specification & - cessna
TRANSCRIPT
Specification &Description
April 2013
Initial __________________________
Exhibit “A”
MODEL 162
SPEC I F I CAT ION AND DESCR I PT ION
EXH IB I T “A”
APR I L 2 0 1 3
Cessna Aircraft CompanySingle Engine Piston Aircraft
2625 S. Hoover Rd.Wichita, Kansas 67215Copyright 2013 Cessna Aircraft Company
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INTRODUCT IONThis Specification and Description is published for thepurpose of providing general information for the evalua-tion of the design, performance, and equipment of theCessna model 162. This document supersedes all previ-ous Specification and Description documents anddescribes only the Model 162, its powerplant, and equip-ment.
Also included are the warranties applicable to the Model162 aircraft, the Teledyne Continental Motors O-200Dengine, applicable propeller, and the OEM-installedavionics. In the event of any conflict or discrepancybetween this document and the terms and conditions ofthe purchase agreement to which it is incorporated, theterms and conditions of the purchase agreement govern.
Due to the time span between the date of thisSpecification and Description and the scheduled deliverydate of the aircraft, Cessna reserves the right to revisethe "Specification" whenever occasioned by productimprovements, government regulations, or other goodcause.
For additional information contact:
Cessna Aircraft CompanySingle Engine Piston Aircraft2625 S. Hoover Rd.Wichita, Kansas 672151-800-4-CESSNAwww.se.cessna.com
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TABLE OF CONTENTSCessna Model 162 Specification and Description
Section Page
1. General Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31.1 Certification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31.2 Approximate Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3
2. Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
3. Structural Design Criteria . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
4. Fuselage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
5. Wing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
6. Empennage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
7. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
8. Powerplant . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
9. Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
10. Avionics and Instrumentation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
11. Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
12. Exterior Striping Options . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
13. Limited Warranties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
13.1. Cessna Skycatcher Model 162 Piston Aircraft Limited Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
13.2. Garmin Standard Avionics Limited Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
13.3. Teledyne Continental Motors, Inc. New Engine Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
13.4. McCauley Propeller Systems Standard Limited Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
13.5. Cessna Skycatcher Model 162 Paint Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
FIGURE I — MODEL 162 EXTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
FIGURE II — MODEL 162 INTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5
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1 . GENERAL DESCR I PT ION
The Cessna model 162 is an all-metal, single engine pis-ton, high-wing monoplane with a two-person seatingcapacity including the pilot. Suitable allowance for lug-gage is provided aft of the seats. The 162 is equippedper FAR 91.205 to meet both Day and Night VFR flightrequirements. Cessna's worldwide network of author-ized service centers provides a complete source for allservicing needs.
1.1 Certification
The Model 162 is designed and built to comply with theAmerican Society for Testing and Materials International(ASTM) standards for Light Sport Aircraft and it meets
the limitation and Special Certificate of Airworthinessrequirements for a Light Sport category aircraft asdefined by the FAA in CFR Part 1.1 and CFR Part21.190.
The Purchaser is responsible for obtaining aircraft oper-ating approval from the relevant civil aviation authorityprior to aircraft delivery.
1.2 Approximate Dimensions
Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Continental O-200D
Horsepower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 100 hp at 2750 RPM
Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-Blade McCauley Composite Fixed Pitch Propeller
Service Ceiling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14,625 ft (4,457.7 m)
Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,324 lbs (600 kg)
Maximum Gross Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,320 lbs (598.7 kg)
Standard Empty Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 843 lbs (382.3 kg)
Maximum Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 481 lbs (218.1 kg)
Fuel Capacity (Usable) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 gal (90.85 l)
Overall Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 ft 4 in (2.23 m)
Overall Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 ft 1 in (6.80 m)
Wing Span . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 ft 5 in(9.26 m)
Horizontal Tail Span . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9 ft 10 in (3.2 m)
Cabin Width at Shoulders . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44.3 in (112.4 cm)
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1 . GENERAL DESCR I PT ION ( C on t i n u ed )
FIGURE I — MODEL 162 EXTERIOR DIMENSIONS
30 ft 5 in(9.26 m)
22 ft 1 in (6.80 m)
7 ft 4 in (2.23 m)
9 ft 10 in (3 m)
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FIGURE II — MODEL 162 INTERIOR DIMENSIONS
1 . GENERAL DESCR I PT ION ( C on t i n u ed )
40 in (101.6 cm)
90 in (228.6 cm)
30 in (76.2 cm)
32 in (81.2 cm)
Cabin Height Dimensions
Cabin Width Dimensions
24 in (60.9 cm)
35 in (88.9 cm)
47 in (119.3 cm)
40 in (101.6 cm)
30 in (76.2 cm)
28 in (71.1 cm)
24 in (60.9 cm)
37 in (93.9 cm)
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All performance data is based on the standard aircraftconfiguration, operating in International StandardAtmosphere (ISA) conditions with zero wind. Takeoff andlanding field lengths are based on a level, hard surface,
dry runway. Actual performance will vary with individualairplanes and other factors such as environmental con-ditions, aircraft configuration, and operational/ATC pro-cedures.
