ERA21LA156

NTSB accident investigation · Schempp-Hirth K G MINI-NIMBUS C · Groveland, FL · March 16, 2021

Accident · Serious injuriesClass 3 · LimitedFinal report
Date
March 16, 2021, 12:52 local (16:52 UTC)
Place
Groveland, FL
Injuries
1 serious
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N16MGSchempp-Hirth K G MINI-NIMBUS C
Defining event
Takeoff: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20210316022229A
Case key
102767

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

On this page

Probable cause

The pilot’s unsuccessful initial attempt to release from the tow plane at the start of an unstable takeoff roll, which resulted in a runway excursion and collision with a parked vehicle. Contributing to the severity of the accident was the vehicle’s proximity to the active runway.

Findings · 2

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.

Airport facilities/design: ground support/equipmentEnvironmental issues › Operating environment · Contributed to outcomeSchempp-Hirth K G MINI-NIMBUS C: 1 caseAll aircraft: 6 casesProbable cause

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

On the day of the accident, the pilot was participating in a glider competition event. During the takeoff roll under aerotow, the glider yawed to the left as the left wingtip dropped to the ground. As the glider approached an access road east of the runway, the pilot attempted to release from the tow plane; however, his hand slipped off the release handle. He was subsequently able to release from the tow plane and attempted to turn and stop but was unsuccessful. The glider struck an unoccupied parked pickup truck. The pilot was seriously injured, and the glider sustained substantial damage to the forward fuselage and right wing. The pilot reported that there were no preimpact mechanical malfunctions or failures that would have precluded normal operation. If the pilot’s initial attempt to release from the tow plane had been successful, it likely would have allowed him more time to reduce speed or change course before the collision. The reason for the left yaw was not identified. The truck was parked in or near a strip along the left side of the runway that was to remain clear of personal vehicles during landing operations. Had the truck instead been parked in the designated parking area, the collision may have been prevented or its severity may have been reduced.

Factual narrative

On March 16, 2020, at 1252 eastern daylight time, an experimental Schempp-Hirth K G Mini Nimbus C glider, N16MG, was substantially damaged during a glider competition held at the Seminole Lake Gliderport in Groveland, Florida. The pilot sustained serious injuries. The glider was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. A witness described that the glider was on the takeoff roll on runway 18 under aerotow when the left wing dipped and struck the ground, and the glider began to swerve to the left. The pilot released from the towplane and the glider departed the left side of the turf runway. The glider crossed over a paved airport road oriented parallel to the runway, and impacted an unoccupied parked pickup truck, located about 500 ft from the north end of runway 18 and about 150 ft left of the runway centerline. The pilot reported that his glider was lined up on the left side of the runway with the left wingtip about 1 ft from the edge of the runway. Immediately after the towplane began to roll, the glider yawed to the left as the left wing dropped to the ground. As the glider approached the access road, he attempted to release from the tow plane; however, his hand slipped off the release handle. He was subsequently able to release and then attempted to turn and stop before colliding with the truck, but he was unsuccessful. He reported that there were no mechanical malfunctions with the glider that would have precluded normal operation. The towplane pilot reported that the takeoff was performed on the east side of runway 18, and that the line up, rope hookup, and rope tensioning were normal. The wind was from the south at 12 to 15 knots. The tow pilot aborted the takeoff after he observed the glider’s release from the tow rope. Examination of the accident site by a Federal Aviation Administration inspector revealed that the glider sustained substantial damage to the forward fuselage, which was crushed and separated forward of the pilot’s seat. The right wing sustained leading edge impact damage that extended aft of the wing spar, between 1 and 4 ft outboard of the wing root. Flight control continuity was established from the cockpit controls to the control surfaces. The pilot reported that the truck was parked in an area where the event organizers had asked participants to not park. The truck was parked perpendicular to the runway, about 30 ft (to the east, or left) from the single-lane access road that ran parallel to the runway at the runway’s left edge. A review of the guidance materials provided to the event participants revealed a diagram (see figure) that depicted hashed areas on either side of the runway which were denoted as “landing rolloff areas” that were to be clear of personnel and vehicles during landing operations. The width of the hashed areas was not specified. The text portion of the parking guidance indicated that parking was permitted “before the launch” on either side of the runway “at thenorth end.” An approved trailer parking area was located about 50 ft directly east of the truck against a tree line. Approximate location of Collision with Truck Figure - Diagram of Facility

Aircraft

Registration
N16MG
Reported as
Schempp-Hirth K G MINI-NIMBUS C
Category
Glider
Serial number
104
Built
1979
Airframe hours
1,503
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · July 21, 2020
Destination
Same as departure
Airport
6FL0 · Seminole Lake Gliderport, runway 18, 3,000 × 200 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
60
Injuries
Serious
Certificates
Flight engineer, Airline transport, Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
July 1, 2020
Seat
Single
Restraint
4-point
Flight hours
14,800 total · 248 in this make and model · 10,100 as pilot in command · 200 in the last 90 days · 30 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 13 knots
Visibility
10 statute miles
Temperature
82 °F, dew point 63 °F
Altimeter
30.11 inHg
Observed at
ZPH, 21 nm away

Docket · 6

The files NTSB released with the investigation on June 8, 2023, on NTSB’s docket system: statements, records, photos and specialists’ reports. 12.3 MB 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.