Another Cirrus 'chute deployment

"Dan Luke" wrote in message
...

Meanwhile, what backup have you got for your assertion that "None of the
Cirrus models will recover from a spin?" Certification standards
applied to the airplanes don't count.

All of the manuals contain language similar to the following:
Spins

The SR20 is not approved for spins, and has not been tested or

certified for spin recovery characteristics. The only approved and

demonstrated method of spin recovery is activation of the Cirrus

Airframe Parachute System (See CAPS Deployment, this section).

Because of this, if the aircraft “departs controlled flight”, the CAPS

must be deployed.

While the stall characteristics of the SR20 make accidental entry into a

spin extremely unlikely, it is possible. Spin entry can be avoided by

using good airmanship: coordinated use of controls in turns, proper

airspeed control following the recommendations of this Handbook, and

never abusing the flight controls with accelerated inputs when close to

the stall (see Stalls, Section 4).

If, at the stall, the controls are misapplied and abused accelerated

inputs are made to the elevator, rudder and/or ailerons, an abrupt wing

drop may be felt and a spiral or spin may be entered. In some cases it

may be difficult to determine if the aircraft has entered a spiral or the

beginning of a spin.

• WARNING •

In all cases, if the aircraft enters an unusual attitude from

which recovery is not expected before ground impact,

immediate deployment of the CAPS is required.

The minimum demonstrated altitude loss for a CAPS

deployment from a one-turn spin is 920 feet. Activation at

higher altitudes provides enhanced safety margins for

parachute recoveries. Do not waste time and altitude trying to

recover from a spiral/spin before activating CAPS.

Inadvertent Spin Entry

1. CAPS
.................................................. ...........................
...... Activate