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FRONTIER AIRLINES > Limitations > Flashcards

Limitations Flashcards

1
Q

MANEUVERING G-LOAD

A
  • Clean configuration . . . . . - 1 g to + 2.5 g

* Slats and/or flaps extended . . . . . 0 g to + 2 g

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2
Q

APPROACH CATEGORY (bold)

A

A320 Category C

A321 Category D

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3
Q

STABILIZED APPROACH POLICY

A

1000’ to 500’ AFE
• Rate of descent not to exceed 1,200 FPM
• Lateral path ± one dot for ILS/LOC, 0.30 NM cross track for RNAV, or 1/2 dot for VOR
• Vertical path ± one dot
• Landing Gear, Flaps Extended, Speed brakes retracted
• Absent any GPWS Warnings and Cautions

500’ to 0’ AFE
• Rate of descent not to exceed 1,000 FPM
• Within -5 to +15 knots of target speed for approach
• Thrust stabilized to maintain target speed

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4
Q

Runway slope (maximum)

A

+-2%

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5
Q

Minimum runway width

A

148 ft/ 45m

100ft/ 30m (A/C 227, 228, 229)

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6
Q

Maximum X-wind for T/O (bold)

A

• 35 kt (gust included)

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7
Q

Maximum X-wind for Landing (bold)

A

• 38 kts (Gust included)

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8
Q

Maximum tailwind for takeoff (bold)

A
  • A320 is 15kts

* A321 is 10kts

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9
Q

Maximum tailwind for landing (bold)

A

10kts

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10
Q

Maximum wind for passenger door operation (bold)

A

65 kt

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11
Q

Maximum wind for cargo door operation (bold)

A

40 kt (up to 50 kt when Airplane into the wind)

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12
Q

Maximum VMO/MMO

A

350 kt/.82 mach

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13
Q

SEVERE TURBULENT AIR PENETRATION

SPEED (bold)

A
  • FL200 and below. . . . 250 kt (270kt - A321)
  • Above FL200 through FL310 . . .275 kt (300 kt -A321)
  • Above FL310 . . . . . . . . . . . . 0.76 mach

.

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14
Q

Maximum speed at which the landing gear may be extended (VLO extension)

A

250 kts/0.60 Mach

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15
Q

Maximum speed at which the landing gear may be retracted (VLO retraction)

A

220 kts/0.54 Mach

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16
Q

Maximum speed with landing gear extended (VLE)

A

280 kts/0.67 Mach

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17
Q

MAXIMUM TIRE SPEEDS (bold)

A

Max Ground speed 195 kts

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18
Q

WINDSHIELD WIPERS IN USE (bold)

A

230 kts

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19
Q

COCKPIT WINDOW OPEN (bold)

A

200 kts

20
Q

TAXI SPEED (A320 AND 321) (bold)

A

Do not exceed 20 kts in turn if weight is > 167,550 lbs ( 76 Tons 😏)

21
Q

TAKEOFF and GO-AROUND engine time limit? (bold)

A 
5 min
10 min (Only in case of engine failure)
22
Q

Minimum oil quantity is? (bold)

A

CEO- 9.5qt + .5qt per every hour of ETE

NEO- The highest of: 10.6 qts or 9.0qt + .5qt per every hour of ETE

23
Q

Maximum brake temperature for takeoff with (brake fans off)

A

300° C

24
Q

What is a Narrow Runway (bold)

A

A narrow runway is any runway less than 148 ft/45m wide.

25
Q

Takeoff at reduced thrust is prohibited: (bold)

A

1) On slippery or contaminated runways;
2) When suspected, reported or known windshear
3) When a Special Departure Procedure specifies full thrust for takeoff.
4) Performance
5) Thrust reduction must not exceed 25% of the full rated takeoff thrust

26
Q

Minimum oil temperature for takeoff? (bold)

A

19°

27
Q

Max operating altitude with slats and/or flaps extended (bold)

A

FL200

28
Q

AUTOPILOT ENGAGEMENT: After Takeoff/Go-Around (If SRS is indicated) (bold)

A

100 AGL

29
Q

AUTOPILOT ENGAGEMENT: Enroute (bold)

A

900 AGL

30
Q

AUTOPILOT ENGAGEMENT: RNAV Visual Approach (bold)

A

500 AGL

31
Q

AUTOPILOT ENGAGEMENT: Non-Precision Approaches (bold)

A

DDA/ DA

32
Q

AUTOPILOT ENGAGEMENT: Non-Autoland ILS with CAT 1 FMA (bold)

A

160 AGL

33
Q

AUTOPILOT ENGAGEMENT: Non-Autoland ILS with CAT 2/3 FMA (bold)

A

80 AGL

34
Q

AUTOPILOT ENGAGEMENT Autoland ILS Approach (one or two autopilots) (bold)

A

Rollout/Taxi Speed

35
Q

Autoland Required: (bold)

A

Autoland is required below CAT I minimums.

Furthermore, to minimize the chances of a go around, Frontier policy is to set up and brief for an autoland IF the reported RVR/visibility is at or below 1/2 mile or 2400 RVR 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.

NOTE: 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.

36
Q

Maximum altitude for APU battery start

A

FL250

37
Q

The use of AP or FD in OPEN DES or DES mode is not permitted on approach when?

A

inside the FAF or Below 1000 ft AGL on a visual approach.

38
Q

Autolands are prohibited if braking action is reported

A

Less than medium.

39
Q

Autoland Autobrakes. Use “Medium” for runway less than:

A

8,000 feet long

Note: (Low or Medium for 8,000 or longer) Autobrakes (if available) are required for all CAT III approaches.

40
Q

Maximum reverse will not be used below

A

70 knots

41
Q

AUTOLAND WIND RESTRICTIONS

A
  • 30 knots of Headwind
  • 15 knots of Crosswind
  • 10 knots of Tailwind

Wind Correction: Vls + wind correction 5 to 15 knots.

At approach speed (VAPP)=VLS+wind correction Minimum wind correction 5kt, maximum wind correction 15kt.

42
Q

Maximum Runway altitude (Autoland)

A

A320: 9200 ft
A321: 5750 ft

43
Q

Ram Air Inlet only open if differential pressure is

A

Lower that 1 PSI

44
Q

DERIVED DECISION ALTITUDE (DDA)

A

DDA is calculated by adding 50’ to the published MDA

45
Q

SPEED BRAKES LIMITATION (NEO)

A

For approach, the use of​ speed brakes at​ or​ below 240 kt is not permitted if:

  • GWCG is above 35% or
  • In overweight landing conditions

FRONTIER AIRLINES (9 decks)

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