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G7500 > AFM LIMITATIONS > Flashcards

AFM LIMITATIONS Flashcards

1
Q

RVSM equipment on G7500

A 
1 Autopilot
1 Altitude alert
1 Altitude reporting Transponder
2 X Air Data Syst
2 X Pitot tube heater
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2
Q

Structural operational Weights

MRW
MTW
MLW
MZFW
Min Flight W
A 
MRW 	52.208 kg - 115.100 lbs
MTW	52.095 kg - 114.850 lbs
MLW	39.735 kg -   87.600 lbs
MZFW	30.617 kg -   67.500 lbs
MFW	27.216 kg -   60.000 lbs
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3
Q

Procedure for takeoffs and landings above MLW near body’s of water

A

Outflow valve no2 close and one of the packs off

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4
Q

Maximum altitude for takeoff and landing

A

10 000 ft

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5
Q

Max Outside Temp for takeoff and landing

A

55C (131F)

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6
Q

Minimum Outside Temp approved for takeoff

A

-40C

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7
Q

Maximum Operating Altitude

A

51 000 ft

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8
Q

Cowl Anti-ice must be ON

A

OAT is 10C (50F) or less and visible moisture in any form present, visibility 1500 m ( 1 mile) or less, rain, snow, slush or any form of precipitation present

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9
Q

Ice shedding engine procedure

A

When vibrations are detected
Increase engine thrust to 50% N1 for 5 sec minimum until engine vibrations return to normal
Perform this procedure every 18 min prior to takeoff
If takeoff is imminent, do not reduce the power but rather increase to takeoff settings

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10
Q

In flight Cowl Anti-Ice conditions

A

In flight cowl Anti-ice conditions 10C (50F) or bellow with visible moisture
Except when SAT is -40C (-40F)

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11
Q

Wing Anti-Ice

A

OAT is 5C (41F) or less and visible moisture or
TAT 10C (50F) or less - flying
NO Anti-Ice at or below -40C (-40F) or above TAT +10C

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12
Q

Super-cooled Large Droplets SLD

A

Flight into know SLD IS PROHIBITED
SLD is indicated by accumulation of ice on the cockpit windows
Wing and Cowl Anti-Ice must by ON

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13
Q

Max runway slop for Takeoff and Landing

A

+- 2

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14
Q

Tailwind for Takeoff and Landing

A

10 kts

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15
Q

Cold Weather

If airplane is exposed at temps…….

A

-20C the airplane should be operated according to FCOM VOL1 capt10 Adverse weather / Cold Weather Ops

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16
Q

Operation of avionics displays is prohibited in hot temp

A

Excess of 40C for 30 min

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17
Q

North Pole OPS

A

Operations North of 89.5 and

South of 89.5 are PROHIBITED

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18
Q

ENGINE

A

GE PASSPORT 20 19BB1A

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19
Q 
What is the maximum landing mass for the airplane?
A.	95,000 lb (43,091 kg)
B.	78,600 lb (35,652 kg)
C.	87,600 lb (39,735 kg)
D.	93,750 lb (42,524 kg)
A

C

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20
Q 
What is the maximum airspeed at which it is safe to extend/retract the landing gear?
A. 190 KIAS
B. 200 KIAS
C. 250 KIAS
D. 300 KIAS
A

B

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21
Q

Engine operating limits
ITT START
IDLE
TAKEOFF
MAX CONT

A

START on ground 750 C
in flight 875
IDLE. 65.9% minimum 995
TAKEOFF. 1035@ 103.7N1 & 114.9N2
MAX CONT 995@103.7 N1 & 114.9N2
T/O 5 min all engines 10 min one engine out
1077 C for 15 sec in case of Go- Around
975 C for high power fuel cut or quick windmill relight

22
Q

Engines STARTS are not permitted with tailwinds more then …..

A

20 KTS

23
Q

The starter MUST NOT be used if RPM exceeds

A

56% N2

24
Q

Normal Engine start tries?

