Oral Review Flashcards

(118 cards)

1
Q

What are the privileges of a multi-engine rating?

A
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2
Q

What are the requirements to obtain a multi-engine rating?

A
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3
Q

How does this affect the commercial certificate or the instrument rating?

A
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4
Q

If you receive training in a multi-engine aircraft without a published Vmc, what limitation is placed on your certificate? How is this limitation removed?

A
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5
Q

What is the rated horsepower of the Seminole?

A

180 hp

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6
Q

What is the rated engine speed of the Seminole?

A

2700 rpm

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7
Q

What type of propellers are on the Seminole?

A

2 blade constant speed, controllable pitch, full feathering Hartzell propellers

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8
Q

What is the minimum feathering rpm?

A

950

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9
Q

Why is there a minimum feathering rpm?

A
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10
Q

What is the fuel capacity of the Seminole?

A

110 gallons, 55 per wing tank

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11
Q

What is the usable fuel capacity of the Seminole?

A

108 gallons, 54 per wing tank

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12
Q

What is the minimum octane?

A

100/130- green; 100LL-blue

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13
Q

What is the maximum oil capacity?

A

8 quarts

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14
Q

What is the minimum oil quantity for flight?

A

6 quarts

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15
Q

What is the maximum ramp weight?

A

3816 lbs.

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16
Q

What is maximum T.O. weight?

A

3800 lbs.

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17
Q

What is the maximum landing weight?

A

3800 lbs.

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18
Q

What is the maximum allowable baggage?

A

200 lbs.

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19
Q

What is the definition of Vsse?

A

Intentional OEI Speed - the minimum speed selected by the manufacturer for intentionally rendering one engine inoperative in flight for pilot training

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20
Q

Engine out absolute ceiling

A

approx. 5,000 feet

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21
Q

Engine out service ceiling (50 fpm)

A

approx. 3,900 feet

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22
Q

Two engine rate of climb (sea level)

A

1340 fpm

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23
Q

Engine out rate of climb (sea level)

