User manual

Part B Section 6.1
Stichting Catalina PH-PBY TRev No: 01
25 May, 2005 Page: 1
6.1 WEIGHT AND BALLANCE:
01 TAKE-OFF AND LANDING WEIGHT
For this aircraft the take-off and landing weight are the same, And is due various reasons
(conversion to Passenger Plane / Insurance) reduced from original to 11.999 KG (26.458
Lbs)
The various graphs relating to take-off and landing performance are to be referred to, to
determine the distances for a particular day or condition. These figures must then be
compared to available field length
The PIC will make the final decision with regard to AUW for take-off. He will sign the
relevant loading documents prior to take-off and duplicates should be left at the point of
departure for every flight. They can be left with the flight plan or in the possession of a
responsible person for later reference if required.
The PIC is also responsible for the loading of the aircraft and it's airworthiness for flight.
Delegation of duties with regard to the distribution of load, passenger seating and the
security of the cargo do not absolve the PIC of the final responsibility for the overall safety
of the aircraft.
Before take-off the PIC will ensure that all precautions have been taken with regard to the
load, and he will discuss the loading arrangements with the loadmaster and cabin crew.
Safety is paramount, and all crewmembers are jointly to ensure that the aircraft is fully
serviceable and safe for flight.
02 FUEL FOR TAXY AND RUN-UP
A total of 45kg (100 Ibs) of Fuel is to be allowed for Taxi and Run-Up under normal
circumstances.
If more is to be used, this should be reflected in the Weight and Balance Chart calculation.