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PA-44-180 Seminole > Oral Review > Flashcards

Oral Review Flashcards

1
Q

Lost Comm Procedure (FAR 91.185)

A

If VFR, remain VFR, squawk 7600, land as soon as practical.

If IFR, squawk 7600 and fly:

Route (first that applies)

  • Assigned
  • Vectored
  • Expected
  • Filed

Altitude (whichever is highest until descent is required for landing):

  • Minimum IFR Altitude
  • Expected
  • Assigned
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2
Q

To maintain IFR currency, a pilot must have made….

A

6 approaches and demonstrated proper holding procedures as well as radial and bearing tracking in the last 6 months.

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3
Q

An alternate is not required if the weather is….

A

is forecast at least as a 2000’ ceiling and vis of at least 3 miles from 1 hour before and after your ETA.

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4
Q

VA 3800 lbs

A

135 KIAS Maneuvering speed @ 3800 lbs

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5
Q

VA 2700 lbs

A

112 KIAS Maneuvering speed @ 2700 lbs

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6
Q

VNE

A

202 KIAS Red Line Never Exceed Speed

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7
Q

VNO

A

169 KIAS Top of Green Arc

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8
Q

VLE

A

140 KIAS Max speed with gear extended

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9
Q

VLO Down

A

140 KIAS Max gear extension

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10
Q

VLO Up

A

109 KIAS Max gear retraction

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11
Q

VFE

A

111 KIAS Top of White Arc Max Flap Extension

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12
Q

VYSE

A

88 KIAS Blue Line Best Rate of Climb Single Engine

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13
Q

VY

A

88 KIAS Best Rate of Climb

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14
Q

VSSE

A

82 KIAS Safe speed for intentional engine failure

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15
Q

VXSE

A

82 KIAS Best Angle of Climb Single Engine

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16
Q

VX

A

82 KIAS Best Angle of Climb

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17
Q

VR

A

75 KIAS Rotation

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18
Q

VS

A

57 KIAS Bottom of Green Arc Stall Speed Clean

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19
Q

VMC

A

56 KIAS Red Line MCA

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20
Q

VSO

A

55 KIAS Bottom of White Arc

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21
Q

BEFORE LAND CHECKLIST

A 
Gear               3 GREEN
Fuel Selector   ON
FLAPS             25 (VFE 111 KIAS)
Mixtures          FORWARD
Props              FORWARD
Fuel Pumps     ON
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22
Q

CRUISE CHECKLIST

A 
POWER                  Set 22"/2300RPM
Engine Instruments  CHECK
COWL FLAPS          AS REQUIRED
L FUEL PUMP         OFF/CK PRESSURE
R FUEL PUMP         OFF/CK PRESSURE
LANDING LIGHT      OFF
MIXTURES              LEAN AS REQUIRED
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23
Q

AFTER TAKEOFF CHECKLIST

A 
POWER                  24"/2500RPM
FLAPS/GEAR UP     CHECK
COWL FLAPS          AS REQUIRED
88 (Blue Line) VY UNTIL 500' AGL
110 KIAS passing 500'
1000' REDUCE POWER TO 24"/2500 RPM
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24
Q

MMULTI-G-BREST

A 
Max Power +
Max Gross Weight -
Un favorable CG +
Landing Gear Up +
Takeoff Configuration +
Inoperative Engine Windmilling +
Ground Effect +
Bank into Operative Engine (5 degrees) -
Rudder Pressure <150lbs -
Exceptional Pilot Skills
Standard Day +
Twenty Degree Recovery
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25
Q

Useable Fuel

A

108 Gal

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26
Q

Critical engine

A

None

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27
Q

Propeller Feather is not possible when?

A

Engine RPM below 950

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28
Q

Landing gear is held up by…..

A

hydraulic pressure

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29
Q

squat switch is on the….

A

Left main gear

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30
Q

What does an “ALT” light indicate?

A

inoperative alternator

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31
Q

The vacuum pump is located on?

A

Both left and right engines

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32
Q

Inboard stall vane provides stall indication when…..

A

flaps are 25 or 40

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33
Q

Loss of engine causes how much climb performance?

A

80% because of prop drag

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34
Q

The gear horn will sound under what conditions?

A

Gear selector up position on the ground
manifold below 14”
flaps at second or third notch

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35
Q

Max Demonstrated X Wind Component?

A

17 Knots

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36
Q

Describe the Engines

A

Lycoming 0-360 180HP
air cooled
normally aspirated
direct drive

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37
Q

Describe the Electrical system

A

14 volt
12 volt battery 35 AMP
2 70 AMP Alternators
overvolt shut off at 17 volts

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38
Q

Describe the propeller system

A 
Hartzell two blade 
controllable pitch 
constant speed
 full feather 
oil pressure regulates pitch
forward = low pitch (high RPM)
back = high pitch (low RPM) feathered
nitrogen charged cylinder and springs move prop back
no feather below 950 RPM
39
Q

Weight X Arm =

A

Moment

40
Q

Total Moment / Total Weight =

A

CG

41
Q

Moment =

A

Weight X Arm

42
Q

CG =

A

Total Moment / Total Weight

43
Q

Max Ramp Weight - Zero Fuel Weight =

A

Usable Fuel Weight

44
Q

Fuel Weight / 6 =

A

Fuel Gallons

45
Q

Usable Fuel Weight =

A

Max Ramp Weight - Zero Fuel Weight

46
Q

Oil Weight =

A

7.5 Lbs/Gal

47
Q

Fuel Weight =

A

6 Lbs/Gal

48
Q

Unusable Fuel =

A

2 gals (12 Lbs)

49
Q

Max hold speed

A

< 6000 200 KTS
> 6000 < 14000 230 KTS
>14000 265 KTS

50
Q

Hold leg time

A

< 14000 1 min

> 14000 1.5 min

51
Q

How is approach category calculated and what are they?

