BD-700 Global 6500 Version 1.5 - Limits Flashcards

Limits required to be recalled and performed by memory per the Army BBD-700 ATM dated 23 FEB2025. (78 cards)

1
Q

Buoyancy Limitations

Takeoff or landing on runways near bodies of water &
For takeoff weights above the maximum landing weight…

A

OUTFLOW VLV 2 must be closed and one air-conditioning pack must be shutdown for takeoff.

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2
Q

Maximum airport pressure altitude for takeoff and landing

A

10,000 feet

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3
Q

Maximum operating altitude

A

51,000 feet

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4
Q

Maximum ambient air temperature approved for takeoff and landing

A

+50° C (122° F)

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5
Q

Minimum ambient temperature approved for takeoff

A

-40° C (-40° F)

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6
Q

During takeoff, use of cowl anti-ice in AUTO mode is __________.

A

Prohibited

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7
Q

The cowl anti-ice system must be ON when the OAT is ____ or colder and visible moisture in any form is present.

A

10° C

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8
Q

During takeoff, use of the wing anti-ice system in AUTO is __________.

A

Prohibited

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9
Q

The wing anti-ice system must be ON for takeoff when the OAT is ____ or colder and visible moisture in any form is present, or when ICE is annunciation by the ice detection syste.

A

5° C

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10
Q

During single bleed operation, the wing anti-ice system must be selected OFF when above _____.

A

41,000 feet

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11
Q

When in icing conditions, the minimum engine speed N2 limit is:

7000 Feet:

14000 Feet:

A

7,000 feet pressure altitude and below: 75.5%
14,000 feet pressure altitude and above: 79.0%

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12
Q

The maximum runway slopes approved for takeoff and landing are:

A

+2% uphill
-2% downhill

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13
Q

The maximum tailwind component approved for takeoff and landing:

A

10 knots

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14
Q

Operations from unprepared (i.e. gravel, grass, etc.) runways are _____________.

A

Prohibited

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15
Q

N1 Limits:

Ground Ops prohibited:
Caution Range:
Takeoff:
Max Continuous:
20s transient:
Reverse Thrust:

A

Ground Ops prohibited 66-80%
Caution Range (100-102.1%)
Takeoff: 102.1%
Max Continuous: 102.1%
20s transient: 103.3%
Reverse Thrust: 70.4%

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16
Q

N2 Limits:

Idle:
Takeoff:
Max Continuous:
20s transient:

A

Idle: 58.2%
Takeoff: 101.6%
Max Continuous: 99.9%
20s transient: 102.8%

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17
Q

Static ground operations in the range of _______ to _______ N1 is prohibited. Acceleration/deceleration thru this range is permitted.

A

66% to 80% N1

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18
Q

N1 Fan operation in the caution area range between and is permitted with no limitations.

A

100% and 102.1%

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19
Q

Engine operation in FZFG is prohibited.

A

< -19° C

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20
Q

Wind speed limits: Starting & Taxi

A

Crosswind: 35 knots
Tailwind: 20 knots

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21
Q

Wind speed limits: Static Ground

A

Crosswind: 15 knots
Tailwind: 10 knots

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22
Q

Wind speed limits: Takeoff

A

Takeoff crosswind procedure required when:

x-wind component greater than:

20 knots Below 5000’ PA:

15 knots Above 5000’ PA:

Do not exceed 66% N1below 30 KIAS. At 30 KIAS promptly set TO thrust.

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23
Q

Starter Cranking limits: Normal Engine Start

A

3 consecutive cycles of 3 minutes each with 15 seconds cooling between cycles (aka, 3 min on, 15 seconds off)

After 3 attempts, a 15-minute cooling period is required.

