IAD00LA046

NTSB accident investigation · Schweizer SGS 2-33A · Sterling, MA · May 29, 2000

Accident · No injuriesLimited investigationFinal report
Date
May 29, 2000, 13:30 local (17:30 UTC)
Place
Sterling, MA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N1225SSchweizer SGS 2-33A
Weather
Visual (VMC) · Day
Status
Completed · report May 8, 2001
Report
Approved by Office Director
FAA report
20000529040739A
Case key
49303

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 failure to attain a proper touchdown point.

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.

OverrunLanding - flare/touchdown
Proper touchdown point - not attainedPilot in commandCause
On ground/water collision with objectLanding - aborted

Analysis

The pilot entered a right traffic pattern for Runway 16. At the midfield point, on the downwind leg of the traffic pattern, the glider was 1,000 feet above the ground, and the pilot extended the spoilers. The base leg of the traffic pattern was performed about 700 feet above the ground. When the glider was turned onto the final approach, the right wing was kept down and left rudder was applied to initiate a slip. The pilot determined the slip was ineffective, rolled the glider level for a moment, and then entered the slip again. The glider touched down '90% down the runway,' and traveled off the end. The glider became airborne again, turned to the right, and touched down a second time on a road. The glider impacted several road signs with both wings, before turning 180 degrees and coming to rest. The pilot stated that the reason for the accident was an 'ineffective slip.'

Factual narrative

On May 29, 2000, about 1330 Eastern Daylight Time, a Schweizer SGS 2-33A Glider, N1225S, was substantially damaged during landing at the Sterling Airport (3B3), Sterling, Massachusetts. The student pilot was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the instructional flight conducted under 14 CFR Part 91.

According to the student pilot, he took off from 3B3 and was towed to an altitude of 2,700 feet. He reported the weather was "fairly cloudy," and he "could not find any lift." After approximately 15 minutes, the pilot returned to the airport and performed two 360 degree turns to enter a right traffic pattern for Runway 16. At an altitude of 1,200 feet above the ground, the pilot noticed the glider was higher than it should be. At the midfield point, on the downwind leg of the traffic pattern, the glider was 1,000 feet above the ground, and the pilot extended the spoilers. The base leg of the traffic pattern was performed about 700 feet above the ground. When the glider was turned onto the final approach, the right wing was kept down and left rudder was applied to initiate a slip.

The student pilot further stated, "I didn't feel the usual vibrations or hear the usual noise that I'm used to hearing when I slip the airplane." He rolled the glider level for a moment, and then entered the slip again. After flying past "10-20%" of the 3,010 foot long runway, the pilot felt the slip wasn't working, and straightened out the glider. The glider touched down "90% down the runway," and the pilot realized his speed was too fast. The glider became airborne again, turned to the right, and touched down a second time on a road located about 10 feet below the runway elevation. The glider proceeded through an embankment and hit several road signs with both wings, before turning 180 degrees and coming to rest.

The pilot stated that the winds were not a factor in the accident. He reported that a check of the wind sock before takeoff revealed it was "barely off the pole." The pilot additionally stated the reason for the accident was an "ineffective slip."

A Federal Aviation Administration inspector who examined the glider, reported that the skid mount under the nose was broken, the tailwheel was broken, and both wings displayed impact damage.

The winds reported at 1354, at an airport 10 miles away, were from 090 degrees at 9 knots.

Aircraft

Registration
N1225S
Reported as
Schweizer SGS 2-33A
Category
Glider
Serial number
211
Engine
unknown
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Greater Boston Soaring Club
Airworthiness certificate
Standard, Normal
Departed
3B3
Airport
3B3 · Sterling Airport, runway 16, 3,010 × 40 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
38
Certificate
Student
Medical
Unknown
Seat
Front

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 9 knots
Visibility
10 statute miles
Lowest ceiling
3,500 ft broken
Temperature
57 °F, dew point 45 °F
Altimeter
30.00 inHg
Observed at
ORH, 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.