F9

Question 0

Weights

Answer 0

A319 155,200 154,320 134,480 125,660
A319 IGW 167,320 166,440 137,780 128,960
A320 170,630 169,750 142,190 134,480
A320 IGW 170,630 169,750 145,500 137,780
A320 NEO 170,630 169,750 148,590 141,750
A321 207,010 206,130 171,520 162,700

Question 1

FLIGHT MANEUVERING LOAD ACCELERATION LIMITS
Clean configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Slats and/or flaps extended . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Answer 1

Clean -1 to 2.5

Flaps n slats 0 to 2

Question 2

Slope
Runway alt
Min runway width

Answer 2

+- 2

9200

100ft / 30 m

Question 3

Maximum crosswind demonstrated for takeoff . . . . . . . . . . . . . . . . . . . . . . . . .

Maximum crosswind demonstrated for landing. . . . . . . . . . . . . . . . . . . . . . . . .

Maximum tailwind for takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Maximum tailwind for landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Answer 3

Maximum crosswind(1)
Takeoff Landing.
35kts 38kts
Maximum tailwind(1).
A319 &A320s A321s
Takeoff Landing Takeoff Landing
15kts 10kts 10kts. 10kts

Question 4

– A normal runway is any runway at least ……wide.

– A narrow runway is any runway less than ……wide.

Answer 4

150 ft / 45 m

100 ft/ 33 m

Question 5

Diversion to a normal runway is recommended in case of:

Answer 5

• Autoland is not authorized
• Diversion to normal width runway is recommended 
in case of:
– Rudder jam
– Rudder pedal jam
– Yaw damper fault
– No nosewheel steering
– Any wheel brake inoperative

Question 6

PASSENGER & CARGO DOOR LIMITATIONS

Answer 6

MAXIMUM WIND FOR PASSENGER DOOR OPERATION 65kts
MAXIMUM WIND FOR CARGO DOOR OPERATIONS 40kts/50kts(1)
(1) 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

Question 7

SPEED LIMITATIONS

Maximum VMO/MMO . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt/…..mach

Answer 7

350 / .82

Question 8

Turbulence speed
FL200 and below. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt
Above FL200 through FL310 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt
Above FL310 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . mach

Answer 8

250
275
.76

Question 9

Flap slat speed

Answer 9

Flap 319/320. A321 Flt Phase
1 18 0/0/0 1 230 235 Holding
1 18 10/10/10 1 + F 215 225 Takeoff
2 22 15/15/14 2 200 215 TO / App
3 22 20/20/21 3 185 195 TOAppLdg
FULL 27 40/35/25 FULL 177 190 Landing

Question 10

Gear

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

Answer 10

280/.67
250
220

Question 11

Maximum altitude at which the landing gear may be extended . . . . . . . . . ft

Answer 11

25000

Question 12

Maximum Tire Speed (ground speed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . kt

Answer 12

195

Question 13

Maximum speed for use of windshield wipers . . . . . . . . . . . . . . . . . . . . . . . . . . kt

Answer 13

230

Question 14

Maximum speed for opening cockpit window . . . . . . . . . . . . . . . . . . . . . . . . . . kt

Answer 14

200

Question 15

Max taxi speed Weight Greater than 167,550 lbs

Answer 15

20knts

Question 16

Max operating altitude with slats and/or flaps extended is ……..feet.

Answer 16

20000

Question 17

Cabin pressure
Maximum positive differential pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi
Maximum negative differential pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi
Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . psi

Answer 17

9. 0
   - 1
10. 6

Question 18

Ram air inlet
If change in P is greater than …..psi, the check valve located downstream will not open even if
the ram air door has been selected open.

Answer 18

1

Question 19

Air conditioning
WITH LP GROUND UNIT
Do not use conditioned air simultaneously from …..and …..ground unit (to avoid
chattering of the non return valves).

