cessna check list

11. Position Aircraft

2. Maintenance Logbook

3. Control Lock

4. Battery Switch

5. Check Fuel

6. Battery Switch

EXTERNAL CHECK

Check

Signed

Release

On

L & R tank

Off

Completed

THE PRE-FLIGHT CHECK

2 INTERNAL COCKPIT

20091

1. Fire extinguisher

2. Parking brake

3. Fuel valve

4. Throttle

5. Mixture

6. Primer

7. Doors & Windows

1. Look Around

2. Call to Fireman

3. Master Switch

4. Fuel Quantity

5. Call to Fireman

6. Engine Running

7. Set Throttle

1. Eng. Inst & Suction

2. Radio & Avionics

3. Direct. Gyro Indictr.

4. Rotating Beacon

1. Throttle 1400

2. Set Throttle

3. Call Tower for Clearance

4. Closed Throttle

5. Look Around

6. Parking Break

A. Before Starting Check

B. Starting Procedure

C. After Starting Engine

D. Before Taxi

in position

Set

On or Both

1/3 Open

Full Rich

2-6 stroke

Closed & Locked

L/Front/R Clear

Clear

On

Check L/R

Contact

Oil Press Check

1200 Rpm

Check

On & Test

Set

On

Flaps down and up

1200 Rpm

Chocks off

All Clear

Off

20092

1. Seat & Belt

2. Flight Control

3. Trim Check

4. Fuel Valve/Selector

5. Master Switch

6. Ignition

7. Parking Break

8. Altimeter

9. All Light Switch

10. Fuses

11. Carburetor Heater

12. Throttle

13. Mixture

14. Flaps

15. Cabin Air

16. Cabin Heat

17. Chocks

Adjust & Set

Free & Respond

Travel & Neutral

On & Both

Off

Off

Off

Set to Elevation

Off

All In

Off

Open & Closed

Idle Cut Off

Up

Off

Off

In Position

STARTING PROCEDURES3

41. Brake


3. Turn & Bank

Smoothly until

A/C Stop

Check

Check

WHILE TAXI (memory item)

1. Park A/C in position

2. Parking brake

3. Throttle

4. Doors & Windows

5. Engine Instrument

6. Ignition


8. Mixture

1. Look Around

2. Throttle open smoothly

3. Engine inst

4. Magnetos Check

Both to Left

Both to Right

5. Carb Heat Check

6. Idling

7. Ampere

8. Throttle

A. Before Run-up

B. Running Up

45 to R/W in use

Set

Set 1200 Rpm

Closed & Locked

Check

Both

Off

Full Rich

All clear

1700 Rpm

Check

Max Drop 125 Rpm

Max Drop 125 Rpm

Rpm drop slightly,

then Off

650 Rpm

Check

Set 1200 Rpm

RUN-UP PROCEDURES5

20093

TAKE-OFF PROCEDURES

1. Doors & Windows

2. Seat & Belt

3. Flight Control

4. Fuel Valve

5. Ignition

6. Master Switch

7. Flight & Engine Inst


9. Mixture

10. Flaps

11. Trim Set

12. Check Traffic

13. Landing light

14. Parking Brake

15. Taxi


2. Altimeter

3. Artificial Horizon

4. Call Tower

5. Brake Off,

1. Safe Airborne

2. Landing Light

3. Power

4. Speed

5. A/C Climb attitude

6. Engine Instrument

A. Before Take-off

B. Take-off

C. After Take-off

(memory item)

Throttle Open Smoothly

(memory item)

Closed & Locked

Secure

Free & Respond

On Both

Both

On

Check

Off

Full Rich

Up

Take Off Position

Clear, Call Tower

On

Off

To line up position

Set

Set

Set

For clearance

Gears up, Flaps up

Off

Set full

80 Kts Check

Check

Check

20094

6

LANDING PROCEDURES

1. Altimeter & Heading

2. Master Switch

3. Ignition

4. Mixture

5. Fuel valve

6. Seatbelt & Harness

7. Call to Tower

1. Approach Speed

2. Flaps

3. Trim

4. Landing Light

1. Flaps

2. Trim

3. Non-essential electric

1. Parking Brake

2. Throttle

3. Radio & Nav. Aid

4. Rotating Beacon

5. Mixture

6. Propeller stop

7. Master switch

8. Ignition

9. All light Switch

10. Parking Brake

11. Control

12. Log book

A. Pre-landing

B. Final check

C. After landing

D. Stopping Engine

(memory item)

(memory item)

(memory item)

