Systems SO1090 Foot stomps Flashcards

1
Q

What can be tuned into on the backup Nav?

A

VORs and LOCs (ILS)

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2
Q

What will the backup Nav display if tuned into a LOC and “BRG” or “RAD” is selected?

A

It will display “LOC” below the frequency

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3
Q

What does “B + 1000” mean on the HUD?

A

You are 1000 pounds above your selected Bingo

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4
Q

When will the Bingo alert happen?

A

10 pounds below Bingo

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5
Q

What does the CDI and Gliseslope look like on the HUD vs the Flight Director?

A

CRS and GS = straight lines
FD = small circle

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6
Q

What is the greatest bank angle displayed on the HUD?

A

45 degrees (10, 20, 30, 45)

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7
Q

What is the pressure schedule?

A

0 - 8000: Ambient
8000 ft - 23000 ft: 8000 +/- 1000
23,000 ft+ : (Alt - 6000) / 2

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8
Q

How many volts are required close to the battery relay? It will remain closed until?

A

18 volts
10 volts

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9
Q

What must be on for the battery to charge?

A

the battery switch

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10
Q

If you have dual TRU failures, will you lose any busses?

A

Yes. The battery will be the only source of DC power and it automatically sheds the non-essential bus

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11
Q

In what cases will you lose the non-essential DC bus?

A

-Left essential bus failure
-dual TRU failure

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12
Q

Indications: Oil pressure and RPM drop to 0. The T5 system also fails.

What is the malfunction?
Is the engine seized?
Why do these indications make sense?

A

Oil pump shaft failure

-Engine is not seized if EGT is still high

-The oil pump, tachometer generator, and T5 alternator are all mounted on the same drive shaft

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13
Q

Indications: Left Generator Light

What is the malfunction?
Why do these indications make sense?

A

Left Generator Failure (good crossover)

-As long as the crossover relay/bus works properly, either generator can carry the entire electrical load (hence no other indications)

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14
Q

How can you silence the gear warning horn?

A

-Accelerate to 240 KCAS
-Press the silence button
-Put the gear down

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15
Q

What sounds/voice message will you hear for an avionics failure?

A

None. The only indication is “AVIONICS” flashing with a MALF list

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16
Q

What are your oil pressure limits? What are the fluctuation limits?

A

Idle: 5 to 20 psi
Mil/Max: 20 to 55 psi

Sudden changes of > 10 psi are indicative of a malfunction

Do NOT exceed 55 psi for greater than 5 minutes

Fluctuations are +/- 2 psi

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17
Q

How long can you maintain 0 G?

A

10 seconds

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18
Q

Is EGT 625 - 640 in limits?
620 - 660?
620 - 630?
631 - 649?

A

625-640: Yes
620-660: No (>15C)
620-620: No (average)
631-649: No (>15C)

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19
Q

What is the rule for EGT fluctuations?

A

15 C (+/- 7.5 C) if average is within steady state limits of 630-650 C

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20
Q

When would you not use the crossfeed fuel?

A

B: Boost pump inop
I: Indicator light
L: Low altitude
L: Low fuel
L: Leak

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21
Q

Does an alt gear extension impact the utility hydraulic system?

A

No. However, you are unable to use NWS after an alt gear extension

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22
Q

Where are the fuel shutoff switches located?

A

FCP only

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23
Q

What systems are powered by the utility hydraulic system?

A

Flight controls
Augment Stabilizer
Nosewheel steering
Gear
Speed brake

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24
Q

Explain the RA declutter modes.

A

RA0: All traffic appears
RA1: Declutters open triangles
RA2: Leaves only TAs and RAs

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25
Q

Can you declutter TAs and RAs?

A

NO. RA2 still displays TAs and RAs

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26
Q

When does the fuel indicators show red?

A

When EITHER tank is below 250 pounds

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27
Q

What are the uses of the static inverter?

A

-First engine start on the ground
-Airstarts
-Right autosyn instruments (fuel flow, hydro, oxygen, oil px, and fuel state)

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28
Q

What ECS systems remain with total AC power loss?

