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Limitations > F100/70 Limitations > Flashcards

F100/70 Limitations Flashcards

(69 cards)

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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
APU Start Cycles
3 consecutive starts with 2 min between starts.
26
APU shutdown
Allow 70 seconds before switching off the batteries, unless external AC power is available
27
APU bleed air
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
28
Emergency power supply
30 mins & 1 APU Start
29
Minimum voltage for APU start
Battery - 24 Volts EMERG BUS AC - 112 Volts
30
Maximum Fuel Asymmetry In flight
1000 kgs irrespective of Aircraft wgt. -Landing if fuel asymmetry in excess of 350kgs max crosswind is 20kts.
31
Maximum Fuel Asymmetry On ground
F100 Weight above 39000kgs- 500kgs Weight at/or below 39000kgs -1000kgs F70 1000kgs
32
Maximum Fuel Asymmetry Fuel Asymmetry Caution
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
Maximum TGT for start
F70- 700 for 2 seconds F100- 740 for 2 seconds
34
Maximum TGT during relight
F70- 780 for 2 seconds F100- 780 for 2 seconds
35
Maximum TGT for take-off
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
Maximum continuous TGT
F70- 735 F100- 795
37
Maximum over temperature TGT
F70- 820 for 20 seconds F100- 870 for 20 seconds
38
Maximum TGT reverse thrust
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
N2 low idling
47.9% This is the minimum below which N2 should not fall.
40
Engine start bleed pressure
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
Engine warm up time
Oil temp 40 or above - 2 mins Oil temp 20 - 40 - 3 mins Oil temp 20 & below - 4 mins
42
Minimum engine oil pressure for take-off
30 PSI
43
Time Recq at idle thrust before shutdown
1 min (Engine oil returns after 15 mins)
44
Engine start cycle
4 attempts, 2 mins max, 30 seconds off. 15 mins off after 4th attempt.
45
Maximum oil consumption
1.5 L / HR
46
Window heat failure
300 KIAS below 10000 FT
47
Minimum temp take-off with ATS engaged
-54 degrees Celsius
48
Minimum in flight ATS engaged
-70 degrees Celsius
49
Maximum lift dumper Extension Speed
170 kts
50
Maximum take-off - N1 N2
N1 N2 F100 95.5 103.5 F70 96.5 103.5
51
Max Cont. N1. N2.
N1. N2. F100. 95.5. 100.5 F70. 96.5. 100.5
52
Max Overspeed. N1. N2.
N1. N2. F100. 98.3. 100.6. F70. 99.4. 106.6
53
Emergency maximum reverse thrust N1. N2.
N1. N2. F100. 95.5. 99.2. F70. 96.5. 100.
54
Min oil temp for starting
F100 & F70 -50 degrees Celsius
55
Min oil temp before increasing power
F100 & F70 -30 degrees Celsius
56
Maximum oil temperature (Unrestricted)
F100 & F70 + 105 degrees Celsius
57
Maximum transient oil temperature (15 minutes)
F100 & F70 +120 degrees Celsius
58
Max fuel temperature (Unrestricted)
F100 +95 degrees Celsius F70 +90 degrees Celsius
59
Max fuel temperature transient (15 minutes)
F100. +130 degrees Celsius F70. +120 degrees Celsius
60
Minimum AP Engage T/O
F100/F70 Minimum. - 35ft MFDS alert no A/P below 500ft - 500ft
61
Minimum A/P engage cruise
F100/F70 700ft
62
A/P Minimum use height for non precision approaches
F100/F70 250ft
63
A/P minimum use height Precision Approach (ILS GS/LOC)
F100/F70 80ft
64
Normal Operating Max Cabin Dif Pressure
7.46 PSI
65
What is the Diff Pressure limited by the outflow valves?
In both Auto or Manual 7.65 PSI
66
Minimum quantity in each Hydraulic System
F70/F100. 70%.
67
Maximum APU electrical load
SL- 100% 15000ft - 100% 25000ft - 65% 35000ft - 30%
68
Maximum altitude start R APU
FL310 (If cold soaked not guaranteed above FL250)
69
Maximum altitude RR APU start
FL350

Limitations (1 decks)

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