General Knowldge ATR 72 500 yn Flashcards
(62 cards)
Operation Engineering Bulletin
PWER LEVER AND CODITION LEVER FUNCTIONS PART 1:
PWER LEVER AND CODITION LEVER FUNCTIONS PART 2:
What is the purpose of Multi fuction Computers
– monitor, control, authorise operation of the aircraft systems
– manage system failures and flight envelope anomalies and command triggering of associated warning
Crew Centralized Alerting System, 3 visual devices used to indicate fault
– MASTER WARNING and MASTER CAUTION lights
– CREW ALERTING PANEL (CAP) lights
– LOCAL ALERT lights
6 conditions will illuminate T/O “Config” light on Crew Alerting Panel
6 types of Aural Alarms
Functions of “ENG BLEED” switch
“GRD X FEED” function
“OVHT” light indicates
ENG BLEED 1 (2) “Fault” light” indicates
BLEED “LEAK” light indicates
Requirements for PACK VALVE to operate
TEMP SEL “OVHT’ indicates
RECIRC FAN “FAULT’ incates
Flow pressure HIGH vs NORM
Limitation for FULL OPEN position
“FAULT” in center light indicates
“FAULT” on EXHAUST MODE
Max altitude AUTO PRESS will recall departue field elevation
Norm vs Fast descent rate
Maximum rate +/- manual mode
MODE SEL “FAULT” indicates
“MAN” indicates