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Description

December 2012

Beginning with Serial # 172S11284

Initial __________________________

Exhibit “A"

MODEL 172S

SPECIFICATION AND DESCRIPTION

EXHIBIT “A"

DECEMBER 2012

BEGINNING WITH SERIAL # 172S11284

Cessna Single Engine Piston Aircraft

2625 S. Hoover Rd.

Wichita, Kansas 67215

Copyright 2012 Cessna Aircraft Company

December 2012

1

INTRODUCTION

This document is published for the purpose of providing general information for the evaluation of design, perfor- mance and equipment of the Cessna Skyhawk. Should more information be required, please contact:

Cessna Aircraft Company

Single Engine Piston Aircraft

2625 S. Hoover Rd.

Wichita, Kansas 67215

1-800-4-CESSNA

www.se.cessna.com Description documents and describes only the Skyhawk Model 172S, its powerplant and equipment. Also included are the warranties applicable to the Skyhawk Model 172S aircraft, the Textron Lycoming IO-360-L2A engine, the McCauley propeller and the OEM-installed Garmin avi- this document and the basic purchase agreement, the basic purchase agreement language shall govern. Due and Description and the scheduled delivery date of the cation" whenever occasioned by product improvements, government regulations or other good cause.

December 2012

2

Section Page

1. General Description ....................................................

1.2 Approximate Dimensions .................................................

1.3 Design Weights and Capacities ..................................................

2. Performance ............................................................

3. Powerplant & Accessories ............................................................

4. Skyhawk Equipment List .................................................

5. Instrument Panel .......................................................

6. Electrical Power .......................................................

7. Engine Indicating System (Electronic) ................................

8. Environmental ..........................................................

9. Exterior ...............................................................

10. Exterior Lights ........................................................

11. Flight Controls ........................................................

12. Fuel System ............................................................

13. Interior ...............................................................

14. Interior Lighting ......................................................

15. Exterior Striping Options ..............................................

16. Training ................................................................

17. Limited Warranties ..............................................................

17.1 Cessna"s Limited Warranty - Single Engine Piston Aircraft ..................................................

17.2 Aircraft Paint and Graphics - Single Engine Piston Aircraft ..................................................

17.3 Textron Lycoming Warranty (Limited) New Reciprocating Aircraft Engines ..........................

17.4 McCauley Propeller Systems Standard Limited Warranty ....................................................

17.5 Garmin Avionics Installed in Single Engine Aircraft ..............................................................

FIGURE I - SKYHAWK EXTERIOR DIMENSIONS ................................................. FIGURE II - SKYHAWK INTERIOR DIMENSIONS .................................................

FIGURE III - SKYHAWK INSTRUMENT PANEL .......................................................................

TABLE OF CONTENTS

3 3 3 6 7 7 8 9 10 10 10 10 10 11 11 11 12 12 12 13 13 13 14 15 16 4 5 9

December 2012

3 All information herein applies to the Skyhawk (Model

172S). The Skyhawk aircraft is an all-metal, single-en-

gine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. Suitable allowance for luggage is provided. FAA Federal Aviation Regulation Part 23 through amend- ment 23-6, including day, night, VFR and IFR.

1. GENERAL DESCRIPTION

1.2 Approximate Dimensions

Overall Height ......................................................... Overall Length ......................................................... Span (overall) ....................................................... Area ................................................................... Height (max) ......................................................... Width (trim to trim) ................................................. Height (front) ....................................................... Height (rear) ........................................................ Width (top) .......................................................... Width (bottom) ....................................................... Height (front) ....................................................... Height (rear) ........................................................ Width ..................................................................

8 ft 11in (2.72 m)

27 ft 2 in (8.28 m)

36 ft 1 in (11.00 m)

174 sq ft (16.2 sq m)

48 in (1.22 m)

39.5 in (1.00 m)

142 in (3.61 m)

40.5 in (1.03 m)

39 in (0.99 m)

32.5 in (0.83 m)

37 in (0.94 m)

22 in (0.56 m)

21 in (0.53 m)

15.3 in (0.39 m)

December 2012

4

36" - 1"

11' - 4"

27' - 2"

8' - 11"

1. GENERAL DESCRIPTION (Continued)

FIGURE I - SKYHAWK EXTERIOR DIMENSIONS

Note: Optional Wheel Fairings Shown

December 2012

5

1. GENERAL DESCRIPTION (Continued)

FIGURE II - SKYHAWK INTERIOR DIMENSIONS

48.75

Aft Baggage Area

10.25 34.00
41.00

48.0043.00

42.75

Tiedown Rings

Firewall

Face of

Instrument

Panel *Cabin ** Lower Window Line *36.00 **38.50 21.50
*34.00 **39.50

December 2012

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1. GENERAL DESCRIPTION (Continued)

1.3 Design Weight and Capacities

Ramp Weight

Normal Category ........................................................ Utility Category .......................................................

Takeoff Weight

Normal Category ........................................................ Utility Category .......................................................

Landing Weight

Normal Category ........................................................ Standard Empty Weight...................................................................

Maximum Useful Load

Normal Category ........................................................ Utility Category .......................................................

Baggage Allowance

Normal Category ........................................................

Fuel Capacity

Total Capacity .......................................................... Total Useable ........................................................... Total Capacity each Tank ....................................................................

Total Useable Capacity each Tank ....................................................................

Oil Capacity

Sump ................................................................... Total Capacity ..........................................................

