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Cessna 421 > Cessna 421 > Flashcards

Cessna 421 Flashcards

1
Q

Oxygen yellow arc

A

0 - 300 psi

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2
Q

Oxygen green arc

A

1500 - 1850 psi

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3
Q

Oxygen red line

A

2000 psi

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4
Q

Oxygen bottle size

A

11.0 cubic feet

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5
Q

Vacuum range

A

4.75” - 5.25”

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6
Q

Cabin pressurization limit

A

5.0 psi normal; 5.3 psi max

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7
Q

Gear Warning Horn

A
  1. < 15” MP
  2. > 15 degrees
  3. UP selected on ground
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8
Q

“LOW VOLT”

A

< 25 Volts

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9
Q

“CABIN ALT”

A

> 10,000 ft

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10
Q

“L or R FUEL LOW”

A

60 lbs (10 gals) of fuel remaining

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11
Q

Landing gear hydraulic pressure

A

1750 psi

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12
Q

Alternators

A

28 volts; 100 amps

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13
Q

Battery

A

24 volts; 26 amps

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14
Q

Voltammeter

A

L or R ALT = Load in amps
BATT = Discharge or Charge in amps
VOLTS = Batt bus voltage

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15
Q

Cabin Doorway and Instrument panel floodlights

A

15 minute timer

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16
Q

Heater overheat

A

325 degrees F

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17
Q

De-ice boots timer

A

6 secs tail; 6 secs wing; 45 secs total

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18
Q

Windshield Anti-ice

A 
High = < -12C
Low = -12C to 4.4C
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19
Q

Battery Relay

A

17 volts to close; 8 volts to keep closed

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20
Q

Overvoltage relay

A

Tripped at 32 V

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21
Q

Prop Anti-Ice Timer

A

20 Seconds each

  1. RH outboard
  2. RH inboard
  3. LH outboard
  4. LH inboard
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22
Q

Minimum Altitudes for Autopilot

A

Alt Select = 800’ AGL
Approach = 200’AGL
Maximum altitude loss approach = 100’

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23
Q

Autopilot max airspeed and flaps

A

230 KIAS and 30 degrees

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24
Q

Alternator out

A

Restrict load to 80% of rated load

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25
Q

Engine securing

A
  1. Throttle - Close
  2. Mixture - ICO
  3. Prop - Feather
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26
Q

Engine Failure during takeoff

Less than 100 KIAS or gear down

A
  1. Throttles - Close

2. Brake - As Required

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27
Q

Engine Failure during takeoff

Above 100 KIAS and gear up (or transit)

A
  1. Mixtures - Forward
  2. Props - Forward
  3. Throttles - Forward
  4. Gear - UP
  5. Inoperative Engine
    a. Throttle - Close
    b. Mixture - ICO
    c. Propeller - FX
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28
Q

Sudden Engine Roughness

A
  1. Power - Reduce immediately (both engines)
    a. MP - 32.5” max
    b. RPM - 1800 max
  2. Prop Sync - Off
  3. Rough Engine - Determine
  4. Problem - Analyze
  5. Rough Engine - Secure if cannot clear roughness
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29
Q

Engine Failure During Flight

> VMC

A
  1. Inop Engine - Determine
  2. Operative Engine - Adjust as required
  3. Fuel Flow - Check (Aux pump HI)
  4. Fuel Selectors - Main
  5. Fuel Quantity - Check
  6. Oil Pressure and Oil Temp - Check
  7. Magnetos - ON
  8. Mixture - Adjust
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30
Q

Engine Failure During Flight

< VMC

A
  1. Rudder - Apply towards operative engine
  2. Power - Reduce to stop turn
  3. Pitch - Lower to accelerate above VMCA
  4. Inoperative Engine - FX Prop
  5. Operative Engine - Increase power
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31
Q

Single Engine Go-Around

Speed > 111 KIAS

A
  1. Throttle - Full Forward
  2. Flaps - UP
  3. Gear - UP at Positive Rate
  4. Pitch at VYSE - 111 KIAS
  5. Trim - Adjust if needed
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32
Q

Both Engines Failure During Cruise

A
  1. Flaps - UP
  2. Gear - UP
  3. Props - FX
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33
Q

