IAD99LA012

NTSB accident investigation · Pitcairn RAF 2000 · Doylestown, PA · November 3, 1998

Accident · No injuriesLimited investigationFinal report
Date
November 3, 1998, 09:50 local (14:50 UTC)
Place
Doylestown, PA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N52BPPitcairn RAF 2000
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 2000
Report
Approved by Office Director
FAA report
19981103034389A
Case key
45189

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

The pilot's inadequate compensation for wind conditions and his inadequate recovery from a bounced landing. Contributing to the accident were the pilot's fatigue and the crosswind conditions.

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.

Loss of control - in flightLanding - flare/touchdown
Weather condition - crosswind
Compensation for wind conditions - inadequatePilot in commandCause
FatiguePilot in command
Recovery from bounced landing - inadequatePilot in commandCause
In flight collision with terrain/waterLanding - flare/touchdown

Analysis

The pilot flew three traffic patterns in the gyroplane. He reported that he was experiencing difficulty with the gusty, crosswind conditions. On the fourth approach with a crosswind from the left, the gyroplane bounced during the landing, rolled to the right, and collided with terrain. The pilot said there were no mechanical deficiencies with the gyroplane, and the accident could have been prevented if he was 'better rested and mentally sharp.'

Factual narrative

On November 3, 1998, at 0950 eastern standard time, a homebuilt RAF-2000 gyroplane, N52BP, was substantially damaged after a loss of control and collision with terrain during landing at the Doylestown Airport (DYL), Doylestown, Pennsylvania. The certificated private pilot was not injured. Visual meteorological conditions prevailed for the local personal flight that originated at DYL approximately 0910. No flight plan was filed for the flight conducted under 14 CFR Part 91.

In a telephone interview, the pilot said he departed on a local flight without obtaining a weather briefing and remained in the traffic pattern for runway 05. He said:

"I was coming in on final for 05 and there was a crosswind from the left and it was kind of gusty. Just before touchdown, I got out of position. I came in on kind of an angle and the wind got under the rotors and rolled me over."

In a written statement, the pilot said he completed two takeoffs and landings and performed a go-around on the third approach. He said he departed the pattern for spacing and re-entered the downwind leg for landing on runway 05. According to the pilot:

"I decided that this 3rd landing was going to be my last because my second landing was a little rough because of a crosswind, and I was tired and wasn't concentrating well enough to deal with the crosswind...On final I let the airspeed of my gyro get too slow a few feet above the runway, causing my gyro to make a hard landing. [This] caused my gyro to bounce up into the air a little, and a crosswind coming from the left lifted the left side of the gyro."

The gyro plane rolled to the right, collided with terrain, and came to rest on its left side.

When questioned about the airworthiness of the gyroplane, the pilot stated it was "...performing fine." He said he had a total flight experience of approximately 140 hours; 50 hours of which were in the gyroplane.

In the Recommendation section of the NTSB Form 6120.1/2 (How Could This Accident Have Been Prevented), the pilot said:

"This accident could have been prevented if I was better rested, and was mentally sharp and prepared for any problems. The landing during which I had the accident was going to be my last because I knew I was getting tired and [I] wasn't performing very well in the crosswind."

Winds reported at the Willow Grove Naval Air Station, 10 miles south of Doylestown, were from 010 degrees at 7 knots.

Aircraft

Registration
N52BP
Reported as
Pitcairn RAF 2000
Category
Gyroplane, amateur-built
Serial number
H2-96-7-251
Airframe hours
57
Engine
Subaru EJ22, 130 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Brant Pitcairn
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · June 18, 1998 · 49 hours before
Departed
DYL
Airport
N88 · Doylestown Airport, runway 5, 3,004 × 60 ft, asphalt

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
33
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
147 total · 52 in this make and model · 54 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
10° at 7 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
45 °F, dew point 30 °F
Altimeter
29.00 inHg
Observed at
NXX, 10 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.