CESSNA 350 Specification and Description

Cessna 350 is a pre-molded, composite built, semi- monocoque, four seat, single engine, low wing, tricycle design airplane. Suitable allowance for luggage is pro- vided. 1.1 Certification The Cessna 350 is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 through amendment 23-46, including day, night, VFR and IFR. 1.2 Approximate Dimensions Overall Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 ft 0 in (2.74m) Overall Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 ft 2 in (7.68m) Wing Span (overall) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 ft 10 in (10.92 m) Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 141.2 sq ft (13.1sq m) Cabin Height (max) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 in (124.5 cm) Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 in (124.5 cm) Length (firewall to aft limit of baggage compartment) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 140 in (354.6 cm) Cabin Door Minimum Entry Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .33 in (83.8 cm) Minimum Entry Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 in (83.8 cm) Maximum Entry Clearance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46 in (116.8 cm) Baggage Compartment Maximum Baggage Compartment Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .39 in (97.8 cm) Maximum Baggage Compartment Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .52 in (132 cm) (Including Shelf) Maximum Baggage Compartment Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .35 in (87.6 cm) Maximum Baggage Entry Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .28 in (71.1 cm) (Diagonal Measurement) 4 CESSNA 350 June 2008, Revision B FIGURE I — CESSNA 350 EXTERIOR DIMENSIONS 9’ -0” 25’ -2” 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) 35’ -10” 14’ -3” 5 CESSNA 350 June 2008, Revision B FIGURE II — CESSNA 350 INTERIOR DIMENSIONS 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) 49” (124.5 cm) Firewall Baggage Shelf 140” (354.6 cm) Cabin Height Dimensions 35” (87.6 cm) Cabin Width Dimensions 49” (124.5 cm) 39” (97.8 cm) 28” (71.1 cm) 52” (132 cm) Baggage Shelf Firewall 6 CESSNA 350 June 2008, Revision B 1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d ) 1.3 Design Weight and Capacities Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,400 lbs (1,542 kg) Maximum Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3,400 lbs (1,542 kg) Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3,230 lbs (1,465 kg) Standard Empty Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,475 lbs (1,123 kg) Maximum Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .925 lbs (420 kg) Baggage Allowance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .120 lbs (54.4 kg) Fuel Capacity Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .106 gal (401 L) Total Useable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .102 gal (386 L) Total Capacity each Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .53 gal (201 L) Oil Capacity Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 qts (7.6 L) Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10 qts (9.5 L) 7 CESSNA 350 June 2008, Revision B 2 . P E R F O R M A N C E Service Ceiling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18,000 ft Takeoff Distance Ground Roll (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,300 ft Takeoff Distance To Clear 50 ft Obstacle (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,300 ft Max Climb Rate (S.L., ISA, MTOW) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,225 fpm Max Speed ( Max at 8,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .191 kts / 220 mph Economy Cruise Speed (55% at 12,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .158 kts / 182 mph Range at Max Cruise Speed (Max at 12,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,130 nm Range at Economy Cruise Speed (55% at 12,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,395 nm Landing Distance Ground Roll (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,550 ft Landing Distance To Clear 50 ft Obstacle (S.L.) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,350 ft All estimated performance data are based on airplane weights at 3,400 pounds; standard atmospheric condi- tions; level, hard surface, dry runways; and no wind. They are calculated values derived from flight tests under carefully documented conditions and will vary with individual airplanes, pilots, and numerous other factors affecting flight performance. 