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Takeoff & Landing Performance

C172P Short Field
Pacific Flying Club
Calculations Worksheet

Takeoff Calculations Worksheet

Paved (Off)
Active Ground Roll
-- FT
Paved Runway
Total to Clear 50 FT
-- FT
Obstacle Clearance
Reference Speeds
51 / 56 KIAS
Lift Off: 51 kt | 50ft: 56 kt
Wind Analysis
--
Max Demonstrated X-Wind: 15 kt
Field Data and Conditions
/ kts
Note: If From TAF / METAR ect. Convert to Magnetic
Calculate Wind Components
Runway Magnetic Heading: 070°M
Wind Angle off Runway: 20°
Head wind
9.4 Kts
Cross Wind
3.4 Kts
Calculate Wind Factor
Head Wind
9.4 Kts Divided by 9 = 1.04 X 10 = 10.4 % Headwind Factor
Tail Wind
0.0 Kts Divided by 2 = 0.00 X 10 = 0.0 % Tail Wind Factor
Caution: Max 10 kts - No more than 5 kts recommended · ADD Tail Wind Factor
Calculate Pressure Altitude
Note: If result is below sea level use sea level pressure altitude.
29.92 - Altimeter Setting 29.92 = Note: May be Negative or Positive 0.00 X 1000 = 0 + Field Elevation 10 = Pressure Altitude 10 FT
Cessna Charts (POH Short Field)

From the Cessna Charts find the sets of distances that bracket the actual temperature and the actual pressure altitude. Temp 1 will be the low temperature and Temp 2 will be the high temperature. Pressure Altitude 1 will be the low pressure and Pressure Altitude 2 will be the high pressure. Note: if the temperature or pressure matches one in the charts you do not need to do an adjustment for that chart.

Temperature Factor Calculation

15 °C Actual Temp
- 10 °C Temp 1
= 5 °C X 10 = 50 %

Pressure Altitude Factor Calculation

10 Actual Pressure Altitude
- 0 Pressure Altitude 1
= 10 X 0.1 = 1.0 %
Temperature Adjustment
Cessna Chart Pressure Altitude 1 = 0 ft
Ground Roll Total To Clear 50 ft Obstacle
Temp 2 Distances 925 1685
Temp 1 Distances - 850 - 1570
Difference = 75 = 115
Temperature Factor X 50 % X 50 %
Adjustment = 37.5 = 57.5
Temp 1 Distances + 850 + 1570
Temperature Adjusted Distances A1 = 887.5 A2 = 1627.5
Chart Pressure Altitude 2 = 1000 ft
Ground Roll Total To Clear 50 ft Obstacle
Temp 2 Distances 1015 1860
Temp 1 Distances - 940 - 1725
Difference = 75 = 135
Temperature Factor X 50 % X 50 %
Adjustment = 37.5 = 67.5
Temp 1 Distances + 940 + 1725
Temperature Adjusted Distances B1 = 977.5 B2 = 1792.5
Pressure Altitude and Wind Adjustment
Ground Roll Total To Clear 50 ft
Temp Adjusted Distances (B) B1 = 977.5 B2 = 1792.5
Temp Adjusted Distances (A) - A1 = 887.5 - A2 = 1627.5
Deference = 90.0 = 165.0
Pressure Alt. Factor X 1.0 % X 1.0 %
Adjustment = 0.9 = 1.7
Temp Adjusted Distances + A1 = 887.5 + A2 = 1627.5
Adjusted Distances = 888.4 = 1629.2
Subtract Headwind Factor - 10.4 % - 10.4 %
Final Paved Distance = 796 FT = 1460 FT
Caution: Add Tailwind Factor - Max 50%
Grass Runway Adjustment
Takeoff X 15%
Ground Roll Distance 796
X Grass Factor X 15 %
Grass Adjustment = 119
Ground Roll Distance 796
+ Grass Adjustment + 119
Final Ground Roll Distance = 915 FT
Total To Clear 50 Feet 1460
+ Grass Adjustment + 119
Final Total to Clear 50 ft = 1579 FT