414A Flashcards

(47 cards)

1
Q

What model, type and horsepower are the engines on the 414a?

A

Model - TSIO-520-NB
Type - Turbo-charged, fuel injected, direct drive, air-cooled, horizontal opposed, 6 cylinder, 520 cubic inch displaced
HP - 310 HP at 2700 RPM and 38 inches MP

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2
Q

What is the height, width, and length of the 414a?

A

H - 11 feet
W - 44 feet
L - 36 feet

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3
Q

What is the normal prop tip ground clearance?

A

Less than a foot

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4
Q

What type of props are on the 414a?

A

Constant speed, full feathering, non-reversing, hydraulically actuated

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5
Q

What type of fuel does our 414 use?

A

100 AV fuel (green)

100 Low Lead (blue)

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6
Q

Max weight capacity of nose baggage compartment?

A

350 pounds

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7
Q

Max ramp weight?

A

7140 pounds

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8
Q

MAX takeoff weight?

A

7100 pounds

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9
Q

Max landing weight?

A

6750 pounds

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10
Q

What is the is total max luggage weight for both aft baggage sections (Bay A and B)?

A

500 pounds

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11
Q

What is the total fuel capacity of our 414a, how many tanks and their respective fuel quantities?

A

206 gallons

2 tanks - 103 gallons each

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12
Q

What is the total Oil Capacity of each engine?

A

13 quarts

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13
Q

What is the minimum oil capacity to operate?

A

9 quarts

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14
Q

What is the Vmc?

A

68 kts

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15
Q

What is Vy?

A

108 kts

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16
Q

What is Vne?

A

237 kts

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17
Q

What is Vr?

A

95 kts

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18
Q

What is Vbg?

A

120 kts

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19
Q

What is the normal operating range for the Tachometer?

A

2100 - 2450 (green arc)

20
Q

What is the normal operating range for the Manifold Pressure gauge?

A

17.0 - 31.5 inches Hg (green arc)

21
Q

What is Max oil temp?

A

240 degrees F

22
Q

What is the Max Cylinder Head Temp?

A

460 degrees F

23
Q

What is the minimum fuel flow?

24
Q

How many exits, and their locations?

A

2 – entry door (air stair door at rear of cabin), over right wing exit

24
How many exits, and their locations?
2 -- entry door (air stair door at rear of cabin), over right wing exit
25
What is the minimum fuel capacity per tank for departure?
20 gallons
26
What is the MAX pressurization limit for the cabin?
5.3 PSI
27
Cabin is to be depressurized during....?
1) Takeoff 2) Landing 3) Ground operations 4) Inflight when both engines are operating on hot air
28
What memorization item is there for the cabin over-pressurization (higher than 5.3 PSI)?
1) Pressurization Air Controls (Pull) | 2) If above 10,000 feet altitude without Supplementary O2 -- Initate Emergency Descent below 10,000 feet
29
What is the lift off speed (Vr)?
95 kts
30
What is the Cruise Climb setting for the 414a?
2450 RPM and 31.5 inches Hg
31
If an obstruction ahead requires a steep climb angle, the airplane should should be flown at the "all engines best-angle-of-climb speed" with flaps up and max normal operating power?
88 kts at sea level | 92 kts at 20,000
32
Make sure the aircraft does not exceed ______ pound before attempting to land?
6750 pounds
33
What is the empty weight of the 414a?
4628 pounds
34
What is the zero-fuel weight of the 414a?
5535 pounds
35
When preflighting the aircraft, what (2) items need to be checked in the nose compartment?
1) Fluid level of hydraulic reservoir | 2) Nitrogen pressure gauge
36
How many detents on the fuel selector?
3 / main, cross-feed, off
37
How are the brakes powered?
Hydraulics
38
What do you do if after retracting the gear the HYD PRESSURE LIGHT remains on?
1) Cycle Gear switch 2a) Gear down 2b) Gear Hyd CB PULL 2c) Land
39
What are the emergency fuel pump positions?
High, off, low
40
How many times can the gear be blown down?
Once
41
What is the max weight for luggage in the wing lockers?
200 pounds
42
How di you check the gear warning horn?
Gear up... | Flaps > 15%, THT < 17"
43
Where is the Static Source Selector?
Piolt Lower LH panel
44
Where is O2 handle?
Pilots Lower LH Panel
45
Where is the battery located?
LH stub wing
46
How many drains per side?
4 2-tanks 1-sump 1-cross feed