Takeoff Distance S.L. (Ground Roll) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 640 ft (195 m)
Takeoff Distance S.L. (To Clear 50 ft Obstacle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,138 ft (347 m)
Max Climb Rate S.L. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 880 fpm (268.2 m)
Max Speed S.L. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 118 kts (219 km/hr, 136 mph)
Max Range and Endurance at 6,000 ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 440 nm / 5.7 hrs
Cruise Speed (69% pwr. at 6,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 109 kts (202 km/hr,125 mph)
Cruise Range and Endurance (69% pwr. at 6,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 336 nm / 3.1 hrs
Landing Distance (Ground Roll) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 671 ft (205 m)
Landing Distance (To Clear 50 ft Obstacle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,369 ft (417 m)
(Performance shown with 30 minutes of fuel reserve)
2 . P ERFORMANCE
3 . S TRUCTURAL DES IGN CR I TER IAThe airframe is designed and constructed to meet therequirements presented in ASTM standard F2245"Standard Specification for Design and Performance of aLight Sport Airplane".
4 . FUSELAGE
The fuselage is constructed primarily of aluminum alloymaterials. The semi-monocoque structure consists offrames and stringers covered by sheet aluminum skin. A
left hand and right hand door are used to allow access forthe pilot and passenger.
5 . W INGThe wing is constructed primarily of aluminum alloymaterials and incorporates a custom designed airfoil.The wing structure uses a two spar design with a strut
that attaches to the forward spar. Slotted flaps are usedto further lower the stall speed. An integral fuel tank isincorporated in each wing.
The horizontal tail is a fixed design with two elevators.Pitch trim is provided by a single trim tab mounted on the
right hand elevator. The rudder does not have anadjustable trim tab. Includes tail tie down guard.
6 . EMPENNAGE
7 . LAND ING GEARThe main landing gear uses high strength, tapered steeltubes to provide the necessary shock absorption.
Each main wheel is equipped with toe actuated discbrakes. Differential braking is used for nose wheel steer-
ing. Toe brakes are provided at both cockpit seats.
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8 . POWERPLANTThe Teledyne Continental Motors O-200D is an air-cooled, horizontally opposed, four cylinder, naturallyaspirated, spark ignited, four stroke, direct drive engineincorporating a wet sump, updraft intake, carburetor,down draft tuned exhaust system w/ EGT sensors, andoil quick drain.
The engine is designed with the capability to operate on100LL aviation fuel, and has a maximum continuous rat-ing of 100 hp at 2750 RPM with a compression ratio of8.5:1. The time between overhaul is 2000 hours or 12years, whichever occurs first.
9 . S YSTEMSThe flight controls consist of dual control sticks, whichprovide movement to the elevator and ailerons. Rudderpedals, with differential toe brakes, provide control to therudder and brakes. A mechanical flap lever locatedbetween the two occupants provides movement to the
flaps. Electric pitch trim is used to adjust elevator trim. A40 amp engine driven alternator powers a single buss 14volt electrical system. A ground service receptacle isincluded. Position, anti-collision, and landing lights arestandard.
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1 0 . AV ION ICS AND I NSTRUMENTAT IONA dual Garmin G300 display provides primary flight andengine information in a split screen or PFD/MFD format.A Garmin SL40 Com radio, PM3000 Intercom, Garmin
GTX327 Mode C transponder, and a 121.5/233 Mhz ELTare standard equipment.
