Mooney M20F Executive Manuale utente

MOONEY

OPERATORS MANUAL

MODEL SERIAL NUMBERS

M2O F22-1306 &ON

OCTOBER 1975 ISSUE

MOONEY AIRCRAFT CORPORATION

KERRVILLE, TEXAS 78028

MANUAL NUMBER 191O

ONEY OPERATORS MANUAL

OM NEY WARNING: Up to 2000 feet of altitude may

be lost in a one-turn spin and recovery;

therefore stalls at low altitude are extremely

critical.

On entering a spin, the aircraft will roll, very much

like abarrel roll. The wings will be near vertical at

EXECL/77// VE about the first quarter turn of the spin. At about the

half turn point, the wings are approaching level but,

now, the nose will be very low--approaching vertical.

After one full turn has been completed, the nose will

come up somewhat, but will remain well below the

horizon. The rate of rotation during the first portion

of the spin is quite rapid and occupants of the aircraft

OPERATORS MANUAL šÏii.isbecob

esn eho Onuoe orn

pointing mo¡;p nearly toward the ground than the hori-

zon, as the airplane revolves and descends. As the

spin progresses, it may enter into what is referred

MODEL SERIAL NUMBERS to as aflat spin. When the spin becomes flat, the

M2O F22-1306 &ON aircraft nose comes up and remains more on the hori-

zon, with possibly some shallow up and down oscillation.

The rate of descent and rate of rotation both become

slower. An air'craft in aflat spin becomes stabilized

into autorotation and once in this condition, the controls

become ineffective and recovery is very difficult or may

not be possible.

In complying with the FAA Regulation for Normal Cate-

gory aircraft, it has been demonstrated that the air-

plane will recover after delayed stall recovery up to

OCTOBER 1975 ISSUE and including one-turn spins.

This one-turn "margin of safety" is designed to pro-

MOONEY AIRCRAFT CORPORATION vide adequate controllability when recovery from a stall

is delayed. The one-turn "margin of safety" is jeopar-

KERRV ILL E, TEX AS78028 dized if'the airplane is not recovered when the first

evidence of astall is detected.

MANUAL NUMBER 1219

3-19

ONEY PERATORS MANUAL

POSITIVE CONTROL

Positive Control will hold an approximate heading

over aperiod of tifne; however, it will not hold an

exact heading without the installation of amagnetic

heading lock. To check for aP. C. malfunction

while in flight,_ first establish amoderate bank; then,

release the controls to see if the aircraft will return

to straight wings-level flight as indicated by the arti-

ficial horizon. Repeat the procedure with a turn in

the opposite direction. Sluggish, erratic, or in-

complete bank recovery warns of a malfunction in the

P. C. system.

WARNING: Thoroughly familiarize yourself

with the flight characteristics of the aircraft

with Positive Control inoperative. This can

be done by simply holding down the cutoff

button while making turns and maneuvers.

Check the P. C. system frequently during each

flight to insure that it is functioning properly,

particularly when IFR or marginal weather

may be encountered.

In the event of a complete engine power loss, P. C.

will continue to operate as long as the propeller is

windmilling at 1000 RPM or more. Loss of vacuum

will automatically make the P. C. system inoperative.

However, the turn coordinator will continue to oper-

ate on electrical power. The turn coordinator can

be used as a flight reference if other gyro instru-

ments become inoperative.

3-20

ONEY OPERATORS MANUAL ONEY OPERATORS MANUAL

FUELMANAGEMENT

LOG OF PAGES Proper fuel management during flight will help main-

tain lateral trim and will also serve as afuel quantity

ONLY the pages listed herein are applicable check. After takeoff with both tanks full, use fuel

to Model M20 F, Serial Numbers from one tank for one hour; then, switch to the other

tank and note the time. Use all the fuel from the sec-

Page Date SECTION III ond tank. The remaining fuel endurance in the first

Title 10/20/75 Page Date tank can be calculated from the time it took to deplete

i. . . . . . . ...10/20/75 3-1 10/20/75 the second tank, less one hour. You must remember,

ii .... . . . . . . . 10/20/75 3-2 .......10/20/75 however, that this endurance calculating procedure can

iii . ...... . .. . 10/20/75 3-4 .. . .. . . . ..10/20/75 be relied upon only if power and mixture remain the

iv . ... . . .....10/20/75 3-5 ...... . .. . 10/20/75 same and an allowance is made for the extra fuel used

