Limitations

Question 1

Max Landing Weight

502NK-536NK

Answer 1

137,788 lbs

Question 2

Max Landing Weight

601NK-650NK

Answer 2

145,505 lbs

Question 3

Max Landing Weight

901NK-905NK

Answer 3

148,591 lbs

Question 4

Max Landing Weight

587NK, 588NK, 657NK-683NK

Answer 4

171,519 lbs

Question 5

Max Altitude

Answer 5

FL 398

Question 6

Runway Slope (mean)

Answer 6

+/-2%

Question 7

Runway Altitude

All except 535NK, 536NK

Answer 7

9,200 ft

Question 8

Nominal Runway Width

Answer 8

45m (148ft)

Question 9

Max X-wind Landing

Answer 9

38 kt (gust included)

Question 10

Max Tailwind for Takeoff

Answer 10

15 kt

Question 11

Max Tailwind for Landing

Answer 11

10 kt

Question 12

Max Wind for Passenger Door Operation

Answer 12

65 kt

Question 13

Max Crosswind for Takeoff

901NK-905NK

Answer 13

35 kt (gust included)

Question 14

Vle

Answer 14

280kt/M.67

Question 15

Vlo Extension

Answer 15

250kt/M.60

Question 16

Vlo Retraction

Answer 16

220kt/M.54

Question 17

Max Altitude Landing Gear May Be Extended

Answer 17

25,000ft

Question 18

Windshield Wipers Max Speed

Answer 18

230kt

Question 19

When Taxi Weight Higher than 167,550 lb, taxi speed in a turn
587NK, 588NK, 601NK-905NK

Answer 19

20kt

Question 20

Do not use conditioned air simultaneously from…(to avoid any adverse effects on the air conditioning system)

Answer 20

PACKS and LP ground unit

Question 21

Do not use….when the APU supplies bleed air to avoid any adverse effects to the bleed system

Answer 21

HP ground unit

Question 22

Max positive differential pressure

Answer 22

9.0 psi

Question 23

Max negative differential pressure

Answer 23

-1.0 psi

Question 24

Minimum Height for use of Autopilot

Takeoff with SRS mode

Answer 24

100 ft AGL

Question 25

Minimum Height for use of Autopilot | Straight-in non-precision approach

Answer 25

Applicable Minimum

Question 26

Minimum Height for use of Autopilot | Circling Approach

Answer 26

Applicable Circling Minimums -100 ft

Question 27

Minimum Height for use of Autopilot | ILS Approach when CAT 2 or CAT 3 is not displayed on the FMA

Answer 27

160ft AGL

Question 28

Minimum Height for use of Autopilot | Go-Around (AP or FD engagement)

Answer 28

100ft AGL

Question 29

Minimum Height for Use of Autopilot | All Other Phases

Answer 29

``` 500ft AGL (A319/A320) 900ft AGL (A321) ```

Question 30

Minimum Height for use of Autopilot | Use of the AP or FD in OPEN DES or DES mode is not permitted in Approach, unless the FCU Altitude is set at or above:

Answer 30

Highest of: Minimum or 500ft (A319/A320) Minimum or 900ft (A321)

Question 31

NAV mode may be used in the terminal area, provided:

Answer 31

- GPS PRIMARY is available - HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or - FMS navigation is cross-checked with NAVAID raw data

Question 32

If one engine is inoperative, it is not permitted to use the Autopilot to perform NPAs in the following modes:

Answer 32

FINAL APP, NAV V/S, NAV/FPA | Only FD use is permitted

Question 33

``` Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out All Engines Operative(AEO) And One Engine Inoperative (OEI) N502NK-N536NK ```

Answer 33

(AEO) Headwind - 20kt Tailwind - 5kt Crosswind - 15kt (OEI) Headwind - 15kt Tailwind - 5kt Crosswind - 10kt

Question 34

Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out All Engines Operative(AEO) N601NK-N683NK, N587NK, N588NK

Answer 34

Headwind - 30kt Tailwind - 10kt Crosswind - 15kt

Question 35

Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out All Engines Operative(AEO) N901NK-N905NK

Answer 35

Headwind - 20kt Tailwind - 5kt Crosswind - 15kt

Question 36

Max operating Altitude with slats and/or flaps extended

Answer 36

20,000ft

Question 37

Max Fuel Imbalance at Takeoff, Inner Tanks | 502NK-536NK, 601NK-650NK, 901NK-905NK

Answer 37

1,102 lb

Question 38

Max Fuel Imbalance In Flight and At Landing, Inner Tanks | 502NK-536NK, 601NK-650NK, 901NK-905NK

