Limitations Flashcards

1
Q

Flight maneuvering and Load Acceleration limits:

Other configurations

A

0g to 2g

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2
Q

Operational parameters:

Runway slope

A

+/- 2%

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3
Q

Operational parameters:

Runway altitude

A

9200 ft

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4
Q

Operational parameters:

Nominal Runway width

A

45m

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5
Q

Operational parameters:

Minimal Runway width

A

30m

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6
Q

Max Crosswind:

Takeoff

A

35 kt

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7
Q

Max Crosswind:

Landing

A

38 kt

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8
Q

Maximum certified tailwind:

Take off and landing

A

15 kt

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9
Q

Maximum wind for passenger door operation

A

65 kt

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10
Q

Maximum wind FWD and AFT cargo door

A

40 kt (50 kt nose into wind)

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11
Q

Speeds

Maximum flaps/slats speeds

1

A

230 kt

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12
Q

Speeds

Maximum flaps/slats speeds

1 + F

A

215 kt

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13
Q

Speeds

Maximum flaps/slats speeds

2

A

200 kt

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14
Q

Speeds

Maximum flaps/slats speeds

3

A

185 kt

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15
Q

Speeds

Maximum flaps/slats speeds

FULL

A

177 kt

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16
Q

Speeds

Cockpit window open M

A

200 kt

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17
Q

Speeds

VMO

A

350 kt

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18
Q

Speeds

MMO

A

0.82 M

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19
Q

Speeds

Maximum speed with L/G extended

A

280 kt/0.67 M

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20
Q

Speeds

Maximum speed for L/G extension

A

250 kt/0.60 M

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21
Q

Speeds

Maximum speed for L/G retraction

A

220 kt/0.54 M

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22
Q

Speeds

Maximum tire speed

A

195 kt (Ground speed)

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23
Q

Speeds

Wipers maximum speed

A

230 kt

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24
Q

Speeds

Minimum control speed for landing (VMCL)

A

116 kt
(See FCOM p. 2227 for VMCA & VMCG)

