94-23840. Air Tour Operators in the State of Hawaii; Final Rule DEPARTMENT OF TRANSPORTATION  

  • [Federal Register Volume 59, Number 185 (Monday, September 26, 1994)]
    [Unknown Section]
    [Page 0]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 94-23840]
    
    
    [[Page Unknown]]
    
    [Federal Register: September 26, 1994]
    
    
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    Part V
    
    
    
    
    
    Department of Transportation
    
    
    
    
    
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    Federal Aviation Administration
    
    
    
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    14 CFR Parts 91 and 135
    
    
    
    
    Air Tour Operators in the State of Hawaii; Final Rule
    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Parts 91 and 135
    [Docket No. 27919; Special Federal Aviation Regulation (SFAR) No. 71]
    RIN 2120-AF53
     
    Air Tour Operators in the State of Hawaii
    AGENCY: Federal Aviation Administration (FAA), DOT.
    
    ACTION: Final rule; request for comments.
    
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    SUMMARY: This action establishes certain procedural, operational and 
    equipment requirements for air tour operators in the State of Hawaii. 
    This emergency rule is necessary because of an escalation of air tour 
    accidents. The regulation is intended to enhance the safety of air tour 
    operations within the State.
    
    DATES: This final rule is effective October 26, 1994. Comments must be 
    received on or before December 27, 1994.
    
    ADDRESSES: Send comments on this final rule in triplicate to: Federal 
    Aviation Administration, Office of the Chief Counsel, Attention: Rules 
    Docket (AGC-200), Docket No. 27919, 800 Independence Ave., SW., 
    Washington, DC 20591. Comments delivered must be marked Docket No. 
    27919. Comments may be examined in room 915G weekdays between 8:30 a.m. 
    and 5 p.m., except on Federal holidays.
        Commenters who wish the FAA to acknowledge the receipt of their 
    comments must submit with their comments a self-addressed, stamped 
    postcard on which the following statement is made: ``Comments to Docket 
    No. 27919.'' The postcard will be date stamped by the FAA and returned 
    to the commenter.
    
    FOR FURTHER INFORMATION CONTACT: Brian Calendine, Air Transportation 
    Division, AFS-200, Federal Aviation Administration, 800 Independence 
    Avenue, S.W., Washington, D.C. 20591; Telephone (202) 267-8166.
    
    SUPPLEMENTARY INFORMATION:
    
    Availability of Final Rule
    
        Any person may obtain a copy of this final rule by submitting a 
    request to the Federal Aviation Administration, Office of Public 
    Affairs, Attention: Public Information Center, APA-220, 800 
    Independence Avenue, SW., Washington, DC 20591, or by calling (202) 
    267-3485. Requests should be identified by the docket number of this 
    rule.
        Persons interested in being placed on a mailing list for notices of 
    proposed rulemaking should request a copy of Advisory Circular No. 11-
    2A, ``Notice of Proposed Rulemaking Distribution System,'' which 
    describes the application procedure.
    
    Background
    
    The Air Tour Industry
    
        Since 1980, the air tour industry in the State of Hawaii has grown 
    rapidly, particularly on the islands of Oahu, Kauai, Maui, and Hawaii. 
    The growth of the tourist industry, the beauty of the islands, and the 
    inaccessibility of some areas on the islands has generated tremendous 
    growth in the number of air tour flights. In 1982, there were 
    approximately 63,000 helicopter and 11,000 airplane air tour flights. 
    By 1991, these numbers had increased to approximately 101,000 for 
    helicopters and 18,000 for airplanes. After a slight decline due to 
    Hurricane Iniki in 1992, air tour flights in 1994 are projected to 
    reach the 1991 levels. In Hawaii, the air tour industry carries about 
    400,000 passengers annually. Thirty-eight operators are conducting air 
    tours within the State of Hawaii, using approximately 97 helicopters 
    and 16 fixed-wing aircraft. During the 9-year period between 1982 and 
    1991, there were eight fatal accidents with 24 fatalities. The accident 
    data shows an escalation of fatal accidents during the 3-year period 
    between 1991 and 1994. During this time, there were five fatal 
    accidents with 24 fatalities. (See table and figure)
    
