Limitations - Dec '22

Question 1

A319/A320 Wingspan

Answer 1

111ft 10in.

Question 2

A320/A321 with Sharklets wingspan

Answer 2

117ft 5in

Question 3

A319 tail clearance (struts compressed)

Answer 3

13.9°

Question 4

A320 tail clearance (struts compressed)

Answer 4

11.7°

Question 5

A321 tail clearance (struts compressed)

Answer 5

9.7°

Question 6

Maximum Certified Altitude

Answer 6

FL 398

Question 7

Maximum runway slope (mean)

Answer 7

+/- 2%

Question 8

Maximum runway altitude

Answer 8

9,200ft

Question 9

Nominal runway width

Answer 9

45m (148ft)

Question 10

Maximum demonstrated crosswind (including gust)

Answer 10

38kts

Question 11

Maximum tailwind for take-off

Answer 11

15kts

Question 12

Maximum tailwind for landing

Answer 12

10kts

Question 13

Maximum wind for passenger door operation

Answer 13

65kts

Question 14

Maximum window open speed

Answer 14

200kts

Question 15

VMO/MMO

Answer 15

350kts/0.82M

Question 16

Maximum tire speed

Answer 16

195kts (ground speed)

Question 17

Maximum speed with landing gear extended (VLE)

Answer 17

280kts/0.67M

Question 18

Maximum speed for gear extension (VLO EXT)

Answer 18

250kts/0.60M

Question 19

Maximum speed for gear retraction (VLO RET)

Answer 19

220kts/0.54M

Question 20

Maximum altitude with gear extended

Answer 20

25,000ft

Question 21

Maximum taxi speed in a turn with weight above 167,550lbs

Answer 21

20kts

Question 22

Maximum wiper operating speed

Answer 22

230kts

Question 23

Maximum positive pressure differential

Answer 23

9.0PSI

Question 24

Maximum negative pressure differential

Answer 24

-1.0PSI

Question 25

Use of APU bleed air and HP Air start cart

Answer 25

Prohibited

Question 26

Use of PACKS with LP conditioned air connected

Answer 26

Prohibited

Question 27

Max Landing Weight (N502NK thru N536NK) (A319)

Answer 27

137,788 lbs

Question 28

Max Landing Weight (N601NK thru N617NK) (A320 - NonSharklet)

Answer 28

145,505 lbs

Question 29

Max Landing Weight (N618NK thru N656NK, N690NK thru N694NK) (A320 - Sharklet)

Answer 29

145,505 lbs

Question 30

Max Landing Weight (N901NK thru N974NK) (A320Neo)

Answer 30

148,591 lbs

Question 31

Max Landing Weight (N657NK thru N687NK) (321 - Sharklet)

Answer 31

171,519 lbs

Question 32

Min height for AP engagement - T/O with SRS mode

Answer 32

100ft AGL

Question 33

Min height for AP engagement - straight-in non-precision approach *****CANT FIND in COM*****

Answer 33

Applicable Minimums

Question 34

Min height for AP engagement - circling approach

Answer 34

600 ft

Question 35

Min height for AP engagement - ILS (CAT 2 or 3 not displayed in FMA)

Answer 35

160ft AGL

Question 36

Min height for AP or FD engagement – Go-around

Answer 36

100ft AGL

Question 37

Min height for AP engagement for all other phases of flight

Answer 37

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

Question 38

Use of AP or FD in OP DES or DES mode is not permitted in approach unless the FCU altitude is set at or above:

Answer 38

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

Question 39

Take-off with SRS mode – An internal FMGS logic prevents the AP from engaging during:

Answer 39

The fist 5 seconds after lift off

Question 40

After three APU start attempts, the crew must wait:

Answer 40

60 minutes

Question 41

Minimum oil temperature for start

Answer 41

-40°C

Question 42

Minimum oil temperature before exceeding IDLE

Answer 42

-10°C

Question 43

Minimum oil temperature for take-off (CEO)

Answer 43

50°C

Question 44

Minimum oil temperature for take-off (NEO)

Answer 44

52°C

Question 45

Minimum oil pressure (CEO)

Answer 45

60PSI

Question 46

Minimum oil pressure (NEO)

Answer 46

65PSI

Question 47

Maximum crosswind for engine start

Answer 47

35kts

Question 48

Maximum altitude for slats or flaps

Answer 48

20,000ft

Question 49

Maximum fuel imbalance at T/O for inner tanks (A319/A320)

Answer 49

1,102 lbs

Question 50

Maximum fuel imbalance at T/O for inner tanks (N657NK thru N687NK) (A321)

Answer 50

882 lbs

Question 51

Maximum fuel imbalance for landing and in-flight (A319/A320)

Answer 51

3,306 lbs

Question 52

Maximum fuel imbalance for landing and in-flight (N657NK thru N687NK) (A321)

Answer 52

2,910 lbs

Question 53

Maximum brakes temperature for T/O without brake fans?

