Limitations Flashcards

(58 cards)

1
Q

Kind of operations

A

‐ VFR and IFR ‐
Extended overwater flight ‐
Flight in icing conditions

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2
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

A

Clean configuration –1 g to +2.5 g

Other configurations 0 g to +2 g

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3
Q

WEIGHT LIMITATIONS

A4O-DA, A4O-DC, A4O-DF, A4O-DG

A
Max taxi weight. 233900kg
Max takeoff weight. 233000kg
Max landing weight. 182000kg
Max zero fuel weight  170000kg
Min weight 116000kg
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4
Q

Weight limitations

A4O-DB, A4O-DD, A4O-DE

A
Max taxi weight. 233900
Max takeoff weight. 233000kg
Max landing weight. 187000kg
Max zero fuel weight  175000kg
Min weight 121000kg
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5
Q

Weight limitations

A4O-DH, A4O-DI, A4O-DJ

A
Max taxi weight. 235900
Max takeoff weight. 235000kg
Max landing weight. 187000kg
Max zero fuel weight  173000kg
Min weight 121000kg
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6
Q

Runway slope

A

+-2%

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7
Q

Runway altitude

A

12500ft

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8
Q

Max certified crosswind for takeoff

A

32kt (gust included)

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9
Q

Max tailwind takeoff

A4O-DA, A4O-DB, A4O-DC, A4O-DD, A4O-DE, A4O-DF, A4O-DG

A

10kts

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10
Q

Autopilot minimum engagement height

A

100 ft AGL or 5 s after liftoff.

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11
Q

In approach using F-LOC , F-G/S

A

200ft AGL

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12
Q

Autopilot cat 1

A

160fr AGL

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13
Q

Autopilot GLS

A

160ft AGL

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14
Q

Autopilot after a go around

A

100ft

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15
Q

Maximum wind for auto land cat II and III

A

Headwind: 35 kt Tailwind : 10 kt Crosswind: 20 kt

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16
Q

Auto land glide slope

A

-2.5 ° and -3.25 °

For airfield elevation below 9200ft

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17
Q

Weight limitations autoland

A
  • For weights below maximum landing weight

- For weights above 116 000 kg (255 737 lb)

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18
Q

Nominal Runway Width

A

45 m

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19
Q

Max tailwind takeoff

A4O-DH, A4O-DI, A4O-DJ

A

15kts

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20
Q

Max crosswind for landing

A4O-DA, A4O-DC, A4O-DF, A4O-DG

A

45kts

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21
Q

Max crosswind for landing

A4O-DB, A4O-DD, A4O-DE, A4O-DH, A4O-DI, A4O-DJ

A

40kts

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22
Q

Max tailwind landing

A

10kts

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23
Q

The maximum wind for passenger door operation

A

40 kt or 50 kt if the aircraft nose is into the wind

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24
Q

Takeoff is not recommended on the following runway conditions

A

‐ Wet ice,
‐ Water on top of Compacted Snow,
‐ Dry Snow or Wet Snow over Ice.

25
COCKPIT WINDOW OPEN MAXIMUM SPEED
230 kt
26
Max VMO/MMO
330kts/ m0.86
27
Maximum speed with landing gear extended (VLE
250 kt/0.55
28
Maximum speed with the landing gear operating - extension and retraction (VLO)
250 kt/0.55
29
Maximum ground speed tire speed
204kts
30
WIPERS MAXIMUM OPERATING SPEED
230 kt
31
Maximum positive differential pressure
9.25 PSI
32
Maximum negative differential pressure
.-0.73 PSI
33
Safety relief valve setting
8.85 PSI
34
APU start attempts
After three consecutive APU start attempts, the flight crew must wait 60 min before a new start attempt.
35
APU max rotor speed
107 %
36
Maximum EGT for APU start
1 250 °C
37
Maximum EGT for APU running
650 °C
38
APU bleed air and elec power
25000ft
39
APU elec power only
41450 ft
40
When JET B or JP4 is used, APU operation is limited to
25 000 ft
41
Maximum N1 Maximum N2 Maximum N3
99 % 103.3 % 100 %
42
OIL TEMPERATURE Maximum continuous temperature
190 °C
43
Minimum oil temperature before takeoff
20 °C
44
Minimum oil pressure
25 PSI
45
STARTER
‐ Starter maximum continuous operation is 5 min . ‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle. ‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.
46
REVERSE THRUST
Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop.
47
Maximum operating altitude with slats and/or flaps extended
20 000 ft
48
Minimum fuel quantity for takeof
5 200 kg
49
Maximum brake temperature for takeoff (brake fans off)
300 °C
50
If maximum one tire per gear is deflated (consider three gears) Maximum taxi speed during turn
7kts
51
If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed
3 kt
52
For the nosewheel steering (NWS) angle Maximum NWS angle
30 °
53
APU bleed and elec
22500ft
54
APU battery restart limit
25000ft
55
APU ground operation
14600ft
56
APU normal start
41450ft
57
Max fuel temp
55 degrees for jet a1
58
Starter
‐ Starter maximum continuous operation is 5 min . ‐ Two 3 min duty cycles and a consecutive 1 min cycle is permitted with run down to zero N3 between each cycle. ‐ After one continuous operation, or the three cycles wait 30 min to allow the starter to cool. ‐ No running engagement of the starter when the N3 is above 10 % on ground, or 30 % in flight.