1 1 . I N TER IORl Two Metal Framed Seats with Cloth Wrapped Insertsl LED Overhead Panel Lightingl Neutrally Painted Interiorl Cabin Door Armrests
l Sunvisorl Center Console containing Map and General Storagel 23.2 (.66 m3) Cubic Foot Baggage Areal Baggage Net
1 2 . E X TER IOR
l Black Vinyl and Medium Silver Metallic Stripesl Medium Silver Metallic vinyl Cessna logo, SkyCatcherand Light Sport Logo
l Black Vinyl registration number
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1. Ignition/Starter Switch, Key Operated2. Master Switch (ALT and BAT)3. Lighting Switches4. Electrical and Avionics Circuit Breakers
5. Multi-Function Display6. ELT7. PM3000 Intercom8. SL40 Communications radio
9. GTX327 Mode C transponder10. Primary Flight Display (split screen)
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1 3 . L IM I TED WARRANT I ES13.1 Cessna Skycatcher Model 162 Piston AircraftLimited Warranty (Limited Warranty)
Cessna warrants the aircraft and all parts included there-in to be free from defects in material and workmanshipunder normal use and service for a period of twenty-four(24) months or 2,000 hours (whichever occurs first) afterthe warranty start date, except as hereafter noted.Engines, engine part accessories, avionics, batteries,and propellers are specifically excluded from this war-ranty. Paint and graphics warranties are addressed sep-arately.
Spare parts sold by Cessna, excluding engines, enginepart accessories, avionics, and propellers are warrantedfor six (6) months after installation, except as hereafternoted.
Cessna's obligation under this warranty is limited torepairing or replacing, at its option, with exchange, over-hauled, or new parts, items found defective by Cessna'sexamination which are returned at the owner's expensewithin the applicable twenty-four (24) months or 2,000hours (whichever occurs first) or, for spare parts, theremaining portion of the applicable six (6) month war-ranty period.
A new warranty period is not established for replacementparts. Replacement parts are warranted only for theremainder of the applicable twenty-four (24) months or2,000 hours (whichever occurs first) or, for spare parts,the remaining portion of the applicable limited warrantyperiod.
The repair or replacement of defective parts under thiswarranty will be made without charge to the owner forparts and labor for removal, installation, and/or actualrepair, except that the owner shall pay all import dutiesand sales and use taxes on replacements and repairs.
This limited warranty does not apply to parts subjectedto misuse, negligence, improper installation, accident,alteration; repairs not authorized by Cessna; normalmaintenance services (cleaning, control rigging, brakeand other mechanical adjustments, maintenance inspec-tions, etc.); replacement of service items (light bulbs,brake linings, filters, hoses, tires, cowl mounts, etc.); orto normal deterioration of soft trim or appearance items(paint, upholstery, rubber-like items, etc.) due to corro-
sion, wear and exposure.WITH THE EXCEPTION OF THE WARRANTY OFTITLE, TO THE EXTENT ALLOWED BY APPLICABLELAW, THIS WARRANTY IS EXPRESSLY IN LIEU OFANY OTHER WARRANTIES, EXPRESSED OR IMPLIEDIN FACT OR BY LAW, INCLUDING ANY IMPLIED WAR-RANTY OF MERCHANTABILITY OR FITNESS FOR APARTICULAR PURPOSE. THE REMEDIES OF REPAIROR REPLACEMENT AS ABOVE SET FORTH ARE THEONLY REMEDIES UNDER THIS WARRANTY. CESSNADISCLAIMS ANY OBLIGATION OR LIABILITYWHETHER IN CONTRACT OR IN TORT (ANDWHETHER FOR NEGLIGENCE, STRICT LIABILITY,PRODUCT LIABILITY OR OTHERWISE), INCLUDINGLOSS OF USE OF THE PRODUCT WARRANTED,LOSS OF TIME, INCONVENIENCE, COMMERCIALLOSS OR ANY OTHER DIRECT, CONSEQUENTIAL,SPECIAL OR INCIDENTAL DAMAGES. THIS WARRAN-TY IS IN LIEU OF ANY OTHER OBLIGATION OR LIA-BILITY OF CESSNA OF ANY NATURE WHATSOEVERBY REASON OF THE MANUFACTURE, SALE ORLEASE OF SUCH AIRCRAFT PRODUCTS AND CESS-NA NEITHER ASSUMES NOR AUTHORIZES ANYONETO ASSUME FOR IT ANY OTHER OBLIGATION ORLIABILITY IN CONNECTION WITH SUCH AIRCRAFTPRODUCTS.
