Mooney EXECUTIVE 21 1969 Manuale utente

1969

MOONEY

OWNERS

MANUAL

MODELS

1969-M20F

SERIAL NUMBERS

690001

JULY

1968

ISSUE

MOONEY AIRCRAFT CORPORATION

KERRVILLE,

TEXAS

7{J028

MANUAL

NUMBER

69·20F·OM·B

GENERAL DESCRIPTION

..........

SECTION •

SYSTEMS OPERATIONS

...........

SECTION •

NOR.MAL PROCEDURES

...........

SECTION •

EMERGENCY PROCEDURES

........

SECTION •

LIMITATIONS

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

SECTION •

PERFORMANCE

••.....•.••..•..

SECTION •

SERVICING

••...•..•...........

SECTION •

• • • • • • • • • • • • •

This

manual

issued

your

operating

guide

for

the

Mooney

Executive

21.

important

that

you--

regardless

your

experience--carefully

read

the

handbook

from

cover

and

review

frequently.

IMPORTANT: THIS MANUAL CONTAINS

Federal

Aviation

Administration-Delegation

Option

Authority

APPROVED LIMITATIONS AND MUST

CARRIED

THE

AffiCRAFT

ALL

TIMES.

All

information

and

illustrations

this

manual

are

based

the

latest

product

information

available

the

time

publication

approval.

The

right

reserved

make

changes

any

time

without

notice.

Every

effort

has

been

made

present

the

material

in a

clear

and

convenient

manner

enable

you to

use

the

manual

ready

reference.

Your

cooperation

reporting

presentation

and

content

recom-

mendations

solicited

• • • •

''Mooney

Aircraft

Corporation

("Mooney'~

warrants

each

new

airplane

manufactured

and

sold

by Mooney

against

defects

material

and

workmanshipunder

normal

use

and

service

when

operated

lnaccord-

ance

with

Mooney's

operating

instructions

. Mooney

does

not

make

any

warranties

with

respect

airplane

equipment

and

accessories

not

manufactured

by Mooney,

but

Mooneydoesagree

.to

assign

the

Buyer,

request,

any

warranties

Mooney

has

received

from

the

manufacturers

such

airolane

eauioment

and

accessories

"This

warranty

and

any other

expr

es~

1;r

111.le

warranties

made

Mooney

(hereifter

colle

tively

ca.Jled

'Wa

uties

")are

only

enforce-

able

when and

(a) Mooney

receiv

'(11o;

•l

itten

notice

of the

breach

within

least

m1c

(I)

i.1

' " of

the

original

air-

worthiness

ertificate

for lhe new

ai.

plane, (h) ifr e

quired

byMooney, ·

the

defective

part

re moved

from

the

airi

:l;rne, p

perly

packed

and

returned

to Mo

oney's

rrville

, T

<:J<.

as \1i:

w1.

u ·;:msportation and

in-

surance

char

ges

prepa

id,

and

(

nn;,y

•1

mines,

Irr

Its

sole

judgment

that

the

part

defective a.ad

nli

lher

the

part

nor

the

airplane

has

subjected

any

misus

<·, negle

ct,

negligence,

acci-

dent,

impr

per

installation,

rep

ait

Gr alte

ration.

Mooney's

ex-

clusiv

obligati

on under

all

Warranlies

;,.l!

b€

limited

supplying,

free

charg

o. b. Moone

y's

planl),

material

necessary

repair

repl

ace

any

defec

tive

part

, a

la!J

or ,

ir.stallation

and

other

expenses

born

e by

the

Buy,

·Mooney

shall

not

liable

for

11peclal,

consequential

01·

incident

rlr

iag

bt>.

ANY

IMPLIED

WARRANTY

MERCHANTABILITY

FITNESS

FORA

PARTICULAR

PURPOSEISHEREBYEXPRESSLYEXCLUDED

•

SECTION

GENERAL

DESCRIPTION

DESIGN

FEATURES

AIRFRAME . . • . . . . . . . . . . • • • . . • . . . . . . . . 1-2

POWER

PLANT

·. . • . . . . • . . . . . • . . . . . . .

..•

FLIGHT CONTROLS

.••..•......•....•...

1-3

LANDING GEAR

.••....•.•....•........

1-3

SPECIFICATIONS

OUTLINE

POWER PLANT . . • . • . . . . . . • . . . . . . • • . . . •1-3

PROPELLER

••...................•...

1-4

LANDING GEAR

•..•..•....•..•...•....

1-4

FUEL

OIL

.••••..••....••..•...•...•

1-5

WEIGHT & LOADING

.••..•••....•......•

1-5

BAGGAGE COMPARTMENT

.•••..•........

1-5

1-1

MOONEY

ljWPffii>W

OWNERS

MANUAL

DESIGN

FEATURES

The

MOONEY EXECUTIVE

2lis

alow-wingfour-place

air-

craft

with

retractable

gear.

four-cylinder

engine

powers

the

aircraft

for

economical,

high-performance

flight.

Li-

censing

under

Federal

Aviation

Administration

regulations

assures

that

your

Mooney

meets

the

requirements

Nor-

mal

Category

aircraft.

AIRFRAME

The

airframe

has

welded,

tubular-

steel

cabin

structure

en-

closed

sheet-aluminum

skins.

Stressed

skins

rivet

main

and

auxiliary

spars

the

wing,·

stabilizer,

and

ver-

tical

fin.

