2.
Determines that the terrain below the aircraft is suitable for a safe touchdown.
3.
Performs autorotation from a stationary or forward hover into the wind at recommended altitude, and RPM, while maintaining established heading, –10°.
4.
Touches down with minimum sideward movement, and no rearward movement.
5.
Exhibits orientation, division of attention, and proper planning.
B. TASK: POWER FAILURE AT ALTITUDE
REFERENCES: AC 61-13; Helicopter Flight Manual.
NOTE: Simulated power failure at altitude shall be given over areas where actual touchdowns can safely be completed in the event of an actual powerplant failure.
Objective. To determine that the applicant:
1.
Exhibits knowledge of the elements related to power failure at altitude.
2.
Establishes an autorotation and selects a suitable landing area.
3.
Establishes proper aircraft trim and autorotation airspeed, –5 knots.
4.
Maintains rotor RPM within normal limits.
5.
Compensates for windspeed and direction as necessary to avoid undershooting or overshooting the selected landing area.
6.
Terminates approach with a power recovery at a safe altitude when directed by the examiner.
C. TASK: SYSTEMS AND EQUIPMENT MALFUNCTIONS
REFERENCES: AC 61-13; Helicopter Flight Manual.
Objective. To determine that the applicant:
1.
Exhibits knowledge of the elements related to causes, indications, and pilot actions for various systems and equipment malfunctions.
2.
Analyzes the situation and takes action, appropriate to the helicopter used for the practical test, in at least three of the following areas—
a.
engine/oil and fuel.
b.
hydraulic, if applicable.
c.
electrical.
d.
carburetor or induction icing.
e.
smoke and/or fire.
f.
flight control/trim.
g.
pitot static/vacuum and associated flight instruments, if applicable.
h.
rotor and/or antitorque.
i.
various frequency vibrations and the possible components that may be affected.
j.
any other emergency unique to the helicopter flown.
D. TASK: SETTLING-WITH-POWER
REFERENCES: AC 61-13; Helicopter Flight Manual.
Objective. To determine that the applicant:
1.
Exhibits knowledge of the elements related to settling-with-power.
2.
Selects an altitude that will allow recovery to be completed no less than 1,000 feet (300 meters) AGL or, if applicable, the manufacturer’s recommended altitude, whichever is higher.
3.
Promptly recognizes and announces the onset of settling-with-power.
4.
Utilizes the appropriate recovery procedure.
E. TASK: LOW ROTOR RPM RECOVERY
REFERENCES: AC 61-13; Appropriate Manufacturer’s Safety Notices; Helicopter Flight Manual.
NOTE: The examiner may test the applicant orally on this TASK if helicopter used for the practical test has a governor that cannot be disabled.
Objective. To determine that the applicant:
1.
Exhibits knowledge of the elements related to low rotor RPM recovery, including the combination of conditions that are likely to lead to this situation.
2.
Detects the development of low rotor RPM and initiates prompt corrective action.
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本文链接地址：PRIVATE PILOT Practical Test Standards for ROTORCRAFT HELICO(17)