Check

On

Both

Full Rich

Both on

Secure

Down wind

Check

As required

As required

As required

Up & neutral

Neutral

As required

Set on

Set 1000 Rpm

Off

Off

Off

Throttle open

Off

Off

Off

Off

Locked

Signed

7

20095

CHANGE OF CONFIGURATION

Cruise to Climb

Climb to Cruise

Cruise to Descend

Descend to Cruise

100 ft

Cruise to Glide

Glide to Cruise

1. Put the nose to climb attitude, wing level & ball center.

2. Speed will decrease

3. at the same time

4. Apply to maintain wing level & ball center.

5. Maintain climb speed & heading

6. Maintain climb attitude and trim the A/C

1. Put the nose on the cruising attitude, Check

2. Speed increase to

3. Reduce power to

4. Apply left rudder to maintain ball center

5. Maintain altitude, heading and trim the A/C

1. Reduce power to

2. at the same time apply to maintain ball center

3. Push down to descend attitude

4. Maintain heading & VSI at down, trim the A/C

1. Pull the nose to cruise attitude; VSI: , wing level & ball center

2. Open power to before altitude

3. Apply to maintain ball center

4. Maintain heading, altitude & trim the A/C

1. & apply to maintain ball center

2. Set the to glide attitude

3. Check speed

4. Maintain gliding attitude and speed

5. Trim the A/C

1. Set the nose to cruise attitude

2. at the same time open power to

3. Apply to maintain wing level & ball center

4. Maintain cruise altitude, heading and speed

5. Trim the A/C

(85 mph/75 knots)

open power 2500 rpm

right rudder

VSI: 0 fpm

90 mph - 100 mph

2100 rpm

1800 rpm

left rudder

nose

500 fpm

0 fpm

2100 rpm

right rudder

Close power left rudder

nose

80 mph/70 knots

2100 rpm

right rudder

20096

CHANGE OF CONFIGURATION

Cruise to Slow Flight

Slow Flight to Cruise

Cruise to Slow Flight descend

Slow Flight descend to Cruise

1. Reduce power to


3. Maintain altitude & heading

4. Speed white arc, lowering flaps to

5. Hold the nose, check

6. Check speed approaching

7. Open to maintain slow flight speed

8. Apply to maintain ball center

9. Maintain altitude , heading and trim the A/C

1. Open power to

2. Apply to maintain wing level ball center

3. Speed will increase to

4. Flaps

5. Hold the nose, check

6. Maintain wing level ball center

7. Maintain heading & altitude

8. Trim the A/C

1. Reduce power to


3. Speed white arc, lowering flaps to

4. Speed approaching slow speed, set the nose down

5. Trim the A/C

1. Open power to


3. Flap

4. Set the nose to cruising attitude

5. Trim the A/C

1800 rpm

left rudder

10

VSI: 0 fpm

80 mph/70 knots

power as required

right rudder

VSI: 0 fpm

2100 rpm

right rudder

100 mph/87 knots

10 up

VSI: 0 fpm

1500 rpm

left rudder

10down

2100 rpm

right rudder

10up

SHALLOW TURN - 10

NORMAL TURN - 15

MEDIUM TURN - 30

STEEP TURN - 45

RATE ONE TURN - 10% TAS (True Air Speed) + 7 (usually 16-20bank)

VISUAL AIRWORK

20097

PRE - STALL CHECK

1. Min. altitude

2. Check heading

3. Clearing turn

4. While turning

5. Cockpit check

Ignition

Master switch

Carb. heat

Mixture

Flaps

Fuel valve

No loosing object

3000 ft

45 left & right

Check not above town

No low clouds

Not facing the sun

Doors & Windows locked

Both

On

Stand by

Full rich

Stand by

Both on

Check

CLEAN STALL EXERCISE

Execution:

check VSI

Recovery:

After stall check:

1. Close (smoothly)


3. Carburetor heater

4. Maintain & ( )

5. Check speed approaching Vso

1. Lower the


3. Open power


5. Stop sink, check speed

6. Set to climb back to initial altitude

7. Trim the A/C

1. Engine instrument check:

throttle

left rudder

on

heading altitude

57 mph/50 knots

nose positive below horizon

off

full (2500 rpm)

right rudder

80 mph/70 knots

nose

Oil pressure (green)

Oil temperature (green)

Suction (green)

20098

DIRTY STALL EXERCISE

Do Pre-stall check first

Execution:

check VSI=0 fpm

Recovery:

After stall check:

1. Close (smoothly)


3. Check speed then

4. Wing level & ball center

5. Flaps

6. Close throttle


8. Wing level & ball center

9. Maintain & ( )

10. Check speed approaching dirty stall speed

1. Lower the


3. Open power


5. Check speed:

flaps up from 30-20

flaps up from 20-10

flaps full up

6. Speed

7. Set to climb back to initial altitude

8. Trim the A/C

1. Engine instrument check:

throttle to 1800 rpm

left rudder

white arc flaps 10

30/full down

on

heading altitude

49 mph/43 knots

nose positive below horizon

off

full (2500 rpm)

right rudder

60 mph/52 knots:

65 mph/57 knots:

70 mph/60 knots:

75 mph/65 knots

nose

Oil pressure (green)

Oil temperature (green)

Suction (green)

20099

EMERGENCY (Forced landing)

