Foreign Type Certificate Details
Type Certificate: Number A00009CH
Issued by: Federal Aviation Administration
Manufacturer: Cirrus Design Corporation
Model: SR20 SR22
Engines: Teledyne Continental IO-360-ES Teledyne Continental IO-550-N
Propellers: Hartzell BHC-J2YF-1BF/F7694 Hartzell PHC-J3YF-1RF/F7694
Hartzell PHC-J3YF-1xF/F7392-1
MCTOW 2900 lb. 3400 lb.
3000 lb. (s/n 1148 and on, or with SB 20-01-00 embodied)
Noise Category: FAR 36
The certification basis of the Cirrus SR20 is Part 23 of the Federal Aviation Regulations
effective February 1, 1965, as amended by 23-1 through 23-47, except some specified
paragraphs are up to Amendment 23-52. The certification basis of the Cirrus SR22 is Part
23 of the FARs effective February 1, 1965, as amended by 23-1 through 23-53, except for
§23.301 at Amendment 23-47 and three paragraphs being not applicable.
The Cirrus is the first type certificated aircraft equipped with a ballistic recovery parachute
(called Cirrus Airframe Parachute System CAPS) as basic equipment, and a Special
Condition was applied by the FAA to this feature In addition, an equivalent level of safety
finding was required by Cirrus to allow the provision of CAPS to be used in lieu of
meeting stall recovery criteria. Another ELOS was made for the engine controls, similar to
one granted in the past to Cessna. These have been reviewed and accepted by the CAA.
This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21.41,
as FAR 23 is the basic standard for Normal Category Airplanes called up under Part 21
Appendix C. There are no non-compliances and no additional special conditions have been
prescribed by the Director under §21.23.
http://www.caa.govt.nz/aircraft/Type...us_SR20-22.pdf
cant get onto faa website but caa nz refers...