System 2 Check Flashcards

(57 cards)

1
Q

Generator

A
  • Primary source of power
  • 28 VDC/300 amp
  • Regulated by the GCU
  • Location: Right side panel aft cockpit
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2
Q

Generator Switch

A

Only one switch can be one (either front or aft cockpit)

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3
Q

Secondary Aircraft Power

A
  • Battery: 24 VDC/42 amp hr
  • Aux Battery: 24 VDC/5 amp hr
  • External power distributes on the battery bus
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4
Q

Aux Battery Switch

A

Needs to be in β€œON” position to power backup instruments

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5
Q

Kneeboard Lights

A

Rotate towards you to turn on

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6
Q

Taxi/Ldg Gear Lights

A

Only on if gear down and locked

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7
Q

Single Point Refueling

A
  • 1100 lbs
  • 530 lbs per wing
  • 40 lbs in collector tank
  • refuels all tanks at the same time
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8
Q

Over Wing Refueling

A
  • 1200 lbs
  • 580 lbs per wing
  • 40 lbs in collector tank
  • will only fill respective tank at a time
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9
Q

Motive Flow Line Low Px

A

FUEL PX light with MAST WARN will turn on if less than 10 psi

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10
Q

Primary Jet Pump

A

Provides pressure to go up line to engine from collector tank

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11
Q

EDM

A
  • Engine Data Manager

- keeps us within 20 lbs fuel balance

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12
Q

Fuel Imbalance Light On

A

> 30lbs imbalance past 2 min

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13
Q

Fuel Probes

A
  • 7 total
  • 3 each tank
  • 1 in collector tank
  • Provides fuel indication quantity
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14
Q

Fuel Tapes

A
  • turn yellow at 150 lbs

- Less than 110 lbs - Low fuel line in respective tank

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15
Q

Float Valves

A

prevent excess fuel from draining out of heavy wing into vent lines

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16
Q

Aux Battery

A

Will Power:

  • fire detection Loop 1
  • instrument associated lights
  • IRU
  • VHF Radio
  • Standby VHF control head

-will provide power for 30 min

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17
Q

Red OIL PX

A
  • Less than 40 psi when above idle

- Less than 15 psi at or below idle

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18
Q

Amber OIL PX

A
  • Between 15 and 40 psi at idle

- Between 40 and 90 psi for 10 seconds above idle

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19
Q

Red OIL PX and Amber OIL PX

A

-Between 15 and 40 psi for greater than 5 seconds at idle

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20
Q

Needed for engine operation

A

air, fuel, heat

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21
Q

Sections of engine

A
  • Accessory
  • Power Turbine
  • Gas Generator
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22
Q

Reduction Gear Box

A

Steps down 30,000 RPM to 2,000 RPM

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23
Q

PMU Purpose

A

Process power request

Maintain operations limits

24
Q

Propeller

A
  • 100% Np at 2,000 RPM
  • Fine pitch at idle
  • Course pitch at higher RPM
25
PIU
- Receives input from PMU | - Regulates oil pressure to pitch change mechanism
26
Fire Detection
- Kinks don't affect it - Monitors overall engine temp and discrete temp - Monitors outside the engine
27
Engine Failure
- Fuel starvation - Mechanical failure - Compressor stall
28
Fire in Flight
- Fluctuating oil px , oil temp, or hyd px - Excessive turbine temperature - Visual indications (smoke or flames) - Erratic engine operation - Roughness or vibrations
29
Fire in Flight Notifications
- Fire message - MAST WARN light - Aural tone
30
Ram Air Switch
- Opens fresh air valve | - ram air is used for ground ops and unpressurized flight
31
P3 Ports
Left side - OBOGS | Right side - everything else
32
Temp Control Switch
- Control Heat Exchanger Bypass Valve (open - hotter air. Closed - Colder air because it goes through heat exchanger) - Keeps temperature at 60-90*F
33
DEFOG Switch
- front CP only - opens bi-level flow control bypass valve - high bleed air auto select - AC on - temp still set by Temp Control Switch
34
EVAP BLOWER
-only switch in each CP
35
Cockpit Space Temp Sensor
-sends temperature to Temp Control Switch for Bypass valve
36
DUCT TEMP light
>300*F
37
Temp where Heat Exchanger closes Bypass Valve
165*F
38
Pressurization
- right side P3 port - less than 8000 ft is unpressurized - maintains 8000' PALT until 18,069' (delta P 3.6+-0.2 psi) until 16,600' max (31,000' ) cockpit altitude
39
CKPT light
19,000' cockpit light
40
Dump Pressure switch
-dump solenoid opens control valve
41
Ram/Dump Switch
-dump solenoid opens control valve and ram air valve
42
Safety Valve
- delta p regulator will regulate cabin at 3.9 - 4.0 psi | - >3.9 = CKPT PX with MAST WARN
43
CKPT ALT caution
>19,000 ' PALT
44
Anti-G System
- Air goes through water separator to separate contaminants - Safety Valve opens at 7 psi - outside air pressure will bleed system to deflate g-suit
45
Emergency Oxygen
- located in seat bucket - 10 min supply - auto activated when eject - can't stop flow once started
46
Canopy Components
- frame - forward windscreen - forward transperancy - rear transperancy
47
Canopy Seals engage
WOW off and bleed air available
48
CFS
- each handle blows respective cockpit - doesn't need electricity - Auto activated only during ejection
49
Front Cockpit Charge
Flexible Linear Shape Charge
50
Ejection Seat Limits
0'/0 airspeed to 35,000' / 370 knots
51
MOR Handle
- to initiate seat/pilot separation | - ideal over mountain terrain exceeding 8,000'
52
SSK
Auto-deploy 4 seconds after seat/pilot separation
53
ISS
- if set to BOTH, pinned seat will still fire | - rear seat first, front seat 0.37 sec later
54
Ejection Sequence
-At the top of the rail, rocket motor will fire
55
Droge Chute
- Purpose: to stabilize and slow down | - if greater than 16,000' MSL droge chute will stay until 14,000 - 16,000' MSL at which point the main chute will open
56
Seat Adjust
-Electrically driven
57
Ejection Charts
Based on: - sink rate - bank angle - dive angle 2000 ft controlled, 6000 ft uncontrolled