Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook page 53

BEECHCRAFT Sport III
Musketeer A23- 19. 1 9A
Section 11
Limitations
On Left Cabin Door or Left Side Panel (CAS) (MB-289 thru
MB-460)
(Airplanes prior to MB -289 when BEECHCRAFT Kit
23-5003 is installed)
THIS AIRPLANE MUST BE OPERATEO IN COMPLIANCE
WITH THE OPERATING UMITATIONS STATEO IN THE
FORM OF PLA C ARDS . MARKING S AND MANUALS .
NORMAL C ATE GORY
M A XIMUM OESIGN WfiGHT
REFER TO W(IGHT ANO SALANCE DATA
fOR LOAOING INSTRUCTIONS
~ LIGl-IT MANEUVERING LOAO F.G.CTOR
MAXIMUM MANEUV[RING SPEED
2260 LIS
fLAPS UP
'łl
8 - 1 9
DOWN + l 9
1 32 M P H
NO A C ROBATIC MANEUVERS
IN GLUDING SPINS APPROVEO
UliLITY C ATE G OR Y
MAXIMUM OESIGN Wf.IGHT
REFER TO WEIGHT ANO BALANCE DATA
fO R LOAOING INSTRUCTIQNS
FLIG I.łf
MANEUVERING LOAO FACTOR
2030 LBS
FLAPS UP +4 4 - 2 2
DOWN + 2 2
N O ACROBATI C MANEUVERS APPAOVED
EXCEPT THOSE USTED BELOW .
MANEUve R M A xtMUM ENT Rv SPEEO
CHAN OHlES 133 MPH
LAlY EIGI-ITS 133 MPH
STEEP TURNS 133
MPH
STALLS IEXC EPT WI-I IP STAlLS I SlOW OECELER AliON
NOTE M A XIM UM AlfllUOE lOSS DURING STAll
On Left Cabin Door or Left S ide Panel (MB-1 thru MB-252
after compliance with BEECHCRAFT Service Bulletin 67-
23 Revision 1)
NOTE:
@
MAXIMUM ALTITUDE LOSS DURING STALL 300 FT .
Et)
October 1 979
2-21