Caravan 675
Caravan 675 Floatplane
General Description:
The Cessna Caravan is an Unpressurized Single Engine High Wing Turboprop with
Fixed Landing Gear. The Aircraft Can Accommodate up to 14 Persons including a
minimum Crew of One. (Operations with more than Nine Passengers are limited to
countries that issue a Far Part 23 Nine Passenger Limit Waiver.) Suitable
Allowance for Luggage and Optional Equipment is also provided.
The Powerplant is a Pratt and Whitney of Canada PT6A-114A Turboprop Engine
Mounted in the Nose of the Airplane Fuselage.
Certification Basis is to U.S. FAA Far Part 23 Requirements - Day, Night, VFR,
IFR and Flight-Into-Icing Conditions when equipped with the appropriate
options.
- Design Weight
- Maximum Ramp Weight 8035 Lbs.
- Maximum Takeoff Weight 8000 Lbs.
- Maximum Landing Weight 7800 Lbs.
- *Standard Empty Weight 3925 Lbs.
- Maximum Useful Load 4110 Lbs.
- Capacities
- Maximum Fuel 335.6 Gallon/2248 Lbs.
- Usable Fuel 332 Gallon/2224 Lbs.
- Oil 14 Qt.
- Powerplant Pratt & Whitney PT6A-1 14A 675 Shp @ 1900 Rpm
- Propeller Mccauley, Constant Speed, Full Feathering, Reversible, 3 Blades,
106 In. Diameter
- Loading
- Wing 28.6 Lbs/Sq. Ft.
- Power 11.85 Ibs/Shp
Approximate Dimensions
- Overall Height 14 Ft. 10 In.
- Overall Length 37 Ft. 7 In.
- Wing
- Span (Overall) 52 Ft. 1 In.
- Area 279.40ft .2
- Sweepback (At 50% Chord) 0 Degrees
- Dihedral +3 Degrees
- Taper Ratio 0.586
- Aspect Ratio 9.555
- Mean Aerodynamic Chord 66.474 In.
- Horizontal Tail
- Span (Overall) 20 Ft. 6 In.
- Area 70.04 Ft.2
- Sweepback 00 at Elevator Hinge Line
- Dihedral 0 Degrees
- Aspect Ratio 6.0
- Mean Aerodynamic Chord 41.984 In.
- Vertical Tail
- Height (Overall) 8 Ft. 2 In.
- Area (Including Dorsal Fin) 39.92 Ft.2
- Sweepback +9.437'at Rudder Hinge Line
- Cabin
- Height (Floorboard To Headliner) 4 Ft. 3 In.
- Length - Firewall To Aft Bulkhead (Nominal) 17 Ft. 4 In.
- Width (Max.) 5 Ft. 2 In.
- Landing Gear
- Tread: 11.66 Ft.
- Wheelbase: 11.62 Ft.
- Tire Size - Main (Standard) 6.50 X 10, 8 Ply, 83 Psi
- Tire Size - Nose (Standard) 6.50 X 8, 8 Ply, 53-63 Psi
*Standard Empty Weight INCLUDES Unusable Fuel, Full Operating Fluids AND
Full Engine Oil
Performance:
Performance figures are based on the indicated weight, standard atmospheric
conditions, level hard-surface dry runways and no wind. They are calculated
values derived from flight tests conducted by the Cessna Aircraft Company under
carefully documented conditions and will vary with individual airplanes and
numerous factors affecting performance.
- Speed (8,000 Ibs.)
- Maximum Cruise at 10,000 Ft: 186 Kts
- Maximum Cruise at 20,000 Ft: 174 Kts
- Range (With 224 Pounds Usable Fuel And Fuel Allowance For Engine Start,
Taxi, Takeoff, Climb, Descent And 45 Minutes Reserve)
- Maximum Cruise Power at 10,000 Ft :932 Nm
Endurance: 5.1 Hr.
