‘g’ figure that a normal person may experience ‘g’ induced loss of consciousness (G-LOC) ‘g’ limitations for the aircraft being flown aerobatic sequence performance parameters aerodynamic principles applicable to performing an aerobatic sequence aircraft limitations for aircraft flown airspeed limitations CASR Part 61 Manual of Standards Schedule 3 Aeronautical Knowledge relevant to aeroplane aerobatic sequences conditions under which gravity induced loss of consciousness (G-LOC) is likely to occur differences between grey out, black out and G-LOC effect of aircraft weight on VA and what precautions must be taken effect of increased ‘g’ loading on stall speed effect of increasing airspeed on stick force energy management principles applicable to aerobatic sequences engine speed (RPM) limitations for the aircraft flown environmental factors impacting on performing an aerobatic sequence factors that can reduce G-LOC tolerances factors that lead to increased density altitude go/no-go performance criteria hazards and consequences of performing aerobatics with blocked Eustachian tubes how to calculate the rolling ‘g’ limitation of an aircraft human factors applicable to aerobatic flight: physical fitness self-assessment in a Defence context, relevant Defence Orders and Instructions maximum rate turn criteria meaning of the term rolling ‘g’ meaning of the terms positive and negative ‘g’ minimum altitude to perform aerobatic manoeuvres minimum height required to recover from a spin in aircraft type being flown minimum height requirements to complete nose low (including pull through) to maintain above minimum height within aircraft normal operating parameters minimum radius criteria Mueller-Beggs emergency spin recovery technique physiological effects of positive and negative ‘g’ physiological effects of sustained and rapid changes of ‘g’ loading physiological factors that increase and reduce ‘g’ tolerance potential danger associated with conducting aerobatics at 500 ft AGL over unfamiliar terrain (Flight Activity Endorsement 4 only) potential danger associated with conducting aerobatics below 500 ft AGL over unfamiliar terrain (Flight Activity Endorsement 5 only) precautions that should be taken with regard to radius of turn when operating at a high-density altitude recovery technique to regain physiological and aircraft control from manoeuvre-induced disorientation regulatory requirements applicable to performing aerobatic sequences relationship between pre-stall buffet and rate of turn or rate of pitch relationship between tunnel vision and loss of consciousness relationship during rolling manoeuvres between pitch angle required on commencement of a roll and rate of roll relevant sections of Civil Aviation Safety Regulations and Civil Aviation Orders relevant WHS/OHS and environmental protection procedures and regulations rolling ‘g’ limitations for aircraft being flown structural irregularities that indicate an aircraft has been overstressed symmetrical positive and negative ‘g’ limits for aircraft being flown time period that disorientation may occur for, after recovery from G-LOC unusual attitude recovery techniques velocity speeds: manoeuvring speed (VA) velocity never exceed (VNE) normal operating range (VNO.). |