Oklahoma Administrative Code
Title 310 - Oklahoma State Department of Health
Chapter 641 - Emergency Medical Services
Subchapter 11 - Specialty Care Ambulance Service
Section 310:641-11-11 - Specialty care air ambulance aircraft
Current through Vol. 42, No. 1, September 16, 2024
(a) An air ambulance aircraft may be fixed wing, single or multi-engine; or rotary wing, single or multi-engine.
(b) Operations of the aircraft shall be under the appropriate provisions of the Federal Aviation Regulations (FARs).
(c) The interior of the patient compartment of their aircraft shall have the capability of being climate controlled to avoid adverse effects on patients and medical personnel on board by a means other than flight operations and flying to an altitude.
(d) The aircraft design and configuration shall not compromise patient stability in loading, unloading, or in- flight operation to include:
(e) Patients transported by air will be restrained with a minimum of three straps, including shoulder straps, which must comply with FAA regulations. The following additional requirements shall apply to achieve patient stability:
(f) A supplemental lighting system shall be installed in the aircraft/ambulance in which standard lighting is insufficient for patient care, and a self-contained lighting system powered by a battery pack or portable light with a battery source must be available.
(g) An electric power outlet shall be provided with an inverter or appropriate power source of sufficient output to meet the requirements of the complete specialized equipment packages without compromising the operation of any other system or equipment. A back-up power source to enable use of equipment may be provided by an extra battery of appropriate voltage and capacity.
(h) There shall be access and necessary space to ensure any onboard patient's airway is maintained and to provide adequate ventilatory support from the secured, seat-belted position of medical transport personnel.
(i) Medical transport personnel shall be able to determine if medical oxygen is on in the patient care area.
(j) A variety of medical oxygen delivery devices consistent with the service's medical protocols shall be available.
(k) An appropriately secured portable medical oxygen tank with a delivery device shall be carried on the aircraft. Portable medical oxygen tank may not be secured between patient's legs while the aircraft is in motion.
(l) There shall be a back-up source of medical oxygen sufficient to allow completion of the transport in the event the main system fails. For air transports, this back-up source can be the required portable tank as long as the portable tank is accessible in the patient care area during flight.
(m) Storage of oxygen shall comply with applicable standards.
(n) Oxygen flow meters and outlets shall be located to prevent injury to medical transport personnel to the extent possible.
(o) In the event the licensee will be utilizing a substitute aircraft not previously permitted by the Department for a period of more than five (5) days, the licensee shall notify the Department to have the aircraft inspected and permitted by the Department.
(p) Any vehicle initially placed in service after a purchase, lease, contract and/or refurbish shall be inspected, approved, and permitted by the Department as detailed within this section of OAC 310:641 Subchapter 11.