Below 1000 ft

gears up & flaps up

Above 1000 ft

gears up & flaps up

1000 ft loose

1. Fly A/C or push flight control fwd for

2. Clean configuration:

3. Check gliding speed:

4. Trim the A/C

5. Select the field 45 left & right

6. Call MAYDAY 3X

7. Check for cause:

Ignition

Master switch

Carburetor heater

Mixture

Fuel valve

8. Secure the engine:

Ignition

Master switch

Mixture

Fuel valve

1. Fly A/C or push flight control fwd for

2. Clean configuration:

3. Check gliding speed:

4. Trim the A/C

5. Check for cause:

Ignition

Master switch

Carburetor heater

Mixture

Fuel valve

6. Try to restart engine (if failed)

7. Select the field 45 left & right

8. Call MAYDAY 3X

9. Secure the engine:

Ignition

Master switch

Mixture

Fuel valve

10. Every - clearing engine (e.g. from ice or failure)

gliding attitude

gliding attitude

80 mph/70 knots

80 mph/70 knots

Both

On

Off

Full rich

On/both

Off

Stand by (for flaps & radio)

Idle cut off

Off

Both

On

Off

Full rich

On/both

Off

Stand by (for flaps & radio)

Idle cut off

Off

200910

GO AROUND

1. Carburetor heat off

2. Open power, apply right rudder to maintain ball center

3. Check VSI and gears up & speed:

flaps up from 30-20

flaps up from 20-10

flaps full up

climb back to initial altitude

4. Engine instrument check

60 mph/52 knots:

65 mph/57 knots:

70 mph/60 knots:

75 mph/65 knots:

EMERGENCY PROCEDURE at START

A. Oil pressure fail to indicate

B. Engine fire

C. Radio fails

D. Radio transmitter (Tx) fails

D. Radio receiver (Rx) fails

1. Within 30 sec the OIL PRESSURE should be indicated

2. If not, cancel start by pulling the mixture control handle

3. Report to the mechanics

Continue cranking, then followed by:

1. Mixture

2. Throttle

3. Fuel valve

4. All electrical switches

5. Use fire extinguisher

6. Abandon A/C into the wind

1. After start-turn on Radio & ADF system-turn to correct frequencies

2. If there is no sound on Tx or Rx, try to reselect or re-tune to other freq.

3. Tx: turn the volume control to maximum selection

4. Rx: turn to squelch control to maximum selection

5. If there is still no sound, cancel the flight

1. RTB by following the traffic

2. Keep listening, watch for tower instruction & traffic

3. Switch on the landing light on final approach

4. Make a safe landing and cancel the flight

1. Watch the traffic and explain in the trouble (Blind Transmision)

2. Make a low pattern (500 ft), fly along the R/W by rocking wing several times

3. Report your position 2-3 times by mention I say again

4. Make a safe landing and cancel the flight

Idle cut off

Full open

Off

Off

As necessary

200911

EMERGENCY PROCEDURE

DURING TAKE-OFF

(Just After Airborne)

A. Engine fails

B. Engine fire

C. Air speed indicator fail

1. Decide to land again

2. Close throttle smoothly

3. Maintain

4. Apply brake if necessary, till the A/C stops

5. Complete the final check list

6. Call tower and explain the trouble

7. Cancel the flight

1. Decide to land again

2. Mixture idle cut off

3. Maintain

4. Apply brake if necessary, till the A/C stops

5. Try to turn the A/C into tail wind position

6. Complete the final check list


8. Use fire extinguisher if necessary


1. During T/O run, if there is no air speed indicator:

Close throttle

Apply brakes

Cancel the flight

2. Do an external check:

Static holes & pitot tube should be cleared from water or dust

heading or keep straight

heading or keep straight

200912

EMERGENCY PROCEDURE

AFTER TAKE-OFF (Up to 1000 ft)

A. Engine fails

B. Engine fire

C. Air speed indicator fail

1. Push flight control for gliding attitude

2. Close throttle smoothly, maintain gliding speed

3. Proceed to the best field for forced landing

4. Check for causes, if necessary:

Fuel pressure/Qty, Booster/Fuel Pump, Mixture control & Fuel

Selector

Oil Pressure

Switch

Carburetor heater control

Master switch

5. Do final cockpit check


7. Try to land the A/C safely

8. Abandon the A/C after stop rolling

1. Mixture idle cut off

2. Fuel valve off

3. Put the nose into gliding attitude and maintain gliding speed

4. Fly side slip by means of cross control

5. Do final cockpit check & use fire extinguisher

6. Select the best field

7. Try to land the A/C safely, use flaps as necessary

8. Abandon the A/C into the wind


1. Continue flying

2. Watch the A/C attitude and power setting

3. RTB by following the tower (ATC) instruction

4. Make a normal approach and landing

5. After parking the A/C, do external check & report to technician

200913

EMERGENCY PROCEDURE

ENGINE QUIT (at area or at circuit)

