Airplane general Flashcards

1
Q

What is the model designation for the Global 7500? (AFM)

A

BD-700-2A12

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2
Q

What is the minimum flight crew required? (AFM LIM)

A

One pilot and one co-pilot

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3
Q

What is the minimum width required for a 180° turn? (FCOM 2)

A
  • Pavement: 75 ft (22.86 m)
  • Wingtip Clearance: 129 ft (39.34 m)
  • Wing Creep: 4.2 ft (1.28 m)
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4
Q

What is the Global-7500 dimensions? (FCOM 2)

A
  • Length: 111 ft (33.88 m)
  • Wing Span: 104 ft (31.71 m)
  • Tail Height: 27 ft (8.24 m) – depending on how heavy the acft is at the moment.
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5
Q

Which Engines are installed in the airplane? (FCOM 2)

A

GE Passport 20-19BB1A (High Bypass 5.6 : 1)

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6
Q

What is the Fuel consumption rule of thumb for G7500?

A

1st hour: 5,000 lb / -2nd hour: 4,000 lb / - 3rd hour and afterwards: 3,000 lb/hour.

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7
Q

What is the maximum/minimum OAT for takeoff? (AFM LIM)

A
  • Maximum: + 55°C (131°F) or ISA + 40°C.
  • Minimum: - 40°C (-40°F)
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8
Q

What is the prioritization of Checklist from High to Low? (FCOM 1 & AFM)

A

Master Warning - Emergency/RED procedures
Normal/white procedures
Master caution/Amber procedures
Advisory/Cyan procedures
Info Messages - Apply during ground ops only

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9
Q

What is the Tire Limit speed and Maximum Tire Pressure? (AFM LIM)

A

195 KT ground speed
Mains = 216 PSI max tire pressure (hydroplaning speed 132 KT)
Nose= 190PSI

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10
Q

What is the procedure for crosswinds greater than 18kt more 30° from acft centerline? (AFM LIM)

A
  • Advance to maximum 60% N1 below 30 kt (at 30 kt set takeoff pwr).
  • Subtract 1700ft TODA on performance.
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11
Q

What is the Vmcg at Sea Level for Flaps 2 and 3? (AFM chapter 6)

A
  • Flaps 2 Vmcg: 106 Kt
  • Flaps 3 Vmcg: 106 Kt
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12
Q

What is the Vmca at Sea Level for Flaps 2 and 3? (AFM chapter 6)

A
  • Flaps 2 Vmca: 100 Kt
  • Flaps 3 Vmca: 98 Kt
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13
Q

What is the Vmcl at sea level (Minimum control speed, landing - AFM chap 6)

A
  • Flaps 2/Gear Down Vmcl: 103 Kt
  • Flaps 4/Gear Down Vmcl: 96 Kt
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14
Q

What are the Turbulence Penetration Speed Limits? (AFM LIM)

A
  • 265kt from Sea Level to 8,000ft, linearly increasing to 285kt at 10,000ft.
  • 285kt or Mach .85 (whichever is lower) when above 10,000ft.
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15
Q

Maximum Flap Speed Limits? (AFM LIM)

A
  • Flaps 1: 225kt
  • Flaps 2 & 3: 210kt
  • Flaps 4: 185kt
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16
Q

What is the normal Circling Approach acft Configuration and Speed? (FCOM 1)

A
  • Flaps 4 / Gear Down;
  • Vref + 10kt until maneuvering is complete;
  • Set Vref on Final Approach segment.
    Operational Note: Protected Area => Set up a 2.7 NM circle for reference around RWYs.
17
Q

If AC power is lost and Cyan message BATT EMER PWR ON shows, how long do the Batteries Supply
Electrical power?

A
  • At least 5 minutes (2 acft batteries – MAIN & APU).
    Note: Different than the 4 Emergency Batteries (ELPS – Emergency Lighting Power Supply batteries trickle
    charged from DC ESS Bus 1) that can provide a minimum of 15 minutes if fully charged.
18
Q

What happens when APU Fire is detected on the ground?

A

The APU automatically shuts down, and if no crew action is taken within 10 seconds, BTL 2 discharges into
the APU enclosure.

19
Q

After Touchdown, what does the red warning message NORMAL BRAKE FAIL accompanied with an aural
warning indicate?

A
  • Total Failure of Normal Braking. Use the Emergency Brake (Parking Brake) carefully.
20
Q

If there’s visible Smoke/Fire in the flight compartment, the crew oxygen masks and smoke goggles should be
donned with the masks Set to:

A
  • Set to EMERGENCY.
21
Q

Which action should automatically occur when cabin Altitude reaches 14,500ft (+/- 500ft)?

A
  • The Passenger Oxygen Masks automatically deploy.
22
Q

A red EMERGENCY DESCENT warning message indicates the Automatic Emergency Descent Mode (EDM) has
been activated due to cabin altitude reaching:

A

14,500ft (+/- 500ft)

23
Q

Which control on the Pressurization Panel automatically opens the Outflow Valves and Depressurizes the
airplane?

A

EMER DEPRESS guarded PBA.

24
Q

What is the Initial Target Speed during a DUAL ENG OUT emergency procedure?

A

Dual Engine Out Target Speed: 200kt.

25
Q

What is the recommended procedure regarding the Nose Gear before Towing Operations?
(FCOM-1: Chapter 11. Airplane Servicing / 07. Towing / 01. General)

A
  • Disconnect the Nosewheel Steering Torque Links;
  • Ensure minimum of 5,000 lbs is loaded in the tanks or the load on the Nose Gear is not less than 1,900 lbs;
  • The CG envelope is within limits.