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1
Q

Maximum operating altitude

A

39,100 feet

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2
Q

Maximum crosswind for landing

A

38 knots

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3
Q

Maximum tailwind for landing 319/320

A

10 knots or Company page

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4
Q

Maximum tailwind for landing 321/NEO

A

15 knots or Company page

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5
Q

Minimum altitude for autopilot engagement

A

100ft AGL and 5 seconds after liftoff

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6
Q

Engine oil quantity requirements 319/320/321

A

9.5 quarts plus 0.5 quarts per hour of flight

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7
Q

Engine oil requirements 321NEO

A

14 quarts at or above -30C
16.5 quarts below -30C

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8
Q

Minimum oil temp for takeoff 319/320/321

A

-10C

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9
Q

Minimum oil temperature for takeoff 321NEO

A

52C

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10
Q

APU bleed air is usable up to

A

FL200 older 320s
FL225 everything else

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11
Q

Do not extend flaps/slats above

A

FL200

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12
Q

After crossing DECEL, if GWCG is above XX% do not use speed brakes below XXX knots

A

35%, 240 knots

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13
Q

Minimum fuel required for dispatch is

A

8000lbs with no fuel ECAM messages

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14
Q

The reset of any fuel pump circuit breaker is

A

Prohibited

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15
Q

Maximum brake temperature for takeoff without brake fans is

A

275C

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16
Q

Maximum brake temperature with brake fans on is

A

150

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17
Q

Minimum oxygen pressure for dispatch is

A

1000psi

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18
Q

Acceptable rudder trim range for takeoff is

A

0.0-0.3

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19
Q

Engine warm up requirements non-first flight

A

2 minutes

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20
Q

Engine warm up requirements first flight 319/320/321

A

5 minutes if the engines have been off for more than 4 hours

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21
Q

Engine warm up requirements first flight 321NEO

A

5 minutes if the engines have been off for more than 2 hours

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22
Q

Select PACK FLOW to LOW or ECON 319/320 pax less than

A

138

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23
Q

Select PACK FLOW to LOW or ECON 321/NEO pax less than

A

168

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24
Q

Engine cool down time required before shutdown

A

3 minutes at below 40%N1

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25
Battery voltage must be at least
25.5 volts
26
Manual engine start is required for a first flight when the temperature is
10C or less
27
To fly an approach from 1500AGL to landing requires how much fuel?
250lbs
28
Approximate fuel required for a go-around and subsequent pattern and landing 319/320/NEO
1,000lbs
29
Approximate fuel required for a go-around and subsequent pattern and landing 321
1,500 lbs
30
Taxiing across a raised arresting gear cable at speeds up to XX knots does not require a logbook entry
60kts
31
Taxiing across a raised arresting gear cable at speeds above XX knots requires a logbook entry
60 knots
32
On the ground, after ___ minutes in icing conditions, engine ice clearing procedures for the 319/320/321
30 minutes, 70%N1 for 30 seconds
33
On the ground, after 30 minutes in icing conditions, engine ice clearing procedures for he NEO
60% N1 momentarily
34
During icing conditions, accomplish a XXX takeoff
Standing
35
A standing takeoff is accomplished by
Holding the brakes and allowing the engines to stabilize momentarily at 70% N1
36
Wing anti-ice may or may not be used for takeoff?
May NOT be used for takeoff. May be used after flap retraction
37
Do not takeoff with standing water, slush, or wet snow in excess of
1/2 inch
38
Do not takeoff with dry snow in excess of
4 inches
39
Do not land with any braking action report of XXX in the landing or rollout portion of the runway
NIL
40
Do not land if standing water, slush, or wet snow reported more than
1 inch depth
41
Do not land if dry snow reported more than
4 inches depth
42
After landing, if the OAT is greater than XX, leave the flaps at X
35C, flaps 1
43
The flight release is legal if the fuel gauges reflect the Block Fuel +/-
+1,000 lbs, -200 lbs
44
The cockpit fuel gauges should not differ from the FSR by more than ____ without explanation (APU run, etc)
300 lbs
45
319/320/NEO Minimum fuel
3,500 lbs
46
321 Minimum fuel
4,000 lbs
47
319/320/NEO Emergency fuel
3,000 lbs
48
321 Emergency fuel
3,000 lbs
49
A short runway is any runway less than
6,000 feet
50
Minimum runway width for normal operations is
148 feet
51
FOM 14.1.2.2 authorizes runway width as low as XXX with certain conditions
100 feet
52
Largest minimum width for a 180 degree turn is
93 feet for the 321
53
Pilots must refuse a NOTOC if it has
A WARNING header
54
Cabin PR excess altitude or rapid depressurization:
OXYGEN MASKS - ON CREW COMMUNICATIONS - Establish
55
Unreliable Airspeed or Check ADR procedure:
If the safe conduct of the flight is impacted: AP - off A/THR - off FD - off Pitch/Thrust: Below THR RED ALT - 15°/ TOGA Abv THR RED ALT and below FL100 - 10°/CLB Abv THR RED ALT and abv FL100 - 5°/CLB Flaps- If Flaps 0,1,2,3 - Maintain current config If Flaps Full - select & maintain Flaps 3 Speed Brakes - confirm retracted Landing Gear - Up When at MSA or pattern altitude - level off for troubleshooting
56
Loss of Braking
Thrust levers - maximum reverse (as required) Brake pedal - release A/SKID & NWS switch - off Brake pedals - apply (max 1000 psi) Parking brake - use (if required)
57
Emergency evacuation philosophy
STOP CONFIGURE SHUTDOWN EVACUATE
58
Stabilized approach criteria: At 1,000 the aircraft should be
Fully configured for landing Aligned with the intended landing runway Maintain a stabilized descent rate not to exceed 1,000fpm
59
Stabilized approach criteria: At 500 feet the aircraft should be
On speed with the engines stabilized at the thrust setting required to maintain the descent rate and airspeed
60
Aircraft lights required when: The aircraft is powered
NAV and LOGO - 1 or 2 (or NAV - ON) Strobe - AUTO
61
For a Cat II approach, at 50 ft RA the runway environment
Must be in sight
62
For a CAT III approach, at 50 ft RA the runway environment
Is not required to be in sight. No visual reference is required.
63
A static takeoff is accomplished by
Bringing the aircraft to a stop on the runway and centering the nose wheel steering, and then apply takeoff thrust as normal
64
If the runway selected for takeoff is contaminated, you may not:
Use FLEX takeoff power. TOGA is required.
65
A static takeoff is required when:
RVR is less than 1600 (500m)
66
Runway edge lights are required:
For all takeoffs and landings between sunset and sunrise, or anytime visibility is reported 2sm or less

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