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CPL > 182RG Handling Notes > Flashcards

182RG Handling Notes Flashcards

1
Q

Engine

A

LYCOMING O-540-J3C5D

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2
Q

Power & RPM

A

235 BHP @ 2400rpm

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3
Q

Propeller

A

McCauley 82 inch diameter

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4
Q

Maximum Take-off and Landing Weight

A

3100 lbs (1406 kg)

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5
Q

Baggage (Max)

A

Area A & B combined: 90 kg
Area B: 36kg

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6
Q

Empty Weight:

A

863 kg (VH-MNX)

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7
Q

Oil Capacity

A

8 quarts useable min 5 quarts

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8
Q

Tyre Pressure

A

Mains: 68psi Nose: 50psi

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9
Q

Normal Cruise

A

22” 2300rpm 145kts

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10
Q

Total Fuel Capacity

A

302 litres (283 usable)

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11
Q

Flight Plan Fuel (Leaned)

A

55 litres per hour

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12
Q

Endurance (Leaned)

A

283ltrs@55ltrs
231 -45 =263mins

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13
Q

Demonstrated Crosswind

A

18kts

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14
Q

VNE

A

182

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15
Q

VNO

A

143

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16
Q

VA 3100lbs

A

112

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17
Q

VA 2550lbs

A

101

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18
Q

VA 2000lbs

A

89

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19
Q

VFE to 10° Flaps

A

140

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20
Q

VFE to 10° – 40° Flaps

A

95

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21
Q

VLO

A

140

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22
Q

VLE

A

140

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23
Q

Max Cylinder Head Temp

A

500°F (260°C)

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24
Q

Max Oil Temp

A

245°F (118°C)

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25
Q

Oil Pressure

A

Min: 25psi Max: 100psi

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26
Q

Fuel Pressure

A

Min: 0.5psi Max: 8.0psi

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27
Q

What operates the Landing Gear?

A

Retracted and extended by hydraulic actuators, powered by an electrically driven hydraulic pump.

The nose gear hydraulic actuator also operates a mechanical down lock upon extension of the nose gear. A positive mechanical uplock is actuated by a separate hydraulic actuator when the nose gear is retracted. The main gear has positive mechanical up and down locks, operated by separate hydraulic actuators.

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28
Q

How do the Landing Gear Lights Function?

A

Two position-indicator lights show that the gear is either up or down and locked.

The lights are the press-to-test type. The gear-down light (green) has two test positions. With the light pushed in half-way (throttle pulled out), the gear warning horn should sound intermittently, and with the light pushed full in, the light should illuminate.

The gear-up indicator light (amber) has only one test position. With the light pushed in, it should illuminate.

The indicator light contains dimming shutters for night operation.

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29
Q

When does the Landing Gear Horn sound?

A

Whenever the throttle is retarded below approximately 12” of manifold absolute pressure or wing flaps extended beyond 25o with landing gear retracted

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30
Q

Where is the Hydraulic Reservoir located?

A

Behind the central console.

A dipstick and filler are located on the LEFT side of the hydraulic pump

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31
Q

When should hydraulic fluid be added and what type?

A

When the fluid level is at or below the line marked ADD on the dipstick, hydraulic fluid (MIL-H-5606) should be added to the system

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32
Q

What should you do if the hydraulic pump continues to run after gear cycle completion (up or down)?

A

The 30-amp circuit breaker switch labelled GEAR PUMP should be pulled out

33
Q

What are the fuel selector positions and what should be used for climbing, descending, take-off and landing?

A

Left, Right, Both

Both should be used in those scenarios.

34
Q

Where is the Aux fuel pump switch and when should it be used?

A

The auxiliary fuel pump switch is located on the left side of the switch and control panel and is a rocker-type switch.

It should be used whenever the indicated fuel pressure falls below 0.5 PSI, but is not required when gravity flow and/or the engine- driven fuel pump can maintain indicated pressures above 0.5 PSI.

35
Q

What is the voltage of the electrical system and where is the battery?

A

A 28-volt, direct current system powered by an engine-driven alternator, supplies electrical energy. The 24 volt battery is located on the right forward portion of the firewall.

36
Q

What occurs if there is over voltage?

A

In the event an over-voltage condition occurs, the over-voltage sensor automatically removes alternator field current and shuts down the alternator.

