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Printed page 11. PDF page 19.
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 parameters temporarily and can also select operational modes for theOpen official document at PDF page 19Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 32. PDF page 40.
1.15.1.1 Crew injuries The captain had a minor head injury consistent with hitting the glare shield. The FO had a head injury and a serious injury to the right eye, consistent with the FO's upper body twisting to the leftOpen official document at PDF page 40Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 69. PDF page 77.
assembly 2.9.1 Captain Although the captain wore his restraint system, his head struck the glare shield. During the impact sequence, the captain would have been exposed to intermittent acceleration forces as the aircraft struck the ground twice and slid alongOpen official document at PDF page 77Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 70. PDF page 78.
flung about. At some time during the impact sequence, the captain's head struck the glare shield because there were insufficient acceleration forces to lock the shoulder harness and prevent movement of his upper body. 2.9.2 First officer The first officer'sOpen official document at PDF page 78Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 74. PDF page 82.
threshold. 10. At some time during the impact sequence, the captain's head struck the glare shield because there were insufficient acceleration forces to lock the shoulder harness and prevent movement of his upper body.Open official document at PDF page 82Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015
Printed page 75. PDF page 83.
sustained a head injury and serious injury to the right eye as a result of striking the glare shield because the automatic locking feature of the right-side shoulder-harness inertia reel was unserviceable. 12. A flight attendant was injured by aOpen official document at PDF page 83Aviation Investigation Report A15H0002: Collision with terrain, Air Canada, Airbus Industrie A320-211, C-FTJP, 29 March 2015