C
IRRUS
D
ESIGN
S
ECTION
4: N
ORMAL
P
ROCEDURES
SR20
N
ORMAL
P
ROCEDURES
P/N 11934-005
4-9
Before Engine Start
13.Left Wing Trailing Edge
• N
OTE
•
Verify bolt located under the inboard edge of aileron is secured
with safety wire.
a. Hinges, actuation arm, bolts, and cotter pins........................SECURE
b. Aileron Gap Seal ................................................................... SECURITY
c. Aileron ...................................................FREEDOM OF MOVEMENT
d. Flap and Rub Strips (if installed).... CONDITION AND SECURITY
(Continued)
1. Preflight Inspection ............................................................... COMPLETED
• WARNING •
Ensure that the airplane is properly loaded and within the AFM’s
weight and balance limitations prior to takeoff.
2. Weight and Balance ......................................... VERIFY WITHIN LIMITS
3. Emergency Equipment............................................................. ON BOARD
4. Passengers ........................................................................................BRIEFED
• N
OTE
•
Ensure all the passengers have been fully briefed on smoking, the
use of the seat belts, doors, emergency exits, egress hammer, and
CAPS.
Verify CAPS handle safety pin is removed.
5. Seats, Seat Belts, and Harnesses ..........................ADJUST AND SECURE
• WARNING •
Crew seats must be locked in position and control handles fully down
before flight. Ensure seat belt harnesses are not twisted.
Reissue A
