Cessna 310 1975 Manual de usuario

'--"

'-'

Cessna®

___,·

'--"

PEOPLE

BUY

AND

'--'

FLY

CESSNA

AIRPLANES

THAN

ANY

OTHER

MAKE

'---"""

'--'

1975

WORLD'S

LARGEST

PRO-

DUCER

GENERAL

AVIATION

AIRCRAFT

SINCE

1956

MODEL

310

OWNER'S

MANUAL

PERFORMANCE

AND

SPECIFICATIONS

GROSS

WEIGHT:

T&keoff

• • • • , •

La.nding . . . . .

SPEED BEST

POWER

MIXTURE:

Maximum -

Sea

Level

. ,

Maximum

Recommended

Cruise

75%

Power

7500

ft.

RANGE,

RECOMMENDED

LEAN

MIXTURE:

Maximum Recommended

Cruise

75%

Power

7500

ft.

600

lbs.

, No

Reserve

75'.£

Pow'er

7500

ft.

978

lbs.,

Reserve

75%

Power

7500

ft.

1218

lbs.

Reserve

Maximum Range

10,

000

ft.

600

lbs.

Reserve

10,000

ft.,

978

lbs.,

Reserve

10,000

ft.,

1218

lbs.,

Reserve

RATE-OF-CLHfB

SEA

LEVEL:

Twin

Engine

. .

Single

Engine

SERVICE

CEILING:

Twin

Engine

TA~5;;i;E~~~~~cE:

·Takeoff

Spe~d

(s2

·KIAs, '150

Fiap~)

Ground

Run

. . . . . . , . .

Total

Distance

Over

50-foot

Obstacle

, .

LANDING

PERFORMANCE:

Approach

Speed

(93

KIAS,

5400

lbs)

Ground

Roll

, . . . , • . . .

Total

Distance

Over

50-foot

Obstacle

EMPTY

WEIGHT:

(Approximate}

310

. ,

BAGGAGE

ALLOWANCE:

WING

LOADING:

POWER

LOADING:

FUEL CAPACITY: TOTAL

Sta:~~~dA~xiiia~y

Tanks

(40°gai.

~sable)

With

Auxiliary

Tanks

(63

gal.

usable)

. . . . , . .

With

Auxiliary

Tanks

(63

gal.

usable)

and

Wing

Locker

Tanks

OIL

CAPACITY: TOTAL

ENGINES:

Continental

6-Cylinder

Fuel

Inject

ion

Engines

285

Rated

2700

RPM

PROPELLERS :

Constant

Speed,

Full

Feathering

Three

Blade

76.

Diameter

5500

lbs.

5400

lbs,

207

Knots

194

Knots

616

Naut.

Mi.

3.19

hrs.

193

Knots

1006

Naut.

Mi.

5.21

hrs.

193

Knots

1253

Na.ut.

Mi.

6.49

hrs.

193

Knots

772

Naut.

Mi.

4.98

hrs.

155

Knots

1258

Naut.

Mi.

8.12

hrs.

155

Knots

1567

Naut.

Mi,

10.11

hrs.

155

Knots

1662

fpm.

370

fpm.

19,750

ft.

7400

ft.

1335

ft.

1700

ft.

640

ft.

1790

ft.

3251

lbs.

3417

lbs.

950

lbs.

30.73

lbs./sq.

ft.

9.65

lbs.

/hp.

102

gals.

143

gals.

166

gals.

207

gals.

6.5

gals.

I0-520-M

3AF32C87

/82NC-5.

•Single

engine

service

ceiling

increases

300

feet

for

each

minutes

flight.

THIS OWNER'S MANUAL

COVERS

THE

OPERATION

THE

310

AND

31011

AIRCRAFT

SERIAL

NUMBER

310R0001

THRU

310R0500

1985

Cessna Aircraft Company

Wichita, Kansas USA

CONGRATULATIONS

...............

Welcome to

the

ranks

Cessna

owners!

Your

Cessna

has

been

designed

and

con-

structed

give

you

the

most

performance

economy,

and

comfort .

our

desire

that

you

will find

flying

it,

either

for

business

pleasure,

pleasant

and

profitable

experience.

