Mooney M20J Pilot Operating Handbook

PILOT'S

AIRPUNE

OPERATiNG

AND

FM

APPROVED

FLIGHT

HANDBOOK

MANUAL

Advanced

THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO

TO

THE PILOT

CONSTITUTES THE

THIS

DOCUMENT

BY

THE FEDERAL AVIATION WEGUUTIONS, AND

FM

MUST

APPROVED AIRPLANE FLIGHT MANUAL.

BE

CARRIED

Trainer

IN

THE

AIRCRAm

--------

FAA

APPROVED:

MOONEV

B.O.

BOX

SERIAL. NUMBER:_"

REGISTRATION NUMBER:-

Airplane Certification
FEDERAL A\llKf'ION ABMINISTWATlON
Fort

Worlti,

761

9351

AlRCRAR

72,

KERRVILLE,

Texas

50

CGORPORATlON

TEm8

Offieo

AT

980280072

BE

FURNISHED

A

ISSUED

REV.

A

RM.

B

FM

APPROVED

applimble

8 - 89

3-90

1-92

In

Normal

to

Mdel

Cetegcay

M2OJ

SIN

based

listed

on

CAR

PART

above

only.

MANUAL NUMBER

3;

3210

MOBNEY

MODEL

M28J

AT

INTRODUCTEON

LTGG

L--"-L=-"

ORIGINAL
REVISION
REVISION

Always destroy superseded pages when inseflir~g
TITLE

"K

page

i

lhru iv

v

thru

I-

1

1-2

1-3

thru

1-9

thru

3-4,

3-2

3-3

thru

3-9,

3-10

3-'11
3-12

Ghi'LI

4-1

4-2 ...

4-3,

4-4

4-5,

4-6

4-7

Ghru 4-12

4-i3

4-94

5-1,

5-2

53,

5-4

5-5

thru
5-49 thru
5-33 1Rru 5-36

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

A

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

B

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

PAGE

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

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

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

vi

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

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

.

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

l-fi

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

1-10

3-8

...

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

1

,

3-'I

4.

...

.

.

.

,

...

...

.

.

,

,

5-1

8

5-32

EFFECT~VEE~]

----

revis4

pages.

8

-

8

9

3

-

90

1

-

92

B

Original

.

B

Original
Original

A

B

Original

Original
.A

.B

.A
Original

6-3

thru

6-6

6-7

lhru

ISSUED 8 -

6-5

6-i

89

.

This POWIAFM

PBHIAFM

i.

effective

NUMBER

beginning

3218

with

1

~~~1810~da

*---

M203,9/N

24-lW14

T

OF

EFFECTIVE

PAQ

MQONEY

MODEL

M20J

7-1 thru 7-8
7-40

...

7-1 1 thru 7-4
7-15

...

8-1 thru 8-5

8-6

8-7 thru 8-4'0

4

0-1 thru 10-4

Original

.B

4

2

.A
Original

.A

.

B

Original
.A
Original

Original

.a

Original
Original
Original

This

PQHlAFM

effective

REV.

B

beginning wLh

1 - 92

M20J

SIN 24-1686-1

ISSUED

4.

8

-

89

MOONEY

MODEL

M20J

MOBNEY

MODEL

M20J

iv

REV.

B

1

-

92

ISSUED

8

-

89

MOONEV
MODEL

M20J

'l'l~is I 'ilot's Ol-,uraiing I le#~dbcro!c conlom~:;

~r>i:lr~t~facttl~i>rs

the applicable Federal Aviation Regulations. SECTION

plied b Mooney Aircraft Corporation.

sEGT~~N

the terminology used in this Operators Manual.
This Pilot's Operating
flight instruction,

tions or advisory circulars It is not
training
status

All limitations, procedures, safety practices,

lished in this POH/AFM are consider& mandatory for the Continued Aiwo~h~ness of

airplane in a condition equal to that of its original manufacture.

Number
Engine Manufacturer
Model
~ecornrnendid

Ty lse

Number of cylinders
Bisplacerner?t

Bore
Stroke
Compression ratio

I

hatoi

ial anti

FA/\

f1I'I"I

I

contains information of general interest tothe pilot.

Haridbook is

kr~owledge ofcurrent aiwrrrtkiness directives, applicable federal air regula-

manual and should not be us& for operational purposes ~rrsless kept in an up todate

of

engines

TC

. .

not

...

..

.....

.
.
.

.......

.

.......

.

.........

E(j

(4/41\9A

1O\/tYl) rr~nleri;ll ~.etluirc?ci

designed as a substitMefor adeq~aate and competent

interlded to

sewicing and maintenarlce requiu~ments pup-

Sl~ocilic;iatior~

IX

contains supplemental d&ta sup

be

a

guide for basic Right instruction or a

....

.
.
...

No.

i

to

it

.Reciprocating, aircooled,

:artcl Illcludas boll1

bo

funii::llotl tc)

also contains dsfinniona of

~~~kON-&comin

361

Cia.

the:

s,ilu(r

4

.10-3m-~3~68

2000 Hours

fuel

injected.

