Mooney Executive 21 1968 Bedienungsanleitung

MOONEY

OWNERS

MANUAL

SERIAL NUMBERS

680001

JULY

7967

ISSUE

MOONEV

A IRCRAFT,

/NC.

KERR

LE,

TEXAS

78028

MANUAL NUMBER 68-20F-OM-B

#I197

LIST

REVISED

PAGES

ISSUED

INSERT LATEST REVISED PAGES

DESTROY SUPERSEDED PAGES.

DATE

PAGE

NUMBER LATEST REVISION

NUMBER

LATEST REVISION

*THE ASTERISK INDICATES PAGES REVISED, ADDED, OR DE-

LETED BY THE CURRENT REVISION.

ADDITIONAL COPIES OR CURRENT REVISIONS OFTHIS PUBLICATION

MAY BE PURCHASED FROM YOUR LDCAL MOONEY DISTRIBUTOR OR

DEALER.

......

SECTION

GENERAL DESCRIPTION

.......

SECTION

11.

SYSTEMS OPERATIONS

SECTION

IV.

EMERGENCY PROCEDURES

...

4- 1

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

SECTION V.

LIMITATIONS.

...........

SECTION VI. PERFORMANCE

6-1

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

SECTION VII. SERVICING

7-1

This manual

issued

your operating guide for the

Mooney Executive

21.

importantthatyou--regardless of

your previous experience--carefully read the handbook

from cover to cover and review

frequently.

IMPORTANT: THIS MANUAL CONTAINS Federal

Aviation Agency-Delegation Option Authority AP-

PROVED LIMITATIONS AND

MUST

CARRIED

THE AIRCRAFT AT ALL

TIMES.

All information and illustrations in this mama1 are based

on the latest product information available at the time of

publication approval, Theright

reservedto make changes

at any time without notice. Every effort has been made to

present the material in

clear and convenient manner to

enable you to use the manual as a ready reference. Your

cooperation in reporting presentation and content recom-

mendations

solicited.

The Company warrants eaehnew airplane manufactured by

it to be free from defects in material and workmanship

under normaluse andservice, provided, however, that this

warranty

limited to making good

Company's factory

any part or parts thereof which shall, within

months

from the date of the original Airworthiness Certificate,

be returned to the Company with transportation charges

prepaid, and which upon Company's examination shall dis-

close to Company's satisfaction to have been thus defec-

tive; this warranty being expressly in lieu of all warran-

ties expressed or implied and

all

other obligations or lia-

bilities onthepartof theCompany, andthe Company neither

assumes nor authorizes any other person to assume for it

any other liability inconnectionwiththe saleof

its

airplanes.

This warranty shall not apply to any airplane which shall

havebeen repairedor alteredoutside of Company's factory

which in the judgment of Company affects the airplane's

stability or reliability, nor which in the opinion of Com-

pany has been subject to misuse, negligence, or accident.

Equipment and accessories not manufactured by sellerare

guaranteedonly to the extent of the originalmanufacturer's

guarantee.

SECTION

GENERAL

DESCRIPTION

DESIGN FEATURES

AIRFRAME

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

.....-a.

POWERPLANT

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

1-2

FLIGHT CONTROLS

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

LANDING GEAR

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

SPECIFICATIONS OUTLINE

POWERPLANT

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

1-3

PROPELLER

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

1-4

LANDING GEAR

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

1.4

FUEL

OIL

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

WEIGHT

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

-1-5

BAGGAGE COMPARTMENT

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

1.5

MooNEY

@--

OWNERS

MANUAL

DESIGN FEATURES

The

MOONEY

EXECUTIVE 21is

low- wingfour-place

air-

craftwith

retractable gear. Afour-cylinder enginepowers

the aircraft for economical, high-performance flight. 1,i-

censing under Federal Aviation Agency regulations assures

that your Mooney meets the requirements of Normal Cate-

gory aircraft at full gross weight.

AIRFRAME

The airframehasawelded, tubular-steel cabinstructure en-

closed in sheet-aluminum skins. Stressed skins rivet to

main andauxiliary spars in the wing, stabilizer, and ver-

tical fin. Thelaminar-flow wing has fullwrap- around skins

with flush riveting over the forward two thirds of the wing

area.

