G’day Guys,
Doing a Navajo rating and require a bit of in sight into the aircraft.
The aircraft has vortex generators and the serial no. is greater than 31 - 7812001;
The Max landing light speeds
The optimum glide speed for the aeroplane and a/c config
Waste gate failure procedure
Cold start procedure
The RPM for the governing system
Recommended climb power setting / IAS /and fuel flow
A typical 65% power setting , IAS and fuel flow at 5000’ pressure height
Location of fuel tank and drain points
The position of the fuel tank vents
Describe the priming system and it’s use
Where are the fuel boost pump/auxiliary pump’s located in the aircraft
Are these electrical or mechanical the fuel pumps
What conditions apply to tank selection for takeoff and landing
When refueling to less than full tanks, what restrictions apply and how is the fuel quantity checked
Describe the cross feed system
Normal hydraulic capacity
Minimum oil quantity before flight
The max quantity of oil
Minimum and normal engine oil temperatures
What effect will full flap have on VMCA
What is the fuel flow rate with one engine shut down at 1000 AMSL on an ISA day
What prevents the engine from being over boosted
Describe the propeller governing system
If the oil pressure to the prop dome is lost, does the prop go into coarse or fine pitch
How many brake applications would be expected from a fully pressurized brake accumulator
Which if any, ancillary system(s) will be lost if the left/right engine was shut down, and the propeller feathered
What is the fuel consumption of the heater
Which flight instrument are operated electrically
Which instruments are operated by vacumn
And does anyone have any fuel flows to used as a rough guide or SAR's????
Cheers,
DW
