N520RJ

Substantial
None

SCHEMPP-HIRTH DISCUS CSS/N: 217CS

Accident Details

Date
Saturday, October 8, 2022
NTSB Number
ERA23LA013
Location
Woodstock, VA
Event ID
20221010106089
Coordinates
38.882050, -78.557789
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Improper repair of a crack by maintenance personnel, which resulted in a subsequent failure of the glider canopy.

Aircraft Information

Registration
Make
SCHEMPP-HIRTH
Serial Number
217CS
Engine Type
None
Year Built
1996
Model / ICAO
DISCUS CSDISC
Aircraft Type
Glider
No. of Engines
0
Seats
1
FAA Model
DISCUS CS

Registered Owner (Current)

Name
SKYLINE SOARING CLUB INC
Address
424A SOUTH ST # 172
City
FRONT ROYAL
State / Zip Code
VA 22630-2116
Country
United States

Analysis

On October 8, 2022, about 0950 eastern daylight time, an experimental Schempp-Hirth Discus CS glider, N520RJ, was substantially damaged when it was involved in an accident near Woodstock, Virginia. The private pilot was not injured. The glider was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the glider was at 3,700 ft mean sea level when the canopy suddenly, without warning, separated from the glider. The pilot double-checked the canopy latch and jettison handle and confirmed that he did not jettison the canopy. He subsequently landed uneventfully at his intended destination airport.

Review of maintenance records revealed a work order dated August 9, 2020, which stated “…Found canopy crack at rear hinge along frame and stop holed crack….”

Separated sections of the glider canopy were recovered and forwarded to the National Transportation Safety Board Materials Laboratory, Washington, D.C. Metallurgical examination revealed that the drilled hole appeared to halt progression of the original crack along its initial propagation direction. However, both the primary separation crack and a secondary crack propagated out of the hole in diametrically opposite directions, consistent with occurrence due to a stress state along the same plane. Additionally, both cracks propagated from internal surface corners of the hole, consistent with the corners acting as stress risers that facilitated crack initiation (for more information, see Materials Laboratory Factual Report in the public docket for this accident).

According to a representative from the glider manufacturer, the canopy was made from plexiglass and there are no manufacturer instructions for repairing cracks in the canopy. Additionally, it has been common practice for decades that cracks in the plexiglass are drilled out to stop the crack progression as a temporary solution; however, for a proper repair, the canopy must be removed and re-glued.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA23LA013