During an emergency descent, he saw smoke and flames coming from underneath the floor boards adjacent to the rudder pedals. The pilot elected to ditch the airplane in shallow ocean water, just short of the beach. Upon touchdown, the airplane nosed over. The pilot said, in part: 'My legs were on fire and I just wanted to put the fire out, and get the airplane on the ground.' An FAA airworthiness inspector traveled to the accident scene, and examined the airplane wreckage. He said that upon closer inspection of the engine, it was discovered that the top portion of the number three cylinder was separated between the cylinder barrel, and the cylinder head. He added that the main fuel supply line was burned through, and disconnected from the carburetor inlet fitting. In his written statement the FAA inspector wrote, in part: '...the vibration shook loose the left engine exhaust pipe which then directed the exhaust onto the fuel line to the carburetor which caused the fire.'

Factual narrative

On May 7, 1999, about 1825 Alaska daylight time, a wheel equipped Aeronca 15AC airplane, N1315H, sustained substantial damage during an emergency landing and ditching, about 35 miles east of Pedro Bay, Alaska. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, when the accident occurred. The solo commercial pilot sustained serious injuries. Visual meteorological conditions prevailed, and a VFR flight plan was filed. The flight originated at the Pedro Bay Airport, about 1800, and was en route to Soldotna, Alaska.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge on May 8, the pilot reported that while climbing through 7,000 feet msl, approaching the coast of Chinitna Bay, he smelled smoke in the airplane, followed by a rough running engine. He made a 180 degree turn to return to Pedro Bay, and then saw smoke and flames coming from underneath the floor boards adjacent to the rudder pedals. He then advised the Kenai Flight Service Station (FSS) that he was making an emergency descent, and that he would be attempting to land on a tidal beach within Chinitna Bay. During the emergency descent, the airplane cabin filled with smoke, hindering his vision. The pilot said that the top portion of the clamshell door was torn off when he attempted to clear the smoke from the cockpit area by opening the door during the emergency decent. The pilot said, in part: "My legs were on fire and I just wanted to put the fire out, and get the airplane on the ground." The pilot landed in the water, just short of the beach, and the airplane nosed over upon touchdown. After ditching, the fire was self-extinguished by ocean water, and the pilot waded ashore.

The airplane sustained substantial damage to the wings, and fuselage.

A Federal Aviation Administration (FAA) airworthiness inspector from the Anchorage Flight Standards District Office, traveled to the accident scene on June 23, 1999, and examined the airplane wreckage. The inspector reported that the engine compartment, firewall, instrument panel, and floor boards exhibited heavy fire damage. He said that upon closer inspection of the engine, it was discovered that the top portion of the number three cylinder was separated between the cylinder barrel and the cylinder head. He added that the main fuel supply line was burned through, and disconnected from the carburetor attach point. In a written statement the FAA inspector wrote, in part: "...the vibration shook loose the left engine exhaust pipe which then directed the exhaust onto the fuel line to the carburetor which caused the fire."

Aircraft

Registration
N1315H
Reported as
Aeronca 15AC
Category
Airplane
Serial number
15AC-345
Engine
Franklin 6A-4165, 165 horsepower, reciprocating
Damage
Substantial damage
Fire
In-Flight
Flight
Personal · Part 91
Registered owner
Vincent L. Spady
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 1, 1999 · 20 hours before
Departed
AK04 · AK
Destination
SXQ · Soldotna, AK
Flight plan
VFR

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
51
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Medical
Unknown, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
1,500 total · 50 in this make and model · 20 in the last 90 days · 10 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 12 knots
Visibility
100 statute miles
Lowest ceiling
None
Temperature
45 °F

FAA reports on this event · 1

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