SA 160
AIRCRAFTA I R C R A F T
Symphony
AIRCRAFT
2-9
SECTION 2
LIMITATIONS
2.29 PLACARDS
The following placards must be attached inboard and outboard of the
aircraftintherequiredplaces.
1.Infullviewofthepilot:
WITH FUEL BELOW 12 LITERS (3 U.S. GAL.) IN
EACH WING TANK (”Lo” IND.), POWER ON
DESCENTS WITH FLAPS DOWN ARE
LIMITEDTO10 MINUTES MAXDURATION.
(SEEPOH)
Feb 25, 2005
For IFR
equipped
aircraft
only.
For VFR
equipped
aircraft
only.
OPERATING MODE: NORMAL CATEGORY
FOR FLIGHTS IN VFR, DAY AND NIGHT CERTIFIED
FLIGHTS INTO KNOWN ICING CONDITIONS ARE PROHIBITED!
FLIGHTS IN HEAVY TURBULENT AIR AND
CLOSE TO THUNDERSTORMS ARE PROHIBITED!
SEE THE LIMITATION SECTION IN THE POH
MAXIMUM GROSS WEIGHT:
MANEUVERING SPEED:
MAX. FLAP EXTENDED SPEED:
MAX. DEMONSTRATED CROSSWIND
COMPONENT:
MAXIMUM LANDING WEIGHT:
2150 [lbs]
2042 [lbs]
116 [kts]
90 [kts]
20 [kts]
17 [kts]
TAKEOFF
LANDING
OPERATING MODE: NORMAL CATEGORY
FOR FLIGHTS IN VFR, IFR, DAY AND NIGHT CERTIFIED
FLIGHTS INTO KNOWN ICING CONDITIONS ARE PROHIBITED!
FLIGHTS IN HEAVY TURBULENT AIR AND
CLOSE TO THUNDERSTORMS ARE PROHIBITED!
SEE THE LIMITATION SECTION IN THE POH
MAXIMUM GROSS WEIGHT:
MANEUVERING SPEED:
MAX. FLAP EXTENDED SPEED:
MAX. DEMONSTRATED CROSSWIND
COMPONENT:
MAXIMUM LANDING WEIGHT:
2150 [lbs]
2042 [lbs]
116 [kts]
90 [kts]
20 [kts]
17 [kts]
TAKEOFF
LANDING
To Next Page
Loading...