13.2 Garmin Standard Avionics Limited Warranty(Limited Warranty)
Aircraft OEM-Installed Avionics 2-Year Limited WarrantyPolicy:
The GARMIN G300 components are warranted to befree from defects in materials or workmanship for twoyears from the date of warranty activation. The SL40Com Radio and the GTX327 Transponder are warrantedto be free from defects in materials or workmanship fortwo years from the date of warranty activation. Withinthis period, GARMIN International, Inc. will at its soleoption, repair or replace any components which fail innormal use. Such repairs or replacement will be made atno charge to the customer for parts or labor, providedthat the customer shall be responsible for any trans-portation cost. This warranty does not cover failures dueto abuse, misuse, accident or unauthorized alteration orrepairs.
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1 3 . L IM I TED WARRANT I ES ( C on t i n u ed )
THE WARRANTIES AND REMEDIES CONTAINEDHEREIN ARE EXCLUSIVE AND IN LIEU OF ALLOTHER WARRANTIES EXPRESS OR IMPLIED ORSTATUTORY, INCLUDING ANY LIABILITY ARISINGUNDER ANY WARRANTY OF MERCHANTABILITYOR FITNESS FOR A PARTICULAR PURPOSE,STATUTORY OR OTHERWISE. THIS WARRANTYGIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAYVARY FROM STATE TO STATE.
IN NO EVENT SHALL GARMIN BE LIABLE FOR ANYINCIDENTAL, SPECIAL, INDIRECT OR CONSE-QUENTIAL DAMAGES, WHETHER RESULTINGFROM THE USE, MISUSE OR INABILITY TO USETHIS PRODUCT OR FROM DEFECTS IN THE PROD-UCT.
In states that do not allow the exclusion of incidental orconsequential damages, the above limitations may notapply.
GARMIN retains the exclusive right to repair or replacethe product or offer a full refund of the purchase price atits sole discretion. SUCH REMEDY SHALL BE THESOLE AND EXCLUSIVE REMEDY FOR ANY BREACHOF WARRANTY.
To obtain warranty service, contact a local GARMINauthorized Service Center. For assistance in locating aService Center near by, call GARMIN Customer Serviceat one of the numbers shown below.
GARMIN International1200 East 151st StreetOlathe, Kansas 66062, U.S.A.Toll free: 1-800-800-1020Phone: 1-913-397-8200FAX: 1-913-397-0836
GARMIN (Europe) Ltd.Unit 5, The QuadrangleAbbey Park Industrial EstateRomsey, SO51 9AQ, U.K.Phone: 44-1794-519944FAX: 44-1794-519222
13.3 Teledyne Continental Motors, Inc. New EngineWarranty
Each new aircraft engine shipped from the TeledyneContinental Motors (TCM) plant on or after April 2, 2010is warranted as follows:
1. (a) For a period of twenty-four (24) months or until theexpiration of TCM’s recommended Time BetweenOverhaul (TBO), whichever occurs first after the war-ranty activation date TCM will, except as excludedbelow, at its option repair or replace on an exchangebasis any engine, component, or part manufacturedor supplied by it which is returned to a TCM author-ized to handle the engine covered by this warrantyand which upon examination is found to the satisfac-tion of TCM to be defective in material or workman-ship. The warranty activation date is the date theengine is first operated for any use or the 180th dayafter TCM’s invoice date, whichever occurs first. Afterthe expiration of the first twelve (12) months of theapplicable twenty-four (24) month period describedabove, TCM will not assume any responsibility for therepair or replacement of engine accessories, i.e.parts which have been purchased by TCM from amanufacturer as a complete and finished unit andincluded in the assembly of an engine without alter-ing the unit, including, but not limited to, carburetors,starters, alternators, turbochargers and fuel controls.After the expiration of the initial twelve (12) monthperiod, accessories will be subject to such warrantycoverage as may be provided by their manufacturer.