The red warning light will then turn on, indicating to the pilot that the alternator is not operating and the aircraft battery is supplying all electrical power.

37
Q

What should you do if the voltage light illuminates?

A

The over-voltage sensor may be reset by turning the Avionics Master Switch off and then turning the MASTER switch off and back on again.

If the warning light does not illuminate, normal alternator charging has resumed; however, if the light does illuminate again, a malfunction has occurred and the flight should be terminated as soon as practical.

38
Q

What power settings should you have for take-off?

A

Mixture - Rich
Pitch - Fine
Throttle - Full

39
Q

What speed should you rotate?

A

55-60

40
Q

What height should you gear up?

A

Safe height: 200-300ft

41
Q

What power settings should you set in post take-off climb?

A

23” 2400rpm

42
Q

What speed should you climb out at?

A

90-100kts

43
Q

What speed should you rotate at with a crosswind?

A

Higher (65kts)

44
Q

What is the process for a short field take-off?

A
  • Flaps 20°
  • Full power rotate 50kts
  • Take-off safety speed 55kts by 50’
  • Initial climb speed 64kts
  • When obstacle cleared, nose down normal climb
45
Q

What is the process for a soft field take-off?

A
  • Flaps 20°
  • Full power
  • Raise nose wheel as soon as possible
  • Aim to be airborne at minimum speed
  • Lower nose once airborne
  • Allow speed to increase
  • Establish a positive rate of climb
  • Brakes ON, Retract GEAR, Retract FLAPS
  • Follow normal procedures
46
Q

What is the settings for a normal climb?

A
  • 90-100kts
  • 23” MP - 2400rpm
  • Cowl flaps open
  • Monitor manifold pressure
47
Q

What is the best settings for Best Rate climb?

A
  • 88kts (@ sea level)
  • Full throttle - 2400rpm
  • Cowl flaps open
  • Monitor manifold pressure
48
Q

What is the best settings for Best Angle climb?

A
  • 64kts (@ sea level)
  • Full throttle - 2400rpm
  • Cowl flaps open
  • Monitor manifold pressure
49
Q

What are the settings for a cruise?

A
  • Check cylinder head temperature
  • Close cowl flaps if temps are in green
  • Let aircraft accelerate to approx 100kts
  • Power to 22” MP - 2300rpm
  • Lean mixture
  • Note: Cowl flaps may be partially opened if necessary to maintain oil and cylinder head temperature within the normal operating range.
50
Q

What are the settings for a cruise descent?

A
  • Top of descent checks completed
  • Reduce power to obtain desired rate of descent (18” 2300rpm)
  • Cowl Flaps CLOSED
    Note: Recommended rate of descent - 500’/minute
51
Q

What are the settings for a glide descent?

A
  • Top of descent checks completed
  • Carb heat hot
  • Power to idle
  • Adopt the glide
  • Trim
52
Q

What are the glide speeds?

A

Gross weight:
(1409kg – 80kts)
(1159kg – 72kts)
(909kg – 64kts)

53
Q

What is the normal approach process?

A

Base:
- Carb heat: hot
- Reduce power
- Flaps 20°
- Adopt 70kts

Final:
- P.U.F.F. checks
- Carb heat: cold
- Full flaps
- Speed 65 – 70kts

54
Q

What is the flapless approach process?

A

Base:
- Carb heat: hot
- Reduce power
- Adopt 75kts

Final:
- P.U.F.F. checks
- Carb heat cold
- Reduce speed to 70kts short final
- Monitor rate of descent with small power changes
- Flatter approach with little or no round out

55
Q

What is the short field approach process?

A

Base:
- As for normal approach

Final:
- P.U.F.F. checks
- Carb heat cold
- Full flaps
- Reduce speed to 63kts
- Aim to round-out at threshold
- After landing smooth positive braking as required

56
Q

What is the baulked approach process?

A
  • Full power 2400rpm
  • Carb heat: cold
  • Establish climb
  • Gear up
  • Flaps up
  • Adjust MP and rpm
  • Trim
57
Q

What do you do if the gear doesn’t extend?

A
  • Slow aircraft to below 140kts
  • Pull landing gear pump circuit breaker
  • Gear selector DOWN
  • Extend pump forward
  • Pump up and down (approx. 20 times) until steady GREEN light illuminates and resistance is felt
  • Check visually gear is down
  • Reset landing gear pump circuit breaker

WARNING: DO NOT operate landing gear electrically with manual system engaged.