    Use of Helicopters in Air Tours
    
        Helicopters are uniquely suited for air tours in Hawaii because 
    they can operate at slow speeds and hover over scenic areas. Helicopter 
    air tours are often conducted close to the ground, near scenic 
    attractions so passengers can see and experience the thrill of being 
    close to geological and terrain features, such as lava flows and 
    waterfalls.
        Some air tour operators advertise dramatic overwater flights to 
    view whales, shorelines, cliffs, and waterfalls; entry into one-way 
    canyons; flying close to hot molten lava; and hovering over the 
    shoreline where molten lava flows into the ocean. Some advertising 
    brochures, for example, describe air tours as ``excitement to the 
    boiling point,'' and invite tourists to ``fly into the heart and heat 
    of an active volcano'' and ``close enough to waterfalls to feel the 
    cooling mist.'' One fixed-wing air tour operator formerly advertised 
    that ``[w]e fly you lower and slower than any twin engine plane can . . 
    . lower and slower than many helicopters do . . .''
        While passengers are often attracted to the thrill associated with 
    low-flying air tours, they are generally not aware of the risks 
    involved. Risks associated with low flying air tour operations include: 
    unpredictable winds that create less stable flying conditions; fewer 
    options to escape unforeseen weather; unmarked or unknown obstructions; 
    less time to select suitable emergency landing areas; increases in 
    pilot workload because of quick stops, rapid turns, and watching for 
    obstructions; inability to be detected by air traffic control radar; 
    inability to conduct two-way radio communication; increased likelihood 
    of ingesting foreign debris, including salt water spray, into the 
    engine; less overall reaction time; and congestion of low flying 
    traffic at scenic locations. Further, many air tours are conducted over 
    scenic areas along rugged coasts, where, in the event of an engine 
    failure, the pilot must ditch in the ocean. A helicopter without 
    flotation devices, unlike most light airplanes, may sink within 
    moments.
    
    History and Escalation of Accidents
    
        The growth of the air tour sightseeing industry in Hawaii has been 
    associated with an escalation of accidents. The proximate causes of the 
    accidents range from engine power loss to encounters with adverse 
    weather. Contributing factors to the causes and seriousness of 
    accidents are: operation beyond the demonstrated performance envelope 
    of the aircraft, inadequate preflight planning for weather and routes, 
    lack of survival equipment, and flying at low altitudes (which does not 
    allow time for recovery or forced landing preparation in the event of a 
    power failure).
        The following table is a synopsis of selected air tour accidents 
    involving aircraft damage, minor or serious injuries, or fatalities 
    that occurred between September 1982 and September 1994.
    
                          Selected Air Tour Accidents in Hawaii, September 1982-September 1994                      
    ----------------------------------------------------------------------------------------------------------------
        Date                 Type              Part           Location                  Injuries          Fatalities
    ----------------------------------------------------------------------------------------------------------------
    9/2/82        Bell 206-L...............      135  Lihue...................  2 serious...............  ..........
                                                                                3 minor.................            
    4/8/84        Grumman AA-5A............       91  Kamuela.................  ........................           4
    9/26/85       Aerospatiale.............      135  Kula....................  5 minor.................           1
    1/1/86        Cessna R172K.............      135  Kamuela.................  4 serious...............           1
    5/18/86       Bell 206B................       91  Maui....................  1 serious...............           2
                                                                                1 minor.................            
    3/29/87       Bell 206B................      135  Kona....................  3 serious...............           1
                                                                                1 minor.................            
    4/24/87       Cessna 172N..............       91  Lihue...................  ........................           4
    5/29/88       Bell 206B................      135  Honolulu................  2 minor.................  ..........
    5/20/89       Aerospatiale AS350D......      135  Waialae Falls...........  7 minor.................  ..........
    6/11/89       Beech H18................      135  Waipio Valley...........  ........................            
    8/19/89       Aerospatiale AS350D......      135  Volcano.................  1 serious...............          11
                                                                                5 minor.................            
    5/5/91        Hughes 369HS.............      135  Keanae..................  3 minor.................  ..........
    6/6/91        Bell 206B................       91  Lihue...................  3 serious...............  ..........
                                                                                1 minor.................            
    11/9/91       Bell 206B................      135  Hilo....................  1 serious...............  ..........
                                                                                2 minor.................            
    4/22/92       Beech E18S...............      135  Mount Haleakala.........  ........................           9
    9/16/92       Aerospatiale AS350B......      135  Hana....................  ........................           7
    9/21/92       Bell 47..................       91  Volcano National Park...  3 minor.................  ..........
    1/25/93       Fairchild Hiller FH-1100.       91  Volcano National Park...  1 minor.................           4
    2/23/94       Aerospatiale AS350B......      135  Volcano National Park...  1 serious...............  ..........
                                                                                1 minor.................            
    3/25/94       Hughes 369D..............      135  Hawaii National Park....  ........................  ..........
    4/18/94       Hughes 369D..............      135  Waimea..................  4 serious...............           1
    7/14/94       Aerospatiale AS350D......      135  Hanalei.................  ........................           3
    7/14/94       Aerospatiale AS350D......      135  Molokai.................  ........................  ..........
    8/11/94       Aerospatiale AS350D......      135  Waipio Valley...........  ........................  ..........
    9/3/94        Hughes 369D..............      135  Hilo....................  ........................  ..........
    ----------------------------------------------------------------------------------------------------------------
    