A

Only the defog

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29
Q

How do you adjust the defog temperature?

A

You can’t. You can only change the quantity of defog

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30
Q

If you have total AC power loss, where position does the air conditioning fail to?

A

It’s last selected position (AC power dies and rheostats are AC power)

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31
Q

What does the Q hotkey do? What about H? G?

A

Q: sets 29.92
H: snaps HDG bug to current
G: turns guard off for 1 minute

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32
Q

When will hot keys be inactive?

A

If any data field allowing letters is open

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33
Q

What is an XMFR RECT OUT light indicative of?

A

Dual TRU failure

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34
Q

Indications: Hydraulic caution light + normal hydraulic pressure

What is the malfunction?
Why do these indications make sense?

A

Hydraulic overtemp

-The hydraulic caution light indicates for BOTH low hydro pressure and overtemp

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35
Q

What is the normal hydraulic pressure range?

A

2850 to 3200 psi

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36
Q

What is the oil pressure limit for 0 G flight?

A

10 seconds

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37
Q

What is RPM for ground idle?

A

46 - 50%

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38
Q

What is the airspeed limitation of the canopy?

A

50 kts

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39
Q

What is the airspeed limitation for full flaps?

A

220 KCAS

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40
Q

How does the MFD order PFLs?

A

By the most recent occurrence, NOT severity

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41
Q

How do you select different modes using the HOTAS?

A

Master Mode Switch

42
Q

How do you select different primary displays with the HOTAS?

A

Default Display Switch

43
Q

What is providing air for engine anti-ice and where is the air routed to?

A

8-stage bleed air is routed to the bullet nose and inlet guide vanes

44
Q

What system and its components help ensure compressor stall-free operation?

A

Variable Geometry System
-consists of the variable inlet guide vanes and the air bleed valves

45
Q

What does the landing/taxi light switch do?

A

ONLY turns on the filament

46
Q

How long must the EGI be off prior to engine shutdown?

A

10 seconds

47
Q

How can you prevent idle decay?

A

Keeping the throttles at 80% RPM minimum

48
Q

What is the flight path marker showing you?

A

Your velocity vector

49
Q

When is Break X not active?

A

When banked >45 degrees or greater than 5000 AGL (b/c Break X requires Radar Altimeter)

50
Q

When does the generator come online?

A

43-48% RPM

51
Q

What is the generator shift range?

52
Q

The EGI switch turns on the EGI, the SAS, and the?

A

Radar Altimeter

53
Q

The NAV backup control panel is active when

A

the MDP fails or is OFF, or the AAP mode switch is in B/U or BOTH

54
Q

Pressing the ON/OFF know on the UHF backup control panel

A

applies and removes squelch

55
Q

How many channels are programable in the backup UHF radio?

A

20 + guard

56
Q

What happens if both cockpits try to transmit on the radio at the same time?

A

The rear cockpit has priority and only the IP will be able to transmit

57
Q

During normal operations, crossfeeding is recommended when the fuel difference between the systems is greater than ____ pounds

A

200 pounds

58
Q

Low pressure air is directed against the ____ to rotate the engine for ground starts

A

turbine rotors

59
Q

What are all mounted on the same drive shaft as the oil pump?

A

T5 generator and tachometer generator

60
Q

If there is an EED failure that prevents fuel system display, the normal solid white bar on the vertical fuel quantity

A

is blanked (DC)

61
Q

What directs the flow of air into the first stage compressor blades at the proper angle

A

front frame

62
Q

The boost pumps are a part of which system?

A

Fuel system

63
Q

What does the Generator switches do? Where are they located?

A

Gen switches disconnect the generator output from its bus
Gen switches are FCP only

64
Q

Fuel shutoff switches _____ shut off fuel within ____

A

electrically; 1 second

65
Q

Nozzle position should stabilize within?

A

10 seconds

66
Q

When does T5 close the nozzle?

A

NEVER. T5 only opens the nozzle

67
Q

What bus is fire detection system?

