Document ID: chunk:federal_register_of_legislation:F2019L01205:body:0:p4
Version: federal_register_of_legislation:F2019L01205
Segment Type: other
Provision Reference: 
Character Range: 8262–11274

with an automatic flight control system that simulates the operation of an autopilot fitted to a helicopter.
       4.11If the device is fitted with a traffic collision avoidance system (TCAS), activation of the TCAS must simulate activation of a TCAS fitted to a helicopter.
       4.12If the device is fitted with a terrain awareness warning system (TAWS), activation of the TAWS must simulate activation of a TAWS fitted to a helicopter.

    5 Flight control forces and control travel
       5.1Flight control forces on the device must simulate those of a multi-crew helicopter.
       5.2The device must have a cyclic control trim system operable in the pitch and roll axis by each of the FCMs.
       5.3 Flight control travel must simulate that of a multi-crew helicopter.
       5.4 Reactions to the operation of the flight controls must simulate the reactions of a multi-crew helicopter to its flight controls.

    6 Sound cues
        6.1Flight deck sounds in the device resulting from pilot actions or helicopter system malfunctions must simulate those of a multi-crew helicopter responding to the same actions or malfunctions.

    7 Visual display cues
       7.1The visual display of the device must produce at least a generic textured representation of ambient conditions, and be free of optical discontinuities that may create non-realistic visual cues.
       7.2 The visual display field of view must be not less than: 110° horizontally and 40° vertically.
       7.3 For each FCM, distance from the FCM's eye position to the surface of a direct view display must not be less than the distance from the FCM's eye position to the instrument panel.
       7.4The visual display must be capable of producing the same changes to runway or HLS perspective as arise in a multi-crew helicopter from changes to its height during:
(a) approach to a landing and a touchdown; and
(b) the hover; and
(c) lift off and departure.
       7.5 The visual display contrast ratio must be capable of the following:
(a) displaying variations in ground terrain;
(b) distinguishing landing sites, and runway and taxiway surfaces, at aerodromes;
       as they would appear to the FCMs of a multi-crew helicopter.
       7.6 The visual display brightness must be sufficient to support daylight, twilight and night environment conditions.

8 Motion cues — Reserved
Note   There is no requirement for motion cues.

9 Air traffic control environment simulation
       The device must be capable of generating at least 1 simulated automated airport weather reporting message of an Automated Terminal Information Service (ATIS) broadcast.

10 Navigation environment — replication of real-world operations
       10.1The navigation data and corresponding landing approach facilities programmed into a device must be capable of supporting scenario-based training designed to simulate operations in the environment of specific, real-world, locations.
       10.2The navigation database, and its supporting maps and charts for