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Frontier A320 Intitial (Cottrell) > Limitations (other) !UPDATING! > Flashcards

Limitations (other) !UPDATING! Flashcards

1
Q

Flight Maneuvering Load Acceleration Limits

Clean configuration

Other configurations (Slats and/or Flaps extended)

A
  • 1.0g to +2.5g
    0. 0g to +2.0g
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2
Q

Environmental Envelope

Maximum Operational Pressure Altitude

Maximim Pressure Altitude for Takeoff & Landing

Minimum Pressure Altitude for Takeoff & Landing

A

39,800 ft

9,200 ft

-2,000 ft

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3
Q

Runway Limits

Runway slope

Maximum runway altitude

Minimum runway width

Length

A

+/-2% (mean)

9,200ft

148ft/45m

5000ft, unless the DO authorizes a shorter length.

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4
Q

Speed Limitation - Airspeed

VMO/MMO

A

350kt/0.82 Mach

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5
Q

Landing Gear Speeds

Retraction (VLO)

Extension (VLO)

Extended (VLE)

A

220 KIAS

250 KIAS

280 KIAS

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6
Q

Pressurization - Cabin Differential

Negative

Positive

Safety Relief Valve

A
  • 1.0 psi
    9. 0 psi
    8. 6 psi
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7
Q

Maximum Differences Between Altitude Indications

A

Ground Check:
ADR1 and ADR2: 20’ (on PFD)
STBY ALT: 300’
ISIS: 100’

FL390/0.78M:
ADR1 and ADR2: 130’ (on PFD)
STBY ALT: 445’
ISIS: 445’

(Vol II, System Tolerances)

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8
Q

APU Starter Duty Cycle

Between each start attempt

After three consecutive start attempts

A

1 minute

60 minutes

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9
Q

Autoland - Maximum Winds: A319

A

20 KTS headwind

15 KTS crosswind

5 KTS tailwind

Wind correction: Vls + wind correction

5 KTS to 15 knots

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10
Q

Autoland - Maximum Winds: All A320s & A321

A

30 KTS headwind

15 KTS crosswind

10 KTS tailwind

Wind correction: Vls + wind correction

5 KTS to 15 knots

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11
Q

Autoland/Autobrake limitations: When are Autolands not Authorized due to braking action?

A

Braking action less than Medium

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12
Q

When visibility is less than _____ RVR or __, the approach must be flown with the autopilot(s) engaged if operable.

A

4000 RVR or 3/4SM

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13
Q

Electrical Outlet Limitation

A

May not be used during takeoff and landing.

Note: The 115v, 400hz outlet located on the rear circuit breaker panel should never be used for charging PEDs (including EFBs) as it could pose a fire risk.

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14
Q

Engine Starter Limitations - CEO

A
  • 3 cycles with 20 seconds in between, then 15 minutes to allow starter to cool before another 3 cycles.
    1. A standard automatic start that includes up to three start attempts is considered one cycle.
  • Do not engage above 20% N2
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15
Q

Engine Starter Limitations - NEO

A
  • 3 cycles with 60 seconds in between, then 15 minutes to allow starter to cool before another 3 cycles.
    1. A standard automatic start that includes up to three start attempts is considered one cycle.
  • Do not engage above 59% N2
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16
Q

Flight Crew Oxygen (CEO)

A

Always OK With:

900psi - 2 crew

1100psi - 2 crew + 1 observer

1400psi - 2 crew + 2 observers

17
Q

Flight Crew Oxygen (NEO)

A

Always OK With:

600psi - Per side (No observer)

800psi -Per side (With observer)

18
Q

Fuel Temperature Limits

Jet A minimum & maximum

A

Minimum: -36° C*

Maximum: 49° C**

*If TAT reaches -34° C, monitor ECAM FUEL page to ensure fuel temperature remains higher than -36° C

**Above 49° C reference FUEL LIMITATIONS

19
Q

Inner Tanks Max Imbalance for Takeoff with One Tank Full

A

A319/320/NEO: 1102 lbs

A321: 882 lbs

20
Q

Brake Temperature

Maximum for takeoff (Brake Fans OFF)

A

300° C

21
Q

Continuous Load Per Generator - Maximum

A

100% (90kVA)

22
Q

Continuous Load Per TR - Maximum

A

200 amps

23
Q

Engine Oil Temperature

Maximum continuous

Maximum transient (15 minutes)

Minimum starting temperature

Minimum temperature before takeoff

A

Maximum continuous: 140° C

Maximum transient (15 minutes): 155° C

Minimum starting temperature: -40° C

Minimum temperature before takeoff: 19° C

24
Q

Max EGT for APU Start

A

Below 35,000: 1090° C

Above 35,000: 1120° C

25
Q

Max Engine EGT for Start

A

NEO:

On Ground: 750° C

In Flight: 875° C

CEO:

725° C

26
Q

Max Engine EGT for TO/GA

A

NEO: 1060° C

CEO: 950° C

27
Q

Max Engine N1 and N2 NEO

A

N1: 101%

N2: 116.5%

28
Q

Max Engine N1 and N2 CEO

A

N1: 104%

N2: 105%

29
Q

Maximum APU EGT

A

675° C

30
Q

Maximum APU Operating Altitudes

A

APU Start using battery power only - 25,000ft

APU Start using normal electrics - 39,000ft

One Pack Operation w/electrical - 22,500ft

For Engine Start - 20,000ft

Two Pack Operation w/electrical - 15,000ft

31
Q

Maximum APU RPM

A

107% - Auto shutdown

32
Q

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

A

Inside the FAF or below 1000ft AGL on a visual approach.

33
Q

Reverse Thrust Limitations

A

Prohibited in flight

Backing up with reverse prohibited

Max reverse thrust will not be used below 70 knots

Except in emergency, reverse not used to reduce taxi

34
Q

What is Frontier’s operational procedure in regards to flap extension speeds?

A

To extend slats/flaps at a maximum of VFE - 10 knots except for Flaps Full which should be extended at a maximum of VFE - 15 knots to avoid inadvertently exceeding placarded speeds.

35
Q

Hydraulics Limitations

Maximum Operating Pressure

A

3200 psi

36
Q

When is diversion to a Normal Width runway recommended?

A

Directional control issues -

Rudder Jam

Rudder Pedal Jam

Yaw Damper Fault

No nosewheel steering

Any wheel brake inoperative

37
Q

Maximum Brake Temperature for Takeoff?

A

300° C

(brake fans off)

38
Q

Runway Slope?

Maximum Runway Altitude?

Minimum Runway Width?

A

+/- 2%

9,200 ft

A/C 227, 228, 229: 100 ft/30m

All Other Aircraft: 148 ft/45m

Frontier A320 Intitial (Cottrell) (6 decks)

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