F100/70 Limitations Flashcards

1
Q

Maximum operating Pressure Altitude?

A

F70/F100
35,000ft.

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2
Q

Runway slope limit?
-Auto land operation ?

A

2% up & 2% down
0.8% up & 0.8% down

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3
Q

Manoeuvring load limits
-Flaps up
-Flaps Down

A

+2.5g/-1.0g
+2.0g/-0.0g

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4
Q

Maximum Operating Temperatures
-Take-off,flight and LND with A/C operative
-On ground with avionics cooling operative and the air conditioning inoperative

A

ISA +35 degrees Celsius
44 degrees Celsius

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5
Q

Minimum runway width

A

30 m

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6
Q

Maximum zero fuel weight

A

F70 - 33565kgs
F100 - 36740kgs

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7
Q

Maximum taxi weight

A

F70- 41955kgs
F100- 44680 kgs

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8
Q

Maximum take-off weight

A

F70- 41730kgs
F100- 44450kgs

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9
Q

Maximum landing weight

A

F70- 36740kgs
F100- 39915kgs

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10
Q

Vmo/Mmo

A

320 KIAS / 0.77 M

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11
Q

Vra/Mra

A

250 KIAS / 0.65 M

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12
Q

Vfe/Mfe

A

Flap 8- 250 KIAS
Flap 15- 220 KIAS
Flap 25- 220 KIAS
Flap 42- 180 KIAS

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13
Q

Vlo/Vle
(Landing gear operation/ extension)

A

200 KIAS

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14
Q

Maximum demonstrated speed for flight with an open sliding window

A

160 KIAS

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15
Q

Normal rate of climb

A

250 KIAS / 280 KIAS / 0.7 M

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16
Q

Maximum rate of climb

A

250 KIAS / 0.65 M

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17
Q

Maximum Angle of climb

A

Green Dot

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18
Q

Maximum demonstrated crosswind component for take-off & landing

A

35kts

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19
Q

Tailwind component for take-off and landing

A

10kts

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20
Q

CAT 1 ILS approaches (precision approach) where the visibility is less than 1200m, crosswind limitation

A

30kts

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21
Q

Non-grooved. Wet runways operations , take-off & landing crosswind limitation

A

30kts

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22
Q

ILS Coupled approach crosswind limit

A

25kts

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23
Q

Maximum tail wind landing with low pressure tyres flaps 25 degrees

A

F70- 5kts
F100- N/A

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24
Q

Emergency lights

A

Duration of 10 mins

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25
Q

APU Start Cycles

A

3 consecutive starts with 2 min between starts.

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26
Q

APU shutdown

A

Allow 70 seconds before switching off the batteries, unless external AC power is available

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27
Q

APU bleed air

A

F70- Select APU bleed air OFF before shutting down engines on the bay to reduce ingestion of exhaust fumes into the cabin.
After approx 5 minutes, select APU bleed air back to ON.

F100- N/A

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28
Q

Emergency power supply

A

30 mins & 1 APU Start

29
Q

Minimum voltage for APU start

A

Battery - 24 Volts
EMERG BUS AC - 112 Volts

30
Q

Maximum Fuel Asymmetry
In flight

A

1000 kgs irrespective of Aircraft wgt.
-Landing if fuel asymmetry in excess of 350kgs max crosswind is 20kts.

31
Q

Maximum Fuel Asymmetry
On ground

A

F100
Weight above 39000kgs- 500kgs
Weight at/or below 39000kgs -1000kgs

F70
1000kgs

32
Q

Maximum Fuel Asymmetry
Fuel Asymmetry Caution

A

F100/F70
Alert will be presented if the difference between the contents of the wing tanks is more than 350kgs. (770lbs)
The alert will disappear when the difference in wing tank contents is reduced to below approx 250kgs. (600 lbs).
F70/F100
If fuel asymmetry in excess of 350kgs max crosswind 20kts.

