N220TP

Substantial
Minor

Palmer/Wilgus Fokker F1S/N: F1-103

Accident Details

Date
Sunday, July 29, 2001
NTSB Number
NYC01LA197
Location
Rhinebeck, NY
Event ID
20010810X01655
Coordinates
41.920932, -73.900955
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to maintain directional control while landing, resulting in an inadvertent ground-loop. A factor related to the accident was the crosswind conditions.

Aircraft Information

Registration
Make
PALMER/WILGUS
Serial Number
F1-103
Engine Type
Reciprocating
Model / ICAO
Fokker F1FEST
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
FOKKER F1

Registered Owner (Current)

Name
RHINEBECK AERODROME MUSEUM
Address
PO BOX 229
City
RHINEBECK
State / Zip Code
NY 12572-0229
Country
United States

Analysis

On July 29, 2001, about 1610 eastern daylight time, a homebuilt Fokker F-1, N220TP, was substantially damaged while landing at the Old Rhinebeck Airport, Rhinebeck, New York. The certificated commercial pilot sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91.

According to the pilot, as he was landing on the south runway, a 2,200-foot long, 75-foot wide, grass runway, the airplane "ballooned" upward before touching down. The pilot added power and the airplane settled down onto the runway. As the airplane was rolling out, it suddenly ground looped to the left side of the runway. The pilot regained control of the airplane by turning to the right. During the turn, the left wing dug into the ground and the airplane nosed over, before coming to rest inverted.

The pilot added that the airplane's landing gear consisted of skids, and no brakes were installed.

According to the Federal Aviation Administration Airplane Flying Handbook, "The pilot must be alert for directional control difficulties immediately upon and after touchdown due to the ground friction on the wheels. The friction creates a pivot point on which a moment arm can act. Loss of directional control may lead to an aggravated, uncontrolled, tight turn on the ground, or a ground loop. The combination of centrifugal force acting on the center of gravity (CG) and ground friction of the main wheels resisting it during the ground loop may cause the airplane to tip or lean enough for the outside wingtip to contact the ground. This may even impose a sideward force which could collapse the landing gear."

The winds reported at a nearby airport, about the time of the accident were, from 130 degrees at 10 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC01LA197