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CS 25.103 Stall speed

Large Aeroplanes (CS-25) · CS-25 · EAR revision 26 Jan 2023

IRImplementing rule

CS 25.103Stall speed

(See AMC 25.103)

(a)The reference stall speed VSR is a calibrated airspeed defined by the applicant. VSR may not be less than a 1-g stall speed. VSR is expressed as:

where – VCLMAX = Calibrated airspeed obtained when the loadfactor-corrected lift coefficient is first a maximum during the manoeuvre prescribed in sub-paragraph (c) of this paragraph. In addition, when the manoeuvre is limited by a device that abruptly pushes the nose down at a selected angle of attack (e.g. a stick pusher), VCLMAX may not be less than the speed existing at the instant the device operates; nzw = Load factor normal to the flight path at VCLMAX; W = Aeroplane gross weight; S = Aerodynamic reference wing area; and q = Dynamic pressure.

(b)VCLMAX is determined with:

(1)Engines idling, or, if that resultant thrust causes an appreciable decrease in stall speed, not more than zero thrust at the stall speed;

(2)Propeller pitch controls (if applicable) in the take-off position;

(3)The aeroplane in other respects (such as flaps, landing gear, and ice accretions) in the condition existing in the test or performance standard in which VSR is being used;

(4)The weight used when VSR is being used as a factor to determine compliance with a required performance standard;

(5)The centre of gravity position that results in the highest value of reference stall speed; and

(6)The aeroplane trimmed for straight flight at a speed selected by the applicant, but not less than 1.13 VSR and not greater than 1.3 VSR. (See AMC 25.103(b))

(c)Starting from the stabilised trim condition, apply the longitudinal control to decelerate the aeroplane so that the speed reduction does not exceed 0.5 m/s2 (one knot per second). (See AMC 25.103(b) and (c)).

(d)In addition to the requirements of sub-paragraph (a) of this paragraph, when a device that abruptly pushes the nose down at a selected angle of attack (e.g. a stick pusher) is installed, the reference stall speed, VSR, may not be less than 3,7 km/h (2 kt) or 2%, whichever is greater, above the speed at which the device operates. (See AMC 25.103(d))

[Amdt 25/3]

[Amdt 25/18]

IR · CS 25.103 — CS-25 · ED Decision 2016/010/R · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.103(b)Stalling speed

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The airplane should be trimmed for hands-off flight at a speed 13 percent to 30 percent above the anticipated VSR with the engines at idle and the airplane in the configuration for which the stall speed is being determined. Then, using only the primary longitudinal control for speed reduction, a constant deceleration (entry rate) is maintained until the airplane is stalled, as defined in CS 25.201(d). Following the stall, engine thrust may be used as desired to expedite the recovery. The analysis to determine VCLMAX should disregard any transient or dynamic increases in recorded load factor, such as might be generated by abrupt control inputs, which do not reflect the lift capability of the aeroplane. The load factor normal to the flight path should be nominally 1.0 until VCLMAX is reached.

AMC · AMC 25.103(b) — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.103(c)Stall speed

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The stall entry rate is defined as the mean rate of speed reduction (in m/s2 (knots CAS/second)) in the deceleration to the stall in the particular stall demonstration, from a speed 10% above that stall speed, i.e.

AMC · AMC 25.103(c) — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

AMCAcceptable means of compliance

AMC 25.103(d)Stall speed

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In the case where a device that abruptly pushes the nose down at a selected angle of attack (e.g. a stick pusher) operates after CLMAX, the speed at which the device operates, stated in CS 25.103(d), need not be corrected to 1g. Test procedures should be in accordance with AMC 25.103(b) to ensure that no abnormal or unusual pilot control input is used to obtain an artificially low device activation speed.

AMC · AMC 25.103(d) — CS-25 · ED Decision 2003/2/RM · CS-25 Easy Access Rules · EAR revision 26 Jan 2023

All rules in SUBPART B – FLIGHT

Consolidated from the EASA Easy Access Rules (revision 26 Jan 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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