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Swissair 111

Printed page 5. PDF page 17.

months. 1.5 Personnel Information 1.5.1 General The SR 111 flight crew consisted of a captain and a first officer. The cabin crew consisted of a maƮtre de cabine (M/C) and 11 flight attendants. A flight operations officer provided standard flight
Open final report at PDF page 17TSB A98H0003: In-flight fire leading to collision with water

Swissair 111

Printed page 6. PDF page 18.

FACTUAL INFORMATION 1.5.2.1 Captain The pilot-in-command (captain) of SR 111 was described as being in good health, fit, and not taking any prescribed medication. He was described as someone who created a friendly
Open final report at PDF page 18TSB A98H0003: In-flight fire leading to collision with water

Swissair 111

Printed page 7. PDF page 19.

FACTUAL INFORMATION Based on a review of the captain's medical records, there was no indication of any pre-existing medical condition or physiological factors that would have adversely affected his performance during the flight. H
Open final report at PDF page 19TSB A98H0003: In-flight fire leading to collision with water

Swissair 111

Printed page 21. PDF page 33.

The left window diffuser slide control is located in the left ceiling liner behind the captain's position, just inboard of the left aft window. 17 For the purposes of this report, the pressure vessel or pressurized portion of the aircraft
Open final report at PDF page 33TSB A98H0003: In-flight fire leading to collision with water

Swissair 111

Printed page 28. PDF page 40.

and 3 are on the left side; DUs 4, 5, and 6 are on the right side (see Figure 11). The captain's DUs (DUs 1, 2, and 3) receive display information from display electronic unit (DEU) 1, and the first
Open final report at PDF page 40TSB A98H0003: In-flight fire leading to collision with water

Swissair 111

Printed page 31. PDF page 43.

and airspeed) are located in the centre of the lower instrument panel for use by the captain or first officer (see Figure 11). There was no provision for a self-contained, independent electrical power supply for standby communication and electronic navigation
Open final report at PDF page 43TSB A98H0003: In-flight fire leading to collision with water