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Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 103

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, , ,,...--......,

CESSNA

MODEL T210M

SECTION 5

PERFORMANCE

CONDITIONS:

3800 Pounds

RANGE PROFILE

45 MINUTES RESERVE

534 LBS. USABLE FUEL

Recommended Lean Mixture for

Cruise

Standard Temperature

Zero Wind

NOTES

:

1.

This chart allows for the

fuel used

for

engine

start, taxi, takeoff

and

climb and

the

distance during climb (as shown in Figure 5-6) for

a

normal

climb

up

to

20 ,000

feet

and

maximum

rate

of

climb above 20,000 feet.

2.

Reserve

fuel is based

on 45

minutes

at 45%

BHP and is 46

lbs.

24,000

192 KTAS

'

I

I

I

I

~155

d'.]

176 KTAS

~

~

KTAS

202 KTAS ·1

20,000

I

j

I

I

,

I

,

I

16,000

I

,

191 KTAS

l

180 KTAS:'.'

~

;166 KTAS' 149

KTAS'

f - ~

I-

w

j

j

I

I

I

I

w

u..

12,000

,

I

'

J

J

j

LU

Cl

:::)

,

I

-

J

J

j

I-

i' . =

8000

...J

c:i:

4000

,

I

'

I

___

177 KTASl

_

168 KTAS11~ 156 KTAS-( 142 KTAS'

~

I

~

~

0:-

-

-

-

f~

I~

I~

~

If~

I~

1~

~

'

o'f'

I

~

J~

'&

JC

lo

j

~

- 154-f-f--

,

I

,~

I

~

I

,"&

-

KTAs::::l/ 156

KTAS,,

-

146 KTAS~r1

-

134

KTAS-.

S.L.

700

750

800

850

900

950

1000

RANGE

-

NAUTICAL MILES

Figure

5-8.

Range Profile

5-29

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