NYC06CA148

NTSB accident investigation · Taylorcraft DC-65 · Parma, NY · June 17, 2006

Accident · Serious injuriesData collectionFinal report
Date
June 17, 2006, 12:00 local (16:00 UTC)
Place
Parma, NY
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N50VSTaylorcraft DC-65
Weather
Visual (VMC) · Day
Status
Completed · report October 3, 2006
Report
Approved by Office Director
Parties
Rochester
FAA report
20060617022279A
Case key
63925

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

An uncontrolled descent into trees and terrain after takeoff for undetermined reasons.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Altitude deviation,uncontrolledTakeoff - initial climb
Reason for occurrence undeterminedCause
Aircraft weight and balance - exceededPilot in command
Weather condition - high density altitude
In flight collision with objectDescent - uncontrolled
Object - tree(s)

Analysis

The airplane collided with trees shortly after takeoff. The pilot stated that after a "normal" ground roll and initial climb, the airplane "started to lose airspeed and rate-of-climb," and that he was "unable to maintain altitude at full throttle." The pilot reported that he did not hear any unusual engine noises. According to a Federal Aviation Administration (FAA) inspector, no mechanical anomalies with the airplane or engine were evident. According to weight and balance calculations, the airplane was approximately 66 pounds over the maximum allowable gross weight for the airplane, which was 1,250 pounds. The calculated density altitude at the time of the accident was 2,300 feet.

Factual narrative

The 1942 Taylorcraft DC-65 airplane collided with trees shortly after takeoff. The pilot stated that after a "normal" ground roll and initial climb, the airplane "started to lose airspeed and rate-of-climb," and that he was "unable to maintain altitude at full throttle." The pilot reported that he did not hear any unusual engine noises. According to a Federal Aviation Administration (FAA) inspector, no mechanical anomalies with the airplane or engine were evident. According to weight and balance calculations, the airplane was approximately 66 pounds over the maximum allowable gross weight for the airplane, which was 1,250 pounds. The calculated density altitude at the time of the accident was 2,300 feet.

Aircraft

Registration
N50VS
Reported as
Taylorcraft DC-65
Category
Airplane
Serial number
6159
Airframe hours
1,788
Engine
Continental C-85-12, 85 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 1, 2006 · 10 hours before
Departed
7NK4 · Spencerport, NY
Airport
7NK4 · Ridge Road West Airport, runway 18, 1,800 × 45 ft, grass/turf

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
49
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
April 1, 2006
Seat
Front
Flight hours
1,006 total · 18 in this make and model · 877 as pilot in command · 40 in the last 90 days · 18 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 13 knots
Visibility
10 statute miles
Lowest ceiling
25,000 ft broken
Temperature
86 °F, dew point 59 °F
Altimeter
30.04 inHg
Observed at
KROC, 9 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.