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A319/320 Limitations > A319/320 Limitations > Flashcards

A319/320 Limitations Flashcards

0
Q

WEIGHT LIMITATIONS
A319/A319IGW

Maximum Takeoff Weight
(brake release)
(lb)

A

154,320/166,440

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1
Q

WEIGHT LIMITATIONS
A319/A319 IGW

Maximum Taxi Weight (lb)

A

155,200/167,320

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2
Q

WEIGHT LIMITATIONS
A319/A319IGW

Maximum Landing Weight
(lb)

A

134,480/137,780

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3
Q

WEIGHT LIMITATIONS
A319/A319IGW

Maximum Zero Fuel Weight
(lb)

A

125,660/128,960

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4
Q

WEIGHT LIMITATIONS
A320/A320IGW

Maximum Taxi Weight
(lb)

A

170,630/170,630

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5
Q

WEIGHT LIMITATIONS
A320/A320IGW

Maximum Takeoff Weight
(brake release)
(lb)

A

169,750/169,750

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6
Q

WEIGHT LIMITATIONS
A320/A320IGW

Maximum Landing Weight
(lb)

A

142,190/145,500

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7
Q

WEIGHT LIMITATIONS
A320/A320IGW

Maximum Zero Fuel Weight
(lb)

A

134,480/137,780

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8
Q

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

Clean configuration

Slats and/or flaps extended

A
  • 1 g to + 2.5 g

0 g to + 2 g

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9
Q

AIRPORT OPERATIONS

Runway Slope (mean)
Min Runway Width
Runway Altitude

A

+/- 2%
100ft/30m
9200 ft

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10
Q

Max Crosswind FOR TAKEOFF AND LANDING

A

319/320/321

Maximum Crosswind …………………….T.O.35kts/LNDG 38kts

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11
Q

CONTAMINATED RUNWAY

Maximum
crosswind (kt)

Takeoff/Landing

A 
Good-35/38
Good to Medium-29/29
Medium-25
Medium to Poor-20
Poor-15
Nil-Not Authorized
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12
Q

NARROW RUNWAYS

A

NOTES:
– A normal runway is any runway at least 150 ft/45m wide.
– A narrow runway is any runway less than 150 ft/45m wide.

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13
Q

NARROW RUNWAYS

Maximum demonstrated cross wind for takeoff and landing:

A

– Dry runway . . . . . . . . . . . . . . . . . . . . . . . . . . . 38 kt (gust included)
– Wet runway . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 kt (gust included)
– Contaminated runway . . . . . . . . . . . . . . . . . . .10 kt (gust included)

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14
Q

WIND FOR PASSENGER/CARGO DOOR

OPERATION

A

Maximum wind for passenger door operation . . . . . . . . . . . . . . . 65 kt
Maximum wind for cargo door operation . . . . . . . . . . . . . .40 kt/*50 kt
* If the aircraft nose is oriented into the wind, or if the cargo door is on the leeward side of the aircraft, operation of the cargo door is permitted in winds up to 50 knots. If wind speed begins to exceed these limitations, the cargo door must be closed before the wind speed exceeds 65 kts.

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15
Q

SPEED LIMITATIONS

Maximum VMO/MMO

A

350 kt/.82 mach

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16
Q

SPEED LIMITATION

SEVERE TURBULENT AIR PENETRATION
SPEED

A

FL200 and below. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .250 kt
Above FL200 through FL310 . . . . . . . . . . . . . . . . . . . . . . . . . .275 kt
Above FL310 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .0.76 mach

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17
Q

MAXIMUM FLAPS/SLATS SPEEDS A-320

1/1+F/2/3/4

A

230/215/200/185/177

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18
Q

GEAR DOWN SPEEDS

VLE

A

280kt 0.67M

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19
Q

GEAR DOWN SPEEDS

VLO

A

Extension-250kt

Retraction-220kt

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20
Q

Maximum altitude at which the landing gear may be extended

A

25,000 ft

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21
Q

MAXIMUM TIRE SPEEDS

A

195 kt

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22
Q

Maximum speed for use of windshield wipers

A

230 kt

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23
Q

Maximum speed for opening cockpit window

A

200 kt

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24
Q

TAXI SPEED (A320/321)

A

When the taxi weight is higher than 167,550 lbs do not exceed a taxi speed of 20 kt during a turn.

