BE30 - Fuel & Fire extinguisher systems Flashcards

1
Q

Mains qty

each & total

A

each 1273
tot 2546

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2
Q

Aux qty

each & total

A

each 533
tot 1065

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3
Q

Total usable fuel

A

3611

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4
Q

Yellow Arc qty

& associated limit

A

265
No take-off

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5
Q

[L/R FUEL QTY]

Qty (lbs & time)

A

300 lbs / 45 g
30 min at MCP

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6
Q

Max imbalance

A

300

Includes both fuel & wing lockers load

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7
Q

Approved grades

  • Regular (3)
  • Military (3)
A

Regular =
- Jet A
- Jet A-1
- Jet B

Military =
- JP4
- JP5
- JP8

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8
Q

Commercial Grades -
Limitations (3)

A
  • Max 150hr between engine overhauls
  • Both standby pumps must be operative
  • Crossfeed must be operative for flights ≥ FL200
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9
Q

Fuel freezing point -
JetA / JetA-1

A

-40°
-50°

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10
Q

[FUEL PRESS LO]

  • Trigger
  • Limit
A

9-11psi decreasing pressure

  • Limited to (10) hours before overhaul /or/ replacement of engine-driven fuel pump
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11
Q

CROSSFEED
- When can it be used?

A

Restricted to single engine ops

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12
Q

STANDBY PUMPS
- How many are required for takeoff?

A

Approved engine fuels = (1)
* But crossfeed capability will not be available on the side of the inop stdby pump

Commercial Grade fuels = (2)
* Crossfeed must be operative for flights > FL200

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13
Q

How is fuel moved from the AUX tanks to the Nacelle tank?

A

Motive Flow Jet pump

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14
Q

How is fuel moved from the WING tank to the Nacelle?

A

Gravity

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15
Q

What happens if the High Pressure engine-driven fuel pump fails?

A

The engine flames-out immediatly

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16
Q

[NO FUEL XFR]

  • Trigger
A

Fuel is the AUX tank
&
Fuel pressure < 6 psi at the motive flow valve.

17
Q

During CROSSFEED operation :
- In which position should the Standby Pump switches be?
- Which Standby Pump will be activated?

A

Both switches should be OFF

The Standby Pump on the FEEDING SIDE will be automatically activated

18
Q

How is fuel moved from the NACELLE tank to the FCU?

A

Engine-Driven Boost Pump (or STDBY Boost pump, if inop)
&
Engine-Driven High Pressure Pump

19
Q

FUEL NOZZLES =
- How many of them?
- When does the 2nd stage activates?

A
  • 14 nozzles, divided in 2 sets
  • N1 > 35%
20
Q

FIRE EXTINGUSHER =
- How many spray tubes in each engine?

A

8

21
Q

ENGINE FIRE EXTINGUISHERS - Tests purpose :
- DET ?
- EXT ?

A

DET =
Checks the continuity of the detection loop

EXT =
Checks the continuity of wiring ti the squib and cartridge

22
Q

FIRE EXTINGUISHER - Cartridge =
- Conditions for its discarge to be available?

  • Electrical
  • Switches circuitry
A

BAT BUS - NORM

The BAT BUS switch must be set to NORM (not EMER OFF) - In order to power the DUAL-FED Bus.

However, the BATTERY switch itself may be OFF.

Firewwall Valve - PUSHBUTTON

First, the firewall fuel valve push button must be in the closed position to complete the circuit to the fire extinguisher push button.

Then, once the circuit is complete, the fire extinguisher push button, placarded “EXTINGUISHER PUSH”

DUAL-FED (HOT BAT)
- FW Valve PUSHBUTTON
- Engine Fire Extinguisher PUSHBUTTON & SYSTEM

TPL-FED (BAT)
- FW Valve closing SYSTEM
- - - - -
Therefore, the circuitry can be completed - and the cartridge can be discharged - while having solely the BAT BUS EMER switch ON (BAT can be OFF).

However, BAT power is required to actually close the FW Valve and completly cutoff fuel supply to the engine.