N1735S

Substantial
None

AERO COMMANDER S2RS/N: 1438R

Accident Details

Date
Wednesday, August 3, 2011
NTSB Number
CEN11LA543
Location
Washington, IA
Event ID
20110804X24224
Coordinates
41.268611, -91.687500
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

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

Aircraft Information

Registration
N1735S
Make
AERO COMMANDER
Serial Number
1438R
Engine Type
Turbo-jet
Year Built
1968
Model / ICAO
S2RL29
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CAT AVIATION INC
Address
1563 HIGHWAY 91
Status
Deregistered
City
WALNUT RIDGE
State / Zip Code
AR 72476-8403
Country
United States

Analysis

On August 3, 2011, about 1743 central daylight time, an Aero Commander S2R, N1735S, sustained substantial damage during a forced landing following a loss of engine power near Washington, Iowa. The pilot was not injured. The airplane sustained damage to both wings, the fuselage, and the engine. The aircraft was registered to and operated by Cat Aviation, Inc, of Walnut Ridge, Arkansas under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight was originating from the Washington Municipal Airport (AWG), Washington, Iowa, when the accident occurred.

The pilot reported that the airplane's engine stopped producing power during climb out after takeoff. The airplane impacted terrain as the pilot was attempting to avoid a house during the forced landing.

According to maintenance records, the most recent maintenance performed on the airplane was an annual inspection on January 17, 2011.

A postaccident examination of the airplane confirmed crankshaft and accessory system continuity. The magnetos and fuel system could not be tested due to impact damage. No preimpact anomalies were noted during the examination that would explain the loss of engine power.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA543