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G280 Playing Cards Flashcards

(54 cards)

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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?

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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?

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A

Dedicated power source for the Standby Multifunction Controllers (SMCs)

24
Q

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

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A

60 minutes if one of the SMCs is depowered

25
Fuel is supplied to the APU from where?
Right feed tank
26
What is the capacity of the water system?
10 gallons
27
What happens when a fire handle is pulled?
Fire shutdown signal sent to FADEC Closes Hydraulic Shutoff Valve Closes Engine Fuel Shutoff Valve
28
Is hydraulics available after pulling the FIRE HANDLE?
Yes, with the Electrical Motor Pump (EMP)
29
What are the prerequisites for the Automatic Descent Mode (ADM)?
Cabin Altitude at or above 10,000 ft Aicraft altitude at or above FL 340 Autopilot engaged
30
Maximum number of occupants?
19 Maximum
31
Yaw damper inoperative limitations
Maximum speed - 250 KIAS Maximum altitude - 25,000 ft
32
Mach trim inoperative speed
Mach trim functions inoperative, the maximum operating limit speed is 340KIAS / 0.77 Mi.
33
Alternate stabilizer trim limited to
MMO = 0.77 Mi
34
Maximum slope approved for takeoff and landing operations are?
+2% (uphill) and -2% (downhill)
35
Maximum tailwind component approved for takeoff and landing is?
10 Knots.
36
Maximum approved airport pressure altitude for takeoff or landing is?
14,000 ft field elevation.
37
Minimum and Maximum operating altitudes are?
45,000 ft -1400 ft
38
Flaps extended speeds (Vfe)
10deg - 250 KIAS 20deg - 220 KIAS LND - 180 KIAS
39
Landing gear operation speeds (Vlo), Landing gear extended speed (Vle), Emergency landing gear extension
Vlo = 195 kts Vle = 195 kts Emergency extension = 175 kts
40
Maximum tire speed
Maximum main landing gear tire ground speed is 195 kt. Maximum nose landing gear tire ground speed is 182 kt.
41
Minimum holding speed
The minimum holding speed in icing conditions is 185 KIAS.
42
Maximum weights
Zero Fuel = 28,200 lbs Landing = 32,700 lbs Takeoff = 39,600 lbs Ramp = 39,750 lbs
43
Maximum hydraulic temperature
95C
44
Electrical Motor Pump (EMP) operation above 39,000 ft is limited to
10 minutes
45
The icing envelope is defined as
+10C TAT to -40C TAT with visible moisture present
46
Minimum / maximum operating temperature?
-20C / ISA +35C
47
Baggage compartment loading:
Maximum 1980 lb Floor load 120 lb/ft2
48
Maximum wing fuel imbalance
Takeoff is 450 lb In flight, approach and landing is 900 lb
49
Maximum cabin pressure differential
9.2 psi inflight 0.2 taxi takeoff landing
50
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
200 ft. 80 ft. from an ILS approach 80 ft. from an LNAV / VNAV, and LPV approach 61 ft. Single engine operations
51
GENERATOR LIMITATIONS Engine ground and flight operations APU ground and flight operations
100% maximum continuous 100% maximum continuous
52
Maximum indicated battery charge current for takeoff: APU GEN Available: APU GEN Unavailable:
20A 8A
53
Total usable fuel weight
Single point fueling 14,620 lb Gravity fueling 9,760 lb
54
Left and right brake accumulator pre-charge pressure:
700 +/- 30 psi @ 70F/21C +/- 25 psi for each increment of 10F/5C

Aviation (6 decks)

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