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FAR/AIM: Subpart A—National Air Tour Safety Standards

Subpart A—National Air Tour Safety Standards


Source: Docket No. FAA–1998–4521, 72 FR 6912, Feb. 13, 2007, unless otherwise noted.
 

§ 136.1 Applicability and definitions.

(a) This subpart applies to each person operating or intending to operate a commercial air tour in an airplane, powered-lift, or rotorcraft and, when applicable, to all occupants of those aircraft engaged in a commercial air tour. When any requirement of this subpart is more stringent than any other requirement of this chapter, the person operating the commercial air tour must comply with the requirement in this subpart.

(b) This subpart applies to:

(1) Part 121 or 135 operators conducting a commercial air tour and holding a part 119 certificate;

(2) Part 91 operators conducting flights as described in § 119.1(e)(2); and

(3) Part 91 operators conducting flights as described in 14 CFR 91.146

(c) This subpart does not apply to operations conducted in balloons, gliders (powered and un-powered), parachutes (powered and un-powered), gyroplanes, or airships.

(d) For the purposes of this subpart the following definitions apply:

Commercial air tour means a flight conducted for compensation or hire in an airplane, powered-lift, or rotorcraft where a purpose of the flight is sightseeing. The FAA may consider the following factors in determining whether a flight is a commercial air tour for purposes of this subpart:

(i) Whether there was a holding out to the public of willingness to conduct a sightseeing flight for compensation or hire;

(ii) Whether the person offering the flight provided a narrative that referred to areas or points of interest on the surface below the route of the flight;

(iii) The area of operation;

(iv) How often the person offering the flight conducts such flights;

(v) The route of the flight;

(vi) The inclusion of sightseeing flights as part of any travel arrangement package;

(vii) Whether the flight in question would have been canceled based on poor visibility of the surface below the route of the flight; and

(viii) Any other factors that the FAA considers appropriate.

Commercial Air Tour operator means any person who conducts a commercial air tour.

Life preserver means a flotation device used by an aircraft occupant if the aircraft ditches in water. If an inflatable device, it must be un-inflated and ready for its intended use once inflated. In evaluating whether a non-inflatable life preserver is acceptable to the FAA, the operator must demonstrate to the FAA that such a preserver can be used during an evacuation and will allow all passengers to exit the aircraft without blocking the exit. Each occupant must have the physical capacity to wear and inflate the type of device used once briefed by the commercial air tour operator. Seat cushions do not meet this definition.

Raw terrain means any area on the surface, including water, devoid of any person, structure, vehicle, or vessel.

Shoreline means that area of the land adjacent to the water of an ocean, sea, lake, pond, river or tidal basin that is above the high water mark and excludes land areas unsuitable for landing such as vertical cliffs or land intermittently under water during the particular flight.

Suitable landing area for rotorcraft means an area that provides the operator reasonable capability to land in an emergency without causing serious injury to persons. These suitable landing areas must be site specific, designated by the operator, and accepted by the FAA.

(e) In an in-flight emergency requiring immediate action, the pilot in command may deviate from any rule of this subpart to the extent required to meet that emergency.

[Docket No. FAA–1998–4521, 72 FR 6912, Feb. 13, 2007, as amended by Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§ 136.3 Letters of Authorization.

Operators subject to this subpart who have Letters of Authorization may use the procedures described in § 119.51 of this chapter to amend or have the FAA reconsider those Letters of Authorization.

[Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§ 136.5 Additional requirements for Hawaii.

Any operator subject to this subpart who meets the criteria of § 136.71 must comply with the additional requirements and restrictions in subpart D of this part.

[Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§ 136.7 Passenger briefings.

(a) Before takeoff each pilot in command shall ensure that each passenger has been briefed on the following:

(1) Procedures for fastening and unfastening seatbelts;

(2) Prohibition on smoking; and

(3) Procedures for opening exits and exiting the aircraft.