        The table shows a total of 24 air tour fatalities between 1982 and 
    1991 (9 years). Even though there was a decline in the number of air 
    tour flights in 1992, the accident data show an escalation of fatal 
    accidents between 1991 and 1994. From July 1991 through July 1994 (3 
    years), there were 20 air tour accidents involving 24 fatalities. (See 
    figure.) Since January 1993, three helicopter accidents have involved 
    landings in the ocean with two of those accidents resulting in seven 
    fatalities. The most recent fatal accident occurred on July 14, 1994. 
    The most recent non-fatal accident occurred on September 3, 1994. (See 
    table.)
    
    BILLING CODE 4910-13-M
    
    TR26SE94.001
    
    
    BILLING CODE 4910-13-C
    
    National Transportation Safety Board Recommendations
    
        Based on its investigation of the April 22, 1992, accident in 
    Haleakala National Park, the National Transportation Safety Board 
    (NTSB) recommended that the FAA ``[c]reate a specific classification 
    for, and operating rules governing, commercial air tour operators based 
    on the complexity of flight operations, aircraft flown, flight 
    frequency, number of passengers carried, air traffic densities in the 
    area of operation, and other relevant factors'' (A-93-8). In addition, 
    the NTSB recommended that the FAA ``[i]dentify airspace which warrants 
    special protection due to air tour operations,'' and ``[c]reate special 
    operating rules for such airspace to reduce the potential for midair 
    collisions and other accidents commensurate with meteorological and 
    terrain considerations.'' (A-93-10) In response to the NTSB's 
    recommendations, the FAA has informed the NTSB that it is considering a 
    special rule for air tour operators in Hawaii.
        Based on the NTSB recommendations, accident investigations, and 
    discussions with the NTSB, the FAA has identified the following as 
    needing to be addressed:
        (1) Air tour operators fly too close and too low to various 
    attractions and land features.
        (2) There is no clear definition of ``suitable landing site'' for 
    helicopters.
        (3) Sightseeing helicopters are operating in the avoid area of the 
    height-speed envelope (deadman's curve) where successful autorotations 
    are not possible.
        (4) Helicopters operating along the shorelines of the Hawaiian 
    Islands should be equipped with appropriate flotation equipment.
        (5) Passengers should be briefed before flights on the use of 
    flotation gear.
    
