Study Guide Questions Flashcards

1
Q

APU guaranteed Start up

A

39,000 ft
(May start up to 43,000 ft,
Max Operating ALT 45,000 ft)

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2
Q

What design features help guarantee an APU Airstart

A

1) Heated Oil Sump
2) Bleed Air Augmentation Valve
(Delays start for 15 sec when above 35,000 ft)

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3
Q

When does the APU generator come “online”

A

Once Reaching 99% RPM for 2 sec

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4
Q

When is APU bleed air available?

A

After reaching 100% for 1 min

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5
Q

APU bleed air for T/O is usable up to

A

1,500 ft AGL

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6
Q

What is the shutdown sequence for the APU below 20,000 ft?

A

1) It load-sheds Immediately
2) It Slowly winds down to 70% RPM over 1 min, then shuts-down

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7
Q

What is the shutdown sequence for the APU above 20,000 ft?

A

1) It load-sheds Immediately
2) Stays at 100% RPM for 1 min, then shuts-down

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8
Q

APU Max TGT for start

A

1050 C

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9
Q

APU Started cuts out at

A

46% RPM

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10
Q

APU fuel comes from

A

Left Tank

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11
Q

Can you start the APU with external DC power?

A

Yes (but multiple start attempts require 15 min between starts)

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12
Q

How many MAUs (Modular Avionics Unit) do we have

A

3 (16 Cards per MAU)

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13
Q

What do AGMs (Advanced Graphics Modules) do?

A

They take Data and create the images you see on the DUs (Display Units 1-4)

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14
Q

Where do the DUs get their power from

A

DU1 - Left ESS DC
DU2 - Left Main DC
DU3 - Right Main DC
DU4 - Right ESS DC

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15
Q

DUs 1 & 4 can be powered by

A

HMG if you have dual gen and APU gen failure

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16
Q

What is the Color of your Track (on Moving Map) until you reach the waypoint?

A

Magenta

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17
Q

What is the dotted Magenta Line?

A

Aircraft IRS track

18
Q

On the PFD, speed and altitude have a “trend vector.” that gives a __ forecast.

19
Q

What is needed for In-Flight alignment?

20
Q

Water tank capacity

21
Q

What is needed for a No-Break Power Transfer

A

An IDE must be part of the transfer
(An

22
Q

Using the HMU (hydraulic Motor Generator)

A

Use other Hydro systems/controls slowly (speed brake - 3 sec to open or close)

23
Q

When airborne, where does the GSB (ground service Bus) get its power

A

Right Main DC Bus

24
Q

What do the TRUs do?

A

Convert AC power to DC
(there are 5 of them
L ESS
L Main
Aux TRU
R Main
R ESS)

25
What buses are powered immediately when you put the HMG on?
L and R Standby AC buses
26
Main Batteries
24 VDC, 53 Amp, NICAD
27
If you select the L Main TRU where does it get power from?
The R Main AC Bus
28
What do the GCUs (Generator Control Unit) do?
The monitor volts, freqs, and loads for over and under conditions and faults
29
How do you Reset the GCU?
Use the associated Gen switch on the overhead panel
30
What do the BPCUs (Bus Power Control Unit - two of them) do?
Provide electrical power distribution and protection. It will prioritize the Aux TRU - ESS before Main, Left before Right
31
How to reset the BPCUs?
Reset (AC/DC) button on the overhead panel
32
What is the battery charger capacity in AMPS if using the AUX TRU?
50 Amps
33
Battery chargers will not charge the batteries if they are below.
7 VDC
34
Min Battery Volts for DC Start
22 VDC
35
Which bus powers the Avionics E-Batts?
L / R Standby AC Buses
36
If the grounds service bus light is illuminated
The GSB gets power from the Right Main Battery or the External DC power chart.
37
When do the battery lights come on?
1) When powering an APU START 2) When the Aux Pump is running 3) When powering the L and R ESS DC Bus
38
39
How many temperature zones are there in the aircraft?
3 zones. (Cockpit, Forward cabin, aft cabin)
40
Manual temp mode range
35 F - 230 F
41
Auto temp mode range
60 F - 90 F