- Date
- September 25, 1999, 11:30 local (15:30 UTC)
- Place
- River Ranch, FL
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N55BPBanting Glasair II
- Weather
- Visual (VMC) · Day
- Status
- Completed · report June 21, 2000
- Report
- Approved by Office Director
- FAA report
- 19990925041309A
- Case key
- 47449
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 total loss of engine power for undetermined reasons, which resulted in a forced landing to non-suitable 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.
Analysis
Upon arrival at his destination airport, the pilot entered the traffic pattern for landing. When engine power was reduced, the engine started to sputter. The pilot increased power, turned the boost pump on, and changed the fuel selector valve with negative results. He informed UNICOM that he would be unable to make the runway. A local highway was obstructed due to vehicle traffic and a forced landing was conducted to a marshy area. Examination of the engine assembly and accessories did not reveal the cause of engine roughness or subsequent total loss of engine power.
Factual narrative
On September 25, 1999, at about 1130 eastern daylight time, a Banting Glasair II, N55BP, registered to a private owner, operated by the pilot as a 14 CFR Part 91 personal flight, experienced a total loss of engine power in the vicinity of River Ranch, Florida, and a forced landing was made to a marshy area. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The private pilot reported no injuries. The flight originated from Lakeland, Florida, about 45 minutes before the accident.
The pilot stated he had been working on a fuel problem with the airplane for the last 2 1/2 months. He had replaced several components on the engine, and the problem went away. He decided to take the airplane on a cross-country flight in preparation for a longer flight. Upon arrival at the destination airport, he called UNICOM and another airplane reported in for landing. He eventually entered the traffic pattern for a left downwind to runway 16. Power was reduced to 2,000 rpm, the airspeed decreased to 140, and flaps were lowered. The engine started to sputter. He increased power, turned the boost pump on, and changed the fuel selector valve from the main tank to the header tank with negative results. He informed UNICOM that he would be unable to make the runway, and turned the airplane to line up with highway 60 as a forced landing area. The approach was discontinued due to vehicle traffic. He made another turn towards a marshy area located next to the highway, and made a forced landing.
Examination of the crash site by the FAA revealed the forced landing area was unsuitable, and no other forced landing areas were available. No determination could be made as to the cause of engine roughness or stoppage resulting in the accident.
Aircraft
- Registration
- N55BP
- Reported as
- Banting Glasair II
- Category
- Airplane, amateur-built
- Serial number
- 2281
- Airframe hours
- 550
- Engine
- Lycoming IO-360, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Banting W / Pardee K
- Airworthiness certificate
- Special, Experimental (Special)
- Last inspection
- Continuous airworthiness · January 10, 1999 · 50 hours before
- Departed
- LAL · Lakeland, FL
- Destination
- 2RR
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 53
- Certificate
- Private
- Airplane ratings
- Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 3, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 484 total · 312 in this make and model · 484 as pilot in command · 7 in the last 90 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 130° at 14 knots
- Visibility
- 15 statute miles
- Lowest ceiling
- 1,500 ft broken
- Temperature
- 86 °F, dew point 79 °F
- Altimeter
- 30.00 inHg
- Observed at
- LAL
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.