Operating Limitations (BOLD) Flashcards

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1
Q

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

A
  • 1.0g to +2.5g

0. 0g to +2.0g

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2
Q

Approach Category A320/321NEO

A

Category C

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3
Q

Approach Category A321

A

Category D

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4
Q

Max Crosswind

A

TO - 35kts

Landing - 38kts

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5
Q

Max Tailwind Takeoff

A

A320/321NEO - 15kts

A321CEO - 10kts

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6
Q

Max Tailwind Landing

A

ALL A/C - 10kts

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7
Q

(Bonus) Runway Width Limitations

A

Normal Runways - 148 ft.

Minimum Runway Width - 100ft

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8
Q

(Bonus) Max Runway Slope

A

-/+ 2%

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9
Q

(Bonus) Max Pressure Alt for TO & LNDG

A

9200ft

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10
Q

(Bonus) Minimum Runway Width

A

AC 227-229 & 601-699
100FT

All Other
148ft

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11
Q

(Bonus) Max Wind for Passenger Door Operation

A

65kts

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12
Q

(Bonus) Max wind for Cargo Door Operations

A

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.

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13
Q

(Bonus) VMO/MMO

A

350KIAS / .82 Mach

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14
Q

VLO (Retraction)

A

220kts / 0.54 Mach

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15
Q

VLO (Extension)

A

250kts / 0.60 Mach

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16
Q

VLE (Extended)

A

280kts / 0.67 Mach

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17
Q

Max Tire Speed

A

195kts Groundspeed

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18
Q

Max Windshield Wiper Operation Speed

A

230 KIAS

Only for sweeping wipers

19
Q

Max Cockpit Window Speed

A

200 KIAS

20
Q

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

A

(greater than 167,550 lbs)

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

21
Q

Maximum Flaps/Slats Extended Altitude

A

20,000ft MSL

22
Q

Max Landing Weight 321NEO

A

174,606 lbs

23
Q

Max landing weight 320

A

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

24
Q

Max landing weight 321

A

171,520 lbs

25
Q

Stabilized Approach Policy

A

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
26
Q

(Bonus) T.O Inhibit duration?

A

1500 ft or 2 min after liftoff

27
Q

(Bonus) LDG Inhibit duration?

A

Below 800ft till 80kts

28
Q

(Bonus)
Max Operational Pressure Altitude

A

39,800ft

29
Q

Landing on Narrow Runways

A

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)

30
Q

Speed Brake Limitation

A

Use of speed brakes at or below 240kts is not permitted if:

  • GWCG is above 35% or
  • In overweight landing conditions.
31
Q

Max Altitiude to start the APU using battery power only?

A

25,000ft

32
Q

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

A

100ft AGL and at least 5s after liftoff.

33
Q

What is the A/P min engagment height enroute?

A

900ft AGL

34
Q

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

A

500ft AGL

35
Q

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

A

DDA/DA

36
Q

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

A

160ft AGL

37
Q

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

A

80ft AGL

38
Q

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

A

ROLLOUT/Taxi Speed

39
Q

When is autoland required?

A

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).

40
Q

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

A

5 Min - 2Eng
10 Min - Single Engine

41
Q

Takeoff at reduced thrust is proibited when?

A
  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.
42
Q

(Bonus) VLO Max retract speed

A

220kts/.54 Mach

43
Q

(Bonus) VLO Max Extend

A

250kts / .60 Mach

44
Q

(Bonus) VLE

A

280 kts / .67 Mach