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GIV > GIV Limits > Flashcards

GIV Limits Flashcards

1
Q

Clean VMO/MMO

A

340 KIAS / 0.88M or 0.86M

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2
Q

Flaps 10°

A

250 kts / 0.60M

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3
Q

Flaps 20°

A

220 kts / 0.60 M

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4
Q

Flaps 39°

(Speed & Alt)

A

170 kts / 0.60 M

≤ 20,000 ft

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5
Q

Gear Extended

(Speed & Alt)

A

250 kts

≤ 20,000 ft

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6
Q

Gear Extension/Retraction Speed

A

225 kts / 0.70M

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7
Q

Turbulence Penetration Speed

A

270 KCAS / 0.75M

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8
Q

Mach Trim/Electric Elevator Trim Inoperative

(Speed)

A

0.75M

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9
Q

Engine Airstart

(Speed & Alt)

A

200-324 KCAS

≤25,000 ft

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10
Q

Manual Reversion/Dual Hyd Failure

(Speed & Alt)

A

250 KCAS

25,0000 ft

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11
Q

Guaranteed APU start in flight

(Speed & Alt)

A

250 KCAS

≤ 15,000 ft

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12
Q

Windshield Wipers

A

200 KCAS

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13
Q

Tire Speed

(GIV NON-SP (without ASC 190/266))

A

182 KCAS

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14
Q

Wing vortex generator not installed

A

0.80M

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15
Q

Yaw Damper inop > 18,0000 ft

“Maintain at least” (Speed & Alt)

A

220 KCAS

<41,000 ft (not correct, only if Mach Trim also inop)

<18,000 ft - maintain speed as a function of fuel qty

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16
Q

Reverse thrust cancellation (Initiate at…)

A

70 KCAS

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17
Q

VMCA

A

104 KCAS

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18
Q

VMCG

A

111 KCAS

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19
Q

Max Emergency Landing Gear Extension speed

A

175 KCAS

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20
Q

Maximum Thrust Reverser deployed in flight speed

A

200 KCAS

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21
Q

Ceiling

A

45,000 ft

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22
Q

Engine Bleed Air switch Off

(max altitude)

A

41,000 ft

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23
Q

APU Alternator

  • 100% electrical power
  • 75% electrical power
  • 50% electrical power
A
  • 100%: 20,000 ft if < 300 kts
  • 75%: 30,000 ft
  • 50%: 35,000 ft
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24
Q

Take off & landing airport max elevation

A

15,000 ft

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25
Q

APU temp limits:

  • 0%-50%
  • 51%-87%
  • Max running
  • Max with APU Air ON
A
  • 0%-50%: 973°C
  • 51%-87%: 972°C to 732°C
  • Max running: 732°C
  • Max with APU Air ON: 680°C
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26
Q

APU Starter Limits:

  • Battery
  • Ext DC
A
  • Battery: (30”/30”/30”, wait 20’,
    30”/30”/30”, wait 1 hr)
    • 3 consecutive starts (30 secs/start)
    • 20 mins cooldown
    • 3 add’l starts may be made
    • 1 hr cooldown (before next full starter cycle)
  • Ext DC: (15”/15”, wait 20’, 15”/15”, wait 1 hr)
    • 2 consecutive starts (15 secs/start)
    • 20 mins cooldown
    • 2 add’l starts may be made
    • 1 hr cooldown (before next full starter cycle)
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27
Q

APU successful consecutive start limit

A

6 at 10 min intervals

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28
Q

Engine starter duty limits

A
  • 30”/3’/30”/3’/30”, then wait 15’
    • 3 crank cycles , 30 secs per cycle
    • 3 mins between start attempts
    • After 3 cycles, delay use of starter for at least 15 mins
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29
Q

Fuel Tank Limits

  • Right/Left
  • Total
A
  • Right/Left: 14,750 lbs
  • Total: 29,500 lbs

(Fuel in excess permitted if max ramp/takeoff weight not exceeded and CG w/in limits)

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30
Q

Max Fuel Imbalance

A
  • 2,000 lbs @ 55,000 lbs GW
  • 400 lbs @ 60,500 lbs GW
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31
Q

Max Fuel Tank Temp

A

+54°C

32
Q

Min Fuel Tank Temp

A

-40°C

33
Q

Max Engine Fuel Temp

A

90°C (120°C for max 15 mins)

34
Q

Minimum Engine Fuel Temp

A

-40°C

35
Q

Max Oil Inlet Temp

A

105°C (up to 120°C for max 15 mins)

36
Q

Min Oil Temp for starting

A

-40°C

37
Q

Min Oil Temp for operating power levers

A

-30°C

38
Q

Min Oil Px at idle

A

16 psi

39
Q

Min Oil Px for takeoff (T/O pwr)

A

30 psi

40
Q

Takeoff EPR

A

must not exceed rated value by more than 0.01

41
Q

Fuel Boost Pump use

(CAUTION: Suction feed alt limit)