1. Fly the A/C with gliding speed

2. Trim the A/C

3. Check for causes

Master switch

Ignition

Mixture

Fuel valve

4. No remedy (no respond)

5. Select field for landing

6. Say: MAYDAY 3X, PK-....make force landing at...area

7. A/C force landing patern S or 8

8. A/C on final - flap full down

Master switch

Ignition

Mixture

Fuel valve

9. Altitude ~300 ft AGL, A/C go around:

Carburetor heat

Ignition

Mixture

Fuel valve

Return to base by means of ADF Homing procedure

1. Fly with long range power setting (down wind power setting)

2. Call tower or other A/C in the air

3. Explain your last position, if possible explain easy observable

visual fix

or

1. During report to tower, explain that you picked a new

heading: North

2. Continue with heading north (compass) till reaching coast line

3. Turn to heading east or west (compass) and try to observe

a known check point

4. Fly home, if you are sure your last check point

5. Avoid cloud or fly below the cloud but do not fly below

500 ft, if possible

A. RTB

B. ADF fail

LOST POSITION

200914

129.90

118.30

118.60

128.80

122.30

122.20

127.90

119.75

122.10

116.40

113.30

115.80

882

215

400

399

250

365

275

Jkt Info

HLM TWR

HLM TWR

ATIS

Atang TWR

Budiarto TWR

JKT APP

JKT APP

PGG TWR

IMU VOR

HLM VOR

Budiarto VOR

TMII

AL 9 Nm NE HLM

Budiarto

Atang

PW

CA

PG

200915

Cessna 172 Type Rating

Gross weight

Rate of climb at sea level

Service ceiling

Standard tank

Long range tank

Oil capacity

Engine

Take-off ground run

50 ft obstacle

Landing ground roll

50 ft obstacle

Vne (never exceed)

Caution range

Vno (normal operation)

Vfe (flap extended)

Vx (best angle of climb)

Vy (best rate of climb)

Vso (dirty stall speed)

Vs1 (clean stall speed)

Vmu (maneuvering speed)

Oil temp normal operating range

Maximum allowable

Oil pressure minimum idling

Normal operating range

Maximum

Panjang pesawat

Lebar wing span

Lebar horizon stabilizer

Lebar main wheel

Tinggi pesawat

Propeller

Nose wheel tire pressure

Main wheel tire pressure

Nose gear shock strut

2300 lbs

645 fpm

13100 ft

42 gallon (usable 38)

52 gallon (usable 48)

8 quartz (min. 6 quartz)

Lycoming O-320-E2D

(150 BHP at 2700 rpm)

865 ft

1525 ft

520 ft

1250 ft

182 mph ( )

145-182 mph ( )

61-145 mph ( )

54-100 mph (white arc)

80 mph/70 knots

85 mph/75 knots

49 mph/43 knots

57 mph/50 knots

112 mph/97 knots

245F ( )

25 psi ( )

60-90 psi ( )

100 psi ( )

26 ft 11 in (323 in)

36 ft (432 in/10.8 m)

11 ft 4 in (136 in/3.45 m)

8 ft 4.5 in (100.5 in/2.67 m)

8 ft 9.5 in (105.5 in/2.5 m)

6 ft 3 in (75 in/1.9 m)

31 psi on 5.00-5.4 ply rated



Keep filled with MIL-H-5506 hydraulic

fluid & inflated air to 45 psi

red line

red line

red line

yellow arc

green arc

green arc

green arc

red line

200916

COCKPIT/BRIEFING EXERCISES

200917

TIMING TURN

Rate One Turn (ROT)

10 before:

5 before:

3 before:

Preparation

Clearing turn

Start turn

Descending Turn

15 before:

10 before:

5 before:

3 before:

Preparation

Clearing turn

Reduce power to descend

Start turn

Climbing Turn

15 before:

10 before:

5 before:

3 before:

Preparation

Clearing turn

Set the nose to climb, open power

Start turn

Slow Flight Rate One Turn

15 before:

10 before:

5 before:

3 before:

Preparation

Clearing turn

Reduce power, flaps 10

Start turn

Slow Flight Rate One Turn

20 before:

15 before:

10 before:

5 before:

3 before:

Preparation

Clearing turn

Reduce around 1400, flaps 10

Descend

Start turn

10 sec

30 sec

60 sec

90 sec

120 sec

30

90

180

270

360

loosing 250 ft

loosing 500 ft

loosing 750 ft

loosing 1000 ft

Climb turn:

Altitude Heading

Maintain speed climbing

VSI

Descending turn:

Altitude = Heading

VSI = 500 fpm down

Speed

Slow Flight Descending turn:

Altitude = Heading

VSI = 500 fpm down

Speed = slow flight

CONVERSIONS

1 nautical mil (nm)

1 mph

1 naut, mph

1 knot/hr

1 mile

1 feet

1 meter (m)

1 kg

1 US gal

1 liter

1.853 km

88.0 fpm

1 knot

1.15 mph

1.609 km

5280 ft

0.3 m

3.28 ft

2.205 lbs3.78543 liters

0.264 US gal

+10

-15

pass

pass

passp

ass

+5+5

-5-5

-10-10

NOTE

(+AFTER)(-BEFORE)

