I don't know for sure, but last time I checked, years ago, not sure how many, the stall and recovery requirement for a PPL, was taken out....
Entry into, and recovery from fully developed Power-On and Power-Off stalls is a PTS requirement in the US. Should include accelerated stalls as well, as the base-to-final turning stall is most likely to kill a PPL.
www.faa.gov/training_testing/testing/test.../FAA-S-8081-14B.pdf
Task B: Power-Off Stalls (ASEL and ASES)
References: FAA-H-8083-3; AC 61-67; POH/AFM.
Objective: To determine that the applicant:
1. Exhibits satisfactory knowledge of the elements related to power-off stalls.
2. Selects an entry altitude that allows the task to be completed no lower than 1,500 feet AGL.
3. Establishes a stabilized descent in the approach or landing configuration, as specified by the examiner.
4. Transitions smoothly from the approach or landing attitude to a pitch attitude that will induce a stall.
5. Maintains a specified heading, ±10°, if in straight flight; maintains a specified angle of bank not to exceed 20°, ±10°; if in turning flight, while inducing the stall.
6. Recognizes and recovers promptly after a fully developed stall occurs.
7. Retracts the flaps to the recommended setting; retracts the landing gear, if retractable, after a positive rate of climb is established.
8. Accelerates to VX or VY speed before the final flap retraction; returns to the altitude, heading, and airspeed specified by the examiner.
Task C: Power-On Stalls (ASEL and ASES)
NOTE: In some high performance airplanes, the power setting may have to be reduced below the practical test standards guideline power setting to prevent excessively high pitch attitudes (greater than 30° nose up).
References: FAA-H-8083-3; AC 61-67; POH/AFM.
Objective: To determine that the applicant:
1. Exhibits satisfactory knowledge of the elements related to power-on stalls.
2. Selects an entry altitude that allows the task to be completed no lower than 1,500 feet AGL.
3. Establishes the takeoff or departure configuration as specified by the examiner. Sets power to no less than 65 percent available power.
4. Transitions smoothly from the takeoff or departure attitude to the pitch attitude that will induce a stall.
5. Maintains a specified heading, ±10°, if in straight flight; maintains a specified angle of bank not to exceed 20°, ±10°, if in turning flight, while inducing the stall.
6. Recognizes and recovers promptly after a fully developed stall occurs.
7. Retracts the flaps to the recommended setting; retracts the landing gear if retractable, after a positive rate of climb is established.
8. Accelerates to VX or VY speed before the final flap retraction; returns to the altitude, heading, and airspeed specified by the examiner.