C172S · Performance · 05 of 12
Stall Speeds
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- 02 · LOCKEDThe Worked Cross-Country Problem
- 03 · LOCKEDAirspeed Calibration: Normal Static Source
- 04 · LOCKEDAirspeed Calibration: Alternate Static Source
05 · Reading now
Stall Speeds
Twenty-four stall speeds in one table, arranged by flap setting, bank angle and centre of gravity. The surprise is how little the centre of gravity matters here: four of the six rows are identical between the forward and rearward limits.
At a glance
- Conditions2550 lb, power off
- Flaps up, 0° bank48 KIAS / 53 KCAS
- Flaps 10°, 0° bank, rearward C.G.42 KIAS / 50 KCAS
- Flaps 30°, 0° bank40 KIAS / 48 KCAS
- Flaps up, 60° bank68 KIAS / 75 KCAS
- Flaps 30°, 60° bank57 KIAS / 68 KCAS
- Altitude loss in a stall recoveryas much as 230 feet
At the most rearward centre of gravity
Flaps up, by angle of bank
0° — 48 KIAS / 53 KCAS
30° — 52 / 57
45° — 57 / 63
60° — 68 / 75
Flaps 10°, by angle of bank
0° — 42 / 50
30° — 45 / 54
45° — 50 / 59
60° — 59 / 71
Flaps 30°, by angle of bank
0° — 40 / 48
30° — 43 / 52
45° — 48 / 57
60° — 57 / 68
At the most forward centre of gravity
The flaps up row is identical to the rearward one: 48/53, 52/57, 57/63, 68/75. So is the flaps 30° row: 40/48, 43/52, 48/57, 57/68.
Flaps 10°, most forward C.G., by angle of bank
0° — 43 / 51
30° — 46 / 55
45° — 51 / 61
60° — 61 / 72
That row is one knot higher at every bank angle than the same row at the most rearward centre of gravity — the only place in the whole table where the loading makes a difference, and it makes a difference of one knot.
Reading the pattern
Two trends run through the table and they are worth internalising as trends rather than as twenty-four numbers. Flap lowers the stall speed: eight knots between flaps up and 30 degrees at wings level. Bank raises it: twenty knots between level and 60 degrees of bank with the flaps up.
Bank costs more than flap saves. That is the arithmetic behind every stall-spin accident in a steep turn low down.
Two notes
NOTE — A stall recovery can cost as much as 230 feet of altitude.
NOTE — The KIAS values in the table are approximate.
Check yourself
Under what weight and power condition is the whole table quoted?
Give the wings-level stall speed in KIAS for each of the three flap settings.
How much does 60° of bank add to the flaps up stall speed?
Which single row differs between the forward and rearward centre of gravity, and by how much?
How much altitude may a stall recovery consume?
Study aid — always fly your aircraft's current AFM/POH.
Source: Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, Cessna Model 172S, Revision 5 (19 July 2004), p. 5-12, Revision 5 (19 July 2004)
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