A

All shall be ON for all phases of flight unless fuel balancing is in progress

(CAUTION: Suction feed ≤ 20,000 ft)

42
Q

Max load limits (Gs)

  • Flaps Up
  • Flaps Down
A
  • Flaps Up: -1 to 2.5 Gs
  • Flaps Down: 0 to 2.0 Gs
43
Q

Personnel Limits

  • Min Flight Crew
  • Max Pax
  • Max Occupants
A
  • Min Crew: 3
  • Max Pax: 26
  • Max Occ: 30
44
Q

Max Tailwind - takeoff/landing

A

10 kts

45
Q

Max Crosswind

  • landing
  • Wet runway / Touch & Gos
A
  • Landing: 24 kts (max demo’d)
  • Wet rwy / T&G: 15 kts
46
Q

Max Runway Slope

A

± 2%

47
Q

Cabin Differential:

  • Max
  • Max T/O / Landing
A
  • Max: 9.8 psi
  • Max T/O / Landing: 0.3 psi
48
Q

Max wind with Cargo Door Strut installed

A

50 kts

(Do not open cargo door if actual or anticipated wind will exceed 40 kts)

49
Q

Do not operate _________ without Engine Bleed Air switches ON and each engine being bled by either the ACM Pack or Engine Cowl A/I.

A

> 41,000 ft

50
Q

AOA indication and use

A

Must be in white band one fwd motion;

May not be used for takeoff rotation speed reference

51
Q

Max fuel quant for takeoff with Yaw Damp inop

A

9,000 lbs

52
Q

Speed with Yaw Damp inop <18,000 ft

A

Maintain airspeed as a function of fuel quantity [QRH EE-14]

53
Q

Speed with Yaw Damp and Mach trim compensation inop

(& max alt)

A

Observe speed limitations for both failures

≤ 41,000 ft

54
Q

Operation of cowl anti-ice when:

(Engine recommendations)

A
  • taxi & takeoff when SAT is < +10°C w/ visible moisture, precipitation, or wet runway

(Engine operation of 85% LP for 1 min is recommended just prior to takeoff and at 60 min intervals)

55
Q

Speed brakes not approved when:

A
  • Flaps - 39°
  • Landing Gear - DOWN
  • Above Vmo/Mmo
56
Q

Ground Spoilers inop takeoff permitted when:

A
  • Anti-skid is operative
  • Flaps 20°
57
Q

Radar Limits

A

Do not operate:

  • During refueling
  • <300 ft (92 m) of other refueling ops
  • <33 ft (10 m) of ground personnel (w/ 18” antenna installed)
58
Q

Landing Lights ground op limit

A

5 mins on the ground

59
Q

Auto-throttle limit w/ wing anti-ice:

A

Takeoff & Go Around: PROHIBITED

60
Q

Auto-throttle landing limit

A

Disengage by 50 ft AGL

61
Q

Autopilot limits:

  • Takeoff
  • Landing
  • IMC during VNAV
A
  • Takeoff: Do not engage < 200 ft AGL
  • Landing: Disengage by 50 ft AGL
  • IMC during VNAV: 300 ft AGL or 50 ft below MDA, whichever is higher
62
Q

Battery

  • Number installed
  • Type
  • Rating
  • Power for
A
  • 2 installed
  • NICAD
  • 24 VDC / 40 AMP / 20 cell
  • 2 APU starts + 20 mins of power
63
Q

E-batts

  • Number installed
  • Rating
  • Life
A
  • 2-8 installed
  • 6 AMP/Hrs
  • Approx 40 mins life
64
Q

Max Zero Fuel Weight

A

49,000 lbs

65
Q

Max Ramp Weight

A

73,600 lbs

66
Q

Max Takeoff Weight

A

73,200 lbs

67
Q

Max Landing Weight

A

58,500

68
Q

Max Ground Start TGT

A

700°C (momentary/2 secs)

69
Q

Max Airstart TGT

A

780°C (momentary/2 secs)

70
Q

TGT Limits

  • Takeoff & Go Around
  • Max Continuous
  • Max Reverse
  • Max Overtemp
A
  • Takeoff & Go Around: 716-800°C
  • Max Continuous: 715°C
  • Max Reverse: 695°C
  • Max Overtemp: 801-820°C
71
Q

LP Limits

  • Takeoff & Go Around
  • Max Continuous
  • Max Overspeed
A
  • Takeoff & Go Around: 95.5%
  • Max Continuous: 95.5%
  • Max Overspeed: 98.3%
72
Q

Maneuvering Speed (VA)

A

170 kts

73
Q

APU Operating RPM

Overspeed

A

Operating RPM: 100% ±3%

Overspeed: 110%

74
Q

Record APU time operating above ________?

A
  • FL300
75
Q

EPR pilot selectable range?

A

0.85-2.0

76
Q

Can you dispatch with Stall Barrier/Warning inop?

A

One allowed inop with reference to MEL.

GIV (7 decks)

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