- Maximum Cruise Power at 20,000 Ft: 1220 N
Endurance: 7.13 Hr
- Maximum Range Power at 10,000 Ft: 1085 Nm
Endurance: 7.0 Hr
- Maximum Range Power at 20,000 Ft: 1295 Nm
Endurance: 8.3 Hr.
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- Rate of Climb at Sea Level: 1234 fpm
- Service Ceiling: 25,000+ Ft.
- Maximum Operating Altitude: 25,000 Ft.
- Takeoff Performance (Sea Level, 8000 Lbs.)
- Ground Roll: 1160 Ft.
- Total Distance Over 50 Ft.Obstacle: 2053 Ft.
- Landing Performance (Sea Level, 7800 Lbs, No Reverse)
- Ground Roll: 745 Ft.
- Total Distance Over 50 Ft. Obstacle: 1665 Ft.
- Stall Speed,CAS
- Flaps Up, Idle Power: 75 Kts
- Flaps Down, Idle Power: 61 Kts
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Additional Optional Accessories:
Floatplane
- The Caravan can be converted to a floatplane or an amphibian when equipped
with the optional Floatplane Provision Kit and Wipline 8000 Series Floats
(manufactured by Wipaire, Inc.)
- The floats are part of a Wipaire, Inc. STC, and are installed by Wipaire,
Inc.
- For additional information on the floats contact:
- Wipaire, Inc.
8520 River Rd.
Inver Grove Heights, Minnesota 55076
Phone 612-451-1205
Fax 612-451-1786
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Floatplane |
Amphibian |
| Maximum Ramp Weight |
8035lbs.... |
8035lbs |
| Maximum Takeoff Weight |
8000lbs |
8000lbs |
| Maximum Landing Weight |
7800 lbs. |
7800 lbs. |
| Standard Empty Weight |
4548 lbs. |
4895 lbs. |
| Maximum Useful Load |
3487 lbs. |
3140 lbs. |
| Takeoff (Sea Level) |
|
|
| Time on Water |
28 sec. |
28 sec. |
| Water Run |
1919 ft. |
1919 ft. |
| Over 50 ft. Obstacle |
3015 ft. |
3015 ft. |
| Rate of Climb (Sea Level) |
1110 fpm |
1110 fpm |
| Maximum Operating Altitude |
20,000 ft. |
20,000 ft. |
| Maximum Cruise Speed (10,000 ft.) |
162 kts |
162 kts |
| Range - Maximum |
|
|
| Cruise Speed* (10,000 ft.) |
790 n.m. |
790 n.m. |
| Stall Speed (Landing Configuration) |
59 kts |
59 kts. |
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| Range based on 332 gal. usable fuel and
includes takeoff, climb, descent and 30 minute reserve. |
Documentation and Technical Publications
Equipment List:
- Weight and Balance Report
- Plotter, Weight & Balance (Cargo & Passenger)
- Pilots Operating Handbook
- Maintenance Manual (Airframe and Engine as required)
- Illustrated Parts Catalog (Airframe and Engines as required)
- Wiring Diagram Manuals (Airframe and Avionics)
- CESCOM/Cessna Customer Care Handbook
- Miscellaneous Information concerning Engine and Airframe Support
Cessna will provide Service Information and manual revisions as required.
Warranty
Cessna's Limited Warranty (Model Cessna Caravan)
- The Cessna Aircraft Company, Wichita, Kansas, U.S.A. ("Cessna"),
expressly warrants each new Model Cessna Caravan aircraft manufactured by it
and new aircraft equipment and accessories therefor except as noted below, to
be free from defects in material and work manship under normal use and service
for a period of twelve (12) months after delivery to the original retail
purchaser or first user. Engines and engine accessories supplied by Pratt &
Whitney Aircraft of Canada Ltd. ("Pratt and Whitney"), and avionics
supplied by King Radio Corporation ("King"), are specifically
excluded from this warranty and are covered by their respective manufacturer's
separate warranty.
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