The

laminar-

flow wing

has

full

wrap-

around

skins

with

flush

riveting

over

the

forward

top

two

thirds

the

wing

area.

For

pitch

trim

control,

the

empennage

pivots

the

aft

fuse-

lage.

torque-tube-driven

jack

screw,

bolted

the

rear

tail

cone

bulkhead,

sets

the

stabilizer

angle.

The

forward-opening

cabin

door

provides

access

both

front

and

rear

seats.

The

baggage

compartment

door

above

the

wing

trailing

edge

enable

baggage

from

the

ground.

POWER PLANT

The

power

plant

four-cylinder

fuel-injected

engine

that

develops

200

horsepower.

60-ampere

12-volt

alternator

supplies

ample

electrical

power

for

all

standard

and

option-

equipment

all

engine

speeds

from

warmup

to flight

power

settings.

The

hydraulic

propeller

governor,

using

oil

pressure

for

increasing

blade

pitch

control

engine

speed,

regulates

the

controllable-pitch

constant-

speed

propeller.

Spring

and

blade

aerodynamic

forces

decrease

blade

pitch.

1-2

MOONEY

ljffelbJi>.#1

OWNERS

MANUAL

FLIGHT CONTROLS

Conventional

dual

controls

link

the

control

surfaces

through

push-pull

tubes.

The

co-pilot's

rudder

pedals

are

removable.

The

Mooney

Positive

Control

(P.

C.)

system

standard

equipment,

lateral

stability

augmentation

system

that

provides

high

degree

roll

and

yaw

stability,

thereby

enhancing

the

inherent

wings-

level

flight

characteristics

the

aircraft.

The

system

works

full

time

from

takeoff

through

landing

but

can

easily

deactivated

overpowered

for

flight

maneuvers.

P.C.

allows

you,

the

pilot,

to devote

time

to navigation,

traffic

surveillance,

and

com-

mu'

iications.

LANDING

GEAR

The

tricycle

landing

gear

allows

maximum

taxi

vision

and

ground

maneuvering.

Hydraulic

disc

brakes

and

steer-

able

nose

wheel

aid

positive

directional

control

during

taxiing

and

crosswind

landings.

The

landing

gear

electrically

retracted.

gear

warning

horn

along

with

amber

and

green

positfon

lights

help

prevent

inadvertent

gear-up

landings.

The

retraction

system

in-

corporates

airspeed-actuated

switch

that

prevents

gear

retraction

until

safe

airspeed

attained.

emergency

gear

extension

system_

provided.

SPECIFICATIONS OUTLINE

POWER PLANT

TYPE:

Four-cylinder,

air

cooled,

horizontally

opposed,

1-3

MOONEY

ljWihhi>..fl'

OWNERS

MANUAL

and

fuel-injected

engine

with

wet-sump

lubricating

sys-

tem.

Model (Lycoming)

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

I0-36(}..AlA

Rated

Horsepower

@ 2700

RPM

. . . . . . . . . 200

BHP

Bore

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

5.125

IN".

Stroke

. . . . . . . . . . . . . . . . . . . . . . . . . . 4. 375 IN".

Displacement

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

361. 0 CU. IN".

Compression

Ratio

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

Fuel

Injector,

Bendix

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

RSA-5-ADl

Magnetos,

Scintilla

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

S4LN-200

Series

PROPELLER

TYPE:

Constant-

speed,

hydraulically

controlled

propeller

with

single-acting

governor.

Model (Hartzell}

..........

HC-

C2YK-1B/7666

A-

Diameter

. . . . . . . ·. . . . . . . . . . . . . . . . . . . .74 IN".

Blade

Angle

IN.

STA):

Low

...............•...........

14°

±o

High . . . . . . ... . . . . . . . . . . . . . . . . . . 290 ±

LANDING

GEAR

TYPE:

Electrically

retracted

tricycle

gear

with

rubber

shock

discs,

steerable

nose

wheel,

and

hydraulic

disc

brakes.

Wheel

Base

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

11-9/16

IN".

Wheel

Tread

.........

..........

3/4

IN.

Tire

Size:

Nose

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

5.00x5

Main . . . . . . . . . . . . . . . . . . . . . . . . . . 6. 00 x 6

Tire

Pressure:

Nose

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

.....

PSI

Main

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

...

PSI

1-4

MOONEY

fiU@b'i*W

OWNERS

MANUAL

FUEL

& OIL

Usable

Fuel

Capacity

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

64 GAL

Minimum

Fuel

Octane

Rating

(aviation

grade}

100/130

Oil

Capacity

QTS

MIN

for

flight) . . . . . . . . . 8 QTS

WEIGHT & LOADING

Gross

Weight

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

2740

LBS

Approximate

Empty

Weight

(with

standard

equipment)

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

1640 LBS

Useful

Load

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

1100 LBS

Wing

Gross

Weight

. . . . . . . . . . 16.4

PSF

~ower

Loading@

Gross

Weight

.........

13. 7

PHP

BAGGAGE COMPARTMENT

Maximum

(unless

limited

envelope):

Baggage

Area

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

120 LBS

Hat

Rack

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

.10

LBS

1-5

MOONEY

~ljWJUhi*W

OWNERS

MANUAL

8'4"

FIGURE

1-1.

DIMENSIONED

THREE

VIEW

1-6

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