3 . P O W E R P L A N T & A C C E S S O R I E S z Teledyne Continental IO-550-N Engine z 310 HP @2700 RPM z Certified for 100LL & 100 Fuel z Fuel Injection System z High-Pressure Wet-Sump Oil System z Oil Cooler z Induction Air Filter z Full Flow Oil Filter z Throttle Control - Vernier z Mixture Control - Vernier z Propeller Control - Vernier z Dual Ignition System z Dual Engine Exhaust Muffler z McCauley Constant Speed, 3 Blade Metal Propeller with Blade Heaters z Propeller Governor z Propeller Heat Module with Harness z Propeller Spinner, Polished z Electric Starter 8 CESSNA 350 June 2008, Revision B z GMA-1347 Digital Audio Panel w/Marker Beacon/Intercom z GCU-476 Keypad Controller z GTX-33 Transponder-Mode S w-TIS z GIA-63W NAV/COM/GPS/WAAS w/GS #1 z GIA-63W NAV/COM/GPS/WAAS w/GS #2 z GDU-1040 Primary Flight Display (PFD) z GDU-1044 Multi-Function Display (MFD) z GEA-71 Engine/Airframe Computer z GRS-77 AHRS z GDC-74A Air Data Computer w/OAT Probe z GMU-44 Magnetometer z GDL-69A Flight Information System (FIS) w/XM Radio z GFC-700 Autopilot • Go-Around Switch • Electric Trim • A/P Disconnect • Control Wheel Steering Button z E-Prox+ TM - Terrain Awareness System z Garmin SafeTaxi & FliteCharts (FliteCharts do not provide Geosynchronous Positioning) z T-WatchTM Traffic Advisory System z Backup Airspeed, Altimeter and Attitude (electric) Indicator z Control Stick Push-To-Talk Switch-Pilot/Copilot z Mic & Phone Jacks-Pilot/Copilot/Passengers (Bose and Standard) z Antennas: • Marker Beacon Antenna • Transponder Antenna • WAAS (1) • GPS / XM Antenna (1) • COMM Antenna (2) • NAV Antenna z Artex ELT-ME406 Emergency Locator Transmitter z Pitot System - Heated z Static System z Alternate Static Source 4 . C E S S N A 3 5 0 E Q U I P M E N T L I S T The following list of equipment is included on the stan- dard aircraft and it does not reflect optional equipment. GARMIN G1000 Avionics Package 9 CESSNA 350 June 2008, Revision B 5 . I N S T R U M E N T PA N E L 1. Primer Switch 2. Ignition Switch 3. Backup Altimeter 4. Pitot Heat, Door Seals, and Optional Switches 5. Backup Attitude Indicator 6. Backup Airspeed Indicator 7. Primary Flight Display (PFD) 8. Audio Panel 9. Multi-Function Display (MFD) 10. Autopilot Controls 11. ELT Remote Switch 12. Air Vents (2) 13. Flap Panel – Flap Switch and Annunciator 14. Engine Controls 15. Automatic Climate Control System (ACCS) Panel 16. Heated Induction Air 17. Alternate Static Air 18. Go Around Switch 19. Rocker Switches: Backup Fuel Pump and Vapor Suppression FIGURE III — CESSNA 350 INSTRUMENT PANEL 2 16 1 17 18 3 4 5 6 7 8 10 9 11 1213 14 15 19 Push To Talk Switch Autopilot Disconnect/Trim Interrupt Switch Trim Switch Control Wheel Steering Switch (CWS) GCU-476 Keypad Controller 10 CESSNA 350 June 2008, Revision B 6 . E L E C T R I C A L P O W E R z Belt Driven Alternator, 28 Volts, 70 amps rated z Gear Driven Alternator, 28 Volts, 70 amps rated z Dual 28 Volt, 8.5 AH Batteries z Dual Voltage Regulators, 28 Volt z Cross-Tie ability during alternator failure z Cold Weather starting ability with either Battery or both Batteries z Digital Ammeter displaying either Both Batteries or Alternator Conditions on MFD z Overhead Master Switch Panel z Dual 12 Volt, 2 amp Auxiliary Power Outlets z External Ground Power Plug 7 . E N G I N E I N D I C AT I N G S Y S T E M z Ammeter z Voltmeter z Manifold Pressure z Oil Pressure and Temperature z Tachometer - Hour Recorder z Fuel Flow (GPH) z LH/RH Fuel Quantity z CHT - Cylinder Head Temperature (6) z EGT - Exhaust Gas Temperature (6) z Annunciation – Caution and Warning Alerts (PFD) 11 CESSNA 350 June 2008, Revision B 9 . E X T E R I O R z Fiberglass and Honeycomb Structure z LH and RH Gull Wing Style Doors w/Lock and Key z Remote Keyless Entry with Automatic Light System z Pneumatic Door Seal System z LH Cargo Door, w/Lock and Key z Fixed Landing Gear w/castering Nose Wheel z Lighted Entrance Step z Entry Assist and Exit Handles z Main Gear Fairings z Nose Gear and Strut Fairings z Tie Down Rings, LH/RH Wing & Tail z Tube Type Tires • Nose – 5.00 X 5 • Mains - 15x6.00 X 6 z Static Wicks (9) z Emergency Exterior Door Release z Rear Tinted Passenger Window z Automatic Climate Control System (ACCS) z Precise Flight TM Semi-Portable Oxygen System z Individual Eyeball Vents z Floor Vent System z Defrosting System z Insulation / Soundproofing 8 . E N V I R O N M E N T A L z Navigation, LH/RH Wing Tip z Wing Tip Strobe, LH/RH z Taxi Lights, LH Wing - HID z Landing Light - HID 1 0 . E