SOP Flashcards
What happens when the APU STAR/STOP SWITCHLIGHT is pressed during APU start?
- start light illuminates
- apu start status message is displayed
- 50% the start light and apu start status not displayed
What happens when the APU PWR/FUEl switch light is pressed during APU start?
– APU SOV OPEN status message is displayed.
– APU IN BITE status message is displayed (5-6 seconds).
– APU gauges displayed.
– APU DOOR MID/OPEN indication on ED-2.
What is the required flight deck emergency equipment required during the safety check?
Emergency rope -1 Escape hatch - 1 Flashlights - 2 Crash axe -1 Pbe-1 Life vests-3 Halon fire extiquisher-1 Crew o2 masks-3
Which aircraft documents are required on board for flight?
AFM/CDL Gear/ADG pins Mel/nef FMS pilot handbook/ EGPWS guide Dangerous goods & hazardous materials guide Airworthiness certificate Jeppesen airside set MX can/MX LOG QRH 1&2 Registration certificate Speed cards
During an engine failure Below 1000 ft AGL and no special procedure exists, what route should be flown?
Climb straight ahead to 1,000 feet then turn directly to the heading or NAVAID listed in the single engine procedure. If NAVAID is listed hold on the inbound radial right turns. If heading fly heading until safe ALT. Reaching 1000 ft radar vectors may be accepted.
What makes a simple special different from a special departure procedure?
A turn below 1000 feet may be required
Mandatory in IMC
mandatory in VMC until 1000 ft.
In IMC if vectors not available comply until 3000 ft
What is different about a complex special departure procedure from a simple special?
Usually to complex to fit on one line
Mandatory in IMC AND VMC
When is a new TLR required on a release with respect to the planned altimeter setting?
The actual QNH can not be more than .10 lower than the planned QNH.
Explain method 1
Method 1 requires that if an engine failure occurs anywhere between v1 and the destination the aircraft will be able to clear all obstacles by 1000 feet with 5 NM on either side while still maintaining 1.1% climb gradient available.
It also must be able to maintain a positive climb at 1500 feet above the destination airport.
Explain method 2
Method 2 provides that if engine failure occurs the aircraft will be able to drift down to an alternate airport and maintain 2000 feet above all obstacles with 5 nm each side of the route.
