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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
TAXI SPEED (A320/321)
When the taxi weight is higher than 167,550 lbs do not exceed a taxi speed of 20 kt during a turn.
25
Max operating altitude with slats and/or flaps extended
20,000 feet
26
CABIN PRESSURE LIMITATIONS
Maximum positive differential pressure . . . . . . . . . . . . . . . . . . . .9.0 psi Maximum negative differential pressure . . . . . . . . . . . . . . . . . . . .- 1 psi Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8.6 psi
27
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:
10 hours of APU operation
28
APU Starter Duty Limits
After three starter motor duty cycles, each separated by a one minute cool down, wait 60 minutes before attempting three more cycles
29
APU Maximum N
107% NOTE: The APU automatically shuts down at 107% N speed (ECAM display).
30
APU Maximum EGT
675C
31
APU Maximum EGT for start (below 35,000 feet)
1090C
32
APU Maximum EGT for start (above 35,000 feet)
1120C
33
Maximum altitude for APU electrical and start
39,000ft
34
Maximum altitude for APU battery start
25,000ft
35
Maximum altitude for APU pneumatics (1 pack w/electrical)
22,500ft
36
Maximum altitude for APU assisted engine start
20,000ft
37
Maximum altitude for APU pneumatics (2 packs w/electrical)
15,000ft
38
AUTO FLIGHT After Takeoff/Go-Around (If SRS is indicated)
100ft AGL
39
AUTO FLIGHT Enroute
900ft AGL
40
AUTO FLIGHT Non-Precision Approaches
DA/DDA
41
AUTO FLIGHT Non-Autoland ILS Approach with CAT 1 displayed on FMA
160ft AGL
42
AUTO FLIGHT Non-Autoland ILS Approach with CAT 2/3 displayed on FMA
80ft AGL
43
AUTO FLIGHT Autoland ILS Approach (one or two autopilots)
Rollout/Taxi Speed
44
AUTO FLIGHT Autoland with braking action less than fair?
Prohibited
45
AUTOLAND WIND RESTRICTIONS
– 30 knots of headwind – 15 knots of crosswind – 10 knots of tailwind
46
ENGINES THRUST SETTING/EGT LIMITS. TAKEOFF and GO-AROUND
``` 5 min (950C) (NEO 1060C) 10 min-Only in event of an engine failure ```
47
ENGINES THRUST SETTING/EGT LIMITS MCT
Unlimited (915C)
48
ENGINES THRUST SETTING/EGT LIMITS STARTING
725C
49
OIL Maximum continuous oil temperature
140C
50
OIL Maximum transient oil temperature (15 minutes)
155C
51
OIL Minimum starting oil temperature
-40C
52
OIL Minimum oil temperature for takeoff
19C
53
OIL Minimum oil quantity
11 quarts plus .5 quarts per hour of estimated flight time
54
ENGINES Maximum N1
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
ENGINES Maximum N2
105%
56
ENGINES STARTER
– 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
REVERSE THRUST
– 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
REDUCED THRUST TAKEOFF
– 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
FUEL FUEL TEMPERATURE LIMITS
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
FUEL APPROXIMATE USABLE FUEL WEIGHT AND VOLUME
Total Pounds=41,285 or 41,893
61
FUEL MINIMUM FUEL FOR TAKEOFF
The minimum fuel quantity for takeoff is 3300 lbs. The WING TK LO LVL warning must not be displayed on ECAM.
62
FUEL MAXIMUM ALLOWED WING FUEL IMBALANCE  Inner tanks – Outer tanks balanced:
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
FUEL MAXIMUM ALLOWED WING FUEL IMBALANCE  Outer tanks:
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
FUEL MANAGEMENT
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
HYDRAULIC MAX hydraulic pressure
3200 psi
66
BRAKES Maximum brake temperature for takeoff
300C
67
TAXI WITH DEFLATED TIRES
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
NAVIGATION RNP 10 oceanic/remote area operations are approved:
* With GPS PRIMARY | * Without GPS Primary (GPS deselected or inoperative), for 6.2 hours following the loss of the second GPS.
69
MINIMUM FLIGHT CREW OXYGEN PRESSURE
Crew-600 psi Crew + 1-800 psi Crew + 2-1000 psi
70
WEIGHT LIMITATIONS A321 Maximum Taxi Weight (lb)
207,010
71
WEIGHT LIMITATIONS A321 Maximum Takeoff Weight (lb)
206,130
72
WEIGHT LIMITATIONS A321 Maximum Landing Weight (lb)
171,520
73
WEIGHT LIMITATIONS A321 Maximum Zero Fuel Weight (lb)
162,700
74
Maximum Tailwind for Takeoff (A321)
10kt
75
Approach Category for 319/320
Category C
76
Approach Category for 321
Category D
77
Max Tailwind for TO and LNDG
319/320 TO-15kts/LNDG-10kts 321 TO&LNDG-10kts
78
AUTOLAND REQUIRED
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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