N20128

Substantial
Serious

CESSNA 177B S/N: 17702634

Accident Details

Date
Sunday, August 22, 1993
NTSB Number
NYC93LA170
Location
SKANEATELES, NY
Event ID
20001211X13243
Coordinates
42.890838, -76.370880
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

THE IMPROPER INSTALLATION OF THE ENGINE OIL FILTER, AND THE SUBSEQUENT LOSS OF OIL AND ENGINE POWER, RESULTING IN FORCED LANDING AND COLLSION WITH TREES.

Aircraft Information

Registration
N20128
Make
CESSNA
Serial Number
17702634
Engine Type
Reciprocating
Year Built
2005
Model / ICAO
177B C177
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
ATLANTIC FERRY SERVICE INC
Address
1910 AUDUBON DR
Status
Deregistered
City
WATERLOO
State / Zip Code
IA 50701-8905
Country
United States

Analysis

On Sunday, August 22, 1993, at 1230 eastern daylight time, a Cessna 177B, N20128, registered to Charles Burns, and piloted by Fred C. Ziemer, sustained substantial damage during a forced landing in Skaneateles, New York. The pilot was seriously injured, and the passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The flight was being conducted under 14 CFR 91.

The pilot departed the Skaneateles Aero Drome on runway 10. In his report, the pilot stated:

Did run-up and departed....at approximately 1500 ft...the engine began to run rough, and stopped suddenly.

The pilot was unable to restart the engine, and he initiated a forced landing. The airplane collided with trees during the landing.

Federal Aviation Administration Inspectors Tony James and Edward Dick conducted an examination of the wreckage. In his report, Mr. James stated:

...inspection of the dip stick-no oil appeared. Visit to FBO...I saw oil on the taxiway where the A/C was parked and when the A/C taxied out the oil trail led to the run-up and takeoff.

Mr. Dick's report stated:

Upon arrival at the accident site, I noticed the following: 1) The aircraft was in an upright position...3) The engine was intact...no major engine failure was noted. 4) upon further inspection, the only area of oil leakage was directly below the oil canister that contained the oil filter...5) The oil canister was removed from the housing and upon doing so noticed the oil seal between the canister and housing was slipped completely into the housing...6) The seal was removed and was crushed inward...The oil canister was crushed into the housing during improper installation. This led to complete oil loss and engine stopping.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC93LA170