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25
***Cabin Pressure*** Maximum ***positive*** differential pressure
9.0 PSI
26
***Weight limitations*** Maximum taxi weight
77.400 kg
27
***Weight limitations*** Maximum takeoff weight (brakes release)
77.000 kg
28
***Weight limitations*** Maximum landing weight
67.400 kg
29
***Weight limitations*** Maximum zero fuel weight
64.300 kg
30
***Weight limitations*** Minimum weight
40.600 kg
31
***Cabin Pressure*** Maximum ***negative*** differential pressure
-1.0 PSI
32
***Cabin Pressure*** Safety relief valve setting
8.6 PSI
33
***Auto Flight System*** ***Minimum AGL for autopilot use:*** At take off
100 ft and at least 5s after lift off
34
***Auto Flight System*** ***Minimum AGL for autopilot use:*** In APCH with FINAL APP, V/S, or FPA
250 ft
35
***Auto Flight System*** ***Minimum AGL for autopilot use:*** In circling
500 ft
36
***Auto Flight System*** ***Minimum AGL for autopilot use:*** ILS when CAT I is displayed on the FMA
160 ft
37
***Auto Flight System*** ***Minimum AGL for autopilot use:*** ILS when CAT2 or CAT3 SINGLE or DUAL displayed on the FMA
0 ft if autoland
38
***Auto Flight System*** ***Minimum AGL for autopilot use:*** After manual go-around
100 ft
39
***Auto Flight System*** ***Minimum AGL for autopilot use:*** All other phases
500 ft
40
***Auto Flight System*** ***Minimum AGL for autopilot use:*** ILS CAT2 manual landing
80 ft
41
***Auto Flight System*** ***Minimum AGL for autopilot use:*** CAT II and CAT III fail passive autoland
approved in CONF 3 or FULL
42
***Auto Flight System*** ***Minimum AGL for autopilot use:*** Maximum wind for ILS CAT II or CAT III Headwind
30 kt
43
***Auto Flight System*** ***Minimum AGL for autopilot use:*** Maximum wind for ILS CAT II or CAT III Tailwind
10 kt
44
***Auto Flight System*** ***Minimum AGL for autopilot use:*** Maximum wind for ILS CAT II or CAT III Crosswind
20 kt (15 for automatic rollout with OEI)
45
***Automatic Landing*** ILS CAT I, CAT II, CAT III autoland
approved in CONF 3 or FULL
46
***Automatic Landing*** Glide slope angle
-2.5° to 3.25°
47
***APU*** After 3 start attempts
60 min before next attempt
48
***APU*** Maximum EGT for start (below 35.000ft)
1090°C
49
***APU*** Maximum EGT for start (above 35.000ft)
1120°C
50
***APU*** APU running (Max temp)
675°C
51
***APU*** APU start or shutdown is permitted during refueling/defueling (see conditions in FCOM)
***APU*** APU start or shutdown is permitted during refueling/defueling (see conditions in FCOM)
52
***APU*** Operation (elec. power) and normal restart limit
41.000 ft
53
***APU*** Battery start limit altitude
25.000ft
54
***Maximum altitude:*** Assist engine start
20.000 ft
55
***Maximum altitude:*** Air conditioning and pressurization (single pack)
22.500 ft
56
***Maximum altitude:*** Air conditioning and pressurization (dual pack)
15.000 ft
57
***Maximum altitude:*** APU bleed air for wing anti-ice is not permitted
***Maximum altitude:*** APU bleed air for wing anti-ice is not permitted
58
***Engines (CFM LEAP-1A26)*** *Thrust Setting/EGT Limits* Takeoff(1) and Go-around *(normal)* ## Footnote (1) = Incl. TOGA, FLEX, and DERATE (if installed) thrust modes
Time limit: 5 min EGT limit: 1060°C
59
***Engines (CFM LEAP-1A26)*** *Thrust Setting/EGT Limits* Takeoff(1) and Go-around **(One engine out)** ## Footnote (1) = Incl. TOGA, FLEX, and DERATE (if installed) thrust modes
Time limit: **10 min** EGT limit: **1060°C**
60
***Engines (CFM LEAP-1A26)*** *Thrust Setting/EGT Limits* MCT
Time limit: **No limit** EGT limit: **1025°C**
61
***Engines (CFM LEAP-1A26)*** *Thrust Setting/EGT Limits* Starting (on ground)
Time limit: - EGT limit: **750°C**
62
***Engines (CFM LEAP-1A26)*** *Thrust Setting/EGT Limits* Starting (In flight)
Time limit: - EGT limit: **875°C**
63
***Engines (CFM LEAP-1A26)*** *OIL* Maximum continuous temperature
140°C
64
***Engines (CFM LEAP-1A26)*** *OIL* Maximum transient temperature
15 min / 155°C
65
***Engines (CFM LEAP-1A26)*** *OIL* Minimum starting temperature
-40°C
66
***Engines (CFM LEAP-1A26)*** *OIL* Minimum temperature before take off
19°C
67
***Engines (CFM LEAP-1A26)*** *OIL* Minimum oil quantity
***highest of:*** *10.6 qt* **Or** *8.9 qt + est. consumption* *(max. 0.45 qt/hr)*
68
***Engines (CFM LEAP-1A26)*** *OIL* Minimum oil pressure
17.4 PSI
69
***Starter*** Ground starts
**60s pause required between succesive cycles** **(Cycle = max. 3 automatic start attemps)** ## Footnote *after three failed cycles 15 min cooling period required*
70
GA SOFT mode is prohibited with OEI
GA SOFT mode is prohibited with OEI
71
***Flight controls*** Max. altitude with slats and/or flaps extended
20.000 ft
72
***Fuel*** JET A1 min. temperature
-43°C
73
***Fuel*** Maximum temperature
(+55°C)
74
***Fuel*** Minimum fuel quantity for take off
1500 kg
75
***Landing gear*** Maximum brake temperature for take off *(Brake fans off)*
300°C
76
***Landing gear*** Maximum brake temperature for take off *(Brake fans on)*
150°C
77
***Temperatures*** Maximum lowest temperature for operation
-70°C at 39.800 ft
78
***Icing conditions*** Temperature on ground or after takeoff?
at or below **10°C** + **Visible moistre** ## Footnote Visible moisture forms: - clouds - fog with vis. 1600m or less - rain - snow - sleet - ice crystals + when operating on twy/rwy with **wet** surface + **temp ≤10°C**