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25
Q

Max operating altitude with slats and/or flaps extended

A

20,000 feet

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26
Q

CABIN PRESSURE LIMITATIONS

A

Maximum positive differential pressure . . . . . . . . . . . . . . . . . . . .9.0 psi
Maximum negative differential pressure . . . . . . . . . . . . . . . . . . . .- 1 psi
Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8.6 psi

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27
Q

APU

The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within the next:

A

10 hours of APU operation

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28
Q

APU

Starter Duty Limits

A

After three starter motor duty cycles, each separated by a one minute cool down, wait 60 minutes before attempting three more cycles

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29
Q

APU

Maximum N

A

107%

NOTE: The APU automatically shuts down at 107% N speed (ECAM display).

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30
Q

APU

Maximum EGT

A

675C

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31
Q

APU

Maximum EGT for start (below 35,000 feet)

A

1090C

32
Q

APU

Maximum EGT for start (above 35,000 feet)

A

1120C

33
Q

Maximum altitude for APU electrical and start

A

39,000ft

34
Q

Maximum altitude for APU battery start

A

25,000ft

35
Q

Maximum altitude for APU pneumatics (1 pack w/electrical)

A

22,500ft

36
Q

Maximum altitude for APU assisted engine start

A

20,000ft

37
Q

Maximum altitude for APU pneumatics (2 packs w/electrical)

A

15,000ft

38
Q

AUTO FLIGHT

After Takeoff/Go-Around (If SRS is indicated)

A

100ft AGL

39
Q

AUTO FLIGHT

Enroute

A

900ft AGL

40
Q

AUTO FLIGHT

Non-Precision Approaches

A

DA/DDA

41
Q

AUTO FLIGHT

Non-Autoland ILS Approach with CAT 1 displayed on FMA

A

160ft AGL

42
Q

AUTO FLIGHT

Non-Autoland ILS Approach with CAT 2/3 displayed on FMA

A

80ft AGL

43
Q

AUTO FLIGHT

Autoland ILS Approach (one or two autopilots)

A

Rollout/Taxi Speed

44
Q

AUTO FLIGHT

Autoland with braking action less than fair?

A

Prohibited

45
Q

AUTOLAND WIND RESTRICTIONS

A

– 30 knots of headwind
– 15 knots of crosswind
– 10 knots of tailwind

46
Q

ENGINES

THRUST SETTING/EGT LIMITS.

TAKEOFF and GO-AROUND

A 
5 min (950C) (NEO 1060C)
10 min-Only in event of an engine failure
47
Q

ENGINES

THRUST SETTING/EGT LIMITS

MCT

A

Unlimited (915C)

48
Q

ENGINES

THRUST SETTING/EGT LIMITS

STARTING

A

725C

49
Q

OIL

Maximum continuous oil temperature

A

140C

50
Q

OIL

Maximum transient oil temperature (15 minutes)

A

155C

51
Q

OIL

Minimum starting oil temperature

A

-40C

52
Q

OIL

Minimum oil temperature for takeoff

A

19C

53
Q

OIL

Minimum oil quantity

A

11 quarts plus .5 quarts per hour of estimated flight time

54
Q

ENGINES

Maximum N1

A

104%

NOTE: The N1 limit depends upon ambient conditions and engine air bleed configuration. These may limit N1 to a value lower than the one noted above.

55
Q

ENGINES

Maximum N2

A

105%

56
Q

ENGINES

STARTER

A

– Four consecutive cycles, each of two minutes duration, maximum.
– 20 seconds between cycles to allow for starter relubrication.
– After four cycles, 15 minutes to allow starter to cool before attempting a new start or motoring.
– Do not engage the starter when the N2 is above 20%.

57
Q

REVERSE THRUST

A

– Selecting reverse thrust in flight is prohibited.
– Backing the aircraft with reverse thrust is not permitted.
– Maximum reverse should not be used below 70 knots (Idle reverse is allowed down to aircraft stop).
– Except in an emergency, reverse thrust is not authorized to reduce taxi speed.

58
Q

REDUCED THRUST TAKEOFF

A

– Takeoff at reduced thrust is permissible, only if the airplane meets all applicable performance requirements at the planned takeoff weight, with the operating engines at the thrust available for the assumed temperature.
– Thrust reduction must not exceed 25% of the full rated takeoff thrust. To meet this requirement, the flexible temperature (T MAX FLEX) must not be higher than ISA + 60° C for A319 and ISA + 53° C for A320. +43 for A321
– The assumed temperature must not be lower than the flat rating temperature or the actual OAT.
– Takeoff at reduced thrust is allowed with any inoperative item affecting the performance, only if the associated performance shortfall has been applied to meet all performance requirements at the takeoff weight, with the operating engines at the thrust available for the flex temperature.
– Takeoff at reduced thrust is prohibited:
• on slippery or contaminated runways;
• when reported or known windshear is present, including predictive windshearindications or a windshear alert for the departure runway;
• when a Special Departure Procedure specifies full thrust for takeoff.

