| Cessna 172P -
1981 |
|
Performance - Specifications (as of 30 May
1980) |
Speed:
Maximum at Sea Level
Cruise, 75% Power at 8000 Feet
Vne (Never Exceed Speed)
Vno (Maximum Structural Cruising) |
123 knots
120 knots
158 KIAS
127 KIAS |
Do Not
Use This Information For Flight Planning
|
|
Cruise: |
|
75% Power at
8000 Feet
40 Gallons Usable Fuel
50 Gallons Usable Fuel
62 Gallons Usable Fuel |
Range: 440 NM / Time: 3.8 HRS
Range: 585 NM / Time: 5.0 HRS
Range: 755 NM / Time: 6.4 HRS |
Max. Range at 10,000 Feet
40 Gallons Usable Fuel
50 Gallons Usable Fuel
62 Gallons Usable Fuel |
Range: 520 NM / Time: 5.6 HRS
Range: 680 NM / Time: 7.4 HRS
Range: 875 NM / Time: 9.4 HRS |
| Rate
of Climb at Sea Level: |
700 FPM |
|
Service Ceiling: |
13,000 Feet |
Takeoff Performance:
Ground Roll
Total Dist. over 50-FT Obstacle |
890 Feet
1625 Feet |
Landing Performance:
Ground Roll
Total Dist. over 50-FT Obstacle |
540 Feet
1280 Feet |
Stall
Speed (KCAS):
Flaps Up, Power Off
Flaps Down, Power Off |
51 Knots
46 Knots |
Maximum Weight:
Ramp
Takeoff or Landing |
2407 Pounds
2400 Pounds |
Standard Empty Weight:
Skyhawk
Skyhawk II |
1414 Pounds
1440 Pounds |
Maximum Useful Load:
Skyhawk
Skyhawk II |
993 Pounds
967 Pounds |
|
Baggage Allowance: |
120 Pounds |
| Wing
Loading: |
13.8 Pounds/Sq.Ft. |
| Power
Loading: |
15 Pounds/HP |
Fuel
Capacity (Total):
Standard Tanks
Long Range Tanks
Integral Tanks |
43 Gallons
54 Gallons
68 Gallons |
| Oil
Capacity: |
8 Quarts |
|
Engine: |
Avco Lycoming O-320-D2J / 160 BHP at 2700
RPM |
|
Propeller: |
75 Inch (diameter) / Fixed Pitch |
| |
|
