The Take-off run is 6,250 ft.
There is a 250 ft Obstacle
9,740 ft from Start of Roll.
The runway altitude is 7,200 ft.
It's a 5 kt. tailwind.
It's 1.2% uphill.
It's 30° C.
It's a wet runway.
It's 2,350 nm to JFK.
HOW?
With Maestro Aviation's
on a Hewlett-Packard handheld Computer
The Maestro Electronic Flight Manual holds all the performance information for the aircraft and can carry out all the performance related calculations required to operate a safe flight.
The system provides pilots with the following benefits :-
Accurate and Fast performance calculations
Fast recalculation when there is a sudden change in runway or weather conditions.
Optimum flap setting to get the Maximum Gross Take-off Weight.
Maximum landing weight at departure and destination airport.
Maximum reduced thrust settings.
Contaminated runway calculations.
Runway Performance
The runway performance computer has the following features:
ALL calculations are in accordance with the AFM
Balanced and Unbalanced field length take-off calculations
Full obstacle clearance calculations
IATA world wide runway and obstacle data-base
Calculates intersection take-offs where required
Full V speed information including V1 range
Weight and Balance
The system has a full interactive weight and balance computer and provides the pilot with :
A full trip CG down to minimum fuel at the diversion
Warning if the CG would go outside the limits at any stage of the flight
Rapid re-calculation if the passenger load changes
Visual display of CG position
In-flight Data Reporting
The use of the hand-held computer allows the pilot to generate all the in-flight reports required using the systems calculation and data storage capabilities. These include :
Voyage Report & Technical Log
Pilot's Navigation Log ( PLOG )
Safety Reports
Weather & Notams
Minimum Equipment Lists
All the data required for these functions can be transferred electronically to and from flight operations using the Maestro Operations Procedures Management System.
ETPs and Oxygen Planning
The ETP and Oxygen Planning system provides the pilots of long range corporate jets with a comprehensive planning tool to cover a loss of cabin pressure during a long over water or arctic flight. It takes the wind data from the flight-plan and calculates the ETPs for :
Engine failure in the cruise with a gradual loss of cabin pressure
Catastrophic engine failure with a puncture of the pressure cabin
Medical emergency
The system calculates the optimum altitude at which to fly following the emergency and the time and distance to the closest diversion airport.
Once the airplane is at the appropriate level to continue on to the diversion airport the system will give the pilots the :
Minimum altitude before fuel becomes a problem
Maximum altitude before oxygen becomes a problem
Effect on range and fuel flow of any damage to the airplane
Effect on range of any change in the forecast winds
Ability to recalculate plan to allow for a sick passenger or deteriorating weather at the diversion
For detailed information about Maestro Aviation's fixed wing systems, please contact