C
IRRUS
D
ESIGN
S
ECTION
4: N
ORMAL
P
ROCEDURES
SR20
N
ORMAL
P
ROCEDURES
P/N 11934-005
4-7
• N
OTE
•
Verify bolt located under the inboard edge of aileron is secured
with safety wire.
d. Hinges, actuation arm, bolts, and cotter pins........................SECURE
6. Right Wing Tip
a. Tip..................................................................................ATTACHMENT
b. Wing Tip Light and Lens................. CONDITION AND SECURITY
c. Fuel Vent (underside) ............................................ UNOBSTRUCTED
7. Right Forward Wing and Main Gear
a. Leading Edge and Stall Strips.......................................... CONDITION
b. Fuel Cap .................................... CHECK QUANTITY AND SECURE
c. Fuel Drains (2 underside)............................... DRAIN AND SAMPLE
d. Wheel Fairings ...........SECURITY, ACCUMULATION OF DEBRIS
e. Tire....................................CONDITION, INFLATION, AND WEAR
f. Wheel and Brakes ............................. FLUID LEAKS, EVIDENCE OF
OVERHEATING, GENERAL CONDITION, AND SECURITY
g. Chocks and Tiedown Ropes...................................................REMOVE
8. Nose, Right Side
• CAUTION •
The engine must not be operated with less than six quarts of oil in
the sump (dipstick indication). Seven quarts is recommended for
extended flights.
a. Engine Oil .............................................CHECK 6-7 QUARTS, LEAKS
b. Engine Oil Dipstick/Filler Cap & Door..................................SECURE
c. Ice Inspection Light.......................... CONDITION AND SECURITY
d. Cowling ......................................................ATTACHMENTS SECURE
e. Exhaust Pipe ..........CONDITION, SECURITY, AND CLEARANCE
(Continued on next page)
(Continued)
Reissue A