This

Owner's

Manual

has

been

prepared

guide

help

you

get

the

most

pleas-

ure

and.utility

from

your

aircraft.

contains

information

about

your

Cessna's

equip-

ment,

operating

procedures,

and

performance;

and

suggestions

for

its

servicing

and

care.

urge

you

read

from

cover

cover,

and

refer

to it

frequently.

Our

interest

your

flying

pleasure

has

not

ceased

with

your

purchase

of a

Cessna.

Worldwide

the

Cessna

Dealer

Organization

backed

the

Cessna

Service

Department

stands

ready

serve

you.

The

following

services

are

offered

most

Cessna

Dealers:

THE

CESSNA WARRANTY

designed

provide

you

with

the

most

comprehen-

sive

coverage

possible:

exclusions

Coverage

includes

parts

and

labor

Available

Cessna

Dealers

worldwide

Best

the

industry

Specific

benefits

and

provisions

warranty

plus

other

important

benefits

for

you

are

contained

your

Customer

Care

Program

book

supplied

with

your

aircraft.

Warranty

service

available

you

any

authorized

Cessna

Dealer

throughout

the

world

upon

presentation

your

Customer

Care

Card

which

establishes

your

eligibility

under

the

warranty.

FACTORY TRAINED PERSONNEL

provide

you

with

courteous

expert

service.

FACTORY APPROVED SERVICE EQUIPMENT

provide

you

with

the

most

efficient

and

accurate

workmanship

possible.

A STOCK

GENUINE CESSNA SERVICE PARTS

hand

when

you

need

them.

THE LATEST AUTHORITATIVE INFORMATION

FOR

SERVICING CESSNA AIRCRAFT,

since

Cessna

Dealers

have

all

the

Service

Manuals

and

Parts

Catalogs,

kept

cur-

rent

Service

Letters

and

Service

News

Letters,

published

Cessna

Aircraft

Company.

urge

all

Cessna

owners

use

the

Cessna

Dealer

Organization

the

fullest.

current

Cessna

Dealer

Directory

one

your

cross-country

flight

planning

aids;

warm

welcome

awaits

you

every

Cessna

Dealer.

*Maximum

height

aircraft

with

nose

gear

depressed

10'-11

3/4"

31'

11''

---------..i

17'0"

----.!

PRINCIPAL

DIMENSIONS

36'11"----------i

DIAMETER 76.5"

TABLE

CONTENTS.

Page

SECTION I -OPERATING CHECKLIST··················

1-1

SECTION

-DESCRIPTION

AND

OPERATING

DETAILS

....................... 2-1

SECTION

Ill

EMERGENCY

PROCEDURES

..........

3-1

SECTION

-OPERATING LIMITATIONS .......... 4-1

SECTION

V - CARE OF

THE

AIRCRAFT

.............

5-1

OWNER

FOLLOW-UP

SYSTEM

.................

5-8

SECTION

-OPERATIONAL

DATA

...................... 6-1

SECTION

VII

-OPTIONAL SYSTEMS*..................... 7-1

ALPHABETICAL

INDEX

............................................

Index

- 1

*This

manual

describes

the

operation

and

performance

both

the

Cessna

310

and

310

aircraft.

Equipment

described

"Optional"

de-

notes

that

the

subject

equipment

optional

the

310

aircraft.

Much

this

equipment

standard

the

310

II.

iii.

INSTRUMENT

PANEL

FLIGHT

INSTRUMENT

GROUP

AVIONICS

CONTROL PANEL

(OPTIONAL)

ECONOMY

MIXTURE

INDICATOR

(OPTIONAL)

ENGINE

INSTRUMENT

GROUP

FUEL

QUANTITY

SELECTOR

SWITCH

(OPTIONAL)

OXYGEN

CYLINDER

PRESSURE GAGE

(OPTIONAL)

HEATER

AND

CABIN

AIR

CONTROL

PANEL

8. FLAP POSITION SWITCH

ALTERNATE

AIR

CONTROLS

10. AUTOPILOT CONTROL HEAD

(OPTIONAL)

11.

RUDDER TRIM CONTROL

12. COWL

FLAP

CONTROLS

13.

AILERON

TRIM CONTROL

14.

ELEVATOR TRIM CONTROL

15. LANDING GEAR POSITION SWITCH

16. LEFT-HAND SWITCH PANEL

17.

