Br Legend TURBINE LEGEND N42BR
23 May 2015 · West Columbia, South Carolina, United States · Fatal
Summary
On 23 May 2015 at about 13:21 local time, a Br Legend TURBINE LEGEND registered N42BR was involved in an accident near West Columbia, South Carolina, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 13:21
- Classification
- Accident
- Location
- West Columbia, South Carolina, United States
- Nearest airport
- Columbia Metropolitan Airport (CAE)
- Coordinates
- 33.9475, -81.1622
- Aircraft
- Br Legend TURBINE LEGEND
- Registration
- N42BR
- Category
- Airplane
- Year built
- 2003
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Personal
- Phase of flight
- Not recorded
- Route
- West Columbia → Asheville
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- ERA15FA221
People
1 person died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 1 | 0 | 0 | 0 |
Probable cause
An engine flame-out due to fuel starvation as the result of an improperly-installed auxiliary fuel pump fitting, and the pilot's failure to promptly feather the propeller following the engine-flame out, which resulted in decreased glide capability and impact with terrain. Contributing to the accident was the pilot's operation of the airplane with no emergency electric propeller feathering system.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The commercial pilot departed on a cross-country flight in the experimental, amateur-built, turboprop airplane. About 3 minutes after takeoff, the pilot initiated a return to the departure airport. About 6.8 nautical miles (nm) from the runway, at an altitude of about 6,500 ft mean sea level, the pilot declared an emergency, stating that he had "lost" the engine. Shortly thereafter, he informed air traffic control that the airplane had experienced a loss of fuel pressure. Witnesses saw the airplane collide with a tree and subsequently impact a pond about 1.2 nm from the runway. They reported no engine sound. Examination of the airplane revealed no evidence of preimpact failures or malfunctions of the flight controls that would have precluded normal operation. The landing gear and flaps were found retracted. There was no evidence of preimpact failure or malfunction of the engine core. The engine-driven fuel pump showed signs of internal cavitation, while the auxiliary fuel pump, which provided fuel under pressure to the engine-driven fuel pump, flowed nearly 48% less than specified by the manufacturer, and had an inconsistent/intermittent laboring sound during testing. Disassembly revealed an improperly-installed fitting, which resulted in the decreased fuel flow rate, a loss of fuel pressure, and a subsequent engine flame-out. Inspection also revealed that a component of the fuel pump had been replaced after manufacture, but there was no record of this maintenance in the airplane's logbooks. While it was not known if the pilot attempted to perform an air restart of the engine, a worn ignitor box and ignitor plug may have precluded a successful restart of the engine. Although the pilot descended the airplane at its published best glide airspeed in his attempt to return to the airport, because the airplane was not equipped with an electrically-operated feathering pump, the propeller blade angle remained where it was set when the engine flame-out occurred, which was likely flat pitch. The flat pitch of the propeller blades significantly decreased the airplane's engine-out glide ratio. Had the pilot promptly feathered the propeller blades to reduce drag following engine flame-out, or had the airplane been equipped with a feathering pump, it is likely the airplane would have been able to reach the intended runway and land uneventfully. Although an enlarged heart was noted during the autopsy and toxicological testing detected quinine, given that the pilot was actively controlling the airplane just before the accident, there is no evidence that a medical condition or use of quinine contributed to the pilot's inability to fly the airplane.
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 30 Oct 2015 | Hughes 369D | Marion, South Carolina, United States | Rotor Blade LLC | No injuries | - |
| 16 Apr 2015 | Short Bros SD 360-300 | Greer, South Carolina, United States | Air Cargo Carriers | No injuries | - |
| 2 Aug 2015 | Stol JA30 SUPERSTOL | West Union, South Carolina, United States | Stol LLC | No injuries | - |
| 25 Jul 2015 | Johnny F Anderson BUCKEYE DREAM MACHIN | Trenton, South Carolina, United States | Logue Glenn R | Minor injuries | - |
| 2 Oct 2015 | Piper PA32R | Westminster, South Carolina, United States | - | Fatal | 4 |
| 7 Jul 2015 | Cessna 150M | Moncks Corner, South Carolina, United States | - | Fatal | 2 |