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PA-44-180 Seminole > Oral Review > Flashcards

Oral Review Flashcards

(94 cards)

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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
Useable Fuel
108 Gal
26
Critical engine
None
27
Propeller Feather is not possible when?
Engine RPM below 950
28
Landing gear is held up by.....
hydraulic pressure
29
squat switch is on the....
Left main gear
30
What does an "ALT" light indicate?
inoperative alternator
31
The vacuum pump is located on?
Both left and right engines
32
Inboard stall vane provides stall indication when.....
flaps are 25 or 40
33
Loss of engine causes how much climb performance?
80% because of prop drag
34
The gear horn will sound under what conditions?
Gear selector up position on the ground manifold below 14" flaps at second or third notch
35
Max Demonstrated X Wind Component?
17 Knots
36
Describe the Engines
Lycoming 0-360 180HP air cooled normally aspirated direct drive
37
Describe the Electrical system
14 volt 12 volt battery 35 AMP 2 70 AMP Alternators overvolt shut off at 17 volts
38
Describe the propeller system
``` 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
Weight X Arm =
Moment
40
Total Moment / Total Weight =
CG
41
Moment =
Weight X Arm
42
CG =
Total Moment / Total Weight
43
Max Ramp Weight - Zero Fuel Weight =
Usable Fuel Weight
44
Fuel Weight / 6 =
Fuel Gallons
45
Usable Fuel Weight =
Max Ramp Weight - Zero Fuel Weight
46
Oil Weight =
7.5 Lbs/Gal
47
Fuel Weight =
6 Lbs/Gal
48
Unusable Fuel =
2 gals (12 Lbs)
49
Max hold speed
< 6000 200 KTS > 6000 < 14000 230 KTS >14000 265 KTS
50
Hold leg time
< 14000 1 min | > 14000 1.5 min
51
How is approach category calculated and what are they?
``` 1.3 VSO A = 0-90 kts B = 91 - 120 kts C = 121 - 140 kts D = 141 - 165 kts E = above 165 kts ```
52
Calculate VDP using DISTANCE
HAT/300 = Distance in NM from appraoch end of the runway
53
Calculate VDP using TIME
HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.
54
Aircraft inspections: A-AVIATES
``` 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
Aircraft Docs ARROWE
``` Airworthiness Cert Registration Cert Radio License Operating Limitations (POH) Weight and Balance Equipement list ```
56
IFR Take Off mins
2 engines or less = 1 sm vis | + 2 engines = 1/2 sm vis
57
Alternate Mins
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
Alternate required when....
1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only
59
MMULTI-G-BREST
``` 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
Useable Fuel
108 Gal
61
Critical engine
None
62
Propeller Feather is not possible when?
Engine RPM below 950
63
Landing gear is held up by.....
hydraulic pressure
64
squat switch is on the....
Left main gear
65
What does an "ALT" light indicate?
inoperative alternator
66
The vacuum pump is located on?
Both left and right engines
67
Inboard stall vane provides stall indication when.....
flaps are 25 or 40
68
Loss of engine causes how much climb performance?
80% because of prop drag
69
The gear horn will sound under what conditions?
Gear selector up position on the ground manifold below 14" flaps at second or third notch
70
Max Demonstrated X Wind Component?
17 Knots
71
Describe the Engines
Lycoming 0-360 180HP air cooled normally aspirated direct drive
72
Describe the Electrical system
14 volt 12 volt battery 35 AMP 2 70 AMP Alternators overvolt shut off at 17 volts
73
Describe the propeller system
``` 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
Weight X Arm =
Moment
75
Total Moment / Total Weight =
CG
76
Moment =
Weight X Arm
77
CG =
Total Moment / Total Weight
78
Max Ramp Weight - Zero Fuel Weight =
Usable Fuel Weight
79
Fuel Weight / 6 =
Fuel Gallons
80
Usable Fuel Weight =
Max Ramp Weight - Zero Fuel Weight
81
Oil Weight =
7.5 Lbs/Gal
82
Fuel Weight =
6 Lbs/Gal
83
Unusable Fuel =
2 gals (12 Lbs)
84
Max hold speed
< 6000 200 KTS > 6000 < 14000 230 KTS >14000 265 KTS
85
Hold leg time
< 14000 1 min | > 14000 1.5 min
86
How is approach category calculated and what are they?
``` 1.3 VSO A = 0-90 kts B = 91 - 120 kts C = 121 - 140 kts D = 141 - 165 kts E = above 165 kts ```
87
Calculate VDP using DISTANCE
HAT/300 = Distance in NM from appraoch end of the runway
88
Calculate VDP using TIME
HAT/10 = Time in SECONDS to subtract from the time from FAF to MAP depicted on the chart.
89
Aircraft inspections: A-AVIATES
``` 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
Aircraft Docs ARROWE
``` Airworthiness Cert Registration Cert Radio License Operating Limitations (POH) Weight and Balance Equipement list ```
91
IFR Take Off mins
2 engines or less = 1 sm vis | + 2 engines = 1/2 sm vis
92
Alternate Mins
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
Alternate required when....
1 hour before and after ETA weather is forecast less than 2000/s of if airport is VFR only
94
At least one of the following visual references required for decent from MDA....
- 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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