CEN14CA280

NTSB accident investigation · Schempp-Hirth Nimbus 3/24.5 · Wallis, TX · June 6, 2014

Accident · Minor injuriesData collectionFinal report
Date
June 6, 2014, 14:06 local (19:06 UTC)
Place
Wallis, TX
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N245ABSchempp-Hirth Nimbus 3/24.5
Defining event
Takeoff: Abrupt maneuver
Weather
Visual (VMC) · Day
Status
Completed · report September 24, 2014
Report
Approved by Office Director
NTSB office
Central Region
FAA report
20140606007939A
Case key
89397

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 maintain direction control of the glider during takeoff in gusty wind conditions.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedSchempp-Hirth NIMBUS 3/24.5: 1 caseAll aircraft: 3,958 casesProbable cause
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationSchempp-Hirth NIMBUS 3/24.5: 1 caseAll aircraft: 1,199 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The glider pilot reported that he was to be towed by a tow plane and make a "no assist launch." The glider's wings were loosely supported by wing stands and the tow rope was attached from the tow plane to the glider. When the slack was out of the tow rope, the glider pilot made a radio call "Go, go, go" to the tow pilot. The glider began to lift off from the grass runway when pilot noticed that the tow plane moved left laterally from what he assumed was a gust of wind. The tow pilot corrected back to the right and the glider pilot readied to do the same. When the glider entered the area of suspected wind gust, it suddenly ascended about 8 feet and the left wing lifted. The pilot applied full left aileron and left rudder and forward pressure on the control stick in order to descend and regain the correct flight path. The left wing continued to lift so the glider pilot released the tow rope as the glider made a 30 degree right turn. The glider exited the area of suspected wind gust and the glider pilot was unable to maintain directional control and the glider impacted the runway. The glider sustained substantial damage to the rear fuselage and empennage. He also reported that there were no mechanical malfunctions or failures with the glider that would have precluded normal operation.

Factual narrative

The glider pilot reported that he was to be towed by a tow plane and make a "no assist launch." The glider's wings were loosely supported by wing stands and the tow rope was attached from the tow plane to the glider. When the slack was out of the tow rope, the glider pilot made a radio call "Go, go, go" to the tow pilot. The glider began to lift off from the grass runway when pilot noticed that the tow plane moved left laterally from what he assumed was a gust of wind. The tow pilot corrected back to the right and the glider pilot readied to do the same. When the glider entered the area of suspected wind gust, it suddenly ascended about 8 feet and the left wing lifted. The pilot applied full left aileron and left rudder and forward pressure on the control stick in order to descend and regain the correct flight path. The left wing continued to lift so the glider pilot released the tow rope as the glider made a 30 degree right turn. The glider exited the area of suspected wind gust and the glider pilot was unable to maintain directional control and the glider impacted the runway. The glider sustained substantial damage to the rear fuselage and empennage. He also reported that there were no mechanical malfunctions or failures with the glider that would have precluded normal operation.

Aircraft

Registration
N245AB
Reported as
Schempp-Hirth Nimbus 3/24.5
Category
Glider
Serial number
65
Built
1984
Airframe hours
1,815
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Coggins David L
Registered owner
Coggins David L
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 5, 2014
Departed
TE71 · Wallis, TX
Destination
TE71 · Wallis, TX
Airport
TE71 · Ghsa-Wallis Glideport, runway 18, 4,000 × 125 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
57
Injuries
Minor
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, With waivers/limitations
Seat
Single
Restraint
3-point
Flight hours
2,782 total · 477 in this make and model · 2,645 as pilot in command · 30 in the last 90 days · 16 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
170° at 11 knots, gusting 18
Visibility
10 statute miles
Lowest ceiling
4,100 ft broken
Temperature
90 °F, dew point 73 °F
Altimeter
29.95 inHg
Observed at
KSGR, 19 nm away

Docket · 3

The files NTSB released with the investigation on September 15, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 855 KB in all.

FAA reports on this event · 1

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