Cessna 414/A Flashcards

0
Q

N2734B–Max Ramp Weight?

A

7140lbs

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1
Q

N5293J–Max Ramp Weight?

A

7140lbs.

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2
Q

N5293J–Max Takeoff Weight?

A

7085lbs

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3
Q

N2734B–Max Takeoff Weight?

A

7085lbs

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4
Q

N5293J–Max Landing Weight?

A

6750lbs

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5
Q

N2734B–Max Landing Weight

A

6750lbs

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6
Q

N5293J–Max Zero Fuel Weight?

A

6640lbs

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7
Q

N2734B–Max Zero Fuel Weight?

A

6520lbs

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8
Q

N5293J–Empty Weight?

A

5070lbs

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9
Q

N2734B–Empty Weight?

A

5062.5lbs

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10
Q

N5293J–Useful Load?

A

2070lbs

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11
Q

N2734B–Useful Load?

A

2078lbs

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12
Q

Fuel Quantity?

A

213- Total

206- Useable

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13
Q

Oil Quantity?

A

26 quarts total…12 per engine +1 in each filter

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14
Q

Oil requirements for flight?

A

9 quarts minimum

12 quarts for flights over 3 hours

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15
Q

N5293J–Engine Horsepower?

A

310 each side

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16
Q

N2734B–Engine Horsepower?

A

335 each side

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17
Q

Engine critical altitude?

A

20,000ft (due to turbocharger)

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18
Q

Max Wing Locker baggage weight?

A

200lbs per locker (2 total)

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19
Q

Max Aft Baggage?

A

400lbs

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20
Q

Max Aft Baggage rear bay?

A

100lbs

21
Q

Vso ?

A

71 KIAS

22
Q

Vs ?

A

81 KIAS

23
Q

Vmc ?

A

79 KIAS

24
Q

Vx ?

A

88 KIAS

25
Q

Vx/Vxse ?

A

98 KIAS

26
Q

Vy/Vyse ?

A

108 KIAS

27
Q

Max X-wind?

A

19 KIAS

28
Q

No Flap landing?

A

107 KIAS

29
Q

VLE/VLO ?

A

177 KIAS

30
Q

Vfe ?

A

(15°) 177 KIAS

(45°) 146 KIAS

31
Q

Vno ?

A

203 KIAS

32
Q

Vne ?

A

237 KIAS

33
Q

N2734B max speed with visible ice?

A

185 KIAS

34
Q

Engine failure during takeoff below Vmca?

A
  • Throttles…close
  • Maintain directional control
  • Brakes……as required
35
Q

Fire on the ground

A
  • Throttles…close
  • Brakes…as required
  • Mixture…idle cut off
  • Battery…off (use gang bar)
  • Magnetos…off (use gang bar)
  • Evacuate as soon as possible
36
Q

Engine Failure after Takeoff (98 KIAS gear up)

A
  • Mixture…Full Rich
  • Propellers…Full Forward
  • Throttles…Full Forward (38.0 inches)
  • Landing Gear…Check up
  • Inop Engine…Throttle closed…propeller feather…mixture idle cutoff
  • Bank…5° toward good engine
  • Climb…98 or 108 depending on obstacles
  • Trim Tabs…5° bank with 1/2 ball on TC
  • Cowl Flap…close on Inop engine.
  • Secure Inop engine…fuel off…mags off…alt off…land as soon as practical.
37
Q

Engine fail during flight (below Vmca)

A
  • Rudder…apply
  • Power…reduce to stop turn
  • Pitch attitude…lower nose to accelerate above Vmca
  • Inop engine prop…feather
  • Op engine…increase power as speed increases
  • Inop engine…secure
  • Trim…adjust 5° bank to good engine
  • Op engine cowl flap…adjust as required.
38
Q

Engine failure in flight (above Vmca)

A
  • Inop engine…determine
  • Operative Engine-Adjust as required.
  • Before securing inoperative engine…
  • Fuel flow-check…if deficient, aux fuel pump to high.
  • Fuel selectors–main tanks.
  • Fuel Quantity–check.
  • Oil pressure and Oil Temp–check.
  • Magneto switch–check ON.
  • Mixture–Adjust. Lean until manifold pressure begins to increase, then enrichen as power increases.
  • If engine does not restart, then proceed with engine feather and securing.
39
Q

Engine Inoperative Go-Around

A
  • Throttle–full forward (38.0 in Hg.)
  • Wing Flaps–up
  • Positive rate of climb–establish
  • Landing gear–up.
  • Cowl Flaps–open.
  • Climb at Vx or Vy depending on obstacles.
40
Q

Both Engines Failure during cruise flight

A
  • Wing Flaps–up
  • Landing Gear–up
  • Propellers–feather
  • Airspeed–120 KIAS
41
Q

In Flight Wing or Engine Fire

A
  • Both Aux fuel pumps–off
  • Operative engine fuel selector–main tank (Feel for detent)
  • Emergency cross-feed shutoff–off (pull up)
  • Appropriate engine–feather and secure.
42
Q

Inflight Cabin Electrical Fire or Smoke.

A
  • Electrical load–reduce
  • Fuel selectors–main tanks (feel for detent)
  • Emergency cross-feed shutoff valve–off (pull up)
  • Attempt to isolate the source of the fire or smoke.
  • Cabin Air Controls–OPEN all vents including windshield defrost…CLOSE if intensity of the smoke increases.
  • Pressurization Air contamination procedure–initiate if required.
  • Land and evacuate as soon as practical.
43
Q

Emergency Descent Procedure (Smooth Air)

A
  • Throttles–idle
  • Propellers–full forward
  • Mixture–Adjust for smooth engine operation
  • Wing Flaps–up
  • Landing gear–up
  • Moderate bank–initiate
  • Airspeed–235 KIAS (Vne)
44
Q

Emergency Descent Procedure (Turbulent Air)

A
  • Throttles–idle
  • Propellers–full forward
  • Mixture–adjust for smooth engine operation
  • Wing Flaps–down 45°
  • Landing gear–down
  • Moderate Bank–initiate
  • Airspeed–not to exceed 146 KIAS.
45
Q

Air Inlet or Filter Icing

A
  • Alternate Air Controls–pull out
  • Propellers–increase (2550 RPM for normal cruise)
  • Mixture–lean as required.
46
Q

Cabin Overpressure (over 5.3 PSI)

A
  • Pressurization Air controls–pull
  • If above 10,000–pull emergency oxygen knob, assure each occupant is using oxygen, and descend as soon as practical below 10,000 feet.
47
Q

Loss of Pressurization above 10,000 feet

A
  • Without supplementary oxygen–Emergency descent to 10,000 feet
  • With supplementary oxygen–pull emergency oxygen knob, assure each occupant is using oxygen, and descend as soon as practical below 10,000 feet
48
Q

Pressurization Air contamination

A
  • Pressurization air controls–pull LH and/or RH as necessary

* Proceed with loss of pressurization checklist.

49
Q

Spins

A

•Throttles–close immediately
•Ailerons–neutralize
•Rudder–Hold full rudder opposite the direction of rotation.
•Control wheel–Forward Briskly, 1/2 turn of spin after applying full rudder.
•Inboard engine–Increase power to slow rotation. (If necessary)
After Rotation has stopped:
•Rudder–neutralize.
•Inboard engine–decrease power (if used) to equalize engines.
•Control wheel–pull to recover from resultant dive. Apply smooth steady control pressure.