18.05.2017 Views

Talon Helicopters Ltd COM Edition 2 Amend 0 submission 3 TC Stamped

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

<strong>Talon</strong> <strong>Helicopters</strong> <strong>Ltd</strong>.<br />

4.14.7 Fuel weight<br />

- <strong>Edition</strong> 2 -<br />

Company Operations Manual<br />

Chapter 4 § Operational Control System<br />

Refer to the Canada Flight Supplement for volume to weight conversions for maximum density at various<br />

temperatures. The actual fuel weight for specific conditions may be obtained from the dealer supplying the fuel.<br />

4.14.8 Calculation<br />

The PIC shall calculate the weight of the helicopter for the flight to ensure that the maximum take-off weight does<br />

not exceed the maximum allowable take-off weight specified in the Flight Manual.<br />

The C of G shall be determined by the PIC to be within the limitations specified in the Flight Manual. The PIC may<br />

use the following methods to determine the C of G:<br />

§ pre-calculated worst-case scenarios;<br />

§ electronic (using Microsoft Excel or similar) weight and balance program; and,<br />

§ manual calculation using the weight and balance forms found in the Flight Manual.<br />

Worst-case scenarios have been generated for the helicopters in the various configurations flown. This is the<br />

primary method for weight and balance calculations. The master documents for the scenarios are stored on the<br />

Company’s internal server and copies are kept in the helicopter. If the load falls within the limits of these worstcase<br />

scenarios then further calculation of C of G is not required.<br />

If the load exceeds the worst-case scenarios, if the scenarios are not available to the pilot, or if the pilot is<br />

concerned about the load, then the C of G must be calculated using one of the following methods:<br />

§ electronic (using Microsoft Excel or similar) weight and balance program; or<br />

§ manual calculation using the weight and balance forms found in the Flight Manual.<br />

4.14.9 Retention of Weight and Balance Forms<br />

Completed weight and balance forms shall be kept until the completion of the flight.<br />

4.14.10 Training<br />

Each pilot shall receive initial and annual training in this weight and balance system which shall include a full<br />

weight and balance calculation.<br />

4.15 Accident/Incident Reporting Procedures<br />

Refer to the information contained in Chapter 10 - Emergency Procedures and Equipment.<br />

4.16 Overdue Aircraft Reporting Procedures<br />

Refer to the information contained in Chapter 10 - Emergency Procedures and Equipment.<br />

4.17 Use of Checklists and Flight Manual<br />

Pilots shall be familiar with the Flight Manual and shall operate the aircraft in accordance with the limitations set<br />

out in the Flight Manual and with the aircraft checklists.<br />

Normal, abnormal, and emergency checklists must be carried on-board each aircraft.<br />

Checklists or placards, as applicable, shall include:<br />

December 31, 2015 <strong>Amend</strong>ment 0 4-8

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!