Prog 1 Excel Tester.xlsm - Prog 1 Test Flashcards

1
Q

Warning Definition

A

(people) If not observed may result in injury or loss of life

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2
Q

Caution definition

A

(equipment) If not observed may result in damage or destruction of equipment

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3
Q

Landing weights - Recommended Max & Normal

A

recommended Max (114,000); Normal (103,880)

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4
Q

Ladder operation caution – how many times can you use it before you have to let it cool?

A

After three continuous ladder operations, allow 20 minutes before further operation.

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5
Q

Runaround Relays allow any operating generator to power what buses?

A

Essential Buses

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6
Q

What is the Gen priority that the Transfer relays provide for Main AC Bus A

A

Gen 2, 4, APU, 3

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7
Q

What is the Gen priority that the Transfer relays provide for Main AC Bus B

A

Gen 3, 4, APU, 2

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8
Q

What is the purpose of the Transfer relay

A

allow any operating generator to power the main AC busses A and B and establish generator
priorities for those busses

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9
Q

What is the function of GEN 4 AUX Control Relay

A

Controls operation of Transfer relays 5 & 6

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10
Q

If Bus A fails, Mon Ess AC bus can be powered by any available generator via the runaround relays with what priorities

A

Gen 2, 4, APU, 3

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11
Q

What do sup panels do?

A

Voltage regulation & bus transfer control
Under frequency protection (auto reset)
Over voltage and under voltage protection (manual reset)
Feeder fault protection (not resettable)

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12
Q

Main DC Bus is powered by __________ Through _______________

A

Main DC Bus is powered by MAIN AC BUS A & B Through TRU 1 & 2

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13
Q

Mon Essential DC bus is powered by ______________ through _______________

A

Mon Essential DC bus is powered by MON ESS AC Bus through TRU 3

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14
Q

External power monitor relay – what does it do?

A

Prevents power with improper phase, voltage or frequency to power the AC

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15
Q

When do you have to turn a gen off

A

109% RPM

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16
Q

What does a yellow gen light mean

A

Indicates a primary gen drive bearing failure, aux bearing in use

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17
Q

What is the purpose of the EMP DE-ICE MONITOR switch ?

A

TO ALLOW THE USE OF EMP DE-ICE DURING SINGLE GENERATOR (APU) OPS ABOVE 8000’

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18
Q

With only one engine driven generator operating above 8000 feet, when will the electrical system load monitor ?

A

WHEN PROP DE-ICE OR EMP DE-ICE IS SELECTED ON

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19
Q

When operating with APU generator only above 8000 feet, what additional items are load monitored?

A

NO. 1A HYDRAULIC PUMP AND EMP DE-ICE

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20
Q

When operating with APU generator only (single generator) above 8000 feet , you need to use:

A

emp de-ice

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21
Q

Single (engine) Gen Ops - Before using prop and/or emp de-ice, you must manually load shed;

A

No. 2 hyd pump
Cabin Exhaust fan
Air Conditioning (F18 CB)
V/UHF-3 (receive only)

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22
Q

Single (engine) Gen Ops - Once you select prop and/or emp de-ice you will automatically lose;

A

(feeders) electronic DC feeders No 1,2,3
(Feeders) electronic AC feeders No 1,2
(eaters) rack H (galley) CB panel
(heaters) radiant floor heaters
(foggers) side window defogging

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23
Q

Single (APU) Gen Ops (below 8,000’) - Before using prop and/or emp de-ice, you must manually load shed;

A

No. 2 hyd pump
Cabin Exhaust fan
Air Conditioning (F18 CB)
V/UHF-3 (receive only)
V/UHF-1 and 3 receive only
HF-1 low power only

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24
Q

Single (APU) Gen Ops (below 8,000’) - Once you select prop and/or emp de-ice you will automatically lose;

A

(feeders) electronic DC feeders No 1,2,3
(Feeders) electronic AC feeders No 1,2
(eaters) rack H (galley) CB panel
(heaters) radiant floor heaters
(foggers) side window defogging

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25
Q

Single (APU) Gen Ops (above 8,000’) - If you go above 8000’ you will automatically lose;

A

No. 1A hyd pump
Emp de-ice
Circuits de-energized by load monitoring circuit (a-e above)

26
Q

Single (APU) Gen Ops (above 8,000’) -Once you select prop and/or emp de-ice you will automatically lose;

A

a. No. 1 hyd pump (boost out)
b. 3 fuel boost pumps
c. Cabin exhaust fan

27
Q

What does a Transformer Rectifier Unit (TRU) Do?

A

Converts AC to DC

28
Q

What does the Emergency inverter do and what does it power?