A

210 fpm

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24
Q

Heater output

A

45,000 BTU

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25
Instructional cruise power
21" MAP, 2300 RPM
26
Engine out cruise
25" MAP, 2500 RPM
27
Engine out climb power
Full power
28
Engine-out zero sideslip
2-3 degrees bank toward operating engine; 1/2 dot ball toward operating engine
29
VS0
55 KIAS
30
VMC
56 KIAS
31
VS1
57 KIAS
32
VX
82 KIAS
33
VY
88 KIAS
34
VSSE
82 KIAS
35
VXSE
82 KIAS
36
VYSE
88 KIAS
37
VA (3800 lbs.)
135 KIAS
38
VA (2700 lbs.)
112 KIAS
39
VFE
111 KIAS for full flaps
40
VLE
140 KIAS
41
VLO (extending)
140 KIAS
42
VLO (retracting)
109 KIAS
43
VNO
169 KIAS
44
VNE
202 KIAS
45
Storm window speed
129 KIAS
46
How many red lines are there? What numbers do they represent?
2; VMC and VNE
47
What does the blue line on the ASI denote?
VYSE
48
What is the maximum demonstrated crosswind component?
17 KIAS
49
What are the gyro suction limits?
4.8"-5.2" Hg
50
What is the first indication of an engine failure?
A yawing and rolling tendency toward the inoperative engine
51
What steps must be taken if an engine failure occurs during flight below VMC?
1. Retard throttles 2. Rudder and bank toward operating engine 3. Lower the nose to increase airspeed 4. Maintain directional control
52
When is the gear extended before landing with one engine inoperative?
Final descent to landing (when landing assured)
53
What is the final approach speed and configuration on one engine?
90 KIAS, gear down, flaps 25
54
What restrictions are there to crossfeeding?
Level flight only
55
What is the purpose of the red gear unsafe light?
The warning gear unsafe light operates anytime the gear position and the gear selector switch disagree
56
When does the gear horn sound?
- on the ground with the gear down and selector switch up - anytime either throttle is below 14" MAP and all 3 gear are not down and locked - anytime 25 degrees or more of flaps are extended and all 3 gear are not down and locked
57
What should be done if section is below 4.3" Hg?
Increase power by descending or be aware that the attitude indicator and directional gyro will not operate correctly; increase RPM's to 2700
58
How is a vacuum pump failure noted?
The red button annunciator on the vacuum gauge will show in case of a feathered engine or vacuum pump failure
59
What instruments are powered by the vacuum pump?
Attitude indicator and vacuum gauge since one vacuum pump remains inoperative
60
What happens if the heater overheats?
Red heater over temp annunciator light on the instrument panel will illuminate
61
What is the primary indication the heater is overheating and what can be done to remedy the situation?
Cold air coming in the cabin; nothing can be done until the aircraft is on the ground. The reset button is on the heater unit itself in the nose compartment.
62
What could cause the heater to overheat?
Blockage of the air intake valve due to snow, ice, or other foreign obstruction
63
What is the maximum allowable RPM drop during the feathering check in the runup?
500 RPM
64
What is the ground limitation for pitot heat?
Off except for short intervals to remove ice
65
What is the limit on cranking the starter?
30 seconds on, 2 minutes minimum off
66
What is the normal magneto drop during the runup and what are the limitations?
100 RPM drop is normal, 175 RPM drop apiece is allowed with a differential of 50 RPM
67
What should be done if the cylinder head temperature becomes too hot? (greater than 500 F)
Reduce power, open cowl flaps, and enrichen the mixture, lower nose if climbing
68
What holds the gear up in the retracted position?
Hydraulic pressure
69
What happens if the hydraulic system malfunctions or leaks?
The gear extends slowly
70
Why are the prop controls pushed forward before landing?
To provide maximum power simply by adding full throttle in the event of a go-around
71
What are the 12 factors that affect Vmc?
critical engine inoperative, inop engine windmilling, up to 5 degrees bank toward op engine, landing gear retracted, aft CG, max gross weight, max power on op engine, sea level, flaps TO position, cowl flaps TO position, trimmed for TO, ground effect negligible
72
What is VMCA?
The minimum flight speed at which the airplane is directionally controllable with one engine inoperative
73
What does basic empty weight include?
Optional equipment, full oil and unusable fuel, hydraulic and brake fluid
74
What happens to the CG as fuel is burned or the gear retracted?
The CG is not significantly affected
75
How many fuel tanks does the Seminole have and where are they located?
2 tanks. 1 behind each engine (in the nacelle)
76
What is the fuel capacity of each tank?
55 gallons total, 54 gallons usable
77
How many fuel pumps total are there?
70 & 71: 6 total- 2 engine driven, 4 electric (2 for heater) 72 & 73: 5 total- 2 engine driven, 3 electric (1 for heater)
78
What is the purpose of carburetor heat?
Carb heat provides heated air to the carburetor in the event of icing and also serves as the alternate source of engine air
79
What is the temperature range where carb ice is most likely to occur?
-7 C to 21 C; also when relative humidity is high
80
How many cowl flap settings are there?
3 - full open, full closed, intermediate
81
What is the advantage of counter-rotating props?
This eliminates the "critical engine" and lowers VMCA
82
What is the critical engine?
The engine whose failure most adversely affects the aircraft, i.e. the one with the shortest moment arm thus requiring less resisting force to maintain directional control
83
What controls the pitch of the prop?
Oil pressure supplied by the governor and nitrogen from the propeller dome. Oil pressure sends the propeller toward the high rpm or unfeather position, nitrogen and a large spring send the prop toward the low rpm or feather position and prevents over speeding
84
What is the precharge pressure of the unfeathering accumulator?
70-75 PSI (depending on temperature)
85
How long does it take for the prop to feather?
10-17 seconds
86
What is the PSI in the prop governor?
200-300 PSI
87
What kind of gear system is installed in the Seminole?
electrically controlled/activated, hydraulically actuated
88
How long does gear take to cycle?
6-7 seconds
89
How is the gear held in the extended position?
Down locks hooks, springs maintain force on each hook
90
What happens when the emergency gear extension is used?
Hydraulic pressure is released and the gear freefalls
91
Where is the gear pump and reservoir located?
In the tail section
92
Where is the squat switch?
Left main gear
93
Is the hydraulic reservoir for the brakes the same as for the gear?
No, the brake reservoir is in the nose compartment
94
What are the possible flap settings on the Seminole?
0, 10, 25, 40
95
How are the flaps actuated?
Manually
96
What are the limitations on crossfeed?
Level flight only and only one engine
97
What is the electrical system on the Seminole?
70 & 71: batt- 35 amp-hr, 12 V; 2 belt-driven alts- 70 amp, 14 V 72 & 73: 2 batts- 13.6 amp-hr, 24 V; 2 alts- 65 amp, 28 V
98
What happens if the alternator voltage becomes too high?
The overvoltage relay trips the alternator off automatically and the alternator overvoltage light illuminates (72 & 73: 32 V voltage regulator will kick off alternator)
99
What should be done if the alternator overvoltage light illuminates?
Check circuit breakers, turn the alternator switch off and then back on to reset the alternator, reduce the electrical load and monitor the ammeter
100
Where is the external power plug located and what is it's purpose?
Under the nose on the right side; allows current to flow from an external power source to the starter contactors
101
Where is the actuator for the alternate static source?
Left side wall
102
How is the static system drained?
By pushing the 2 pitot/static drain buttons on the left side wall by the left pilot seat
103
Where is the heater located?
In the nose compartment
104
When does the heater fan automatically shut off?
When the gear retracts
105
Where is the fuel drawn for the heater?
From the left tank at 1/2 gal/hr by an electric fuel pump
106
What is a synchrophaser?
A synchrophaser automatically synchronizes the engines (the Seminole does not have this option)
107
Where is the battery located?
In the nose cone
108
What is the engine setting for zero thrust?
11.5" MAP and 2000 RPM
109
How is the stall warning horn differentiated from the gear warning horn?
The stall horn is continuous; the gear horn is intermittent
110
With an engine inoperative and feathered, where is the ball?
The ball should slide 1/2 out toward the operating engine
111
As altitude increases, stall speed (TAS) ____?
increases
112
As altitude increases, VMC (TAS) _____?
decreases
113
What is the highest single drag item on the Seminole?
Full flaps
114
The second highest single drag component in the Seminole is?
Landing gear
115
As the CG moves aft, VMC ____?
increases
116
How would VMC be affected with a larger engine?
VMC would increase
117
How would turbocharging affect VMC?
VMC would remain constant as altitude increased
118
According to the ACS, when performing the demonstration of VMC, what is the maximum amount of bank the pilot can use?
5 degrees