Answer 19

Packs, LP

Question 20

WITH HP GROUND UNIT
An external ….. source may be used for air conditioning, provided the air supply is
confirmed to be free from ….. contamination. Do not use …. ground unit when ….. supplies bleed air to avoid bleed system damage.

Answer 20

HP, oil, HP, APU

Question 21

Avionics ventilation
The airplane electrical system should not be powered for more than …. hours without
a cooling system when the outside air temperature is above ….C.

Answer 21

2, 49

Question 22

Reporting sheet
Airframe vibrations shall be recorded in the aircraft …….and on the ………….. (Form 31048), which contains detailed
information used by maintenance to isolate and resolve airframe vibration issues.
Whenever possible this form should be filled out in …… and as soon as practical after
experiencing airframe vibration. Completed forms shall be left in the ………… .

Answer 22

Logbook, airframe vibration reporting sheet, flight, aircraft logbook

Question 23

APU
The APU may be started and operated even if the …………….. advisory is
displayed. Maintenance action is required within the next …… hours of APU operation.
NOTE: A logbook entry is not required after receiving this advisory message.
Contact …… to determine the status of required maintenance action.

Answer 23

Low oil level exam,10 , mcc

Question 24

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

Answer 24

3, 1, 60

Question 25

APU Maximum N . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . % NOTE: The APU automatically shuts down at % N speed (ECAM display). Maximum EGT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C Maximum EGT for start (below 35,000 feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . C Maximum EGT for start (above 35,000 feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . C

Answer 25

``` 107 107 675 1090 1120 ```

Question 26

Maximum altitude for APU electrical and start . . . . . . . . . . . . . . . . . . . . . . . . . ft

Answer 26

39000

Question 27

Maximum altitude for APU battery start . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ft

Answer 27

25000

Question 28

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

Answer 28

22500

Question 29

Maximum altitude for APU assisted engine start . . . . . . . . . . . . . . . . . . . . . . . Ft

Answer 29

20000

Question 30

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

Answer 30

15000

Question 31

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

Answer 31

100

Question 32

Autopilot enroute

Answer 32

500

Question 33

Autopilot Non-Precision Approaches

Answer 33

DDA/DA

Question 34

Autopilot Non-Autoland ILS Approach with CAT 1 displayed on FMA

Answer 34

160

Question 35

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

Answer 35

80

Question 36

Autopilot Autoland ILS Approach (one or two autopilots)

Answer 36

Rollout/taxi

Question 37

Autopilot When visibility is less than .....RVR or ....,the approach must be flown with the autopilot(s) engaged if operable.

Answer 37

4000 / 3/4

Question 38

Autopilot The use of AP or FD in OPEN DES or DES mode is not permitted inside the ......or below .......ft AGL on a visual approach.

Answer 38

FAF | 1000

Question 39

The use of autothrust is approved with or without ......in selected or managed mode.

Answer 39

AP/FD

Question 40

NON PRECISION APPROACHES WITH ENGINE-OUT If one engine is inoperative, it is ...........to use the autopilot to perform non precision approaches in the following modes: FINAL APP, NAV V/S, NAV/FPA (not applicable on A/C 205 - 216, 220, 223 & 227). Only.....use is authorized.

Answer 40

Not permitted, | Fad

Question 41

FLIGHT MANAGEMENT FUNCTION FMGS lateral and vertical navigation has been certified for takeoff, departure, en route, arrival (terminal area operations), instrument approach procedures (except ...., .... and ....) and missed approach/go around procedures.

Answer 41

ILS, LOC, LDA

Question 42

``` RNP accuracy with GPS PRIMARY, or radio updating, has been demonstrated to be: With AP ON in NAV With AP OFF and FD on in NAV With AP OFF and FD OFF En route ...nm ....nm ....nm Terminal area ....nm .....nm ....nm Approach ....nm ....nm ...... ```

Answer 42

1 1 1.1 .5. .51. .51 .3. .3. Not authorized

Question 43

Without ............ (GPS deselected or inoperative), .....accuracy has been demonstrated provided the appropriate RNP value is checked or entered on the MCDU and .......accuracy is displayed.