For pitchtrim control, the empennagepivotsonthe aftfuse-

lage.

torqueAube-driven jack screw, bolted to tie rear

tail cone bulkhead, sets the stabilizer angle of attack.

The forward-opening cabin door-provides access to both

front and rear seats. The baggage compartment door

abovethe wingtrailing edgeto enable baggage loading from

the ground.

POWER PLANT

Thepower plant

a four-cylinder fuel-injected enginethat

develops 200 horsepower.

50-ampere 12-volt generator

supplies ample electricalpower for

all

standardandoptional

equipment whenthe engine

operating at flight power set-

tings.

Thehydraulic propeller governor, using engineoilpressure

fpr increasingblade pitchto control engine speed, regulates

the controllable-pitch constant-speedpropeller. Spring.and

blade aerodynamic forces decrease blade pitch.

MOONEY

OWNERS MANUAL

FLIGHT

CONTROFS

Conventional dual controls link to the control surfaces

through push-pull tubes.

The Mooney Positive Control

(P.C.)

system

standard

equipment.

a lateral stability control system that

provides a high degree of roll and yaw stability, thereby

enhancing the inherent wings-level flight characteristics

of the aircraft. The system works full time from takeoff

throughlandingbut canbe easilydeactivatedoroverpowered

for flight maneuvers.

P.C.

allows you, the pilot, to devote

more time to navigation, traffic surveillance, and com-

munications.

LANDING

GEAR

The

tricycle landing gear allows maximum taxi vision and

ground maneuvering, Hydraulic disc brakes and

steer-

able nose wheel aid in positive directional control during

taxiing and crosswind landings.

The standard gear

manually retracted.

gear warning

horn along with red and green position lights help prevent

inadveqtent gear-up landings. An electrically operated

gear

available at extra cost. The electric gear system

incorporates

airspeed-actuated switch that helps pre-

vent gear retraction until

safe airspeed

attained. An

emergency gear extension system

installed with the op-

tional electric gear system.

SPEClPlCATlONS OUTblNE

POWER

PLANT

TYPE:

Four-cylinder, air cooled, horizontally opposed,

and fuel- injected engine with

wet- sump lubricating sys-

tem.

Model (Lycoming).

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

.I8-

360-A1A

Rated Horsepower

2700 RPM

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

200

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

Bore 5.125

IN.

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

Stroke 4.375

IN.

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

Displacement 361.0

CU.

IN.

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

Compression Ratio

8.7:

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

Fuel Injector, Bendix RSA-

5-AD1

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

Magnetos, Scintilla S4LN- 200 Series

PROPELLER

TYPE: Constant- speed hydraulically- controlled propeller

with a single- acting governor.

..........

Model (Bartzell) Hc- 62~

K-

1~/'7666

A-

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

Diameter .94

IN.

Blade Angle

IN.

STA):

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

Low. 14O

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

High

..........'.

290

LANDING

GEAR

TYPE: Manually retractedtricycle gear withrubber shock

discs, steerable nose wheel, and hydraulic disc brakes.

Wheel Base

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

5 FT 11-9/16

IN.

Wheel Tread.

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

....

314

IN.

Tire Size:

Nose

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

5.00

Main

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

.'-.

......

6. OOx

Tire Pressure:

Nose

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

49 PSI

Main

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

30 PSI

MOONEY

OWNERS

MANUAL

FUEL

911

Usable Fuel Capacity

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

GAL

Minimum Fuel Octane Rating (aviation grade)

100/130

.........

Oil Capacity

QTS

MIN for flight)

QTS

WEIGHT

Gross Weight

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

2740 1,BS

Approximate Empty Weight (with standard

equipment)

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

1640 LBS

Useful Load

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

,1100

LBS

Wing Loading

Gross Weight (PSF)

......

.P6.4

Power Loading

Gross Weight

(PHP)

........

.13.7

BAGGAGE COMPARTMENT

Maximum Loadif@ (unless limited

weight envelope):

Baggage Area

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

.I20 LIBS

Hat Rack

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

.I0

L.BS

FIGURE

DIMENSIONED

THREE

VIEW

"$6

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