A

Right Essential DC bus
but confirm with chart

68
Q

What are the reasons for a GEN light?

A

You disconnect the generator via the switch, the protection panel disconnects the generator, gearbox shift failure

69
Q

What is the difference in advisories for a single vs. dual TRU failure?

A

Single: NO voice, AVIONICS, PFL
Dual: CAUTION from Betty and XMFR RECT OUT

70
Q

Can the RCP disconnect the generators?

71
Q

What converts DC power to AC power?

A

Static Inverter

72
Q

What converts AC power into DC power?

73
Q

If you have a right gen fail no cross, what will the static inverter show you?

A

Only right autosyn instruments and fuel state (which is right AC)

Hydraulics
Oil pressure
Oxygen
Fuel

74
Q

What must you have on for the landing/taxi light to work?

A

Landing/taxi light switch, position lights, gear down

75
Q

Can you change the brightness of the landing light?

A

NO, not as the pilot

76
Q

What does Aural mean?

A

Tones, beeps, squeaks (not Betty’s voice)

77
Q

What are the Warnings in order?

A

-Break X
-Fire
-Stall
-Altitude
-Gear

78
Q

When will the gear warning activate?

A

<210 knots, BOTH throttles below 96% RPM, and below 10,000’ MSL

79
Q

How does the UFCP display bad data?

A

it flashes the bad data at you

80
Q

Up to where can the engine be gravity fed by the fuel pump?

A

At Mil, up to 25,000’

However, it is only guaranteed up to 6,000’ as flameouts have occurred as low as 7,000’

81
Q

What solo limits are there on Cg?

A

Not allowed to have twice the amount in the right tank vs. the left

82
Q

What components are supplied with 8-stage bleed air for engine anti-ice?

A

Bullet Nose and variable guide vanes

83
Q

What RPM is required for an airstart? Where is the heart of the airstart?

A

12% RPM
18-20% RPM

84
Q

What triggers a Fuel Low light?

A

EITHER tank below 250 pounds (for 7.5 seconds)

85
Q

How do you transfer fuel between the tanks?

A

You canNOT transfer fuel

86
Q

What happens if you turn the boost pump OFF before turning the crossfeed ON?

A

You get a Master Caution (ALWAYS turn something on before you turn something off)

87
Q

When should you crossfeed?

A

Greater than 200 pound difference

88
Q

When should you NOT crossfeed?

A

Boost pump inop
Indicator light
Low fuel
Low altitude
Leak

89
Q

When does the fuel show red for balance?

A

200 pounds

90
Q

When does the fuel balance show white numbers?

A

60-190 pounds

91
Q

What checklist should you run if oil pressure drops to 0?

A

Oil system malfunction checklist (Oil px should NEVER be zero)

92
Q

If you have 0 RPM and 0 Oil pressure, what is likely the malfunction?

A

Sheared oil pump shaft

93
Q

What should the instruments read for Mil power t/o check?

A

RPM: 99-101% (+/- 1%)
EGT: 630-650 C (+/- 7.5)
Nozzle: 0-20% (+/- 3%)
Oil px: 20-55 psi (+/- 2)
Hydraulic: 2850 - 3200 psi

94
Q

How can the RCP extend the alt gear?

A

the canNOT

95
Q

How does the alt gear extension effect the utility hydraulic system?

A

It doesn’t. However, NWS will be inop

96
Q

What is the only ECS system that doesn’t die with AC power loss?

97
Q

Does divert mode provide an aural tone?

98
Q

What is the cabin altitude at 28,000’?

A

11,000 +/- 2,000

99
Q

Indications: Generator light + hydraulic pressure light

What is the malfunction?
Why do these indications make sense?

A

Airframe mounted gearbox failure

-the generator and hydraulic pump are both mounted on the airframe gearbox

100
Q

How will EGT differ from a low-altitude and high-altitude compressor stall?

A

High altitude: decreasing EGT
Low altitude: increasing EGT
(RPM always decreases)