    Actions Other Than Rulemaking to Address the Problems
    
        The FAA, the State of Hawaii, and the air tour industry have been 
    attempting to correct safety problems that affect air tour operations.
        In 1986, the FAA conducted a study of helicopter sightseeing 
    operations in Hawaii. The study team was composed of representatives 
    from the FAA, the State of Hawaii, and industry. Based on the study, 
    recommendations were made to the State and to operators in Hawaii to 
    improve safety and community relations. Recommendations included the 
    following:
        (1) The FAA should study the possibility of imposing limitations, 
    through operations specifications, that would require the helicopter to 
    be operated at a combination of height and forward speed (including 
    hover) that would permit a safe landing in event of engine power loss, 
    in accordance with the height-speed envelope for that helicopter under 
    current weight and aircraft altitude. These limitations would also 
    prevent the helicopter from being flown over areas in which a safe 
    forced landing could not be made.
        (2) The FAA should advise helicopter operators who conduct 
    passenger-carrying operations under part 91 or part 135 that a flight 
    (1) over an area in which a successful forced landing could not be 
    made, or (2) at an airspeed and altitude combination that places the 
    aircraft beyond its performance capability to successfully autorotate, 
    would be considered a reckless operation under Sec. 91.13 (formerly 
    Sec. 91.9).
        The study team was also concerned about the lack of helicopter 
    flotation equipment on some aircraft, particularly for operations along 
    the coastlines of the islands, where cliffs and rocks make a successful 
    autorotation to shore virtually impossible. The team believes that the 
    shoreline must offer a reasonable chance to land safely in the event of 
    engine failure, and that, if no such area exists, appropriate 
    helicopter flotation equipment should be required.
        Also, in 1986, the FAA conducted a joint study with the State of 
    Hawaii on helicopter heliport and airport access. A result of that 
    study was the Helicopter Operating Plan for Hawaii. Based on portions 
    of that plan, the Hawaiian Helicopters Operators Association (HHOA) 
    developed its ``Fly Neighborly'' program. The HHOA plan calls for 
    voluntary compliance with a standoff distance of 1,500 feet and a 
    minimum altitude of 1,500 feet over communities. In addition, the plan 
    calls for a 3,000-foot standoff distance in areas of Volcanoes National 
    Park. The HHOA program includes part 91 operators as well as part 135 
    certificated operators. This is a voluntary program without FAA 
    oversight.
        On January 17, 1992, the FAA issued Handbook Bulletin No. 92-01, 
    Air Tour/Sightseeing Operations. The bulletin advises principal 
    operations inspectors to recommend to operators that they include 
    procedures in their operations manuals for conducting air tour/
    sightseeing operations. The bulletin also advises the inclusion of 
    charts of air tour areas, procedures for obtaining current weather, 
    provisions for pilot training, and other information specific to air 
    tour operations.
        In January 1994, the FAA held four public meetings in Hawaii to 
    investigate complaints regarding flight safety, aircraft noise, and 
    possible intrusive flights of helicopters. While the vast majority of 
    the commenters addressed the noise issue, some commenters did raise 
    safety issues. Some of the public meeting comments and subsequent 
    comments submitted to the FAA highlight a number of personal 
    experiences of individuals who witnessed helicopters flying dangerously 
    low over scenic areas and above people and property on the ground. In 
    some instances, witnesses claimed that the aircraft flew lower than the 
    people who were walking on high elevation trails.
        The Honolulu Flight Standards District Office, during the past 3 
    years, has conducted an extensive inspection and surveillance program 
    of the air tour industry. On July 15, 1994, in response to a number of 
    recent accidents, the FAA initiated a comprehensive review of 
    operations and maintenance practices of the Hawaiian air tour 
    operators. In addition, the FAA requested that all air tour operators 
    in the State of Hawaii immediately conduct a ``stand down'' safety 
    review of their operational and maintenance practices.
    
    Need for Emergency Rulemaking
    
        Despite the voluntary measures, the cooperation of the Hawaii air 
    tour operators, and the FAA's inspections, the accident data show that 
    additional measures are necessary to ensure safe air tour operations in 
    Hawaii. The current regulatory scheme is not comprehensive enough to 
    ensure the safety of all air tour operations in Hawaii.
        Section 91.119 prescribes minimum altitudes for airplanes and 
    helicopters that provide for the protection of persons and property on 
    the surface. Generally, a pilot may not operate below an altitude 
    allowing, if power failure occurs, an emergency landing without undue 
    hazard to persons or property on the surface. Helicopters may be 
    operated at lower altitudes than airplanes if the operation is 
    conducted without hazard to persons or property on the surface and the 
    pilot can conduct a safe emergency landing in the event of power 
    failure.
        Under ideal conditions, a helicopter, unlike an airplane, can land 
    at or near zero forward speed, provided the landing area is relatively 
    level and free of obstructions. Factors that make an emergency landing 
    site unsuitable include obstacles, rugged terrain, congested areas and 
    water. Obstacles range from natural terrain features and trees to 
    buildings and utility towers with wires strung between them.
        A major factor affecting safety of flight in any single engine 
    aircraft at low altitude is the limited choice of suitable emergency 
    landing areas. Hawaii's unique topography--active volcanoes spewing hot 
    molten lava, sharp cliffs, cascading waterfalls, rugged coastlines, 
    mist-shrouded mountains, dense tropical rainforests and deep, closed 
    canyons--often complicates access to suitable emergency landing areas. 
    The air tour accidents in Hawaii indicate that helicopter pilots have 
    had insufficient time to locate suitable landing areas after engine 
    power loss or other problems leading to accidents.
        Based on the recent escalation of accidents caused by unsafe 
    operating practices, and the fact that voluntary measures are 
    insufficient, the FAA is implementing this emergency final rule as 
    Special Federal Regulation (SFAR) No. 71.
    