.4,

Horizontally

In.

(591

5.7

8.711

Fuel System

Type Fuel injedion Flow

Make

F5.A

..........

....... . .

..

Aviation Gasolit7e

...

$06

Octane or

Bendix, RSA-5-AD1

lC10Ll.

(min. grade)

Accessories

Magnetos Bendix

Spark

Plugs

Alternator Prestolite 12V, 6QA

Starter Prestoli're

Ratings:

.........

18

MM

X

......

.........

..........

.75Q-20 Thd. Connection

or

D4LN

WLN3024

42

2021

Volts

Ijy

thls

cc

Maximurn

Continuous Sea

Level-BWP/RPM

PROPELLER

~imber of Blades
Diameter

Min.

Type

Max.

...

..........

....

...

.

SECTION

GENERAL

I

MOONEY

MODEL M20J

Governing
Blade Angles

Low
High

FUEL

v

Minimum Fuel Grade (Color)
Total Capacity

Usable

Total Oil Capacity
Oil Capcity Minimum for Flight
Oil Filter

Oil grades, specifications and changing

MNDING

TYPE: Electrically operated, fully retractable tricycle gear with rubber shock discs. The main
wheels have hydraulically operated disc brakes. The nose wheel is fully steerable
right of center.

Wheel Base

I

Wheel Track
Tire Size:

Nose
Main

.

@

30 in. Sta.(75 cm):

...

...

.

......

........

.

......

......

recommendations are contained in SECTION VIiI.

I-lydraulically controlled by engine oil

13.9 degrees

33.0 degrees

100 Octane (Green)/100 LL (Blue)

(251.8 b/ters)(55.4 Imn. Gal.)

,-

(242.4

...

+I-

.2

degrees*

+/-

.5 degrees*

.

-

66.5 U.S. Gal.

-~,\--

.64.0

L/ters)(53.3 Imp. Gal.)

8

5 (11s. 14.73 Liter$

u$.

Qts. 7.57 Liters

.Full Flow

~a(

GEAR

14' left or

......

.......

..

.

71 9/16 in.

5.00 x 5 (6 ply Type Ill

6.00 x 6 (6 pldType Ill

(1

1 10 in. (279.4 cm)

81.73 cm

Tire Pressure:

Nose
Main

Min. Turning Radius

(No brakes applied)

MAXIMUM CERTIFICATED WEIGHTS

Gross Weight
Bag age Area
Hat Wack
argo (Rear ~eats'~oidk Down)

STANDARD AlRPURlE

&sic Empty Weight
UMLmd Varies with installed equipment

1-4

........

.........

....

........

......

...

.

WEIGHTS

......

.41

2740 Lbs. (1243 Kg

120 Lbs. 54.4 Kg]

10 ~bs. 14.54 ~g

340 Lbs. (154.2 Kg!

See Page 1-1 0

.....

See

S~fllOkI VI for specific airplane weight.

REV.

8

1 - 92 ISSUED 8 - 89

M.

(12.5 m)

49PSI
30PSI

MOONEY

MODEL

M28J

CABllN

AND

ENTRY

DIMENSIONS

AT

SECTION

GENERAL

1

Cabin Width Maximum)
Cabin Length [Maimurn)
Cabin Hei
Entry ~id8 binimum)
Entry Weight (Minimum)

BAGGAGE

Compaf?mene Width
Compafiment Length
Con?par%men% Height
Cam artment Volume

Cargo Area
Entry Height

Entry Width
Ground to Bottom

Wing Loading @ Mwimum Gross Weight

Power Loading @ Maxim~dm Gross Weight

correspundonce regalditlg your airplar:e should i!:clude tho

Ail

oil

the

identification

tile Tail cone, below the horizorltal stabilizer loadirlg edge.
'The aircraft Serial Nurnber and type cel-sificare are si-rown.

