Bold Limits - Rev 92 03/24/25 Flashcards

(29 cards)

1
Q

Are you permitted to start the APU during refueling? If a fuel spill occurs and the APU is running, what should you do?

A

During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:

  • If the APU failed to start or following an automatic APU shutdown, do not start the APU
  • If a fuel spill occurs, perform a normal APU shutdown.

Aircraft System Limitations 2.10 p.2

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2
Q

Are you permitted to use the APU if the LOW OIL LEVEL advisory is displayed on the ECAM? When is maintenance action required? Is a logbook entry required?

A

The APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed. Maintenance action is required within the next 10 hours of APU operation.

NOTE: A logbook entry is not required after receiving this advisory message. Contact MCC to determine the status of required maintenance action.

Aircraft System Limitations 2.10 p.2

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3
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with CAT 1 FMA?

A

160 AGL

Aircraft System Limitations 2.10 p.3

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4
Q

At what height must the autopilot be turned off for a Non-Autoland ILS with CAT 2/3 FMA?

A

80 AGL

Aircraft System Limitations 2.10 p.3

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5
Q

At what height must the autopilot be turned off for an RNAV VISUAL APPROACH?

A

500 feet AGL

Aircraft System Limitations 2.10 p.3

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6
Q

At what height must the autopilot be turned off for Non-Precision Approaches?

A

DDA/DA

Aircraft System Limitations 2.10 p.3

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7
Q

If one or more of the autoland requirements cannot be met, may an approach still be conducted if the weather is below 1/2 mile or 2400 RVR?

A

Yes, if one of the autoland requirements cannot be met (e.g. strong crosswind) a non-autoland CAT I approach may be conducted down to our lowest authorized CAT I minimums (i.e. 1800 RVR or as published).

Aircraft System Limitations 2.10 p.5

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8
Q

Is takeoff with center tank fuel supplying the engines permitted?

A

Takeoff with center tank fuel supplying the engines is PROHIBITED.

Aircraft System Limitations 2.10 p.12

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9
Q

For 201-299 the maximum taxi speed when making a turn is ___ when the aircraft weight is greater than _____?

A

20 kt

167,550lbs

General Limitations 2.5 p.7

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10
Q

What are the maximum cross wind limitations for takeoff and landing?

A

Takeoff: 35kts

Landing: 38kts

General Limitations 2.05 p.2

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11
Q

What are the maximum tailwind limitations for takeoff and landing?

A

Takeoff for 201-299, 301-399, 601-699: 15kts

Takeoff for 701-799: 10kts

Landing for all aircraft: 10kts

General Limitations 2.05 p.2

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12
Q

What is Frontier’s stabilized approach policy?

A

At 1,000 AFE:

  • Steady rate of descent not to exceed 1,200FPM
  • On correct lateral path (1 dot ILS/LOC, .3NM RNAV or 1/2 dot VOR)
  • On the correct vertical path (1 dot)
  • In the final landing configuration (Gear & Flaps Extended, Speed Brakes Retracted)
  • Absent any GPWS Warnings and Cautions

At 500 AFE:

  • Landing Checklist Completed
  • Steady rate of descent not to exceed 1,000FPM
  • Within -5 to +15 knots of target speed for approach
  • Thrust Stabilized, usually above idle, commensurate with what is required to maintain the target speed criteria

GeneralLimitations 2.05 p.2

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13
Q

What is the approach category of the A320 and A321?

A

A320CEO, A320NEO and A321NEO - Category C

A321CEO - Category D

General Limitations 2.05 p.1

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14
Q

What is the autopilot minimum engagement height after takeoff (if SRS is indicated)?

A

100 feet AGL and at least 5 seconds after liftoff

Aircraft System Limitations 2.10 p.3

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15
Q

What is the autopilot minimum engagement height enroute?

A

900 feet AGL

Aircraft System Limitations 2.10 p.3

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16
Q

What is the maximum altitude that the Flaps or Slats may be extended?

A

20,000 feet MSL

Aircraft System Limitations 2.10 p.9

17
Q

What is the maximum altitude to start the APU using battey power only (Elec Emerg Config)?

A

25,000 feet MSL

Aircraft System Limitations 2.10 p.2

18
Q

What is the maximum time limit to use TOGA thrust with all engines operating? How about if one engine is inoperative?

A

All Engines Operating: 5 min

One Engine Inop: 10 min

Aircraft System Limitations 2.10 p.7

19
Q

What is the maximum tire speed?

A

195 kts (groundspeed)

General Limitations 2.05 p.6

20
Q

What is the maximum windshield wiper operation speed?

A

230 KIAS

General Limitations 2.05 p.6

21
Q

What is the minimum height the autopilot can be engaged during a Go-Around (if SRS is indicated)?

A

100 AGL

Aircraft System Limitations 2.10 p.3

22
Q

(Non-Memory)
What is VMO/MMO for the A320/A321?

A

350kt/0.82 Mach

General Limitations 2.05 p.6

23
Q

What is the maximum aircraft speed with the cockpit window open?

A

200 KIAS

General Limitations 2.05 p.6

24
Q

When is an autoland required?

A

Autoland is required below CAT I minimums.

Furthermore, to minimize the chances of a go around, Frontier’s policy is to set up and brief for an autoland IF the reported RVR/visibility is at or below 1/2 mile or 2400RVR AND all of the requirements for an autoland can be met (environmental, aircraft approach capability, ground equipment, etc.), the approach will be briefed and flown as a CAT II or CAT III autoland.

Aircraft System Limitations 2.10 p.5

25
When must the autopilot be turned off after an autoland approach?
ROLLOUT/Taxi Speed ## Footnote Aircraft System Limitations 2.10 p.3
26
When is a takeoff with reduced thrust prohibited?
* On slippery or contaminated runway * When suspected, reported or known windshear is present (e.g. predictive windshear alerts, or ATC issued windshear alerts for the departure runway or departure path) * When a Special Departure Procedure specifies full thrust for takeoff ## Footnote Aircraft System Limitations 2.10 p.9
27
(Non-Memory) What is the maximum speed at which the landing gear may be extended (VLO Extension)?
250kts/0.60 Mach ## Footnote General Limitations 2.05 p.6
28
(Non-Memory) What is the maximum speed while the landing gear is extended (VLE Extended)?
280kts/0.67 Mach ## Footnote General Limitations 2.05 p.6
29
(Non-Memory) What is the maximum speed that the landing gear may be retracted (VLO Retraction)?
220kts/0.54 Mach ## Footnote General Limitations 2.05 p.6