(7) – Cessna 172P
Engine
| Number of engines: 1 |
| Engine Manufacturer: Avco Lycoming |
| Engine Model Number: O-320- D2J |
| Engine Type: Normally aspirated, direct-drive, air-cooled, horizontally opposed, carburetor equipped, four-cylinder engine with 319.8 cu.in. displacement |
| Horsepower Rating and Engine Speed: 160 rated HP at 2700 RPM |
Propeller
| Propeller Manufacturer: McCauley Accessory Division |
| Propeller Model Number: 1C160/DTM7557 |
| Number of Blades: 2 |
| Propeller Diameter Maximum: 75 inches, Minimum: 74 inches |
Fuel
| Approved Fuel Grades: 100LL Grade Aviation Fuel (Blue), 100 (Formerly 100/130) Grade Aviation Fuel (Green) |
| Fuel Standard Capacity Tanks: Total Capacity: 43 gallons, Total Capacity Each Tank: 21.5 gallons, Tatoal Usable: 40 gallons. |
| Fuel Long Range Capacity Tanks: Total Capacity: 54 gallons Total Capacity Each Tank: 27 gallons, Tatoal Usable: 50 gallons. |
| Fuel Integral Capacity Tanks Total Capacity: 68 gallons Total Capacity Each Tank: 24 gallons, Tatoal Usable: 62 gallons. |
Performance
| Velocidade: Maximum at sea level: 123 Knots, Cruise, 75% power at 8000 ft: 120 Knots |
| Razão de subida: 700 FPM |
| Service Ceiling: 13000 FT |
| Takeoff Performance: Ground Roll: 890 FT, Total Distance Over 50-ft Obstacle: 1625FT |
| Landing Performance (KCAS): Ground Roll: 540 FT, Total Distance Over 50-ft Obstacle: 1280 FT |
| Stall Speesds (KCAS): Flaps Up, Power Off: 51 Knots, Flaps Down and Power Off: 46 Knots |
| Maximum Weight: Ramp: 2407 LBS, Takeoff or Landing: 2400 LBS |
| Standard Empty Weight: Skyhawk: 1414 LBS, Skyhawk II: 1440 LBS |
| Maximum Useful Load: Skyhawk: 993 LBS, Skyhawk II: 967 LBS |
| Baggage Allowance: Pounds/Sq Ft: 13.8 |
| Fuel Standard Capacity Tanks: 43 GAL |
| Fuel Long Range Capacity Tanks: 54 GAL |
| Fuel Integral Capacity Tanks: 68 GAL |
| PROPELLER: Fixed Pitch, Diameter: 75 IN |
Cruise
| 75% power at 8000 ft: 440 NM |
| 40 gallons usable fuel: 3.8 HRS |
| 75% power at 8000 ft: 585 NM |
| 50 gallons usable fuel: 5.0 HRS |
| 75% power at 8000 ft: 755 NM |
| 62 gallons usable fuel: 6.4 HRS |
| Maximum Range at 10000 ft: 520 NM |
| 40 gallons usable fuel: 5.6 HRS |
| Maximum Range at 10000 ft: 680 NM |
| 50 gallons usable fuel: 7.4 HRS |
| Maximum Range at 10000 ft: 875 NM |
| 62 gallons usable fuel: 9.4 HRS |
| *Recommended lean mixture with fuel allowance for engine start, takeoff, climb and 45 minutes reserve |