24-16%-14

SIN

24-1687-44

ht

Maximum)

SPACE

(with

AND

Zhru

rear seats fold&

(Minitrscim)

24-2'%9

...

csii

Sill

plate. The identification piate is located

...

.

...

..
.

ENTRY

DIMENSIONS

.

..

.

....

.....

,

down)

...

....

43.5

In.

(410.5

.

...

17.0cu.M.

.

15.3

j.924

46.0

...

Serial

on

the [eft

CU.

R.

cubic meters)

In.

15.68
(79.03

Niimbei

!l~atfd

sir:le,

,481

1.933

33.0

(116.8

Lbs.lSq.

Kg/Sq.

cum
cu mi

CU.

as

depicted

aft

ci~s

~t.%.

cm

R.

rn)

et~i

08

G

S

KCAS

KIA$

KTAS

Va

Yf,

GROUND

KNOTS
aircraft,
Calibrated airspeed

81

KNOTS
on its aifspsed indicator.
assume

KNOTS

~~ridisturbd

temperature.

MANEUVERING

of

Ril,UiMklM

with

SPEED

-

Speed

of

CALIBRATED

correcte,d for position and instrument error.

Sea

!BV@/.

iNDiCKrED

zero

irsstrumenl error.

TRUE MRSPEED - The airsped

air

full available aoumynamic contrd

FLAP

wing

flaps

AIRSPEED

is

equal to fr~ie

AIRSPEED - Thc

lAS

irawirich

is the

SPEED

-

Ttse

EKrENDFD

in

a aarescrrbed

KCAS

aur

airplane relative

..

The indicated

airspeed

speed

vailies publisk~&

corrected for aitut~asde and

n~aimum speed at which

will

r~o%

SPEED

-The

ex%ef\ded

lo

the

speed

in

standard

of

PXTI

aircraft as

iin

this haitdbosk

d

an

airplane relative

a?\~e~s$r'@ss

highegt

psWbf2.

SIJ&

ground.

d

an

atmosphere

show;?

to

appiwtion

ti-ie

alrflane.

imfn7hs8Me

1

MMIMUM LANDING GEAR EXTENDED SPEED - The maximum
speed at which an aircraft can be safely flown with the landing gear
extended.

MAXIMUM
speed at which the landing gear can be safely extended or retracted

NEVER

exceded at any time.
MNIMUM STRUCTURAL CRUISING SPEED -The speed that

should not be
caution.

STALLING SPEED
airplane is controllable.

STALLING SPEED
airplane is controllable in the landing configuration.

BEST ANGLE-OF-CLIMB SPEED
greatest gain of altitude in the shortest possible horizontal distance.

LANDING GEAR OPERATING SPEED -The maximum

EXCEED SPEED - The speed limit that may not be

exceeded, except in smooth air, and then only with

-The minimum steady flight speed at which the

-

The minimum steady flight speed at which the

-

The airspeed which delivers the

<

-

BEST RATE-OF-CLIMB SPEED
ireatest gain in altitiide in the shortest possible time with gear and

aps up.

BRAKE

BHP
CHT

EGT

MCP

MP

WPM REVOLUTIONS PEW MINUTE - Engine speed.

Demon- The velocity of the crosswind component for which adequate
strated control of the airplane during takeoff and landing test was
Crosswind

%

"

Service
Ceiling capability of climbing at the rate of

ENGlaalf

-----

Propeller
Control

Throltle The control used to select engine power by controlling MP.
Control

CONTROLS & INSTRUMERn 9 TERMINOLOGY

HORSEPOWER

CYLINDER
engine

EXHAUST GAS TEMPERATURE

fuellair mixture during engine operation.
MMIMUM CONTINUOUS POWER - The maximum power for

talteoff, norma1,abnormal or emergency operations.
MANIFOLD PRESSURE

induction system and is expressed in inches of mercury

actually demonstrated during certification. The value shown Velocity

NOT

is
Acceleration due to gravity.
The maximum altitude at which aircraft at gross weight has the

The control used

HEAD

cylincler(s) being monitored by a sensor unit. Expressed inO~.

considered to be limiting.

-.

TEMPERATURE - Operating temperature of

-

to select engine speed.

REV.

B

-The? airspeed which delivers the

-The power developed by the engine

-

Temperature of the exhaust gas

-

Pressure measured in the engine's

100

ftlmin.

.-

1

-

92

(Wg).

ISSUED

8

-

89