N560FL

Substantial
None

Piper PA-28-140S/N: 28-7125401

Accident Details

Date
Sunday, June 8, 2003
NTSB Number
NYC03LA124
Location
Aurora, NY
Event ID
20030611X00846
Coordinates
42.711666, -76.621665
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to obtain the proper climb rate.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-7125401
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
PA-28-140P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-140

Registered Owner (Current)

Name
BANCROFT ROBERT W
Address
1036 LEVANNA RD
City
AURORA
State / Zip Code
NY 13026-9733
Country
United States

Analysis

On June 8, 2003, about 1900 eastern daylight time, a Piper PA-28-140, N560FL, was substantially damaged during the initial climb after takeoff from a private grass airstrip in Aurora, New York. The certificated private pilot and passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local flight. The personal flight was conducted under 14 CFR Part 91.

The pilot stated that he performed a normal engine run-up, and departed to the south, on his 2,000-foot-long, 60-foot-wide, grass runway. The airplane was configured with "two notches" of flaps. He rotated at 60 mph, and climbed at 75 mph. The pilot then realized that the airplane was not climbing fast enough to clear the 50-foot-high trees located at the end of the runway. As the airplane approached the trees, the pilot made a right turn; however, the left wing struck a tree and the airplane came to rest in a field.

The pilot further stated that he did not experience any mechanical malfunctions, and "everything seemed perfectly normal."

The pilot reported that he purchased the airplane about 6 months prior to the accident. He also reported 170 hours of total flight experience, which included about 16 hours in the accident airplane.

The weather reported at an airport about 22 miles southwest of the accident site, at 1853, included winds from 150 degrees at 10 knots, with 17 knot gusts, a temperature of 73 degrees F, and an altimeter setting of 29.73 in/hg.

The pilot reported that the airplane's gross weight at the time of the accident was about 1,900 pounds. Review of the takeoff distance chart in the airplane owner's handbook revealed that the distance to clear a 50-foot obstacle, at a gross weight of 1,950 pounds was about 1,900 feet. However, the chart was predicated on a takeoff from a level hard surface runway, in a no wind, zero flap configuration. The airplane's maximum takeoff gross weight was 2,150 pounds.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC03LA124