    The Special Federal Aviation Regulation
    
        The FAA is promulgating these requirements in an SFAR, rather than 
    a general rule, to address the unique problems associated with the 
    Hawaiian air tour operating environment.
        This emergency regulatory action establishes additional operating 
    procedures, including minimum safe altitudes (and associated increases 
    in visual flight rules (VFR) weather minimums), minimum equipment 
    requirements, and operational limitations for air tour aircraft in the 
    State of Hawaii.
    
    Applicability and Definitions
    
        This SFAR applies to parts 91 and 135 air tour operators in the 
    State of Hawaii (section 1). In section 2, ``air tour'' is defined as 
    any VFR sightseeing flight conducted in an airplane or helicopter for 
    compensation or hire. ``Air tour operator'' is defined as any person 
    who conducts an air tour.
    
    Flotation Devices
    
        The SFAR requires that any single-engine air tour helicopter flown 
    beyond the shore of any island must be amphibious or equipped with 
    emergency floats and approved flotation gear easily accessible for each 
    occupant, or that each person on board the helicopter wear approved 
    flotation gear. An amphibious helicopter or one equipped with floats 
    will allow a safe emergency ditching. This requirement is specific to 
    helicopters because helicopters, unlike airplanes, may sink rapidly 
    after forced landings on water.
        These requirements should reduce the risk of drowning, such as the 
    deaths that occurred on January 25, 1993, when a helicopter, operating 
    under part 91, crashed in deep water while on a sightseeing flight to 
    view molten lava flowing into the ocean off the coast of Volcanoes 
    National Park. Before the accident, the pilot had been hovering near 
    the shoreline between 100 and 150 feet above sea level. When the pilot 
    attempted to resume forward flight, he experienced a total left pedal 
    failure. The pilot lost control and the helicopter landed in the ocean 
    and sank. The helicopter was not equipped with flotation devices, and 
    the pilot and four passengers were not wearing lifevests. Only the 
    pilot survived. The NTSB found that a factor which contributed to the 
    passengers' fatal injuries was the operator's failure to provide 
    lifevests to the passengers.
        In a July 14, 1994, accident, an air tour helicopter with seven 
    people on board made a forced landing in the Pacific Ocean after losing 
    power off Kauai's Na Pali Coast. Three passengers swam to shore and 
    another was rescued from the water. The pilot and two other passengers 
    drowned. The helicopter was not equipped with flotation devices, and 
    the passengers did not have sufficient time to don the lifevests on 
    board the helicopter.
        Later, on the same day, a different air tour helicopter made a 
    forced landing after losing power off the north coast of Molokai. All 
    persons aboard the helicopter swam to shore and were rescued the next 
    day. The helicopter was equipped with flotation devices, and the pilot 
    and passengers had sufficient time to don the lifevests.
        Flotation equipment on a helicopter should allow the helicopter to 
    remain afloat long enough for the persons to egress safely; the 
    individual flotation gear should allow the survivors an opportunity to 
    swim to shore or to be picked up by rescue personnel. Flotation 
    equipment/lifevests helped to ensure the survival of the passengers in 
    the second accident on July 14.
        The FAA is considering changing the rule to require that all 
    single-engine helicopters conducting air tour operations beyond the 
    shore of any island be amphibious or fitted with flotation devices. 
    Therefore, the FAA is requesting comments on this possibility. At the 
    close of the comment period, the FAA will analyze the comments received 
    and, based on its analysis, determine if further rulemaking is 
    necessary.
    
