Airplane General Flashcards by Catalin Milea

What is the minimum pavement width for a 180° turn?
A. 15ft6in.(4.73m)
B. 58ft2in.(17.72m)
C. 68 ft (20.73 m)
D. 75 ft (22.86 m)

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What is the wingspan of the airplane?
A. 98ft10in.(30.11m)
B. 104ft(31.71m)
C. 111 ft 2 in. (33.88 m)
D. 129 ft (39.34 m)

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What is the total length ?
A. 98ft10in.(30.11m)
B. 104ft(31.71m)
C. 111 ft 2 in. (33.88 m)
D. 129 ft (39.34 m)

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What is the model designation for the Global 7500?

BD-700-2A12

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What is minimum flight crew required

One pilot and one co-pilot

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What is the maximum number of occupants allowed?

22 total; consisting of 19 passengers and 3 crewmembers, or the number for which seating
accommodation approved for takeoff and landing is provided, whichever is less.

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What is the Global 7500 wing span, length and tail height?

· 104 ft (31.71 m) wing span
· 111 ft 2 in (33.88 m) length
· 27 ft (8.24 m) tail height

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What is the minimum width for wing tip clearance?
And the distance in front of the airplane to assure that?

129 ft 1 in
5 ft 2 in

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What is maximum ramp weight?

115.100 lb

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What is maximum landing weight?

87,600 lb

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What is minimum/maximum runway slope?

±2%

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May operations from unprepared runways be conducted?

· No

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What is the normal circling approach aircraft configuration and speed?

· Gear Down, Flaps 4
· Vref +10 until maneuvering is complete; Vref on final approach

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What is the prioritization of handling checklist procedures, from high to low?

· Emergency procedures
· Relevant normal procedures
· Caution procedures
· Advisory procedures
· INFO messages during ground operations

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What are the buoyancy limitations for takeoff or forced/emergency landings near bodies of water above maximum landing weight?

Outflow valve 2 closed, one Pack OFF

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What is the maximum airspeed at which it is safe to extend/retract the landing gear?
A. 190KIAS
B. 200KIAS
C. 250 KIAS
D. 300 KIAS

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What is the tire limit speed?
A. 187ktgroundspeed
B. 178ktgroundspeed
C. 183 kt ground speed
D. 195 kt ground speed

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What is the maximum allowable altitude with slats/flaps extended?
A. 15,000ft
B. 20,000ft
C. 18,000 ft
D. 37,000 ft

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What is the total maximum usable fuel load based on a fuel density of 6.75 lb/USG

A. 51,850lb(23,500kg)
B. 45,100lb(20,425kg)
C. 44,092 lb (20,000 kg)
D. 57,292 lb (25,987 kg)

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What is the maximum operating altitude of the airplane?
A. 51,000ft
B. 41,000ft
C. 47,000 ft
D. 49,000 ft

For takeoff at weights above the maximum landing weight on runways near bodies of water:
A. OUTFLOW VLV2 must be closed and the left PACK must be shutdown for takeoff.
B. OUTFLOW VLV2 must be closed and one PACK must be shutdown for takeoff.
C. OUTFLOW VLV 1 must be closed and one PACK must be shut down for takeoff.
D. One OUTFLOW VLV must be closed and the right PACK must be shut down for
takeoff.

What is the maximum airport pressure altitude for takeoff and landing?
A. 11,000ft
B. 15,000ft
C. 13,700 ft
D. 10,000 ft

What is the minimum ambient temperature for starting a cold soaked APU on the ground?
A. –40°C
B. –20°C
C. –10°C
D. –30°C

Below what altitude must the flight spoilers be retracted?
A. 200ftAGL
B. 300ftAGL
C. 600 ft AGL
D. 900 ft AGL

Engine starts are not permitted when the tailwind component exceeds: A. 15kt. B.20kt if less than 30° either direction from airplane center line. C. 20 kt. D. 30 kt if more than 30° either direction from airplane centerline.

What is the minimum required fuel quantity per wing during a go-around? A. 181kg(400lb) B. 227kg(500lb) C. 363 kg (800 lb) D. 340 kg (750 lb)

Which of the following is NOT found on the EICAS? A. Engine parameters B. INFO messages C. CAS message list D. Flight control TRIMS

If the MUTED light comes on when pressing the SPKRS pushbutton annunciator (PBA) on the AURAL WARNING panel: A. flight crew headphones are enabled. B. cabin speakers are enabled. C. flight compartment speakers are muted but aural alerts are still heard in the headphones. D. flight compartment speakers and headphones are muted.

Which of the following sections of the airplane are unpressurized? Select three responses. A. Aft equipment bay B. Auxiliary power unit (APU) compartment C. Tail section D. Fuselage

A, B, C

Which bank angle will cause wingtip contact with the ground at a pitch angle of 8°?

At takeoff power, at what distance behind the engines can winds of 65 mph be felt? A. 76 ft B. 284 ft C. 458 ft D. 834 ft

Which controls are used to drain the potable water system prior to landing? Select two responses. A. Waste servicing panel – aft left side B. Waste servicing panel – aft right side C. Water system control panel – baggage bay D.Forward galley control panel – cabin management system (CMS)

C, D

What is the benefit of disconnecting the nose torque link and the tire pressure indicating system harness before attaching the towbar? A. It avoids an incorrect tire pressure indicating system reading. B. It eliminates any towing angle limit. C. It avoids tire damage. D. There is no reason to disconnect the nose torque link.

What is stored in the emergency console immediately behind the right seat? Select three responses. A. Protective breathing equipment B. First aid kit C. Fire extinguisher D. Ax

A C D

What panels can be used to control the cursor? Select two responses. A. Cursor control panel (CCP) B.Multifunction keyboard panel (MKP) C. Control tuning panel (CTP) D. .Reversion switch panel (RSP)

A B

What is the MEM key on the multifunction keyboard panel used for? Select two responses. A. To store the current configuration automatically B. To revert to previous configuration C. To recall display unit configurations D. To store display unit configurations

C D

Which of the following statements are true regarding cursor bumping? Select three responses. A. When a cursor enters a multifunction window (MFW) occupied by the other cursor, the first cursor is bumped and removed from the display unit. B. A cursor is bumped when the MFW format is changed to a format that does not support cursor operation. C. The pilot and copilot cursors may simultaneously occupy the same display unit (DU) but not the same MFW. D. When a cursor is bumped, a CURSOR BUMPED status message is shown on the EICAS.

A B C

What happens to the primary flight display (PFD) on display unit (DU) 1 if DU 1 fails with the other DUs functioning normally? A. It moves to DU 2. B. It is not shown. C. It moves to DU 3. D. It moves to DU 4.

Main landing gear tyre pressure

206-216 PSI

Nose Landing Gear tyre pressure

190-200 PSI

Number of independent Hydraulic systems

Number of independent Hydraulic pumps

Hydraulic system pressure

3000 PSI Emergency system 2850 PSI

Electric System Number of AC GEN

4 1 each ENG 1 APU 1 RAT

Electric System GEN Capacity

ENG 60 KVA each APU 60 KVA nominal RAT 9 KVA - 13.5 KVA for 5 min and 18 KVA for 5 sec

Electric System TRU - Transformer Rectify Unit

3 Units @ 300A each

Flight compartment Viewing Angle

15,5•/ 8.5 ft in front