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)

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)

24
Q

What is a Narrow Runway (bold)

A

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

25
Takeoff at reduced thrust is prohibited: (bold)
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
Minimum oil temperature for takeoff? (bold)
19°
27
Max operating altitude with slats and/or flaps extended (bold)
FL200
28
AUTOPILOT ENGAGEMENT: After Takeoff/Go-Around (If SRS is indicated) (bold)
100 AGL
29
AUTOPILOT ENGAGEMENT: Enroute (bold)
900 AGL
30
AUTOPILOT ENGAGEMENT: RNAV Visual Approach (bold)
500 AGL
31
AUTOPILOT ENGAGEMENT: Non-Precision Approaches (bold)
DDA/ DA
32
AUTOPILOT ENGAGEMENT: Non-Autoland ILS with CAT 1 FMA (bold)
160 AGL
33
AUTOPILOT ENGAGEMENT: Non-Autoland ILS with CAT 2/3 FMA (bold)
80 AGL
34
AUTOPILOT ENGAGEMENT Autoland ILS Approach (one or two autopilots) (bold)
Rollout/Taxi Speed
35
Autoland Required: (bold)
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
Maximum altitude for APU battery start
FL250
37
The use of AP or FD in OPEN DES or DES mode is not permitted on approach when?
inside the FAF or Below 1000 ft AGL on a visual approach.
38
Autolands are prohibited if braking action is reported
Less than medium.
39
Autoland Autobrakes. Use “Medium” for runway less than:
8,000 feet long Note: (Low or Medium for 8,000 or longer) Autobrakes (if available) are required for all CAT III approaches.
40
Maximum reverse will not be used below
70 knots
41
AUTOLAND WIND RESTRICTIONS
* 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
Maximum Runway altitude (Autoland)
A320: 9200 ft A321: 5750 ft
43
Ram Air Inlet only open if differential pressure is
Lower that 1 PSI
44
DERIVED DECISION ALTITUDE (DDA)
DDA is calculated by adding 50' to the published MDA
45
SPEED BRAKES LIMITATION (NEO)
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