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Frontier Pilot Updated 3/22 Main > General Limitations > Flashcards

General Limitations Flashcards

1
Q

Approach Category 320/321/321 NEO

A

320/321 NEO Category C
321 CEO Category D

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2
Q

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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3
Q

Max Crosswind TO and landing

A

TO - 35kts
Landing - 38kts

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4
Q

Max Tailwind Takeoff

A

A320/320neo/321neo - 15kts
A321 - 10kts

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5
Q

Max Runway Slope

A

-/+ 2%

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6
Q

Max Tailwind Landing

A

All AC - 10kts

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7
Q

Minimum Runway Width Limitations

A

Minimum Runway Width - 148 ft / 45 m

AC 227-229 and 321 NEOs 100 ft / 30 m

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8
Q

Max and Min Pressure Alt for TO & LNDG

A

9200ft
-2000ft

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9
Q

Narrow Runway Width

A

Less than 148 ft. / 45 m

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10
Q

Max Wind for Passenger Door Operation

A

65kts

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11
Q

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.

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12
Q

VMO/MMO

A

350KIAS / .82 Mach

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13
Q

VLO (Retraction)

A

220kts / 0.54 Mach

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14
Q

VLO (Extension)

A

250kts / 0.60 Mach

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15
Q

VLE (Extended)

A

280kts / 0.67 Mach

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16
Q

Max Tire Speed

A

195kts Groundspeed

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17
Q

Max Windshield Wiper Operation Speed

A

230 KIAS

18
Q

Max Cockpit Window Speed

A

200 KIAS

19
Q

Max Taxi Speed (greater than 167,550 lbs)

A

A320 CEO - 20kts during a turn

20
Q

Maximum Flaps/Slats Extended Altitude

A

20,000ft MSL

21
Q

Stabilized Approach Policy

A

1000ft:
1. Rate of Descent 1200FPM or less
2. One dot ILS/LOC .3, 1/2 tot VOR, 0.30 NM RNAV (Lateral) RNP
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 completed

22
Q

T.O Inhibit duration?

A

1500 ft or 2 min after liftoff

23
Q

LDG Inhibit duration?

A

Below 800ft till 80kts

24
Q

Max Operational Pressure Altitude

A

39,800ft

25
Q

Speed Brake Limitation 320 NEO

A

Use of speed brakes at or below 240kts is not permitted if:
- GWCG is above 35% or
- In overweight landing conditions.

26
Q

Landing on Narrow Runways 227-229 and 602-699

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 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)

27
Q

Minimum oil quantity

A

320 CEO - 9.5 qt + 0.5 qt for each hour of flight
320 NEO - 9.0 qt + 0.5 qt for each hour of flight or 10.6 qt, whichever is higher
321 NEO - OAT at or above -30C 14 qt below -30C 16.5 qt

28
Q

Minimum oil temp for takeoff

A

19 degrees c
321 NEO 52 degrees C

29
Q

At what temp do we leave the flaps at 1 after landing

A

30 degrees C

30
Q

Minimum oil temp for engine start

A

-40 degrees C

31
Q

When is an autoland required

A

When below cat I minimums

Furthermore when visibility is at or below 1/2 mile or 2400 RVR the approach will be set up and briefed as an autoland

32
Q

What is the minimum runway width for an autoland

A

148ft/45m

33
Q

Max altitude for a APU battery restart

A

25000 ft

34
Q

Autoflight altitude limitations
* After TO
* Enroute
* RNAV visual
* Non-precision approach
* Non-autoland with Cat I FMA
* Non-autoland with CAT II/III FMA
* Autoland approach
* Go-around

A
  • After TO - 100’ and 5 sec after TO
  • Enroute - 900’
  • RNAV visual - 500’
  • Non-precision approach - DDA/DA
  • Non-autoland with Cat I FMA - 160’
  • Non-autoland with CAT II/III FMA - 80’
  • Autoland approach - Taxi rollout speed
  • Go-around - 100’
35
Q

Which decent modes are not permitted inside the FAF or below 1000’ AGL

A

OPEN DES
DES

36
Q

Autoland authorizations

A

Must be flown by captains
Not less than a 148’/45m wide runway
Braking action must not be less than MED

37
Q

Autoland brake selection requirements

A

Less than 8000’ - MED
8000’ or greater - LOW or MED

38
Q

Engine thrust time limitations

A

Takeoff go around
* all engine 5min
* one engine 10 min

39
Q

When is a reduced thrust TO prohibited

A
  • On a slippery or wet runway
  • When suspected, reported, or known windshear is present
  • When a special Dept procedure specifies full thrust for TO
40
Q

Is TO with the center tanks supplying fuel prohibited?

A

Yes

Frontier Pilot Updated 3/22 Main (13 decks)

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