CESSNA 172S NAV III Skyhawk SP. Information Manual (2016)

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 7

MODEL 172S NAV III

GENERAL (CONTINUED)

ANT/ADF MODE ANNUNCIATOR - Antenna (ANT) is selected

when the ADF button is in the OUT position. This mode improves

the audio reception and is usually used for station identification.

The bearing pointer is deactivated and will park in the 90° relative

position. Automatic Direction Finder (ADF) mode is selected by

pushing the ADF button. This mode activates the bearing pointer

and will point in the direction of the station relative to the aircraft

heading.

ACTIVE FREQUENCY DISPLAY - The frequency to which the

ADF is tuned is displayed here. The active ADF frequency can be

changed directly when either of the timer functions is selected.

BFO (Beat Frequency Oscillator) ANNUNCIATOR - The BFO

mode is activated and annunciated by pushing the BFO button.

When BFO mode is active, the carrier wave and its morse code

identifier can be heard.

NOTE

CW signals (Morse Code) are unmodulated and no audio

will be heard without use of BFO. This type of signal is not

used in the United States air navigation. It is used in some

foreign countries and marine beacons.

STANDBY FREQUENCY/FLIGHT TIME OR ELAPSED TIME

DISPLAY - When FRQ is shown, the STANDBY frequency is

shown in the right display. The STANDBY frequency is selected

using the frequency select knobs. The selected STANDBY

frequency is put into the active frequency window by pushing the

frequency transfer button. Either the standby frequency, the flight

timer, or the elapsed time is shown in this position. The flight

timer and elapsed timer replace the standby frequency which

goes into blind memory to be called back at any time by pushing

the FRQ button. Flight time or elapsed time are shown and

annunciated by depressing the FLT/ET button.

FLIGHT TIMER AND ELAPSED TIMER MODE ANNUNCIATION

- Either the elapsed time

(ET) or flight time

(FLT) mode is

annunciated here.

(Continued Next Page)

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CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 7

GENERAL (CONTINUED)

6. FREQUENCY SELECT KNOBS - Selects the standby frequency

when FRQ is displayed and directly selects the active frequency

whenever either of the time functions is selected. The frequency

selector knobs may be turned either clockwise or

counterclockwise. The small knob is pulled out to tune the 1's.

The small knob is pushed in to tune the 10's. The outer knob

tunes the 100's with rollover into the 1000's up to 1799. These

knobs are also used to set the desired time when the elapsed

timer is used in the countdown mode.

7. ON/OFF/VOLUME CONTROL SWITCH

(ON/OFF/VOL)

Controls power and audio output level. Turn the control switch

clockwise from the OFF position to energize the receiver and

increase audio volume. The KR87 has audio muting which

causes the audio output to be muted unless the receiver is locked

on a valid station.

8. SET/RESET ELAPSED TIMER BUTTON (SET/RST) - The SET/

RST button resets the elapsed timer whether it is being displayed

or not.

9. FLIGHT TIMER/ELAPSED TIMER MODE SELECTOR BUTTON

(FLT/ET) -- The FLT/ET button selects either Flight Timer mode or

Elapsed Timer mode when pushed.

10.FREQUENCY TRANSFER BUTTON (FRQ) - The FRQ transfer

button interchanges the active and standby frequencies when

pushed.

11.BFO (Beat Frequency Oscillator) BUTTON - The BFO button

selects the BFO mode when pushed in. (See note under item 3).

12.ADF BUTTON - The ADF button selects either the ANT mode or

the ADF mode. The ANT mode is selected when the ADF button

is in the out position. The ADF mode is selected when the ADF

button is pushed in.

13.LUBBER LINE - Indicates magnetic heading of the airplane.

14.ROTATING COMPASS ROSE (HSI COMPASS CARD) - The

rotating compass rose turns as the heading of the airplane

changes. The magnetic heading of the airplane is under the

lubber line.

15.BEARING POINTER - Shows magnetic bearing to the station.

16.BEARING INFORMATION WINDOW - Shows the type of pointer

that is being used as the ADF bearing pointer. If ADF is not

shown, push the BRG1 or BRG2 softkey until ADF is shown.

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 7

MODEL 172S NAV III

OPERATING LIMITATIONS

Refer to Section

2 of the Pilot's Operating Handbook and FAA

Approved Flight Manual (POH/AFM).

EMERGENCY PROCEDURES

There is no change to the airplane emergency procedures when the

Bendix/King KR 87 Automatic Direction Finder (ADF) is installed.

NORMAL PROCEDURES

TO OPERATE AS AN AUTOMATIC DIRECTION FINDER:

1. OFF/VOL Control - ON

2. Frequency Selector Knobs - SELECT desired frequency in the

standby frequency display.

3. FRQ Button - PUSH to move the desired frequency from the

standby to the active position.

4. ADF Selector Switch (on audio control panel) - SELECT as

desired.

5. OFF/VOL Control - SET to desired volume level and identify that

desired station is being received.

6. PFD Softkey (on PFD)

- PUSH to show BRG1 and BRG2

softkeys.

7. BRG1 or BRG2 Softkey (on PFD) - PUSH to show ADF in

Bearing Information Window.

8. ADF Button - SELECT ADF mode and note magnetic bearing on

HSI.

(Continued Next Page)

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 7

NORMAL PROCEDURES (CONTINUED)

ADF TEST (PREFLIGHT or IN FLIGHT):

1. ADF Button - SELECT ANT mode and note pointer moves to 90°

position.

2. ADF Button - SELECT ADF mode and note the pointer moves

without hesitation to the station bearing. Excessive pointer

sluggishness, wavering or reversals indicate a signal that is too

weak or a system malfunction.

TO OPERATE BFO:

1. OFF/VOL Control - ON

2. BFO Button - PRESS ON

3. ADF Selector Buttons (on audio control panel) - SET to desired

mode.

4. VOL Control - ADJUST to desired listening level.

NOTE

A 1000-Hz tone and Morse Code identifier is heard in the

audio output when a CW signal is received.

TO OPERATE FLIGHT TIMER:

1. OFF/VOL Control - ON

2. FLT/ET Mode Button - PRESS (once or twice) until FLT is

annunciated. Timer will already be counting since it is activated

by turning the unit on.

3. OFF/VOL Control - OFF and then ON if it is desired to reset the

flight timer.

TO OPERATE AS A COMMUNICATIONS RECEIVER ONLY:

1. OFF/VOL Control - ON

2. ADF Button - SELECT ANT mode

3. Frequency Selector Knobs - SELECT desired frequency in the

standby frequency display.

4. FRQ Button - PRESS to move the desired frequency from the

standby to the active position.

5. ADF Selector Buttons (on audio control panel) - SET to desired

mode.

6. VOL Control - ADJUST to desired listening level.

(Continued Next Page)

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 7

MODEL 172S NAV III

NORMAL PROCEDURES (CONTINUED)

TO OPERATE ELAPSED TIME TIMER-COUNT UP MODE:

1. OFF/VOL Control - ON

2. FLT/ET Mode Button

- PRESS (once or twice) until ET is

annunciated.

3. SET/RST Button - PRESS momentarily to reset elapsed timer to

zero.

NOTE

The Standby Frequency which is in memory while Flight

Time or Elapsed Time modes are being displayed may be

called back by pushing the FRQ button, then transferred to

active by pushing the FRQ button again.

TO OPERATE ELAPSED TIME TIMER COUNT DOWN

MODE:

OFF/VOL Control - ON

FLT/ET Mode Button - PRESS (once or twice) until ET is

annunciated.

SET/RST Button - PRESS until the ET annunciation begins to

flash.

FREQUENCY SELECTOR KNOBS - SET desired time in the

elapsed time display. The small knob is pulled out to tune the 1's.

The small knob is pushed in to tune the 10's. The outer knob

tunes minutes up to 59 minutes.

NOTE

Selector knobs remain in the time set mode for 15 seconds

after the last entry or until the SET/RST, FLT/ET or FRQ

button is pressed.

SET/RST Button - PRESS to start countdown. When the timer

reaches 0, it will start to count up as display flashes for 15

seconds.

NOTE

While FLT or ET are displayed, the active frequency on the

left side of the window may be changed, by using the

frequency selector knobs, without any effect on the stored

standby frequency or the other modes.

(Continued Next Page)

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 7

NORMAL PROCEDURES (CONTINUED)

ADF OPERATION NOTES:

ERRONEOUS ADF BEARING DUE TO RADIO FREQUENCY

PHENOMENA:

In the U.S., the FCC, which assigns AM radio frequencies, occasionally

will assign the same frequency to more than one station in an area.

Certain conditions, such as Night Effect, may cause signals from such

stations to overlap. This should be taken into consideration when using

AM broadcast stations for navigation.

Sunspots and atmospheric phenomena may occasionally distort

reception so that signals from two stations on the same frequency will

overlap. For this reason, it is always wise to make positive identification

of the station being tuned, by switching the function selector to ANT

and listening for station call letters.

ELECTRICAL STORMS:

In the vicinity of electrical storms, an ADF indicator pointer tends to

swing from the station tuned toward the center of the storm.

NIGHT EFFECT:

This is a disturbance particularly strong just after sunset and just after

dawn. An ADF indicator pointer may swing erratically at these times. If

possible, tune to the most powerful station at the lowest frequency. If

this is not possible, take the average of pointer oscillations to determine

station bearing.