OXYGEN

CONTROL

KNOB

(OPTIONAL)

~~©lTD®~

OPERATING

CHECKLIST

One

the

first

steps

obtaining

the

utmost

perfor-

mance,

service,

and

flying

enjoyment

from

your

Cessna

familiarize

yourself

with

your

aircraft's

equipment,

systems,

and

controls.

This

can

best

done

reviewing

this

equip-

ment

while

sitting

the

aircraft.

Those

items

whose

func-

tion

and

operation

are

not

obvious

are

covered

Section

II.

Section

lists,

Pilot's

Checklist

form,

the

steps

necessary

operate

your

aircraft

efficiently

and

safely.

covers

briefly

all

the

points

that

you

should

know

con-

cerning

the

information

you

need

for

typical

flight.

The

flight

and

operational

characteristics

your

aircraft

are

normal

all

respects.

All

controls

respond

the

normal

way

within

the

entire

range

operation.

MAKE

PREFLIGHT

INSPECTION

ACCORDANCE

WITH

FIGURE

1-1.

BEFORE

STARTING

THE

ENGINES

(1)

Preflight

Inspection

COMPLETE.

(2)

Control

Lock(s)

REMOVE.

(3)

Seats,

Seat

Belts

and

Shoulder

Harness

ADJUST

and

SECURE.

(4)

Brakes

TEST

and

SET.

(5)

Landing

Gear

Switch

DOWN.

(6)

Emergency

Alternator

Field

Switch

-OFF.

(7)

Emergency

Avionics

Power

Switch

OFF.

(8)

Avionics

Master

Switch

OFF.

(9)

Circuit

Breakers

-IN.

(10)

All

Switches

-OFF.

(11)

Battery

and

Alternators

ON.

1-1

PREFLIGHT

INSPECTION

NOTE

Visually

check

inspection

plates

and

general

aircraft

condition

during

walk-

around

inspection.

night

flight

planned,

check

operation

all

lights

and

make

sure

flashlight

avail-

able.

Refer

inside

back

cover

this

manual

for

quantities,

materials,

and

specifications

frequently

used

service

items.

1-2

Control

Lock(s)

REMOVE

and

STOW.

Parking

Brake

-SET.

Alternate

Static

Source

CLOSED.

All

Switches

-OFF.

All

Circuit

Breakers

-IN.

Landing

Gear

Switch

DOWN.

Left

Fuel

Selector

LEFT

MAIN

(feel

for

detent).

Right

Fuel

Selector

RIGHT

MAIN

(feel

for

detent).

Trim

Tab

Controls

(3)

NEUTRAL.

Oxygen

CHECK

quantity,

masks,

and

hoses

OFF.

Battery

Switch

ON.

Fuel

Gages

CHECK

quantity

and

operation.

Wing Fla11s -

EXTEND.

Baggage

Door

SECURE.

Static

Port(s)

CLEAR.

Deice

Boots

CHECK

condition

and

security,

installed.

Control

Surface

Locks

REMOVE,

elevator

and

rudder.

Elevators

and Tab -Check

condition,

freedom

movement, and

tab

position.

Tie

Down

REMOVE.

Rudder Tab -

CHECK

condition,

freedom

movement, and

tab

position.

Static

Port(s)

CLEAR.

Wing

Locker

Baggage

Door

-SECURE.

Battery

Compartment

Cover

SECURE.

Wing

Flap

CHECK

security

and

attachment.

Bottom

outboard

wing

CHECK

for

fuel

stains.

Control

Surface

Lock -

REMOVE.

Aileron

and

T~.b

CHECK

condition,

freedom

movement, and

tab

position.

Tip

Tank

Transfer

Pump -LISTEN

for

operation.

Fuel

Sump

(Main

Tank)

-DRAIN.

Fuel

Vent

and

Sniffle

Valve

CLEAR.

Fuel

Quantity

(Main

Tank)

CHECK,

cap

secure.

Deice

Boot

CHECK

condition

and

security,

installed.

Stall

Warning Vane -

CHECK

freedom

movement and

audible

warning.

Wing

Tie

Down

REMOVE.

Figure

1-1

(Sheet

(J)

Fuel

Quantity

(Au><iliary

Tank)

CH.ECK,

cap

secure.

Fuel

Vent

(Wing

Locker

Tank)

CLEAR,

installed.

Fuel

Sump

(Auxiliary

Tank

and

Wing

Locker

Transfer

Line,

installed)

DRAIN.

