Document ID: chunk:federal_register_of_legislation:F2015L01428:body:0:p3
Version: federal_register_of_legislation:F2015L01428
Segment Type: other
Provision Reference: 
Character Range: 5411–8462

thrust that are normally encountered in the flight of a multi-crew aeroplane, and that give rise to changes in the following:
(a) aeroplane attitude;
(b) thrust;
(c) drag;
(d) altitude;
(e) aeroplane configuration.

3 Ground reaction and handling
       3.1The ground reaction and ground handling models of the device (the models) must enable sound and visual systems to simulate the touchdown effects of a multi-crew aeroplane.
       3.2The stopping and directional control forces of the models must enable simulation of dry runway conditions.

4 Aeroplane systems
       4.1Aeroplane systems of the device, as used in training, must simulate those of a multi-crew aeroplane.
       4.2 The systems must be functionally correct to simulate specified normal, non‑normal and emergency operating procedures to be carried out by FCMs during training.
       4.3 The systems must simulate system operations, including interdependencies, both on the ground and in flight.
       4.4Circuit breakers operated in the conduct of MCC training must be functionally accurate and simulate the functions of circuit breakers in an aeroplane.
       4.5 Instrument indications must automatically respond:
(a) to simulated flight control movements by an FCM; and
(b) to simulated atmospheric disturbance;
       as they would in a multi-crew aeroplane.
       4.6 For subclause 4.5, numerical values displayed or otherwise conveyed by the instruments must be presented in units relevant to a multi-crew aeroplane.
       4.7 The device must simulate the following multi-crew aeroplane systems:
(a) the communication system;
(b) the navigation system;
(c) the caution and warning system.
       4.8 The simulated systems mentioned in subclause 4.7 must include the following:
(a) a headset-capable communications system that is integrated with the crew oxygen system for each FCM;
(b) a method of identifying selected navigation aids;
(c) push-to-transmit switches for each FCM, installed on the flight controls;
(d) a system which enables each FCM to select the radio frequency that he or she intends to use;
(e) a system which enables the instructor to know if each FCM is transmitting on the correct frequency.
       4.9 Approach to a simulated aerodynamic stall must be indicated in the same way as it is indicated in a multi-crew aeroplane.
       4.10 Activation of the traffic collision avoidance system (TCAS), and the terrain awareness warning system (TAWS) must be simulated in the same way as in an aeroplane.
       4.11 Activation of the anti-icing system must be simulated in the same way as in a multi-crew aeroplane.

    5 Flight control forces and control travel
       5.1Flight control forces on the device to simulate those of a multi-crew aeroplane, may be produced by active or passive arrangement.
Note   Passive arrangement does not modify control forces with changes in aircraft flight conditions. Active arrangement modifies control forces with changes in aircraft flight conditions.
       5.2Flight control travel must simulate that of a