20080624839769A

Accident · Substantial damage

FAA accident report · Beech A36 · Olathe, KS · June 24, 2008

Date
June 24, 2008 · 15:11 local
Place
Olathe, KS
Airport
Johnson County Executive
Phase of flight
Practice Training Manuevers
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N28HN
NTSB investigation
NTSBDFW08LA169
Reported as
Beech A36
Reported engine
Continental IO520BA
Fatal injuries
0
Pilot’s flight hours
15,000 total13,000 in this make and model100 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Prior to accident, ATC radar display showed the aircraft maneuvering east of klwc at approximately 2,200' MSL, with the last radar return showing 2,000' (terrain elevation 813'). Three witnesses who were surveying a field adjacent to the crash site stated that they saw the aircraft in level flight when the engines quit abruptly, and the airplane pitched down and crashed. Post-accident investigation indicated that both propellers were in their low pitch position with damage consistent with low RPM rotational forces. The fuel lines to the boost pumps, and the lines from the pumps to the fuel injector dividers, were devoid of fuel on both engines; however, both fuel valves were found in their open position. The fuel valve and boost pump switches for each engine are next to each other on the cockpit overhead panel. While the fuel valves must be on during flight operations, the company check list calls for the boost pump switches to be placed in the off position at the completion of maneuvering flight.

As the FAA filed it

(-23) PRIOR TO ACCIDENT, ATC RADAR DISPLAY SHOWED THE AIRCRAFT MANEUVERING EAST OF KLWC AT APPROXIMATELY 2,200' MSL, WITH THE LAST RADAR RETURN SHOWING 2,000' (TERRAIN ELEVATION 813'). THREE WITNESSES WHO WERE SURVEYING A FIELD ADJACENT TO THE CRASH SITE STATED THAT THEY SAW THE AIRCRAFT IN LEVEL FLIGHT WHEN THE ENGINES QUIT ABRUPTLY, AND THE AIRPLANE PITCHED DOWN AND CRASHED. POST-ACCIDENT INVESTIGATION INDICATED THAT BOTH PROPELLERS WERE IN THEIR LOW PITCH POSITION WITH DAMAGE CONSISTENT WITH LOW RPM ROTATIONAL FORCES. THE FUEL LINES TO THE BOOST PUMPS, AND THE LINES FROM THE PUMPS TO THE FUEL INJECTOR DIVIDERS, WERE DEVOID OF FUEL ON BOTH ENGINES; HOWEVER, BOTH FUEL VALVES WERE FOUND IN THEIR OPEN POSITION. THE FUEL VALVE AND BOOST PUMP SWITCHES FOR EACH ENGINE ARE NEXT TO EACH OTHER ON THE COCKPIT OVERHEAD PANEL. WHILE THE FUEL VALVES MUST BE ON DURING FLIGHT OPERATIONS, THE COMPANY CHECK LIST CALLS FOR THE BOOST PUMP SWITCHES TO BE PLACED IN THE OFF POSITION AT THE COMPLETION OF MANEUVERING FLIGHT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.