Cirrus SR20 N526CD

Summary

On 9 January 2006 at about 21:32 local time, a Cirrus SR20 registered N526CD, operated by Gene Hudson Flight Training, was involved in an accident near Lancaster, California, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

9 January 2006 at 21:32

Classification

Accident

Location

Lancaster, California, United States

Nearest airport

General Wm J Fox Airfield (WJF)

Coordinates

34.7508, -118.1956

Aircraft

Cirrus SR20

Registration

N526CD

Category

Airplane

Engines

1

Operator

Gene Hudson Flight Training

Operating rule

Part 91: General Aviation

Purpose of flight

Instructional

Phase of flight

Not recorded

Route

Van Nuys → Lancaster

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

LAX06FA087

2 people died.

The student pilot's failure to maintain an adequate airspeed while maneuvering, and, the flight instructor's inadequate supervision of the flight. A factor in the accident was the strong tailwind encountered as the airplane turned from an upwind to a downwind during the teardrop maneuver.

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

Read the full NTSB narrative

While simulating an engine failure on climb-out, the airplane was observed to enter a left teardrop maneuver as it attempted to return to the airport. During the turn, the airplane stalled, entered a spin, and impacted level terrain 1 nautical mile northeast of the departure end of runway 06. The reported winds were 060 degrees at 15 knots. According to the air traffic controller working the local control position, after completing several touch-and-go landings on runway 06, the instructor requested the first of two teardrop return to runway engine-out maneuvers. During the first one, the airplane made a left teardrop 180-degree turn as it attempted to land on runway 24. During the turn, the airplane appeared to lose a significant amount of altitude. The controller stated that the airplane recovered prior to landing, and then executed a go-around to reenter the traffic pattern. During the second attempt, the airplane again entered a teardrop turn to the left and then "spin to the ground." An examination of the wreckage revealed that the airplane impacted the terrain in a 70-degree nose down, left wing low attitude. All flight control surfaces, engine, propeller, and Cirrus Airframe Parachute System (CAPS) components were located at the site. The engine and propeller were embedded in the ground approximately 2 feet, and all three propeller blades exhibited rotational scoring. Recorded data was retrieved from the Avidyne Primary Flight Display (PFD) and Multi-Function Display (MFD). The data log retrieved for the accident flight included data from a time stamp of 12:17:36 to 13:32:00 on January 9, 2006. The next scheduled data-logging event would have been at 13:33:00; however, the unit operation ceased prior to reaching the next recording point. At the last data sampling point, the engine rpm (revolutions per minute) was at 2,680 rpm, the engine manifold pressure was 27.5 inches, and the airplane electrical bus voltage was 27.5 volts. The recorded data did not show any engine or system anomalies. The information from the download of the MFD was consistent with the visual information provided by witnesses.

Quoted verbatim from the NTSB record.