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MILLER AVIATION > 310R General Info > Flashcards

310R General Info Flashcards

1
Q

At what temperature does the Heater Overheat Switch actuate?

A

325 degrees F (163 degrees C)

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2
Q

Can an over heated heater be turned back on from inside the cockpit?

A

No

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3
Q

How do you know when the heater has overheated?

A

An OVERHEAT amber warning light will illuminate

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4
Q

What happens automatically when the OVERHEAT amber warning light illuminates?

A

The heater is turned off.

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5
Q

Where is the location of the HEATER RESET SWITCH?

A

Accessible from the inside of the nose wheel well.

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6
Q

How long is the 310R

A

32 feet

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7
Q

How wide is the 310R?

A

37 feet

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8
Q

What is the Turning Radius of the 310R?

A

48.71 feet

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9
Q

Normal propeller clearance for the 310R?

A

10 and 1/3 inches

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10
Q

How many fuel tank sumps does N5336C have?

A

8

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11
Q

How many fuel tank sumps do our 310s have?

A

9 - N6309X

8 - N5336C

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12
Q

How many fuel pumps does N5336C have?

A

7 (N5336C) – 8 (N6309X)

(2) engine driven
(2) aux fuel pump
(2) main tank transfer
(1) wing locker transfer
(1) heater fuel pump

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13
Q

Where does the heater gets its fuel?

A

Draws from the airplanes fuel crossfeed system

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14
Q

Where are the trim tabs located on control surfaces?

A

Aileron - 1 on left
Elevator - 1 on right
Rudder - 1 lower

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15
Q

How many exits on the 310?

A

2 - entry door & pilot window

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16
Q

What kind of construction is the 310?

A

Semi-monocoat design

17
Q

What are the specifics on the props for the 310?

A

1) Verible pitch
2) Constant speed
3) Full Feather
4) Non-reversing

18
Q

What type of deice or anti-ice equipment do we have on the the 310?

A 
Wing Boots
Windshield heat
Pilot & Static heat
Stall warning heat
Prop heat
19
Q

When must fuel pumps be on?

A

Takeoff & climb (on low)
Descent & landing (on low)

Engine failure emergency (on high)

20
Q

What is the “Mechanical Interruption Summary Report.”

A

The PIC will submit to the Director of MX a report, all interruption to a flight.
Whereby, an unscheduled change of aircraft or stop was made, caused by a known or suspected MX difficulty or malfunction that are not required under Part 135.415.

21
Q

What instruments will be affected during Pitot/Static blockage?

A

Airspeed indicator
Altimeter
Vertical speed indicator

22
Q

What instruments will be affected during Gyro/Vacuum pump failure?

A

Attitude Indicator
D.G.
Turn Coordinator (unless electric)

23
Q

What type of deice can be used on the 310)?

A

Type 1

MILLER AVIATION (5 decks)

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