Answer 53

300°C

Question 54

Use of FLEX on a contaminated runway

Answer 54

Prohibited

Question 55

FLEX thrust is prohibited when the OAT is within

Answer 55

10°C of the FLEX Temp

Question 56

Maximum reverse thrust use is not allowed below

Answer 56

70kts

Question 57

IDLE thrust reverse is permitted down to

Answer 57

Aircraft stop

Question 58

APU Max Altitude for bleed air extraction (Single PACK)

Answer 58

20,000ft

Question 59

APU Max Altitude for bleed air extraction (Both PACKs)

Answer 59

15,000ft

Question 60

**Thrust setting EGT Limits (N502NK thru N656NK, N690NK thru N698NK) [A319/A320]** -All engine operating – T/O & Go-around -One engine inoperative – T/O & Go-around -Max Continuous Thrust -Engine Start

Answer 60

-635°C -635°C -610°C -635°C

Question 61

**Thrust setting EGT Limits (N657NK thru N687NK) [A321]** -All engine operating – T/O & Go-around -One engine inoperative – T/O & Go-around -Max Continuous Thrust -Engine Start

Answer 61

-650°C -650°C -610°C -635°C

Question 62

**Thrust setting EGT Limits (N901NK thru N974NK) [A320neo]** -All engine operating – T/O & Go-around -One engine inoperative – T/O & Go-around -Max Continuous Thrust -Engine Start

Answer 62

-1083°C -1083°C -1043C -1083°C

Question 63

**Thrust setting time limit** -All engines operating – T/O & Go-around thrust time limit -One engine inoperative – T/O & Go-around thrust time limit -Max Continuous Thrust time limit

Answer 63

-5 Minutes -10 Minutes -No Time Limit

Question 64

Fuel Temp Restrictions for Jet-A

Answer 64

If the TAT reaches -34°C, monitor the fuel SD page, the fuel temperature must remain above -36°C

Question 65

NAV mode maybe used in the terminal area provided that:

Answer 65

- GPS Primary is available, or - Required RNP is checked or entered in the MCDU and high accuracy is displayed, or - FMS navigation is crosschecked with raw data

Question 66

If one engine is inoperative, use of the AP is not permitted to perform non-precision approaches in the following modes (use of FD is permitted)

Answer 66

- FINAL APP - NAV V/S - NAV FPA

Question 67

**Starter Limits (N502NK thru N698NK) [CEO]** A standard automatic start that includes only **XX** start attempt is considered one cycle. For ground starts (automatic or manual), a **XX** second pause is required between successive cycles. A **XX** minute cooling period is required, subsequent to **XX** failed cycles or **XX** minutes of continuous crank. For manual start, observe a **XX** minute maximum cycle time For crank, observe a **XX** minute maximum cycle time The starter must not run when the N2 is above **XX** on the ground and **XX**% in flight

Answer 67

-One -15 Second -30 Minute -3 Failed Cycles -5 Min Cont. Crank -2 Min max cycle for man. Start -5 Min max cycle time for crank -10% N2 on Ground -18% N2 in flight

Question 68

**Starter Limits (N901NK thru N974NK) [NEO]** A standard automatic start that includes up to **XX** start attempts is considered one cycle. For ground starts (automatic or manual), a **XX** seconds pause is required between successive cycles. A **XX** minute cooling period is required subsequent to **XX** failed cycles, or **XX** minutes of continuous or cumulative crank. The starter must not be run when the N2 is above **XX**%

Answer 68

-Two -35 Second pause -15 minute -3 Failed cycles -15 Min. continous or cumulative crank -20% N2 ground/flight

Question 69

Minimum height for autopilot: In approach with Final APP, V/S, or FPA mode:

Answer 69

250ft AGL