N35241

Substantial
Minor

Cessna 177B S/N: 17702285

Accident Details

Date
Thursday, November 2, 2000
NTSB Number
NYC01LA029
Location
PROSPERITY, PA
Event ID
20001212X22326
Coordinates
40.020286, -80.250946
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The failure of the dual magneto ignition system points to open.

Aircraft Information

Registration
N35241
Make
CESSNA
Serial Number
17702285
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
177B C177
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
A B C FLYING CLUB INC
Address
ALLEGHENY COUNTY AIRPORT
Status
Deregistered
City
PITTSBURGH
State / Zip Code
PA 15122
Country
United States

Analysis

On November 2, 2000, about 1200 Eastern Standard Time, a Cessna 177B, N35241, was substantially damaged after a forced landing near Prosperity, Pennsylvania. The certificated private pilot and pilot-rated passenger received minor injuries. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight conducted under 14 CFR Part 91.

According to the pilot, he and the passenger were practicing maneuvers, for the commercial pilot practical test. While at an altitude of about 2,500 feet above the ground, the pilot heard a loud "pop," and the engine lost all power. The pilot made a force landing to a field. After touching down in the field, the airplane struck a fence and came to rest in briar bushes.

The pilot did not report any prior mechanical difficulties with the airplane's engine.

The airplane's magneto system, a Teledyne Continental Motors D-3000 Magneto Ignition system, was forwarded to Teledyne Mattituck Services Inc., Mattituck, New York, on January 10, 2001, and examined in the presence of a Federal Aviation Administration inspector. The inspector observed that both sets of points remained closed, regardless of the cam position, when the magneto system was tested. The inspector also stated that all securing hardware torque seals were intact and there was no evidence of point adjustment shifting.

A Safety Board investigator examined the magneto system on February 7, 2001. As the impulse coupling was turned, the lobes of the cam would not push the cam follower far enough to open the points.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC01LA029