Fuel

Strainer

-DRAIN.

Fuel

Quantity

(Wing

Locker

Tank)

-CHECK,

cap

secure,

installed.

Oil

Level

CHECK,

minimum 9

quarts.

Engine

Compartment

General

Condition

CHECK

for

fuel,

oil

and

exhaust

leaks

stains.

Propeller

and

Spinner

EXAMINE

for

nicks,

security

and

oil

leaks.

Leading

Edge

Air

Intake

CLEAR.

Main

Gear

Strut,

Doors

and

Tire

CHECK.

Fuel

Sump

(Wing

Locker

Tank)

-DRAIN,

installed.

Nose

Baggage

Door

-SECURE.

Nose

Gear,

Strut,

Doors

and

Tire

CHECK.

Lower

fuselage,

nose

and

center

section

CHECK

for

fuel

stains.

Pitot

Cover(s)

REMOVE,

installed.

Pitot

Tube(s)

CLEAR.

Tie

Down -

REMOVE

Heater

Inlet

-CLEAR.

Leading

Edge

Air

Intake

CLEAR.

Cross

feed

Lines

DRAIN.

Fuel

Sump

(Wing

Locker

Tank)

-DRAIN,

installed,

Maio

Gea.r,

Strut

Doors

and

Tire

CHECK,

Fuel

Quantity

(Wing

Locker

Tank)

CHECK,

cap

secure,

installed.

Oil

Level

CHECK,

minimum 9

quarts.

Engine

Compartment

General

Condition

CHECK

for

fuel,

oil

and

exhaust

leaks

stains.

Propeller

and

Spinner

EXAMINE

for

nicks,

secu:ri

and

oil

leaks.

Fuel

Vent

(Wing

Locker

Tank)

CLEAR,

installed.

Fuel

Swnp

(Auxiliary

Tank

and

Wing

Locker

Transfer

Line,

installed)

DRAIN.

Fuel

Strainer

-DRAIN.

Fuel

Quantity

(Auxiliary

Tank)

CHECKJ

cap

secure.

Wing

Tie

Down -

REMOVE.

Deice

Boot

CHECK

condition

and

security,

installed.

Fuel

Quantity

(Main

Tank)

CHECK,

cap

secure.

Fuel

Vent

and

Sniffle

Valve

CLEAR.

Fuel

Sump

(Main

Tank)

-DRAIN.

Tip

Tank

Transfer

Pump -LISTEN

for

operation.

Control

Surface

Lock

REMOVE.

Aileron

CHECK

condition

and

freedom

movement.

Bottom

outboard

wing

CHECK

for

fuel

stains.

Wing

Flap

CHECK

security

and

attachment.

Wing

Locker

Baggage

Door

-SECURE.

Battery

Switch

-OFF.

Figure

1-1

(Sheet

1-3

NOTE

When

using

external

power

source,

not

turn

battery

alternator

switches

until

external

power

disconnected,

avoid

damage

the

alternators

and a weak

battery

draining

off

part

the

current

being

supplied

the

external

source.

(12)

Lighting

Rheostats

REQUIRED.

(13)

Altimeter

and

Clock

-SET.

(14)

Heater

Overheat,

Low

Volt

and T &B - PRESS-TO-

TEST.

(15)

(16)

(17)

(18)

(19)

(20)

(21)

(22)

(23)

(24)

Landing

Gear

Position

Indicator

Lights

CHECK

(press-to-test

required).

Cabin

Air

Controls

REQUIRED.

Fuel

Quantity

CHECK.

Throttles

OPEN

ONE

INCH.

Propellers

FULL

FORWARD.

Mixtures

FULL

RICH.

Cowl

Flaps

OPEN.

Fuel

Selectors

Left

Engine

LEFT

MAIN

(feel

for

detent).

Right

Engine

RIGHT

MAIN

(feel

for

detent).

Alternate

Air

Controls

-IN.

Anti-Collision

Lights

ON.

STARTING

ENGINES

(Left

Engine

First}

NORMAL

ART

(NO

EXTERNAL

POWER)

1-4

(1)

Propeller

CLEAR

(2)

Magneto

Switches

ON.

(3)

Engine

START.

(a)

Starter

Button

-PRESS.

(b)

Primer

Switch

Left

Engine

LEFT.

Right

Engine

RIGHT.

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