C
D
IRRUS
ESIGN
SR22
Descent
1. Altimeter ....................................................................................................SET
2. Cabin Heat/Defrost ............................................................. AS REQUIRED
3. Landing Light ............................................................................................ ON
4. Fuel System ........................................................................................ CHECK
5. Mixture.................................................................................. AS REQUIRED
6. Brake Pressure ................................................................................... CHECK
Before Landing
1. Seat Belt and Shoulder Harness .....................................................SECURE
2. Fuel Pump........................................................................................... BOOST
3. Mixture.................................................................................. AS REQUIRED
4. Flaps ....................................................................................... AS REQUIRED
5. Autopilot ............................................................................... AS REQUIRED
Landing
Landings should be made with full flaps. Landings with less than
full flaps are recommended only if the flaps fail to deploy or to
extend the aircraft's glide distance due to engine malfunction.
Landings with flaps at 50% or 0%: power should be used to achieve
a normal glide path and low descent rate. Flare should be mini-
Normal Landing
1. Flaps ......................................................................................................... 100%
2. Airspeed ..................................................................................... 80 - 85 KIAS
3. Power Lever .......................................................................... AS REQUIRED
After touchdown:
4. Brakes .................................................................................... AS REQUIRED
Normal landings are made with full flaps with power on or off. Surface
winds and air turbulence are usually the primary factors in determining the
most comfortable approach speeds.
P/N 13772-006
Reissue A
S
• CAUTION •
mized.
4: N
ECTION
ORMAL
N
ORMAL
P
ROCEDURES
P
ROCEDURES
4-21