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Gulfstream G450 > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum zero fuel weight:

A

49,000 lbs

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2
Q

Maximum ramp weight:

A

75,000 lbs

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3
Q

Maximum takeoff weight:

A

74,600 lbs

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4
Q

Maximum landing weight:

A

66,000 lbs
ASC 007 lowers it to 58,500 lbs for Cat C approaches

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5
Q

Maximum permissible fuel imbalance in-flight:

A
  • Up to weight 55,000 = 2000lbs
  • Greater than 55,000 less than 60,500 = consult chart
  • 60,500 to 75,000 = 400 lbs
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6
Q

Maximum cabin differentials:

A

9.94 psi

0. 3 psi for taxi, takeoff or landing

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7
Q

Single engine autopilot coupled go-around:

A

Not Approved

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8
Q

Minimum autopilot engagement height:

A

200 ft

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9
Q

Minimum autopilot disengage height:

A
  • 60 ft from an ILS Approach

- 50 ft below MDA/DA from an LNAV/VNAV Approach

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10
Q

Use of auto-throttles on single-engine approach:

A

Not permitted

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11
Q

Use of speed brakes with the HMG in operation:

A

Slow Operation (approx 3 seconds for full range of movement)

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12
Q

IDG electrical load limit:

A

45% (18kVa) when ambient temperature is greater than 43°c (110°f)

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13
Q

Speed brakes not approved for extension in-flight when:

A

Flaps are at 39°, or landing gear extended

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14
Q

Take off permitted with automatic ground spoilers inoperative provided:

A
  • Antiskid is operative
  • 20° flaps are used
  • Cowl and wing anti-ice systems are not used
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15
Q

Usable fuel capacity:

A

29,500 lbs

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16
Q

Wing anti-icing must be turned on:

A

If icing conditions are imminent, or immediately upon detection of ice formation on wings, winglets or windshield edges

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17
Q

Cowl anti-icing is required on the ground:

A

When SAT is +10°c or below and visible moisture, precipitation or wet runways are present

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18
Q

Cowl anti-icing is required in flight:

A

As indicated in the cowl anti-icing table, when visible moisture or precipitation is present or when signs of icing are observed

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19
Q

Procedure to shed engine ice in flight is:

A

Quickly retard one engine at a time to idle, hold for 5 seconds and then accelerate engine to 85% LP RPM for 2 seconds

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20
Q

Take off is permitted with anti-skid inoperative, provided:

A
  • Runway is dry
  • Ground spoilers are operative
  • 20° flaps are used
  • Cowl and wing anti-ice systems are not used
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21
Q

Do not operate weather radar on the ground:

A
  • During refueling of the airplane
  • Within 300 ft of fueling operations
  • Within 49 ft of ground personnel
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22
Q

A current FMS database is required for:

A

GPS Approaches

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23
Q

Localizer based approaches must be flown using the following displayed / coupled navigation source:

A

NAV (green data)

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24
Q

The following approaches may be flown using FMS as the displayed / coupled source:

A

RNAV (GPS)
VOR, VOR/DME, VOR/DME RNAV
NDB
GPS

25
Q

TCAS operation with one engine inoperative:

A

TA only as operating mode

26
Q

Maximum speed for RVSM operations:

A

0.85 M

27
Q

Crew and passenger oxygen masks are not approved for use above:

A

40,000 ft cabin altitude

Newer Scott EROS crew masks is approved for use to a cabin altitude of 45,000 ft

28
Q

General EICAS range marking colors:

A

Green or White = Normal Range Values
Amber = Caution Range Values
Red = Warning Range Values

29
Q

APU starting limits (battery power):

A

Three consecutive start attempts, followed by 1 hour cooldown

30
Q

APU starting limits (external DC power):

A

3 start attempts, 15 minute cool down in between each attempt

31
Q

Maximum APU operating altitude:

A

37,000 ft

32
Q

APU generator electrical load limit:

A
  • 100% (40kVa) Sea Level to 37,000 ft

- 85% between 30,000 and 37,000 at speeds faster than 0.85 M

33
Q

Maximum engine TGT prior to ground start:

A

200 °c

34
Q

Maximum takeoff TGT:

A

800°c
5 minutes both engines
10 minutes on one engine

35
Q

Maximum continuous TGT:

A

715°c

36
Q

Maximum crosswind component for engine start:

A

25 knots

37
Q

Maximum tailwind component for engine start:

A

25 knots

38
Q

Stabilized engine operation on the ground (static) is prohibited between:

A

60% and 72% LP RPM

39
Q

Maximum runway slope for takeoff and landing operations:

A

+/- 2%

40
Q

Maximum tailwind component approved for takeoff and landing:

A

10 knots

41
Q

Maximum approved airport pressure altitude for takeoff or landing:

A

15,000 ft

42
Q

Maximum operating altitude:

A

45,000 ft

43
Q

Maximum operating altitude with the yaw damper inoperative, coupled with failure of the mach trim compensation:

A

41,000 ft

44
Q

Maximum landing gear extension altitude:

A

20,000 ft

45
Q

Maximum altitude for extending flaps 39°:

A

20,000 ft

46
Q

Maximum altitude for extending flaps 10 or 20 degrees:

A

25,000 ft

47
Q

Minimum control speed, air:

A

106 kcas

48
Q

Minimum control speed, landing:

A

99 kcas

49
Q

Minimum control speed, ground:

A

109 kcas

50
Q

Maneuvering speed (Va):

A

206 kcas

51
Q

Flaps extended speeds (Vfe / Mfe):

A

Takeoff (10°): 250 kcas / 0.60 m
T/O APP (20°): 220 kcas / 0.60 m
Down (39°): 180 kcas / 0.60 m

52
Q

Landing gear extended speed (Vle / Mle):

A

250 kcas / 0.70 M

53
Q

Landing gear operation speeds (Vlo / Mlo):

A 
225 kcas / 0.70 M (normal operation)
175 kcas (alternate operation)
54
Q

Minimum speeds with yaw damper inoperative:

A

210 knots above 20,000 ft

Use reference table below 20,000 ft

55
Q

Maximum speed with Mach trim or electric elevator trim inoperative:

A

0.75 M

56
Q

Turbulence penetration speeds:

A

270 kcas / 0.75 M above 10,000 ft

240 kcas below 10,000 ft

57
Q

Maximum tire speed:

A

195 knots

58
Q

Maximum speed with emergency stabilizer trim armed, autopilot engaged and a jammed elevator:

A

270 kcas / 0.75 M

59
Q

Max demonstrated crosswind for takeoff and landing

A

24 knots

Gulfstream G450 (20 decks)

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