X T E R I O R L I G H T S 12 CESSNA 350 June 2008, Revision B z Dual Hydraulic Brakes, Toe-Operated z Parking Brake z Dual Flight Controls - Aileron/Elevator/Rudder z Precise Flight Speedbrake TM 2000 System z LH/RH Control Sticks, All Purpose Pilot/Copilot z Pilot Control Stick • Pitch Trim • AP Disconnect • Control Wheel Steering Button z Go-Around Switch z Electric Elevator/Aileron Trim z Rudder Limiter System 1 1 . F L I G H T C O N T R O L S z Electric Auxiliary Fuel Pump z Engine Driven Fuel Pump z Integral Wet Wing Fuel Tanks, 102 Gal. Usable z Fuel Selector Valve, Left//Right/Off z Fuel Strainer, Incorporated with Fuselage Quick Drain z Fuel Tank Quick Drain z Fuel Sampler Cup z Fuel Vapor Suppression System 1 2 . F U E L S Y S T E M z Pilot and Copilot Control Stick (2) z Pilot and Copilot Cupholders z Front Seat Eyeball Fresh Air Vents (2) z Rear Seat Eyeball Fresh Air Vents (2) z Air Conditioned, Controllable Air Vents (6) z Reclining Sport Seats z Rear Seat and Seatback Cushion z Pilot’s and Copilots Three Point Restraint System z Rear Seat Passengers Three Point Restraint System z Baggage Tie Downs and Restraining Net z Fire Extinguisher and Mounting Bracket z Pilot's Check List z Pilot's Operating Handbook z Instrument Panel Glareshield z Center Console Storage Area z Radio Call Plate z Console Headset Hanger and Flashlight Holder z Rear Passenger Entry/Exit Assist Strap 1 3 . I N T E R I O R 13 CESSNA 350 June 2008, Revision B z Pilot/Copilot Cabin Overhead Flip Lights z Overhead Reading Lights (4) z Interior Lights Dimming Control z LED Instrument Flood Bar z Sub-Panel /Switch Panel Lighting (Backlighted) • GCU-476 Keypad Controller • Pitot Heat • Door Seals • Optional Equipment Switches • Flap Panel • Position Bar • Slide Dimmer Labels • Master Switches • Circuit Breaker panel z LCD Lighted Glass Panel Displays: • Electronic Flight Instruments • Electronic Avionics Instruments • Electronic Engine Instruments z Backup Attitude, Altimeter, Airspeed Internally Lighted 1 4 . I N T E R I O R L I G H T I N G 1 5 . E X T E R I O R S T R I P I N G O P T I O N S z As defined on Purchase Agreement 14 CESSNA 350 June 2008, Revision B 1 6 . L I M I T E D W A R R A N T Y 16.1 Cessna’s Limited Warranty - Single Engine Piston Aircraft Cessna warrants the aircraft and all parts included there- in to be free from defects in material and workmanship under normal use and service for a period of twenty-four (24) months after delivery to the original retail purchaser or first user, except as hereafter noted. Engines, engine part accessories, avionics, batteries, propellers and gov- ernors are specifically excluded from this limited war- ranty. Spare parts sold by Cessna, excluding engine part accessories, avionics and batteries are warranted for six (6) months after installation, except as hereafter noted. Paint is covered by a separate one (1) year war- ranty as defined in 16.2. Cessna's obligation under this warranty is limited to repairing or replacing, at its option, with exchange, over- hauled, or new parts, items found defective by Cessna's examination which are returned at the owner's expense within the applicable twenty-four (24) or six (6) month period (for spare parts only) to any authorized Cessna Service Station. A new warranty period is not estab- lished for replacement parts. Replacement parts are warranted only for the remainder of the applicable twen- ty-four (24) or six (6) month original warranty period. The repair or replacement of defective parts under this limited warranty will be made without charge to the owner for parts and labor for removal, installation and/or actual repair, except that the owner shall pay all import duties, and sales and use taxes on replacements and repairs. This limited warranty does not apply to parts subjected to misuse, negligence, improper installation, accident, alteration; repairs not authorized by Cessna; normal maintenance services (cleaning, control rigging, brake and other mechanical adjustments, maintenance inspections, etc.); replacement of service items (light bulbs, brake linings, filters, hoses, tires, cowl mounts, etc.); or to normal deterioration of soft trim or appear- ance items (upholstery, rubber-like items, etc.) due to corrosion, delamination, wear and exposure. TO THE EXTENT ALLOWED BY APPLICABLE LAW, THIS LIMITED WARRANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EXPRESSED OR IMPLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT, AS ABOVE SET FORTH, ARE THE ONLY REMEDIES UNDER THIS LIMITED