19960621014809A

Accident · Destroyed

FAA accident report · Beech 23 · Fulton, MO · June 21, 1996

Date
June 21, 1996 · 19:37 local
Place
Fulton, MO
Airport
Elton Hensley Memorial Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N2397J
NTSB investigation
NTSBCHI96FA209
Reported as
Beech 23
Reported engine
Lycoming O320D2B
People aboard
2
Fatal injuries
2
Pilot’s flight hours
220 total218 in this make and model2 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.

Crashed on takeoff end of the runway into some trees. (.4)witnesses reported an abnormal amount of black smoke trailing from the aircraft after takeoff. The airplane subsequently descended through trees and power lines. Postaccident investigation revealed the engine's #1 cylinder did not have compression when checked. After the intake valve of the #1 cylinder was pried back, the cylinder had compression when the propeller was rotated. The #1 cylinder's intake and exhaust manifold areas were darker in color than those of the other cylinders. The #1 cylinder's valve springs were not within the tolerances as listed by the manufacturer.

As the FAA filed it

CRASHED ON TAKEOFF END OF THE RUNWAY INTO SOME TREES. (.4)WITNESSES REPORTED AN ABNORMAL AMOUNT OF BLACK SMOKE TRAILING FROM THE AIRCRAFT AFTER TAKEOFF. THE AIRPLANE SUBSEQUENTLY DESCENDED THROUGH TREES AND POWER LINES. POSTACCIDENT INVESTIGATION REVEALED THE ENGINE'S #1 CYLINDER DID NOT HAVE COMPRESSION WHEN CHECKED. AFTER THE INTAKE VALVE OF THE #1 CYLINDER WAS PRIED BACK, THE CYLINDER HAD COMPRESSION WHEN THE PROPELLER WAS ROTATED. THE #1 CYLINDER'S INTAKE AND EXHAUST MANIFOLD AREAS WERE DARKER IN COLOR THAN THOSE OF THE OTHER CYLINDERS. THE #1 CYLINDER'S VALVE SPRINGS WERE NOT WITHIN THE TOLERANCES AS LISTED BY THE MANUFACTURER.

NTSB investigation

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