LIMITATIONS Flashcards

1
Q

Flight maneuvering / load acceleration Limits

A

Clean = -1g to +2.5g

Other config = 0g to +2g

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2
Q

Airport operation

A

RWY slope = +/- 2%
RWY altitude = 14100ft
Nominal RWY width = 45m
Minimum RWY width = 30m

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3
Q

Maximum crosswind for T/O and LDG

A

XWIND T/O = 35kt gust included (NEO)
= 38kt gust included (CEO)

XWIND LDG = 38kt

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4
Q

Maximum tailwind for T/O and LDG

A

15kt

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5
Q

Passenger and cargo door operations :

A

PAX door operation = 65kt

FWD & AFT cargo doors = 40kt (50kt if A/C nose into wind or door on leeward side)

FWD & AFT cargo doors must be closed by 65kt

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6
Q

Cockpit window open maximum speed

A

200kt

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7
Q

Maximum flaps & slats speeds

A
CONF 0 = Vmo 350kt / Mmo 0.82
CONF 1 = 230kt
CONF 1+F = 215kt
CONF 2 = 200kt
CONF 3 = 185kt
CONF FULL = 177kt
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8
Q

Maximum operating speed :

A
Vmo = 350kt
Mmo = 0.82
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9
Q

Maximum tire speed

A

195kt

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10
Q

Weight limitations

A
A319 = 61 tonnes
A320 = 64,5 or 66 tonnes
A321 = 77,3 tonnes
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11
Q

Maximum taxi speed

A

A320 CEO TOW > 76T = 20kt

Straight line = 30kt
90* turn = 10kt
<90* turn = as required
RET = as defined by aerodrome

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12
Q

Maximum tire deflated speed

A

1 tire deflated/gear = 7kt
2 tires deflated/gear = 3kt

Max NWS angle = 30*

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13
Q

Maximum wipers operating speed

A

230kt

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14
Q

Avionics ventilation

A

OAT less than 49*c = no limits

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15
Q

Cabin pressure

A

Max deltaP = 9 psi
Max -deltaP = -1 psi

Safety relief valve setting = 8.6 psi

Minimum cabin altitude selection = -2000ft
Maximum cabin altitude selection = 14000ft

Maximum normal cabin altitude = 8000ft

Cabin altitude warning = 9550ft (+/- 350ft)

Outflow valve closure = 15000ft

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16
Q

A/P function

A

T/O = 100ft AGL and at least 5sec after liftoff

FINAL APP / V/S / FPA / PAR = 250ft AGL

Circling approach = 500ft AGL (cat C)

CAT 1 ILS = 160ft AGL

CAT 2/3 ILS = 0ft AGL if autoland

all other phases = 500ft AGL (909ft AGL A321)

17
Q

Non precision approach with OEI

A

A319 not allowed to use A/P to perform NPA in :

  • FINAL APP
  • NAV V/S
  • NAV FPA

Only FD use is permitted

18
Q

Precision approach

A

ILS CAT 1 : 550m MDA 200ft - any lights

ILS CAT 2 : 300m DH 100ft RA - 3 consecutive lights + 1 lateral element

ILS CAT 3A : 200m DH 50ft RA - 3 consecutive lights

ILS CAT 3B : 75m NO DH (none or 1 light for CAT 3B with DH)

19
Q

AUTOLAND Engine Out

A

A320 CEO = CONF FULL only

A319-A320NEO- A321 = CONF FULL or CONF 3

20
Q

Autoland limits (GPA and airport elev)

A

ILS CAT 2/3 = CONF 3 and CONF FULL

A319-A320CEO = -2.5 to -3.15 GPA
NEO = -2.5 to -3.25 GPA

AirPort elevation less than 9200ft (2500ft for A320 CEO)

21
Q

APU

A

APU start : max 3 consecutive start attempts then 60min cooling period

APU max rotor speed = 107%

APU EGT :
max running 675
Max start below FL350 = 1090
Max start above FL350 = 1120

APU dual pack operation = FL150
APU assisting engine start = FL200
APU single pack operation = FL225
APU start on batteries = FL250

22
Q

TOGA LIMIT / ENGINE EGT

A

TOGA max 5min 2 engines / 10min OEI
MAX EGT = 750 for airborne start
915 for MCT
950 for TOGA

23
Q

Engine shaft speed

A

Max N1 = 104%
Max N2 = 105%
Max N1 APU = 107%

24
Q

Oil

A

Max continuous temp = 140
Max transient = 155
Min temp for start = -40
Mon temp for T/O = -10 / 19 NEO

Nominal oil pressure 13 to 90 psi

25
Oil quantity
9. 5 QT + 0,5/flight hour CEO | 10. 6 or 8.9 + 0.45/flight hour NEO
26
Starter
Standard automatic start including up to 3 start attempts = 1 cycle Must respect 20sec pause between cycles (60sec NEO) 15 min cooling period must be respected after 4 failed cycles (3 for NEO) DO NOT RUN STARTER WITH N2>20% (63% NEO)
27
Reverse thrust
Do not select reverse in flight Backing the A/C with reverse is forbidden MAX REV shall be used down to 70kt max IDLE REV can be used down to stop
28
Flex takeoff
Not permitted on contaminated RWY TFLEX cannot be higher than : - TMAX FLEX ISA +60 (a319) - TMAX FLEX ISA+55 (a320) - TMAX FLEX ISA +52 (NEO) TLFEX cannot be higher than TREF : - a319 = ISA+30 - a320 = ISA+29 - a321 = ISA+15 TFEX cannot be lower than OAT
29
Crosswind operation on ground NEO
Max crosswind for engine start = 45kt | Max engine crosswind TO = 35kt gust included
30
SOFT G/A NEO
Do not use SOFT GA when OEI
31
Max altitude slat/flap extended
FL200
32
Fuel temperature
``` Mini = - 43 Maxi = 54 ```
33
Minimum fuel quantity for takeoff
1500kg
34
FO operating limitations
- Max crosswind = 20kt - No planned tailwind landing for*** FO - No flap 3 landing for *** FO - TAKEOFF RVR = 400m minimum - Approach minim : CAT 1 for ILS, published minima for NPA, 5000m of vis for visual approach - minimum runway width = 45m - no contaminated or slippery runway conditions - no reported windshear - no autoland for normal operations