Specification & Description - BenAir

1 Specification &DescriptionJuly 2010(G1000 equipped units 208B-2000 and on) Specification AND DESCRIPTIONEFFECTIVE WITH SERIAL NUMBER 208B-2160 AND ONJULY 2010 caravan MarketingCessna Aircraft Box 7704 Wichita, Kansas 67277-7704 Telephone (316) 517-6081 Fax (316) 517-7250 July 20101 INTRODUCTIONThis Specification and Description is published for thepurpose of providing general information for the evalua-tion of the design, performance and equipment of theCessna Grand caravan aircraft. Should more detaileddata be required, it can be obtained by contacting:Cessna Aircraft Box 7704 Wichita, Kansas 67277 Telephone: 316-517-6081 Fax: 316-517-7850 This document describes only the Cessna Model 208 BGrand caravan aircraft, Unit Serial Number 2160 andon, and its powerplant and included is the Cessna warranty applicable to theCessna Model 208B Grand caravan aircraft and theGrand caravan Crew Training Agreement.

2 In the eventof any conflict or discrepancy between this documentand the basic purchase agreement to which it may beappended, terms specified in the basic purchase agree-ment 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 and Description whenever :This product contains Halon 1211, Halon 1301, and also R-134A. Furthermore, the product wasmanufactured with CFC-12 and 1-1-1 Trichloroethane, substances which harm public health and environment bydestroying ozone in the upper atmosphere.

3 2 TABLE OF CONTENTSC essna Grand caravan Specification and of Contents ..21. General Description ..3-42. Performance ..43. Structural Design Criteria ..74. Fuselage Group ..7-85. Wing Group ..86. Empennage Group ..87. Landing Powerplant .. Propeller ..99. Controls .. System .. System .. Systems .. System .. System .. G1000 Avionics Corrosion Standard Grand caravan Avionics .. Engine Flight Instruments .. Flight Controls .. Electrical Power .. Exterior Interior Lights .. Fuel Exterior ..1412.

4 Documentation and Technical Maintenance Programs ..15-1714. Limited Cessna s Limited Warranty .. Pratt & Whitney Canada Inc.. McCauley Limited Warranty .. Honeywell/Bendix/King Warranty .. Garmin Warranty .. Goodrich Avionics Systems Limited Grand caravan Crew Training Agreement ..22 FIGURE I GRAND caravan EXTERIOR II GRAND caravan CABIN, DOORS, AND WINDOWS DIMENSIONS ..6 FIGURE III GRAND caravan FLIGHT DECK ..12 July 20103 MANUFACTURERCESSNA AIRCRAFT COMPANYMODEL208B1. GENERAL DESCRIPTIONThe Cessna Grand caravan is an unpressurized single-engine high wing turboprop aircraft with fixed landinggear.

5 The aircraft can accommodate up to 14 personsincluding a minimum crew of one. (Operations with morethan nine passengers must be approved by the register-ing country s aviation authority.) Suitable allowance forluggage and optional equipment is also powerplant is a Pratt and Whitney of Canada PT6A-114A turboprop engine mounted in the nose of the air-craft basis is to FAA FAR Part 23 Requirements day, night, VFR, IFR and flight-into-icingconditions when equipped with the appropriate certification requirements may require additionalequipment and.

6 Pratt & Whitney PT6A-114A 675 shp @ 1900 rpmPROPELLER ..McCauley, Anti-Ice, Constant Speed, Full Feathering, Reversible Pitch, 3 Blades, 106 in. lb/ft2 Power .. lb/shpAPPROXIMATE DIMENSIONSO verall Height ..14 ft 10 inOverall Length ..41 ft 7 inWingSpan (overall) ..52 ft 1 inArea .. ft2 Sweepback (at 50% chord) ..0 degreesDihedral ..+3 degreesTaper Ratio .. Ratio .. Aerodynamic Chord .. inHorizontal TailSpan (overall) ..20 ft 6 inArea .. ft2 Sweepback ..0 at elevator hinge lineAspect Ratio .. Aerodynamic Chord .. inVertical TailHeight (overall) ..8 ft 2 inArea (including dorsal fin).

7 Ft2 Sweepback ..+ at rudder hinge lineCabinHeight (floorboard to headliner) ..4 ft 3 inLength Firewall to Aft Bulkhead (nominal) ..21 ft 4 inWidth (max.) ..5 ft 2 inLanding GearTread .. ftWheelbase .. ftTire Size Main .. x 10, 8 plyTire Size x x 8, 6 ply42. PERFORMANCE1. GENERAL Description (Continued)DESIGN WEIGHT AND CAPACITIESM aximum Ramp lbMaximum Take Off Weight ..8750 lbMaximum Weight (Cargo Pod Installed Flight into Icing) ..8550 lbMaximum Landing lb*Standard Empty Weight ..4514 Est. lbMaximum Useful Load ..4271 Est. lbFuel Capacity (usable) @ gal/2224 lbOil.

8 14 qt*Approximate standard empty weight includes unusable fuel, full operating fluids and full engine performance data is based on a standard aircraft con-figuration in International Standard Atmosphere and landing field lengths are based on level, hardsurface, dry runways with zero wind. Actual performancewill vary with individual airplanes and other factors such asenvironmental conditions and aircraft ..Without cargo pod (8,750 lbs.) ..With cargo pod (8,750 lbs.)Cruise at 10,000 ft..184 ktsCruise at 20,000 ft..174 ktsRANGE (with 2224 pounds usable fuel and fuel allowance for engine start, taxi, takeoff, climb, descent and 45 minutes reserve)Maximum Cruise Power at 10,000 nm.

9 862 nmEndurance .. hr .. hrMaximum Cruise Power at 18,000 ft ..1109 nm ..1044 nmEndurance .. hr .. hrMaximum Range Power at 10,000 ft ..1026 nm ..963 nmEndurance .. hr .. hrMaximum Range Power at 18,000 nm ..1076 nmEndurance .. hr .. hrRate of Climb at Sea fpm ..925 fpmService Ceiling ..23,700 ft ..22,800 ftMaximum Certified Altitude ..25,000 ft ..25,000 ftMaximum Altitude in Icing Conditions ..20,000 ft ..20,000 ftTakeoff Performance (sea level, 8750 lb)Ground Roll ..1365 ft ..1405 ftTotal Distance Over 50 ft Obstacle ..2420 ft ..2500 ftLanding Performance (sea level, 8500 lb, no reverse)Ground Roll.

10 950 ft ..915 ftTotal Distance Over 50 ft. Obstacle ..1795 ft ..1740 ftSTALL Speed, CASF laps Up, Idle Power ..78 kts ..78 ktsFlaps Down, Idle Power ..61 kts ..61 ktsJuly 20105(Shown with Optional Cargo Pod Installed)52 ft 1 in 106 in (McCauley)11 ft 8 in 20 ft 6 in PIVOT POINT* PIVOT POINT* 15 ft 5 1/2inMAX. 41 ft 7 inFIGURE I GRAND caravan EXTERIOR DIMENSIONSNOTES:1. Dimensions shown are based onstandard empty weight and properinflation of nose and main gear Wing span dimension includesstrobe Maximum height shown with nosegear depressed as far as Wheel base length is 13 -31/2.