COMPASS ERROR

200918

BEFORE START BRIEF

START ENGINE BRIEF

BEFORE & DEPARTURE BRIEF

TAKE-OFF BRIEF

Destination...Fuel qty L/R...Endurance...Oil qty...MLB sign...Wx...QAM

1. Start engine from left hand seat

2. During start if engine fire or electrical fire occurs, I will:

Open power to for a few second to flame out

3. If still firing, abort start engine for evacuation and follow your instruction

1. Taxi from left hand seat,

2. Departure to...stand by altitude...R/W in use...via taxiway...

3. While taxi if engine fire or electrical fire occurs, I will:

4. If brake fails, shut down engine & bring A/C to an open & clear area

1. Take-off from left hand seat, for static or normal T/O

2. Check unstick seed (Vr)

3. If anything malfunction before Vr, I will abort take-off:

If enough R/W continue landing

If out of R/W, continue for T/O

I will fly A/C check 45 L/R select the field

execute force landing

RTB to join down wind

Execute emergency landing

1. Continue flying

2. Check the A/C attitude & power setting

3. RTB following ATC instruction

4. Make normal landing

5. At parking area, external check

6. Check static hole & pitot tube from water & dusts

1700 rpm

a. apply brake

b. close throttle

c. mixture idle cut off

d. call ATC for cancellation of flight

a. close throttle

b. max brake

c. out of R/W

d. call ATC for cancellation of departure

START ENGINE BRIEF COMPLETED

TAXI & DEPARTURE BRIEF COMPLETED

Engine malfunction after airborne

Malfunction at 500 ft

Malfunction at 1000 ft

TAKE-OFF BRIEF COMPLETED, ANY QUESTION?

AIRSPEED INDICATOR FAILS DURING FLIGHT

200919 200920

C-1

72

left

dow

n w

ind R

/W 2

4 N

OR

MA

L C

IRC

UIT

W

AR

NIN

G: K

no

t sp

ee

d a

re a

n e

stim

ate

con

ve

rsio

n o

f 1

nm

/hr

= 1

.15 m

ph

2406

150

240

330

060

Lin

e u

p:

DG

I A

H &

Altim

ete

r

pow

er

full

Rig

ht ru

dder

1. C

ente

r lin

e,

apply

bra

ke

2.

to c

om

pass,

set

3. C

all

To

wer

4. B

rake

re

lease,

foot

dow

n t

o r

udder

5. O

pen

6.

to k

eep c

ente

r lin

e

Positiv

e c

limb 2

00 f

t:

up

off

85 m

ph/7

5 k

1.

Gears

2.

Landin

g lig

ht

3.

Speed

t cont.

to c

limb

4.

Main

tain

headin

g

5.

Win

g level, b

all

cente

r

Rolli

ng:

1.

Keep c

ente

r lin

e b

y r

ight

rudder

2.

Speed 6

0 m

ph/5

0 k

t U

nstick

Safe

altitude 4

00 f

t: 85 m

ph/7

5 k

t

1.

Fla

ps u

p

2.

Pow

er

set

3.

Speed c

limbin

g

4.

Win

g level, b

all

cente

r

5. T

/O p

ath

check

Turn

ing c

ross w

ind b

y c

he

ck p

oin

t

(fre

e w

ay/5

00 f

t):

1.

Cle

aring t

urn

2. T

urn

(ra

te o

ne t

urn

)

3.

Continue c

limb

Cro

ss w

ind leg:

1. A

fter

T/O

check

2.

Continue c

limb t

o 1

000

ft

Ente

ring D

ow

n w

ind (

red s

oil)

:

Altitude 1

000 f

t

headin

g r

ecip

roca

l R

/W in

use

1. T

urn

to d

ow

n w

ind (

rate

one t

urn

)

2.

3.

Spacin

g 1

win

g &

4.

Speed m

ax w

hite a

rc

Dow

n w

ind (

pre

-landin

g c

x):

altitude 1

000 f

t

speed (

~90-1

00 m

ph)

DG

I to

com

pass

Cockpit c

heck

1.

Check

2.

Check

3.

Check d

ista

nce t

o R

/W (

1 w

ing)

4.

Check w

ind s

ock

5.

Check

6.

Check A

/C f

ly p

ara

llel R

/W

7.

8.

Call

tow

er

Co

ckp

it c

heck:

on

both

off

full

rich

both

or

on

secure

d

locked

Maste

r sw

itch

Ignitio

n

Carb

ure

tor

heat

Mix

ture

Fuel valv

e

Seat

belt

Doors

& w

indow

s

DO

WN

WIN

D (

betw

een 2

lakes)

Ab

eam

(para

llel th

resh

old

):

1800 r

pm

flaps 1

0 d

ow

n

85 m

ph/7

5 k

t

VS

I =

300-4

00 fpm

gears

dow

n

1. R

educe

pow

er

to

2. S

peed w

hite a

rc,

3. S

peed

, set nose

dow

n

4.