    Helicopter Performance Plan
    
        Section 4 requires that, before departure, the air tour operator 
    must complete a performance plan for the helicopter flight. The pilot 
    in command (PIC) is required to comply with the performance plan. The 
    plan must be based on information in the rotorcraft flight manual 
    (RFM), considering the maximum density altitude to which the operation 
    is planned and must address such elements as maximum gross weight and 
    center of gravity, maximum gross weight for hovering in or out of 
    ground effect, and maximum combination of weight, altitude, and 
    temperature for which height-velocity information in the RFM is valid. 
    This requirement is necessary in light of accidents attributable to the 
    failure of the pilot to stay outside the avoid area of the helicopter 
    height-velocity envelope. The flight is not limited to the out-of-
    ground effect (OGE) ceiling, and the helicopter may be operated at a 
    higher altitude provided no hovering is planned.
        This requirement should enhance flight safety in light of certain 
    accidents, including that which took place on May 20, 1989. On that 
    date, an Aerospatiale AS350D was on a local sightseeing flight to view 
    Waialae Falls with six passengers on board. After hovering at a low 
    altitude near the falls, the pilot began a pedal turn and forward 
    movement for the initial climb away from the falls. The main rotor 
    revolutions per minute (rpm) decayed, and the pilot turned back toward 
    the upper falls, where he thought he could land. However, the 
    helicopter settled into a ravine, damaging the helicopter and injuring 
    the pilot and passengers. The NTSB determined that the probable cause 
    of the accident was the pilot's failure to maintain rotor rpm, while 
    turning and taking off from a hover with a relatively heavy gross 
    weight. Additional factors related to the accident were the high 
    density altitude and rough/uneven (rocky) terrain in the emergency 
    landing area.
    
    Helicopter Operating Limitations
    
        Section 5 requires that the PIC shall operate the helicopter at a 
    combination of height and forward speed (including hover) that would 
    permit a safe landing in the event of engine power loss, in accordance 
    with the height-velocity envelope for that helicopter under current 
    weight and aircraft altitude. This requirement is necessary to prevent 
    pilots from hovering for periods of time beyond the performance 
    capability of the helicopter and outside what the height-velocity 
    diagram permits for safe operation.
        This requirement prohibits aircraft from being operated in 
    dangerous flight regimes, such as the January 25, 1993, accident 
    discussed previously (when the pilot was hovering at a low altitude 
    over a lava flow). It also is intended to prevent the type of accidents 
    that occurred on March 25, 1994, and April 18, 1994. On March 25, 1994, 
    the pilot of a Hughes 369D helicopter operated under part 135 lost 
    control and collided with mountainous terrain by the Puu'oo Vent in 
    Hawaii National Park. The helicopter had become enveloped in a steam 
    cloud at a 40-foot hover just before the pilot lost control. The 
    helicopter was destroyed; the pilot and passengers sustained minor 
    injuries. On April 18, 1994, a Hughes 369D helicopter lost power during 
    an OGE hover and collided with rocky terrain below Waimea Falls, 
    Waimea, Kauai. The helicopter was on a sightseeing flight operated 
    under part 135. The pilot and three passengers were seriously injured. 
    One passenger was fatally injured.
        The requirement increases the possibility of safe landing in the 
    event of engine failure. A safe landing may not be possible if the 
    helicopter is within the avoid area of the height-velocity envelope 
    when the engine failure occurs.
    
