No fatalities

16 Dec 2013: MAARTEN H VERSTEEG ZENITH 601XL(B) NO SERIES (N581SL) — VERSTEEG MAARTEN H — Leakey, TX

Leakey, TX, United States

On 16 Dec 2013, a MAARTEN H VERSTEEG ZENITH 601XL(B) NO SERIES (registration N581SL) operated by VERSTEEG MAARTEN H was involved in an aviation accident near Leakey, TX. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain control of the airplane after the canopy opened on takeoff. Contributing to the accident was the pilot’s failure to properly secure the canopy latch before takeoff. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On December 16, 2013, an experimental-homebuilt Versteeg Zenith 601XL(B) (N581SL) was substantially damaged after a hard landing following canopy opening shortly after takeoff in Leakey, Texas. The pilot was seriously injured.

Event Overview

On December 16, 2013, at 1634 central standard time, an experimental-homebuilt Versteeg Zenith 601XL(B) (registration N581SL) was substantially damaged when it collided with terrain shortly after takeoff from Real County Airport (49R), Leakey, Texas. The private pilot, who was also the builder and registered owner, was seriously injured. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under 14 CFR Part 91.

Pilot Account

The pilot reported that shortly after takeoff, when the airplane was about 100 feet above the runway, the canopy "popped" open. He stated that this created a large amount of drag, so he pushed the control stick forward to gain airspeed. The airplane then landed hard, resulting in substantial damage to the motor mounts, both wings, and the fuselage.

Flight Data Analysis

The airplane was equipped with a Dynon Skyview-D1000 primary flight display (PFD). The unit was sent to the National Transportation Safety Board (NTSB) vehicle recorders laboratory, where data from the accident flight was extracted and plotted. The data revealed that the accident flight was about 18 seconds long from departure until impact. The canopy latch was tied into the PFD and recorded the canopy latch becoming unsecured about 14 seconds into the flight.

Postaccident Examination

A Federal Aviation Administration (FAA) inspector conducted a postaccident examination of the airplane and found nothing mechanically wrong with the canopy latch that would have precluded it from properly securing the canopy.

Contributing factors

Causes

PilotPerformance/control parameters — Not attained/maintained

Other contributing factors

Passenger/crew doors