5. 20 s

eco

nd

Turn

ing b

ase leg (

gre

en m

osque):

45/~

33 s

econd/9

00-9

50 ft/check p

oin

t

Bank 2

0

20

VS

I=30

0-4

00 fpm

1.

2. C

learing turn

3.

4. F

laps

dow

n

5. C

ontinue d

escend

Base leg: h

eadin

g 75 m

ph/6

5 k

t

1. C

heck

2. C

heck s

peed

3. C

all

tow

er Fin

al:

on s

lope

1. A

/C

()

2. C

heck s

peed

3. C

all

tow

er

1st to

4. T

hen fla

p

5.

oncente

r lin

e

70 m

ph/6

0 k

t

get cle

ara

nce

30 (

or

as r

equire

d)

Landin

g lig

ht

At short

:

1. C

all

tow

er

2. Landin

g lig

ht on

DO

WN

WIN

D (

betw

een 2

lakes)

C-1

72

left

dow

n w

ind R

/W 2

4 F

LA

PL

ES

S C

IRC

UIT

W

AR

NIN

G: K

no

t sp

ee

d a

re a

n e

stim

ate

con

ve

rsio

n o

f 1

nm

/hr

= 1

.15 m

ph

2406

150

240

330

060

Lin

e u

p:

DG

I A

H &

Altim

ete

r

pow

er

full

Rig

ht ru

dder

1. C

ente

r lin

e, apply

bra

ke

2.

to c

om

pass,

set

3. C

all

To

wer

4. B

rake

re

lease,

foot

dow

n t

o r

udder

5. O

pen

6.

to k

eep c

ente

r lin

e

Positiv

e c

limb 2

00 f

t:

up

off

85 m

ph/7

5 k

1.

Gears

2.

Landin

g lig

ht

3.

Speed

t cont.

to c

limb

4.

Main

tain

headin

g

5.

Win

g level, b

all

cente

r

Rolli

ng:

1.

Keep c

ente

r lin

e b

y r

ight

rudder

2.

Speed 6

0 m

ph/5

0 k

t U

nstick

Safe

altitude 4

00 f

t: 85 m

ph/7

5 k

t

1.

Fla

ps u

p

2.

Pow

er

set

3.

Speed c

limbin

g

4.

Win

g level, b

all

cente

r

5. T

/O p

ath

check

Turn

ing c

ross w

ind b

y c

heck p

oin

t

(fre

e w

ay/5

00 f

t):

1.

Cle

aring t

urn

2. T

urn

(ra

te o

ne t

urn

)

3.

Continue c

limb

Cro

ss w

ind leg:

Continue t

urn

700 ft

1. A

fter

T/O

check

2.

3.

Continue c

limb t

o

Ente

ring D

ow

n w

ind (

red s

oil)

:

Altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

headin

g r

ecip

roca

l R

/W in

use

1. T

urn

to d

ow

n w

ind (

rate

one t

urn

)

2.

3.

Spacin

g 1

win

g &

4.

Speed m

ax w

hite a

rc

Dow

n w

ind (

pre

-landin

g c

x):

altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

speed (

~90-1

00 m

ph)

DG

I to

com

pass

Cockpit c

heck

1.

Check

2.

Check

3.

Check d

ista

nce t

o R

/W (

1 w

ing)

4.

Check w

ind s

ock

5.

Check

6.

Check A

/C f

ly p

ara

llel R

/W

7.

8.

Call

tow

er

Co

ckp

it c

heck:

on

both

off

full

rich

both

or

on

secure

d

locked

Maste

r sw

itch

Ignitio

n

Carb

ure

tor

heat

Mix

ture

Fuel valv

e

Seat

belt

Doors

& w

indow

s

Ab

eam

(para

llel th

resh

old

):

1600-1

700 r

pm

90 m

ph/8

0 k

t

300-4

00 fpm

gears

dow

n

1. R

educe

pow

er

to

2. S

et nose

dow

n, S

peed

3. V

SI

4. 20 s

eco

nd

Turn

ing b

ase leg (

gre

en m

osqu

e):

45/~

33 s

econd/9

00-9

50 ft/check p

oin

t

Bank 2

0

VS

I=300-4

00 fpm

1.

2. C

learing turn

3.

4. C

ontinue d

escend

Base leg: h

eadin

g 80 m

ph

/70 k

t

1. C

heck

2. C

heck s

peed

3. C

all

tow

er Fin

al:

on s

lope

1. A

/C

()

2. C

heck s

peed

3. C

all

tow

er

1st to

4.

oncente

r lin

e

75 m

ph/6

0 k

t

get cle

ara

nce

Landin

g lig

ht

At sh

ort

:

1. C

all

tow

er

2. Landin

g lig

ht on

200922200920

Ente

ring D

ow

n w

ind (

red s

oil)

:

Altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

headin

g r

ecip

rocal R

/W in

use

1. T

urn

to d

ow

n w

ind (

rate

one t

urn

)

2.