59
Q

FUEL

FUEL TEMPERATURE LIMITS

A

JetA1: -43C to 54C
JetA: -36C(1) to 54C

(1) For JET A only, if TAT reaches - 34C, monitor on ECAM FUEL page that fuel temperature remains higher than - 36C.

60
Q

FUEL

APPROXIMATE USABLE
FUEL WEIGHT AND VOLUME

A

Total Pounds=41,285 or 41,893

61
Q

FUEL

MINIMUM FUEL FOR TAKEOFF

A

The minimum fuel quantity for takeoff is 3300 lbs. The WING TK LO LVL warning must not be displayed on ECAM.

62
Q

FUEL

MAXIMUM ALLOWED WING FUEL IMBALANCE

 Inner tanks – Outer tanks balanced:

A

Full 3305 lbs / 1102* lbs
9480 lbs / 6613* lbs 3520 lbs / 2310* lbs
4960 lbs / 3196* lbs 4960 lbs / 3195* lbs

*Takeoff imbalance limitations for Sharklet-equipped aircraft only (e.g., A/C 220, 227). All other imbalance limitations remain the same.

63
Q

FUEL

MAXIMUM ALLOWED WING FUEL IMBALANCE

 Outer tanks:

A

Maximum allowed imbalance 1520 lbs / 815* lbs

*Takeoff imbalance limitation for Sharklet-equipped aircraft only (e.g., A/C 220, 227). All other imbalance limitations remain the same.

64
Q

FUEL MANAGEMENT

A

Center tank must be emptied first, followed by the wing tanks.

Takeoff on center tank is prohibited. Engines 1 and 2 must be completely segregated for take-off (i.e., crossfeed valve closed).

65
Q

HYDRAULIC

MAX hydraulic pressure

A

3200 psi

66
Q

BRAKES

Maximum brake temperature for takeoff

A

300C

67
Q

TAXI WITH DEFLATED TIRES

A

If tire damage is suspected after landing or after a rejected takeoff, an inspection of the tires is required before taxi. If the tire is deflated but not damaged, the aircraft can be taxied at low speed with the following limitations:

  1. If one tire is deflated on one or more gears (i.e., a maximum of three tires) the speed should be limited to 7 knots when turning.
  2. If two tires are deflated on the same main gear (the other main gear tires not being deflated), speed should be limited to 3 knots and the nose wheel steering angle limited to 30 degrees.

Taxiing the aircraft with deflated tires should only be done if absolutely necessary and all other means of moving the aircraft have been exhausted.

68
Q

NAVIGATION

RNP 10 oceanic/remote area operations are approved:

A
  • With GPS PRIMARY

* Without GPS Primary (GPS deselected or inoperative), for 6.2 hours following the loss of the second GPS.

69
Q

MINIMUM FLIGHT CREW OXYGEN PRESSURE

A

Crew-600 psi
Crew + 1-800 psi
Crew + 2-1000 psi

70
Q

WEIGHT LIMITATIONS
A321

Maximum Taxi Weight (lb)

A

207,010

71
Q

WEIGHT LIMITATIONS
A321

Maximum Takeoff Weight (lb)

A

206,130

72
Q

WEIGHT LIMITATIONS
A321

Maximum Landing Weight (lb)

A

171,520

73
Q

WEIGHT LIMITATIONS
A321

Maximum Zero Fuel Weight (lb)

A

162,700

74
Q

Maximum Tailwind for Takeoff (A321)

A

10kt

75
Q

Approach Category for 319/320

A

Category C

76
Q

Approach Category for 321

A

Category D

77
Q

Max Tailwind for TO and LNDG

A

319/320

TO-15kts/LNDG-10kts

321

TO&LNDG-10kts

78
Q

AUTOLAND REQUIRED

A

Autoland is required below CAT I minimums.
Furthermore, to minimize the chances of a go around, Frontier’s policy is to set up and brief for an autoland IF
the reported RVR/visibility is at or below 1/2 mile or 2400 RVR AND all of the requirements for an autoland
can be met (environmental, aircraft approach capability, ground equipment, etc.), the approach will be
briefed and flown as a CAT II or CAT III autoland.

A319/320 Limitations (1 decks)

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