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Lear 45 Additional Questions > José gouge > Flashcards

José gouge Flashcards

1
Q

What is the definition of icing

A

10 to -40 visible moisture and visibility less than a mile

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2
Q

What is the rule regarding contaminants on the airplane?

A

Clean aircraft concepts all contaminant should be removed prior to takeoff

“pre contamination check”

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3
Q

What are some things to consider if there is snow to be expected prior to takeoff?

A

Deicing procedures hold overtimes area for deicing airport considerations regarding Taxi routes and frequencies for this procedure

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4
Q

Give one Risk regarding the situation of snow covered taxiways and runway?

A

Ramp congestion slippery surfaces incursions

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5
Q

If the FBO can accomplish deicing what type of fluid should we request not necessarily brands but what type?

A

Type 1 is used for clearing and
type 4 is for prevention

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6
Q

What must the engines be warm to before attempting to start them

A

-23°C

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7
Q

What temperature must the cabin be before Dispatch?

A

-15°C

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8
Q

Just like the batteries to the opposition what is the minimum voltage you need?

A

14 V less than that the batteries are no longer viable

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9
Q

What will the battery switch for the emergency battery indicate?

A

EMER

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10
Q

Are there any other presentations for the emergency battery?

A

 (CWP) Crew warning panel indicate
white EMER BATT

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11
Q

Regarding the CWP there are two emergency items that do not indicate on this panel what are they?

A

Engine fire
APU fire

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12
Q

What provides power from the landing and recog lights

A

Main battery bus

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13
Q

Would you consider Landing Recog lights a high or low draw item?

A

High Draw

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14
Q

What type of emergency would this come in to play?

A

Dual Gen fail, you will need to consider that likes to draw down the batteries

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15
Q

What is the max amperage for the GPU?

A

1500 Amps

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16
Q

Where is the GPU receptacle located?

A

Aft lower left part of aircraft near the baggage compartment

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17
Q

How do you know the GPU is a usable source of electricity?

A

The GPS which indicator aluminate
- green indicating the power and polarity are safe for the aircraft

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18
Q

What are the available power sources for the aircraft on the ground?

A

GPU, APU, three batteries, or engine driven generators

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19
Q

What is the amp limit on the generators?

A

300 amps

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20
Q

How many batteries do we have and how long are they stated as lasting?

A

Three batteries and 50 minutes for the main 60 minutes for the EMER battery

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21
Q

Can the batteries power the entire aircraft?

A

No only the main’s an emergency bus

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22
Q

Can the GPU power the entire electrical system?

A

Yes through the power distribution panels and the bus tie contactor

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23
Q

What is the purpose of the bus tie contactor?

A

To reroute powered electrical malfunction or when on a single power source

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24
Q

During flight if we lose a generator what can we expect from electrical system?

A

A single generator is capable of powering the electrical system

  • the non essential buses will shut automatically and power will be routed through the bus tie contactor
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25
Q

Is there any way to reenergize nonessential buses? During a single generator failure

A

Yes by selecting the not essential switch indicator on electrical panel

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26
Q

During the walk around you notice the lower static wick on the right wing is missing can you go?

A

Reference MEL, yes

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27
Q

During walk around you check the hydraulic panel which is located where?

A

Aircraft right towards the tail just forward of the engine location

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28
Q

What are we looking for during pre-flight of the hydraulic panel?

A

Greenlight OK, and no brush light

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29
Q

If the hydraulic panel brush light is on what should you do?

A

Call Maintenance…it must be changed at the next suitable opportunity

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30
Q

How many hydraulic pumps does the aircraft have?

A

Three, two engine and one auxiliary

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31
Q

How do you preflight the APU maintenance panel?

A

Press the button to test looking to make sure the oil level is proper.

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32
Q

APU maintenance panel test how do I know proper oil level?

A

No light illuminated and either
-low indication
Or
-add indication

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33
Q

If the APU hydraulic panel Illuminates add, what does this mean?

A

Oil is low level and only 5 hours are permitted on the APU

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34
Q

Can I use the APU while deicing?

A

No

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35
Q

What are the starter limitations for the APU?

A

One wait one minute, to wait two minutes, three wait 15 minutes

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36
Q

Can you use the APU in flight?

