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Printed page 3. PDF page 11.
briefings included the corrected altitudes and amended FPA. The approach was to be coupled-selected 10 with a manual landing. During the descent, the flight crew discussed the holding requirements and then contacted the CYHZ terminal controller to request a holdOpen official document at PDF page 11Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 4. PDF page 12.
reported. The flight crew continued the approach and, at about 0022, the landing lights were selected OFF, which turned the lamps off. Less than a minute later, AC624 contacted the tower to confirm that the runway lights were on settingOpen official document at PDF page 12Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 5. PDF page 13.
the vertical speed/flight path angle (V/S-FPA) knob on the flight control unit, the PF selected FPA mode; the aircraft was now being flown with the FPA selected to 0.0°. 16 At 0027, the PM began the countdown for the distanceOpen official document at PDF page 13Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 6. PDF page 14.
time, the aircraft crossed over a lighted facility. At 0029:47, the landing lights were selected ON, followed in very quick succession by the PF disconnecting the autopilot 18 an automated call of “100,” an automated call of “50,” and theOpen official document at PDF page 14Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 10. PDF page 18.
annunciator, which appears across the top of the PFD, is the primary indicator of the selection status of the flight control unit. The flight mode annunciator displays the autothrust mode, the vertical and lateral modes of the autopilot and flightOpen official document at PDF page 18Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 11. PDF page 19.
the primary interface between the flight crew and the autoflight system for short-term selection (Figure 3), is located in the centre area of the glare shield. Flight crew operation of the flight control unit can modify any current flight parametersOpen official document at PDF page 19Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015