A Good Pilot is Always Learning

PTS CFI CFII (2) (2)

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159 FAA-S-8081-6D References: FAA-H-8083-3, FAA-S-8081-12, FAA-S-ACS-6; POH/AFM. Objective: To determine that the applicant exhibits instructional knowledge of the elements related to flight principles engine—inoperative by describing: 1. Meaning of the term "critical engine." 2. Effects of density altitude on the V MC demonstration. 3. Effects of airplane weight and center of gravity on control. 4. Effects of bank angle on V MC . 5. Relationship of V MC to stall speed. 6. Reasons for loss of directional control. 7. Indications of loss of directional control. 8. Importance of maintaining the proper pitch and bank attitude, and the proper coordination of controls. 9. Loss of directional control recovery procedures. 10. Engine failure during takeoff including planning, decisions, and single-engine operations. Task D: Maneuvering with One Engine Inoperative (AMEL and AMES) References: FAA-H-8083-3, FAA-S-8081-12, FAA-S-ACS-6; POH/AFM. Note: The feathering of one propeller can be demonstrated in any multiengine airplane equipped with propellers that can be safely feathered unless the manufacturer prohibits the intentional feathering of the propellers during flight. Feathering for pilot flight test purposes should be performed only under such conditions and at such altitudes (no lower than 3,000 feet above the surface) and positions where safe landings on established airports can be readily accomplished, in the event difficulty is encountered during unfeathering. At altitudes lower than 3,000 feet above the surface, simulated engine failure will be performed by throttling the engine and then establishing zero thrust. In the event a propeller cannot be unfeathered during the practical test, it should be treated as an emergency. Objective: To determine that the applicant: 1. Exhibits instructional knowledge of the elements related to maneuvering with one engine inoperative by describing:

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