58
Q

What do you do if the gear doesn’t retract?

A
  • Master Switch - ON
  • Landing Gear Lever – CHECK UP
  • Landing Gear and Gear Pump
  • Circuit Breakers – IN
  • Gear Up Light – CHECK
  • Landing Gear Lever – RECYCLE
  • Gear Motor – CHECK operation (ammeter and noise)
  • If the gear fails to retract or intermittent and the gear up light is present:
  • If period of one minute following gear handle retraction actuation, pull the hydraulic pump circuit breaker to prevent the electric motor from overheating
  • Re-engage the circuit breaker just prior to landing
59
Q

What are the phase one checks if you have engine failure during take-off roll?

A

Throttle: Idle
Brakes: Apply

60
Q

What are the phase one checks if you have engine failure immediately after take-off?

A

Lower Nose
Landing Area within 30°
Gear Down
Flap as required

61
Q

What are the phase one checks if you have engine failure during flight?

A

Airspeed: 80kts
Fuel Selector Valve: Both
Carby Heat: Hot

If restart has not occured:

Mixture: Rich
Auxiliary Fuel Pump: On
Ignition Switch: Both (Start if prop has stopped)

62
Q

What are the phase one checks if your gear doesn’t retract?

A

Gear Lever: Recycle
Master: On

63
Q

What are the phase one checks if your gear doesn’t extend?

A

Gear Pump Circuit Breakers: Check/Reset
Master: On
Gear Lever: Recycle

64
Q

What are the phase one checks if you have engine fire during start?

A

Ignition: Start/continue cranking

65
Q

What are the phase one checks if you have engine fire on the ground and your engine doesn’t start?

A

Throttle: Full Open
Mixture: Idle Cutoff
Cranking: Continue
Fuel Selector Valve: Off
Auxiliary Fuel Pump: Off

66
Q

What are the phase one checks if you have engine fire during flight?

A

Mixture: Idle Cutoff
Fuel Selector Valve: Off
Auxiliary Fuel Pump: Off
Master: Off

67
Q

What are the phase one checks if you have electrical fire during flight?

A

Master: Off
Vents, Cabin Heat and Air: Closed
Avionics: Off
All other switches (except ignition): Off
Activate Fire Extinguisher

68
Q

What are the phase one checks if you have cabin fire during flight?

A

Master: Off
Vents, Cabin Heat and Air: Closed
Activate Fire Extinguisher

After fire extinguished, ventilate cabin

69
Q

What are the phase one checks if you have wing fire during flight?

A

Landing/Taxi Lights: Off
Navigation Lights: Off
Strobes: Off
Pitot Heat: Off

70
Q

What is the clean stall speed?

A

42kts

71
Q

What is the 10° stall speed?

A

40kts

72
Q

What is the 30° stall speed?

A

37kts

73
Q

What is the process for a 45° AOB turn?

A

Mixture: Rich
Pitch: 2400 RPM
Throttle: 23”
Small Backpressure

74
Q

What is the process for a 60° AOB turn?

A

Mixture: Rich
Pitch: 2400RPM
Throttle: Full
Backpressure as you roll through 45°

75
Q

What is the process for a steep descending turn?

A

Mixture: Rich
Carby: Hot
Throttle: 15” and settle
Throttle: Idle
Gear: Down
45° AOB turn maintaining 95-100kts

76
Q

What is the process for a baulked approach?

A

Power: Full
Gain Speed
Flap: 20°
Gear: Up
Flap: 10°, hold, fully retracted
Normal Climb

77
Q

What is the process for a clean stall?

A

HASELL
Carby Hot
Power 15” and settle
Stay straight and level
Power Idle
Stall horn: carby cold
Stall recovery

78
Q

What is the process for a landing configuration stall?

A

HASELL
Carby hot
Power 15”
140kts - Gear down and verify
Flap 10°
White arc - flap 40°

79
Q

What is the stall recovery for a landing configuration stall?

A

Stall horn: Carby cold
Full power with opposite rudder to wing drop.
Nose down gain speed.
Flap 20°
Gear Up
Flap 10°, hold, flap fully retracted
Climb out

CPL (2 decks)

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