WARRANTY. CESSNA DIS- CLAIMS ANY OBLIGATION OR LIABILITY WHETHER IN CONTRACT OR IN TORT (AND WHETHER FOR NEGLIGENCE, STRICT LIABILITY, PRODUCT LIA- BILITY OR OTHERWISE), INCLUDING LOSS OF USE OF THE PRODUCT WARRANTED, LOSS OF TIME, INCONVENIENCE, COMMERCIAL LOSS OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL OR INCIDENTAL DAMAGES. THIS WARRANTY IS IN LIEU OF ANY OTHER OBLIGATION OR LIABILITY OF CESSNA OF ANY NATURE WHATSOEVER BY REA- SON OF THE MANUFACTURE, SALE OR LEASE OF SUCH AIRCRAFT PRODUCTS AND CESSNA NEI- THER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIA- BILITY IN CONNECTION WITH SUCH AIRCRAFT PRODUCTS. COMPLIANCE AND/OR TIMELY COM- PLIANCE WITH THIS LIMITED WARRANTY MAY BE AFFECTED IF EXPORT LICENSES ARE REQUIRED TO BE REQUESTED AND APPROVED BEFORE SPARE PARTS CAN BE SHIPPED TO CERTAIN FOR- EIGN COUNTRIES. 16.2 Aircraft Paint And Graphics - Single Engine Piston Aircraft Cessna endeavors to select and use high quality polyurethane paints from the leading manufacturers. Polyurethane paints and graphics are used because of their high gloss characteristics and ability to withstand dramatic temperature and pressure changes. The paint on your new aircraft will maintain its high gloss charac- teristics for an extended period of time provided it is cared for properly. The painted exterior surfaces require an initial curing period which may be as long as ninety (90) days after the finish is applied. During this curing period, some pre- cautions should be taken to avoid damaging the finish or interfering with the curing process. The finish should be cleaned only by washing with clean water and mild soap, followed by a water rinse and drying with a cloth or chamois. Do not use polish or wax, which would exclude air from the surface, during this ninety (90) day curing period. Once the finish has cured completely, it may be waxed with a good automotive wax, but power buffing should be avoided to prevent damage to the paint sur- face. Normal paint maintenance will include but is not limited to; touchup of abrasion and wear of the paint on screws heads, around access panels, the radome, wing leading edges, vertical and horizontal stabilizer leading edges, windshield retainers and other leading edge surfaces including parts on the landing gear subject to damage or erosion from airborne particles. Proper maintenance includes keeping surfaces clean, polished, and touching up chipped or eroded areas to prevent further damage and corrosion. Paint and graphics warranty applies only to defects in material and workmanship for a period of one (1) year from the Warranty Start Date. Deterioration of paint and graphics due to normal wear, exposure, or improper care is not covered by the warranty. If proper paint main- tenance procedures have been followed and paint peel- ing, blistering or cracking is evident in areas other than 15 CESSNA 350 June 2008, Revision B immediate leading edge surfaces, warranty considera- tion may be requested thorough a Cessna Service Station. Generally speaking, warranty repair of paint is confined to a limited surface area. Workmanship or material defects can usually be identified to localized surface areas that were improperly prepared prior to paint appli- cation, or to areas where the paint or subsurface primer has been improperly applied. Complete strip and repaint of an entire airplane can ONLY be authorized if there is evidence of paint defects on several major surface areas of the aircraft. Contact your Cessna Field Service Engineer concerning paint defects on any major surface of an aircraft. 16.3 Teledyne Continental Motors - Platinum Engine Warranty Each Platinum aircraft engine shipped from Teledyne Continental Motors' plant on or after August 1, 1999 is warranted as follows: 1. (a) For a period of twenty-four (24) months or until expiration of the recommended Time Between Overhaul (TBO) of the engine covered by this warranty, whichev- er occurs first, after the warranty activation date Teledyne Continental Motors (TCM) will at its option repair or replace on an exchange basis any engine, component or part manufactured or supplied by it which within the applicable twentyfour (24) month or TBO peri- od is returned to a TCM representative authorized to handle the engine covered by this warranty and which upon examination is found to the satisfaction of TCM to be defective in material or workmanship. The warranty activation date is the date the engine is first operated for any use or the 180th day after TCM’s invoice date, whichever