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Aviation > Gulfstream GIV > Flashcards

Gulfstream GIV Flashcards

1
Q

What are the Length, Height and Wingspan of the GIV?

A

Length: 88’4”
Height: 24’ 5 1/8”
Wingspan: 77’10”

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2
Q

What are the maximum weights for the GIV-SP & GIV w/o ASC-190?

Zero Fuel Weight?
Max Ramp Weight?
Max Takeoff Weight?
Max Landing Weight?

A

Zero Fuel: 49,000/46,500 lbs.
Max Ramp: 75,000/73,600 lbs.
Max Takeoff: 74,600/73,200 lbs.
Max Landing: 66,000/58,500 lbs.

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3
Q

What is the minimum taxi strip width for a 180 degree turn based on a maximum nose wheel deflection of 80% +- 2%?

A

54 Feet 2 Inches

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4
Q

What is the maximum runway slope approved for takeoff and landing operations?

A

+2% Uphill and -2% Downhill.

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5
Q

When is use of the Autothrottles prohibited?

A

Use of the Autothrottles with wing anti-ice ON during takeoff and go-arounds is prohibited.

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6
Q

What is the Turbulent Air Penetration Speed?

A

270 KCAS/.75M

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7
Q 
Max Tailwind Component?
Max Airport Altitude?
Max Runway Slope?
Max Number of Pax?
Max Number of Occupants?
A 
10 Knots
15,000 Feet
\+2/-2%
19
22
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8
Q

What is the Maximum Landing Gear extended altitude and Maximum Landing Gear extension & retraction speed?

A

20,000 Feet & 225 KCAS/0.70M

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9
Q

What is the Fuel Capacity for the GIV?

Can the Fuel Capacity be exceeded and what are the limitations?

A

29,500 lbs.

Upload in excess of 29,500 Lbs. is permitted provided the Max Ramp and/or Max Takeoff weight is not exceeded.

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10
Q

What is the Minimum Engine Fuel Temperature for starting?

A

-40 degrees C for Starting.

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11
Q

What is the Maximum Engine Fuel Temperature?

A

+90 degrees C. Fuel temp up to 120 degrees C for a maximum of 15 minutes is permissible.

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12
Q

What is the Minimum Engine Oil Temperature for throttle movement?

A

-30 degrees C for throttle movement.

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13
Q

Above and Below what Gross Weights are the Maximum Permissible Fuel Imbalance?

A

Above 60,500 GW: 400 Lbs

Below 55,000 GW: 2,000 Lbs

Between the above GW’s: sliding scale.

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14
Q

What are the specifications of the Alternator and Converter?

A

Alternator:
115VAC, 3 Phase, 30KVA

Converter:
115VAC, 400Hz, 3 Phase, 23KVA &
28VDC, 50 Amps.

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15
Q

What is the Voltage & Amperage per hour of the aircrafts main batteries?

A

Two 24V, 40 Amp/Hour

20 Cell Nicad

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16
Q

External AC Power is capable of powering what busses?

A

Selecting External AC power ON with the AUX PWR switch will power all aircraft electeical busses.

In addition, the main batteries will be charged using EXT AC power.

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17
Q

What batteries connect to the Ground Service Bus?

A

Battery #2. With standard configuration, powers:

Wheelwell Lights, Utility Lights, and Service Lights.

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18
Q

When will you have Battery On Bus?

A
  1. The main batteries are powering the Essential DC Buses when either manually or automatically selected
  2. Starting the APU
  3. AUX Hydraulic Pump is operating
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19
Q

What are the Four Sources for the Remote Power Supply?

A

2 from the Aircraft Batteries

2 from Essential DC Bus

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20
Q

What Bus is powered by the

E-Inverter?

A

Essential AC Bus (Phase A Only)

Note: The E-Inverter supplies 0.8KVA, 115VAC, 400Hz, Phase A Only.

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21
Q

When the Emergency Power System is Armed, when will the “E” Batts activate?

A
  1. Either manually selected ON
  2. Loss of power to the Essential DC Bus, or
  3. 2.5 “G” or greater deceleration.
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22
Q

What capabilities are lost
if you lose the
Flight Hydraulic System pressure?

A

Onside Thrust Reverser

Yaw Damper (without windmilling pressure)

Autopilot (due to loss of Y/D)

Utility Pump

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23
Q

The Utility Pump is driven by the Flight Hydraulic System and uses fluid from the Combined Hydraulic System. When armed, what will cause the Utility Pump to turn on automatically?

A

CMB HYD FAIL CAS Message illuminates to indicate less than 800 Lbs pressure in the Combined System.

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24
Q

What condition will prevent automatic Utility Operation when the Utility Pump is armed?

A

FLT HYD HOT CAS message illuminates when the Flight Hydraulic System fluid temperature indicates 220 degrees F or greater.

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25
Q

When armed, under what conditions will cause the Auxiliary Hydraulic Pump to turn on automatically?

A

Combine & Utility Hydraulic pressure < 1,500 psi

Toe pedals depressed > 10 %

Nut Crackers in Ground Mode

26
Q

The Auxiliary Hydraulic Pump is capable of powering which components?

A 
Main Entrance Door
Flaps
Brakes
Parking/Emergency Brakes
Landing Gear/Doors (Ground Only)
27
Q

Ground Spoilers deploy automatically when what conditions are met?

A 
Power to Essen DC & Left Main Bus
Ground Spoilers are ARMED
Thrust Levers IDLE
Nut Crackers in GROUND MODE
Flaps > 22 degrees with wheel spin up or GPWS O'Ride switch ON
28
Q

When is use of the Speed Brakes Prohibited?