MOUNTAIN EFFECT:

Radio waves reflecting from the surface of mountains may cause the

pointer to fluctuate or show an erroneous bearing. This should be taken

into account when taking bearings over mountainous terrain.

COASTAL REFRACTION:

Radio waves may be refracted when passing from land to sea or when

moving parallel to the coastline. This also should be taken into account.

FAA APPROVED

172SPHAUS-S7-00

U.S.

S7-11

Pilot’s Operating Handbook and

FAA Approved Airplane Flight Manual

CESSNA MODEL 172S

NAV III AVIONICS OPTION

Serials 172S9810 and On

SUPPLEMENT 8

RUSSIAN FEDERATION (RF) AND OTHER

COMMONWEALTH OF INDEPENDENT

STATES (CIS) COUNTRIES

SERIAL NO.

REGISTRATION NO.

This supplement must be inserted into Section 9 of the Pilot's Operating Handbook

and FAA Approved Airplane Flight Manual when the airplane is operated within the

territory of the Russian Federation (RF) and other Commonwealth of Independent

States (CIS) Countries. This supplement is approved by the U.S. Federal Aviation

Administration (FAA) on behalf of the Russian Aviation Register.

4 APRIL 2006

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

172SPHAUS-S8-00

U.S.

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

SUPPLEMENT 8

RUSSIAN FEDERATION

(RF) AND OTHER

COMMONWEALTH OF INDEPENDENT STATES

(CIS) COUNTRIES

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status Date

Original Issue

4 April 2006

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

S8-1 thru S8-21/S8-22

Original

Approved for RF and CIS Countries Only

FAA APPROVED

S8-2

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172SPHAUS-S8-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Airplane Serial

Revision

Incorporated

Number

Title

Effectivity

Incorporated

in Airplane

Approved for RF and CIS Countries Only

FAA APPROVED

172SPHAUS-S8-00

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

RUSSIAN FEDERATION

(RF) AND OTHER

COMMONWEALTH OF INDEPENDENT STATES

(CIS) COUNTRIES

GENERAL

This supplement must be placed in Section 9 of the basic Pilot’s

Operating Handbook and FAA Approved Airplane Flight Manual, when

the airplane is operated within the territory of the Russian Federation

(RF) and other Commonwealth of Independent States (CIS) Countries.

The information contained herein supplements the information of the

basic Pilot’s Operating Handbook and FAA Approved Airplane Flight

Manual. Limitations, procedures, and performance found in this

supplement supersedes those found in the basic Pilot’s Operating

Handbook and FAA Approved Airplane Flight Manual. For limitations,

procedures, and performance information not contained in this

supplement, consult the basic Pilot’s Operating Handbook and FAA

Approved Airplane Flight Manual.

NOTE

In RF and CIS countries, FAA operating rules (i.e., 14 CFR

Part 91 and 14 CFR Part 135) are not applicable. The

airplane must be equipped and operated in accordance

with RF and CIS applicable operational requirements.

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

OPERATING LIMITATIONS

The following Limitations supersede and/or are in addition to the

Limitations set forth in the basic Pilot’s Operating Handbook and FAA

Approved Airplane Flight Manual:

Maximum number of airplane occupants: 1 Pilot plus 3 Passengers

Maximum bank angle: 60°

Operation in heavy precipitation (rain or snow) is prohibited.

Flight into known significant convective activity and thunderstorms is

prohibited.

Flight into known icing or freezing rain is prohibited.

Operations in RF and CIS airspace are approved only on routes

covered by ATC ground facilities using RBS mode.

The Nav III Avionics Option is approved for Category I ILS approach

operations only.

The Global Positioning Satellite (GPS) system is not approved for

approach.

Operation over water beyond the Maximum Glide distance from shore

is prohibited (Refer to the POH/AFM, Section 3, Figure 3-1).

Spins are prohibited at weight more than 2100 pounds.

Autopilot must be installed and operational for all operations within RF

and CIS airspace.

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

KINDS OF OPERATION LIMITS

The following Kinds of Operations Equipment List (KOEL) identifies the

equipment required to be operational for airplane airworthiness in the

listed kind of operations for airplanes operating within the territory of the

Russian Federation and other Commonwealth of Independent States

countries.

The following KOEL supersedes the KOEL located in Section 2 of the

POH/AFM.

KINDS OF OPERATIONS EQUIPMENT LIST

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

PLACARDS AND MARKINGS

172S Nav III POH/AFM

Accessible to pilot

in flight

Accessible to pilot

Garmin G1000^TM Cockpit

in flight

Reference Guide

AIR CONDITIONING

1 - Forward Avionics Fan

2 - PFD Fan

3 - MFD Fan

4 - Aft Avionics Fan

AUTOFLIGHT

1 - Bendix/King KAP 140 POH

Accessible to pilot

Supplement

in flight when using

autopilot

2 - Bendix/King KAP 140

Autopilot

(Continued Next Page)

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

COMMUNICATIONS

1 - VHF COM

ELECTRICAL POWER

1 - 24V Main Battery

2 - 28V Alternator

3 - 24V Standby Battery

* Refer to Note 1

4 - Main Ammeter

5 - Standby Ammeter

* Refer to Note 1

EQUIPMENT AND

FURNISHINGS

1 - Seat Belt Assembly

Each Seat

Occupant

2 - Shoulder Harness

Front Seat

Occupants

NOTE

1. The European Aviation Safety

Agency (EASA) requires the

24V Standby Battery and Standby Ammeter to successfully

complete the pre-flight check before operating the airplane in

VFR night, IFR day, or IFR night conditions in Europe. Correct

operation of the 24V Standby Battery and Standby Ammeter is

recommended for all other operations.

(Continued Next Page)

Approved for RF and CIS Countries Only

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

FLIGHT CONTROLS

1 - Flap Position Indicator

2 - Flap Motor

3 - Elevator Trim System

4 - Elevator Trim Indicator

FUEL SYSTEM

1 - Electric Fuel Pump

2 - Fuel Quantity Indicator - LH

Tank

3 - Fuel Quantity Indicator - RH

Tank

ICE AND RAIN PROTECTION

1 - Alternate Static Air Source

2 - Alternate Induction Air

System

INDICATING/RECORDING

SYSTEM

1 - Stall Warning System

2 - System Annunciator and

Warning Displays

LANDING GEAR

1 - Wheel Fairings

Removable

(Continued Next Page)

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

LIGHTING

1 - PFD Bezel Lighting

2 - PFD Backlighting

*Refer to Note 2

3 - MFD Bezel Lighting

4 - MFD Backlighting

*Refer to Note 3

5 - Switch and Circuit Breaker

Panel Lighting

6 - Airspeed Indicator (Standby)

Internal Lighting

7 - Altimeter (Standby) Internal

Lighting

8 - Non-stabilized Magnetic

Compass Internal Lighting

9 - Attitude Indicator (Vacuum)

Internal Lighting

10 - Cockpit Flood Light

11 - Aircraft Position (NAV) Lights

NOTE

2. PDF backlighting is

required

for

day VFR flight if MFD

backlighting has failed. Display backup mode must be active

so engine indicators are shown.

3. MFD backlighting is required for day VFR flight if PDF

backlighting has failed. Display backup mode must be active

so flight instruments are shown.

(Continued Next Page)

Approved for RF and CIS Countries Only

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

LIGHTING (Continued)

12 - STROBE Light System

13 - BEACON Light

14 - TAXI Light

15 - LAND (Landing) Light

Operations for hire

only

NAVIGATION AND PITOT-

STATIC SYSTEM

1 - G1000 Airspeed Indicator

2 - Standby Airspeed Indicator

3 - G1000 Altimeter

4 - Standby Altimeter

5 - G1000 Vertical Speed

Indicator

6 - G1000 Attitude Indicator

7 - Attitude Indicator - Vacuum

(Standby)

8 - G1000 Directional Indicator

(HSI)

9 - G1000 Turn Coordinator

10 - Non-stabilized Magnetic

Compass

11 - VHF Navigation Radio

A/R

As Required Per

(VOR/LOC/GS)

Procedure

(Continued Next Page)

Approved for RF and CIS Countries Only

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

NAVIGATION AND PITOT-

STATIC SYSTEM (Continued)

12 - GPS Receiver/Navigator

A/R

As Required Per

Procedure

13 - ADF Navigation Radio

A/R

As Required Per

Procedure

14 - Marker Beacon Receiver

A/R

As Required Per

Procedure

15 - Blind Altitude Encoder

A/R

As Required Per

Procedure

16 - Clock

VACUUM

1 - Engine-driven Vacuum Pump

2 - Vacuum Indicator

ENGINE FUEL AND CONTROL

1 - Fuel Flow Indicator

ENGINE INDICATING

1 - Tachometer (RPM)

2 - Cylinder Head Temperature

(CHT) Indicator

3 - Oil Pressure Indicator

4 - Oil Temperature Indicator

ENGINE OIL

1 - Engine Crankcase Dipstick

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

FUEL LIMIATIONS

Approved Fuels:100LL (ASTM-D910)

100 (Formerly 100/130) (ASTM-D910)

B91/115 (GOST 1012-72)

See the latest revision of Lycoming Service Instruction No.1070 for

approved fuel grades.