occurs first. (b) TCM will pay for reasonable labor costs associated with repairs or replacements under paragraph 1(a) under this warranty and for "troubleshooting" costs asso- ciated with identifying the need for such repairs or replacements when coordinated through an authorized TCM representative. The amount of repair and replace- ment labor costs allowed will be in accordance with the latest revision of the warranty labor allowance schedule, Form X30552, published by TCM. The amount of "trou- bleshooting" costs allowed will be the reasonable costs under the circumstances of identifying the need for such repairs or replacements, but in no event will the "trou- bleshooting" costs allowed exceed fifteen percent (15%) of the labor costs associated with such repairs or replacements allowed by TCM. No "troubleshooting" cost allowance will be made where the need for repairs or replacements is identified in the course of overhaul, routine maintenance or on the basis of an obvious defect. (c) TCM will pay transportation costs in connection with the repair or replacement of any engine, component or part found to the satisfaction of TCM to be defective in material or workmanship under paragraph 1(a) of this warranty. The engine, component or part must be shipped prepaid to the repair facility designated by TCM. Transportation cost reimbursements for engines will be the actual surface freight charge or $500.00, whichever is less. Engines must be described on the bill of lading as follows: “Internal combustion engine, other than Radial Cyl RVNX $5.00”. Transportation cost reimburse- ment for components or parts will be the actual surface freight charge for shipment of the component or part or the currently published UPS surface rate schedule, whichever is less. 2. (a) After the expiration of the applicable twenty-four (24) month period described above and before the expi- ration of an additional thirty-six (36) month period or expiration of the applicable recommended TBO for the engine covered by this warranty, whichever occurs first, TCM will, except as excluded below, at its option repair or replace on an exchange basis any component or part manufactured or supplied by it which is found to the sat- isfaction of TCM to be defective in material or workman- ship. During this period TCM reserves the right at its option to replace the defective component or part with either a new or rebuilt engine or part. During this period TCM will not assume any responsibility for the repair or replacement of engine accessories, i.e. parts which have been purchased by TCM from a manufacturer as a complete and finished unit and included in the assembly of an engine without altering the unit, including, but not limited to Unison R magnetos and harnesses, Precision Airmotive Corporation R carburetors and fuel controls, Electrosystems R starters and alternators and Alliedsignal R and Consolidated Fuel Systems R tur- bochargers. During this period such engine accessories will be subject to such warranty coverage as may be provided by their manufacturer. (b) In the event that TCM elects to repair in the field, rather than replace, any component or part under para- graph 2(a) of this warranty, TCM will pay labor costs for the repair of the component or part only. The amount of repair labor costs allowed will be in accordance with the latest revision of the warranty labor allowance schedule, Form X30552, published by TCM. TCM will not assume any responsibility for labor costs for the removal and/or re-installation of the engine or part, costs associated with “troubleshooting” or any other labor costs associat- ed with repairs or replacements under paragraph 2(a) of this warranty. (c) TCM will not assume any responsibility for trans- portation costs associated with repairs or replacements under paragraph 2(a) of this warranty. 3. The coverage under this warranty applicable to cylin- 1 6 . L I M I T E D W A R R A N T Y ( C o n t i n u e d ) 16 CESSNA 350 June 2008, Revision B der assemblies and related parts shall be subject to the terms, conditions and limitations set forth in the applica- ble TCM TopCare SM Cylinder Warranty. 4. Repair or replacement of any engine or part under this warranty will not extend the period of warranty coverage set forth above. 5. This warranty applies only to engines in which parts manufactured or supplied by TCM or parts manufac- tured pursuant to an FAA Parts Manufacturer Approval have been used and nothing contained herein should be construed as a warranty by TCM of any engine or part not manufactured or supplied by TCM. TCM accepts no responsibility for the failure of any engine or part which it does not manufacture or supply or damage resulting from such damage. 