Engine Fire on the Ground

A
  1. Throttles - Close
  2. Brakes - As required
  3. Mixtures - ICO
  4. Battery - OFF (gang bar)
  5. Magnetos - OFF (gang bar)
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34
Q

Engine or Wing Fire in Flight

A
  1. Aux Fuel Pumps - Both OFF
  2. Fuel Selector - MAIN (operative engine)
  3. Emergency Crossfeed Shutoff - Pull
  4. Secure appropriate engine
    a. Throttle - Close
    b. Mixture - ICO
    c. Prop - FX
    d. Fuel selector - OFF
  5. Open guard and push FIRE LIGHT
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35
Q

Cabin Electrical Fire or Smoke

A
  1. Electrical Load - Reduce
  2. Fuel Selectors - MAIN
  3. Emergency Crossfeed Shutoff - Pull
  4. Attempt to isolate source of fire or smoke
  5. Cabin Air Controls
    a. OPEN - All Vents
    b. CLOSE - If smoke increased
  6. Pressurization Air Contamination Procedure - Initiate
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36
Q

Pressurization Air Contamination Procedure

A
  1. Pressurization Air Control(s) - Pull as necessary
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37
Q

Emergency Descent

Smooth Air; Preferred

A
  1. Throttles - Idle
  2. Props - FWD
  3. Mixtures - Adjust
  4. Flaps - UP
  5. Gear - UP
  6. Spoilers - Deploy
  7. Moderate Bank - Initiate
  8. Airspeed - 240 KIAS
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38
Q

Emergency Descent

Turbulent Air

A
  1. Throttles - Idle
  2. Props - FWD
  3. Mixtures - Adjust
  4. Flaps - Down 45 degrees
  5. Gear - Down
  6. Spoilers - Deploy
  7. Moderate Bank - Initiate
  8. Airspeed - 146 KIAS
39
Q

“HYD PRESS” illuminated after gear cycle

A
  1. Landing Gear - Recycle
  2. If still illuminated:
    a. Landing Gear - Down
    b. Gear HYD CB - Pull
    c. If light remains illuminated - Land as soon as practical
40
Q

Obstruction or Icing of Air Inlet Emergency Procedures

A
  1. Alternate Air Control(s) - Pull after loss of 3” MP
  2. Propeller(s) - Increase RPM (Avoid yellow arc)
  3. Mixture(s) - Lean as required
41
Q

Cabin Over Pressure

> 5.3 psi

A
  1. Pressurization Air Controls - PULL
42
Q

Impending skin panel or window failure

A
  1. Cabin pressurization switch - Depressurize
43
Q

Loss of pressurization above 10,000’

A
  1. Without supplementary Oxygen
    a. Emergency Descent to 10,000’
  2. With supplementary Oxygen
    a. O2 knob - Pull On
    b. Assure occupants using O2
    c. Descend to 10,000’ as soon as practical
44
Q

Spin Recovery

A
  1. Throttles - Close immediately
  2. Ailerons - Neutral
  3. Rudder - Full rudder opposite direction of rotation
  4. Control wheel - Full forward
  5. Inboard engine - increase power to slow rotation
    AFTER ROTATION
  6. Rudder - Neutralize
  7. Power - Equalize engines
  8. Control Wheel - Pull out of dive
45
Q

Manifold Pressure

Green arc and Maximum

A

Green Arc - 17.0 to 35.0” Hg

Maximum - 39.0” Hg (20,000)

46
Q

Oil Pressure

Min, Norm, and Max

A

Min - 10 PSI (red)
Norm - 30-60 PSI (green)
Max - 100 PSI (red)

47
Q 
Oil Temp (degrees F)
(Low, Cond, Norm, Cond, and Max)
A 
Low - 75 (red)
Cond - 85-140
Norm - 140-190
Cond - 190-240
Max - 240 (red)
48
Q

CHT (degrees F)

Cond, Norm, Cond, and Max

A

Cond - 200-320
Norm - 320- 400
Cond - 400-460
Max - 460 (red)

49
Q

EGT (degrees F)

Norm, Caution, and Max

A

Norm - 1300-1550 (green)
Caution - 1550-1650 (yellow)
Max - 1650 (red)

