Supplement POH
Cessna 172 R&S
(FAA-Version)
Page 5a-11
Issue 3
Revision -, June 2016
CRUISE PERFORMANCE, RANGE AND ENDURANCE at
1111 kg (2450 lbs)
Conditions:
Take-off weight 1111kg (2450 lbs)
Flaps Up
Zero wind
Notes:
1. Endurance information are based on 168.8 l (44.6 US gal)
usable fuel.
2. The table assumes 4 l (1.1 US gal) for startup and taxi; time,
fuel and distance to climb and 45 min. reserve.
3. Increase true airspeed (KTAS) and maximum range (NM) by
1% per 10°C above ISA temperature.
4. Cruise Power above 75% not recommended. For economic
cruise set load 70% or less.
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