LAX98LA221

NTSB accident investigation · Rolladen-Schneider LS-6 · Llano, CA · July 5, 1998

Accident · Serious injuriesLimited investigationFinal report
Date
July 5, 1998, 13:35 local (20:35 UTC)
Place
Llano, CA
Injuries
1 serious
Damage
Destroyed
Phase of flight
Initial climb
Aircraft
N6686Rolladen-Schneider LS-6
Weather
Visual (VMC) · Day
Status
Completed · report February 22, 2001
Report
Approved by Office Director
FAA report
19980705015849A
Case key
30138

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 failure of the pilot to attach the aileron quick disconnect fitting during assembly of the glider and his inadequate preflight inspection.

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 flightTakeoff - initial climb
Flt control syst,aileron control cable/rod - not connectedCause
Maintenance,installation - inadequatePilot in commandCause
Aircraft preflight - inadequatePilot in commandCause
Aircraft control - not possible
In flight collision with terrain/waterDescent - uncontrolled

Analysis

The glider was towed aloft and witnesses observed the right wing oscillating. After release about 400 to 500 feet agl, the glider went into a right spiral and impacted the ground. The airport owner examined the glider after the accident and reported that the quick disconnect fitting for the right aileron was found disconnected. The pilot had reassembled the glider on the morning of the accident and did not perform a control continuity check prior to takeoff.

Factual narrative

On July 5, 1998, at 1335 hours Pacific daylight time, a Rolladen-Schneider LS-6 glider, N6686, collided with the ground during the takeoff initial climb at the Crystal Gliderport in Llano, California. The glider was destroyed and the pilot/owner, the sole occupant, suffered serious injuries. The local area personal flight was originating at the time of the accident and no flight plan was filed. Visual meteorological conditions prevailed.

The airport owner observed the accident sequence and reported that on the initial takeoff roll, the right aileron and right wing were oscillating. He further reported that as the glider pilot rotated to about 10 feet agl, both wings appeared to be oscillating violently. Approximately 400 to 500 feet agl, the glider pilot released from the tow plane and went into a right spiral and impacted the ground. The airport owner opined that the glider pilot may not have released sooner because he may have attributed the oscillations to turbulence.

The airport owner reported that he examined the glider after the accident. He stated that the glider is equipped with quick disconnect fittings on the control system located in the wing center section that allow it to be disconnected and reconnected as the wings are removed or installed. The right aileron fitting was found disconnected.

The pilot reassembled the glider on the morning of the accident flight and witnesses did not see him perform a control continuity check prior to takeoff. The pilot does not remember the accident or the events leading up to it.

Aircraft

Registration
N6686
Reported as
Rolladen-Schneider LS-6
Category
Glider
Serial number
6002
Airframe hours
904
Engine
unknown
Damage
Destroyed
Flight
Personal · Part 91
Registered owner
Hannes Linke
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 19, 1998 · 7 hours before
Departed
LO1
Airport
LO1 · Crystal Gliderport, runway 25, 2,500 × 400 ft

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
58
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Seat
Center
Flight hours
4,186 total · 550 in this make and model · 9 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 46 °F
Altimeter
29.00 inHg
Observed at
PMD, 12 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.