Operation of Systems Flashcards

1
Q

Describe Flight Controls (Primary and Secondary)

A

Primary:
Pitch: Stabilator - pulleys/cables to yoke.
Roll: Ailerons - pulleys/cables to yoke.
Yaw: Rudder - pulleys/cables to pedals.

Secondary:
Trim
Flaps

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2
Q

Power-plant

A

Lycoming IO-360-C

200hp @ 2700rpm
Fuel injected

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3
Q

Airframe

A

Aluminum Semi-monocoque

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4
Q

Stabilator

A

incorporates anti-servo tab

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5
Q

Ailerons & Rudder

A

Interconnected bus springs to help with adverse yaw

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6
Q

Flaps

A

Slotted.

Manual 4-position handle with push button on end to unlock:
F0 - 0°
F1 - 10°
F2 - 25°
F3 - 40°

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7
Q

Cowl flaps

A

Manual levers below throttle (don’t confuse with alternate air)

3-position:
- closed (up)
- intermediate
- open (down)

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8
Q

Alternate air

A

Manual 2-position levers immediately below pwr quadrant: closed (up) and open (down).

Air filter bypass

Heated by exhaust tube

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9
Q

Max CHT and Oil T

A

475°

245°

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10
Q

How to cool an overheated engine

A

v Pitch (reduce); ^ Airspeed (increase)
v Pwr (reduce)
^ Mix (enrich)
v open cowl flaps

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11
Q

Propellers

A

Counter rotating (left vs right engine)

Constant-speed / controllable pitch

Full feathering

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12
Q

How to Feather Propeller

A

Move Prop Control - FULL AFT

> 800 rpm

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13
Q

How is the propeller pitch controlled?

A

Controlled via the prop control lever adjusting the governor that control oil pressure to the prop hub.

High RPM / Low Pitch
- Oil pressure from governor (prop control)
- Aerodynamic force

Low RPM / High Pitch
- Counter weights

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14
Q

Anti-feathering lock

A

Centrifugal anti-feathering lock
- prevents feathering

impossible to feather < 800rpm

feather before 800rpm

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15
Q

Landing gear
- configuration
- retractable
- how is it held up/down
- actuation

A

Tricycle

Retractable - electric hydraulic pump

  • Held up with hydraulic pressure
  • naturally wants to come down due to gravity, aerodynamics, and spring assist
  • held down with spring loaded hooks
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16
Q

Landing gear is held up with…

A

…hydraulic pressure.

17
Q

What would happen if the landing gear system loss pressure or had a big leak?

A

The landing gear is held in the up position with pressure, so the landing gear would extend down if pressure was loss do to a leak.

The gear unsafe light may illuminate as the up limit switches are no longer contacted.

18
Q

Squat switch

A

left main gear

Oleo > 8” completes ePump circuit

“Horn” - up & on ground

19
Q

Gear warning horn

A

Power < 14” and landing gear is still up.

Gear lever is put in the up position with weight on wheels.

20
Q

How do the Nav Light affect the Landing Gear system?

A

The landing gear indicator light are automatically dimmed when the nav lights are on.

21
Q

What can be done if you don’t see landing gear indicator lights?

A

Turn off navigation lights.

Swap lights around incase it’s a bulb out.

Cycle gear.

Gear extension flow and checklist.
- CBs
-Master
- Alternator
- Nav lights
- <100 knots
- gear lever down
- pull em extension lever
- check indicator lights

22
Q

Gear indicators

A

3G - dn (nav lgts dim)
Red - unsafe
Horn - up <14” OR up w/ squat switch

Lights - pull & move if suspect burnt bulb

23
Q

Manual Gear Extension

A

CBs
Master
Alternator
Nav lgts
<100
check 3G
Gear lover down
Pull em lever

24
Q

Fuel System

A

98 tot / 93 use
100/130 octane

Sumps at low points
Outer tank (vented cap)
Inner tank
Selector on/off/crossfeed
Filter
ePump
Pump
Fuel distribution manifold
Injectors

Fuel P
F Flow

25
Q

X-Feed

A

“Xfeed” pulls fuel from other wing
- only use during level flight

“on” for to/ldg

26
Q

Oil

A

Air scoop > oil cooler > lower cowl

8 qt capacity
Replenish below 6 qt

27
Q

Electrical System

A

60-amp alternators from each engine

14 v voltage regulator

Warning lights

28
Q

When will the alternator warning lights activate?

A
29
Q

Avionics

A

Garmin GNSS 530W

30
Q

Flight Instruments

A
31
Q

Pitot-Static System

A
32
Q

Vacuum System

A

2x pumps

5” at 2000 rpm

< 4.5

Malf buttons

33
Q

Environmentals

A
34
Q

De-ice and Anti-ice

A
35
Q

O2 system

A