33
Q

Maximum TGT for start

A

F70- 700 for 2 seconds
F100- 740 for 2 seconds

34
Q

Maximum TGT during relight

A

F70- 780 for 2 seconds
F100- 780 for 2 seconds

35
Q

Maximum TGT for take-off

A

F70- 800 for 5 mins
F100- 850 for 5 mins

In the event of an engine failure, the remaining engine may be operated at take-off thrust for a maximum total period of 10 mins.

36
Q

Maximum continuous TGT

A

F70- 735
F100- 795

37
Q

Maximum over temperature TGT

A

F70- 820 for 20 seconds

F100- 870 for 20 seconds

38
Q

Maximum TGT reverse thrust

A

F100- 850 degrees. 60 seconds
F70. - 800 degrees. 60 seconds
Stabilised operation in range of 57% to 75% N1 is not permitted in reverse thrust.
Passing through this range while increasing or decreasing thrust is allowed.

39
Q

N2 low idling

A

47.9%
This is the minimum below which N2 should not fall.

40
Q

Engine start bleed pressure

A

APU- 25 PSI to 35 PSI (can be as low as 20 PSI up to 8000ft)
Cross Bleed- 30 PSI
External Air - 30 PSI to 50 PSI

41
Q

Engine warm up time

A

Oil temp 40 or above - 2 mins
Oil temp 20 - 40 - 3 mins
Oil temp 20 & below - 4 mins

42
Q

Minimum engine oil pressure for take-off

A

30 PSI

43
Q

Time Recq at idle thrust before shutdown

A

1 min (Engine oil returns after 15 mins)

44
Q

Engine start cycle

A

4 attempts, 2 mins max, 30 seconds off.
15 mins off after 4th attempt.

45
Q

Maximum oil consumption

A

1.5 L / HR

46
Q

Window heat failure

A

300 KIAS below 10000 FT

47
Q

Minimum temp take-off with ATS engaged

A

-54 degrees Celsius

48
Q

Minimum in flight ATS engaged

A

-70 degrees Celsius

49
Q

Maximum lift dumper Extension Speed

A

170 kts

50
Q

Maximum take-off - N1 N2

A

N1 N2
F100 95.5 103.5
F70 96.5 103.5

51
Q

Max Cont. N1. N2.

A

N1. N2.
F100. 95.5. 100.5
F70. 96.5. 100.5

52
Q

Max Overspeed. N1. N2.

A

N1. N2.
F100. 98.3. 100.6.
F70. 99.4. 106.6

53
Q

Emergency maximum reverse thrust
N1. N2.

A

N1. N2.
F100. 95.5. 99.2.
F70. 96.5. 100.

54
Q

Min oil temp for starting

A

F100 & F70 -50 degrees Celsius

55
Q

Min oil temp before increasing power

A

F100 & F70 -30 degrees Celsius

56
Q

Maximum oil temperature
(Unrestricted)

A

F100 & F70 + 105 degrees Celsius

57
Q

Maximum transient oil temperature
(15 minutes)

A

F100 & F70 +120 degrees Celsius

58
Q

Max fuel temperature
(Unrestricted)

A

F100 +95 degrees Celsius
F70 +90 degrees Celsius

59
Q

Max fuel temperature transient
(15 minutes)

A

F100. +130 degrees Celsius
F70. +120 degrees Celsius

60
Q

Minimum AP Engage T/O

A

F100/F70
Minimum. - 35ft
MFDS alert no A/P below 500ft - 500ft

61
Q

Minimum A/P engage cruise

A

F100/F70
700ft

62
Q

A/P Minimum use height for non precision approaches

A

F100/F70
250ft

63
Q

A/P minimum use height Precision Approach (ILS GS/LOC)

A

F100/F70
80ft

64
Q

Normal Operating Max Cabin Dif Pressure

A

7.46 PSI

65
Q

What is the Diff Pressure limited by the outflow valves?

A

In both Auto or Manual 7.65 PSI

66
Q

Minimum quantity in each Hydraulic System

A

F70/F100. 70%.

67
Q

Maximum APU electrical load

A

SL- 100%
15000ft - 100%
25000ft - 65%
35000ft - 30%

68
Q

Maximum altitude start R APU

A

FL310
(If cold soaked not guaranteed above FL250)

69
Q

Maximum altitude RR APU start

A

FL350