N9222H

Substantial
Minor

CESSNA 185F S/N: 18503423

Accident Details

Date
Monday, September 4, 1995
NTSB Number
SEA95LA208
Location
SALEM, OR
Event ID
20001207X04599
Coordinates
44.840950, -123.081001
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A LOSS OF POWER FOR UNDETERMINED REASONS AND THE PILOT'S FAILURE TO MAINTAIN AIRSPEED WHILE MANEUVERING FOR A FORCED LANDING.

Aircraft Information

Registration
Make
CESSNA
Serial Number
18503423
Engine Type
Reciprocating
Year Built
2014
Model / ICAO
185F C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172S

Registered Owner (Current)

Name
DHS OPERATIONS LLC
Address
251 LITTLE FALLS DR
City
WILMINGTON
State / Zip Code
DE 19808-1674
Country
United States

Analysis

On September 3, 1995, at 1744 Pacific daylight time, a Cessna 185, N9222H, sustained substantial damage during a forced landing while conducting a low pass while towing a banner at the Salem, Oregon, airport. The airline transport pilot, the sole occupant, received minor injuries. No flight plan was filed for the flight, which was a banner tow operation to be conducted under 14 CFR 91. Visual meteorological conditions prevailed at the time of the flight. The ELT actuated, but did not assist in the location of the accident.

An FAA inspector who went to the scene reported that this was a banner tow operation. The cable had wrapped around the tail wheel during pickup and the pilot had reported rudder problems and had made a low pass at 65 knots indicated airspeed over the runway for his ground crew to observe the aircraft. The pilot stated that the engine sustained a loss of power when he opened his throttle as he finished his pass, and he did a sharp left turn and attempted a forced landing on the northwest corner of the airport.

Witnesses noted that the aircraft nose dropped abruptly during the turn and also stated that there was no indication of a loss of power from the sound of the engine. FAA inspectors noted strike marks in the pavement at the accident site that appeared to have been made from a rotating propeller. Both propeller blade tips were curled forward, with the rest of the blade surfaces curled aft. The engine was inspected and the fuel injection fuel pump, electric boost pump, and the fuel injection fuel control were tested. No mechanical anomalies were noted that would preclude the engine from operating.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA95LA208