3-6 .. . . . . . .. . 10/20/75 during climb. For estimation purposes, consider fuel

3-7 . . . . . . . . . . 10/20/75 consumption during afull-power climb to be 40 percent

SECTION I•••••••••higher than that of best-power cruise, and 50 percent

Page Date 3-10 .. . . ...10/20/75 higher than that of best-economy cruise.

3-11..........10/20/75

1-1 . . .... . . . . 10/20/75 3-12 . . ....... . 10/20/75 CAUTION: Do not allow the engine to lose power

11-2 . . ........1 2200 3-13 ... . .. . ...10/20/75 or quit before switching friel tanks. If atank

1-4 . . . . . . . . . 10/20/75 3-1 .. . . ......2runs dry and the engine quits, retard the throttle

1-5 . . . . . . . . . . 10/20/75 3-16 10/20/75 before restarting. Restarting with an advanced

1-6 . . . . . . . .. . . 10/20/75 3-17 . . . .. . . . . 10/20/75 throttle may cause engine overspeeding that can

3-18 .... . .....10/20/75 lead to mechanical malfunction.

SECTION II 3-19 .... .

.· .,. . . 10/20/75

3-20...........10/20/75

Page Date 3-21 ... . . . . . ..10/20/75 INFLIGHT RESTARTING

3-22..........10/20/75

2-1 . . ..... . . . 10/20/75 3-23 10/20/75

2-2 ...... . ...10/20/75 3-24 . . . . . 10/20/75 1. Propeller--HIGH RPM.

2-3 ..........10/20/75 3-25..........10/20/75

2-4 ... . .. . ...10/20/75 3-26 .. . . . .... . 10/20/75 2. Fuel Selector--Fuller tank.

2-5 ..........10/20/75

2-6 . . ... .. . . . 10/20/75 SECT ION IV 3. Mixture Control--IDLE CUTOFF.

2-7 . . ... .. . . . 10/20/75 (FAA APPROVED)

2-8 ..........10/20/75

2-9 ..........10/20/75 Page Date 4. Boost Pump--ON.

2-10..........10/20/75 4-1 ..........10/20/75

2-11 . . . . ......10/20/75 4-2 ... . . . . . ..10/20/75 5. Throttle--OPEN 1/4 travel.

2-12..........10/20/75 4-3 ..........10/20/75

2-13..........10/20/75 4-4 ..........10/20/75

2-14..........10/20/75 4-5 ..........10/20/75

2-15..........10/20/75 4-6 ..........10/20/75

2-16..........10/20/75 4-7 ..........10/20/75

2-17..........10/20/75 4-8 ..........10/20/75

2-18 ... . . .. . . . 10/20/75 4-9 . . .. . . . . ..10/20/75 3-21

4-10..........10/20/75

ONEY OPERATORS MANUAL

OONEY OPERATORS MANUAL -

6. Ignition Switch--BOTH. LOG OF PAGES (CONT.)

7. Mixture Control--Move slowly and smoothly SECTION VSECTION Vil

to FULL RICH. (FAA APPROVED)