(b) For flight segments over water beyond the shoreline, briefings must also include:

(1) Procedures for water ditching;

(2) Use of required life preservers; and

(3) Procedures for emergency exit from the aircraft in the event of a water landing.

 

§ 136.9 Life preservers for operations over water.

(a) Except as provided in paragraphs (b) or (c) of this section, the operator and pilot in command of commercial air tours over water beyond the shoreline must ensure that each occupant is wearing a life preserver from before takeoff until flight is no longer over water.

(b) The operator and pilot in command of a commercial air tour over water beyond the shoreline must ensure that a life preserver is readily available for its intended use and easily accessible to each occupant if:

(1) The aircraft is equipped with floats;

(2) The airplane is within power-off gliding distance to the shoreline for the duration of the time that the flight is over water; or

(3) The aircraft is a multiengine that can be operated with the critical engine inoperative at a weight that will allow it to climb, at least 50 feet a minute, at an altitude of 1,000 feet above the surface, as provided in the approved aircraft flight manual for that aircraft.

(c) No life preserver is required if the overwater operation is necessary only for takeoff or landing.

[Docket No. FAA–1998–4521, 72 FR 6912, Feb. 13, 2007, as amended by Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§ 136.11 Rotorcraft floats for over water.

(a) A rotorcraft used in commercial air tours over water beyond the shoreline must be equipped with fixed floats or an inflatable flotation system adequate to accomplish a safe emergency ditching, if—

(1) It is a single-engine rotorcraft; or

(2) It is a multi-engine rotorcraft that cannot be operated with the critical engine inoperative at a weight that will allow it to climb, at least 50 feet a minute, at an altitude of 1,000 feet above the surface, as provided in the approved aircraft flight manual for that aircraft.

(b) Each rotorcraft that is required to be equipped with an inflatable flotation system under this section must have:

(1) The activation switch for the flotation system on one of the primary flight controls; and

(2) The flotation system armed when the rotorcraft is over water beyond the shoreline and is flying at a speed that does not exceed the maximum speed prescribed in the approved aircraft flight manual for flying with the flotation system armed.

(c) Neither fixed floats nor an inflatable flotation system is required for a rotorcraft under this section when that rotorcraft is:

(1) Over water only during the takeoff or landing portion of the flight; or

(2) Operated within power-off gliding distance to the shoreline for the duration of the flight and each occupant is wearing a life preserver from before takeoff until the aircraft is no longer over water.

[Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§ 136.13 Performance plan.

(a) Each operator that uses a rotorcraft must complete a performance plan before each commercial air tour or flight operated under § 91.146 or § 91.147 of this chapter. The pilot in command must review for accuracy and comply with the performance plan on the day the flight occurs. The performance plan must be based on information in the approved aircraft flight manual for that aircraft taking into consideration the maximum density altitude for which the operation is planned, in order to determine:

(1) Maximum gross weight and center of gravity (CG) limitations for hovering in ground effect;

(2) Maximum gross weight and CG limitations for hovering out of ground effect; and

(3) Maximum combination of weight, altitude, and temperature for which height/velocity information in the approved aircraft flight manual is valid.

(b) Except for the approach to and transition from a hover for the purpose of takeoff and landing, or during takeoff and landing, the pilot in command must make a reasonable plan to operate the rotorcraft outside of the caution/warning/avoid area of the limiting height/velocity diagram.

(c) Except for the approach to and transition from a hover for the purpose of takeoff and landing, during takeoff and landing, or when necessary for safety of flight, the pilot in command must operate the rotorcraft in compliance with the plan described in paragraph (b) of this section.

[Docket No. FAA–2022–1563; Amdt. No. 136–2, 88 FR 48091, July 26, 2023]
 

§§ 136.15-136.29 [Reserved]

"[Reserved]" is used simply to indicate that regulatory information might be inserted into this location at some time in the future, and is a placeholder to indicate that the section was intentionally left blank, and not dropped due to a computer error.