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24
Q

Fuel Imbalance: On ground

A

Below 20,250lbs of fuel: 1100 lb
Above 20,250lbs of fuel: 600 lb

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25
Usable Fuel Load (pressure refuel)
Wing: 15,050 lb each Center: 12,700 lb Aft: 2,300 lb Total: 45,100 lb
26
Usable Fuel Load (gravity refuel)
Wing: 13,850 lb each Center: 11,150 lb Aft: not available
27
Takeoff with engine fuel temperature indications below is prohibited.
5° C
28
Fuel crossfeed must be __________ for takeoff and landing.
OFF
29
Oil temperature limits:
Minimum for starting: -40° C Minimum before acce above idle: +20° C Maximum permissible: +160° C
30
Oil consumption limit in US qt per hour.
0.2
31
Operating Speeds: Slat/Flap Extended Speeds
Slats extended: 225 KIAS Flaps 6*: 210 KIAS Flaps 16*: 210 KIAS Flaps 30*: 185 KIAS
32
Operating Speeds: Landing gear extension / retraction
200 KIAS
33
Operating Speeds: Landing gear extended
250 KIAS
34
Flights at altitudes above with the landing gear extended is prohibited.
20,000 feet
35
Operating Speeds: Tire Limit Speed
196 knots
36
Operating Speeds: Turbulence Penetration Speed
300 KIAS or 0.80 Mach maximum, whichever is lower
37
Operating Speeds: Minimum Operating Limit Speed
Vmca in Takeoff: 88 KIAS Vmcg: 82 KIAS Vmcl in landing configuration: 87 KIAS
38
Operating Speeds: RVSM Maximum Cruise Mach Number
0.89
39
Maneuvering Limit Load Factors Slats/Flaps Retracted: Slats/Flaps Extended:
Slats/Flaps retracted: -1.0G to +2.5G Slats/Flaps extended: 0.0G to +2.0G
40
APU limits Min Temp to Start: Max temp for bleed air: Max RPM: EGT Start: EGT Ops:
Min Temp to Start: -40 Max temp for bleed air: 45 Max RPM: 106% EGT Start: 675-1038 EGT Ops: 613 - 732
41
Cabin Diff Rates: Max Neg relief Max diff taxi Max Landing Normal Max Delta P MSG
Max Neg relief: -0.5psi Max diff taxi: 0.1 psi Max Landing: 1.0 psi Normal: 10.33 psi Max: 10.73 psi Delta P MSG: 10.85 psi
42
Max APU Ops
45,000'
43
Max wo Ya Damper
41,000
44
Max APU Start / AUS Press
37,000
45
Max APU Bleed
30,000
46
Max Altitude with Flaps/Slats
18,000
47
Emer Depress Prohibited Below:
15,000
48
Pax mask Deploy:
14,500
49
Cablin ALT WARNING
9000
50
Cablin ALT Light
8200
51
SVS/EVS Switching N/A below
800
52
Min Alt for AP (ON)
400
53
Non Prec Appr AP Use
400
54
5g notam AP 7 AT (off)
400
55
Flight Spoilers
300'
56
Non Precision Appr A/P with Verticle Guidance
160
57
Precision Approach A/T
80
58
Do not hold in icing with:
slats and flaps out.
59
Landing with A/T is N/A without_____
Flaps 30.
60
RTO=
15M Wait
61
Icing Conditions:
10C TAT - -40 SAT
62
Max Spoilers N/A unless:
Emergency
63
N1 Rotation prior to crank requires:
Dry Crank
64
Wind > 20 Knots limited to
min thrust for taxi.
65
Fuel X-Feed off for
Takeoff and Landing
66
ITT Limits: Starting Ground: Starting Flight:
Start: 700° C (on ground) 850° C (in flight)
67
ITT Limits: Idle:
Idle: 850° C
68
ITT Limits: Takeoff: Takeoff thrust for 5 minutes AEO: 2 min for takeoff/Go-around only:
Takeoff: 890°C (Takeoff thrust for 5 minutes AEO), 900° C (2 min for takeoff/Go-around only)
69
ITT Limits: Max Continuous:
Max Continuous: 850° C
70
ITT Limits: 20s transient:
20s transient: 915° C
71
Weight Limits: Max Ramp
Max Ramp 99,750 lbs
72
Weight Limits: Max Takeoff
Max Takeoff 99,500 lbs
73
Weight Limits: Max Landing
Max Landing: 78,600 lbs
74
Weight Limits: Max ZFW
58,000 lbs
75
Weight Limits: Min ZFW
Min ZFW 48,200 lbs
76
Weight Limits: Max Fuel Load (pressurized):
Max Fuel Load (press) 45,100 lbs
77
Weight Limits: Min Op Weight
Min Op Weight 45,000 lbs
78
Weight Limits: Max Fuel Load (Gravity):
38.850 lbs