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ATP > ATP Checkride > Flashcards

ATP Checkride Flashcards

1
Q

What type of engine do we have in the BE-95?

A

-Lycoming
-Horizontally Opposed
-Air cooled
-Naturally Aspirated
-Direct Drive

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2
Q

What type of propellers do we have?

A

Hartzell

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3
Q

Max fuel capacity of the plane and how much is usable

A

112/106

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4
Q

Our flaps are ______ actuated and the flap extension speed (Vfe) is ____

A

Electrically, 130

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5
Q

What are the three ways we can check that the gear is down and locked?

A

Mirror
Gear Lights
Wiper window / Window box

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6
Q

Define a constant speed prop and the advantages it provides. Additionally, describe how the prop governor works

A

Propeller maintains a constant RPM, selected by the propeller control lever regardless of the airplane’s pitch attitude or throttle position. Changes in pitch from ported oil to/from hub.

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7
Q

What does an unfeathering accumulator do?

A

Nitrogen Precharge to push oil out, decrease blade angle and unfeather (300 psi)

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8
Q

Why doesn’t the propeller feather below 800 rpm?

A

Anti-feather lock pin

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9
Q

What type of fuel grade and color does the BE-95 aircraft use?

A

100 LL (blue)

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10
Q

How many fuel indicators vs fuel tanks do we have?

A

2 / 4

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11
Q

How many total fuel pumps do we have and how do they operate?

A

4 pumps (2 engine drive, 2 electric)

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12
Q

How many drains do we have on the aircraft?

A

9

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13
Q

What is the amperage of our engine-driven alternators and how many do we have?

A

28V / 50 AMP, 2

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14
Q

Descrive the electrical system of the be-95

A

two 12 volt batteries producing 24-volts regulated for a 28 volt system utilizing a 50 amp alternator

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15
Q

Battery life if both alternators fail

A

It depends on the load, but roughly 30 minutes

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16
Q

How many buses does the electrical system on the be-95 aircraft have and how are they referenced

A

2 elec buses; avionics/main

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17
Q

Will the engines quit in flight if the alternator and batteries die in the aircraft? Why

A

No, eng ignition via magnetos independent of elec sys

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18
Q

What type of landing gear do we have on the aircraft?

A

Tricycle / elec activated

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19
Q

What prevents us from bringing up the gear while we are on the ground?

A

Squat switch

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20
Q

Max gear extension speed?

A

165 mph

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21
Q

Hyde sys controls:

A

Wheel / disc brakes

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22
Q

What is not a kind of hypoxia?

A

Hallucinogenic

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23
Q

What are airmets, sigmets , and convective sigmets?

A

Meteorological conditions forecasted for aviation. Each deals with different types and severity of weather and has their own valid times

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24
Q

How often do TAFs update?

A

Every 6 hours

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25
Q

What is mach tuck?

A

Nose down pitch tendency due to a change in the position of the center of pressure resulting from a rearward movement of the shock wave which occurs as an aircraft in transonic flight accelerates beyond its limiting mach number (MMO). As an aircraft accelerates, the aerofoils create more lift

26
Q

Does temperature affect mach number?

A

Yes

27
Q

What is coffin corner?

A

The region of flight where a fast but subsonic fixed-wing aircraft’s stall speed is near the critical mach number at a given gross weight and g-force loading

28
Q

What are the differences between MEL and CDL?

A

MEL- required items to fly
CDL (config deviation list)- IDs parts that can be missing along with associated operation limitations

29
Q

Can any kind of oxygen be used in flight?

A

No, not if it isn’t approved aviation oxygen

30
Q

What are the two types of decompression?

A

Rapid/explosive

31
Q

What is blue line / its significance?

A

Vyse - 108. Best climb rate single engine

32
Q

What is the BTU of the janitrol heater

A

50,000 BTUs

33
Q

How much fuel does the heater use, and which tank does it draw from?

A

1/2 gph from the left main tank

34
Q

How can we cool the heater, How long does it have to cool down for?

