Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p350
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 1216027–1219481

with deck loading limits.
1.3                    Helicopter landing sites (HLS)
1.3.1              Recall the standards recommended for "basic" and "secondary" helicopter landing sites (HLS).
1.4                    Explain ground effect, Vne and retreating blade stall.
1.5                    Rotor disc behaviour under reduced/negative "g"
1.5.1              Explain the relationship between cyclic input, disc attitude, rotor hub and shaft position and fuselage responsiveness on a teetering head helicopter system under 1 "g", negative "g" and normal disc loading conditions.
1.6                    Control power
1.6.1              Explain the term "control power" and how it relates to aircraft performance.
1.7                    Dynamic rollover
1.7.1              Explain each of the following:
(a)           what is dynamic rollover; and
(b)           how to avoid dynamic rollover; and
(c)           how to correct in a dynamic rollover situation.
1.8                    Loss of tail rotor effectiveness (LTE)
1.8.1              Explain each of the following:
(a)           the phenomenon of LTE; and
(b)           factors that contribute to LTE (high density altitude, high gross weight, turning down wind at low airspeed i.e. below the speed for minimum powered level flight, exceeding manufacturer recommended relative wind and operating gross weight limits); and
(c)           indications of LTE; and
(d)           recovery from LTE.
1.9                    Height-velocity curve
1.9.1              Explain the implications of flying inside the helicopter height-velocity curve.
1.10                Blade contamination
1.10.1          Explain the degradation of performance with contamination on rotor blades (e.g. mud picked up by rotor wash during hovering operations).

Unit 2.3.4 AAGG:  aerial application rating – gyroplane endorsement

1. Aircraft performance

1.1 Environmental effects
         1.1.1 Explain how loads and turn rate affect aircraft performance (airspeed, rotor RPM, disc angle of attack, inertia).
    1.1.2 Explain ground effect and its impact on aircraft performance.
    1.1.3 Explain possible aerodynamic and controllability effects associated with load dumping.
         1.1.4 Explain how temperature, height above mean sea level (AMSL), pressure, humidity, weight, field surface and relative wind affect each of the following:
     (a) lift-off distance;
     (b) climb angle;
     (c) rate of climb;
     (d) landing stop distance.
         1.1.5 Explain how temperature, height above mean sea level (AMSL), pressure, and humidity affect power available and power required.

1.2 Determine payload
 Determine the following using information from the aircraft flight manual:
     (a) the maximum payload and fuel that may be carried;
     (b) calculation of CG under different load configurations.

1.3 Height-velocity diagram
         1.3.1 Explain the implications of flying inside the gyroplane height-velocity diagram.
    1.3.2 Explain the implications of allowing speed to decay behind the power curve.

1.4 Rotor disc behaviour
    1.4.1 Explain rotor disc behaviour under negative 'g'.
    1.4.2  Explain the effect of rapid load reduction on the rotor disc and aircraft performance.

1.5 Rotor blade contamination
         1.5.1 Explain the degradation of performance with contamination on rotor blades (e.g. mud picked up by rotor during operations).

2. Flight and duty times
2.1 Explain the flight and