(b) TCM will pay for reasonable labor costs associatedwith repairs or replacements under paragraph 1(a) ofthis warranty and for "troubleshooting" costs associ-ated with identifying the need for such repairs orreplacements, when coordinated through an author-ized TCM representative. The amount of repair andreplacement labor costs allowed will be in accor-dance with the latest revision of the warranty laborallowance schedule, form X30552, published byTCM. The amount of "troubleshooting" costs allowedwill be the reasonable costs under the circumstancesof identifying the need for such repairs or replace-ments, but in no event will the "troubleshooting" costsallowed exceed fifteen percent (15%) of the laborcosts associated with such repairs or replacementsallowed by TCM. No "troubleshooting" costallowance will be made where the need for repairs orreplacements is identified in the course of overhaul,
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1 3 . L IM I TED WARRANT I ES ( C on t i n u ed )routine maintenance, or on the basis of an obviousdefect.
(c) TCM will pay transportation costs in connection withthe repair or replacement of any engine, component,or part found to the satisfaction of TCM to be defec-tive in material or workmanship under paragraph 1(a)of this warranty. The engine, component, or part mustbe shipped prepaid to the repair facility designated byTCM. Transportation cost reimbursement for engineswill be the actual surface freight charge or $500.00,whichever is less. Engines must be described on thebill of lading as follows: “Internal combustion engine,other than Radial Cyl RVNX $5.00”. Transportationcost reimbursement for components or parts will bethe actual surface freight charge for shipment of thecomponent or part or the currently published UPSsurface rate schedule, whichever is less.
2. TCM reserves the right at its option to replace anydefective engine or part with either a new or rebuiltengine or part.
3. Repair or replacement of any engine or part under thiswarranty will not extend the period of warranty cover-age set forth above.
4. This warranty applies only to engines in which partsmanufactured or supplied by TCM or parts manufac-tured pursuant to an FAA Parts ManufacturerApproval have been used and nothing containedherein should be construed as a warranty by TCM ofany engine or part not manufactured or supplied byTCM. TCM accepts no responsibility for the failure ofany engine or part which it does not manufacture orsupply or damage resulting from such failure.
5. This warranty applies only to engines which havebeen installed, inspected, and maintained in accor-dance with the instructions for continued airworthi-ness, including compliance with all applicable servicebulletins issued by TCM, the aircraft manufacturer, orany accessory or component manufacturer.Performance of recommended inspections and main-tenance must be documented by appropriate logbookentries and the logbook must accompany any enginebeing returned for warranty consideration.
6. This warranty does not apply to any engine, compo-nent, or part manufactured or supplied by TCM which(1) has been subject to misuse, neglect, or accident;(2) has been installed, repaired, maintained, oraltered in any way that in the judgment of TCM hasadversely affected the condition of the engine; (3)has been operated inconsistent with TCM and aircraft
manufacturer recommendations and limitations (suchas, but not limited to engine RPM, temperature, man-ifold pressure, fuel flow, and proper system adjust-ment); or (4) has been changed from its original FAAcertificated configuration.
7. TCM will not be responsible for repair or replacementof any engine, component, or part damaged or wornas a result of corrosion, pre-ignition/detonation, oper-ation with non-calibrated engine gauges, improperfuel system adjustment, non-TCM approved fuel andoil grades or additives, or installation of parts, com-ponents, or accessories that alter the engine’s origi-nal type design.
8. The provisions of this warranty do not apply to normalmaintenance service (such as engine tuneups,adjustments, inspections, engine or component over-haul resulting from time between overhaul (TBO) rec-ommendations, etc.) or to the replacement of normalservice items (such as spark plugs, filters, hoses,belts, etc.).
9. TCM reserves the right to change any engine or partspecifications or prices without incurring any respon-sibility with regard to engines or parts previously soldor replaced.
