N9216V

Substantial
None

MOONEY M20C S/N: 690050

Accident Details

Date
Wednesday, August 9, 1995
NTSB Number
NYC95LA184
Location
MONTGOMERY, PA
Event ID
20001207X04347
Coordinates
41.169593, -76.870681
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The partial loss of engine power, as a result of an excessively rich fuel flow in the carburetor, and a subsequent forced landing. A factor relating to the accident was the malfunction of the landing gear.

Aircraft Information

Registration
N9216V
Make
MOONEY
Serial Number
690050
Engine Type
Reciprocating
Model / ICAO
M20C M20P
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BMS AVIATORS INC
Address
2316 BAYNARD BLVD
Status
Deregistered
City
WILMINGTON
State / Zip Code
DE 19802
Country
United States

Analysis

On August 8, 1995, at 2007 eastern daylight time, a Mooney M20C, N9216V, sustained substantial damage during a forced landing in Montgomery, Pennsylvania. The private pilot and two passengers were not injured. Visual meteorological conditions prevailed. There was no flight plan for the personal, local flight that had just departed the Williamsport-Lycoming Airport. The flight was conducted under 14 CFR Part 91.

In the NTSB 6120.1/2 form, the pilot reported that during the takeoff, he noticed that very little right rudder was required. During the climb, he observed a loss of airspeed, and the airplane would not maintain altitude. The pilot made a forced landing in a corn field. Additionally, the pilots attempts to retract the gear during the climb out were unsuccessful, and when the flaps were checked, they were in the retracted position.

The engine was test run at Textron Lycoming, Williamsport, Pennsylvania, under the supervision of an Federal Aviation Administration (FAA) Inspector. The FAA Inspector reported, "...No discrepancies were noted during engine operation testing. Both magnetos tested within limits. Engine performance testing revealed slightly rich carburetor operation...."

The carburetor was test run at Precision Airmotive Corporation, Everett, Washington, under the supervision of an NTSB Air Safety Investigator (ASI). The ASI reported, "...Flow rates for the subject accident carburetor were slightly out of tolerance (excess flow) for all throttle settings greater than idle. The greatest out-of-tolerance situation occurred at 3/4 throttle setting...."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC95LA184