    Minimum Flight Altitudes
    
        Section 6 requires that, unless operating in compliance with an air 
    traffic control clearance, or as otherwise authorized by the 
    Administrator, air tour operations may not be conducted below an 
    altitude of 1,500 feet above the surface; and closer than 1,500 feet 
    from any person or property; or below any altitude provided by Federal 
    statute or regulation. As noted earlier, Hawaii's unique topography 
    often complicates access to suitable emergency landing areas. The air 
    tour accidents in Hawaii have been characterized by insufficient time 
    for pilots to locate suitable landing areas after engine power loss or 
    other problems leading to accidents. The requirement to maintain an 
    altitude of 1,500 feet above the surface is necessary for safety 
    because it allows the pilot sufficient time to react in an emergency, 
    to notify and instruct passengers, and to prepare for a forced landing. 
    An aircraft operating at least 1,500 feet above the surface allows the 
    pilot a greater opportunity to select a suitable landing site than 
    would be the case at lower altitudes. The FAA notes that these minimum 
    distances are consistent with HHOA's Fly Neighborly program.
        The accident data also show low-flying aircraft flying VFR into 
    instrument meteorological conditions (IMC). An additional benefit from 
    the 1,500-foot minimum altitude will be the increased basic VFR weather 
    minimums for these air tour operations. This provision is necessary in 
    light of the numerous accidents that have occurred when the aircraft 
    flew into terrain because of low visibility or because the pilot was 
    flying too low. The accident data show that this is a problem for both 
    airplanes and helicopters. For instance, on April 24, 1987, an air tour 
    flight operated under part 91 collided with terrain in the Waimae 
    Canyon. Marginal visual meteorological conditions were reported in the 
    vicinity of the accident site. The pilot and three passengers were 
    fatally injured. In the January 25, 1993, accident, in which the 
    helicopter crashed in deep water after hovering between 100 and 150 
    feet above sea level, the NTSB noted that a contributing factor to the 
    accident was the pilot's choice of a hover altitude/position inadequate 
    to reach a shoreline in the event of an emergency.
        On June 11, 1989, a Beechcraft BE-H18, operating under part 135 on 
    a sightseeing flight, crashed near a waterfall in the Waipio Valley of 
    the Kohala Mountains on the island of Hawaii. After filing a VFR flight 
    plan, the pilot had departed Hilo International Airport for Maui. The 
    pilot entered a closed canyon and ultimately impacted the canyon wall 
    600 to 900 feet below the rim. The pilot and 10 passengers were fatally 
    injured, and the airplane was destroyed by impact forces and postcrash 
    fire. The NTSB determined that the probable cause of the accident was 
    the pilot's improper decision to maneuver with insufficient altitude in 
    a canyon area.
        On April 22, 1992, a Beechcraft E-18S operating on a VFR air tour 
    flight collided with mountainous terrain in Haleakala National Park in 
    an area where fog had reduced visibility around the mountain top. The 
    FAA had provided a full weather briefing to the pilot, including an 
    advisory that VFR flight was not recommended over the interior sections 
    of all islands, and a forecast indicating isolated areas of 3 miles 
    visibility due to haze and moderate rainshowers. The aircraft was 
    destroyed, and the pilot and eight passengers were killed. Weather 
    reports and witness statements indicate that IMC existed in the area at 
    the time of the accident. The NTSB determined that the probable cause 
    of this accident was the pilot's decision to continue visual flight 
    into IMC that obscured rising mountainous terrain and his failure to 
    use properly available navigational information to remain clear of the 
    island.
        On September 16, 1992, an Aerospatiale AS-350B departed on a 
    sightseeing flight even though adverse weather conditions including 
    thunderstorms, rainshowers, and poor visibility were reported. A 
    witness reported rainshowers and mountain obscuration about the time of 
    the accident. He stated that he saw a helicopter flying in and out of 
    clouds and stated that he could not understand why a helicopter would 
    be flying so close to the mountains given the adverse weather 
    conditions. The NTSB determined that a probable cause of the accident, 
    which involved seven fatalities, was the pilot's inflight decision to 
    continue VFR flight into adverse weather conditions. A factor in the 
    accident was the pilot's inability to see and avoid the mountainous 
    terrain due to the thunderstorms.
    
    Briefing Passengers
    
        Section 7 contains the requirement that passengers be briefed (in 
    addition to Secs. 91.102 and 135.117) before takeoff for an air tour 
    flight with a flight segment beyond the ocean shore of any island. The 
    briefing shall include information on water ditching procedures, use of 
    personal flotation gear, and emergency egress from the aircraft. The 
    PIC must orally brief passengers, distribute written instructions, or 
    ensure that passengers have been briefed on emergency procedures. This 
    provision is necessary in light of the flotation equipment requirements 
    set forth in this emergency rule.
    
    Related Rulemaking
    
        This SFAR is an emergency final rule addressing air tour operations 
    in the State of Hawaii in light of the increasing frequency of 
    accidents. The FAA is considering other rulemaking action to address 
    noise and other issues concerning sightseeing overflights in national 
    parks and other scenic areas. On March 17, 1994, the FAA and the 
    National Park Service (NPS) issued a joint advance notice of proposed 
    rulemaking (ANPRM) (59 FR 12740) seeking public comment on general 
    policy and specific recommendations for voluntary and regulatory 
    actions to address the effects of aircraft overflights on national 
    parks. The FAA is currently analyzing comments submitted in response to 
    the ANPRM. This SFAR is an emergency rule and not a final action in 
    response to the joint FAA/NPS ANPRM.
        The promulgation of requirements and restrictions in this SFAR, 
    including the minimum flight altitude restriction, does not preclude 
    the FAA from revisiting the issues addressed in the SFAR. As mentioned 
    above, changes to this SFAR may be necessitated after a review of the 
    comments received from related regulatory proposals. Additionally, this 
    SFAR may be amended after consideration of the comments received on 
    this SFAR.
    
