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Aviation > G280 Playing Cards > Flashcards

G280 Playing Cards Flashcards

1
Q

Maximum altitude for APU start is
Maximum altitude for APU operation is
Maximum altitude for APU bleed air use is

A

35,000 feet
40,000 feet
20,000 feet

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2
Q

Hydraulic pressure limitations

A

Normal operation - 2700 to 3250 psi
Maximum - 3500 psi

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3
Q

APPR mode for LOC approaches should be selected only when within _____.

A

60deg of approach course

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4
Q

Takeoff Thrust and
Maximum Continuous Thrust

A

Takeoff - 7624 lb
Maximum Continuous - 7240 lb

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5
Q

Takeoff thrust, and manual APR is limited to _____ minutes with all engines operating (AEO).

APR is limited to _____ minutes with an inoperative engine (OEI).

A

5 mins
10 mins

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6
Q

Maximum ITT during ground start:

A

N2 at or below 40% - 650C

N2 above 40% - 950C

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7
Q

Maximum crosswind component for engine start -

Maximum tailwind component for engine start -

A

20 kts

15 kts

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8
Q

Cancellation of reverse thrust should be initiated so as to be at the reverse idle position by _____

A

40KIAS

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9
Q

Minimum fuel temperature at the fuel filter is _____

A

3C

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10
Q

Maximum Engine ITT

A

Max Continuous - 950deg
TO - 955deg
APR - 955deg

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11
Q

Maximum altitude to access internal baggage door?

A

Pre-mod G25-10066: 40,000ft
Post mod G25-10066: 44,000ft

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12
Q

How is the Landing Gear emergency extended?

A

Pneumatic Bottle with 3000 psi nitrogen charge.

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13
Q

What is the rating of the Main Engine Driven Generators?

A

28 VDC 400 amps

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14
Q

What type of electrical system does the G280 have?

A

28 VDC

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15
Q

The tiller will turn the nose wheel how many degrees?

A

60deg

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16
Q

How is an ENGINE START aborted?

A

By moving the Engine Fuel Control switch to OFF

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17
Q

What is the minimum radius for a 180 turn?

A

49.5 ft

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18
Q

ENGINE STARTER DUTY CYCLE:

A

3 consecutive start cycles followed by cooling period of 15 minutes.

Engine motoring for a maximum of 5 minutes, followed by cooling period of 15 minutes

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19
Q

OIL INLET TEMPERATURE

Before engine start:

For continuous operation above ground idle:

A

-40C minimum

5C minimum

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20
Q

In what order will the fuel deplete if all tanks are full?

A

Forward Tank
Aft Tank
Center Tank
Wing Tanks
Feeder Tanks

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21
Q

What is the rating of the main aircraft batteries?

A

24 VDC 38 AH

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22
Q

In flight, what will automatically load shed in the event of a main generator failure?

A

Windshield Heat
Baggage Compartment Heat
60 Hz Inverter
Galley
Water Heaters
Cabin Non-essentials

23
Q

What is the purpose of the STANDBY AIRCRAFT BATTERY?

A

Dedicated power source for the Standby Multifunction Controllers (SMCs)

24
Q

How long can we fly with the STANDBY AIRCRAFT BATTERY only?

A

60 minutes if one of the SMCs is depowered

25
Q

Fuel is supplied to the APU from where?

A

Right feed tank

26
Q

What is the capacity of the water system?

A

10 gallons

27
Q

What happens when a fire handle is pulled?

A

Fire shutdown signal sent to FADEC
Closes Hydraulic Shutoff Valve
Closes Engine Fuel Shutoff Valve

28
Q

Is hydraulics available after pulling the FIRE HANDLE?

A

Yes, with the Electrical Motor Pump (EMP)

29
Q

What are the prerequisites for the Automatic Descent Mode (ADM)?

A

Cabin Altitude at or above 10,000 ft

Aicraft altitude at or above FL 340

Autopilot engaged

30
Q

Maximum number of occupants?

A

19 Maximum

31
Q

Yaw damper inoperative limitations

A

Maximum speed - 250 KIAS

Maximum altitude - 25,000 ft

32
Q

Mach trim inoperative speed

A

Mach trim functions inoperative, the maximum operating limit speed is 340KIAS / 0.77 Mi.

33
Q

Alternate stabilizer trim limited to

A

MMO = 0.77 Mi

34
Q

Maximum slope approved for takeoff and landing operations are?

A

+2% (uphill) and
-2% (downhill)

35
Q

Maximum tailwind component approved for takeoff and landing is?

A

10 Knots.

36
Q

Maximum approved airport pressure altitude for takeoff or landing is?

A

14,000 ft field elevation.

37
Q

Minimum and Maximum operating altitudes are?

A

45,000 ft

-1400 ft

38
Q

Flaps extended speeds (Vfe)

A

10deg - 250 KIAS
20deg - 220 KIAS
LND - 180 KIAS

39
Q

Landing gear operation speeds (Vlo),

Landing gear extended speed (Vle),

Emergency landing gear extension

A

Vlo = 195 kts
Vle = 195 kts
Emergency extension = 175 kts

40
Q

Maximum tire speed

A

Maximum main landing gear tire ground speed is 195 kt.

Maximum nose landing gear tire ground speed is 182 kt.

41
Q

Minimum holding speed

A

The minimum holding speed in icing conditions is 185 KIAS.

42
Q

Maximum weights

A

Zero Fuel = 28,200 lbs
Landing = 32,700 lbs
Takeoff = 39,600 lbs
Ramp = 39,750 lbs

43
Q

Maximum hydraulic temperature

A

95C

44
Q

Electrical Motor Pump (EMP) operation above 39,000 ft is limited to

A

10 minutes

45
Q

The icing envelope is defined as

A

+10C TAT to -40C TAT with visible moisture present

46
Q

Minimum / maximum operating temperature?

A

-20C / ISA +35C

47
Q

Baggage compartment loading:

A

Maximum 1980 lb

Floor load 120 lb/ft2

48
Q

Maximum wing fuel imbalance

A

Takeoff is 450 lb

In flight, approach and landing is 900 lb

49
Q

Maximum cabin pressure differential

A

9.2 psi inflight

0.2 taxi takeoff landing

50
Q

AUTOPILOT

Minimum engage height is

Minimum disengage height ILS approach.

Minimum disengage height LNAV / VNAV, and LPV approach.

Maximum demonstrated altitude loss for coupled go-around is

CAT II operation is not approved for

A

200 ft.

80 ft. from an ILS approach

80 ft. from an LNAV / VNAV, and LPV approach

61 ft.

Single engine operations

51
Q

GENERATOR LIMITATIONS

Engine ground and flight operations

APU ground and flight operations

A

100% maximum continuous

100% maximum continuous

52
Q

Maximum indicated battery charge current for takeoff:

APU GEN Available:

APU GEN Unavailable:

A

20A

8A

53
Q

Total usable fuel weight

A

Single point fueling 14,620 lb

Gravity fueling 9,760 lb

54
Q

Left and right brake accumulator pre-charge pressure:

A

700 +/- 30 psi @ 70F/21C +/- 25 psi for each increment of 10F/5C

Aviation (6 decks)

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