Limitations plus stuff Flashcards
Max takeoff weight
74990
Max landing weight
65317
Max zero fuel weight
61688
Max runway slope
+/- 2%
Max takeoff and landing tailwind component
10kts (15 kts approved airfields)
Max operating altitude
41000 feet
Max takeoff and landing altitude
8400 feet
Max demonstrated takeoff and landing crosswind
33 knots
Max allowable in-flight difference between capt and first officer altitude displays for RVSM operations
200 feet
Max allowable on the ground altitude display differences for RVSM operations are
Sea level to 5000 feet 50 feet
5001-10000 feet. 60 feet
Max difference between capt or first officers altitude and field elevation is
75 feet
Do not engage autopilot for takeoff below how many feet
400
The minimum use height for single channel autopilot operation is
158 feet
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
Max glideslope angle for autoland
3.25 degrees
Minimum glideslope angle for autoland
2.5
Engine ignition must be on for (4 things)
Takeoff
Landing
Anti ice operation
Operation in heavy rain
Max flap extension altitude
20000 feet
Holding in icing conditions with flaps extended is
PROHIBITED
Do not deploy speedbrakes with flaps what or greater
15
Do not deploy speedbrakes in flight below
1000 feet (radio altitude)
Maximum fuel tank temperature
49c
Minimum inflight fuel tank temperature
-43c (or 3’c above freezing temp of fuel being used)
Random fuel imbalance must not exceed
453kgs
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
3
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
4
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?
4
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?
2
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