6. This warranty applies only to engines which have been installed, inspected and maintained in accordance with the instructions for continued airworthiness, includ- ing compliance with all applicable service bulletins, issued by TCM, the aircraft manufacturer or any acces- sory or component manufacturer. Performance of rec- ommended inspections and maintenance must be docu- mented by appropriate logbook entries and the logbook must accompany any engine being returned for warran- ty consideration. 7. 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 or altered in any way that in the judgment of TCM has adversely affected the condition of the engine; (3) has been operated incon- sistent with TCM and aircraft manufacturer recommen- dations and limitations (such as, but not limited to engine RPM, temperature, manifold pressure, fuel flow and proper system adjustment) or (4) has been changed from its original FAA certificated configuration. 8. TCM will not be responsible for repair or replacement of any engine, component or part damaged or worn as a result of corrosion, pre-ignition/detonation, operation with non-calibrated engine gauges, improper fuel sys- tem adjustment, non-TCM approved fuel and oil grades or additives or installation of parts, components or accessories that alter the engine’s original type design. 9. The provisions of this warranty do not apply to normal maintenance service (such as engine tune-ups, adjust- ments, inspections, engine or component overhaul resulting from time between overhaul (TBO) recommen- dations, etc.) or to the replacement of normal service items (such as spark plugs, filters, hoses, belts, etc.). 10. TCM reserves the right to change any engine or part specifications or prices without incurring any responsi- bility with regard to engines or parts previously sold or replaced. 11. THIS WARRANTY IS A WARRANTY TO REPAIR OR REPLACE AND NOT A WARRANTY OF THE CONDITION OR FUTURE PERFORMANCE OF THE PRODUCTS WHICH IT COVERS. THERE ARE NO OTHER WARRANTIES, EXPRESSED OR IMPLIED, SPECIFICALLY, BUT WITHOUT LIMITATION, THERE ARE NO IMPLIED WARRANTIES OF MER- CHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. IN NO EVENT WILL TCM BE RESPONSI- BLE FOR ANY INCIDENTAL OR CONSEQUENTIAL DAMAGES ARISING OUT OF ANY DEFECT IN ANY ENGINE OR PART, ARISING OUT OF THE FAILURE OF ANY ENGINE OR PART TO OPERATE PROPER- LY, OR ARISING OUT OF ANY BREACH OF THE WARRANTY MADE HEREIN. No person is authorized to give any other warranty or to assume any addi- tional obligation or liability on behalf of TCM. 16.4 McCauley Propeller Systems - Standard Limited Warranty McCauley Propeller Systems, a Division of Cessna Aircraft Company, Wichita, Kansas, U.S.A., expressly warrants new and remanufactured products produced and sold by McCauley to be free from defects in materi- al and workmanship under normal use and service for a period 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, whichever occurs 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 which are properly returned by the owner, with a written state- ment describing the alleged defect, to any McCauley Authorized Service Center authorized to service the indi- vidual McCauley product. The repair or replacement of defective parts will be made without charge to the owner for parts, or labor for removal and installation, except export/import duties, and/or sales or use taxes, if any which are solely the owner’s responsibility. McCauley will warrant a part replaced pursuant to this limited war- ranty under the same terms as the original part for the remainder of he applicable warranty period of the origi- nal part. This limited warranty is not intended to and does not cover the costs of normal maintenance of over- haul. In addition, McCauley will repair or replace, at its option, any propeller, propeller parts, governor, or governor parts requiring replacement due to manufacturing defect if found at or before the first recommended overhaul interval as described in McCauley published service information. This first overhaul coverage does not include labor, standard overhaul replacement parts, parts repairable via published service information (re- plating, painting, etc.), other costs associated with the 1 6 . L I M I T E D W A R R A N T Y ( C o n t i n u e d ) 17 CESSNA 350 June 2008, Revision B