10. THIS WARRANTY IS A WARRANTY TO REPAIROR REPLACE AND NOT A WARRANTY OF THECONDITION OR FUTURE PERFORMANCE OFTHE PRODUCTS WHICH IT COVERS. THERE ARENO OTHER WARRANTIES, EXPRESSED ORIMPLIED, SPECIFICALLY, BUT WITHOUT LIMITA-TION, THERE ARE NO IMPLIED WARRANTIES OFMERCHANTABILITY OR FITNESS FOR A PARTIC-ULAR PURPOSE. IN NO EVENT WILL TCM BERESPONSIBLE FOR ANY INCIDENTAL OR CON-SEQUENTIAL DAMAGES ARISING OUT OF ANYDEFECT IN ANY ENGINE OR PART, ARISING OUTOF THE FAILURE OF ANY ENGINE OR PART TOOPERATE PROPERLY, OR ARISING OUT OF ANYBREACH OF THE WARRANTY MADE HEREIN. NOPERSON IS AUTHORIZED TO GIVE ANY OTHERWARRANTY OR TO ASSUME ANY ADDITIONALOBLIGATION OR LIABILITY ON BEHALF OF TCM.
13.4 McCauley Propeller Systems Standard LimitedWarranty
April 2013
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1 3 . L IM I TED WARRANT I ES ( C on t i n u ed )
McCauley Propeller Systems, a Division of CessnaAircraft Company, Wichita, Kansas, U.S.A., expresslywarrants new and remanufactured products producedand sold by McCauley to be free from defects in materi-al and workmanship under normal use and service for aperiod of thirty-six (36) months after delivery to the orig-inal retail purchaser or until the expiration of the maxi-mum hours of use or calendar limits for overhaul pub-lished by McCauley for the subject product, whicheveroccurs first.McCauley’s obligation under this limited warranty is lim-ited to repairing or replacing, at its sole option, any pro-peller, propeller parts, governor, or governor parts deter-mined by McCauley to have been defective and whichare properly returned by the owner, with a written state-ment describing the alleged defect, to any McCauleyAuthorized Service Center authorized to service the indi-vidual McCauley product. The repair or replacement ofdefective parts will be made without charge to the ownerfor parts or labor for removal and installation, exceptimport duties and/or sales or use taxes, if any, which aresolely the owner’s responsibility. McCauley will warrant apart replaced pursuant to this limited warranty under thesame terms as the original part for the remainder of theapplicable warranty period of the original part. This limit-ed warranty is not intended to and does not cover thecosts of normal maintenance of overhaul.In addition, McCauley will repair or replace, at its option,any propeller, propeller parts, governor, or governorparts requiring replacement due to manufacturing defectif found at or before the first recommended overhaulinterval as described in McCauley published serviceinformation. This first overhaul coverage does notinclude labor, standard overhaul replacement parts,parts repairable via published service information (re-plating, painting, etc.), other costs associated with thepropeller or governor overhaul, or import duties and/orsales or use taxes, nor does it apply to defects foundafter McCauley published overhaul hour or calendar lim-its. The provisions of this limited warranty do not applyto: any McCauley parts which have been subject to mis-use, negligence, or accident or which have beenrepaired or altered in any way that, in the sole judgmentof McCauley, adversely affects their performance, stabil-ity, or reliability; to normal maintenance services (suchas cleaning, mechanical adjustments, and maintenanceinspections); to the replacement of service items madein connection with normal maintenance; to normal dete-rioration of soft trim and appearance items (such aspaint and rubber-like items) due to wear and exposure;to propellers, governors, or parts found defective beyondthe McCauley recommended overhaul period; or to partswhich have been improperly installed by entities otherthan McCauley and/or McCauley Authorized ServiceCenters.The McCauley limited warranty is void on any new or
