C172S · Performance · 05 of 12

Stall Speeds

  1. 01 · LOCKEDHow the Charts Were Produced
  2. 02 · LOCKEDThe Worked Cross-Country Problem
  3. 03 · LOCKEDAirspeed Calibration: Normal Static Source
  4. 04 · LOCKEDAirspeed Calibration: Alternate Static Source
  5. 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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  6. 06 · LOCKEDShort Field Takeoff Distance at 2550 Pounds
  7. 07 · LOCKEDShort Field Takeoff at Lighter Weights
  8. 08 · LOCKEDMaximum Rate of Climb
  9. 09 · LOCKEDTime, Fuel and Distance to Climb
  10. 10 · LOCKEDCruise Performance
  11. 11 · LOCKEDRange and Endurance Profiles
  12. 12 · LOCKEDShort Field Landing Distance