LIMITATIONS

Question 1

WINGSPAN, Non-Sharklet

A319, A320

Answer 1

111 feet, 10 inches

Question 2

WINGSPAN, Sharklet

A320, A321

Answer 2

117 feet, 5 inches

Question 3

GROUND CLEARANCE TABLE
Tailstrike Pitch Attitude.

L/G Struts Compressed

A319
A320
A320 NEO
A321

Answer 3

A319 - 13.9

A320 - 11.7

A320 NEO - 11.7

A321 - 9.7

Question 4

MAXIMUM CERTIFIED ALTITUDE

Answer 4

FL398

Question 5

RUNWAY SLOPE (mean)

Answer 5

+- 2%

Question 6

RUNWAY ALTITUDE

Answer 6

9,200 ft

Question 7

NOMINAL RUNWAY WIDTH

Answer 7

45 m (148 ft)

Question 8

MAXIMUM DEMONSTRATED CROSSWIND (takeoff and landing)

Answer 8

38 kt (gust included)

Question 9

MAXIMUM TAILWIND FOR TAKEOFF

Answer 9

15 kt

Question 10

MAXIMUM TAILWIND FOR LANDING

Answer 10

10 kt

Question 11

MAXIMUM WIND FOR PASSENGER DOOR OPERATION

Answer 11

65 kt

Question 12

MAX W/ LANDING GEAR EXTENDED (VLE)

Answer 12

280 kt/M.67

Question 13

MAX LANDING GEAR EXTENSION (VLO Extension)

Answer 13

250 kt/M.60

Question 14

MAX LANDING GEAR RETRACTION (VLO Retraction)

Answer 14

220 kt/M.54

Question 15

MAX ALTITUDE LANDING GEAR MAY BE EXTENDED

Answer 15

25,000 ft

Question 16

WIPERS MAXIMUM OPERATING SPEED

Answer 16

230 kt

Question 17

APPLICABLE TO 601NK THRU N696NK

When the taxi weight is higher than___________:
Caution: Do not exceed a taxi speed of ____kt during a turn

Answer 17

167,550

20

Question 18

APPLICABLE TO N502NK THRU N536NK

MAX LANDING

Answer 18

137,788

Question 19

APPLICABLE TO N601NK THRU N656NK, N690NK THRU N696NK

MAX LANDING

Answer 19

145,505 lb

Question 20

APPLICABLE TO N901NK THRU N915NK

MAX LANDING

Answer 20

148,591

Question 21

APPLICABLE TO N657NK THRU N687NK

MAX LANDING

Answer 21

171,519

Question 22

APU BLEED USE WITH AIR START UNIT

Answer 22

The flight crew must not use bleed air from the APU BLEED and from the HP Air Unit at the same time, to prevent any adverse effect on the Bleed Air System.

Question 23

CABIN PRESSURE

MAX POSITIVE DIFFERENTIAL

MAX NEGATIVE DIFFERENTIAL

Answer 23

9. 0 PSI

- 1.0 PSI

Question 24

PACKS USE WITH LP AIR CONDITIONING UNIT

Answer 24

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent any adverse effect on the Air Conditioning System.

Question 25

MINIMUM HEIGHT FOR USE OF AUTOPILOT TAKEOFF WITH SRS MODE

Answer 25

100 ft AGL

Question 26

MINIMUM HEIGHT FOR USE OF AUTOPILOT STRAIGHT-IN NON-PRECISION APPROACH

Answer 26

Applicable Minimum

Question 27

MINIMUM HEIGHT FOR USE OF AUTOPILOT CIRCLING APPROACH

Answer 27

Applicable Minimum -100 ft

Question 28

MINIMUM HEIGHT FOR USE OF AUTOPILOT ILS APPR WHEN CAT 2 OR CAT 3 IS NOT DISPLAYED ON THE FMA

Answer 28

160 ft AGL

Question 29

MINIMUM HEIGHT FOR USE OF AUTOPILOT GO-AROUND (AP OR FD ENGAGEMENT)

Answer 29

100 ft AGL

Question 30

MINIMUM HEIGHT FOR USE OF AUTOPILOT ALL OTHER PHASES

Answer 30

500 ft AGL (319/320) | 900 ft AGL (321)

