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