Cessna 402C Pilot Operating Handbook page 289

7.250 POUNDS
7,210 POUNDS
6,850 POUNDS (Unchanged)
UMITATIONS
1. MAXIMUM RAMP WEIGHT
MAXIMUM TAKEOFF WEIGHT:
MAXIMUM LANDING WEIGHT:
MAXIMUM ZERO FUEL WEIGHT:
The original Maximum Zero Fuel Weight of 6515 pounds remains applicable
except as follows:
At
151.0 inches aft datum, the maximum Zero Fuel Weight
Is increased in a straight line to 6750 pounds at 151.9 inches aft datum. and
continues aft at 6750 pounds to
a
point 160.66 inches aft datum. The Zero
Fuel Weight is thus limited to permit takeoff with at least 240 pounds of fuel
and landing with 100 pounds of fuei.
2.
FLIGHT LOAD FACTOR LIMITS
AI Design Takeoff Weight of 7210 pounds:
a. Landing gear up, wing flaps 0·, +3.4G to -1.3G
b. Landing gear down, Wing flaps 45·, 0.00 to +2.0G (Unchanged)
3. 114 Vortex generators constitute the minimum requirement. Micro VG System
consists of 118 vortex generators. jf 4 or more are missing or damaged. the
aircraft must be operated in accordance with the original Pilot's Operating
Handbook and FAA Approved Airplane Flight Manual.
4.
Change all references to Vmca values In text and on placards to: S9KfAS
-
5.
AIRSPEED INDICATOR MARKINGS:
MARKING
OR
RANGE
Red Radial
WhUeArc
Green Arc
Blue Radial
Yellow Arc
Red Radial
KJAS
VALUE
69
71-149
80-205
104
205-235
235
S.AlRSPEED UMITATIONS:
Maneuvering Airspeed, Va
. .. Atrcraft
weight
7210
6850
6500
6000
5000
F"'ERGENCY PROCEDURES
-
Emergency Atrspeeds:
Atr Minimum Control Speed (Ymca)
MICRO VG AFM SUPPLEMENT for:
CESSNA 402C G.W. INCREASE
PIN C402G-AFMS-l
..
".-
/
Airspeed
KIAS
153
149
145
140
127
S9KIAS
FAA APPROVED
DATE: AUG 19, 1996
REVB
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