Density Altitude; Single Engine Climb Data; Single Engine Service Ceiling - Cessna 310 1975 Owner's Manual

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MAXIMUM PERFORMANCE TAKEOFF
15
°
FLAPS
DENSITY ALTITUDE
SEA LEVEL 590y
2500 F1'
so
0
r
5000 FT 410F
7500 FT 320F
Total
Total
Total
Total
Distance
Distance-
Distance
Distance
Gross
KlAS
KIAS
Head
over
O\•er
over
over
Weignt
at
at
\\'ind
Ground
50 Ft
Ground
50 Ft
Ground
50 Ft
Ground
50 Ft
Pounds
Takeoff
Obstacle
Knots
Run
Obstacle
Run
Obstacle
Run
Obstacle
Run
Obstacle
5500
••
83
0
1335
1700
1630
2082
2024
2614
25Ei5
3387
15
1006
1313
1242
1624
1559
2061
1989
2702
30
718
966
900
1212
1147
1561
1485
2077
Figure 6-8
SINGLE ENGINE CLIMB DATA
SEA LEVEL 59°F
2500 FT 50°F
5000 FT 41°F
7500 FT 32°F
10' 000 FT 23°F
Gross
Best
Rate
Best
Rate
Best
Rate
Best
Rate
Best
Rate
Weight
Climb
of
Climb
of
Climb
of
Climb
of
Climb
of
Pounds
KIAS
Climb
KIAS
Climb
KIAS
Climb
KIAS
Climb
KIAS
Climb
Ft/Min
Ft/Min
Ft/Min
Ft/Min
Ft/Min
5500
106
370
103
265
100
156
97
48
94
-60
5100
102
448
99
340
96
230
93
122
90
13
4700
98
520
95
414
92
305
89
197
86
90
-··
NOTE:
Flaps and gear up, inoperative propeller-feathered, wings
banked 5° toward operating engine, full throttle, 2700
RPM and mixture at recommended fuel flow.
Decrease
rate of
climb 15 FT/MIN for
each
ioop
above standard
temp-
erature for particular
altitude.
Figure 6-9
SINGLE ENGINE SERVICE CEILING
BEST CLIMB SPEED APPROXIMATELY 100 KIAS
OUTSIDE AIR TEMPERATURE Op
Gross
l
1
I
I
I
I
Weight
-10
0
10
20
30
40
50
Pounds
ALTITUDE-FEET
5500
8190
1
8000
l
7850
I
7650
I
7500
I
7320
I
7100
5100
9790
9630
9420
9260
9100
8920
8690
4700
11,490
11,310
11,140
10' 930
10, 730
10' 520
10' 290
NOTE:
Table provides performance information to aid in route selection
when operating under FAR 135.145 and FAR 91.119 requirements.
lncrease indicated service ceilings 100
feet for each 0.10
inch
Hg,
altimeter setting greater than 29. 92.
Decrease indicated service ceilings 100 feet for
each
0.10 inch
Hg.
altimeter setting less than 29. 92.
The
service ceilings are
the highest attainable
while
maintaining
a minimum rate-of-climb of 50 ft/min.
Figure 6-10
6-8

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