3.

Spacin

g 1

win

g &

4.

Speed m

ax w

hite a

rcD

OW

N W

IND

(betw

een 2

lakes)

Ab

eam

(para

llel th

resh

old

):

1800 r

pm

flaps 1

0 d

ow

n

85 m

ph/7

5 k

t

700 ft

gears

dow

n

1. R

educe

pow

er

to

2. S

peed w

hite a

rc,

3. S

peed

, set nose

dow

n

4. M

ain

tain

5. 20 s

eco

nd C

-172

left

dow

n w

ind R

/W 2

4 L

OW

CIR

CU

IT

WA

RN

ING

: K

no

t sp

ee

d a

re a

n e

stim

ate

con

ve

rsio

n o

f 1

nm

/hr

= 1

.15 m

ph

2406

150

240

330

060

Lin

e u

p:

DG

I A

H &

Altim

ete

r

pow

er

full

Rig

ht ru

dder

1. C

ente

r lin

e, apply

bra

ke

2.

to c

om

pass,

set

3. C

all

To

wer

4. B

rake

re

lease,

foot

dow

n t

o r

udder

5. O

pen

6.

to k

eep c

ente

r lin

e

Positiv

e c

limb 2

00 f

t:

up

off

85 m

ph/7

5 k

1.

Gears

2.

Landin

g lig

ht

3.

Speed

t cont.

to c

limb

4.

Main

tain

headin

g

5.

Win

g level, b

all

cente

r

Rolli

ng:

1.

Keep c

ente

r lin

e b

y r

ight

rudder

2.

Speed 6

0 m

ph/5

0 k

t U

nstick

Safe

altitude 4

00 f

t: 85 m

ph/7

5 k

t

1.

Fla

ps u

p

2.

Pow

er

set

3.

Speed c

limbin

g

4.

Win

g level, b

all

cente

r

5. T

/O p

ath

check

Turn

ing c

ross w

ind b

y c

heck p

oin

t

(fre

e w

ay/5

00 f

t):

1.

Cle

aring t

urn

2. T

urn

(ra

te o

ne t

urn

)

3.

Continue c

limb

Cro

ss w

ind leg:

Continue t

urn

700 ft

1. A

fter

T/O

check

2.

3.

Continue c

limb t

o

Dow

n w

ind (

pre

-landin

g c

x):

altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

speed (

~90-1

00 m

ph)

DG

I to

com

pass

Cockpit c

heck

1.

Check

2.

Check

3.

Check d

ista

nce t

o R

/W (

1 w

ing)

4.

Check w

ind s

ock

5.

Check

6.

Check A

/C f

ly p

ara

llel R

/W

7.

8.

Call

tow

er

Co

ckp

it c

heck:

on

both

off

full

rich

both

or

on

secure

d

locked

Maste

r sw

itch

Ignitio

n

Carb

ure

tor

heat

Mix

ture

Fuel valv

e

Seat

belt

Doors

& w

indow

s

Turn

ing b

ase leg (

gre

en m

osqu

e):

45/~

33 s

econd/9

00-9

50 ft/check p

oin

t

Bank 2

0

20

VS

I=300-4

00

fpm

1.

2. C

learing turn

3.

4. F

laps

dow

n

5. S

tart

descend

Base leg: h

eadin

g 75 m

ph/7

0 k

t

1. C

heck

2. C

heck s

peed

3. C

all

tow

er

Fin

al:

on s

lope

1. A

/C

()

2. C

heck s

peed

3. C

all

tow

er

1st to

4. T

hen fla

p

5.

oncente

r lin

e

70 m

ph/6

0 k

t

get cle

ara

nce

30 (

or

as r

equire

d)

Landin

g lig

ht

At sh

ort

:

1. C

all

tow

er

2. Landin

g lig

ht on

200923

Base leg: h

eadin

g 80 m

ph/7

0 k

t

1. C

heck

2. A

pply

fla

ps g

radually

if n

ece

ssary

3. C

heck s

peed

4. C

ontinue g

lidin

g

5. C

all

tow

er

WA

RN

ING

: K

no

t sp

ee

d a

re a

n e

stim

ate

con

ve

rsio

n o

f 1

nm

/hr

= 1

.15 m

ph

60

3090

0

330

300

270240210

180

150

120

C-1

72

left

dow

n w

ind R

/W 2

4 S

HO

RT

AP

PR

OA

CH

2406

150

240

330

060

Lin

e u

p:

DG

I A

H &

Altim

ete

r

pow

er

full

Rig

ht ru

dder

1. C

ente

r lin

e, apply

bra

ke

2.

to c

om

pass,

set

3. C

all

To

wer

4. B

rake

re

lease,

foot

dow

n t

o r

udder

5. O

pen

6.

to k

eep c

ente

r lin

e

Positiv

e c

limb 2

00 f

t:

up

off

85 m

ph/7

5 k

1.