Page Date Page Date

8. Re-establish cruise power and RPM, then lean 5-1 ····..... . 10/20/75 7-1 ........ . .10/20/75

mixture. 5-2 •• • • · ·····10/20/75 7-2 .... . . . ...10/20/75

5-3 •• • •••····10/20/75 7-3 .... . .. . . .10/20/75

LETDOWN 5-4 • • • ···· · ··10/20/75 7-4 . . .... . .. . 10/20/75

7-5 . . . . . . . .. . 10/20/75

Plan your letdown well in advance of estimated landing 7-6 ... . . . . . . .10/20/75

time. Generally, apower-on descent is most desir- SECTION VI 7-7 . . .. . . . . . .10/20/75

able. A gradual rate of descent at cruising speed per¯ Pa eD7-8 ..... . . . . .10/20/75

mits power settings sufficiently high to maintain proper 9ate 7-9 ..... . . ...10/20/75

engine temperatures and to prevent spark plug fouling. 6-1 .... . . . . . . 10/20/75 7-10 . . . . . . ... . 10/20/75

Sudden power reductions at higher airspeeds can damage 6-2 .. . . . . . .. . .10/20/75 7-11 ....... . . .10/20/75

the engine by causing it to cool too rapidly. 6-3 ... . . . . ...10/20/75 7-12 ... . . . . . . . 10/20/75

6-4 . . . . . . . .. . 10/20/75

Establish a gradual letdown by reducing power below 6100/2200

cruise while maintaining cruise airspeed throughout 6-7 . . ..... . ..10/20/75

the descent. Monitor cylinder head and oil tempera- 6-8 . . . . . . . . . .10/20/75

tures throughout descent to guard against over cooling. 6-9 . . . . . .. . ..10/20/75

Oil in the oil cooler can congeal very rapidly after a 6-10 . . . . . . . . ..10/20/75

power reduction when flying in cold weather. 6-11 ....... . ..10/20/75

6-12 ..... . . . . .10/20/75

6-13 .. . . . .. . ..10/20/75

CAUTION: Do not lower gear above 120 MPH 6-14 .. . . . . . . ..10/20/75

(104 Knots) IAS. Do not lower flaps above

125 MPH (109 Knots) IAS. Do not exceed 125

MPH (109 Knots) IAS with the flaps down or

120 MPH (104 Knots) IAS with gear down.

BEFORE-LANDING CHECK

1. Seat Belts--FASTENED.

2. Fuel Selector Handle--SET for fuller tank.

3. Electric Fuel Pump--ON.

4. Mixture Control--FULL RICH.

5. Ram Air Control--CLOSED; warning light off.

3-22

ONE_Y OPERATORS MANUAL

GENERAL DESCRIPTION . . . . . . . . . . SECTION 6. Airspeed--REDUCE to 120 MPH (104 Knots).

7. Propeller--FULL INCREASE.

8. Landing Gear--DOWN and LOCKED; green an-

nunciator light on.

SYSTEMS OPERATIONS . . . . . . . . ...SECTION 9. Flaps--As required.

10. Trim--As required.

NORMAL PROCEDURES .... . . . . ...SECTION O i r ly, you should complete the Before-Landing

Check on the downwind leg. To allow for asafe mar-

gin above stall speed throughout approach, hold air-

speed above 90 MPH (78 Knots) until the flaps are

lowered. Degree of flap deflection needed will vary

according to landing conditions, but for most landings you

LIMITATIONS .... . . . . ........ . . SECTION should lower flaps to TAKEOFF position just prior to

turning on to base leg. Extend flaps as required on

final approach to adjust for variations in wind, glide

angle, and other variables.

WARNING: The stall warning horn and the

landing gear warning horn are inoperative when

EMERGENCY PROCEDURES ...... . . SECTION the master switch is in the OFF position.

On final, trim the aircraft to fly hands-off at an

approach speed of about 80 MPH (70 Knots). As you

cross the runway end markers, reduce power to idle.

Slow the rate of descent by increasing back pressure

PERFORMANCE ....... . ... . .. . .SECTION on the control wheel until the aircraft settles on the

runway in aslightly nose-high attitude. (When high,

gusty winds prevail, or when landing crosswind,

approach at a higher airspeed.) Slowly relax back

pressure and gently lower the nose wheel to the run-

way after main gear contact so the nose gear steering

system can be used to help control landing rollout

SERVICING....................SECTION direction.

3-23

ONEY OPERATORS MANUAL ggg ...............