Fuels must contain an anti-icing fuel additive (Isopropyl Alcohol or

DiEGME) in concentrations mixed as noted in Section 8 of the POH/

AFM.

MAXIMUM OPERATING ALTITUDE LIMIT

MAXIMUM APPROVED OPERATING ALTITUDE: 3000 meters (9800

Feet).

If oxygen is provided for each occupant, the airplane can be operated

up to the maximum altitude for the oxygen system, or 4200 meters

(13,779 feet), whichever altitude is lower.

OUTSIDE AIR TEMPERATURE LIMITS

Ground operations limits for a cold day:

Minus 40°C

Ground operations limits for a hot day:

40°C

Approved for RF and CIS Countries Only

FAA APPROVED

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MODEL 172S NAV III

SUPPLEMENT 8

TAXI OPERATIONAL LIMITS

Uncontaminated paved taxiway:

• Maximum wind velocity while taxiing:

14 m/s (27 Knots)

Paved taxiway contaminated with precipitation:

• Maximum wind velocity while taxiing:

3 m/s (5 Knots)

Refer to Section 4 of the POH/AFM for additional information on taxiing.

TAKEOFF AND LANDING OPERATIONAL LIMITS

Maximum Takeoff and Landing Altitude:

2438 meters (8000 Feet)

Maximum Headwind Velocity:

14 m/s (27 Knots)

Maximum Tailwind Velocity:

5 m/s (10 Knots)

Maximum crosswind velocity on

uncontaminated paved runway:

7m/s (15 Knots)

ALLOWABLE RUNWAY SURFACE CONDITIONS

1. Uncontaminated runway with paved surface.

2. Paved runway contaminated with precipitation (average depth

and types):

a. Water, less that 10.0 mm.

b. Slush, less than 10.0 mm.

c. Loose snow less than 30.0 mm.

3. Unpaved runway

a. Surface hardness must be greater than 7 kg/cm².

NOTE

Landing on contaminated unpaved runways is prohibited.

Operating with the landing gear fairings removed is recommended on

wet or unpaved runways when temperatures are near or below

freezing.

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

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SUPPLEMENT 8

MODEL 172S NAV III

MAXIMUM CROSSWIND ON CONTAMINATED RUNWAYS

Contaminated paved runways with:

Water, less than 10.0 mm

3 m/s (5 Knots)

Slush, less than 10.0 mm

3 m/s (5 Knots)

Loose snow, less than 30.0 mm

3 m/s (5 Knots)

Paved runway with less than 3 mm of water, snow or slush and braking

coefficient of friction(µ) of:

µ=0.3 (poor braking)

3 m/s (5 Knots)

µ=0.4 (average braking)

5 m/s (9 Knots)

µ=0.5 (good braking, dry or

equivalent to dry runway)

7 m/s (15 Knots)

REQUIRED PLACARDS AND MARKINGS

Above exit doors, in clear view of each occupant:

EMERGENCY PROCEDURES

The following pages from Section 3 of the POH/AFM have instructions

for operations in RF and CIS countries. These pages replace the

procedures found in Section 3 of the POH/AFM for those operations:

(Continued Next Page)

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

EMERGENCY PROCEDURES (Continued)

FORCED LANDINGS

EMERGENCY LANDING WITHOUT ENGINE POWER

1. Passenger Seats - MOST UPRIGHT POSITION

2. Seats and Seat Belts - SECURE

3. Airspeed - 70 KIAS Flaps UP

65 KIAS Flaps 10° - FULL

4. Mixture Control - IDLE CUT OFF

5. FUEL SHUTOFF Valve - OFF (pull full out)

6. MAGNETOS Switch - OFF

7. Wing Flaps - AS REQUIRED (FULL recommended)

8. STBY BATT Switch - OFF

9. MASTER Switch (ALT and BAT) - OFF (when landing is assured)

10.Doors - UNLATCH PRIOR TO TOUCHDOWN

11.Touchdown - SLIGHTLY TAIL LOW

12.Brakes - APPLY HEAVILY

13.Emergency Radio

- Operate

(P-855A1) Russian made

Emergency Radio according to attached instructions.

PRECAUTIONARY LANDING WITH ENGINE POWER

1. Passenger Seats - MOST UPRIGHT POSITION

2. Seats and Seat Belts - SECURE

3. Airspeed - 65 KIAS

4. Wing Flaps - 20°

5. Selected Field - FLY OVER, noting terrain and obstructions.

6. Wing Flaps - FULL (on final approach)

7. Airspeed - 65 KIAS

8. STBY BATT Switch - OFF

9. MASTER Switch (ALT and BAT) - OFF

10.Doors - UNLATCH PRIOR TO TOUCHDOWN

11.Touchdown - SLIGHTLY TAIL LOW

12.Mixture Control - IDLE CUT OFF

13.MAGNETOS Switch - OFF

14.Brakes - APPLY HEAVILY

15.Emergency Radio

- Operate

(P-855A1) Russian made

Emergency Radio according to attached instructions.

(Continued Next Page)

Approved for RF and CIS Countries Only

FAA APPROVED

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SECTION 9 - SUPPLEMENTS

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SUPPLEMENT 8

MODEL 172S NAV III

EMERGENCY PROCEDURES (Continued)

DITCHING

1. Radio - TRANSMIT MAYDAY on 121.5 MHz, giving location and

intentions and SQUAWK 7700.

2. Heavy Objects (in baggage area) - SECURE OR JETTISON (if

possible)

3. Passenger Seats - MOST UPRIGHT POSITION

4. Seats and Seat Belts - SECURE

5. Wing Flaps - 20° to FULL

6. Power - ESTABLISH 300 FT/MIN DESCENT AT 55 KIAS

NOTE

If no power is available, approach at 65 KIAS with Flaps UP

or 60 KIAS with Flaps 10°.

7. Approach - High Winds, Heavy Seas - INTO THE WIND

Light Winds, Heavy Swells - PARALLEL TO SWELLS

8. Cabin Doors - UNLATCH

9. Touchdown - LEVEL ATTITUDE AT ESTABLISHED RATE-OF-

DESCENT.

10.Face - CUSHION at touchdown with folded coat.

11.ELT - ACTIVATE

12.Airplane - EVACUATE through cabin doors. If necessary, open

window and flood cabin to equalize pressure so doors can be

opened.

13.Life Vests and Raft - INFLATE WHEN CLEAR OF AIRPLANE.

14.Emergency Radio

- Operate

(P-855A1) Russian made

Emergency Radio according to attached instructions.

(Continued Next Page)

Approved for RF and CIS Countries Only

FAA APPROVED

S8-16

U.S.

172SPHAUS-S8-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

EMERGENCY PROCEDURES (Continued)

FORCED LANDINGS

If all attempts to restart the engine fail and a forced landing is imminent,

select a suitable field and prepare for the landing as discussed under

the Emergency Landing Without Engine Power checklist. Transmit

Mayday message on 121.5 MHz giving location and intentions and

squawk 7700.

Before attempting an "off-airport" landing with engine power available,

one should fly over the landing area at a safe, but low altitude, to

inspect the terrain for obstructions and surface conditions, proceeding

as discussed in the Precautionary Landing With Engine Power

checklist.

Prepare for ditching by securing or jettisoning heavy objects located in

the baggage area and collect folded coats for protection of occupants'

face at touchdown. Transmit Mayday messages on 121.5 MHz giving

location and intentions and squawk

7700. Avoid a landing flare

because of the difficulty in judging height over a water surface. The

checklist assumes the availability of power to make a precautionary

water landing. If power is not available, use of the airspeeds noted with

minimum flap extension will provide a more favorable attitude for a

power off ditching.

In a forced landing situation, do not turn off the AVIONICS switch or

MASTER switch until a landing is assured. Premature deactivation of

the switches will disable all airplane electrical systems.

Following evacuation from the airplane, operate (P-885A1) Russian

made Emergency Radio according to the attached instructions

provided with the radio.

Approved for RF and CIS Countries Only

FAA APPROVED

172SPHAUS-S8-00

U.S.

S8-17

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

NORMAL PROCEDURES

NOTE

• In a left slip maneuver, the airspeed indicator may show

a maximum of 20 knots below the actual airspeed. In a

right slip maneuver, the airspeed indicator may show a

maximum of 5 knots above the actual airspeed. This is

because of the single static pressure port on the 172S

left forward fuselage.

• At airspeeds greater than 120 KIAS, close the throttle if

necessary to keep engine speed below 2700 RPM.

In the event of GPS failure when operating along routes that are + 5 km

wide without VOR/DME facilities and no NDB coverage, airplane

position between the width of such routes can only be assured up to

approximately 140 km from the last known position.

The pilot is to disregard Supplement 1 of the POH/AFM describing the

pointer Model 3000-11 or 4000-11 Emergency Locator Transmitter

(ELT).

COLD WEATHER OPERATIONS

NOTE

• The Garmin GDU 1040 PFD/MFD requires a warm-up

time of up to 30 minutes when exposed to Minus 40°C

for an extended period. A warm-up time of up to 15

minutes may be required when exposed to Minus 30°C

for an extended period of time.

• During operation at outside temperatures below ISA

Standard, the engine may develop greater than rated

power at normal rated RPM, particularly at lower

altitudes.

