Cessna Aircraft Company Sales Engineering, Propeller Marketing December, Cessna Skylane compared to the Cirrus SR20 GTS

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1 Cessna Aircraft Company Sales Engineering, Propeller Marketing December, 2010 Cessna compared to the

2 Takeoff Performance Takeoff distance represents the runway length necessary to depart at the aircraft's maximum takeoff weight. 2,500 Takeoff Distance 1 2,221 2,000 Runway Required (feet) 1,500 1, ,478 1,515 The shorter the runway length required, the more airports that are available for use Ground Roll Distance to 50 ft 1. Zero Wind, Dry Level Runway, Maximum Takeoff Weight, Sea Level, ISA.

3 Range Capability The provides greater range than the. Range Capability 1 Range 200 lb Payload 924 nm 682 nm Range 400 lb Payload 924 nm 682 nm Range 600 lb Payload 905 nm 682 nm Range 800 lb Payload 496 nm 285 nm The will complete more of its missions non-stop. 1,000 Range versus Payload Payload (pounds) , minute Reserves, ISA, Zero Wind, Max Power Range (nautical miles)

4 Baggage Capacity The can haul more baggage than the. Total Baggage Capacity 200 pounds 130 pounds 32 cu ft 32 cu ft Weight Capacity (pounds) Volume Capacity (cubic feet) The imposes fewer restrictions on the amount of luggage you can take. 20 0

5 Operating Costs Operating Cost Comparison 1 Estimated Variable Cost per Hour Fuel ($ 4.75 per gallon) 2 $ $ Oil $ 1.24 $ 1.14 Maintenance Labor ($ per hour) 3 $ $ Parts Airframe/Engine/Avionics 3 $ $ Engine Restoration 4 $ $ Propeller Overhaul 5 $ 1.26 $ 1.02 Total Variable Cost per Hour $ $ Operating cost estimates are based on information from Conklin & de Decker Associates' The Aircraft Cost Evaluator (2010 Vol II). Cessna does not warrant this information but merely provides this data for the customer's convenience. 2. Fuel flow and average speed are based on a 200 nautical mile trip using performance data derived from flight manuals includes ground fuel. Conklin adds 15% to the calculated fuel burn amount to " account for less than ideal operating conditions." 3. Labor costs: "The average cost of routine, scheduled and unscheduled maintenance labor for the airframe and avionics." Parts costs: "The average cost of all airframe, avionics and minor engine consumable parts required for normal scheduled and unscheduled maintenance." Maintenance costs cover a 10-year period and are " based on an analysis of data available from operator experience, manufacturer's data and surveys." 4. A per hour allowance that is"...a set aside estimate to cover the cost of an overhaul of the engine at the recommended TBO." 5. "Includes both parts and labor required for overhaul of the propeller, including the cost of any life-limited parts." December, 2010

6 Customer Support Cessna maintains a large customer support organization dedicated to maintaining the worldwide single engine fleet of more than 100,000 aircraft. A network of 350 service stations around the globe provide local service and maintenance to Cessna aircraft owners. A McCauley service station network of 65 facilities provide propeller support. Cessna Parts Distribution maintains a large inventory of parts that allows for same day shipping on most orders. Cessna offers an extensive service organization to assure maximum control and utilization of your investment.

7 Warranty The Cessna warranty is one of the most comprehensive in the industry. Warranty Coverage Major Airframe 2 Years 2 Years / 1,000 Hours Paint and Graphics 1 Year Unknown Standard Avionics 2 Years 2 Years / 1,000 Hours Engine 2 Years 2 Years / 1,000 Hours Propeller 3 Years 1 Year / 1,000 Hours Cessna administers all warranty issues there is no need to deal with multiple vendors. Cessna typically pays warranty claims in less than 3 days.

8 Specifications External Dimensions Length 29 ft 0 in 26 ft 0 in Height 9 ft 4 in 8 ft 11 in Wing Span 36 ft 0 in 38 ft 4 in Cabin Specifics Length 11 ft 2 in 10 ft 2 in Height 49 in 39 in - 50 in Width 42 in 40 in - 49 in Number of Seats 4 4 Baggage Capacity 200 lb / 32 cuft 130 lb / 32 cuft Engines Manufacturer Textron Lycoming Teledyne Continental Model IO-540-AB1A5 IO-360-ES Output 230 hp 200 hp

9 Specifications Performance Maximum Cruise Speed 150 kt 160 kt Maximum Range (reserves, power setting) Takeoff Distance - MTOW, S.L., ISA Ground Roll To Clear 50 ft Obstacle Landing Distance - MLW, S.L., ISA Ground Roll To Clear 50 ft Obstacle 927 nm (45 minutes, 55%) 795 ft 1,515 ft 590 ft 1,350 ft 769 nm (45 minutes, 55%) 1,478 ft 2,221 ft 853 ft 2,636 ft Rate of Climb at Sea Level 924 ft 828 ft Certified Ceiling 18,100 ft 17,500 ft Weights Maximum Ramp Weight 3,110 lb 3,050 lb Maximum Takeoff Weight 3,100 lb 3,050 lb Maximum Landing Weight 2,950 lb 3,050 lb Usable Fuel Capacity 87 gal 56 gal Typical Empty Weight 1,984 lb 2,080 lb Useful Load 1 1,126 lb 970 lb Full-Fuel Payload lb 634 lb 1. Total amount of fuel and payload the aircraft can carry. 2. Passengers and/or cargo capacity with full fuel on-board.

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