Answer 38

3,306 lb

Question 39

Max Fuel Imbalance in Flight and At Landing | 587NK, 588NK, 657NK-683NK

Answer 39

2,910 lb

Question 40

Max Fuel Imbalance at Takeoff | 657NK-683NK

Answer 40

882 lb

Question 41

Max brake temperature for Takeoff (brake fans off)

Answer 41

300 C

Question 42

APU Starter duty cycles

Answer 42

After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles

Question 43

EGT limits Takeoff and Go Around 502NK-536NK, 601NK-650NK

Answer 43

5 min, 635 C | 10 min, 635 C only in case of engine failure

Question 44

EGT limits MCT 502NK-536NK, 601NK-650NK 587NK, 588NK, 657NK-683NK

Answer 44

Unlimited 610 C

Question 45

EGT limits Starting 502NK-536NK, 601NK-650NK 587NK, 588NK, 657NK-683NK

Answer 45

635 C

Question 46

EGT limits Takeoff and Go Around 901NK-905NK

Answer 46

5 min, 1,083 C | 10 min, 1,083 C only in case of engine failure

Question 47

EGT limits MCT 901NK-905NK

Answer 47

Unlimited, 1,043 C

Question 48

EGT limits Starting 901NK-905NK

Answer 48

1,083 C

Question 49

EGT limits Takeoff and Go Around 587NK, 588NK, 657NK-683NK

Answer 49

5 min, 650 C | 10 min, 650 C only in case of engine failure

Question 50

Minimum Oil Temperature prior to exceeding idle | 502NK-683NK

Answer 50

-10 C

Question 51

Minimum Oil Temperature for Starting | 502NK-683NK

Answer 51

-40 C

Question 52

Minimum Oil Pressure | 901NK-905NK

Answer 52

65 psi

Question 53

Stater Cycles | 502NK-683NK

Answer 53

3 consecutive cycles, for manual start, observe a 2 min max start cycle time Pause 15s between starts Cooling period, following 3 start attempts or 5 min of continuous cranking wait 30 min No running engagement if the starter, when N2 is above 10% on ground, or 18% in Flight

Question 54

Starter Cycles | 901NK-905NK

Answer 54

3 consecutive start attempts, 35s in between each cycle After 3 cycles, or 15 min of continuous or cumulative cranking: 15 min cooling period No running engagement of the starter, when N2 is above 20%

Question 55

Maximum reverse should not be used below

Answer 55

``` 70 kt (Idle reverse is permitted down to aircraft stop) ```

Question 56

Takeoff on contaminated runway

Answer 56

Reduced thrust takeoff is not permitted on contaminated runways

Question 57

Max Crosswind for engine start

Answer 57

35kt

Question 58

Vmo/Mmo

Answer 58

350kts/M.82

Question 59

Max Tire Ground Speed

Answer 59

195 kts

Question 60

Cockpit Window Open Max Speed

Answer 60

200 kt

Question 61

Max Continuous Load per Generator

Answer 61

100% | 90KVA

Question 62

Max Continuous Load per TR

Answer 62

200 A

Question 63

For JET A only, if TAT reaches...,monitor the FUEL SD page that the fuel temp remains higher than...

Answer 63

-34C, -36C

Question 64

Minimum Fuel Quantity for Takeoff

Answer 64

3,307 lb and the WING TK LO LVL warning must not be displayed on the ECAM

Question 65

Fuel Management, tanks must be emptied in the following order: N502NK-N536NK, N601NK-N628NK

Answer 65

Center tank then wing tanks | Takeoff on center tank is prohibited

Question 66

Hydraulic normal operating pressure

Answer 66

3,000psi +/- 200

Question 67

Taxi with deflated Tires | If one tire is deflated on one or more gears( maximum of 3 tires) Speed should be limited to

Answer 67

7kts

Question 68

Taxi with deflated Tires If two tires are deflated in the same main gear(the other main gear tires not being deflated) Speed should be limited to...and nose wheel steering angle limited to...

Answer 68

3kt and 30*

Question 69

Nosewheel steering limits with hand wheels and for towing and pushback

Answer 69

75* when using hand wheels | 95* for towing and pushback

Question 70

Tail Strike Pitch Attitude A319 (Struts Compressed)

Answer 70

13.9*

Question 71

Tail Strike Pitch Attitude A320 (Struts Compressed)

Answer 71

11.7*

Question 72

Tail Strike Pitch Attitude A321 (Struts Compressed)

Answer 72

9.7*