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Airplanes > T182-T > Flashcards

T182-T Flashcards

1
Q

Wingspan

A

36’

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2
Q

Wheel span

A

9’

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3
Q

Engine

A

Lycoming TIO-540-AK1A

Turbocharged, air cooled, fuel injected,

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4
Q

Horsepower

A

235 BHP @ 32” MAP & 2400rpm

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5
Q

Fuel capacity

A

Total
92 Gal / 87 Usable

Each Tank
46 Gal / 43.5 Gal Usable

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6
Q

Oil capacity

A

8 Qt sump
9 Qt total
4 Qt Minimum for flight

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7
Q

Ramp weight

A

3110 lbs

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8
Q

Takeoff Weight

A

3100 lbs

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9
Q

Landing Weight

A

2950 lbs

(150 lbs / 25gal 100LL below max t/o)!

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10
Q

Baggage area weight limit

A

200 lbs total (A + B + C)
A - 120 lbs
B - 80 lbs
C - 80 lbs

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11
Q

VNE

A

175 KIAS

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12
Q

VNO

A

140 KIAS

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13
Q

VA

A

3100 lbs - 110 KIAS
2600 lbs - 101 KIAS
2100 lbs - 92 KIAS

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14
Q

VFE

A

Flaps 0-10 deg -—-140 KIAS
Flaps 10-20 deg — 120 KIAS
Flaps 20-Full ——- 100 KIAS

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15
Q

Airspeed Indicator Markings

A

White Arc:
41–100 Kts (Vso to Vfe full flap)

Green Arc:
51–140 Kts (Vs to Vno)

Yello Arc:
140–175 (Vno to VNE)

Red line
175 (VNE)

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16
Q

Tachometer marking

A

Green range
2000–2400 rpm

Red Arc
2400–2700 rpm

Note: 2400 rpm is max operating limit

17
Q

Manifold Pressure marking

A

Green Arc
S.L - 15,000 Ft
15”-28”

15,000ft - 20,000ft
15”-27”

Red Arc
32”-35”

Note: 32” MAP is max operating limit

18
Q

Max Glide airspeed

A

3100 lbs - 75 KIAS
2600 lbs - 69 KIAS
2100 lbs - 62 KIAS

19
Q

Making Power changes in flight, increasing power

A

Avoid High Manifold Pressure and Low RPM.

Increasing Power: increase rpm first, then manifold pressure

20
Q

Making Power changes in flight, decreasing power

A

Avoid High Manifold Pressure and Low RPM

Decreasing Power: Decrease Manifold Pressure, then decrease rpm

21
Q

Takeoff: Normal

Power setting & Procedure

A

Flaps 0-20 Deg

Throttle: 32” MAP
Propeller: 2400 RPM
Mixture: 24 GPH

Rotate @ 50-60 Kts
Climb @ 70 (flaps 20) or 80 Kts (flaps up)

22
Q

Takeoff: Short Field

Power Setting & Procedure

A

Flaps: 20 Deg
Brakes: Hold

Throttle: Full
Propeller: 2400 Rpm
Mixture: 24 GPH

Elevator hold Tail-Low
Climb @ 60 Kts until obstacles are cleared
Accelerate to 70 before raising flaps

23
Q

Enroute Climb: Normal

Power Setting & Procedure

A

Airspeed 90-100 Kts

Throttle: 25” MAP
Propeller: 2400 RPM
Mixture: 16 GPH

Fuel Selector: Both
Cowl Flaps: Open (as required)
Oxygen Control: Open (as required)

24
Q

Enroute Climb: Max Performance

Power setting & Procedure

A

Airspeed: 84 Kts @ Sea Level
80 Kts @ 20,000 ft

Throttle: 32” MAP
Propeller: 2400 RPM
Mixture: 24 GPH

Fuel Selector: Both
Cowl Flaps: Open
Oxygen Control Lever: On (as required)

25
Q

Cruise

Power Setting & Procedure

A

Power:

S.L. to 15,000ft:
Throttle:15”-28” MAP
Propeller: 2000-2400 RPM
Mixture: Lean for desired Perform or Econ

15,000 to 20,000ft: 
Throttle: 15”-27” MAP 
Propeller: 2000-2400 RPM
Mixture: Lean for desired Perform or Econ
Cowl flaps: Closed
Oxygen: monitor quantity if in use
26
Q

Descent:

Power Setting & Procedure

A 
Power: As Desired
Mixture: Adjust as Necessary for smooth engine operation 
Cowl Flaps: Closed
Fuel Selector: Both
Flaps: As Desired 
(0-10 DEG below 140Kts)
(10-20 DEG below 120Kts)
(20 Deg-full below 100Kts)
27
Q

Leaning procedure

A

In cruise, 50 deg Rich of Peak using the G1000 Lean Assist

Or: 50 deg rich of 1685 degrees (Hunter’s) airplane

28
Q

Fuel Vapor Procedures for Ground Operations

A

If engine roughness is observed and fuel vapor formation is suspected, increase rpm to 1800-2000 for 1-2 minutes,

Alternatively, switch on fuel pump until just before takeoff

If symptoms persist, select opposite fuel tank

29
Q

Cowl Flap Operation

A

Cowl Flap: Open during Start, Ground Operations, Climb

Cowl Flaps: Closed during Cruise (referencing CHT), Extended Descent

30
Q

Preferred Propeller RPM in Cruise

A

2200 RPM

Airplanes (6 decks)

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