P & FP 2 Flashcards
The Accelerate Stop Distance Available (ASDA} is defined as:
The Take off Run Available (TORA} plus the length of any declared Stopway.
For Performance calculation purposes, if a Runway is ‘damp’ can it be considered as Dry?
It may be consider considered ‘Dry’.
The maximum permitted take-off mass (MTOM} must be corrected:
if the runway is wet and reverse thrust is not available.
When considering OAT for MTOW calculation:
Interpolation between the published values in the ‘OAT’ column is permitted.
Generally, use of Config 1+F for take-off rather than config 3 will
oIncrease the take-off run and improve climb performance.
Under which conditions is a FLEX temperature take-off NOT approved:
One or more anti-skid units are inop
Following and Eng Failure on take-off, the performance calculation for any specified turn assumes that bank angle should be limited to:
15 degrees below 1500’ aal.
Flexible take-off thrust must never be less than what percentage of the full rated take-off thrust?
75%
The approximate fuel consumption, for planning purposes, while taxying is:
25 kg/min
Entering a lower cost index in the FMGC will:
Increase flight time and reduce fuel consumption.
The Maximum permitted landing mass is:
182,000 Kgs
The Maximum permitted taxy mass is:
233,900 Kgs
The Maximum permitted Fwd CG for take-off and landing is:
18%
The potable water contents are displayed:
on the Forward Attendant’s Panel (FAP} and the water service panel.
Refuelling with one engine running is only permitted if the following criteria are met, these include:
The refuel system must be fully operational.
In order to complete a low visibility approach to a decision height of 100 ft RA, the approach capability on the FMA must show:
At least ‘CAT 2’
What is the minimum RVR associated with Cat 2 minima?
300m
What is the minimum decision height for Cat 3 Fail passive?
50ft RA
What criteria are normally used by UK airport authorities when deciding to promulgate that Low Visibility Procedures (LVPs} are in force?
RVR less than 550m and/or cloudbase below 200’
Following an in-flight malfunction, an automatic approach may be continued provided that any necessary abnormal procedures are completed before reaching what RA/DH/AAL?
1000’ AAL
The maximum headwind for an autoland and auto-rollout is:
35 kts
The minimum aircraft weight for an autoland is:
123,000 Kgs
An automatic approach to a CAT 3 Fail Operational DH requires that:
Both APs must be engaged
