The Canadian Airlines DC-10 Flight Crew Operating Manual (FCOM) defines V1 as follows:
The Flight Crew Operating Manual and the Training Manual do not contain information on the unavailability of audio panel 2 when the aircraft emergency power switch is ON.
SDAs are not normally reviewed by pilots and do not require amendments of the pilots' source documents, the HS 748 Flight Manual and Crew Manual.
The DC-10 FCOM provides information on the amount of reverse thrust generated by each engine.
Students will learn not only what is written in cabin crew manual, but also from the trainer experience and tips too.
The CAI DC-10 FCOM and the OD43J Performance Manual also do not incorporate a performance-reduction correction for operations at below-sea-level pressure altitudes.
There may also be an anomaly between the sequencing of the evacuation command and signal as described in the Flight Attendants' Manual and the sequence outlined in the DC-10 Flight Crew Manual.
The aircraft manufacturer has indicated that it is possible to have failures in the system that will not result in the warning features outlined in the FCOM.
The DC-10 FCOM states than an ABS malfunction will cause the system to automatically disarm and to illuminate the AUTO BRAKE light and the MASTER CAUTION light.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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