Approved for RF and CIS Countries Only

FAA APPROVED

S8-18

U.S.

172SPHAUS-S8-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 8

COLD SOAK

If extended exposure to cold weather is expected, refer to Maintenance

Manual procedures to prepare the airplane for cold soak. If the airplane

has cold soaked for more than two hours at temperatures colder than

Minus 10°C, refer to Maintenance Manual procedures to prepare the

airplane for flight. Cold temperatures will affect control cable tension.

See Chapter 27 of the Maintenance Manual for flight control cable

tensions. See Chapter 12 of the Maintenance Manual for information

on lubrication and greasing of moving parts. See Section 8 of the POH/

AFM for correct engine oil viscosity. See paragraphs on Cold Weather

Operation in Section 4 of the POH/AFM for additional information on

procedures for operating the airplane in cold temperatures.

When the outside temperature is less than Minus 34ºC, the airplane

batteries should be removed and stored in the warm conditions.

The engine must be preheated before starting if engine temperature is

less than Minus 6°C.

When the outside temperature is less than

0°C, moisture from

combustion can freeze on the engine spark plugs if the engine does not

continue to operate after it is started. This will prevent the engine from

starting again. Preheat the engine to more than 0°C before starting the

engine again.

Preheat the engine by directing warm air into the engine cooling inlets

behind the propeller. The temperature of the preheating air should not

be more than 120°C to prevent damage to the exterior paint. Open

flames are prohibited near the airplane.

Before takeoff, preheat the airplane cabin to more than Minus 30°C for

correct operation of the standby altimeter. If there is no warning that an

instrument is operating incorrectly, all other instruments will operate

down to the minimum temperature of the airplane.

Before operating the airplane, it is recommended to heat the cabin to a

comfortable temperature for the cabin occupants.

Approved for RF and CIS Countries Only

FAA APPROVED

172SPHAUS-S8-00

U.S.

S8-19

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 8

MODEL 172S NAV III

PERFORMANCE

OPERATION ON CONTAMINATED RUNWAY

The takeoff distance on a paved runway with no more than 3 mm of

precipitation is equal to dry runway takeoff distance.

The takeoff distance on a paved runway with precipitation greater than

3 mm is 20% greater than the dry runway takeoff distance.

To determine the required landing distance on a contaminated paved

runway, the dry runway landing distance shall be multiplied by the

following K factors:

Conditions

Basic Airfield

Alternate Airfield

µ > 0.5

K = 1.67

K = 1.43

(good braking and runway with no

standing water)

0.5 > µ > 0.4

K = 1.72

(Average Braking)

More than 3 mm precipitation

K = 2.00

0.4 > µ > 0.3

(Poor Braking)

For unpaved runway landing distance, refer to figure 5-12 in the POH/

AFM for the correction applied to grass runway landing distance.

Approved for RF and CIS Countries Only

FAA APPROVED

S8-20

U.S.

172SPHAUS-S8-00

CESSNA MODEL 172S

NAV III AVIONICS OPTION

Serials 172S9810 and On

SUPPLEMENT 9

ARTEX ME406

EMERGENCY LOCATOR TRANSMITTER (ELT)

SERIAL NO.

REGISTRATION NO.

This supplement must be inserted into Section 9 of the Pilot's Operating Handbook

and FAA Approved Airplane Flight Manual when the Artex ME406 Emergency

Locator Transmitter (ELT) is installed.

30 OCTOBER 2006

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

172SPHAUS-S9-00

U.S.

S9-1

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 9

MODEL 172S NAV III

SUPPLEMENT 9

ARTEX ME406 EMERGENCY LOCATOR TRANSMITTER

(ELT)

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status

Date

Original Issue

30 October 2006

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

S9-1 thru S9-8

Original

FAA APPROVED

S9-2

U.S.

172SPHAUS-S9-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 9

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Airplane Serial

Revision

Incorporated

Number Title

Effectivity

Incorporated

in Airplane

FAA APPROVED

172SPHAUS-S9-00

U.S.

S9-3

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 9

MODEL 172S NAV III

ARTEX ME406 EMERGENCY LOCATOR

TRANSMITTER (ELT)

GENERAL

The Artex ME406 Emergency Locator Transmitter (ELT) installation

uses a solid-state

2-frequency transmitter powered by an internal

lithium battery. The ME406 is also equipped with an instrument panel-

mounted remote switch assembly, that includes a red warning light, and

an external antenna mounted on the top of the tailcone. The remote

switch assembly is installed along the upper right instrument panel and

controls ELT operating modes from the flight crew station. When the

remote switch is set to the ARM position, the transmitter is energized

only when the internal "G” switch senses longitudinal inertia forces per

TSO-C91a/TSO-C126. When the remote switch is set to the ON

position, the transmitter is immediately energized.

The ME406 transmitter unit is located in the tailcone along the right

side behind the baggage compartment aft panel. On the ELT

transmitter unit is a panel containing an ARM/ON switch and a

transmitter warning light.

The ELT installation uses two different warnings to tell the pilot when

the ELT is energized. The aural warning is an unusual sound that is

easily heard by the pilot. The visual warning is a flashing red light

directly above the remote switch that shows the pilot that the ELT has

been activated.

When the ME406 is energized, the ELT transmits the standard swept

tone signal on the international VHF frequency of 121.5 MHz until

battery power is gone. The 121.5 MHz signal is mainly used to pinpoint

the beacon during search and rescue operations, and is monitored by

general aviation, commercial aircraft, and government agencies.

In addition, for the first 24 hours of the ELT being energized, a 406.028

MHz signal is transmitted at 50 second intervals. This transmission

lasts 440 milliseconds and contains identification data programmed into

the ELT and is received by COSPAS/SARSAT satellites. The

transmitted data may include the Aircraft ID, ELT Serial Number,

Country Code, and COSPAS/SARSAT ID.

(Continued Next Page)

FAA APPROVED

S9-4

U.S.

172SPHAUS-S9-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 9

ARTEX ME406 ELT CONTROL PANEL

ELT PANEL SWITCH (2-Position Toggle Switch):

a. ARM

(OFF)

- Turns OFF and ARMS transmitter for

automatic activation if “G” switch senses a predetermined

deceleration level.

b. ON

- Activates transmitter instantly. The ON position

bypasses the automatic activation switch. The RED

warning light on ELT panel and on the remote switch

assembly mounted on the instrument panel should come

on.

TRANSMITTER WARNING LIGHT - Light comes on RED to

indicate the transmitter is transmitting a distress signal.

ANTENNA RECEPTACLE - Connects to the antenna mounted

on top of tailcone.

REMOTE CABLE JACK - Connects to the ELT remote switch

assembly located on the upper right instrument panel.

REMOTE SWITCH ASSEMBLY - (2-Position Rocker Switch):

a. ARM

(OFF)

- Turns OFF and ARMS transmitter for

automatic activation if “G” switch senses a predetermined

deceleration level.

b. ON

- Remotely activates the transmitter for test or

emergency situations. The RED warning light above the

rocker switch comes on to indicate that the transmitter is

transmitting a distress signal.

Figure S9-1

FAA APPROVED

172SPHAUS-S9-00

U.S.

S9-5

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 9

MODEL 172S NAV III

OPERATING LIMITATIONS

There are no additional airplane operating limitations when the Artex

ME406 ELT is installed.

The airplane owner or operator must register the ME406 ELT with the

applicable civil aviation authority before use to make sure that the

identification code transmitted by the ELT is in the COSPAS/SARSAT

database. Refer to www.cospas-sarsat.org for registration information.

Refer to 14 CFR 91.207 for ELT inspection requirements. The ME406

must be inspected and tested by an approved technician using the

correct test equipment under the appropriate civil aviation authorities

approved conditions.

FAA APPROVED

S9-6

U.S.

172SPHAUS-S9-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 9

EMERGENCY PROCEDURES

If a forced landing is necessary, set the remote switch to the ON

position before landing. This is very important in remote or

mountainous terrain. The red warning light above the remote switch will

flash and the aural warning will be heard.

After a landing when search and rescue aid is needed, use the ELT as

follows:

NOTE

The ELT remote switch assembly could be inoperative if

damaged during a forced landing. If inoperative, the inertia

“G” switch will activate automatically. However, to turn the

ELT OFF and ON again requires manual switching of the

ELT panel switch which is located on the ELT unit.

MAKE SURE THE ELT IS ENERGIZED:

a. If the red warning light above the remote switch is not

flashing, set the remote switch to the ON position.

b. Listen for the aural warning. If the COM radio(s) operate and

can be energized safely (no threat of fire or explosion),

energize a COM radio and set the frequency to 121.5 MHz.

The ELT tone should be heard on the COM radio if the ELT

is working correctly. When done, de-energize the COM

radio(s) to conserve the airplane battery power.

c. Make sure that nothing is touching or blocking the ELT

antenna.

AFTER RESCUE - Set the remote switch to the ARM position to

de-energize the ELT. If the remote switch does not function, set

the switch on the ME406 (in the tailcone) to the ARM position.

FAA APPROVED

172SPHAUS-S9-00

U.S.

S9-7

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 9

MODEL 172S NAV III

NORMAL PROCEDURES

When operating in a remote area or over hazardous terrain, it is

recommended that the ELT be inspected by an approved technician

more frequently than required by 14 CFR 91.207.