2,558 lbs (1,160 kg)

2,208 lbs (1,002 kg)

2,550 lbs (1,157 kg)

2,200 lbs (998 kg)

2,550 lbs (1,157 kg)

1,641 lbs (744 kg)

917 lbs (415 kg)

567 lbs (257 kg)

120 lbs (54 kg)

56 gal (212 L)

53 gal (200.6 L)

28 gal (106 L)

26.5 gal (100.3 L)

8 qts (7.6 L)

9 qts (8.5 L)

NOTES

1. Standard empty weight based upon:

a) 0.6-mil primer on all details, 0.6-mil primer on all exterior surfaces and 2.0-mil paint on all exterior surfaces.

December 2012

7 Service Ceiling ........................................................ Takeoff Distance S.L. (Ground Roll) ........................................ Takeoff Distance S.L. (To Clear 50 ft. Obstacle) .............................................. Maximum Climb Rate S.L. ................................................ Maximum Speed S.L. ..................................................... Maximum Range and Endurance ............................................ Cruise Speed (75% pwr at 8,500 ft) ................................... Cruise Range and Endurance (75% pwr at 8,500 ft) ..................... Landing Distance (Ground Roll) ....................................... Landing Distance (To Clear 50 ft. Obstacle) ..............................................

2. PERFORMANCE

All estimated performance data are based on airplane weights at 2,550 po unds; standard atmospheric conditions; lev- Aircraft Company under carefully documented conditions and will vary wit h individual airplanes, pilots, and numerous

14,000 ft

960 ft

1,630 ft

730 fpm

126 kts / 145 mph

638 nm / 6.72 hrs

124 kts / 143 mph

518 nm / 4.26 hrs

575 ft

1,335 ft

3. POWERPLANT & ACCESSORIES

Lycoming IO-360-L2A Engine

180 HP @ 2700 RPM

Fuel Injection System

Tubular Steel Engine Mount

Dynafocal Rear Mount

Engine Driven Vacuum Pump

Automatic Alternate Engine Air

Oil Cooler

Shock Mounted Cowling

Induction Air Filter

Full Flow Oil Filter

Throttle Control

Vernier Mixture Control

Dual Ignition System, Shielded Magneto

McCauley Fixed Pitch 2 - Blade Metal Propeller

Propeller Spinner, Polished

Electric Starter

December 2012

8

4. SKYHAWK EQUIPMENT LIST

GMA-1347 Digital Audio Panel w/Marker Beacon/

Intercom

GTX-33 Transponder-Mode S w-TIS

GIA-63W NAV/COM/GPS/WAAS w/GS #1

GIA-63W NAV/COM/GPS/WAAS w/GS #2

GDU-1040 Primary Flight Display (PFD)

GDU-1040 Multi-Function Display (MFD)

GEA-71 Engine/Airframe Computer

GRS-77 Attitude & Heading Reference System

(AHRS)

GDC-74A Air Data Computer w/OAT Probe

GMU-44 Magnetometer

Garmin SafeTaxi & FliteCharts

Electronic Checklists

ME406 Two Frequency Emergency Locator Trans-

mitter

Emergency Locator Transmitter Remote Mounted

Switch

Backup Attitude Gyro, Altimeter and Airspeed Indi- cator

Control Wheel Push-To-Talk Switch-Pilot/Copilot

Mic & Phone Jacks-Pilot/Copilot/Passengers

Auxiliary Stereo Input Jack

Antennas:

Antenna

Pitot System - Heated

Static System

Hand Held Microphone

Alternate Static Source

Compass

The following list of equipment is included on the standard

December 2012

9

5. INSTRUMENTATION

FIGURE III - SKYHAWK INSTRUMENT PANEL

1.

MASTER Switch (ALT and BAT)

2.

STBY BATT Switch

3.

STBY BATT Test Annunciator

4.

AVIONICS Switch (BUS 1 and BUS 2)

5.

Electrical Switches

6.

GDU-1040 Primary Flight Display

7. Backup Attitude Gyro, Airspeed & Altimeter Indicator 8.

GMA-1347 Audio Panel

9.

Compass

10.

GDU-1040 Multi-Function Display

11.

ELT Remote Switch/Annunciator

12.

Flight Hour Recorder (Hobbs Meter)

13.

Cabin Air Control

14.

Wing Flap Switch Lever And Position Indicator

15.

Mixture Control

16.

Throttle (With Friction Lock)

17.

ALT Static Air Valve Control

18.

Electrical and Avionics Circuit Breakers

19.

Ignition/Starter Switch, Key Operated

20.

Dimming Panel

20 19 18 17 16 11 15 1413
12 9 8 6 4 5 7 3 2 10 1

December 2012

10

6. ELECTRICAL POWER

Alternator, 28 Volt, 60 Amp

Battery, 24 volt, 8.0 AH (1 hr rate), Manifold Type Standby Battery, 24 volt, 6.2 AH (1 hr rate), Sealed Type

Standby Battery Controller

Electrical Circuit Panel

Electrical J-Box

Cabin Power Jack - 12 Volt, 10 Amp

7. ENGINE INDICATING SYSTEM (ELECTRONIC)

Ammeters

Voltmeters

Vacuum

Oil Pressure and Temperature

Tachometer - Hour Recorder

Fuel Flow (GPH)

LH/RH Fuel Quantity

CHT - Cylinder Head Temperature

EGT - Exhaust Gas Temperature

Standby Vacuum System

Annunciation - Caution and Warning

Alerts (PFD)

8. ENVIRONMENTAL

Windshield Defroster, Pilot/Copilot

Ventilator, Adjustable (6 places)

Carbon Monoxide Detection System

9. EXTERIOR

LH Door, Pilot w/Hinged Window, Lock and Key

RH Door, Copilot w/Hinged Window

LH Baggage Door, w/Lock and Key

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