in transference of risk to ground operations must
be mitigated to the extent possible.
2. In addition, crew resource management
discussions must occur between the pilot,
Prescribed Fire Burn Boss, Helicopter Manager,
and PLDO’s prior to all ignition operations. The
discussion shall focus on a heightened awareness
of the risks involved in low level flights the
limitations section of the flight manual and be
familiar with the limitation of flight with the door(s)
removed.
3. Helicopters shall be equipped with a power source
for PSD.
4. A bulkhead mounted MS 3112E- 12 3S, 3-pin
connector shall be provided. Pin B shall be
airframe ground. Pin A shall be +28 V.C. for a 28-
volt aircraft system. Pin C shall be +14 for a 14-
volt aircraft system. The circuit shall be protected
by a 5-amp circuit breaker. The mating connector
for the Government-furnished PSD shall be an MS
3116E-12-3P wired with the same pin
assignments. Reference a wiring diagram in the
aircraft procurement document.
5. Remove appropriate door/doors.
6. Remove all loose cushions and other loose
materials.
7. Locate and assure proper electrical connections.
8. Utilize approved aircraft hard point anchor or
install tether attachments to hard points per
instructions on MTDC drawing # 993 (See
Appendix B.)
9. Install secondary restraint using approved
carabiner and adjust tether length. A properly
adjusted tether shall insure that the operator is
restrained inside the aircraft and will not reach
beyond the sill of the aircraft if the seat belt should
become unbuckled during flight.
10. Fill glycol tank at least 25 feet from aircraft.
11. Fill water storage tank.
12. Ensure adequate supply of plastic spheres is
available to complete project.
13. Ensure one-gallon container of water and seatbelt
cutter is on board, secured, and are readily
accessible.
14. Fire shelters for all occupants must be on board
and accessible, and one or more hand tools are
recommended.