AMSA 490 Final Exam – Practice Questions & Answers PDF 1 of 7 2026-03-23
AMSA 490 Final Exam –
Practice Questions &
Answers PDF
Page 1 of 7Guidehttps://www.stuvia.com/dashboard!@_)#*)(@$)($@*($@)($@*_Page 1 AMSA 490 Final Exam – Practice Questions & Answers PDF.pdf
, AMSA 490 FInal 2 of 7 2026-03-23
In order to carry cargo on the passenger level in a passenger Must be secured in bins that can withstand 1.15 times the emergency landing g loads
aircraft, the cargo or, alternatively, the cargo may be properly restrained behind a bulkhead
Landing gear aural warning devices must sound a warning if A landing is attempted with the gear not locked down
To be used in Part 121 operations, aircraft with more than 44 90 seconds or less
seats must be shown to be able to conduct an evacuation in
Transport category aircraft elevators typically are interconnected but may be operated separately in an emergency
The takeoff warning system of a transport category aircraft the aircraft is rotated for takeoff
must operate from the initial portion of the takeoff
(application of takeoff power) until
Under normal operating conditions, the pressurized cabin of 8,000 feet
a Part 121 aircraft must maintain a maximum cabin pressure
altitude of
Page 2 of 7 Page 2 AMSA 490 FInal.pdf
AMSA 490 Final Exam –
Practice Questions &
Answers PDF
Page 1 of 7Guidehttps://www.stuvia.com/dashboard!@_)#*)(@$)($@*($@)($@*_Page 1 AMSA 490 Final Exam – Practice Questions & Answers PDF.pdf
, AMSA 490 FInal 2 of 7 2026-03-23
In order to carry cargo on the passenger level in a passenger Must be secured in bins that can withstand 1.15 times the emergency landing g loads
aircraft, the cargo or, alternatively, the cargo may be properly restrained behind a bulkhead
Landing gear aural warning devices must sound a warning if A landing is attempted with the gear not locked down
To be used in Part 121 operations, aircraft with more than 44 90 seconds or less
seats must be shown to be able to conduct an evacuation in
Transport category aircraft elevators typically are interconnected but may be operated separately in an emergency
The takeoff warning system of a transport category aircraft the aircraft is rotated for takeoff
must operate from the initial portion of the takeoff
(application of takeoff power) until
Under normal operating conditions, the pressurized cabin of 8,000 feet
a Part 121 aircraft must maintain a maximum cabin pressure
altitude of
Page 2 of 7 Page 2 AMSA 490 FInal.pdf