NORMAL OPERATION

1. Check that the remote switch (on the upper right instrument

panel) is set to the ARM position.

Normal operation of the ME406 from the flight crew station is only to

de-energize and arm the ELT after it has been accidentally energized

(no emergency).

The ELT can be energized by a lightning strike or hard landing. If the

red light above the remote switch is flashing and the aural warning is

heard, the ELT is energized. Check for the emergency signal on a COM

radio set to 121.5 MHz. To stop the transmissions, set the remote

switch to the ON position momentarily and then set to the ARM

position. Tell the nearest Air Traffic Control facility about the accidental

transmissions as soon as possible to hold search and rescue work to a

minimum.

PERFORMANCE

There is no change to the airplane performance when the Artex ME406

ELT is installed.

FAA APPROVED

S9-8

U.S.

172SPHAUS-S9-00

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 10

MODEL 172S NAV III

SUPPLEMENT 10

JAR-OPS OPERATIONAL ELIGIBILITY

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status

Date

Original Issue

16 November 2006

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

S10-1 thru S10-5/S10-6

Original

FAA APPROVED

S10-2

U.S.

172SPHAUS-S10-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 10

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Number

Title

Airplane Serial

Revision

Incorporated

Effectivity

Incorporated

in Airplane

FAA APPROVED

172SPHAUS-S10-00

U.S.

S10-3

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 10

MODEL 172S NAV III

JAR-OPS OPERATIONAL ELIGIBILITY

GENERAL

OPERATIONAL ELIGIBILITY

The JAA TGLs noted below specify that Operational Eligibility

information be included in the airplane POH/AFM or POH/AFM

Supplement for convenience in the JAR-OPS approval process. This

Supplement provides a consistent location for the requested

information. This information does not address the operation of the

airplane or equipment by the pilot.

NAVIGATION OPERATIONAL ELIGIBILITY

The GPS/GNSS receivers in the G1000 System are certified to TSO

C129a Class A1 and ETSO C129a Class A1 or TSO C145a and ETSO

2C145a.

The installed performance of the G1000 System has been tested and

approved for IFR enroute, terminal and non-precision (RNAV or GPS)

approach operations per AC 20-138A when using GPS/GNSS with the

correct navigation database.

The G1000 System meets the requirements for GPS/GNSS as a

Primary Means of Navigation for Oceanic/Remote Operations (RNP-

10) per AC 20-138A, FAA Notice N8110.60, FAA Order 8400-12A and

FAA Order 8700-1. Both GPS/GNSS receivers are required to be

operating and receiving usable signals except for routes requiring only

one Long Range Navigation sensor.

The G1000 System has been shown to be eligible for BRNAV (RNP-5)

and PRNAV (RNP-1) Enroute and Terminal navigation per JAA TGL-2

(ACJ20X4), JAA TGL-10 and AC 90-96A provided that the G1000 is

receiving usable navigation information from at least one GPS receiver.

Eligibility does not constitute Operational Approval.

(Continued Next Page)

FAA APPROVED

S10-4

U.S.

172SPHAUS-S10-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 10

GENERAL (Continued)

SSR MODE S ENHANCED SURVEILLANCE

OPERATIONAL ELIGIBILITY

The GTX 33 Transponder is certified to TSO C112a and ETSO 2C112a.

The installed performance of the GTX

33 has been tested and

approved per AC 20-131A, Draft AC-131B and AC 23-8B.

The GTX 33 is able to respond to interrogations in Modes A, C and is

fully compliant with the requirements of Mode S Elementary

Surveillance per TGL 13 Rev 1 and Draft TGL 13 Rev 2. Extended

Squitter functionality is supported by the GTX

33. This does not

constitute airworthiness or operational approval for Extended Squitter

functionality.

OPERATING LIMITATIONS

There is no change to the airplane operating limitations for JAR-OPS

Operational Eligibility. JAR-OPS may require separate airspace

operating limitations.

EMERGENCY PROCEDURES

There is no change to the airplane emergency procedures for JAR-

OPS Operational Eligibility.

NORMAL PROCEDURES

There is no change to the airplane normal procedures for JAR-OPS

Operational Eligibility.

PERFORMANCE

There is no change to the airplane performance for JAR-OPS

Operational Eligibility.

FAA APPROVED

172SPHAUS-S10-00

U.S.

S10-5/S10-6

CESSNA MODEL 172S

NAV III AVIONICS OPTION - KAP 140 AUTOPILOT

Serials

172S9810 thru 172S10467 and 172S10469 thru 172S10506

and

172S10508 thru 172S10639 and 172S10641 thru 172S10655

SUPPLEMENT 12

GARMIN G1000 SYNTHETIC VISION TECHNOLOGY

SERIAL NO.

REGISTRATION NO.

This supplement must be inserted into Section 9 of the Pilot's Operating Handbook

and FAA Approved Airplane Flight Manual when the Garmin G1000 Synthetic

Vision Technology is installed.

9 MARCH 2009

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

REVISION 1 - 2 FEBRUARY 2010

172SPHAUS-S12-01

U.S.

S12-1

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 12

MODEL 172S NAV III

KAP 140 AUTOPILOT

SUPPLEMENT 12

GARMIN G1000 SYNTHETIC VISION TECHNOLOGY

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status

Date

Original Issue

9 March 2009

Revision 1

2 February 2010

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

* S12-1 thru S12-2

Revised

S12-3

Original

* S12-4 thru S12-5/S12-6

Revised

FAA APPROVED

S12-2

U.S.

172SPHAUS-S12-01

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 12

KAP 140 AUTOPILOT

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Number

Title

Airplane Serial

Revision

Incorporated

Effectivity

Incorporated

in Airplane

FAA APPROVED

172SPHAUS-S12-00

U.S.

S12-3

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 12

MODEL 172S NAV III

KAP 140 AUTOPILOT

GARMIN G1000 SYNTHETIC VISION TECHNOLOGY

GENERAL

The Garmin G1000 Synthetic Vision Technology (SVT) is primarily

composed of a computer-generated, forward looking attitude aligned

view of the topography immediately in front of the airplane from the

pilot’s perspective. The SVT information is shown on the Primary Flight

Display

(PFD) and offers a three dimensional view of potentially

hazardous terrain, obstacles and traffic complete with the requisite red

or yellow shading overlaid. For complete system description and

operation, refer to the Garmin G1000 Cockpit Reference Guide (CRG).

NOTE

• Not all airport runways are depicted with SVT.

• All G1000 SVT Pathways are disabled prior to system

software build 0563.17. Software Build 0563.17 supports

WAAS G1000 installations only.

OPERATING LIMITATIONS

The G1000 limitations listed in Section 2, of the POH apply when using

SVT. In addition to, SVT is not available in locations north of 75° North

latitude or south of 60° South latitude due to the absence of terrain data

in these geographical areas.

Airplane maneuvering in any flight phase shall not be based solely on

information from the G1000 SVT. SVT shall not be used as the primary

means of terrain, obstacle or traffic avoidance.

The G1000 SVT shall not be used for primary flight guidance.

Descent below published IFR minimums shall not be predicated upon

the use of G1000 SVT.

The G1000 SVT Pathways are not a substitute for standard course and

altitude deviation information provided by the primary lateral and

vertical guidance.

The current Garmin G1000 Cockpit Reference Guide Part number for

SVT that must be available to the pilot during flight is displayed on the

MFD AUX group, SYSTEM STATUS page.

FAA APPROVED

S12-4

U.S.

172SPHAUS-S12-01

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 12

KAP 140 AUTOPILOT

EMERGENCY PROCEDURES

AMPLIFIED EMERGENCY PROCEDURES

G1000 SVT PATHWAYS MALFUNCTION OR ERRONEOUS

LATERAL AND/OR VERTICAL GUIDANCE

If G1000 SVT Pathways malfunctions or provides an erroneous

indication contrary to the primary lateral and vertical guidance, use the

following procedure to turn off SVT Pathways:

1. PFD Softkey - PRESS (located on PFD bezel)

2. SYN VIS Softkey - PRESS (located on PFD bezel)

3. PATHWAY Softkey - PRESS (located on PFD bezel)

(verify SVT Pathway guidance is removed from the PFD display)

NORMAL PROCEDURES

There is no change to the airplane normal procedures when the Garmin

G1000 Synthetic Vision Technology is installed.

PERFORMANCE

There is no change to the airplane performance when the Garmin

G1000 Synthetic Vision Technology is installed.

FAA APPROVED

172SPHAUS-S12-01

U.S.

S12-5/S12-6

CESSNA MODEL 172S

NAV III AVIONICS OPTION

Serials

172S9810 and On

SUPPLEMENT 13

ARGENTINE CERTIFIED AIRPLANES

SERIAL NO.

REGISTRATION NO.

This supplement must be inserted into Section 9 of the Pilot's Operating Handbook

and FAA Approved Airplane Flight Manual when used for Argentine Certified

Airplanes. This Airplane Flight Manual Supplement is approved in accordance with

Section 21.29 of DNAR 21 for Argentine registered airplanes and is approved by

the US Federal Aviation Administration (FAA) on behalf of the Dirección Nacional

de Aeronavegabilidad (D.N.A.).

8 SEPTEMBER 2008

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

172SPHAUS-S13-00

U.S.

