Cessna 185F Flashcards

1
Q

Maximum Speed at Sea Level

A

140 KIAS

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2
Q

Cruise, 75% Power at 7000 Ft

A

133 KIAS

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3
Q

75% Power at 7000 FT,
84 Gallons Usable Fuel
Range? Time?

A

585 NM, 4.5 Hrs

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4
Q

Maximum Range at 10000 FT,
84 Gallons Usable Fuel
Range? Time?

A

745 NM, 7.4 Hrs

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5
Q

Rate of Climb at Sea Level

A

960 FPM

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6
Q

Service Ceiling

A

16,400 Ft

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7
Q

Takeoff Performance
Water Run?
Total Distance Over 50-Ft Obstacle?

A

1430 Ft
2125 Ft

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8
Q

Landing Performance
Water Run?
Total Distance Over 50-Ft Obstacle?

A

830 Ft
1565 Ft

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9
Q

Stall Speed (KCAS)
Flaps Up, Power Off
Flaps Down, Power Off

A

56 KNOTS
52 KNOTS

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10
Q

Maximum Weight
Ramp?
Takeoff or Landing?

A

3332 Lbs
3320 Lbs

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11
Q

Standard Empty Weight
185 Skywagon Floatplane?
185 Skywagon II Floatplane?

A

2002 Lbs
2052 Lbs

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12
Q

Maximum Useful Load
185 Skywagon Floatplane?
185 Skywagon II Floatplane?

A

1330 Lbs
1280 Lbs

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13
Q

Baggage Allowance

A

170 Lbs

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14
Q

Wing Loading: Pounds/Sq Ft

A

19.1

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15
Q

Power Loading: Pounds/HP

A

11.1

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16
Q

Fuel Capacity: Total

A

88 Gal

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17
Q

Oil Capacity

A

13 Qts

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18
Q

Engine: Description

A

Teledyne Continental, Fuel Injection
IO-520-D

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19
Q

Engine: Horsepower
5-Minute Takeoff Rating
Maximum Continuous Rating

A

300 BHP at 2850 RPM
285 BHP at 2700 RPM

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20
Q

Propeller: Derscription

A

3-Blade Constant Speed
Diameter: 80 In

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21
Q

Dimensions of the Cessna 185
Wing width
Tail width
Float width
Height
Length

A

36 Ft
11 Ft
7’10” Ft
12’2” Ft
27 Ft

22
Q

Vne

A

184 KIAS

23
Q

Vno

A

149 KIAS

24
Q

Va
3320 Pounds
2820 Pounds
2320 Pounds

A

3320 Pounds, 117 KIAS
2820 Pounds, 109 KIAS
2320 Pounds, 99 KIAS

25
Q

Vfe
10 degrees flaps
20 degrees flaps
30-40 degrees flaps

A

10 degrees flaps, 120 KIAS
20 degrees flaps, 110 KIAS
30-40 degrees flaps, 90 KIAS

26
Q

Flap Limitations
Approved Takeoff Range
Approved Landing Range
Wing flaps immediately after balked landing

A

0 to 20 degrees
0 to 40 degrees
Must be retracted to 20 degrees

27
Q

Water rudder always ____ except _______ taxiing

A

up, water

28
Q

In floatplane, avoid ______ with flaps extended

A

Slips

29
Q

Engine failure after takeoff
Wings flaps up?
Wing flaps down, 20 degrees?

A

70 KIAS
65 KIAS

30
Q

Maximum Glide
3320 Lbs
2820 Lbs
2320 Lbs

A

3320 Lbs: 75 KIAS
2820 Lbs: 69 KIAS
2320 Lbs 63 KIAS

31
Q

Precautionary landing with engine power, Flaps down

A

65 KIAS

32
Q

Landing without engine power
Wing Flaps Up
Wing Flaps Down

A

Wing Flaps Up: 75 KIAS
Wing Flaps Down: 70 KIAS

33
Q

Engine Failure During Takeoff Run (5 Steps)

A
  1. Throttle- Idle
  2. Control wheel- Full Aft
  3. Mixture- Idle Cut Off
  4. Ignition Switch- OFF
  5. Master Switch- OFF
34
Q

