Aviation Crash Map

Charles Raymond GLASAIR 2SFT N16CD

30 June 1996 · Apalachicola, Florida, United States · No injuries

Summary

On 30 June 1996 at about 14:45 local time, a Charles Raymond GLASAIR 2SFT registered N16CD was involved in an accident near Apalachicola, Florida, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 14:45
Classification
Accident
Location
Apalachicola, Florida, United States
Nearest airport
St George Island (F47)
Coordinates
29.7199, -84.9905
Aircraft
Charles Raymond GLASAIR 2SFT
Registration
N16CD
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Cartersville → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
MIA96LA172

People

Nobody was injured.

On board Died Serious Minor Uninjured
2 0 0 0 2

Probable cause

Inadequate application of throttle input and up elevator input by the pilot-in-command. Contributing to the accident was the in-flight encounter with a downdraft and inadequate design of the airplane by the kit manufacturer.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot stated that she entered the traffic pattern to land on runway 14 with a crosswind from the left of about 10 knots. While on short final approach with partial flaps extended and an indicated airspeed of 90 miles-per-hour, the flight encountered a downdraft. She added only partial power and the airplane landed short of the runway separating the nose landing gear. She further stated that the engine responded when she added power and she only applied a slight pitch up correction when adding power. Examination of the airplane revealed that the 4 AN3-14A bolts that secure the nose gear trunnion attach plate to the nose gear support rib were bent and the threads were stripped. The original prototype engine/propeller combination was approximately 100 pounds lighter than the installed engine/propeller combination but with the same size and number of bolts used to secure the nose gear trunnion attach plate.

Quoted verbatim from the NTSB record.

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