A

2 consecutive cycles of 5 min each with 5 min cool down after each one
After the 3 one up to the 10 trial a 15 min cool down in between cycles

25
Q

Fuel imbalance
Ground
Flight

A

On the ground / take off / landing
600 LBS
Flight 1.100 LBS

26
Q

Min Fuel for GO-AROUND

A

750 LBS / each Wing

27
Q

Min Fuel for Wing to Wing transfer

A

2500 LBS / each Wing

28
Q

Fuel crossfeed …. TO & Landing
Bellow 10.000 ft dual engine ops?

A

Must be OFF for TakeOff & Landing
Must be off Bellow 10.000 ft

29
Q

OIL Temp
Min for START
Min before selecting TO power
Maxim for Cont Ops
Transient Ops

A

-40C
+43C
+160C
+160 - +165C

30
Q

Max Oil consumption

A

0.31 Q/Hour

31
Q

Operation of the oil replenish syst

A

Prohibited with OAT -12 or colder

32
Q

The Oil replenish syst must contain for take off at least

A

2.5 Q

33
Q

APU
Type

A

SPU 300

34
Q

APU
MAX RPM

A

105%

35
Q

APU
MAX EGT
Start
Normal OPS

A

1032C
718C

36
Q

APU
Max Ops altitude

A

51000 ft

37
Q

APU
Min ambient temp for start a cold soak on the ground

A

-40C

38
Q

APU
Max number of start / hour

A

3

39
Q

APU
Max starting Altitude

A

45000 ft

40
Q

APU
Bleed Air Extraction Limit
Altitude
Temp on ground

A

25000 ft
+48 C OAT

41
Q

What is the maximum speed for flap 4 extension?
A. 200KIAS
B. 185KIAS
C. 210KIAS
D. 220KIAS

A

B

42
Q

The airplane has a maximum zero fuel weight of:
A. 67,500 lb (30,617 kg).
B. 76,000 lb (34,473 kg).
C. 78,600 lb (35,655 kg).
D. 65,000 lb (29,483 kg).

A

A

43
Q

The airplane has a maximum takeoff weight of:
A. 114,950lb (52,140 kg).
B. 115,100 lb (52,209 kg).
C. 114,850lb (52,095 kg).
D. 114,650 lb (52,001 kg).

A

C

44
Q

Minimum oil temperature for starting an engine is beforetakeoff power can be applied
A. -30°C, +33°C
B. -30°C, +43°C
C. -40°C, +33°C
D. -40°C, +43°C

A

D

45
Q

Maximum speed for turbulence penetration is:
A. 265 KIAS from sea level to 8000 ft, linearly increasing to 285 KIAS at 10.000 ft
B. 285 KIAS from sea level to 8000 ft, linearly increasing to 300 KIAS at 10.000 ft.
C. 300 KIAS from sea level to 8000 ft, linearly increasing to 335 KIAS at 10,000 ft.
D. 265 KIAS from 10,000 ft and above or 0.80 Mach, whichever is lower.

A

A

46
Q

Maximum speed for gear manoeuvre is …… and to operate with gear extended is …….
A. 200, 250
B. 200,225
C. 250, 185
D. 250, 210

A

A

47
Q

The minimum ambient air temperature approved for takeoff is:
A. -45°C
B. -40°C
C. -35°C
D. -30°C

A

B

48
Q

Auxiliary pressurization (AUX PRESS) system operations are prohibited at altitudes greater than:
A. 30,000 ft.
B. 37,000f.t
C. 41,000 ft.
D. 45,000f.t

A

C

49
Q

APU bleed air extraction is limited to:
A. 45,000ft.
B. 25,000ft.
C. 51,000 f.t
D. 23,000ft.

A

B

50
Q

APU bleed air extraction on the ground for ECS operation is limited to what OAT?
A 50°C
B. 40°C
C. 43°C
D. 48°C

A

D

51
Q

Engine START inflight limitations

A

Via APU speed below 250 kts up to FL 230
CrossBLEED below 250 kts up to FL300
Windmill assist speed above 250 kts N2 greater 7.5% up to FL 300

52
Q

Flying an approach with a glide path greater than ….. degrees is prohibited

A

More then 5.5 degrees is prohibited
Between 3.5 and 4.5 could be flown with Supp. 8
Between 4.5 to 5.5 degrees with Supp 20

G7500 (30 decks)

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