CAUTION: Do not allow the aircraft to touch

down in anose-low attitude or at too high an This manual is issued as your operating guide for the

airspeed. Either of these conditions will allow Mooney Executive. It is important that you--regardless

the nose wheel to contact the runway first, of your previous experience--carefully read the hand-

which may cause the aircraft to porpoise and book from cover to cover and review it frequently.

damage the gear.

Unless ashort roll is necessary, you should allow the IMPORTANT: THIS MANUAL CONTAINS

aircraft to slow to amoderate taxi speed before ap- Federal Aviation Adininistration APPROVED

plying brakes. After leaving the runway, turn off the LIMITATIONS AND MUST BE CARRIED IN

electric fuel pump, open the cowl flaps, retract the THE AIRCRAFT AT ALI TIMES.

flaps, and reset the trim to TAKEOFF. Hold taxi

power setting between 1000 and 1200 RPM to permit All information and illustrations in this manual are

uniform engine cooling• based on the latest product information available at

the time of publication approval. The right is reserved

Execute short-field landings with partial power and to make changes at any time without notice. Every

full flaps on final approach. Reduce power to idle effort has been made to present the material in aclear

during flareout, and touch down first on the main and convenient manner to enable you to use the manual

wheels. before allowing the nose wheel to make con-

tact. You may apply brakes as soon as all wheels as aready reference. Your cooperation in reporting

are firmly on the ground. For maximum braking presentation and content recommendations is solicited.

effect, raise the flaps and apply back pressure on

the control wheel as you apply brakes. Do not skid

the main wheels, as doing so will reduce braking

effectiveness and damage the tires.

AFTER LANDING

1. Wing Flaps--RETRACT.

2. Electrical Fuel Pump--OFF.

3. Cowl Flaps--OPEN.

TAX1 CHECK

1. Throttle--1000 to 1200 RPM.

2. Lighting--As required.

3. Stabilizer Trim--TAKEOFF.

3-24 i i

.. . . . . . . . . . . . . . ONEY PERATORS MANUAL

Mooney warrants each Aircraft (which includes SHUTDOWN CHECK

its accessories and equipment) sold hereunder,

to be free from defects in materialand workman- 1. Throttle--IDLE at 1000 to 1200 RPM until cy-

ship under normal use and service when operated linder head temperature starts to drop.

in accordance with Mooney's operating instruc-

tions during the period of six (6) months following 2. Cowl Flaps--OPEN.

delivery of the Aircraft to the original retail pur-

chaser or the first user or during the period of 3. Radios--OFF.

one (1) year foÈowing

the date of issue of the ori- 4. Electrical Switches--OFF.

ginal airworthiness certificate for the Aircraft,

whichever period first terminates. Mooney does 5. Mixture Control--IDLE CUTOFF.

not make any warranties with respect toequipment

and accessories not manufactured by Mooney but 6. Throttle--RETARD as engine stops firing.

Mooney assigns to any owner of such Aircraft (to

the extent same may be assignable) any warranties 7. Ignition Switch--OFF when propeller stops.

Mooney has received from the manufacturers of

such equipment and accessories and will, on re- 8. Parking Brake--Set (for short-term parking).

quest, provide and execute such instruments as may

be reasonably required to evidence such assignment. 9. Trim--TAKEOFF.

Mooney's obligation under this warranty is limited

to repairing or replacing, at Mooney's option, any 10. Flaps--RETRACTED.

part or parts which within the applicable warranty 11. Master Switch--OFF.

period set forth above, shall be returned, trans-

portation charges prepaid, to Mooney's plant in 12. Control Wheel--LOCK with seat belt.

Kerrville, Texas or to such other location desig-

nated by Mooney, and which upon examination, shall 13. Overhead Air Scoop--CLOSED.

disclose to Mooney's satisfaction that such part is

defective. Anew warranty period is not established 14. Wheel Chocks and Tiedown--As required.

for parts replaced hereunder. Parts replaced here-

under are warranted for the remainder of the original

warranty period applicable to Aircraft sold hereunder.

