19981122044759I

Incident · Minor damage

FAA incident report · Piper PA-32R-301 · Marshall, MO · November 22, 1998

Date
November 22, 1998 · 19:10 local
Place
Marshall, MO
Airport
Marshall Memorial Municipal Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N186CA
Reported as
Piper PA32R301
Reported engine
Lycoming IO540K1G5D
People aboard
2
Fatal injuries
0
Pilot’s flight hours
727 total677 in this make and model32 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.

Aircraft departed carrollton, Missouri (K26) adn was in a cruise climb configuration when at 7000 feet the pilot stated that the aircraft started to shake violently. Pilot declared an emergency and landed on runway 18 in Marshall, Missouri (mhl)without further incident. The owners aircraft maintenance personnel inspected the aircraft and believe the server vibration was due to the failure of the engines number three connecting rod bolt. The owner is presently in litigation with the engine manufacturer and will provide m&d report upon final disassembly and inspection of the engine. This incident #CE99IGAOO15 is considered closed.

As the FAA filed it

AIRCRAFT DEPARTED CARROLLTON, MISSOURI (K26) ADN WAS IN A CRUISE CLIMB CONFIGURATION WHEN AT 7000 FEET THE PILOT STATED THAT THE AIRCRAFT STARTED TO SHAKE VIOLENTLY. PILOT DECLARED AN EMERGENCY AND LANDED ON RUNWAY 18 IN MARSHALL, MISSOURI (MHL)WITHOUT FURTHER INCIDENT. THE OWNERS AIRCRAFT MAINTENANCE PERSONNEL INSPECTED THE AIRCRAFT AND BELIEVE THE SERVER VIBRATION WAS DUE TO THE FAILURE OF THE ENGINES NUMBER THREE CONNECTING ROD BOLT. THE OWNER IS PRESENTLY IN LITIGATION WITH THE ENGINE MANUFACTURER AND WILL PROVIDE M&D REPORT UPON FINAL DISASSEMBLY AND INSPECTION OF THE ENGINE. THIS INCIDENT #CE99IGAOO15 IS CONSIDERED CLOSED.