A

Ram air in flight, blower on deck for 2 mins

35
Q

Define “accelerate stop distance”

A

total distance required to accelerate the twin engine airplane to a specified speed and, assuming failure of an engine at the instant that speed is attained, to bring the airplane to a stop on the remaining runway

36
Q

What acronym do we use to define the factors used in determining Vmc?

A

SMACFUM
S-Standard Day; higher temp, lower air density, lower performance
M- Most unfavorable weight (light)
A- aft CG, lower CG
C- Critical engine windmilling, greater Vmc
F- Flaps T/O, Gear Up (keel effect)
U- up to 5* bank, lower Vmc
M- max power on operating eng

37
Q

What acronym do we use to define the factors which determine which engine is “critical?”

A

P- P factor
A- Accel Slip Stream
S- Spiraling Slip Stream
T- Torque

38
Q

Define Absolute ceiling and Service ceiling

A

Absolute ceiling: Altitude where rate of climb is zero
Service ceiling: Altitude where you can no longer maintain more than a 50fpm rate of climb

39
Q

When do you start configuring on a precision approach?

A

When you are one dot below?

40
Q

When do you start configuring on a non-precision approach?

A

2 nm before FAF

41
Q

What is the number one cause of runway incursions?

A

loss of SA

42
Q

what is the maximum airspeed in which we can simulate an aborted takeoff

A

half of Vmc

43
Q

what is the minimum altitude that we can simulate a single engine failure on takeoff climb?

A

400’ AGL

44
Q

What advisory circular provides info regarding endorsements endorsements required to take knowledge tests, practical tests (checkrides), and even student solo flights?

A

AC 61-65H

45
Q

How many years does an instructor need to keep their certificate endorsements?

A

3 yrs

46
Q

Part 61-certifications pilots/cfi/grd instructors

A

a. general
b. aircraft ratings and pilot authorizations
c. atp

47
Q

Part 91

A

A. Gen flight rules
B. Flight rules
C. equip/ints/certs
f. Large turbine / fractional ownership
G. Additional for large turbine
h. foreign a/c ops of u.s. civil oconus

48
Q

part 117

A

Flight duty req and rest limitations

49
Q

Part 121

A

operational requirements for domestic/ flag and supplemental op scheduled operations

50
Q

Part 135

A

Op reqs commuter and on demand operators and roles of passengers/ unscheduled operators

51
Q

49 CFR 830

A

Notification and reporting of a/c accidents (ntsb)

52
Q

Describe the flaps

A

Single slotted, actuated by electrical motor, maximum deflection of 28 degrees, Vfe=130

53
Q

Fuel tanks

A

2 mains (baffles installed) 25 gallons (22 usable). 2 aux (cruise only) 31 gallons, all usable. Minimum 13 gallons on the mains for takeoff. Max duration of a slip is 30”

54
Q

How many drains are there and what are they for?

A
  1. 2 mains, 2 aux, 2 crossfeed, 2 fuel strainer, 1 janitrol heater
55
Q

Where is the motor for the landing gear?

A

Under the pilot’s seat?

56
Q

When will the gear warning horn activate?

A

Throttle reduced to 14” and gear is not down, or if the gear handle is brought to UP position while on deck (squat switch).

57
Q

Where is the squat switch and what does it do?

A

Left main, stops gear from coming up, activates the heater blower

58
Q

What type of landing gear are on the BE-95

A

Tricycle, retractable

59
Q

How long are TAFs valid?

A

24 hours

60
Q

V speeds
Manuevering-
Best angle-
Best Rate-
Best Angle se-
Best Rate se-
Safe SE speed
Min cont speed-
stall (landing)-
Stall (controllable)-
Never exceed-

A

Manuevering-160 (4.2k) / 148 (3.6k)
Best angle- 83
Best Rate- 103
Best Angle se- 98
Best Rate se- 108 (blue line)
Safe SE speed- 98
Min cont speed- 80 (red line)
stall (landing)- 75
Stall (controllable)- 85
Never exceed- 240

ATP (2 decks)

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