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NetJets - Bombardier Global 6000 > Global - Limitations (Black Limits) > Flashcards

Global - Limitations (Black Limits) Flashcards

1
Q

Max 6000 taxi/ramp weight? 5000/5500?

A
  • 6000: 99,750 lb.
  • 55/5000: 92,750 lb.
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2
Q

Max 6000 takeoff weight? 5000/5500?

A
  • 6000: 99,500 lb.
  • 55/5000: 92,500 lb.
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3
Q

Max Landing weight?

A
  • 78,600 lb.
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4
Q

Max ambient air temp for takeoff and landing?

A
  • +50°C.
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5
Q

Min ambient air temp for takeoff and landing?

A
  • -40°C.
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6
Q

Cowl anti-ice during takeoff limit?

A
  • Must not be in AUTO.
  • OFF or ON only.
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7
Q

Wx conditions for turning on cowl anti-ice while inflight?

A
  • TAT ≤ 10°C + Visible Moisture (i.e., rain, snow, or visibility < 1sm), unless SAT ≤ -40°C.
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8
Q

Wx conditions for turning on cowl anti-ice while on the ground? What about Wing Anti-Ice on the ground?

A
  • Cowl Anti-Ice: OAT/SAT ≤ 10°C + Visible Moisture (i.e., rain, snow, or visibility < 1sm) or operating on contaminated surfaces.
  • Wing Anti-Ice: OAT/SAT ≤ 5°C + Visible Moisture (i.e., rain, snow, or visibility < 1sm) or operating on contaminated surfaces.
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9
Q

Define inflight icing conditions?

A
  • TAT ≤ 10°C with visible moisture, unless SAT is ≤ -40°C.
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10
Q

Minimum engine speed, while in icing conditions?

A
  • 76% N2.
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11
Q

Maximum tail wind component approved for takeoff and landing?

A
  • 10 kt.
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12
Q

Maximum number of occupants for operation?

A
  • 22 (19 pax + 2 pilots + 1 f/a).
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13
Q

Prohibited runway conditions for operations?

A
  • Unprepared surfaces (i.e., gravel, dirt, grass, etc.).
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14
Q

Limitation for operating display units with flight compartment temperatures in excess of 40°C?

A
  • Operations greater than 30 minutes are prohibited.
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15
Q

Maximum glidepath angle?

A
  • Maximum of 5.5°
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16
Q

Maximum ITT for start on the ground and inflight?

A
  • 700°C ITT for starting on the ground.
  • 850°C ITT for starting inflight.
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17
Q

Minimum N2 speed during idle?

A
  • 5/6000: 58.0% N2 Minimum.
  • 5500: 58.2% N2 Minimum.
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18
Q

Max N2 speed for takeoff?

A
  • 5/6000: 99.6% N2.
  • 5500: 101.6% N2.
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19
Q

Max N1 fan speed for takeoff?

A
  • 5/6000: 102.0% N1.
  • 5500: 102.1% N1.
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20
Q

Max ITT for takeoff?

A
  • 5/6000: 900°C.
  • 5500: 890°C (900°C transient for 2 min on T/O & G/A).

NOTE: 5 min 2 eng,10 min 1 eng.

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21
Q

Max continuous N2?

A
  • 5/6000: 98.9% N2 (Transient 99.8% N2 for 20 sec).
  • 5500: 99.9% N2 (Transient 102.8% N2 for 20 sec).
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22
Q

Max continuous N1 fan speed?

A
  • 5/6000: 102.0% N1 (Transient 102.5% N1 for 20 sec).
  • 5500: 102.1% N1 (Transient 103.3% N1 for 20 sec).
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23
Q

Max continuous ITT?

A
  • 5/6000: 860°C (Transient 905°C for 20 sec).
  • 5500: 850°C (Transient 915°C for 20 sec).
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24
Q

Time limit for takeoff thrust all engines operating?

A
  • 5 min.
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25
Q

Time limit for takeoff thrust, one engine inoperative (OEI)?

A
  • 10 min.
26
Q

Minimum crank time for engine start with N1 rotation due to tailwind?

A
  • Hold START switch to L or R CRANK for 30 seconds, then go right to AUTO start.
27
Q

Thrust limit for taxing when winds exceed 20 kts?

A
  • Minimum only.
28
Q

Max N2 RPM for engine starter engagement?

A
  • 42% N2.
29
Q

Maximum wing fuel imbalance during flight?

A
  • 1100 lb.
30
Q

Usable fuel in each main wing tank?

A
  • 15,050 lb (30,100 lb total wings).
31
Q

Usable fuel in center tank?

A
  • 6000: 12,700 lb.
  • 55/5000: 9,150 lb.
32
Q

Usable fuel in aft tank?

A
  • 6000: 2,300 lb (5500 has no aft tank).
33
Q

Minimum fuel for a go-around?

A
  • 600 lb per side.
  • Wings level, max 10° nose up.
34
Q

Minimum engine fuel temperature for takeoff?

A
  • +5°C.
35
Q

Minimum oil temperature for starting?

A
  • -40°C.
36
Q

Maximum oil temperature?

A
  • 160°C.
37
Q

Maximum oil consumption rate per engine?

A
  • 5/6000: 0.21 US qt/hr.
  • 5500: 0.20 US qt/hr.
38
Q

Maximum APU rpm?

A
  • 106%.
39
Q

Maximum altitude for APU bleed air extraction?

A
  • 30,000’.
40
Q

Maximum OAT for APU bleed extraction for air conditioning?

A
  • 45°C.
41
Q

Maximum slats extended speed?

A
  • 225 kt.
42
Q

Maximum speed for flaps 16°?

A
  • 210 kt.
43
Q

Maximum speed for flaps 6°?

A
  • 210 kt.
44
Q

Maximum speed for flaps 30°?

A
  • 185 kt.
45
Q

Landing gear extended speed (Vle)?

A
  • 250 kt / 0.7M
46
Q

Maximum altitude for landing gear extended?

A
  • 20,000’ (200 kt to extend is a bigger issue).
47
Q

Tire limit speed?

A
  • 5/6000: 183 kt.
  • 5500: 196 kt.
48
Q

Maneuvering limit load factors - slats/flaps retracted?

A
  • -1.0 G to +2.5 G.
    (FCOM 1- Limits)
49
Q

Maneuvering limit load factors - slats/flaps extended?

A
  • 0.0 G to +2.0 G.
    (FCOM 1 - Limitations)
50
Q

Cooling pack discharge temperature range during manual mode operations?

A
  • 5°C to 60°C.
51
Q

Pack limit during manual mode operations?

A
  • One pack must be selected off.
52
Q

Maximum differential pressure?

A
  • 10.73 psi
53
Q

Maximum negative relief?

A
  • -0.5 psi
54
Q

Maximum differential pressure during taxi and takeoff?

A
  • 0.1 psi
55
Q

Maximum differential pressure during touchdown?

A
  • 1.0 psi.
56
Q

Maximum altitude with a yaw damper disengaged?

A
  • 41,000 ft.
57
Q

Minimum speed to set auto-throttles on takeoff?

A
  • 60 kt.
58
Q

APU generator load limit?

A
  • 40 kVA.
59
Q

Maximum altitude for slats/flaps extended?

A
  • 18,000 ft (gear extension is FL200).
60
Q

Limitations on the use of MAX spoilers?

A
  • Prohibited, except during emergencies, or if required by AFM procedure.
61
Q

Minimum Runway Dimensions (L x W x Slope)?

A
  • 4,500’ (L) x 75’ (W) x ±2% (Slope).

NetJets - Bombardier Global 6000 (5 decks)

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