INTRODUCTION
This handbook includes the
material required to be furnished
to the pilot by CAR Part 3.
Section 1 provides basic data and
information of general interest.
PERFORMANCE-SPECIFICATIONS
SPEED:
Maximum at sea level
Cruise, 75% power at 8000 ft
CRUISE: Recommended lean mixture with fuel allowance
for engine start, takeoff, climb and 45 minutes reserve
75% power at 8000 ft
40 gallons usable fuel
75% power at 8000 ft
50 gallons usable fuel
75% power at 8000 ft
62 gallons usable fuel
Maximum Range at 10000 ft
40 gallons usable fuel
Maximum Range at 10000 ft
50 gallons usable fuel
Maximum Range at 10000 ft
62 gallons usable fuel
RATE OF CLIMB AT SEA LEVEL
SERVICE CEILING
TAKEOFF PERFORMANCE
Ground Roll
Total Distance Over 50-ft Obstacle
LANDING PERFORMANCE (KCAS)
Ground Roll
Total Distance Over 50-ft Obstacle
STALL SPEESDS (KCAS)
Flaps Up, Power Off
Flaps Down, Power Off
MAXIMUM WEIGHT
Ramp
Takeoff or Landing
STANDARD EMPTY WEIGHT
Skyhawk
Skyhawk II
MAXIMUM USEFUL LOAD
Skyhawk
Skyhawk II
BAGGAGE ALLOWANCE
WING LOADING: Pounds/Sq Ft
POWER LOADING: Pounds/HP
FUEL CAPACITY
Standard Tanks
Long Range Tanks
Integral Tanks
PROPELLER: Fixed Pitch, Diameter
123 Knots
120 Knots
440 NM
3.8 HRS
585 NM
5.0 HRS
755 NM
6.4 HRS
520 NM
5.6 HRS
680 NM
7.4 HRS
875 NM
9.4 HRS
700 FPM
13000 FT
890 FT
1625 FT
540 FT
1280 FT
51 Knots
46 Knots
2407 LBS
2400 LBS
1414 LBS
1440 LBS
993 LBS
967 LBS
120 LBS
13.8
15.0
43 GAL
54 GAL
68 GAL
75 IN
NOTE:
The 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.
FLIGHT SIMULATION USE ONLY
GENERAL INFORMATION
PAGE 1
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