N4356A

Substantial
None

PIPER PA 22-150S/N: 22-3712

Accident Details

Date
Wednesday, March 2, 2016
NTSB Number
WPR16LA079
Location
Fountain Hills, AZ
Event ID
20160302X02559
Coordinates
33.599998, -111.603057
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.

Aircraft Information

Registration
N4356A
Make
PIPER
Serial Number
22-3712
Engine Type
Turbo-shaft
Year Built
1956
Model / ICAO
PA 22-150M600
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
REGISTRATION PENDING
Address
3556 N REYNOLDS CIR
Status
Deregistered
City
MESA
State / Zip Code
AZ 85215-0758
Country
United States

Analysis

On March 2, 2016, about 1600 mountain standard time, a Piper PA-22-150 airplane, N4356A, executed a precautionary landing onto a sandy wash following a partial loss of engine power near Fountain Hills, Arizona. The private pilot and passenger were not injured; and the airplane sustained substantial damage to the wings. The airplane was registered to, and operated by, a private party as a 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The local flight originated from Phoenix-Mesa Gateway Airport (IWA), Phoenix, Arizona at about 1540.

The pilot reported that after a normal preflight and run-up, he took off and circled a nearby mountain before descending to about 750 feet above the ground at a 2,400 RPM. As they followed a nearby river, the engine started to sputter and decrease to about 900 RPM; the pilot increased and decreased the throttle several times, but the engine never went above 1,200 RPM before it decreased again. He observed that the oil pressure was low; therefore, he attempted to switch fuel tanks, turned on carb heat, ensured the mixture was full rich, but the engine never responded. The pilot elected to land the airplane onto a dry wash. When the airplane touched down, the right main landing gear sunk into the dirt and the airplane made a sharp turn to the right. The airplane rolled along the dirt, impacted a tree, and came to rest nose down.

During a postaccident examination by a Federal Aviation Administration Inspector, the engine cowling was removed and no visual anomalies were noted with the engine. The propeller and spinner were removed; and a test run propeller and temporary fuel tank were installed. The engine was started and operated normally; slowly, the power was increased to 2,400 RPM and the oil pressure was normal. After operating for a short time, the power was decreased and the engine was shutdown. There were no anomalies noted that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR16LA079