A

No

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37
Q

What is the Fire test telling me?

A

The continuity of the various detection systems for the bleedlines engines and APU

it also test the warning system visual indications oral and extinguishing ability is also tested

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38
Q

I start the APU, and I see a fail indication. What does the AFM say about a fail indication for the AP?

A

We cannot take off with a fail indication present

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39
Q

What happens if I start APU and I get a fire?

A
  • A triple chime,
  • CAS fire indication
  • APU fire push button will illuminate
  • horn will sound.

After one minute it will eject extinguishing agent

40
Q

What controls on the aircraft are hydraulic?

A
  • Gear
  • flaps
  • spoilers
  • thrust reverser’s
  • brakes
41
Q

What controls the ailerons elevator and rudder?

A

Cable and pulley system with auto pilot servos attached

42
Q

How do we trim the aircraft for pitch?

A

Are using the barrel switch on the yoke or by the secondary control located on the pedestal

43
Q

What is actually being moved when using the pitch trim?

A

The horizontal stabilizer is being adjusted

44
Q

What are the secondary flight controls? What are the balance tabs used for? Where is the aileron trim located?

A

Flaps, trims, balance tabs, spoilers.
- Alleviate control forces.
Left side

45
Q

What is the max fuel quantity for Lear 45?

A

6062 pounds

46
Q

What are the types of fuel allowed ? Can we mix fuels?

A

Jet a, jet A1, JP5, and JP8. Yes

47
Q

What is the maximum fuel inbalance?

A

200 pounds

48
Q

How do you correct a fuel inbalance?

A

Open the crossflow and activate the standby pump on the high side

49
Q

How long will it take for the imbalance the correct using the standby pumps?

A

50 pounds per side times two equals 100 pounds per minute… So for a 400 pound in balance four minutes

50
Q

If while the engines are running you receive a master warning fuel low pressure what would this indicate?

A

Less than 1 psi in the manifold feeding the engine

51
Q

In the event of a total electrical
Failure just engines running how long will standby attitude indicator last?

A

Nine minutes until failure

52
Q

What are the minimum and maximum oil pressure is for all thrust settings?

A

50 to 100 psi

53
Q

What is the minimum oil temperature before anything but idle thrust?

A

30°C

54
Q

What are some of the functions of the deec?

A

Seeastar

Spool prot/ Temp limiting
Eng sync
Eng Overspeed prot
Auto start sequence
Surge PROT
Thrust management
Apr
Ref n1 bugs

55
Q

During the before taxi check you check the manual mode governor what are you checking?

A

Control of the engine manually

56
Q

When you move the engine computer switching to Manual position what functions of the DEEC is still active?

A

Overspeed protection
107, 109

57
Q

Prior to takeoff how close should the N1 bugs be to each other?

A

1 %

58
Q

What types of oil can we use? Can we mix oil’s?

A

Reference the addendum

Mobil Jet 254
Exxon
BP 2197

Yes

59
Q

You were taken off with a strong crosswinds you consider turning on the ignition what conditions will the DEEC turn the ignition on?

A

SUE

START
Uncommanded deceleration
Excessive Deceleration

60
Q

What are the memory items for the midair engine start after an Uncommanded deceleration?

A

Immediate engine air start

• Thrust lever - idle
• Standby fuel – on

61
Q

What memory items did you perform if your engine flamed out inside the final proach fix on approach?

A

• MSW depress and release
• Thrust lever operative engine increases required
• Flaps 20
• airspeed Vref +5

62
Q

How long can the thrust lever remain in the takeoff detent?

A

Five minutes

63
Q

Thrust Reverser limits

A

• No touch and Go’s
• do not use for reverse
• do not pull CB in flight
• max Reverse speed 40kts
• idle only in manual mode

64
Q

Under part 135 and part 91 when is one member of the crew required to use supplemental oxygen at all times?

A

Above FL350 (part 135)

Above FL410 (Part 91)

65
Q

In-flight you observe the pilot side turn blue and a red heading fail annunciation of the Pilot side HSI what has failed?

A

AHRS # 1

66
Q

What is the memory item for overspeed?