remanufactured product installed, without McCauley’sprior written approval on a non-type certificated engine,or on any engine which has received an overhaul ormodification which is not approved by the engine manu-facturer and that results in a change to the vibratoryenvironment of the engine such as, but not limited to, analteration of horsepower, operating RPM, crankshaftdamper configuration, compression ratio, magneto tim-ing, camshaft design, or any other overhaul or modifica-tion not expressly approved by the original engine man-ufacturer. The McCauley limited warranty is also void onany McCauley product shipped new from the factory ordistributor in disassembled state, then later re-assem-bled by an unauthorized party. Parties authorized to re-assemble factory-new product must have specific writ-ten permission from McCauley to do so, otherwise allMcCauley warranty on the affected unit is void. NoMcCauley warranty coverage is offered for leakage onproduct assembled outside McCauley, regardless of theassembling party.To the extent allowed by applicable law, THIS WAR-RANTY IS EXPRESSLY IN LIEU OF ANY OTHERWARRANTIES, EXPRESSED OR IMPLIED IN FACTOR BY LAW, INCLUDING ANY IMPLIED WARRANTYOF MERCHANTABILITY OR FITNESS FOR A PAR-TICULAR PURPOSE. THE REMEDIES OF REPAIR ORREPLACEMENT SET FORTH HEREIN ARE THEONLY REMEDIES UNDER THIS LIMITED WARRAN-TY. McCAULEY DISCLAIMS ANY OBLIGATION ORLIABILITY, WHETHER IN CONTRACT OR IN TORT ,INCLUDING LOSS OF USE OF THE PRODUCT WAR-RANTED, LOSS OF TIME, INCONVENIENCE, LOSSOF PROFITS, COMMERCIAL LOSS, OR ANY OTHERDIRECT, CONSEQUENTIAL, SPECIAL, OR INCIDEN-TAL DAMAGES. THIS WARRANTY IS IN LIEU OFANY OBLIGATION OR LIABILITY ON THE PART OFMcCAULEY TO ANYONE OF ANY NATURE WHAT-SOEVER BY REASON OF THE MANUFACTURE,SALE, LEASE, OR USE OF THE WARRANTEDPRODUCTS AND McCAULEY NEITHER ASSUMESNOR AUTHORIZES ANYONE TO ASSUME FOR ITANY OTHER OBLIGATION OR LIABILITY IN CON-NECTION WITH SUCH WARRANTED PRODUCTS.THE UNITED NATIONS CONVENTION ON CON-TRACTS FOR THE INTERNATIONAL SALE OFGOODS, 1980, AND ANY SUCCESSOR THERETO, ISEXPRESSLY EXCLUDED FROM THIS WARRANTY.Issued 9/1/2003
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April 2013
1 3 . L IM I TED WARRANT I ES ( C on t i n u ed )13.5 Cessna Skycatcher Model 162 Paint Warranty
Cessna endeavors to select and use high qualitypolyurethane paints from leading manufacturers.Polyurethane paints are used because of their highgloss characteristics and ability to withstand dramatictemperature and pressure changes. The paint on yournew aircraft will maintain its high gloss characteristics foran extended period of time provided it is cared for prop-erly.
The painted exterior surfaces require an initial curingperiod which may be as long as ninety (90) days afterthe finish is applied. During this curing period, some pre-cautions should be taken to avoid damaging the finish orinterfering with the curing process. The finish should becleaned only by washing with clean water and mild soap,followed by a water rinse, and drying with a cloth orchamois. Do not use polish or wax which would excludeair from the surface during this ninety (90) day curingperiod. Once the finish has cured completely, it may bewaxed with a quality automotive wax, but power buffingshould be avoided to prevent damage to the paint sur-face.
Normal paint maintenance will include, but is not limitedto touchup of abrasion and wear of the paint on screwsheads, around access panels, wing leading edges, ver-tical and horizontal stabilizer leading edges, windshieldretainers, and other leading edge surfaces includingparts on the landing gear subject to damage or erosionfrom airborne particles. Proper maintenance includeskeeping surfaces clean, polished, and touching upchipped or eroded areas to prevent further damage andcorrosion.
Paint and graphics warranty applies only to defects inmaterial and workmanship for a period of one (1) year or1,000 hours (whichever occurs first) from the warrantystart date. Deterioration of paint and graphics due to nor-mal wear, exposure, or improper care is not covered bythe warranty. If proper paint maintenance procedureshave been followed and paint peeling, blistering, orcracking is evident in areas other than immediate lead-ing edge surfaces, warranty consideration may berequested thorough a Cessna Service Station.
Generally speaking, warranty repair of paint is confinedto a limited surface area. Workmanship or materialdefects can usually be identified to localized surfaceareas that were improperly prepared prior to paint appli-
cation, or to areas where the paint or subsurface primerhas been improperly applied.
Complete strip and repaint of an entire airplane canONLY be authorized if there is evidence of paint defectson several major surface areas of the aircraft. Contactyour Cessna Field Service Engineer concerning paintdefects on any major surface of an aircraft.
Cessna Single Engine Piston Aircraft, 2625 S. Hoover Rd, Wichita, Kansas 67215, Telefax 316-517-2772