Beechcraft Baron 58 - Page 156

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1775 FT
8071 rr
1
Soc
5650n
4850
LBS
9_5 KTS
2000
4000
5000
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3000~
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Q
6000
1000
GROUND ROLL
TOTAL DISTANCE OVER
50
rr
OBSTACLE
EXAMPLE,
OAT
PRESSURE ALTITUDE
TAKE-OFF WEIGHT
HEAD WIND COMPONENT
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4000
0
10
20
3D
0 50
WIND COMPONENT OBSTAClEHEIGHT
......
KNOTS "'FEET
TAKE·OFF SPEEDS (ALL WEIGHTS)
Lin
·OFF 86 KNOTS
50 FEET 94 KNOTS
ACCELERATE - GO
DISTANCE
TAKE-OFF POWER
UP
RETRACT
AnER
L1n·OFF
PAVED. LEVEL, DRY SURFACE
ASSOCIATED CONDITIONS,
FLAPS
LANDING GEAR
RUNWAY
POWER
NOTES·
1 DISTANCES ASSUME AN ENGINE FAILURE AT
LIFT-OFF AND PROPELLER IMMEDIATELY FEATHERED
2. WEIGHTS IN SHADED MAY NOT PROVIDE ONE ENGINE
INOPERATIVE CLlMB_ REFER TO TAKE·OFF
WEIGHT
GRAPH FOR
MAXIMUM
WEIGHT AT
WHICH
THE
ACCELERATE·GO PROCEDURE
SHOULD
BE ATTEMPTED
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