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Global 6000 PK > Limitations > Flashcards

Limitations Flashcards

1
Q

Global 6000 model designation

A

BD700-1A10

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2
Q 
Structural weight limits
Max Taxi/ramp
Max T.O.
Max landing
Max zero fuel
Min flight
Min op. Empty
A 
MRW       99,750 
MTO        99,500
MLW        78,600
MZFW     58,000
MFW        48,200
MOEW     45,000
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3
Q

T.O. and land near body of water
Above max landing weight

A

Outflow valve 2 closed and 1 pack off

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4
Q

VMO < 8,000
> 8,000

A

< 8,000 300
> 8,000 340

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5
Q

MMO

30,260’ - 35,000’

A

0.89 M

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6
Q

VMCG / VMCA 6/16 flaps

A

80 kts / 86kts

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7
Q

VMCG / VMCA 0 flaps, sup. 24

A

92 kts / 95 kts

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8
Q

Slats extended

A

225 kts

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9
Q

Flaps 6
16
30

A

210 kts
210 kts
185 kts

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10
Q

Gear VLO / VLE

A

200 kts

250 kts / 0.70M

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11
Q

Tire limit

A

183 kts

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12
Q

Turbulence

A

300 kts / 0.80M

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13
Q

Load Factor Limits

Slats / flaps retracted
Slats / flaps extended

A

-1.0 to +2.5G

  1. 0 to +2.0G
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14
Q

Approach
Max glide angle _____

Glide angle between ___ and___ must be……

Glide angle ___ to ___ see supplement ___

A

3.5

3.5 and 4.5
w/restrictions listed in sup. 29

4.5 to 5.5….40

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15
Q

Spoilers retracted by

A

300’ AGL

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16
Q

Max occupancy

A

22 including 19 pax or the number of certified seats, whichever is less.

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17
Q

Min crew

A

1 pilot and 1 copilot

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18
Q

Slope

A

+2% to -2%

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19
Q

Max alt. for T.O. and land

A

10,000’

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20
Q

Max alt for T.O. and land IAW sup. 20

A

13,700’

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21
Q

Max operating alt.

A

51,000’

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22
Q

Max alt. With gear extended

A

20,000’

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23
Q

Max alt. With flaps extended

A

18,000’

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24
Q

Min. Temp

Max. Temp

A

-40 C
+50 C

note:
See AFM 02-04-01 for temp.
Limits at altitude

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25
Q

Cowl AI on ( ground )

A

+10 C OAT or below and visible moisture,

Less than 1sm vis., or on contaminated surfaces

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26
Q

Wing AI on ( ground )

A

+5 C OAT or below and visible moisture,

Less than 1sm vis., or on contaminated surfaces

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27
Q

Wing and cowl AI on ( in flight )

A

+10 C TAT to -40C SAT in visible moisture

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28
Q

AI holding limitation

A

No slats

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29
Q

Min N2 ( accept on final Aprch ) with green wing ice indications

A

76%

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30
Q

Cold weather supplement

A

FCOM 1, sup. 1

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31
Q

True or False

T.O. permitted with frost on bottom of wing

A

True

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32
Q

True or False

Takeoff prohibited with contamination on any surface

A

False

T.O. Prohibited with contamination on critical surfaces

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33
Q

AI switch position when ice is detected

A

ON

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34
Q

True or False

AI auto prohibited for T.O.

A

True

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35
Q

Max demonstrated crosswind

A

29 kts

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36
Q

Max tailwind T.O. and land

A

10 kts

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37
Q

Max tailwind for start

A

20 kts

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38
Q

Max X wind comp. for engine start

A

35 kts

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39
Q

Max X wind comp. for take off

A

35 kts

40
Q

Thrust limit when wind exceeds
20 kts ( taxi )

A

Minimum thrust

41
Q

Crosswind T.O. Over 20 kts

A

N1 66% max below 30 kts

42
Q

Tailwind start

A

Any external or EICAS indication of N1 rotation
Crank for 30 seconds then immediate
Auto start and Run

43
Q

True or False

OMS mode can be engaged for flight

A

False

44
Q

True or False

One stall pusher can be off in flight

A

False

Both must be on

45
Q

True or False

IMS panel must be closed for flight

A

True

46
Q

APU type and max rpm

A

RE 220 and 106%

47
Q

APU Altitudes

Max operating
Max start
Max bleed extraction

A

Max operating 45,000’
Max start 37,000’
Max bleed 30,000’

48
Q

Min temp ( ground ) APU

A

-40 C

49
Q

APU Gen. Load limit

Ground
In flight

A

40 KVA

50
Q

APU starter limit

A

3 start attempts with 1 min. Rest

Between then 60 min. Rest

51
Q

APU above 37,000’

A 
Associated hydraulic pump must be selected off
1B - AC bus 3
2B - AC bus 2
3B - AC bus 1
3A-  AC bus 4
52
Q

When is APU oil replenishment allowed?

