OK, I have a bit more time to elaborate this morning. As has been said, the apparent accident rate is not indicative of the actual comparison with other models in the same class / category. There has been a lot of study and comparison in this area and based on fleet hours flown, the rate is on par with the C-182, Beech A-36, etc. The obvious question remains, why? The Cirrus should be the safest aircraft to fly given all its safety features and advanced avionics, but it is not. Something to keep in mind is that Cirrus (for the most part) are used as X-country aircraft meaning that the flights are often long and cover a lot of ground. This exposes the pilots to changing and often challenging weather conditions that pilots of other aircraft in the same category often do not encounter as frequently. Couple this with the advanced avionics, FIKI systems, and BRS parachute and quite often the aircraft is much more capable than the pilots and / or the pilots are lulled into a false sense of capability both for the aircraft and themselves.
Cirrus did / does an excellent job of designing the "stupid" our of the aircraft meaning they have taken a lot of the workload off of the pilot to help prevent "stupid mistakes". For instance, the Cirrus has a constant speed propeller, but it is automatically controlled by an interconnection with the throttle. If equipped with the DFC90 autopilot the aircraft will right itself from any attitude back to wings level at the touch of a button and never exceed 2.5 g's. (Dave Hirschman tested this in a roll and loop scenario with excellent results and documented his findings in a video log)
Everything is digital and easy to find with just the touch of a button. If a pilot wants to run ROP or LOP all he has to do is tell the computer which he chooses and then pull the mixture back until the light illuminates that he has done so. The wing has been designed as "stall resistant" and it does a great job, but is not stall proof. The Cirrus will fly rock steady all the way into a stall with ample warning and maintain excellent aileron authority...it reminds me of the Maule in its stall characteristics. When all else fails, pull the parachute.
In my opinion the reason for the accident rate not being any better than its competitors is due to the pilot personalities that it attracts coupled with the false sense of security the Cirrus will lull pilots into. When all is going smoothly you can sit back and enjoy the ride, but when it hits the fan you had better have the basic stick and rudder skills to fly without the magic avionics. This (in my opinion) is what is lacking in a large majority of the Cirrus pilot community. They have learned or become so accustom to the glass and ease of the aircraft that their stick & rudder skills have either atrophied or never developed. When the glass goes dark, they have trouble navigating with the backup round dials and dual 430 GPS units…a major handicap to be sure.

If the crosswinds get gusty or they are a bit fast on final, they often do not know how to compensate. Rudder is only used to assist the brakes in turning the aircraft on the ground. Yes I meant to say assist the brakes to turn the aircraft…this is why they have hot brake issues…if they would use the rudder and assist it with limited braking it would not be a problem. As I mentioned before, Cirrus accidents would drop considerably if they were required to obtain a TW rating (again my opinion).
With regards to the BRS…the chute has successfully saved lives as low as 400 ft in normal flight conditions, or 1,000 feet in a spin condition. It has been pulled inverted and saved the aircraft successfully. There has only been one instance that I know of where the chute departed the aircraft and that one was pulled at speeds in excess of 180 kts. There is no speed limit for activating the BRS, only a max demonstrated speed of 133 kts. By the way, if you are coming down under canopy you will be doing so at around 1,700 fpm depending on the weight of the aircraft.
The Cirrus is a nice aircraft to fly and easy to do so, although not very capable in the load carrying department. It has its purpose and it does it fairly well, but in comparison to the Corvalis I think it is inferior…again just my opinion. The Corvalis is built much better with noticeable craftsmanship differences, controls are smoother, roomier cabin, and much better load carrying capability. Where Cirrus took the sales lead is in their marketing.
That should give you enough topics for further discussion…I have attached copies of the POH concerning the Spins and CAPS deployment.