S13-1

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 13

MODEL 172S NAV III

SUPPLEMENT 13

ARGENTINE CERTIFIED AIRPLANES

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status

Date

Original Issue

8 September 2008

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

S13-1 thru S13-13/S13-14

Original

FAA APPROVED

S13-2

U.S.

172SPHAUS-S13-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 13

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Airplane Serial

Revision

Incorporated

Number Title

Effectivity

Incorporated

in Airplane

FAA APPROVED

172SPHAUS-S13-00

U.S.

S13-3

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 13

MODEL 172S NAV III

GENERAL

This supplement is required for Argentine operation of Cessna Model

172S airplanes. The information herein supplements the information of

the basic Pilot's Operating Handbook and FAA Approved Airplane

Flight Manual. For limitations, procedures and performance information

not contained in the supplement, consult the basic FAA Approved

Airplane Flight Manual.

OPERATING LIMITATIONS

GLOBAL POSITIONING SYSTEM (G.P.S.)

If the GPS is installed: Pilot is not authorized to use the Global

Positioning System (GPS) for precision approach and landing.

EMERGENCY LOCATOR TRANSMITTER (E.L.T.)

The Emergency Locator Transmitter (ELT) must comply with RAAC

91.207.

KINDS OF OPERATIONS LIMITS

The necessary equipment for the different kind of operations must

comply with the applicable regulations for Argentina.

FAA APPROVED

S13-4

U.S.

172SPHAUS-S13-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 13

PLACARDS

The following information must be displayed in the form of composite or

individual placards.

In full view of the pilot:

(The "DAY-NIGHT-VFR-IFR" entry,

shown on the example below, will vary as the airplane

equipped).

The markings and placards installed in this airplane contain operating limitations

which must be complied with when operating this airplane in the Normal

Category. Other operating limitations which must be complied with when

operating this airplane in this category or in the Utility Category are contained in

the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual.

Normal Category - No acrobatic maneuvers, including spins, approved.

Utility Category - No acrobatic maneuvers approved, except those listed in the

Pilot's Operating Handbook.

Baggage compartment and rear seat must not be occupied.

Spin Recovery - Opposite rudder-forward elevator-neutralize controls.

Flight into known icing conditions prohibited.

This airplane is certified for the following flight operations as of date of original

airworthiness certificate:

DAY - NIGHT - VFR- IFR

Las marcas y placas instaladas en este avión contienen limitaciones operativas

que deben ser cumplidas al operar este avión en la Categoría Normal. En el

Manual de Operaciones del Piloto y en el Manual de Vuelo del Avión aprobado

por la DNA están contenidas otras limitaciones operativas que se deben cumplir

al operar el avión en esta categoría o en la categoría utilitarios.

Categoría Normal - No están aprobadas las maniobras acrobáticas, incluido

tirabuzón.

Categoría Utilitarios - No están aprobadas las maniobras acrobáticas, excepto

aquellas que se encuentran en el Manual de Operaciones

del Piloto.

No se deben ocupar los compartimentos para equipaje ni los asientos traseros.

Salida de tirabuzón - Timón contrario, elevador hacia delante, centrar los

comandos.

Está prohibido el vuelo en condiciones conocidas de formación de hielo.

Este avión está certificado para las siguientes operaciones de vuelo a partir de la

fecha del certificado de aeronavegabilidad original:

DÍA - NOCHE - VFR- IFR

(Continued Next Page)

FAA APPROVED

172SPHAUS-S13-00

U.S.

S13-5

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 13

PLACARDS (Continued)

3. Near both fuel tank filler caps:

FUEL

100LL/100 MIN. GRADE AVIATION GASOLINE

CAP. 26.5 U.S. GAL. USABLE

CAP. 17.5 U.S. GAL. USABLE TO BOTTOM

OF FILLER INDICATOR TAB.

NAFTA DE AVIACIÓN GRADO 100LL/100 MIN.

CAP. 100 LTS

(26.5 GALONES ESTADOUNIDENSES)

CAP. UTILIZABLE DE 66 LTS

(17.5 GALONES ESTADOUNIDENSES)

UTILIZABLE HASTA LA PARTE INFERIOR DE LA ALETA

INDICADORA DE LLENADO.

4. On flap control indicator:

(Partial flap range with blue color code;

UP to 10^o

110 KIAS

also, mechanical detent at 10^o.)

(White color code; also, mechanical detent

10^o to FULL

85 KIAS

at 20^o.)

(Alcance del movimiento parcial del flap

HASTA 10^o

110 KIAS

con código de color azul; detención

mecánica en la posición 10º.)

(Código de color blanco, detención

10^o HASTA

85 KIAS

mecánica a 20º.)

EL MÁXIMO

(Continued Next Page)

FAA APPROVED

172SPHAUS-S13-00

U.S.

S13-7

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 13

MODEL 172S NAV III

PLACARDS (Continued)

5. In baggage compartment:

54 KG MÁXIMO

EQUIPAJE ADELANTE DE LA TRABA DE LA PUERTA DE EQUIPAJE

22 KG MÁXIMO

EQUIPAJE POSTERIOR A LA TRABA DE LA PUERTA DE EQUIPAJE

MÁXIMO: 54 KG COMBINADOS

PARA INSTRUCCIONES ADICIONALES DE CARGA

VER DATOS DE PESO Y BALANCEO

6. A calibration card must be provided to indicate the accuracy of

the magnetic compass in 30° increments.

Se debe proporcionar una tarjeta de calibración para indicar la

precisión de la brújula magnética en incrementos de 30º.

(Continued Next Page)

FAA APPROVED

S13-8

U.S.

172SPHAUS-S13-00

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 13

MODEL 172S NAV III

PLACARDS (Continued)

10. On the upper right side of the aft cabin partition:

TRANSMISOR LOCALIZADOR DE EMERGENCIA

INSTALADO EN LA PARTE POSTERIOR DE ESTE TABIQUE

SERVICE EN CONFORMIDAD CON RAAC 91.207

11. On forward face of firewall adjacent to the battery:

ADVERTENCIA

24 VOLTIOS C.C.

ESTA AERONAVE ESTÁ EQUIPADA CON ALTERNADOR Y UN

SISTEMA DE CONEXIÓN A MASA NEGATIVO

RESPETAR LA POLARIDAD APROPIADA

LA POLARIDAD INVERSA DAÑARÁ LOS COMPONENTES

ELÉCTRICOS

(Continued Next Page)

FAA APPROVED

S13-10

U.S.

172SPHAUS-S13-00

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 13

MODEL 172S NAV III

EMERGENCY PROCEDURES

There is no change to the airplane emergency procedures when used

for Argentine Certified Airplanes.

NORMAL PROCEDURES

There is no change to the airplane normal procedures when used for

Argentine Certified Airplanes.

PERFORMANCE

There is no change to the airplane performance when used for

Argentine Certified Airplanes.

FAA APPROVED

S13-12

U.S.

172SPHAUS-S13-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 13

LOG OF D.N.A. ACCEPTED SUPPLEMENTS

The following list contains D.N.A. accepted supplements. Refer to Log

of Approved Supplements in the basic Pilot's Operating Handbook and

FAA Approved Airplane Flight Manual for revision status.

Supplement

Name

Equipment

Number

Installed

Pointer Model 3000 -11 or Model 4000-11

Emergency Locator Transmitter (ELT)

_____________

Reserved

Bendix/King KAP 140 2 Axis Autopilot

_____________

Winterization Kit

_____________

Reserved

Artex C406-N Emergency Locator

Transmitter (ELT)

_____________

Bendix/King KR

87 Automatic Direction

Finder (ADF)

_____________

Reserved

Artex ME406 Emergency Locator

Transmitter (ELT)

_____________

Reserved

Argentine Certified Airplanes

_____________

FAA APPROVED

172SPHAUS-S13-00

U.S.

S13-13/S13-14

CESSNA MODEL 172S

NAV III AVIONICS OPTION - KAP 140 AUTOPILOT

Serials

172S9810 thru 172S10467 and 172S10469 thru 172S10506

and

172S10508 thru 172S10639 and 172S10641 thru 172S10655

SUPPLEMENT 15

UKRAINIAN CERTIFIED AIRPLANES

SERIAL NO.

REGISTRATION NO.

This supplement must be inserted into Section 9 of the Pilot's Operating Handbook and FAA

Approved Airplane Flight Manual for Ukrainian Certified Airplanes. This supplement is approved by

the U.S. Federal Aviation Administration (FAA) on behalf of the State Aviation Administration of

Ukraine (SAA).

8 MAY 2012

CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA

172SPHAUS-S15-00

U.S.

S15-1

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

SUPPLEMENT 15

UKRAINIAN CERTIFIED AIRPLANES

Use the Log of Effective Pages to determine the current status of this

supplement.

Pages affected by the current revision are indicated by an asterisk (*)

preceding the page number.

Supplement Status

Date

Original Issue

8 May 2012

LOG OF EFFECTIVE PAGES

Page

Revision

Number

Status

Number

S15-1 thru S15-23/S15-24

Original

FAA APPROVED

S15-2

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

SERVICE BULLETIN CONFIGURATION LIST

The following is a list of Service Bulletins that are applicable to the

operation of the airplane, and have been incorporated into this

supplement. This list contains only those Service Bulletins that are

currently active.

