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Gulfstream G550 > G550 Limitations > Flashcards

G550 Limitations Flashcards

1
Q

Maximum runway slope for takeoff and landing operations

A

+/- 2%

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2
Q

Maximum tailwind component approved for takeoff and landing

A

10 knots

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3
Q

Maximum approved airport pressure altitude for takeoff and landing

A

14,500 normal
12,000 early models without mod
15,000 later models with high alt mod

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4
Q

Maximum operating altitude

A

51,000 feet

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5
Q

Maximum altitude with a single air conditioning pack operating

A

48,000 feet

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6
Q

Maximum operating altitude with the yaw damper inop

A

45,000 feet

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7
Q

Maximum landing gear extension altitude

A

20,000 feet

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8
Q

Maximum altitude for extending flaps 39

A

20,000 feet

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9
Q

Maximum altitude for extending flaps 10 or 20

A

25,000 feet

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10
Q

Minimum control speed, air

A

112 KCAS

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11
Q

Minimum control speed, landing

A

110 KCAS

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12
Q

Minimum control speed, ground

A 
107 KCAS (Sea Level)
86 KCAS (15,000 ft)
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13
Q

Maneuvering speed (Va)

A

206 KCAS

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14
Q

Flaps extended speed (Vfe/Mfe)

A

Takeoff (10): 250 KCAS/0.60M
T/O APP (20): 220 KCAS/0.60M
DOWN (39): 170 KCAS/0.60M

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15
Q

Landing gear extended speed (Vle/Mle)

A

250 KCAS/0.70M (gear doors open or closed)

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16
Q

Landing gear operation speeds (Vlo/Mlo)

A 
225 KCAS/0.70M (normal ops)
175 KCAS (alternate ops)
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17
Q

Maximum speeds with yaw damper inop

A

210 knots above 20,000 ft

Use ref table below 20,000 ft

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18
Q

Maximum speed with Mach Trim or electric elevator trim inop

A

0.80M

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19
Q

Turbulence penetration speeds

A

270KCAS/0.80M above 10,000 ft

240 KCAS below 10,000 ft

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20
Q

Maximum tire speed

A

195 knots

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21
Q

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

A

270 KCAS / 0.80M

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22
Q

Maximum zero fuel weight

A

54,500 lbs

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23
Q

Maximum ramp weight

A

91,400 lbs

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24
Q

Maximum takeoff weight

A

91,000 lbs

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25
Q

Maximum landing weight

A

75,300 lbs

26
Q

Maximum fuel imbalance in flight

A

2,000 lbs

27
Q

Proceed with fuel balancing before the fuel imbalance exceeds:

A

1,000 lbs

28
Q

Maximum cabin pressure differentials:

A
  1. 48 psi

0. 3 psi for taxi, takeoff and landing

29
Q

Internal baggage door shall remain closed above:

A

40,000 feet (limited to 5 mins open)

30
Q

Is a single engine autopilot-coupled go-around approved?

A

No

31
Q

Minimum autopilot engage height

A

200 feet

32
Q

Minimum autopilot disengage height

A

60’ below DH on ILS

50’ below MDA from LNAV/VNAV

33
Q

Are autothrottles allowed for single-engine approaches?

A

No

34
Q

Use of speedbrakes with the HMG in operation:

A

Slow operation (3 seconds for full range of movement)

35
Q

Speedbrakes not approved for extension in flight when:

A

Flaps 39 or Landing Gear Extended

36
Q

Takeoff permitted with automatic ground spoilers inoperative provided:

A

Anti-skid is operative
20 Flaps used
Cowl and Wing anti-ice systems are not used

37
Q

Usable fuel capacity:

A

41,300 lbs

38
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

39
Q

Cowl anti-icing is required on the ground:

A

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

40
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

41
Q

Procedure to shed engine ice in flight:

A

Quickly retard one engine at a time to idle, hold for 5 seconds and then accelerate engine to 90% LP RPM.
The power lever may then be returned to its original position

42
Q

Use of flaps while holding in icing conditions:

A

Not permitted

43
Q

Takeoff is permitted with anti-skid inoperative, provided:

A

Runway is dry
Ground spoilers are operative
20 Flaps used
Cowl and wing anti-ice systems are not used

44
Q

Do not operate weather radar on the ground:

A

During refueling
Within 300 feet of fueling ops
Within 49 feet of ground personnel

45
Q

A current FMS database is required for:

A

GPS approaches

46
Q

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

A

NAV (“Green” data)

47
Q

What approaches may be flown using FMS as the displayed/coupled source?

A

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

48
Q

TCAS operation with one engine inoperative:

A

TA ONLY

49
Q

Maximum speed for RVSM operations

A

0.87 M

50
Q

Crew and passenger masks are not approved for use above:

A

25,000 for passenger masks
40,000 for crew masks
45,000 if a/c has Scott EROS crew masks

51
Q

General EICAS range markings colors:

A

Normal range values - green or white
Caution range values - Amber
Warning range values - Red

52
Q

APU starting limits (battery power):

A

3 consecutive start attempts, followed by 1 hour cooldown

53
Q

APU starting limits (external DC power):

A

3 start attempts, 15 minute cooldown between each attempt

54
Q

Maximum APU operating altitude

A

45,000 feet

55
Q

APU generator electrical load limit:

A

100% (40kVA) sea level to 45,000 feet

56
Q

Maximum engine TGT prior to ground start:

A

150 C

57
Q

Maximum takeoff TGT:

A

900 C
5 minutes with both engines
10 minutes on one engine

58
Q

Maximum continuous TGT:

A

860 C - no time limit

59
Q

Maximum crosswind component for engine start:

A

30 knots

60
Q

Maximum tailwind component for engine start:

A

20 knots

61
Q

Stabilized engine operation on the ground (static) is prohibited between what power settings?

A

66% - 80% LP RPM

62
Q

The preferred method of engine airstart is:

A

Automatic

Gulfstream G550 (18 decks)

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