A

On ground with APU off

Reservoir quantity greater than 1.5 qt

Within 45 min after APU shutdown

OAT -12 C or above

53
Q

Ground operation with flight compartment
Temp in excess of ___ for greater than ___ minutes is ___

A

40 C
30 minutes
Prohibited

54
Q

Engine type

A

BR700-710A2-20

55
Q

Engine ITT limits

Start ground
Start flight
Idle
T.O.
Max cont.
Transit

A

Start ground 700 C
Start flight 850 C
Idle 860 C
Take off 900 C
Max cont. 860 C
Trans. 905 C
( 20 sec. )

56
Q

Engine T.O. Thrust lim.

ITT
N2
N1
Time

A 
ITT Max     900 C
N2              99.6% 
N1               102.0%
5 min 2 eng. 
10 min 1 eng.
57
Q

Engine Max continuous operation

ITT
N2
N1

A

ITT 860 C
N2 98.9%
N1 102.0%

58
Q

What rpm range is to be avoided

During ground ops?

A

Steady operation
66 -80% N1
( FADEC will not allow it )

59
Q

What min. Oil pressure is engine

Required to be shut down?

A

25 PSI

As directed by checklist

60
Q

Engine oil temps

Start
Above idle
Max

A

-40 C
+20 C
+160 C

61
Q

Engine oil

consumption rate and
Replenishment lim.

A

0.21 qt / hr max

Prohibited below -12 C

62
Q

Engine oil replenishment time

A

Between 5 - 30 minutes post shutdown

63
Q

T.O. thrust time lim.

2 engine
1 engine

A

5 min.

10 min.

64
Q

Engine start max N2 engage

A

42%

65
Q

Engine starter cycle limit

A

1st attempt 3 min on / 15 sec off
2nd attempt 3 min on / 15 sec off
3rd attempt 3 min on / 15 min off

66
Q

Pack discharge temp in manual

A

5 - 60 C

67
Q

Air cond. and pres. in manual mode

A

1 pack off

68
Q

Aux press max alt.

A

41,000’

69
Q

APU bleed extraction for air cond.

A

45 C OAT max

70
Q

Air cond. and press QFE ops

A

Manually set 0 landing elevation

71
Q

Emer Depress max alt

A

15,000’

72
Q

Differential pressure

Pos.
Neg.
Taxi T.O.
Landing

A
  1. 73 psi max
    - 0.5 psi max
    0.1 psi max
    1.0 psi max
73
Q

Fuel imbalance max inflight

A

1100 lbs

74
Q

Fuel imbalance max ground

A

Below 19,450 lbs 1100 lbs

19,450 - 20,250
1100 - 600

Above 20,250 600

75
Q

Useable fuel

Wings
Center
Aft
Total

A

15,050 lbs each
12,700
2,300
45,100

76
Q

Min fuel aft and center

A

500 lbs min aft and center
Aft and center unusable unless
Center - wing full and cruise alt > FL300
Aft - wing above 5,500 and cruise > FL300

77
Q

Towing fuel

A

5000 lb min. Unfinished interior. In actuality, 1900 lbs on nose wheel.
12000 max per wing to avoid spillage

78
Q

Engine fuel temp for T.O.

A

+5 C min

79
Q

True or False

Cross feed can be on for T.O. And land

A

False

80
Q

Min fuel go around

A

600 lbs / wing and max 10 deg. NU

81
Q

Wide cut fuel limited to FL___ and below
Until fuel temp is
>? Or < ? ___C

A

FL130

Below 15 C

82
Q

Recirculation system lim.

A

Prohibited with wide cut fuel

Asymmetric use prohibited

83
Q

Yaw damp off max alt

A

41,000’

84
Q

Autothrottle engage on T.O.

A

Below 60 kts

85
Q

True or False

AT is permitted with one inop.

A

False

86
Q

Autopilot height

Engage ( climbing )
Precision
Non prec w/o VNAV
Non prec w/ VNAV

A

400’
80’
400’
160’

87
Q

True or False

Remaining in TO / VTO vertical mode
After eng. failure is prohibited

A

True

88
Q

EDM selection below FL____ prohibited

A

FL250

89
Q

Max available reverse thrust above

65 KIAS

A

70% N1 for 30 sec.

EEC controls this value

90
Q

What is required for a flight

To China

A

Ask JT

91
Q

True or False

FMS TOLD can be used on
Contaminated runways

A

False

92
Q

True or False

FMS TOLD prohibited for
QFE operations

A

True

93
Q

True or False

Use of VNAV during
QFE ops. Prohibited

A

True

94
Q

At What altitude is switching from

SVS to EVS prohibited

A

Below 800’

95
Q

Max crosswind for HUD EVS

Approach

A

15 kts

96
Q

Is HUD EVS approach without

FD and AP authorized

A

No

FD or AP guidance is required

97
Q

Is HUD EVS approach
Authorized with
flaps half speed

A

No

Global 6000 PK (10 decks)

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