A

In Flight with Landing Gear Down and/or Flaps 39 degrees

29
Q

What are the Maximum Speeds for Flap Extension:

10 Degrees?
20 Degrees?
39 Degrees?

A

10: 250 Kts
20: 220 Kts
39: 170 Kts/GIV
180 Kts/SP

30
Q

What is the maximum operating altitude for extending the Flaps to 10 or 20 degrees?

A

45,000 Feet MSL

31
Q

What is the maximum operating altitude for extending the Flaps to 39 degrees?

A

20,000 Feet MSL

32
Q

Activation of the Master Warning Inhibit Switch will inhibit all aural tones associated with CAS messages, except for?

A

All Red CAS Messages

Coupled Data Invalid -
Lateral or Vertical

CAT II Invalid

33
Q

What are the two types of Windshear Warnings?

A

Amber - Caution:
Increasing Performance

Red - Warning:
Decreasing Performance

34
Q

When is the Windshear Warning active?

A

Rotation to 1,500’ AGL

Approach from 1,500’ feet
down to 10’ AGL

Missed Approach up to 1,500’ AGL

35
Q

What is the Emergency Landing Gear Nitrogen Blowdown Bottle Pressure?

A

3,000 PSI @ 70 Degrees F

36
Q

What is the Maximum Speed for Gear Retraction or Extension?

A

225 Knots

37
Q

Anti-Skid Braking is available from which Hydraulic Systems?

A

Combined

Utility

Auxiliary

38
Q

What is the Maximum Tire Speed for the GIV Non-SP w/o ASC-190?

And for the GIV-SP (SN 1214 & Sub)
Or Non-SP with ASC-190?

A

182 GS

195 GS

39
Q

What is the Maximum Speed for flying with the Landing Gear Extended?

A

Vle = 250 KCAS

40
Q

What is the Maximum Speed for Alternate Extension of the Landing Gear (Operation of the Emergency Gear Handle)?

A

175 KCAS

41
Q

What is the Maximum Permitted Cabin Pressure Differential in flight?

A

9.8 psi

42
Q

What is the Maximum permitted cabin pressure differential for Taxi, Takeoff or Landing?

A

0.3 psi

43
Q

What is the Temperature Range selection in Manual?

A

Manual = Full Cold - Valve Is Closed

Full Hot = Valve Is Full Open

44
Q

What is the Trip Point for the Oxygen System Pressure Relief Valve?

A

High Pressure Burst Disc pops at 2775 psi and Temp of 225 Degrees F +-5 degrees. Relief flow is also vented overboard through an overboard discharge line equipped with a green rupture disc.

45
Q

What Cabin Altitude will cause the Passenger Masks to deploy?

A

13,000 Feet, +- 500 FT Cabin Altitude

46
Q

What are the Cabin Pressure Control Power Sources in Auto? And Manual?

A

1 AC and 1 DC

AUTO: ESS AC Phase “A” Only

MANUAL: ESS DC

47
Q

What functions does the Safety Relief Valve provide?

A

Positive differential pressure relief at 9.7 +- 0.1 psi

Negative differential pressure relief at -0.25 psi

Rate Limiting 3,000’/min

48
Q

What is the Cabin and Cockpit Temperature Range selection in AUTO?

A

AUTO = 60-80 Degrees F

49
Q

What are the FOUR ways to Open the Bleed Air Isolation Valve?

A

Manual Selection of the Isolation Valve.

APU Bleed Air Switch - ON

Crank Master Switch - ON

Start Master Switch - ON

50
Q

What are the FOUR ways to Energize the Pack Valve Closed?

A

Pack Switch - OFF

COOL TURB HOT - ground only

Engine Start Switches - ON

Ram Air Switch - RAM

51
Q

Do not operate above what altitude without both Engine Bleeds ON?

A

41,000 Feet

52
Q

The APU is guaranteed to start at or below what altitude?

A

15,000 Feet

53
Q

Will the APU shut down automatically upon detection of a fire?

A

YES - During Ground or Flight operations if the fire detection circuits detect a fire. But not during the use of the APU Fire Test Switch.

NOTE: APU Fire Bottle will not discharge automatically. Depress the APU Bottle Discharge Switch.

54
Q

After an APU Start, when will the APU Load Control Valve allow APU Air for Engine Start and Pack Operation?

A

APU Air is available after the APU has reached an operating speed of 95% RPM or better for 4 seconds.

Wait at least 2 minutes prior to selecting APU Air ON.

55
Q

Fuel is supplied to the APU from where?

A

Left Wing Fuel Hopper using the Left Main Fuel Pump. The Right Main tank and pump can be used with the cross flow valve open.

56
Q

Pulling the Engine Fire Handle will shut off what items on the associated side?

A

Fuel
Hydraulics
Thrust Reverser
Electrics

57
Q

What is the Engine Start Duty Cycle?

A

3 Crank Cycles:
30 seconds ON, 3 mins OFF
30 seconds ON, 3 mins OFF
30 seconds OO, 15 mins OFF

58
Q

What is the recommended Airstart Envelope?

A

25,000 FT or Below, and

200-324 KCAS.

59
Q

With Wing Anti-Ice Operating, the Wing Warm Capsule Light will illuminate at what temperature?

A

100 degrees F or warmer

60
Q

Use of Cowl Anti-Ice is required for taxi and takeoff when static air temp (SAT) is —— or below and visible moisture, precipitation, or wet runway are present?

A

+10 Degrees C

61
Q

The L-R Low Pressure Warning CAS Message will occur when?

A

Pressure drops below 10+1 PSI
(s/n 1060 & subs and 1000-1189)

Pressure drops below 4+1 PSI and after 15 second delay
(s/n 1190 & subs & 1000-1189 with ASC 243)

Aviation (1 decks)

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