Number

Title

Airplane Serial

Revision

Incorporated

Effectivity

Incorporated

in Airplane

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-3

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

UKRAINIAN CERTIFIED AIRPLANES

GENERAL

This supplement must be placed in Section 9 of the basic Pilot’s

Operating Handbook and FAA Approved Airplane Flight Manual for

Ukrainian Certified Airplanes. The information contained herein

supplements the information of the basic Pilot’s Operating Handbook

and FAA Approved Airplane Flight Manual. Limitations, procedures,

and performance found in this supplement supersedes those found in

the basic Pilot’s Operating Handbook and FAA Approved Airplane

Flight Manual. For limitations, procedures, and performance

information not contained in this supplement, consult the basic Pilot’s

Operating Handbook and FAA Approved Airplane Flight Manual.

NOTE

In Ukraine, FAA operating rules (i.e., 14 CFR Part 91 and

14 CFR Part 135) are not applicable. The airplane must be

equipped and operated in accordance with applicable

Ukraine operational requirements.

FAA APPROVED

S15-4

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS

The following Limitations supersede and/or are in addition to the

Limitations set forth in the basic Pilot’s Operating Handbook and FAA

Approved Airplane Flight Manual:

Minimum Flight Crew:

One (1) Pilot (flying from left seat)

Maximum Number Of Seats:

Four (4)

Maximum Number Of Passengers:

Three (3) Passengers

The Nav III - KAP 140 Autopilot Avionics Option is approved for

Category I ILS approach operations only.

The Global Positioning Satellite (GPS) system is not approved for

approach.

Operation over water beyond the Maximum Glide distance from shore

is prohibited (Refer to the POH/AFM, Section 3, Figure 3-1).

A Flight Data Recorder (FDR) must be installed and operational for all

commercial transportation operations.

A portable COSPAS-SARSAT (406MHz) Emergency Radio Beacon

must be carried and operational for all operations over areas that are

difficult to access, certain regions that are rarely populated and when

flying over large bodies of water.

A HF radio must be installed and operational if airplane operates in

areas where communication through VHF radio stations cannot be

performed.

G1000 LIMITATIONS

The Garmin G1000 integrated avionics system has a minimum

operating temperature of Minus 40º C.

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-5

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATION LIMITS

The following Kinds of Operations Equipment List (KOEL) identifies the

equipment required to be operational for airplane airworthiness in the

listed kind of operations for Ukrainian Certified Airplanes.

The following KOEL supersedes the KOEL located in Section 2 of the

POH/AFM.

KINDS OF OPERATIONS EQUIPMENT LIST

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

PLACARDS AND MARKINGS

1 - 172S Nav III - POH/AFM

Accessible to

pilot in flight

2 - Bendix/King KAP 140 POH

Accessible to

Autopilot Supplement

pilot in flight

3 - Garmin G1000 Cockpit

Accessible to

Reference Guide

pilot in flight

AIR CONDITIONING

1 - Forward Avionics Fan

2 - PFD Fan

3 - MFD Fan

4 - Aft Avionics Fan

(Continued Next Page)

FAA APPROVED

S15-6

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

COMMUNICATIONS

1 - VHF COM

2 - HF COM

* Refer to Note 1

ELECTRICAL POWER

1 - 24V Main Battery

2 - 28V Alternator

3 - 24V Standby Battery

* Refer to Note 2

4 - Main Ammeter

5 - Standby Ammeter

* Refer to Note 2

NOTE

1. A HF COM radio is required if

airplane operates in areas

where communication through VHF radio stations cannot be

performed.

2. The European Aviation Safety Agency (EASA) requires the

24V Standby Battery and Standby Ammeter to successfully

complete the pre-flight check before operating the airplane in

VFR night, IFR day, or IFR night conditions in Europe. Correct

operation of the 24V Standby Battery and Standby Ammeter is

recommended for all other operations.

(Continued Next Page)

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-7

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

EQUIPMENT AND FURNISHINGS

1 - Seat Belt Assembly

Each Seat

Occupant

2 - Shoulder Harness

Front Seat

Occupants

3 - Portable COSPAS-SARSAT

* Refer to Note 3

Emergency Radio Beacon

FLIGHT CONTROLS

1 - Flap Position Indicator

2 - Flap Motor

3 - Elevator Trim System

4 - Elevator Trim Indicator

FUEL SYSTEM

1 - Electric Fuel Pump

2 - Fuel Quantity Indicator - L Tank

3 - Fuel Quantity Indicator - R Tank

NOTE

3. Portable COSPAS-SARSAT Emergency

Radio Beacon

required for all operations over areas that are difficult to

access, certain regions that are rarely populated and when

flying over large bodies of water.

(Continued Next Page)

FAA APPROVED

S15-8

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

ICE AND RAIN PROTECTION

1 - Alternate Static Air Source

2 - Alternate Induction Air System

INDICATING/RECORDING

SYSTEM

1 - Stall Warning System

2 - System Annunciator and

Warning Displays

3 - Flight Data Recorder (FDR)

*Refer to Note 4.

LANDING GEAR

1 - Wheel Fairings

Removable

LIGHTING

1 - PFD Bezel Lighting

2 - PFD Backlighting

*Refer to Note 5.

3 - MFD Bezel Lighting

4 - MFD Backlighting

*Refer to Note 6.

NOTE

4. Flight Data Recorder (FDR) required for all commercial transportation

operations.

5. PDF backlighting is required for day VFR flight if MFD backlighting has

failed. Display backup mode must be active so engine indicators are

shown.

6. MFD backlighting is required for day VFR flight if PDF backlighting has

failed. Display backup mode must be active so flight instruments are

shown.

(Continued Next Page)

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-9

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

LIGHTING (Continued)

5 - Switch and Circuit Breaker

Panel Lighting

6 - Standby Airspeed Indicator

Internal Lighting

7 - Standby Altimeter Internal

Lighting

8 - Non-stabilized Magnetic

Compass Internal Lighting

9 - Standby Attitude Indicator

Internal Lighting

10 - Cockpit Flood Light

11 - Aircraft Position (NAV) Lights

12 - STROBE Light System

13 - BEACON Light

14 - TAXI Light

15 - LAND (Landing) Light

*Refer to Note 7.

NOTE

7. Operations for hire only. Landing light required for airplanes

equipped with single HID landing/taxi light. For airplanes

equipped with dual LED landing/taxi lights, a single LED

landing/taxi light assembly must be operating on either wing,

with all 18 LED bulbs operational.

(Continued Next Page)

FAA APPROVED

S15-10

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

NAVIGATION AND PITOT-

STATIC SYSTEM

1 - G1000 Airspeed Indicator

2 - Standby Airspeed Indicator

3 - G1000 Altimeter

4 - Standby Altimeter

5 - G1000 Vertical Speed

Indicator

6 - G1000 Attitude Indicator

7 - Standby Attitude Indicator

8 - G1000 Directional Indicator

(HSI)

9 - G1000 Turn Coordinator

10 - Non-stabilized Magnetic

Compass

11 - VHF Navigation Radio

A/R

As Required Per

(VOR/LOC/GS)

Procedure

12 - GPS Receiver/Navigator

A/R

As Required Per

Procedure

13 - ADF Navigation Radio

A/R

As Required Per

Procedure

(Continued Next Page)

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-11

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

KINDS OF OPERATIONS EQUIPMENT LIST (Continued)

KIND OF OPERATION

System, Instrument, Equipment

and/or Function

COMMENTS

NAVIGATION AND PITOT-

STATIC SYSTEM (Continued)

14 - Marker Beacon Receiver

A/R

As Required Per

Procedure

15 - Blind Altitude Encoder

A/R

As Required Per

Procedure

16 - Clock

17 - Bendix King KAP 140

Autopilot

VACUUM

1 - Engine Driven Vacuum Pump

2 - Vacuum Indicator

ENGINE FUEL AND CONTROL

1 - Fuel Flow Indicator

ENGINE INDICATING

1 - Tachometer (RPM)

2 - Cylinder Head Temperature

(CHT) Indicator

3 - Oil Pressure Indicator

4 - Oil Temperature Indicator

ENGINE OIL

1 - Engine Crankcase Dipstick

FAA APPROVED

S15-12

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

FUEL LIMITATIONS

Approved Fuels:

100LL (ASTM-D910)

100 (Formerly 100/130) (ASTM-D910)

B91/115 (GOST 1012-72)*

NOTE

* If Russian B91/115 fuel is used, the airplane must be

equipped with either float type or Gen 3.0 fuel level

senders.

See the latest revision of Lycoming Service Instruction No.1070 for

approved fuel grades.

Fuels must contain an anti-icing fuel additive (Isopropyl Alcohol or

DiEGME) in concentrations mixed as noted in Section 8 of the POH/

AFM.

MAXIMUM APPROVED OPERATING ALTITUDE

The maximum operating barometric altitude is limited to the following:

With Passengers

3000 m (9800 feet)

Flight Crew Only (30 Minutes Maximum)

3600 m (11,800 feet)

OUTSIDE AIR TEMPERATURE LIMITS

Ground operations limits for a cold day:

Minus 40°C

Ground operations limits for a hot day:

+40°C

(Continued Next Page)

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-13

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

TAXI OPERATIONAL LIMITS

Uncontaminated paved taxiway:

• Maximum wind velocity while taxiing:

14 m/s (27 Knots)

Paved taxiway contaminated with precipitation:

• Maximum wind velocity while taxiing:

3 m/s (5 Knots)

Refer to Section 4 of the POH/AFM for additional information on taxiing.

