A320/A321 Taxi Speed: Max speed during a turn if weight > 167,500 lbs

20 knots

Air bleed extraction from the APU for wing anti-ice is APU: Maximum EGT for start:

not permitted

Below FL250 . . . . . . . . . . . . . . . . . . . . . . . 900C Above FL250 . . . . . . . . . . . . . . . . . . . . . . . 982C

Autoland Max: Crosswind

20 knots

Autoland Max: Headwind

30 knots

Autoland Max: Tailwind

10 knots -2.5 to -3.25 (A319), -2.5 to -3.15 (A320/A321). -1.0 psi

Automatic Approach, Landing and Roll Out: Glideslope angle must be within the range of

Cabin Pressure: Max negative differential pressure Cabin Pressure: Max positive differential pressure Category I: The FMA must display

8.6 psiCAT 3 DUAL or CAT 3 SINGLE. Autolands to CAT I runways are authorized. Refer to AOM VOL 2 (2.142).

Category II: The FMA must display Category IIIA: The FMA must display Category IIIB: The FMA must display Cockpit Window Open: Max speed Engine Inoperative ApproachesFlaps and Slats Maximum altitude with flaps and/or slats extended is

CAT 3 DUAL or CAT 3 SINGLE

CAT 3 DUAL or CAT 3 SINGLE

CAT 3 DUAL

200 knotsThe following is not authorized with an engine inoperative: Autolands (CAT I, II or III). The use of an autopilot to fly a non-precision approach using NAV or FINAL APP lateral modes. Only FD is permitted in this case.

20,000'.

Gear down Speeds: Max altitude landing gear may be extended

FL250

Gear down Speeds: Max landing gear extension Gear down Speeds: Max landing gear retraction Gear down Speeds: Max with landing gear extended

250 knots

220 knots

280 knots/M.67

High Pressure (HP) ground unit:If fuel imbalance between any two tanks is more than _____ lbs. refer to fuel imbalance limitations in the COM. Jet A fuel temp goes below what temp do you need to monitor and what temp must you keep it warmer then?

Do not use HP ground unit when the APU is supplying bleed air to avoid bleed system damage.

1100

-34C and -36C

Load Acceleration Limits: Clean configuration Load Acceleration Limits: Slats and flaps extended Load Acceleration Limits: Slats extended and flaps retracted Max continuous load per generator Max continuous load per TR

-1g to +2.5g

0g to +2.0g

0g to +2.0g

100% (90 kVA)

200 A

Max crosswind demonstrated

38 knots (gust included)

Max runway altitude

9200'

Max runway slope

+/- 2%

Max tailwind - landing

10 knots

Max tailwind - takeoff Max wind for pax door operation Maximum brake temperature for takeoff (brake fans off) Maximum EGT with APU running: Maximum field elevation for an autoland is:Maximum reverse should not be used below ____ or when _____ starts to fluctuate.

15 knots

65 knots

300C 682 with 5 seconds confirmation time for shutdown or, 700C for immediate shutdown. 9200' (A319) 6500' (A320) 5750' (A321)

70 knots airspeed Applicable Circling Mins - 100'

Minimum height for autopilot disengagement: Circling approachMinimum height for autopilot disengagement: ILS approach (when CAT2 or CAT3 is not displayed on the FMA)

160' AGL

Minimum height for autopilot disengagement: ILS autolandingMinimum height for autopilot disengagement: Straight-in non-precision approach

Certified to remain engaged

Applicable Minimum

Minimum height for autopilot engagement: Go-aroundMinimum height for autopilot engagement: Takeoff with SRS modeMinimum height for autopilot engagement: Takeoff without SRS mode

100' AGL

100' AGL

900' AGL GPS PRIMARY is available or, HIGH accuracy is displayed and, Navaid raw data is monitored.

NAV mode may be used in the terminal area, provided: Nominal runway width Oil temperature: Maximum continuous temperature Oil temperature: Maximum transient temperature (15 min) Oil temperature: Minimum prior to exceeding idle

150'

155C

165C

-10C

Oil temperature: Minimum prior to takeoff Oil temperature: Minimum starting temperature Power Plant: Minimum oil pressure Power Plant: Minimum oil quantityPower Plant: No running engagement of the starter, when N2 is above ____ on Ground and _____ inf flight.

50C

-40C

60 psi 11qts + est. consumption (~0.3 qt/hr) 10% 18%3 consecutive cycles: 2 cycles of 2 minutes each, followed by a 3rd cycle of 1 minute. Pause between start attempts: 15 seconds. Cooling period, following 3 starts attempts or 4 minutes of continuous cranking: 30 minutes.

Power Plant: Start CyclePowerplant: EGT Limits: Maximum Continuous (MCT)

610C Unlimited

Powerplant: EGT Limits: StartingPowerplant: EGT Limits: Takeoff and GoAround (TOGA) (A319/A320)

635C 635C for 5 min or 10 min (if engine fail) 650C for 5 min or 10 min(if engine fail)

Powerplant: EGT Limits: Takeoff and GoAround (TOGA) (A321)

The APU may be started (with normal A/C power supply) and operated up to the maximum certified pressure altitude of

39,100'.3 consecutive start attempts. After the third start attempt, wait 60 minutes before attempting 3 more cycles.

The APU starter duty cycle isThe maximum altitude for a battery start (emergency electrical configuration) of the APU is The maximum altitude for bleed extraction is ______ with one pack operating

FL250.

FL200

The maximum altitude for bleed extraction is ______ with two packs operating.

FL150

The normal hydraulic operating pressure is Tires: Max ground speed Turbulent Air Penetration Speed: A319/A320: Turbulent Air Penetration Speed: A321: Vmo/Mmo

3000 psi +/- 200 psi.

195 knotsBelow FL200, maintain 250 knots. At or above FL200, maintain 275 knots/.76 Mach. Below FL200, maintain 270 knots. At or above FL200, maintain 300 knots/.76 Mach.

350KIAS/.82mach

When is reduced thrust not permitted for takeoff? Windshield Wiper In Use: Max speed

On Contaminated runways or in known windshear conditions.

230 knots