Cruise Practice Problems

Current Conditions

Altimeter Setting Temperature at Cruise Planned Cruise Altitude Planned Power Setting (RPM)
29.04"Hg-18°C10500' ASL2650 RPM

Performance Charts

CRUISE PERFORMANCE

CONDITIONS:

2550 Pounds
Recommended Lean Mixture At All Altitudes (Refer to Section 4, Cruise)

PRESS
ALT
FT
RPM20°C BELOW
STANDARD TEMP
STANDARD
TEMPERATURE
20°C ABOVE
STANDARD TEMP
%
BHP
KTAS GPH %
BHP
KTAS GPH %
BHP
KTAS GPH
2000
25508311711.17711810.5721179.9
25007811510.6731159.9681159.4
2400691119.6641109.0601098.5
2300611058.6571048.1531027.7
220053997.750977.347956.9
210047926.944906.642896.3
4000
26008312011.17712010.4721199.8
25507911810.6731179.9681179.4
25007411510.1691159.5641148.9
2400651109.1611098.5571078.1
2300581048.2541027.7511017.3
220051987.448967.045946.7
210045916.642896.440876.1
6000
26508312211.17712210.4721219.8
26007812010.6731199.9681189.4
2500701159.6651149.0601128.5
2400621098.6571088.2541067.7
2300541037.8511017.448997.0
220048967.145946.743926.4
8000
27008312511.17712410.4711239.7
26507812210.5721229.9671209.3
26007412010.0681199.4641178.9
2500651149.1611128.6571118.1
2400581088.2541067.8511047.4
2300521017.548997.146976.8
220046946.843926.541906.2
10000
27007812410.5721239.8671229.3
26507312210.0681209.4631198.9
2600691199.5641179.0601158.5
2500621138.7571118.2541097.8
2400551067.9511047.5491027.1
2300491007.246976.844956.5
12000
2650691219.5641198.9601178.5
2600651189.1611168.5571148.1
2500581118.3541097.8511077.4
2400521057.5491027.1461006.8
230047986.944956.641926.3

NOTES:

*Speed performance is shown for an airplane equipped with
speed fairings which increase the speeds by
approximately 2 knots. There is a corresponding difference
in range, while all other performance figures are
unchanged when speed fairings are installed.

Solution