A

• Thrust lever - idol
• auto pilot - disengage
• spoiler - extend
• identify aircraft pitch and roll attitude
• level the wings
• elevator and pitch trim - As required

67
Q

In-flight DU1 and DU2 are displaying two large red X’s what has failed?

A

IC600 # 1

68
Q

What is the procedure for resolving failure of DU1 and DU2?

A

Amber tab 25 “IC bus fail “

69
Q

After complying with the “IC bus fail” and DU1 and DU2 fail what equipment is no longer available?

A

• autopilot
• primary pitch trim (bypass is available)
• Config trim
• Mach trim

70
Q

What considerations need to be made with regards to finishing the flight after IC600 #1 fail?

A

No RVSM
Speed between .76 and .78

71
Q

If display unit two fails in flight what is the correct action? On the ground can we go 

A

Tab number 26

On the ground check the MEL list

72
Q

The ADC and AHRS must be selected to what position for takeoff?

A

Normal

73
Q

What is the maximum speed with primary Displays?

A

• 330
• .81

74
Q

Mach trim Inop auto pilot on?
Autopilot off 23400-FL420
Above FL420

A

. 81

.76-.78
.78

75
Q

What is high flow on what pressure is the pack by level PRS of the regulating the pressure the air entering the pack?

A

26 psi

76
Q

What limitation must be observed while using Hi-flow?

A

Hi-flow must be off for:

• takeoff / landing
• anti-ice operations
• flight above 30,000

77
Q

You just lost all electrical power during flight does the pack still operate?

A

Yes

78
Q

Can the temperature of the air entering the cabin be controlled after all electrical powers lost?

A

No

79
Q

Amber ICE detected CAS message?

A
  • Ice is detected but anti-ice protection is off
80
Q

What powers the windshield heat

A

Alternators

81
Q

What triggers a config warning?

A

Parking brake
Spoilers not retracted
Thrust Reversers not stowed
Flaps not set to 8 or 20
Any trim not in TO setting
Pitch Trim Bias employed
Pitch Trim miscompare

82
Q

Under normal conditions during takeoff roll the master warning system alert you to Allman functions that may occur?

A

No some messages are inhibited

83
Q

Paraceta master warning flightless company by a voice aural how should I silence the aural?

A

Master caution inhibit or Mute button

84
Q

What does pushing the fire push switch do?

A

Engine Fuel SOV
Engine Bleed valve closed
Hydraulics SOV closed
Thrust Reverser Isolation valve closed
Generator disconnected
Alternator Disconnected
Ignition disabled
Fire bottle squib armed

85
Q

If I disarm the fire push switch, Are all of these items reversible?

A

Yes

86
Q

If the fire push and fire extinguisher switches are pushed on the ground with aircraft shut down will a bottle discharge why?

A

Yes… on the L & R EMER hot bus

87
Q

What closes when you turn off either the left or right bleed?

A

• ECS PRSOV
• HP SOV
• EMER PRESS valve

88
Q

What happens when you turn on EMER press?

A

• opens the EMER PRESS valve on the bleed side turned on

• closes the other ECS PRSOV and HP SOV

Directing low pressure bleed air into the cabin

89
Q

How will temperature be controlled and the cabin with EMER press on?

A

Through the thrust lever position of the engine which the bleed switch is turned on

90
Q

What is a CAB DUCT OVHT & CKPT DUCT OVERHEAT master caution?

A

The high temperature air from the pack overheat has raised the temperature in the ducts in excess of 300°F

91
Q

During a dual Gen failure in icing conditions what anti-ice equipment is functional

A

NAC heat

92
Q

What hydraulic components are operated by the main hydraulic system?

A

Brakes
Flaps
Gear / doors
Thrust Reversers
Spoilers

93
Q

What does the hydraulic press xflow switch do?

A

Allows the

•flaps
• gear
• gear doors

to be operated by the auxiliary hydraulics system

94
Q

Is there any other way to determine the main gear is down and locked?

A

• taxi light
• gear warning

95
Q

What other ways do we have to determine the nose gear is down and locked besides the green light?

A

• turn on Nose wheel steering arms
• gear warning (when reducing flaps)

96
Q

If the auxiliary hydraulics system is still functional what must you do to have normal braking upon landing?

A

Turn on the aux hydraulic pump

Lear 45 Additional Questions (3 decks)

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