Canadian Aviation Regulations — 604.170
604.170 (1) The aircraft operation component of the training program for flight crew members shall include procedures for the normal, abnormal and emergency operation of an aircraft and its systems and components, including the following elements: (a) aircraft performance during take-off, climb, cruise, holding, descent, landing and diversion; (b) calculations of the aircraft’s take-off and landing distances and speeds, and the aircraft’s fuel consumption, weight and centre of gravity; (c) the flight characteristics of the aircraft, including any abnormal characteristics that are applicable to the aircraft, such as dutch roll, buffet boundary onset and aircraft upset; (d) the effects of airframe and engine icing and the use of de-icing and anti-icing equipment; (e) flight planning and instrument flight procedures, including (i) departure, enroute, holding, arrival and diversion procedures, (ii) precision, non-precision and missed approaches in minimum visibility conditions, with the flight director in automatic mode and in degraded states of operation, and (iii) circling approaches, if applicable; (f) pre-flight checks of the interior and exterior of the aircraft; (g) the use of aircraft checklists; (h) aircraft manoeuvres on the ground; (i) normal, crosswind, noise abatement and maximum performance take-offs and landings; (j) take-offs and landings on contaminated runways; (k) rejected take-offs and landings; (l) steep turns; (m) approach to a stall and recovery from a stall; (n) the operation of the Flight Management Computer System (FMCS), Ground Proximity Warning System (GPWS), Terrain Awareness and Warning System (TAWS), Traffic Alert and Collision Avoidance System (TCAS), Airborne Collision Avoidance System (ACAS) and any other specialized equipment installed in the private operator’s aircraft; (o) the execution in VMC of one collision avoidance manoeuvre in response to a GPWS or a TAWS warning, if the aircraft is equipped with a GPWS or a TAWS; (p) the operation of navigation and communication equipment; (q) the actions to be taken in the event of hydraulic, electrical and other system failures; (r) the actions to be taken in the event of flight control failures and, in the case of an aircraft with split control capability, briefings on degraded states of operation while in flight and during take-off and landing; (s) the actions to be taken in the event of aircraft fire on the ground or in the air; (t) the actions to be taken in the event of engine fire and engine failure while in flight; (u) the recognition of and recovery from turbulence and windshear during an approach, landing and take-off; (v) the actions to be taken in the event of an emergency evacuation of passengers and crew; (w) the actions to be taken in the event of pilot incapacitation while in flight and during take-off and landing; (x) crew resource management; (y) if the private operator provides the training using a flight simulator, the performance of one balked landing initiated in the low-energy regime using the same simulator; (z) in the case of a pressurized aircraft, the actions to be taken in the event of loss of pressurization and emergency descent; (z.1) in the case of a three-engine or four-engine aircraft, take-off, landing and flight with the critical engine inoperative or with two other engines inoperative, including driftdown and engine-inoperative performance capabilities; and (z.2) in the case of a helicopter, (i) hovering manoeuvres, slope landings and confined areas, (ii) autorotations, (iii) transmission and main gear box faults and failures, and (iv) tail rotor, tail rotor drive and tail rotor gear box faults and failures. (2) When the training referred to in subsection (1) is provided on board an aircraft in flight, the private operator shall have procedures to ensure that situations are simulated or presented, and actions are simulated or performed, so as to not adversely affect the safety of the aircraft, its occupants or any othe