Limitations

Question 0

Runway slope (mean)

Answer 0

+- 2%

Question 1

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS

Answer 1

Clean configuration . . . . . . . . . . . . . - 1 g to + 2.5 g

Slats and/or flaps extended . . . . . . . . . . 0 g to + 2 g

Question 2

Runway altitude

Answer 2

9200 ft

Question 3

Minimum runway width

Answer 3

100 ft/30m

Question 4

Maximum crosswind demonstrated for takeoff

Answer 4

38 kt*

*The maximum demonstrated crosswind value is not an Airplane Flight Manual (AFM)
limitation: It is the maximum crosswind condition experienced during the aircraft
certification campaign. Airbus recommends that operators should not intentionally
operate in crosswinds that exceed this value.

Question 5

Maximum crosswind demonstrated for landing

Answer 5

38 kt*

Question 6

Maximum tailwind for takeoff (319 & 320)

Answer 6

15 kts

Question 7

Maximum tailwind for landing (319, 320 & 321)

Answer 7

10 kts

Question 8

NORMAL & NARROW RUNWAY LENGTHS

Answer 8

A normal runway is any runway at least 150 ft/45m wide.

A narrow runway is any runway less than 150 ft/45m wide.

Question 9

Maximum wind for passenger door operation

Answer 9

65 kt

Question 10

Maximum wind for cargo door operation

Answer 10

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.

Question 11

Maximum VMO/MMO

Answer 11

350 kt/.82 mach

Question 12

SEVERE TURBULENT AIR PENETRATION

SPEED

Answer 12

FL200 and below. . . . . . . . . . . . . . . . . . . . . . . 250 kt

Above FL200 through FL310 . . . . . . . . . . . . . 275 kt

Above FL310 . . . . . . . . . . . . . . . . . . . . . .0.76 mach

Question 13

Runway altitude

Answer 13

9,200 ft

Question 14

Minimum runway width

Answer 14

100 ft/30m

Question 15

Contaminated Runway

Maximum demonstrated cross wind for takeoff and landing:

Answer 15

Wet runway . . . . . . . . . . . . . . . .33 kt (gust included)

Contaminated runway . . . . . . . 10 kt (gust included)

Question 16

Maximum wind for cargo door operation

Answer 16

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.

Question 17

SEVERE TURBULENT AIR PENETRATION

SPEED

Answer 17

FL200 and below. . . . . . . . . . . . . . . . . . . . . . .250 kt

Above FL200 through FL310 . . . . . . . . . . . . . 275 kt

Above FL310 . . . . . . . . . . . . . . . . . . . . . .0.76 mach

Question 18

MAXIMUM FLAPS/SLATS SPEEDS

Answer 18

1. 230 Holding
2. 215 Takeoff
3. 200 Takeoff / Approach
4. 185 Takeoff / Approach / Landing
   Full. 177 Landing

It is Frontier’s procedure to extend flaps at a maximum of VFE - 10 knots, except for
Flaps Full, which will be extended at a maximum of VFE - 15 knots.

Question 19

Maximum altitude at which the landing gear may be extended

Answer 19

25,000 ft

Question 20

Maximum Tire Speed (ground speed)

Answer 20

195 kt

Question 21

Maximum speed for use of windshield wipers

Answer 21

230 kt

Question 22

Maximum speed for opening cockpit window

Answer 22

200 kt

Question 23

TAXI SPEED (A320)

Answer 23

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

Question 24

Max operating altitude with slats and/or flaps extended

Answer 24

20000 feet

Question 25

AUTOPILOT ENGAGEMENT

Answer 25

After Takeoff/Go-Around (If SRS is indicated) 100 AGL Non-Autoland ILS Approach with CAT 1 displayed on FMA 160 AGL Non-Autoland ILS Approach with CAT 2/3 displayed on FMA 80 AGL Autoland ILS Approach (one or two autopilots) Rollout/Taxi Speed

Question 26

AUTOLAND WIND RESTRICTIONS

Answer 26

For autolanding, the surface wind conditions are limited to the following: – 30 knots of headwind – 15 knots of crosswind – 10 knots of tailwind

Question 27

Autobrakes (if available) are required when....

Answer 27

Autobrakes (if available) are required for all CAT III approaches. – Runways less than 8000 ft – Medium – Runways 8000 ft or longer – Low or Medium

Question 28

Autolands are prohibited if...

Answer 28

braking action is reported less than fair.

Question 29

The minimum fuel quantity for takeoff is

Answer 29

3300 lbs

Question 30

Maximum brake temperature for takeoff

Answer 30

300 C

Question 31

GEAR DOWN SPEEDS

Answer 31

Maximum speed with landing gear extended (VLE) . . . . . . . . . . . . . . . .280 kt/.67 mach Maximum speed at which the landing gear may be extended . . . . . . . . . . . . . . . 250 kt (VLO extension) Maximum speed at which the landing gear may be retracted . . . . . . . . . . . . . . . 220 kt (VLO retraction)

Question 32

APU LOW OIL LEVEL ECAM

Answer 32

10 hours

Question 33

APU Maximum altitude for APU electrical and start

Answer 33

39,000 ft

Question 34

Maximum altitude for APU battery start

Answer 34

25,000 ft

Question 35

The APU automatically shuts down at

Answer 35

107 %

Question 36

APU starter cycles

Answer 36

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

Question 37

APU Maximum EGT

Answer 37

675 C

Question 38

APU Maximum EGT for start (below 35,000 feet)

Answer 38

1090 C

Question 39

APU Maximum EGT for start (above 35,000 feet)

Answer 39

1120 C

Question 40

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

Answer 40

22,500 ft

Question 41

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

Answer 41

15,000 ft

Question 42

Maximum altitude for APU assisted engine start

Answer 42

20,000 ft

Question 43

MAX hydraulic pressure

Answer 43

3200 psi

Question 44

Maximum brake temperature for takeoff

Answer 44

300 C