The repair or replacement of defective parts under

this warranty shall be made by Mooney without charge

for the parts, or labor for removal, installation and/

or actual repair of defective parts.

This warranty does not apply to Air craft, equipment,

accessories, or other parts manufactured or sold by

iii3-25

Mooney which have been subject to misuse, negligence,

accident or improper installation, or which have been

repaired or altered outside of Mooney's plant in a

way which, in the opinion of Mooney, adversely

affects its performance or reliability. Further, this

warranty does not include normal maintenance ser-

vices (such as engine tune-up; cleaning, control rig-

ging, brake and other mechanical adjustments,

maintenance inspections, etc.) and the replacement

of service items (such as sparksplugs, brake linings,

filters, hoses, belts, tires, etc.) made in connection

with such services or required as maintenance, nor

to normal deterioration of soft trim and appearance

items (such as, paint, upholstery, rubber-like items,

etc.)dueto wear and exposure.

This warranty shall extend to any owner (hereafter

"Owner") of the Aircraft making claim within the

specified warranty period.

THIS WARRANTYBY MOONEY IS MADE EXPRESSLY IN

LIEU OF ANY OTHER WARRANTIES EXPRESSED OR IM-

PLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED

WARRANTYOF MERCHANTABILITY OR FITNESS FOR A

PARTICULAR PURPOSE, AND IS IN LIEU OF ANY OTHER

OBLIGATION OR LI.ABILITY ON THE PART OF MOONEY

TO ANYONE OF ANY NATURE WHATSOEVER BY REASON OF

THE MANUFACTUREAND/OR THE SALE AND/OR THE USE

OF SUCH AIRCRAFT. MOONEY SHALL IN NO EVENT BE

LIABLE TO ANY OWNER OR TO ANY OTHER PARTY OR

PARTIES FOR SPECIAL, INCIDENTAL OR CONSEQUEN-

TIAL LOSS OR DAMAGES 08 FOR ANY OTHER LOSS OR

DAMAGE TO PROPERTY AND/OR INJURY OR DEATH TO

PERSONS OTHER THAN FOR THE PROPERTY DAMAGETO

SUBJECT AIRCRAFT PROXIMATELY RESULTING FROM ANY

BREACH BY MOONEYOF THE AFORESTATED WARRANTY,

MOONEY NEITHER ASSUMES .NOR AUTHORIZES BUYER OF

ANYCNE ELSE TO ASSUME FOR IT ANY OBLI.GATION OR

LIABILITY IN CONNECTION WITH THE AIRCRAFT SUB-

JECT HEREOF, OTHER THAN THOSE EXPRESSLY SET.0UT

HEREIN. NO BILL OF SALE OR TRANSFER OF TITLE

TO THIS AIRCRAFT SHALL NULLIFY THE PROVISIONS

HEREOF.

SECTION I. GENERAL DESCRIPTION

DESIGN FEATURES SECTIONS IV. &V.

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

POWERPLANT........................1-2 FAA APPROVED

FLIGHTCONTROLS.....................1-3 AIRPLANEFLIGHTMANUAL

LANDINGGEAR .......................1-3

SPECIFICATIONSOUTUNE

POWERPLANT........................1-3

PROPELLER .........................1-4 SECTION IV.

LANDINGGEAR .......................1-4 AIRCRAFT LIMITATIONS

FUEL&OIL..........................1-5 AND OPERATIONS

WEIGHT&LOADING....................1-5

BAGGAGE COMPARTMENT . . . . .. . .. . . . . ..1-5

MOONEY MODEL M20F

EXECUTIVE

MOONEY AIRCRAFT CORPORATION

SERIAL NO.:

REGISTRATION NO.:

This Manual Must Be Kept Onboard The Airplane At All Times

APPROVED BY:

CHIEF,ENGINEERING &MANUFACTURING BRANCH,

SOUTHWEST REGION,FEDERAL AVIATION ADMINISTRATION

DATE:

1-1 4-1

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