Supplement POH
Cessna 172 R&S
(FAA-Version)
Page 5a-8
Issue 3
Revision -, June 2016
TIME, FUEL AND DISTANCE TO CLIMB AT 1111 kg (2450 lbs)
Conditions:
Takeoff weight 1111 kg (2450 lbs)
Climb speed v
y
= 70 KIAS
Flaps Up
Full Power
Standard Temperature (ISA)
Notes:
1. Add 4 l (1.1 US gal) of fuel for engine start, taxi and takeoff
allowance.
2. Increase time and distance by 10% for 10°C above standard
temperature.
3. Distances shown are based on zero wind.
4. Time, distance and fuel required are only valid from the point
where the airplane climbs at v
y
= 70 KIAS.