Beechcraft Duchess 76 - Page 51

BEECHCRAFT
Duchess 76
Section II
Limitations
PLACARDS
On Left Cabin
ME-286)
or On
and after}:
)=.
Door (ME-I thru ME-282, ME-284 thru I
Left Cabin Sidewall (ME-283, ME-287
1
1
'3
9
U_
OPERATION LIMITATIONS -----
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY
AIRPLANE IN COMPLIANCE WITH THE OPERATiNG LIMITATION
STATED IN THE FORM OF PLACARDS, MARKINGS AND MANUALS.
MAXIMUM WEIGHT is 3900 LBS. THIS AIRPLANE APPROVED FOR
VFR, IFR, DAY AND NIGHT NON-ICiNG FLIGHT WHEN EOUIPPED IN
ACCORDANCE WITH FAR 91 OR FAR 135.
NO ACROBATIC MANEUVERS INClUDING SPINS APPROVED.
WARNING - TURN OFF STROBE LIGHTS WHEN TAXIING IN
VICINITY OF OTHER AIRCRAFT OR DURING FLIGHT THROUGH
CLOUD, FOG OR HAZE. '
AIRSPEEDS -- .........................
NEVER EXCEED -------------------- 194 KNOTS
MAX.
STRUCTURAL CRUISE ------------- 154 KNOTS
MAX. MANEUVERING ---------------- 132 KNOTS
MAX.
FLAPS 20' ------------------- 120 KNOTS
MAX. FULL DOWN FLAPS 3S' ----------- 110 KNOTS
MAX. LANDING GEAR EXTENSION
--------- 140 KNOTS
MAX. LANDING GEAR RETRACTION -------- 113 KNOTS
ALTITUDE LOST IN ONE ENGINE INOP STAll -----150 FEET
& 10° PITCH DOWN
----i1
eli
8
11
,_ . ..::0,.
Lower Sidewall Adjacent to Pilot:
~
WARNING
ALTERNATE STATIC AIR SOURCE
ON
ALTERNATE
;l
SEE PERFORMANCE
SECTION OF PILOTS
OPERATING
HANDBOOK
FOR AIRSPEED & ALTIMETER
CALIBRATION ERROR
~
October 1979
~>
'\)<)
OFF e I
NORMAL
2-21