Cessna Skyhawk 172N Pilot Operating Handbook page 288

Supplement POH Reims/Cessna (F) 172 N&P
with TAE 125-02-114
CRUISE PERFORMANCE, RANGE AND ENDURANCE
with Integraltanks at 1089 kg (2400 lbs) (Cessna 172P)
Conditions:
Take-off weight 1089 kg (2400 lbs)
Flaps Up
Zero wind
Notes:
1. Endurance information is based on integral tanks with 196.8 l
(52 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.
Page 5b-26
Issue 2
Revision -, April 2015