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CESSNA 172 Skyhawk SP

Used in our FlightAdventures Weekend-to-Solo AdventureÔ, and certain FlightAdventures Explorer-Plus AdventureÔ and FlightAdventures Famous Flight AdventureÔ packages, the Cessna 172 Skyhawk SP epitomizes one of our main philosophical concepts behind all FlightAdventures—unparallelled safety, comfort, and convenience for unforgettable dream-come-true adventure experiences.

Specifications
    SPEED:  
        Maximum at Sea Level 126 KTS
        Cruise, 75% power at 8,500 Ft
            (Best Power Mixture)
    124 KTS

    CRUISE:   Recommended lean mixture with fuel allowance for engine start,
                    taxi, takeoff, climb and 45 minutes reserve.

        75% power at 8,500 Ft Range: 518 NM
            53 gallons usable fuel Time: 4.26 HRS
        Range at 10,000 Ft, 45% Power Range: 638 NM
            53 gallons usable fuel Time: 6.72 HRS
    RATE OF CLIMB AT SEA LEVEL 730 FPM
    SERVICE CEILING 14,000 FT
    TAKEOFF PERFORMANCE:  
        Ground Roll 960 FT
        Total distance over 50 ft. obstacle 1,630 FT
    LANDING PERFORMANCE:  
        Ground Roll 575 FT
        Total distance over 50 ft. obstacle 1,335 FT
    STALL SPEED (KCAS):  
        Flaps off, Power off 53 KCAS
        Flaps down, Power off 48 KCAS
    MAXIMUM WEIGHT:  
        Ramp 2,558 LBS
        Takeoff or Landing 2,550 LBS
    STANDARD EMPTY WEIGHT 1,642 LBS
    MAXIMUM USEFUL LOAD 916 LBS
    BAGGAGE ALLOWANCE 120 LBS
    WING LOADING 14.7 LBS/SQ FT
    POWER LOADING 14.2 LBS/HP
    FUEL CAPACITY 56 US GAL
    OIL CAPACITY 8 QTS
    ENGINE: Avco Lycoming
        180 BHP at 2700 RPM
    IO-360-L2A
    PROPELLER: Fixed Pitch, Diameter 76 IN

The above performance figures are based on the indicated weights, 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 flight performance.

Aircraft Dimensions
Interior Dimensions
Exterior Dimensions
Cabin     Overall Dimensions
 Length 142 in   Length 26 ft 11 in.
 Height 48 in   Height 8 ft 11 in.
 Width 39.5 in   Wing Span 36 ft 1 in.
         
Maximum Seating Capacity - 4      

Information subject to change without notice.

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Equipment List
FLIGHT INSTRUMENTS
Sensitive Altimeter
    (20 ft. increments & inches of Hg)
Digital Clock
Magnetic Compass
Attitude and Directional Gyros 3" Display
    (Includes Vacuum System, Suction
    Gauge, and Low Vacuum Warning)
True Airspeed Indicator
Outside Air Temperature Indicator
Turn Coordinator Indicator
Vertical Speed Indicator

ENGINE INSTRUMENTS
Ammeter / Vacuum
Annunciator Panel
    Left Low Fuel
    Left Low Vacuum
    Low Oil Pressure
    Low Voltage
    Right Low Fuel
    Right Low Vacuum
Flight Hour Recorder
Fuel Flow / Exhaust Gas Temperature
Left and Right Fuel Quantity
Oil Pressure / Temperature
Recording Tachometer

CONTROLS
Hydraulic Toe-Operated Brakes
Parking Brake
Stainless Steel Control Cables
All Purpose Dual Control Wheels
Electric Preselect-Flaps
Dual Flight Controls
Fuel Selector Valve - Left, Both, Right
Fuel Shutoff
Aileron and Elevator Lock
Throttle Control
Vernier Mixture Control
Alternate Static Source
Elevator Trim System

INTERIOR
Leather Seats, Taupe
Seat Belts with Inertia Reel and
    Shoulder Harness (All Seats)
Pilot and Copilot Seats:
    Adjustable Fore and Aft with
    Reclining Backs & Vertical Adjust
Rear Seats:
    Bench with One Piece Reclining Back
Approach Plate Holder
Armrests (outboard)
Wall to Wall Carpet
Pilot's Checklist
Electrical & Avionics Circuit Breakers
Pilot & Copilot Windshield Defroster
Hand Type Fire Extinguisher
Padded Glareshield (with Light)
Pilots Operating Handbook
Shrouded Muffler Heating System
    with Firewall Valve
Clothes Hanger Bar
Metal Instrument Panel with
    Removable Subpanels
Map/Glove Compartment
Baggage Net
Radio Call Plate
Map & Storage Pockets
Cabin Door Scuff Plates
Soundproofing
Sun Visors
Avionics Power Switch
Master Switch
Adjustable Cabin Air Ventilators,
    6 Places
Hinged LH & RH Window
Rear Window
Tinted All-Around Windows

INTERIOR LIGHTS
Variable-Intensity Control Pedestal
Variable-Intensity Backlit Instruments
Variable-Intensity, Indirect Glareshield,
    Instrument Panel Lighting
Variable-Intensity, Yoke Mount Map
Overhead Cabin

EXTERIOR LIGHTS
Omni-Flash Beacon
Navigation
Navigation Lights Detectors
Wing Tip Strobes
Landing and Taxi (Wing Mounted)
Underwing Courtesy (Set of Two)

POWER PLANT AND ACCESSORIES
Lycoming IO-360-L2A Engine
    180 HP @ 2700 RPM
    certified for 100LL Fuel
Fuel Injection System
Tubular Steel Engine Mount
Dynafocal Rear Mount
Automatic Alternate Engine Air
28 Volt, 60 Amp Alternator
Alternator Control Unit
    (with High Voltage Trip Out and
    Low Voltage Warning Capability)
24 Volt, 12.75 Amp Hr. Battery
    (5 hr. Rate)
Oil Cooler
Shock Mounted Cowling
Induction Air Filter
Full Flow Oil Filter
Electric Auxiliary Fuel Pump
Engine Driven Fuel Pump
Fuel Strainer, Incorporated with
    Fuselage Quick Drain
Integral Fuel Tanks, 53 Gal. Usable
Fuel Quick Drains, 5 per Wing and
    Sampler Cup
Ground Service Plug Receptacle
Dual Ignition System, Shielded Magneto
Key Operated Ignition & Starter Switch
Engine Exhaust Muffler
McCauley Fixed Pitch,
    2 Blade, Metal Propeller
Propeller Spinner
Electric Starter
Dual Pump Vacuum System
Emergency Locator Transmitter

EXTERIOR
All Structure Epoxy Corrosion Proofing
Baggage Door
LH Door
RH Door
Wing flaps, (Electrically Operated)
Gear Jack Pads
Fixed Landing Gear
Lockable, Key Operated, Baggage Door
Lockable, Key Operated, Cabin Door
Vinyl Applique Logo and Striping
Steerable Nose Wheel
Overall Paint (Polyurethane)
Heated Pitot System
Audible Stall Warning System
Refueling Steps and Handles
    (Wing Struts and Fuselage)
Fixed Cabin Entrance Steps
Tie Down Rings
Tube Type Tires
    Nose, 5.00 X 5
    Mains, 6.00 X 6
Tow Bar
Conical Camber Wing Tips
Strut Braced, Camber Lift Wings
Winterization Kit
Wheel Fairings

   
Information subject to change without notice.

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