20000910042839A

Accident · Substantial damage

FAA accident report · Beech B24R · Necedah, WI · September 10, 2000

Date: September 10, 2000 · 14:05 local
Place: Necedah, WI
Phase of flight: To Aborted (Fixed Wing)
Operating rules: General operating rules (Part 91)
Damage: Substantial damage
Aircraft: N4342W
NTSB investigation: NTSBCHI00LA294
Reported as: Beech B24R
Reported engine: Lycoming IO360A1B6
Pilot’s flight hours: 213 total72 in this make and model44 in the last 90 days

N4342WRegistration cancelled Feb 22, 2001 · Beech B24RS/N MC-274 Airframe modelBeech B24R

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) Pilot indicates during take-off at 30' AGL, a change in engine sound and lower than 2700 RPM was noted. Flight was aborted-aircraft received substantial damage after running off runway. Engine was run-up several times using RH & LH fuel-the engine performed to max. Power parameters.

As the FAA filed it

(-23) PILOT INDICATES DURING TAKE-OFF AT 30' AGL, A CHANGE IN ENGINE SOUND AND LOWER THAN 2700 RPM WAS NOTED. FLIGHT WAS ABORTED-AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE AFTER RUNNING OFF RUNWAY. ENGINE WAS RUN-UP SEVERAL TIMES USING RH & LH FUEL-THE ENGINE PERFORMED TO MAX. POWER PARAMETERS.

NTSB investigation

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

NTSB CHI00LA294Accident · No injuriesLimited investigationFinal reportNecedah, WIThe pilot did not properly flare the airplane during the aborted takeoff and he failed to maintain directional control of the airplane during the landing roll. Factors associated with the accident were the partial power loss for undetermined reasons and the…Sep 10, 2000 · Substantial damage