Answer 43

GPS Primary, NAV, HIGH

Question 44

RNP 0.3 has been demonstrated in normal and non-normal conditions as follows for the following modes. – – – – NOTE: Use of AP for RNP AR operations is recommended.

Answer 44

– Departure in NAV mode, – Initial approach in NAV or APP NAV modes, – Final approach in FINAL APP mode, – Missed approach in NAV mode.

Question 45

Autoland approaches may be conducted when the following conditions are satisfied:

Answer 45

CAT II/III runway, CAT II/III aircraft, crews CAT II/III trained, appropriate ground facilities are operational, wind within limits, braking action medium or better.

Question 46

toland Required: If the requirements for an autoland are satisfied and the ATIS reported RVR/visibility is at or below .......RVR or ......mile, the approach must be briefed and flown as a CAT II or CAT III autoland except as noted below. NOTE: If any of the CAT II/III requirements are not met, and CAT I or better weather conditions prevail upon arrival at the airport, the crew may brief and fly the approach to current CAT I minimums as stated in FOM I, Chapter 20, with a manual landing

Answer 46

2400, 1/2

Question 47

Autolands are prohibited if braking action is reported less than

Answer 47

Medium

Question 48

Autolands are not authorized on runways less than .....feet wide

Answer 48

150

Question 49

Automatic landing is not allowed below ......ft pressure altitude.

Answer 49

-1000

Question 50

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

Answer 50

Medium | Low or medium

Question 51

“PULL UP” - “OBSTACLE AHEAD PULL UP” - “TERRAIN AHEAD PULL UP”

Answer 51

– AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – PITCH. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP Pull to full backstick and maintain in that position. – THRUST LEVERS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA

Question 52

Emergency decent

Answer 52

CREW OXY MASKS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . USE – SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON – EMER DESCENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INITIATE) – THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .IDLE – SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL

Question 53

Loss of braking

Answer 53

– REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE – A/SKID & N/W STRG. . . . . . . . . . . . . . . . . . . . . . . . . . OFF – BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS – MAX BRK PR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 PSI  If STILL NO BRAKING: – PARKING BRAKE . . . . .SHORT AND SUCCESSIVE APPLICATIONS

Question 54

SMOKE / FUMES / AVNCS SMOKE

Answer 54

– OXY MASK/GOGGLE . . . . . . . . . . . . . . . . .USE/100%/EMERG

Question 55

Stall recovery

Answer 55

– NOSE DOWN PITCH CONTROL . . . . . . . . . . . . . . . . . . . .APPLY – BANK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL – THRUST . . . . . . . . . . . . . . .INCREASE SMOOTHLY AS NEEDED – SPEEDBRAKES. . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED – FLIGHT PATH. . . . . . . . . . . . . . . . . . . . . .RECOVER SMOOTHLY – FLAP 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .SELECT

Question 56

Stall warning at lift off

Answer 56

– THRUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA – PITCH ATTITUDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15° – BANK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL

Question 57

Tcas warning

Answer 57

AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – BOTH FDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF – Respond promptly and smoothly to an RA by adjusting or maintaining the vertical speed, as required, to reach the green area and/or avoid the red area of the vertical speed scale.

Question 58

UNRELIABLE SPEED INDICATION/ADR CHECK PROCEDURE | A/C 201 - 204, 218, 219, 221, 223 AND ALL A319

Answer 58

– AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF – A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF – THRUST/PITCH – Below THR RED ALT. . . . . . . . . . . . . . . . . . . . . . . . .15TOGA – Above THR RED ALT and Below FL 100 . . . . . . . . 10CL – Above THR RED ALT and Above FL 100 . . . . . . . . .5CL – FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG – FLAPS (if CONF FULL). . . . . . . . . . SELECT CONF 3 AND MAINTAIN – SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED – L/G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP

Question 59

UNRELIABLE SPEED INDICATION/ADR CHECK PROCEDURE | A/C 205 - 216, 220, 227

Answer 59

– AP/FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF – A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF – THRUST/PITCH – Below THR RED ALT . . . . . . . . . . . . . . . . . . . . . . . . .15TOGA – Above THR RED ALT and Below FL 100 . . . . . . . . .10CL – Above THR RED ALT and Above FL 100 . . . . . . . . . 5CL – FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN CURRENT CONFIG – FLAPS (if CONF FULL) . . . . . . . . . . SELECT CONF 3 AND MAINTAIN – SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . . . . . .CHECK RETRACTED – L/G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Question 60

Wind shear

Answer 60

WINDSHEAR Refer to ABN-80 WINDSHEAR or FOM Vol II 4.10  If after V1  AIRBORNE, INITIAL CLIMB or LANDING – THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA – REACHING VR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ROTATE – SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FOLLOW This includes the use of full back stick, if demanded. – THR LEVERS AT TOGA. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET OR CONFIRM – AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KEEP ON – SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FOLLOW

Question 61

Winds hear ahead

Answer 61

WINDSHEAR AHEAD Refer to ABN-80 WINDSHEAR or FOM Vol II 4.10  When airborne As usual, the slat/flap configuration can be changed, provided the windshear is not entered.  During landing – THR LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .TOGA – AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KEEP ON – SRS ORDERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FOLLOW – GO AROUND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PERFORM – AP (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . KEEP ON

Question 62

321 weights

Answer 62

Max taxi wt 207010 Max to wt 206130 Max ld wt 171520 Zero fuel wt 162700

Question 63

Max tail wind for take off. 319, 320, 321

Answer 63

15,15,10

Question 64

Flap slats 321 ``` 1, 1 +f, 2, 3, 4, ```

Answer 64

``` 235 225 215 195 190 ```

Question 65

Taxi when over 167550 don't go faster than?

Answer 65

20 knots in turn

Question 66

Max altitude with flap/slats extended

Answer 66

20000

Question 67

Only open ram air inlet when pressure diff is?

Answer 67

Lower than 1psi

Question 68

AUTOLAND PERFORMANCE LIMITS (BELOW 500 FT)

Answer 68

``` – Glideslope Deviation < one dot – Localizer Deviation < 1/4 dot – Airspeed ±5 knots of target – Max Rate of Descent 1000 fpm – Airspeed not below VLS – Bank not to exceed 7° – -2.5° < Pitch < 10° ```

Question 69

GENERATOR LOAD – MAXIMUM

Answer 69

Continuous load per generator100% (90 kVA)

Question 70

TR LOAD – MAXIMUM

Answer 70

Continuous load per TR200 amps

Question 71

ENGINE EGT AND THRUST - MAXIMUM

Answer 71

OPERATING CONDITION TIME LIMIT (1) EGT LIMIT NOTE TAKEOFF and GO-AROUND 5 min. 950°C 10 min. Only in case of engine failure MCT Unlimited 915°C STARTING. 725°C

Question 72

ENGINE OIL QUANTITY

Answer 72

11 Quarts plus .5 quart for every hour of estimated flight time

Question 73

Minimum oil temperature for takeoff

Answer 73

19° C

Question 74

Takeoff at reduced thrust is prohibited:

Answer 74

• on slippery or contaminated runways; • when suspected, reported or known wind shear is present (e.g., predictive wind shear alerts, or ATC- issued wind shear alerts for the departure runway or departure path); • when a Special Departure Procedure specifies full thrust for takeoff.

Question 75

AVIONICS VENTILATION

Answer 75

The aircraft electrical system should not be powered for more than 2 hours without a cooling system when the outside air temperature is above 49°C

Question 75

Auto land max wind

Answer 75

Include gusts when applying these wind limits. A320 & A321 A320NEO & A319 Headwind. 30 knots 20 knots Crosswind. 15 knots 15 knots Tailwind. 10 knots 5 knots Wind Correction: Vls + wind correction(2) 5 to 15 knots 5 to 15 knots