Gears

2.

Landin

g lig

ht

3.

Speed

t cont.

to c

limb

4.

Main

tain

headin

g

5.

Win

g level, b

all

cente

r

Rolli

ng:

1.

Keep c

ente

r lin

e b

y r

ight

rudder

2.

Speed 6

0 m

ph/5

0 k

t U

nstick

Safe

altitude 4

00 f

t: 85 m

ph/7

5 k

t

1.

Fla

ps u

p

2.

Pow

er

set

3.

Speed c

limbin

g

4.

Win

g level, b

all

cente

r

5. T

/O p

ath

check

Turn

ing c

ross w

ind b

y c

heck p

oin

t

(fre

e w

ay/5

00 f

t):

1.

Cle

aring t

urn

2. T

urn

(ra

te o

ne t

urn

)

3.

Continue c

limb

Cro

ss w

ind leg:

Continue t

urn

700 ft

1. A

fter

T/O

check

2.

3.

Continue c

limb t

o

Ente

ring D

ow

n w

ind (

red s

oil)

:

Altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

headin

g r

ecip

roca

l R

/W in

use

1. T

urn

to d

ow

n w

ind (

rate

one t

urn

)

2.

3.

Spacin

g 1

win

g &

4.

Speed m

ax w

hite a

rc

Dow

n w

ind (

pre

-landin

g c

x):

altitude 7

00 f

t A

GL/8

00 f

t A

MS

L

speed (

~90-1

00 m

ph)

DG

I to

com

pass

Cockpit c

heck

1.

Check

2.

Check

3.

Check d

ista

nce t

o R

/W (

1 w

ing)

4.

Check w

ind s

ock

5.

Check

6.

Check A

/C f

ly p

ara

llel R

/W

7.

8.

Call

tow

er

Co

ckp

it c

heck:

on

both

off

full

rich

both

or

on

secure

d

locked

Maste

r sw

itch

Ignitio

n

Carb

ure

tor

heat

Mix

ture

Fuel valv

e

Seat

belt

Doors

& w

indow

s

DO

WN

WIN

D (

betw

een 2

lakes)

Abeam

(p

ara

llel th

resh

old

):

Clo

se

thro

ttle

85 m

ph/7

5 k

t

Gears

dow

n

1.

2. F

ly the A

/C

3. S

pee

d

, set nose

to g

lide a

ttitude

4. D

esce

nd turn

5.

sm

ooth

ly

Fin

al:

on s

lope

1. A

/C

()

2. C

heck s

peed

3. C

all

tow

er

1st to

4.

(as r

equire

d)

4.

oncente

r lin

e

75 m

ph/6

0 k

t

get cle

ara

nce

Fla

ps 3

0

Landin

g lig

ht

At sh

ort

:

1. C

all

tow

er

2. Landin

g lig

ht on

200924

60

3090

0

330

300

270240210

180

150

120

C-1

72

left

dow

n w

ind R

/W 2

4 N

OR

MA

L C

IRC

UIT

NO

TE

: 1. T

his

page p

ort

rays c

ircuit p

attern

for

the u

se

of

R

ight dow

nw

ind R

/W 0

6

2. T

he p

rocedure

s in this

circuit p

attern

are

the s

am

e

fo

r each p

ositio

n a

s the p

revio

us p

ages, e

xcept fo

r

th

e c

heck p

oin

ts

2406

150

240

330

060

Rolli

ng

Sa

fe a

ltitude 4

00 ft

Turn

ing c

ross w

ind

Cro

ss w

ind

leg

Ente

ring D

ow

n w

ind

Dow

n w

ind (

pre

-la

ndin

g c

x)

Abeam

(para

llel th

reshold

)

Turn

ing b

ase leg

Base leg

Fin

al

Thre

shold

Lin

e U

pA

t S

hort

Po

sitiv

e c

limb (

200 f

t)

This

red d

ashed p

att

ern

of

left

dow

n w

ind

R/W

06

or

rig

ht

do

wn

win

d R

/W 2

4,

are

no

t u

su

ally

use

d

due t

o n

ois

e a

bate

ment/

restr

icte

d m

ilita

ry a

nd

civ

ilia

n a

rea

. H

ow

eve

r d

ue

to

ce

rta

in c

ircu

msta

nce

s

AT

C m

ay g

ive c

leara

nce t

o u

se t

hese

circu

it p

att

ern

s.

the

pro

ce

du

re a

re t

he

sa

me

as p

revio

us p

ag

es.

Make 3

60:

Som

etim

es A

TC

will

giv

e

instr

uction t

o m

ake 3

60

maneuver

due t

o t

raffic

.

Th

ere

is

and

norm

al 360

sm

all

360/o

rbit

AB

C

Page 1Page 2Page 3Page 4Page 5Page 6Page 7Page 8Page 9Page 10Page 11Page 12

cessna check list

Documents

trim check

master switch

closed throttle

parking breaka

parking brake15

parking brake11

flight engine inst

final check