50
Q

Tachomter (RPM)

A

1600-1900 (green)
1900- 2185 (yellow) AVOID
2185-2235 (green)
2235 (red)

51
Q

Fuel Flow

A

Min - 0 pph (3.4 psi)

Max - 280.0 pph (19.2 psi)

52
Q

Fuel Quantity Indicator

Min and Slip duration

A

Min - 20 gallons each main for takeoff

Max slip duration - 30 secs

53
Q

Fuel Quantity - useable

Mains and Lockers

A

Mains - 206 gals
Lockers - 56 gals
Total - 262 gals

54
Q

Fuel Drains

A 
10 Total
     4 - Main tanks
     2 - Crossfeed
     2 - Fuel filter
     2 - Lockers
55
Q

Propeller Pitch Stops

A

Low - 16.6 degrees

Feather - 84.6 degrees

56
Q

Oil Capacity

A

13 quarts

57
Q

Oil quantity range

A

No less than 9 quarts

Normal - 10 quarts for < 3 hours

58
Q

Wing Locker Transfer

A

Transfer at 200-400 pounds used in mains

start close to 400 lbs

59
Q

Aux Fuel Pump Pressure

A

5.5 psi

60
Q

100LL Fuel Corrections

A

Fuel Flow - Increase by 2%

Fuel Quantity - Reduce by 4%

61
Q

Squat Switch

LH Main

A 
Ground - Energizes
1.  Gear warn horn - If control placed to UP
2. AC Fan - If placed to COOL
3. Pressurization safety valve - Holding it open
Grond - Deenergizes
1.  Landing gear control valve
2. Flight hour recorder (Hobbs)
3. Stall sensor vane to low heat
62
Q

Vfe

15, 30, and 45

A

176 KIAS - 15 degrees

146 KIAS - 30 and 45 degrees

63
Q

Va

A

151 KIAS

64
Q

Vlo

A

176 KIAS

65
Q

Vle

A

176 KIAS

66
Q

Vmca

A

73 KIAS

67
Q

Vyse

A

111 KIAS

68
Q

Vne

A

240 KIAS

69
Q

Vno

A

201 KIAS

70
Q

Vs1

A

79 KIAS

71
Q

Vso

A

70.5 KIAS

72
Q

Vg (Best Glide)

A

122 KIAS

at 7450 lbs

73
Q

Vxse

A

105 KIAS

74
Q

Vsse

A

100 KIAS

75
Q

Maximum demonstrated crosswind

A

17 Knots

76
Q

Vref

A

100 KIAS

77
Q

Maximum Ramp Weight

A

7629 lbs

78
Q

Maximum Takeoff Weight

A

7579 lbs

79
Q

Maximum Landing Weight

A

7200 lbs

80
Q

Maximum Zero Fuel Weight

A

6733 lbs

81
Q

Basic Empty Weight

N904BC

A

5470.10

82
Q

Maximum Operation Altitude Limit

A

With Oxygen - 30,000’

Without Oxygen - 25,000’

83
Q

Micro Vg

A 
106 Vgs
102 Vgs (Minimum)
84
Q

Maximum weight - Wing lockers

A

40 lbs each

85
Q

Maximum weight - Avionics bay

A

250 lbs minus installed equipment

= 169 lbs maximum

86
Q

Maximum weight - Nose bay

A

350 lbs minus installed equipment

= 333 lbs maximum

87
Q

Maximum weight - AFT Cabin (Bay A)

A

400 lbs (200 lbs per side)

88
Q

Maximum weight - AFT Cabin (Bay B)

A

100 lbs (50 lbs per side)

89
Q

Load factors

at 7450 lbs

A

Gear up, Flaps up = 3.6G to -1.44G

Gear down, Flaps 45 = 2.0G to 0G

90
Q

Wing Span

A

41.125 feet

91
Q

Prop Clearance

A

8.52 inches

92
Q

Wheel Base

A

17.38 feet

93
Q

Tire Pressures

A 
Mains = 80 psi
Nose = 35 psi
94
Q

Minimum Turning Distance

A

Wheel Base = 34.77 feet

Wing Tip = 58.51 feet

Cessna 421 (1 decks)

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