N3783M

Substantial
None

PIPER PA 28R-201S/N: 28R-7837137

Accident Details

Date
Saturday, August 6, 2016
NTSB Number
ERA16LA280
Location
Northampton, MA
Event ID
20160806X52719
Coordinates
42.328056, -72.611114
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the alternate air valve plate hinge pin, which caused the alternate air valve plate to lodge in the fuel servo assembly, which resulted in a restriction of air to the fuel servo assembly, a loss of engine power, and an off-airport emergency landing.

Aircraft Information

Registration
N3783M
Make
PIPER
Serial Number
28R-7837137
Engine Type
Turbo-shaft
Year Built
1978
Model / ICAO
PA 28R-201M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HAMPDEN AVIATION SERVICES INC
Address
160 OLD FERRY RD
Status
Deregistered
City
NORTHAMPTON
State / Zip Code
MA 01060-2509
Country
United States

Analysis

On August 06, 2016, about 1145 eastern daylight time, a Piper PA-28R-201, N3783M, was substantially damaged during a forced landing following a partial loss of engine power near Northampton Airport (7B2), Northampton, Massachusetts. The flight instructor and pilot receiving instruction were not injured. The instructional flight was conducted under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the flight, which originated from 7B2, about 1143.According to the flight instructor, during a simulated soft field take-off, the airplane's climb performance deteriorated noticeably. As the airplane reached approximately 150 feet above ground level, the engine started to lose power. He then realized that continuing the climb was not possible, and any increase in pitch resulted in an immediate decrease in airspeed. The flight instructor elected to make an emergency off airport landing in a corn field near the end of the departure runway. During the landing sequence the right wing and firewall were damaged.

A post accident examination of the airplane by a Federal Aviation Administration inspector revealed that the alternate air valve plate had separated from its mounting location and was lodged in the fuel servo air intake, blocking the fuel servo. After further examination of the alternate air valve plate it was noted that the hinge pin was worn completely through the plate assembly. A review of manufacturer engineering drawings showed that the plate assembly was modified using a spring attached to the plate. A review of the logbooks did not reveal an entry of a modification, or repair of the part.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA280