ATL98LA045

NTSB accident investigation · Pitts S-2A · New Smyrna Beac, FL · February 17, 1998

Accident · No injuriesLimited investigationFinal report
Date
February 17, 1998, 17:20 local (22:20 UTC)
Place
New Smyrna Beac, FL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N32TPPitts S-2A
Weather
Visual (VMC) · Day
Status
Completed · report February 15, 2001
Report
Approved by Office Director
FAA report
19980217006069A
Case key
3971

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 loss of engine power for undetermined reasons, and, the jammed engine starter drive assembly, that prevented an engine restart in flight. A factor was the soft terrain.

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) - nonmechanicalManeuvering
Reason for occurrence undeterminedCause
Airframe/component/system failure/malfunctionManeuvering
Engine accessories,engine starter - jammedCause
Forced landingDescent - emergency
In flight collision with terrain/waterEmergency descent/landing
Terrain condition - softFactor

Analysis

The pilot reported that they were performing flat spin maneuvers when the propeller assembly stopped turning, and the engine quit. Attempts, by the pilot, to restart the engine, failed. The pilot surveyed the immediate area for an emergency landing area. The pilot selected a landfill for an emergency landing. The airplane touched down on the main landing gear, sank into the soft soil, and flipped over on the left side. Examination of the airplane disclosed that the starter drive assembly was stuck, and it was also jammed against the engine flywheel. The starter drive assembly was described as being 'gummed up'. After the starter drive assembly was freed the engine started normally. According to the Chief Test Pilot for Aviat Aircraft Inc, Pitts Aviation Enterprises, Inc., and other S-2A pilots, it is not uncommon for the S-2A to experience a loss of engine power during the execution of a flat spin. The normal restart procedure requires the use of the starter assembly. Examination maintenance records disclosed that the airframe maintenance procedures were completed in accordance with prescribed procedures.

Factual narrative

On February 17, 1998, at 1720 eastern standard time, a Pitts S-2A, N32TP, collided with the ground, according to the pilot, as he was attempting an emergency landing five miles north of New Smyrna Beach, Florida. The pilot reported that the flight operated under the provisions of Title 14 CFR Part 91, and he had not filed a flight plan. He also stated that visual weather conditions prevailed at the time of the accident. According to the pilot, the airframe sustained substantial airframe damage. Neither of the two air transport pilots on board the airplane were injured. The flight departed Spruce Creek Airport in Daytona Beach Florida, at 1700.

The pilot reported that they were performing flat spin maneuvers when the propeller assembly stopped turning. At the same time, the pilot realized that the engine had also quit. Attempts, by the pilot, to restart the engine, failed. The pilot surveyed the immediate area for an emergency landing area. The pilot said, he selected a landfill and established an approach for an emergency landing. He recalled, as the airplane touched down, the main landing gear sank into the soft soil, and the airplane flipped over on the left side.

Examination of the airplane disclosed that the starter drive assembly was stuck, and it was also jammed against the engine flywheel. The starter drive assembly was described as being "gummed up".". After the starter drive assembly was freed the engine started normally. The normal restart procedure requires the use of the starter assembly. Examination maintenance records disclosed that the airframe maintenance procedures were completed in accordance with prescribed procedures. According to the pilot the starter assembly had not been serviced in several years.

According to the Chief Test Pilot for Aviat Aircraft Inc, Pitts Aviation Enterprises, Inc., and other S-2A pilots, it is not uncommon for the S-2A to experience a loss of engine power during the execution of a flat spin. The normal in-flight restart procedures are required to recover from this maneuver. (see attached emergency procedures for in-flight engine restart).

Aircraft

Registration
N32TP
Reported as
Pitts S-2A
Category
Airplane
Serial number
2179
Airframe hours
1,390
Engine
Lycoming IO-360-A1A, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Timothy T. Plunkett
Airworthiness certificate
Standard, Aerobatic
Last inspection
Annual · January 12, 1998 · 7 hours before
Departed
44J · Daytona Beach, FL
Airport
44J · Spruce Creek Airport, runway 23, 4,000 × 200 ft, asphalt

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificates
Commercial, Airline transport
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Rear
Flight hours
15,000 total · 600 in this make and model · 6,100 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 12 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F
Altimeter
29.00 inHg
Observed at
DAB, 360 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.