C180H Float Plane POH Exam
The answers to these questions can be found in the Company Operations Manual, Aircraft Pilot Operating Handbook and the Aircraft documentation.
The Maximum Take-off weight on water is?
Which floats are on FUIG?
When using Cabin Heat, it is recommended:
To open the cabin air knob
Set the switch to automatic for heat and airflow
To only use one or the other
To close the cabin air knob
Minimum oil level to operate is..., and engine oil sump capacity is...?
9qt / 12qt
7qt / 12qt
8qt / 10qt
12 qt / 9qt
VFE on floats is:
Total Fuel Capacity and usable fuel in each tank respectively is:
65USG / 29USG
32.5USG / 30USG
80USG / 39.5USG
79USG / 32.5USG
The magneto check should be made at:
Maximum permissible difference between the two magnetos is:
The stall speed at 0 Degrees AOB and 60 Degrees AOB, respectively (Both Flaps UP) are:
65 Mph / 92 Mph
61Mph / 86Mph
64 Knt / 91 Knt
64Mph / 91Mph
The Main fuel strainer drain is located:
Lower front side of the firewall
At the right wing root
Below the pilots seat
At the left wing root
On take-off, the cowl flap setting should be:
Set to automatic
Describe the fuel system:
Fuel tanks in the belly with a positronic fuel flow system
Fuel tank in the left wing & in the belly with a mechanical pump system
Fuel tanks in each wing with a gravity fed system
Fuel tanks in each wing with a fuel pump to supply fuel to the engine
Normal configuration for take-off & landing is:
Water rudders down, Flaps 10
Water rudders up, Flaps 10
Water rudders up, Flaps 20
Water rudders down, Flaps 20
83 Kts, Flaps 10, Power 24"/2400RPM
83Mph, Flaps zero, Full Throttle
83Mph, Flaps 20, Full throttle
83 kts, Flaps up, Power 24"/24RPM
The minimum fuel grade to be used is:
During run-up, to exercise the propeller, the procedure is as follows:
The prop fully feathers, then back to full fine.
RPM decreases, MP increases, Oil pressure decreases.
Pull back propeller control consecutively until the RPM rises to 1200 RPM then back to full fine.
The first sign of RPM reduction, then back to full fine.
What fuel flow would you expect at 2500' with 23MP and 2300 RPM
Best glide speed with engine out and flaps zero is:
85 MPH IAS
65 MPH IAS
92 MPH IAS
78 MPH IAS
In flight you notice an excessive rate of discharge on your ammeter, you should:
Switch off the alternator
Switch off the ignition
Switch off the inverter
Confirm the alternator is on, confirm the alternator circuit breaker is in place, if so, turn of all the unnecessary electrics
The fuel shut off valve is located:
Under each wing
Lower left portion of the wing
to the left of the propeller control
In conjunction with the fuel selector valve
Maximum Cylinder head temperature is?
Normal oil operating Pressure is:
Stall speed at gross weight, flaps 40, 60 degrees AOB is:
The maximum allowable baggage in the aft compartment is:
Send me a copy of my responses.
Never submit passwords through Google Forms.
This content is neither created nor endorsed by Google.
Terms of Service