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CVR CB requirements?
If possible NTSB incident, pull the CB, otherwise it is NORMAL
IF ED 1 fails, how is info desplayed>
Automatically on ED2
If primary is on ED2, how can ED2 info be displayed?
Change Display Control PANEL switch to EICAS.
If ECP fails, what 4 buttions remain active?
How is gear lowered if HYD 3 or gear circuitry fails?
- Manual release handle
- Upocks released
- Nose pulled in to place by dragassisted by HYD 2
- Mains freefall then MLG aux actuators assist
What temp do brakes turn white?
What temp to brakes turn RED?
Detents provided for thrust levers?
- SHUT OFF
- MAX POWER
Indication of starter cutout?
Approx 50% N2, AUTO IGNITION & ENG START msgs extinguish
What powers the FADEC?
- Below 50% N2, Aircraft elect sys powers FADEC
- Above 50% N2, Alternator on acces gearbox powers
How many channels does each FADEC have?
2, one in command and one in standby
How is MCT selected?
Operating thrust lever to CLIMB detent
Aborted start. When must MX be notified?
- ITT exceeds 815*C
- HOT ICON appears
Which ignition system does DC Batt Bus power?
What powers thrust reversers?
HYD 1 & 2
Pressing TOGA for go-around aprovides what?
- Current heading hold with 5* angle of bank
- Pitch 8*
Function of XFR switch on Radar Control panel?
Transfers control of display range to other side
When will ADG deploy?
During complete AC power failure
EMER FLAP swtich will extend the 700 to?
EMER FLAP switch will extend the 900 to?
MAx speed to use the EMER FLAP switch?