TAKEOFF AND LANDING OPERATIONAL LIMITS

Maximum Takeoff and Landing Altitude:

2438 m (8000 feet)

Maximum Headwind Velocity:

14 m/s (27 Knots)

Maximum Tailwind Velocity:

5 m/s (10 Knots)

Maximum crosswind velocity on

uncontaminated paved runway:

7m/s (15 Knots)

ALLOWABLE RUNWAY SURFACE CONDITIONS

1. Uncontaminated runway with paved surface.

2. Paved runway contaminated with precipitation (average depth

and types):

a. Water, less that 10.0 mm.

b. Slush, less than 10.0 mm.

c. Loose snow less than 30.0 mm.

3. Unpaved runway

a. Surface hardness not less than 7 kg/cm² with wheel fairings

installed.

b. Surface hardness not less than 5 kg/cm² with wheel fairings

removed.

c. Landing on contaminated unpaved runways is prohibited.

Operating with the landing gear fairings removed is recommended on

wet or unpaved runways when temperatures are near or below

freezing.

(Continued Next Page)

FAA APPROVED

S15-14

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

OPERATING LIMITATIONS (Continued)

TAKEOFF AND LANDING OPERATIONAL LIMITS

(Continued)

MAXIMUM CROSSWIND ON CONTAMINATED RUNWAYS

Contaminated paved runways with:

Water, less than 10.0 mm

3 m/s (5 Knots)

Slush, less than 10.0 mm

3 m/s (5 Knots)

Loose snow, less than 30.0 mm

3 m/s (5 Knots)

Paved runway with less than 3 mm of water, snow or slush and braking

coefficient of friction(µ) of:

µ=0.3 (poor braking)

3 m/s (5 Knots)

µ=0.4 (average braking)

5 m/s (9 Knots)

µ=0.5 (good braking, dry or

equivalent to dry runway)

7 m/s (15 Knots)

NOTE

• For intermediate values of coefficient of friction

(μ),

crosswind is to be estimated by interpolation.

• Operation is prohibited on a runway covered with ice at a

coefficient of friction μ < 0.3.

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-15

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

EMERGENCY PROCEDURES

FORCED LANDINGS

If all attempts to restart the engine fail and a forced landing is imminent,

select a suitable field and prepare for the landing as discussed under

the Emergency Landing Without Engine Power checklist. Transmit

Mayday message on 121.5 MHz giving location, intentions and squawk

7700.

Before attempting an off airport landing with engine power available,

one should fly over the landing area at a safe, but low altitude, to

inspect the terrain for obstructions and surface conditions, proceeding

as discussed in the Precautionary Landing With Engine Power

checklist.

Prepare for ditching by securing or jettisoning heavy objects located in

the baggage area and collect folded coats for protection of occupants'

face at touchdown. Transmit Mayday messages on 121.5 MHz giving

location, intentions and squawk 7700. Avoid a landing flare because of

the difficulty in judging height over a water surface. The checklist

assumes the availability of power to make a precautionary water

landing. If power is not available, use of the airspeeds noted with

minimum flap extension will provide a more favorable attitude for a

power off ditching.

In a forced landing situation, do not turn off the MASTER switch,

AVIONICS switch or STBY BATT switch until a landing is assured.

Premature deactivation of the switches will disable all airplane electrical

systems.

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-17

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

NORMAL PROCEDURES (Continued)

COLD WEATHER OPERATIONS

The Garmin GDU 1040 PFD/MFD requires a warm-up time of up to 30

minutes when exposed to Minus 40°C for an extended period. A warm-

up time of up to 15 minutes may be required when exposed to Minus

30°C for an extended period of time.

COLD SOAK

If extended exposure to cold weather is expected, refer to Maintenance

Manual, Model 172 Series 1996 and On, Chapter 12 Servicing, Section

12-30-00 Unscheduled Servicing-Description and Operation,

paragraph 3 Cold Soak, for procedures to prepare the airplane for cold

soak.

After extended exposure, for more than two hours, at temperatures

colder than Minus -10°C (14°F), refer to Maintenance Manual, Model

172 Series 1996 and On, Chapter 12 Servicing, Section 12-30-00

Unscheduled Servicing-Description and Operation, paragraph 3 Cold

Soak, for procedures of an airplane for preparing the airplane for flight.

Cold temperatures will affect control cable tension. See Chapter 27 of

the Maintenance Manual for flight control cable tensions. See Chapter

12 of the Maintenance Manual for information on lubrication and

greasing of moving parts. See Section 8 of the POH/AFM for correct

engine oil viscosity. See paragraphs on Cold Weather Operation in

Section 4 of the POH/AFM for additional information on procedures for

operating the airplane in cold temperatures.

When the outside temperature is less than Minus 34ºC, the airplane

batteries should be removed and stored in the warm conditions.

(Continued Next Page)

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-19

SECTION 9 - SUPPLEMENTS

CESSNA

SUPPLEMENT 15

MODEL 172S NAV III

KAP 140 AUTOPILOT

NORMAL PROCEDURES (Continued)

COLD SOAK (Continued)

Engine must be preheated before starting if engine temperature is less

than Minus 6°C. Refer to Lycoming Service Instruction No. 1505 for

recommendation of an engine preheating procedures.

When the outside temperature is less than

0°C, moisture from

combustion can freeze on the engine spark plugs if the engine does not

continue to operate after it is started. This will prevent the engine from

starting again. Preheat the engine to more than 0°C before starting the

engine again.

Preheat the engine by directing warm air into the engine cowling inlets

behind the propeller. The temperature of the preheating air should not

be more than 120°C to prevent damage to the exterior paint. Open

flames are prohibited near the airplane.

The Garmin GDU 1040 PFD/MFD requires a warm-up time of up to 30

minutes when exposed to Minus 40°C for an extended period. A warm-

up time of up to 15 minutes may be required when exposed to Minus

30°C for an extended period of time.

Before takeoff, preheat the airplane cabin to more than Minus 30°C for

correct operation of the standby altimeter. If there is no warning that an

instrument is operating incorrectly, all other instruments will operate

down to the minimum temperature of the airplane.

Before operating the airplane, it is recommended to heat the cabin to a

comfortable temperature for the cabin occupants.

FAA APPROVED

S15-20

U.S.

172SPHAUS-S15-00

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

PERFORMANCE

TAKEOFF DISTANCE

The takeoff distance on a paved runway with no more than 3 mm of

precipitation is equal to dry runway takeoff distance.

The takeoff distance on a paved runway with precipitation greater than

3 mm is 20% greater than the dry runway takeoff distance.

LANDING DISTANCE

DRY RUNWAY - BASIC AIRFIELD

To determine the required landing distance for Ukrainian Certified

Airplanes on a dry paved runway, the dry runway landing distance listed

in Section 5, Performance, Short Field Landing Distance, Figure 5-11,

of the U.S. POH must be multiplied by 1.67.

DRY RUNWAY - DIVERSION OR ALTERNATE AIRFIELD

To determine the required landing distance for Ukrainian Certified

Airplanes on a dry paved runway, the dry runway landing distance listed

in Section 5, Performance, Short Field Landing Distance, Figure 5-11,

of the U.S. POH must be multiplied by 1.43.

CONTAMINATED RUNWAY

To determine the required landing distance for Ukrainian Certified

Airplanes on a contaminated paved runway, the Ukrainian-Factored dry

runway landing distance must be multiplied by 1.43.

WET RUNWAY

To determine the required landing distance for Ukrainian Certified

Airplanes on a wet paved runway, the Ukrainian-Factored dry runway

landing distance must be multiplied by 1.15.

For unpaved runway landing distance, refer to Section 5, Performance,

Short Field Landing Distance, Figure 5-11, of the U.S. POH for the

correction applied to grass runway landing distance.

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-21/S15-22

CESSNA

SECTION 9 - SUPPLEMENTS

MODEL 172S NAV III

SUPPLEMENT 15

KAP140 AUTOPILOT

LOG OF UKRAINE APPROVED SUPPLEMENTS

The following list contains Ukrainian SAA accepted supplements. Refer

to Log of Approved Supplements in the basic Pilot's Operating

Handbook and FAA Approved Airplane Flight Manual for revision

status.

Supplement

Name

Equipment

Number

Installed

Pointer Model 3000-11 or Model 4000-11

Emergency Locator Transmitter (ELT)

_____________

Reserved

Bendix/King KAP 140 2 Axis Autopilot

_____________

Winterization Kit

_____________

Reserved

Artex C406-N Emergency Locator

Transmitter (ELT)

_____________

Bendix/King KR 87 Automatic Direction

Finder (ADF)

_____________

Reserved

Artex ME406 Emergency Locator

Transmitter (ELT)

_____________

Reserved

Garmin G1000 Synthetic Vision

Technology (SVT)

_____________

Reserved

Ukrainian Certified Airplanes

_____________

FAA APPROVED

172SPHAUS-S15-00

U.S.

S15-23/S15-24

CESSNA 172S NAV III Skyhawk SP. Information Manual (2016) - page 5