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NOTE: The speedbrakes/spoilers should be down prior to disconnecting power from the airplane. Ensure control surface areas are clear of personnel and equipment before movement.
1. Provide electrical power.
2. Open WARN ELEC A and WARN ELEC B circuit breakers on the P11 overhead panel.
3. Reset WARN ELEC A circuit breaker.
4. Pressurize the left hydraulic system (AMM 29-11-00/201).
5. Position the flap lever to the 1-unit detente. Verify that the flaps move to 1 (one) and the slats move to the intermediate (takeoff) position.
6. Hold both test STALL test switches in the STALL position.
7. Verify that one (or both) stick shaker(s) operates normally and the slats move to the fully extended (landing) position.
8. Release the test switches.
9. Verify that the stick shaker(s) ceases to operate and the slats retract to the intermediate (takeoff) position.
10. Repeat steps 6 through 9 with the WARN ELEC B circuit breaker closed and the WARN ELEC A circuit breaker open.

　
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