Operating Limitations (Bold/Bonus)

Question 1

(Bonus)
Flight Maneuvering Load Limit:
Clean-
Other Configurations (Slats and/or Flaps Extended) -

Answer 1

• 1.0g to +2.5g

0. 0g to +2.0g

Question 2

Approach Category A320/321NEO

Answer 2

Category C

Question 3

Approach Category A321 ceo

Answer 3

Category D

Question 4

Max Crosswind

Answer 4

TO - 35kts

Landing - 38kts

Question 5

Max Tailwind Takeoff

Answer 5

A320/321NEO - 15kts

A321CEO - 10kts

Question 6

Max Tailwind Landing

Answer 6

ALL A/C - 10kts

Question 7

(Bonus) Runway Width Limitations

Answer 7

Normal Runways - 148 ft.

Minimum Runway Width - 100ft

Question 8

(Bonus) Max Runway Slope

Answer 8

-/+ 2%

Question 9

(Bonus) Max Pressure Alt for TO & LNDG

Answer 9

9200ft

Question 10

(Bonus) Minimum Runway Width

Answer 10

AC 227-229 & 601-699
100FT

All Other
148ft

Question 11

(Bonus) Max Wind for Passenger Door Operation

Answer 11

65kts

Question 12

(Bonus) Max wind for Cargo Door Operations

Answer 12

40kts / 50kts

50kts if nose of plane is oriented into the wind or cargo door is leeward of wind.

FWD/AFT Cargo doors must be closed before 65kts.

Question 13

(Bonus) VMO/MMO

Answer 13

350KIAS / .82 Mach

Question 14

(Bonus) VLO (Retraction)

Answer 14

220kts / 0.54 Mach

Question 15

(Bonus) VLO (Extension)

Answer 15

250kts / 0.60 Mach

Question 16

(Bonus) VLE (Extended)

Answer 16

280kts / 0.67 Mach

Question 17

Max Tire Speed

Answer 17

195kts Groundspeed

Question 18

Max Windshield Wiper Operation Speed

Answer 18

230 KIAS

Only for sweeping wipers

Question 19

Max Cockpit Window Speed

Answer 19

200 KIAS

Question 20

Max Taxi Speed in a turn - A/C 205-299

Answer 20

(greater than 167,550 lbs)

A/C 205-299 - 20kts during a turn

Question 21

Maximum Flaps/Slats Extended Altitude

Answer 21

20,000ft MSL

Question 22

(Bonus) Max Landing Weight 321NEO

Answer 22

174,606 lbs

Question 23

(Bonus) Max landing weight 320

Answer 23

142,198 lbs / 148,591 lbs (NEO)

Question 24

(Bonus) Max landing weight 321CEO

Answer 24

171,520 lbs

Question 25

Stabilized Approach Policy

Answer 25

1000ft: 1. Rate of Descent 1200FPM or less 2. One dot ILS/LOC or .30 NM RNAV (Lateral) 3. Glidepath ONE DOT (Vertical) 4. Final Configuration 5. NO GPWS Warnings and Cautions 500 FT: 1. Rate of Descent 1000FPM or less 2. Speed -5 to +15 KTS. 3. Thrust Stabilized, usually above idle, commensurate with power required to maintain speed 4. Landing checklist complete

Question 26

(Bonus) T.O Inhibit duration?

Answer 26

1500 ft or 2 min after liftoff

Question 27

(Bonus) LDG Inhibit duration?

Answer 27

Below 800ft till 80kts

Question 28

(Bonus) Max Operational Pressure Altitude

Answer 28

39,800ft

Question 29

(Bonus) Landing on Narrow Runways

Answer 29

Autoland is not authorized Dispatch from/to narrow runways not allowed in case of: NWS inop, one or more brake inop. Diversion to normal width runways (148ft) recommended in case of: Rudder Jam, rudder pedal jam, yaw damper system fault, rudder travel limit system fault, all failures leading to loss of NWS(yellow sys loss, double hydraulic/BSCU/LGCIU faults)

Question 30

Max Altitiude to start the APU using battery power only?

Answer 30

25,000ft

Question 31

What is the A/P minimum engagement height after TO (if SRS is indicated)?

Answer 31

100ft AGL and at least 5s after liftoff.

Question 32

What is the A/P min engagment height enroute?

Answer 32

900ft AGL

Question 33

At what height must the A/P be turned off for an RNAV Visual App?

Answer 33

500ft AGL

Question 34

At what height must the A/P be turned off for NON-Precision APP?

Answer 34

DDA/DA

Question 35

At what height must the A/P be turned off a non-autoland ILS with CAT 1 FMA?

Answer 35

160ft AGL

Question 36

At what height must the A/P be turned off for a non-autoland ILS with CAT 2/3 FMA?

Answer 36

80ft AGL

Question 37

When must the A/P be turned off after an autoland app?

Answer 37

ROLLOUT/Taxi Speed

Question 38

When is autoland required?

Answer 38

Autoland is required below CAT 1 mins. Or if the reported RVR/Visibility is at or below 1/2 mile or 2400RVR and for all the requirements to be met (environmental, aircraft, ground equip, and crew).

Question 39

What is the maximum time limit to use TOGA thrust with all engines running? How about of one engine inop?

Answer 39

5 Min - 2Eng 10 Min - Single Engine

Question 40

Takeoff at reduced thrust is proibited when?

Answer 40

1. On slippery or contaminated runways 2. When suspected, reported, or known windshear is present. 3. When a special departure procedure specifies full thrust for TO.

Question 41

What is the max altitude to start the APU using battery power only?

Answer 41

FL250

Question 42

Max time for using TOGA with 2 ENG? What about 1 ENG?

Answer 42

5 min (2 engine) 10 mins (single engine)

Question 43

Takeoff at reduced thrust is prohibited:

Answer 43

A. On Slippery or Contaminated runways B. When suspected, reported or known wind shear is present (Predictive wind shear alerts, ATC issued alerts) C. When a Special Departure Procedure specifies full thrust for takeoff.