N173SS

Substantial
Serious

Burkhart Grob G103 TWIN ASTIR S/N: 3286

Accident Details

Date
Sunday, December 27, 1998
NTSB Number
DEN99LA028
Location
CANON CITY, CO
Event ID
20001211X11550
Coordinates
38.440254, -105.230270
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The glider pilot's failure to follow proper preflight procedures, and his failure to control the aircraft when the latch opened during flight. A factor was his failure to properly latch the canopy, and to utilize all available runway during the forced landing.

Aircraft Information

Registration
N173SS
Make
BURKHART GROB
Serial Number
3286
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
G103 TWIN ASTIR G103
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
UNKNOWN
Status
Deregistered
City
OKLAHOMA CITY
State / Zip Code
OK 73125
Country
United States

Analysis

On December 27, 1998, at 1115 mountain standard time, a Burkhart Grob Flugzeugbau G103 Twin Astir glider, N173SS, was substantially damaged when it impacted the ground following a forced landing after the canopy opened during initial climb from takeoff at Freemont County Airport, Canon City, Colorado. The commercial pilot received minor injuries and one passenger received serious injuries. Visual meteorological conditions prevailed for the local area personal flight being conducted under Title 14 CFR Part 91, and no flight plan was filed. The flight originated approximately five minutes before the accident.

According to the glider pilot, the passenger "was strapped in and [the] canopy [was] latched in the front seat." He then "latched the canopy in the rear seat and performed a normal pre-takeoff checklist." The tow plane was attached and takeoff was normal. After a positive rate of climb was established, the rear canopy "popped open." When the pilot attempted to close the canopy, the glider ballooned above the tow plane. He then instructed the passenger to pull the tow rope release. He turned to the left in an attempt to land on flatter terrain, and lowered the nose to maintain airspeed. According to the pilot, the glider impacted the ground before he could level out.

According to the passenger and several witnesses, the glider pilot signaled the tow pilot that he was ready for takeoff. However, the departure was halted so that the glider pilot could be given a handheld radio in order for communications to be established between the glider and the tow plane. The glider pilot opened the canopy in order to receive the radio, then re-closed it. The glider pilot then signaled a second time that he was ready for takeoff.

After departure, the passenger stated that the aircraft was 5 to 10 feet above the runway when the canopy latch opened. According to a witness, at approximately 100 feet above the ground (agl), "the glider pitched up steeply, lifting the tail of the tow plane. The glider and tow plane both released the rope which landed near taxiway A3 [located mid-runway]... The glider then traveled approximately 1,500 to 2,000 feet down the runway before turning left and impacting the ground left wing first." According to a witness, the first ground scars where the glider impacted the ground were observed approximately 1,100 feet prior to the end of the paved section of runway 29. In addition, there is another 800 feet of dirt beyond the paved runway prior to the existence of any obstructions.

At the request of the Investigator-In-Charge, an FAA inspector supervised an examination of the rear canopy latch. According to the mechanic who performed the inspection, "the rear canopy latch was found to be operational."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN99LA028