Limitations plus stuff Flashcards by daire creaton

Max takeoff weight

74990

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Max landing weight

65317

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Max zero fuel weight

61688

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Max runway slope

+/- 2%

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Max takeoff and landing tailwind component

10kts (15 kts approved airfields)

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Max operating altitude

41000 feet

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Max takeoff and landing altitude

8400 feet

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Max demonstrated takeoff and landing crosswind

33 knots

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Max allowable in-flight difference between capt and first officer altitude displays for RVSM operations

200 feet

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Max allowable on the ground altitude display differences for RVSM operations are

Sea level to 5000 feet 50 feet

5001-10000 feet. 60 feet

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Max difference between capt or first officers altitude and field elevation is

75 feet

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Do not engage autopilot for takeoff below how many feet

400

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The minimum use height for single channel autopilot operation is

158 feet

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Max allowable wind speeds when conducting a dual channel Cat II or Cat III landing are

Headwind. 25 knots
Crosswind. 20 knots
Tailwind. 10 knots

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Max glideslope angle for autoland

3.25 degrees

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Minimum glideslope angle for autoland

2.5

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Engine ignition must be on for (4 things)

Takeoff
Landing
Anti ice operation
Operation in heavy rain

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Max flap extension altitude

20000 feet

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Holding in icing conditions with flaps extended is

PROHIBITED

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Do not deploy speedbrakes with flaps what or greater

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Do not deploy speedbrakes in flight below

1000 feet (radio altitude)

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Maximum fuel tank temperature

49c

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Minimum inflight fuel tank temperature

-43c (or 3’c above freezing temp of fuel being used)

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Random fuel imbalance must not exceed

453kgs

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Main tanks 1 and 2 must be full if centre tank contains more than how much?

453kgs

Operation with assumed temperature is not permitted with what inop?

Anti skid

Max taxi speed when backtracking a runway

50 knots

Max taxi speed in a straight line

30 knots

Max taxi speed on apron

15 knots

Max taxi speed around corners (>90 degrees)

10 knots

Max taxi speed on slippery surface or in low vis.. Straight line? Corners?

Straight 10 knots | Corners 5 knots

Max taxi speed on contaminated runway

5 knots

Standard holding speeds Up to 6000? 6000-14000? 14000 and above?

210 220 240

Max wind speed for air stairs operation

40 knots

Max wind speed with air stairs extended

60 knots

Air stairs should not be operated more frequently than how many consecutive cycles in 20 mins

Max Cabin Differential pressure is

9.1 psi

Max differential pressure for takeoff and landing is

0.125 psi

Allow how many minutes between attempts to start APU

APU start cycle can take up to how long?

120 secs (2 mins)

How long should you leave before using APU as bleed air source

60 secs (1min)

What will shutting battery off do to APU in air and in ground?

Shuts it down

During full shutdown procedure allow how long after APU is switched off to turn BATTERY to OFF

120 secs (2 mins)

Outside of what temperatures can the APU be switched on to heat or cool cabin

Below 5 c | Above 25 c

APU can be used for electrical load up to what altitude?

41000

APU can be used as a bleed air source up to

17000

APU can be used as bleed air source and electrical load up to?

10000

Flight crew reset of a tripped circuit breaker in flight is not recommended unless specifically told to do so by non normal checklist

However a tripped CB may be reset once, after a short cooling period (2 mins approx) if in captains judgement it will not affect safety

CVR has how many independent channels?

CVR record time is?

120 mins (automatically erases after 120 mins)

When CVR on AUTO it records from when to when?

From 1st engine start until 5 mins after last engine shutdown

To erase CVR

Push for 2 secs (operates only on ground with parking brake set)

Where is ELT stored?

Near L2 door

Once ELT is activated how long does it transmit for?

48 hours

How many Engine Integrated Drive Generators are there?

The 2 Engine Integrated Drive Generators supply what power?

3 phase 115 volt 400cps AC

Normal indications for AC Voltmeter Frequency meter DC voltmeter

115v +/- 5v 400cps +/- 10 cps 26v +/- 4v

Under what conditions is requesting an orbit to lose altitude acceptable?

- not less than 10nm from touchdown - not below 3000ft or MSA whichever is higher - max flap 10 with speedbrake extended if necessary - VMC conditions

Define VMC conditions

Cloud base above 1000ft | Vis in excess of 5000m

Night time visuals are

PROHIBITED

Circle to land at night are approved if

PAPI or electronic GS is operational on landing runway

Requirements for a visual approach

- double brief - FO > 500 hours Ryanair - Rwy in sight at all times - use LNAV and VNAV - Do not turn on final unless on path +/- 400ft - Do not close less than 4nm from runway - minimums for visuals are 500ft AAL

What is rule regarding multiple weather related missed approaches?

Following 2 weather related missed approaches, divert unless - vis increases *2 - cloud base *2

Landing on a wet runway of less than how many feet when auto brake U/S is prohibited?

6500

When should Idle Reverse be used?

- Last flight of the day at all RYR bases - last flight of a series of flights when there is at least 60 mins turnaround - last landing prior to aircraft going out of service - any landing where turnaround won't be affected by use of Autobrake

A weather related diversion, capt need to file a?

CSR with details of actual reasons eg. No contact at minimums, RVR actual less than required, severe convective weather etc

If a diversion or go-around is initiated below 1000ft AAL or any safety related event requires a diversion this should be reported in a?

SAIR

What is the required engine cool down time before shutoff?

Minimum 1 minute | If possible 3 mins time at idle or near idle eg taxi

When should fasten belts go on in descent?

On by FL150 or 50nm from destination if an early descent is required

Engine Anti-Ice .....ON | What does turning engine anti-ice on do to stall warning logic?

Stall warning logic sets stick shaker and minimum maneuver speed bars on airspeed indicator and returns to normal when positioned to OFF

Wing Anti-Ice .....ON | What does turning wing anti-ice on do to stall warning logic?

Stall warning logic sets stick shaker and minimum maneuver speed bars on airspeed indicator and remains set for remainder of flight

All Anti-Ice systems use which power?

AC power

When operating on standby power only one pitot probe is heated, which one?

Capt Pitot | But the capt pitot light will not illuminate for a failure