Document ID: chunk:federal_register_of_legislation:F2025C00050:body:0:p217
Version: federal_register_of_legislation:F2025C00050
Segment Type: other
Provision Reference: 
Character Range: 751877–755429

the aircraft flown;
        5.        how to calculate the rolling 'g' limitation of an aircraft;
        6.          relationship during rolling manoeuvres between pitch angle required on commencement of a roll and rate of roll;
        7.        engine RPM limitations for the aircraft flown;
        8.        physiological effects of positive and negative 'g';
        9.          the 'g' figure that a normal person may experience 'g' induced loss of consciousness (G‑LOC);
       10.          differences between grey out, black out, and G-LOC;
       11.         conditions under which G-LOC is likely to occur;
       12.          time period that disorientation may occur for after recovery from G‑LOC;
       13.      factors that can reduce G-LOC tolerances;
       14.        physiological effects of sustained and rapid changes of 'g' loading;
       15.        relationship between tunnel vision and loss of consciousness;
       16.        hazards and consequences of performing aerobatics with blocked eustachian tubes;
       17.        physiological factors that can reduce 'g' tolerance;
       18.          physical actions that may increase 'g' tolerance;
       19.         minimum altitude to perform aerobatic manoeuvres;
       20.          relationship between pre-stall buffet and rate of turn or rate of pitch;
       21.        effect of increasing airspeed on stick force;
       22.         structural irregularities that indicate an aircraft has been overstressed;
       23.       effect of increased 'g' loading on stall speed;
       24.         airspeed limitations;
       25.         VA, VNE and VNO;
       26.         effect of aircraft weight on VA and what precautions must be taken;
    (za) recovery from manoeuvre-induced disorientation;
    (zb) how to assess personal fitness for aerobatic flight;
    (zc) maximum rate turn criteria;
    (zd) minimum radius criteria.

FAE-2 Aerobatics — 1,500 ft AGL

 1.                     Unit description
This unit describes the skills and knowledge required to design and plan an aerobatic routine and conduct aerobatics safely not below 1,500 ft AGL.

 1.                     Elements and performance criteria
     1.               FAE-2.1 – Design an aerobatic routine
            1.        design a sequence of aerobatic manoeuvres that meet a specified requirement, involve practical transitions between manoeuvres, and identify performance parameters that will ensure safe completion of all manoeuvres not below 1,500 ft AGL;
            2.        identify performance parameters based on a combination of aircraft attitude, power setting, altitude and speed that provide go-no go guidance for safe completion of all manoeuvres not below 1,500 ft AGL within the physical limitations of the pilot and structural limitations of the aircraft.
     2.               FAE-2.2 – Plan an aerobatic performance
            1.        identify the stakeholder requirements for the aerobatic sequence and formulate a plan to safely present the sequence, meeting the specified requirements;
            2.        ensure any required aerobatic approvals are appropriate, valid and current;
            3.         analyse prevailing and forecast weather and apply wind velocity, visibility and cloud base to ensure safe and accurate aerobatic performance;
            4.        identify the 'aerobatic box' when appropriate, and plan manoeuvres to remain within the box;
            5.        modify aerobatic performance if weather conditions cause (or controlling authority