propeller or governor overhaul, or export/import duties, and/or sales or use taxes, nor does it apply to defects found after McCauley published overhaul hour or calen- dar limits. The provisions of this limited warranty do not apply to: any McCauley parts which have been subject to misuse, negligence or accident or which have been repaired or altered in any way that, in the sole judgment of McCauley, adversely affects their performance, stabil- ity or reliability; to normal maintenance services (such as cleaning, mechanical adjustments and maintenance inspections); to the replacement of service items made in connection with normal maintenance; to normal dete- rioration of soft trim and appearance items (such as paint and rubber-like items) due to wear and exposure; to propellers, governors or parts found defective beyond the McCauley recommended overhaul period; or to parts which have been improperly installed by entities other than McCauley and/or McCauley Authorized Service Centers. The McCauley limited warranty is void on any new or remanufactured product installed, without McCauley’s prior written approval, on a non-type certificated engine, or on any engine which has received an overhaul or modification which is not approved by the engine manu- facturer and that results in a change to the vibratory environment of the engine such as, but not limited to, an alteration of horsepower, operating RPM, crankshaft damper 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 on any McCauley product shipped new from the factory or distributor 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 all McCauley warranty on the affected unit is void. No McCauley warranty coverage is offered for leakage on product assembled outside McCauley, regardless of the assembling party. To the extent allowed by applicable law, THIS WAR- RANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EXPRESSED OR IMPLIED IN FACT OR BY LAW, INCLUDING ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PAR- TICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT SET FORTH HEREIN ARE THE ONLY REMEDIES UNDER THIS LIMITED WARRAN- TY. McCAULEY DISCLAIMS ANY OBLIGATION OR LIABILITY, WHETHER IN CONTRACT OR IN TORT , INCLUDING LOSS OF USE OF THE PRODUCT WAR- RANTED, LOSS OF TIME, INCONVENIENCE, LOSS OF PROFITS, COMMERCIAL LOSS, OR ANY OTHER DIRECT, CONSEQUENTIAL, SPECIAL, OR INCIDEN- TAL DAMAGES. THIS WARRANTY IS IN LIEU OF ANY OBLIGATION OR LIABILITY ON THE PART OF McCAULEY TO ANYONE OF ANY NATURE WHAT- SOEVER BY REASON OF THE MANUFACTURE, SALE, LEASE, OR USE OF THE WARRANTED PRODUCTS AND McCAULEY NEITHER ASSUMES NOR AUTHORIZES ANYONE TO ASSUME FOR IT ANY OTHER OBLIGATION OR LIABILITY IN CON- NECTION WITH SUCH WARRANTED PRODUCTS. THE UNITED NATIONS CONVENTION ON CON- TRACTS FOR THE INTERNATIONAL SALE OF GOODS, 1980, AND ANY SUCCESSOR THERETO, IS EXPRESSLY EXCLUDED FROM THIS WARRANTY. 16.5 Garmin Avionics - (Limited) Warranty Aircraft OEM-Installed Avionics 2-Year Limited Warranty Policy This GARMIN Product is warranted to be free from defects in materials or workmanship for two years from the date of warranty activation. Within this period, GARMIN International, Inc. will at its sole option, repair or replace any components which fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided that the cus- tomer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, mis- use, accident or unauthorized alteration or repairs. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSE- QUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PROD- UCT. Some states do not allow the exclusion of inciden- tal or consequential damages, so the above limitations may not apply to you. GARMIN retains the exclusive right to repair or replace the product or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. To obtain warranty service, contact your local GARMIN authorized Service Center. For assistance in locating a Service Center near you, call GARMIN Customer Service at one of the numbers shown below. 1 6 . L I M I T E D W A R R A N T Y ( C o n t i n u e d ) 18 CESSNA 350 June 2008, Revision B GARMIN International 1200 East 151st Street Olathe, Kansas 66062, U.S.A. Toll free: 1-800-800-1020 Phone: 1-913-397-8200 FAX: 1-913-397-0836 GARMIN (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9AQ, U.K. Phone: 44-1794-519944 FAX: 44-1794-519222 Visit our web site at: www.garmin.com 1 6 . L I M I T E D W A R R A N T Y ( C o n t i n u e d ) Cessna Single Engine Marketing 2625 S. Hoover Rd. Wichita KS 67215 Telefax: 316.517.2772