Beechcraft C23 SUNDOWNER 180 Pilot Operating Handbook page 55

BEECHCRAFT Sundowner
180
Section
il
C23
(M-1285
and After)
Limitations
On
Instrument Panel in Full View of Pilot (M-1285
through
M-1493, unless modified by Kit No. 23-4007-iSand
Service
Instructions No. 0619-090)
HIS
AIRPLANE
MUST BE OPERATED AS
E
NORMAL OR UTILITY CATEGORY AIRPLANE.
INTENTIONAL SPINS ARE PROHIBITED.
NO
ACROBATIC MANEUVERS APPROVED EXCEPT:
CHANDELLES, LAZY EIGHTS, STEEP TURNS,
ND STALLS (EXCEPT WHIP STALLS)."
On
Left Cabin Door or Left
Side
Panel
(M-1971, M-1980 and after) (CAS)
THIS AIRPLANE MUST BE
OPERATED IN
COMPLIANCE
WITH THE
OPERATING LIMITATIONSSTATED
IN THE
FORM OF
PLACARDS, MARKINGS AND MANUALS.
NORMAL CATEGORY
MAXIMUM DESIGN WEIGHT
2450
LBS
REFER TO WEIGHf AND BALANCE DATA
FOR LOADING INSTRUCTIONS
FLIGHT MANEUVERING LOAD FACTOR FLAPS UP
+3.8
-1.9
DOWN
+1.9
MAXIMUM MANEUVERING SPEED 118 KTS/136 MPH
NO
ACROBATIC MANEUVERS
INCLUDING
SPINS APPROVED
UTILITY CATEGORY
MAXIMUM DESIGN WEIGHT
2030 LBS
REFER TO WEIGHT AND BALANCE DATA
FOR
LOADING
INSTRUCTIONS
FLIGHT
MANEUVERING
LOAD FACTOR
FLAP$ UP
-(-4.4
-2.2
DOWN
+2,2
NO
ACROBATIC MANEUVERS
APPROVED
EXCEPT THOSE LISTED BELOW:
MANEUVER
MAXIMUM ENTRY SPEED
CHANDELLES 116 KTS/133 MPH
LAZY EIGHTS
116 KTS/l33 MPH
STEEP TURNS
116 KTS/133 MPH
STALLS lEXCEPT WHIP STALLS)
SLOW DECELERATION
NOTE: MAXIMUM ALTITUDE LOSS DURING STALL 300 FT
February
1979
2-21