Question 31

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 31

Highest of: Minimum or 500 ft (319/320) Minimum or 900 ft (321)

Question 32

USE OF NAV MODE: IN THE TERMINAL AREA

Answer 32

NAV mode may be used in the terminal area provided that: - GPS Primary is available, or - The appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or - FMS navigation is crosschecked with navaid raw data

Question 33

APPLICABLE TO N502NK THRU N536, N657NK THRU N687NK Non-Precision Approaches with Engine-Out

Answer 33

If one engine is inoperative, it is not permitted to use the autopilot to perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/FPA Only FD use is permitted

Question 34

APU START

Answer 34

After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt

Question 35

POWER PLANT Thrust Setting/EGT Limits Applicable to N502NK THRU N656NK, N690NK THRU N696NK

Answer 35

Takeoff and Go-around All engines operative 5 min One engine inoperative 10 min 635C MCT 610C Starting, On Ground In Flight 635C

Question 36

POWER PLANT Thrust Setting/EGT Limits APPLICABLE TO N657NK THRU N687NK

Answer 36

Takeoff and Go-around All engines operative 5 min One engine inoperative 10 min 650C MCT 610C Starting, On ground In flight 635C

Question 37

POWER PLANT Thrust Setting/EGT Limits APPLICABLE TO N901NK THRU N915NK

Answer 37

Takeoff and Go-around All engines operative 5 min One engine inoperative 10 min 1083C MCT 1043C Starting, On ground In flight 1083C

Question 38

OIL APPLICABLE TO N502NK THRU N696NK Minimum starting temp: Minimum temperature before IDLE is exceeded

Answer 38

- 40 | - 10

Question 39

OIL APPLICABLE TO N901NK THRU N915NK Minimum Oil Pressure

Answer 39

65 PSI

Question 40

STARTER | APPLICABLE TO N502NK THRU N696NK

Answer 40

- A standard automatic start that includes only one start attempt, is considered one cycle - For ground starts (automatic or manual), a 15s pause is required between successive cycles - A 30 min cooling period is required, subsequent to three failed cycles or 5 min of continuous crank - For manual start, observe a two-minute max cycle time - For crank, observe a 5 min max cycle time - The starter must not be run when N2 is above 10% on-ground and 18% in-flight.

Question 41

STARTER | APPLICABLE TO N901NK THRU N915NK

Answer 41

- A standard automatic start that includes up to three start attempts, is considered one cycle - For ground starts (automatic or manual), a 35s pause is required between successive cycles. - A 15 min cooling period is required, subsequent to three failed cycles, or 15 min of continuous or cumulated crank. - The starter must not be run when N2 is above 20%

Question 42

Reverse Thrust | APPLICABLE TO N901NK THRU N915NK

Answer 42

Maximum reverse should not be used below 70kt. Idle reverse is permitted down to aircraft stop.

Question 43

Reduced Thrust Takeoff | Applicable to all A/C

Answer 43

FLEX takeoff is not permitted on contaminated runways

Question 44

Crosswind operation On Ground | Engine Start

Answer 44

The engine is able to start in crosswind up to 35 kt.

Question 45

Flight Controls Maximum altitude Flaps/Slats Extended Maximum operating altitude with slats and/or flaps extended

Answer 45

20,000 ft

Question 46

Fuel Temperature

Answer 46

For Jet A only, if TAT reaches -34 C, monitor on FUEL SD page that fuel temperature remains higher than -36C.

Question 47

Maximum Allowed Wing Fuel Imbalance APPLICABLE TO N618NK THRU N656NK, N690NK THRU N696NK, N901NK THRU N915NK (320 SHARKLET) Fuel Imbalance at takeoff, maximum asymmetry Fuel imbalance In Flight and At Landing, maximum asymmetry

Answer 47

1102 lb 3306 Ib

Question 48

Maximum Allowed Wing Fuel Imbalance APPLICABLE TO N657NK THRU N687NK (A321 SHARKLET) Fuel Imbalance at takeoff, maximum asymmetry

Answer 48

882 Ib

Question 49

BRAKE TEMPERATURE Maximum brake temperature for takeoff

Answer 49

300C