Emergency Landing on Water Without Engine Power (10 Steps)

A
  1. Airspeed- 75 KIAS (flaps UP), 70 KIAS (flaps DOWN)
  2. Mixture- Idle Cut Off
  3. Fuel shutoff Valve- OFF
  4. Ignition Switch- OFF
  5. Master Switch- OFF
  6. Water Rudders- UP
  7. Wing Flaps- As required
  8. Doors- Unlatch prior to approach
  9. Touchdown- Slightly Tail Low
  10. Control Wheel- Hold Full Aft as floatplane decelerates.
35
Q

Emergency Landing on Land Without Engine Power (10 Steps)

A
  1. Airspeed- 75 KIAS (flaps UP), 70 KIAS (flaps DOWN)
  2. Mixture- Idle Cut Off
  3. Fuel shutoff Valve- OFF
  4. Ignition Switch- OFF
  5. Master Switch- OFF
  6. Water Rudders- UP
  7. Wing Flaps- As required (40 degrees recommended)
  8. Doors- Unlatch prior to approach
  9. Touchdown- Level Attitude
  10. Control Wheel- Full Aft (after contact)
36
Q

What are the three operating conditions on the maximum glide chart?

A

1) Propeller windmilling
2) Flaps Up
3) Zero wind

37
Q

Takeoff:
Normal Climb Out?
Maximum Performance, Flaps 20, Speed at 50 Feet?

A

Normal Climb Out: 70 KIAS
Maximum Performance, Flaps 20, Speed at 50 Feet: 63 KIAS

38
Q

Enroute Climb, Flaps Up:
Normal
Best Rate of Climb, Sea Level
Best Rate of Climb, 10,000 Feet
Best Angle of Climb, Sea Level
Best Angle of Climb, 10,000 Feet

A

Normal: 85-95 KIAS
Best Rate of Climb, Sea Level:
83 KIAS
Best Rate of Climb, 10,000 Feet:
76 KIAS
Best Angle of Climb, Sea Level:
68 KIAS
Best Angle of Climb, 10,000 Feet:
69 KIAS

39
Q

Landing Approach
Normal Approach, Flaps Up
Normal Approach, Flaps 40
Maximum Performance Approach, Flaps 40

A

Normal Approach, Flaps Up:
70-80 KIAS
Normal Approach, Flaps 40:
60-70 KIAS
Maximum Performance Approach, Flaps 40: 65 KIAS

40
Q

Balked Landing: Maximum Power, Flaps 20

A

60 KIAS

41
Q

Maximum Recommended Turbulent Air Penetration Speed:
3320 Lbs
2820 Lbs
2320 Lbs

A

3320 Lbs: 117 KIAS
2820 Lbs: 109 KIAS
2320 Lbs: 99 KIAS

42
Q

Maximum Demonstrated Crosswind Velocity:

A

13 Knots

43
Q

Normal Climb (1 Step)

A

Airspeed- 85-95 KIAS

44
Q

Maximum Performance Climb (1 Step)

A

Airspeed- 83 KIAS (sea level) to 76 KIAS (10,000 feet)

45
Q

Before Landing (3 Steps)

A

1) Water Rudders- UP
2) Wing Flaps- 40 degrees
3) Airspeed- 60-70 KIAS

46
Q

Landing (2 Steps)

A

1) Touchdown- Slightly Tail Low
2) Control Wheel- Hold Full Aft as floatplane decelerates to taxi speed

47
Q

After Landing (1 Steps)

A

1) Water Rudders- DOWN

48
Q

Securing Airplane (1 Step)

A

1) Fuel Selector Valve - Left Tank or Right Tank

49
Q

Satisfactory engine cooling has been demonstrated for this floatplane with an outside air temperature _____ above standard.

A

23 C

50
Q

How are the water rudders connected to the rudder pedals?

A

Cables and springs

51
Q

Where is the datum located?

A

Front face of the firewall

52
Q

What is the CG range?

A

34.8 inches to 46.5 inches