Aerodynamic Warnings Flashcards

1
Q

4 types of aerodynamic warning

A

~altitude alert sys
~over speed warning
~stall warning
~take off config warning sys

~flight envolope

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2
Q

Flight envolope protctions

A

Uses data from:
~ADIRU :AoA,speed,pitch,bank
~configuration :flap and slat position

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3
Q

FEP protecte parameters

A

~overspeed protection
~stall protection
~low energy protection
~bank angle limitation
~load g limitation

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4
Q

FEP philosophy

A

BOEING:
~pilots unlimate control

AIRBUS :control sys prevent manouvres outside of the normal operating envolope

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5
Q

Altitude alert sys

A

~alertrs the crew when approaching a pre selcted altitude
~alerts if deviate from the pre selcted altitude

All turbojet a/c and turbo pros over 5700kgsMTOM or with more than 9 pax seats ,need altitude alert sys

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6
Q
A

Altitude alerting is inhibited in flight whenevr g/s is captured in landing config

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7
Q

Stall waring inputs

A

~air direction detector or AoA vane/probe
~flaps and slats position
~air data computer or adirs
~thrust levers
~air ground logic swhicth

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8
Q

Airbus fly wire

A

~normal law: full protection
~altenate law: basic control laws but angle of attack and other protections may be lost
~direct law : relationship between inputs and control surface deflections
~mechanical law : the a/c can be controlled manually using the pitch trim and the rudder

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