A

CONVERT DC POWER TO AC POWER TO POWER START ESS AC START ESS AC – TIT Gauges

29
Q

Max Fuel imbalance for Tanks 1&4 - TO / FLT / LND

A

1400 / 4389 / 4389

30
Q

Max Fuel imbalance for Tanks 2&3 - TO / FLT / LND

A

5025 / NIL / NIL

31
Q

Green Reset Advisory light –

A

RESET Advisory Light – A green light indicates RESET whenever the FUELING SYSTEM panel has control of the fuelling/transfer valves.

32
Q

Source Power for Boost pumps 1, 2, 3, 4?

A

ABAB

33
Q

Fuel Dump Rate?

A

Dump Pump – 650lbs/min; Fwd Transfer Pump – 175lbs/min; Aft Transfer pump – 175lbs/min

34
Q

Where are the Booster Pump located –

A

Surge Box

35
Q

What does a filter light mean?

A

If the differential across the filters exceeds 7.5 psi, the switch completes a circuit to the yellow FILTER caution light on the FUEL MANAGEMENT panel.

36
Q

Temp Limiting Range

A

0-66 deg Coordinator

37
Q

E-handle activates what Mechanically

A

(F) FCU (shutoff fuel)
(F) Feather Valve (mechanically moves it to the Fx position)
(F) Fuel Tank Emergency Shutoff Valve (closes)
(GEN) Generator Cooling Air Shutoff Valve (Closes)

38
Q

E-Handle Activates What Electrically

A

(F) FCU (shutoff fuel)
(F) Feather valve solenoid (actuates)
(B) Bleed air shutoff valve (Closes)
(E) EDC (dump) Firewall shutoff valve(Closes)
(O) Oil tank Shutoff Valve (Close)

39
Q

Fire warning lights, how do they turn off -

A

When the fire or overheat condition is no longer present

40
Q

How do you determine if there has been a Primary Fuel Pump failure in the start sequence -

A

PRIMARY FUEL PUMP FAILURE LT on above 65% rpm

41
Q

How do you determine if there has been a Secondary Fuel Pump failure in the start sequence -

A

No PRIMARY FUEL PUMP FAILURE LT between 16 & 65% rpm

42
Q

How does the Speed Sense valve work?

A

At 94%, the Speed sense valve closes the 5th and 10th stage pneumatic pucks using 14th stage bleed air

43
Q

Acceleration Bleed System –

A

it opens the pucks on the 5th and 10th stages to unload the compressor below 94% RPM and is dumped overboard and into ZONE 1.

44
Q

When is start limiting changed to normal limiting

A

At 94% RPM, a switch on the Speed Sensitive Control system switches the TD Control amplifier from start limiting to normal limiting

45
Q

Functions of the Speed Sensitive Control - 16% (x5)

A

F turns on fuel
I turns on ignition
P parallels fuel pumps
P enables prime
DV closes manifold drain valve

46
Q

Functions of the Speed Sensitive Control - 65% (x3)

A

I turns off ignition
DV de-energizes drain valve
PS puts fuel pumps in series

47
Q

Functions of the Speed Sensitive Control - 94% (x1)

A

shifts TD control amplifier from start limiting to normal limiting

48
Q

Oil Cooler Inducer Valve – how is it closed

A

Coord Below Flight Idle, Flaps fully open, Enginer Starter Switch Off

49
Q

How is the oil tank shutoff valve closed –

A

Electrically via the E-handle

50
Q

In flight, RPM is maintained by

A

Prop Governor

51
Q

In the ground range RPM is controlled by

A

FCU

52
Q

What are the 2 conditions that cause pitchlock

A
  1. Loss of controlling prop fluid pressure; 2. Overspeed of 103.5 % rpm
53
Q

RPM gets its indication from where?

A

Tach Gen

54
Q

Pitch lock RPM range

A

17-57 deg B/A

55
Q

When power levers are below 28 deg coord & blade angle is above 10 deg, pitchlock reset delays rpm needed for pitchlock actuation to ________.

A

109%RPM

56
Q

What 2 features are available with the sync servo switch in the normal ( on ) position ?

A

Anticipation circuitry - limits rpm transients caused by rapid power lever movement
Speed derivative circuitry - limits rpm transients caused by changes in power plant Load

57
Q

The purpose of the POWER LEVER GROUND IDLE position is to -

A

select a blade angle that will offset thrust from jet exhaust.

58
Q

What does the beta follow up system do in flight?

A

prevent overspeed in response to rapid power lever movement
acts as a hydraulic low pitch stop

59
Q

Purpose of the RGB- RGB Input _____ torque/______ RPM of __________ and Outputs ______ torque/_____ RPM ________? -

A

RGB Input low torque/high RPM 13820 and Outputs high torque/low RPM 1020

60
Q

Feathering propeller for loiter is normally accomplished by?

A

Feathering may be accomplished by pushing the feathering button (loiter shutdown) Pushing the feather button initiates feathering electrically.