A 
1.3 VSO
A = 0-90 kts
B = 91 - 120 kts
C = 121 - 140 kts
D = 141 - 165 kts
E = above 165 kts
52
Q

Calculate VDP using DISTANCE

A

HAT/300 = Distance in NM from appraoch end of the runway

53
Q

Calculate VDP using TIME

A

HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.

54
Q

Aircraft inspections: A-AVIATES

A 
ADs - All ADs must be complied with
Annual Inspection - 12 calendar months
VOR check - 30 days for IFR
Inspection - 100 hours if for hire
Altimeter - 24 calendar months
Transponder - every 24 calendar months
ELT - 12 calendar months, 1/2 batt, 1 hr use
Static Pitot System - 24 calendar months
55
Q

Aircraft Docs ARROWE

A 
Airworthiness Cert
Registration Cert
Radio License
Operating Limitations (POH)
Weight and Balance 
Equipement list
56
Q

IFR Take Off mins

A

2 engines or less = 1 sm vis

+ 2 engines = 1/2 sm vis

57
Q

Alternate Mins

A

Precision approach - 600/2
Non Precision approach - 800/2
No IAP - mins allow for VFR approach
Only GPS - can not use as ALT (unless WAAS)

58
Q

Alternate required when….

A

1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only

59
Q

MMULTI-G-BREST

A 
Max Power +
Max Gross Weight -
Un favorable CG +
Landing Gear Up +
Takeoff Configuration +
Inoperative Engine Windmilling +
Ground Effect +
Bank into Operative Engine (5 degrees) -
Rudder Pressure <150lbs -
Exceptional Pilot Skills
Standard Day +
Twenty Degree Recovery
60
Q

Useable Fuel

A

108 Gal

61
Q

Critical engine

A

None

62
Q

Propeller Feather is not possible when?

A

Engine RPM below 950

63
Q

Landing gear is held up by…..

A

hydraulic pressure

64
Q

squat switch is on the….

A

Left main gear

65
Q

What does an “ALT” light indicate?

A

inoperative alternator

66
Q

The vacuum pump is located on?

A

Both left and right engines

67
Q

Inboard stall vane provides stall indication when…..

A

flaps are 25 or 40

68
Q

Loss of engine causes how much climb performance?

A

80% because of prop drag

69
Q

The gear horn will sound under what conditions?

A

Gear selector up position on the ground
manifold below 14”
flaps at second or third notch

70
Q

Max Demonstrated X Wind Component?

A

17 Knots

71
Q

Describe the Engines

A

Lycoming 0-360 180HP
air cooled
normally aspirated
direct drive

72
Q

Describe the Electrical system

A

14 volt
12 volt battery 35 AMP
2 70 AMP Alternators
overvolt shut off at 17 volts

73
Q

Describe the propeller system

A 
Hartzell two blade 
controllable pitch 
constant speed
 full feather 
oil pressure regulates pitch
forward = low pitch (high RPM)
back = high pitch (low RPM) feathered
nitrogen charged cylinder and springs move prop back
no feather below 950 RPM
74
Q

Weight X Arm =

A

Moment

75
Q

Total Moment / Total Weight =

A

CG

76
Q

Moment =

A

Weight X Arm

77
Q

CG =

A

Total Moment / Total Weight

78
Q

Max Ramp Weight - Zero Fuel Weight =

A

Usable Fuel Weight

79
Q

Fuel Weight / 6 =

A

Fuel Gallons

80
Q

Usable Fuel Weight =

A

Max Ramp Weight - Zero Fuel Weight

81
Q

Oil Weight =

A

7.5 Lbs/Gal

82
Q

Fuel Weight =

A

6 Lbs/Gal

83
Q

Unusable Fuel =

A

2 gals (12 Lbs)

84
Q

Max hold speed

A

< 6000 200 KTS
> 6000 < 14000 230 KTS
>14000 265 KTS

85
Q

Hold leg time

A

< 14000 1 min

> 14000 1.5 min

86
Q

How is approach category calculated and what are they?

A 
1.3 VSO
A = 0-90 kts
B = 91 - 120 kts
C = 121 - 140 kts
D = 141 - 165 kts
E = above 165 kts
87
Q

Calculate VDP using DISTANCE

A

HAT/300 = Distance in NM from appraoch end of the runway

88
Q

Calculate VDP using TIME

A

HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.

89
Q

Aircraft inspections: A-AVIATES

A 
ADs - All ADs must be complied with
Annual Inspection - 12 calendar months
VOR check - 30 days for IFR
Inspection - 100 hours if for hire
Altimeter - 24 calendar months
Transponder - every 24 calendar months
ELT - 12 calendar months, 1/2 batt, 1 hr use
Static Pitot System - 24 calendar months
90
Q

Aircraft Docs ARROWE

A 
Airworthiness Cert
Registration Cert
Radio License
Operating Limitations (POH)
Weight and Balance 
Equipement list
91
Q

IFR Take Off mins

A

2 engines or less = 1 sm vis

+ 2 engines = 1/2 sm vis

92
Q

Alternate Mins

A

Precision approach - 600/2
Non Precision approach - 800/2
No IAP - mins allow for VFR approach
Only GPS - can not use as ALT (unless WAAS)

93
Q

Alternate required when….

A

1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only

94
Q

At least one of the following visual references required for decent from MDA….

A
  • Approach lighting system
  • Threshold
  • Threshold Markings
  • Threshold Lights
  • Runway end identifier lights (REIL)
  • Visual approach slope indicator (VASI)
  • Touchdown zone or markings
  • Touchdown zone lights
  • Runway or Runway markings
  • Runway lights

PA-44-180 Seminole (1 decks)

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