    Paperwork Reduction Act
    
        This rule contains no information collection requests requiring 
    approval of the Office of Management and Budget pursuant to the 
    Paperwork Reduction Act (44 U.S.C. 3507 et. seq.).
    
    Regulatory Evaluation Summary
    
    Introduction
    
        Changes to Federal regulations are required to undergo several 
    economic analyses. First, Executive Order 12866 directs each Federal 
    agency to propose or adopt a regulation only upon a reasoned 
    determination that the benefits of the intended regulation justify its 
    costs. Second, the Regulatory Flexibility Act of 1980 requires agencies 
    to analyze the economic effect of regulatory changes on small entities. 
    Third, the Office of Management and Budget directs agencies to assess 
    the effect of regulatory changes on international trade. With respect 
    to this rule, the FAA has determined that it: (1) is ``a significant 
    regulatory action'' as defined in the Executive Order; (2) is 
    significant as defined in the DOT Regulatory Policies and Procedures 
    (44 FR 11034; February 26, 1979); (3) will have a significant impact on 
    a substantial number of small entities; and (4) will not constitute a 
    barrier to international trade. Therefore, a full regulatory analysis, 
    which includes the identification and evaluation of cost-reducing 
    alternatives to this rule, has been prepared. This regulatory 
    evaluation summary presents a concise analysis of the costs and 
    benefits associated with the final rule that amends the Federal 
    Aviation Regulations by establishing certain operational, procedural, 
    and equipment requirements for air tour operators in the State of 
    Hawaii.
    
    Costs
    
        The FAA estimates the total cost of the SFAR to be about $2.0 
    million, with a present value of $1.8 million (7 percent discount 
    rate), from 1995 to 1997. The FAA assumes that air tour operators will 
    elect to have lifevests on board the helicopter rather than installing 
    external flotation gear because the costs are dramatically lower. This 
    present value cost includes the cost of about $190,000 to provide 
    lifevests on the affected helicopters; the potential of $1.6 million in 
    lost revenue to air tour operators due to minimum flight altitudes; and 
    $10,000 for the development of a helicopter performance plan. Other 
    requirements of the rule--helicopter operating limitations and 
    passenger briefing--will impose little if any cost.
    
    Benefits
    
        Since 1982, Hawaiian air tour operators have experienced 15 
    accidents involving at least one serious injury or fatality where the 
    lack of flotation gear, flying into bad weather, or flying low has 
    played a role in the cause of the accident. These accidents have 
    resulted in 48 fatalities and 30 injuries (16 serious and 14 minor). 
    This evaluation divides these accidents into three categories: (1) 
    Inadvertent air tour helicopter water landings without flotation gear; 
    (2) air tour helicopter accidents related to flying into bad weather or 
    flying low; and, (3) air tour airplane accidents related to flying into 
    bad weather or flying low.
        The potential benefits of preventing all potential sightseeing 
    accidents of a similar nature over the next 3 years totals $36.8 
    million, with a present value of about $32.2 million, of which $13.7 
    million would be for the prevention of helicopter accidents and $18.6 
    million would be for the prevention of airplane accidents.
    
    Regulatory Flexibility Determination
    
        The Regulatory Flexibility Act of 1980 (RFA) helps to assure that 
    Federal regulations do not overly burden small businesses, small 
    nonprofit organizations, and airports located in small cities. The RFA 
    requires regulatory agencies to review rules that may have ``a 
    significant economic impact on a substantial number of small 
    entities.'' A substantial number of small entities, defined by FAA 
    Order 2100.14A, ``Regulatory Flexibility Criteria and Guidance,'' is 
    more than one-third, but not less than 11, of the small entities 
    subject to the existing rule. To determine if the rule will impose a 
    significant cost impact on these small entities, the annualized cost 
    must not exceed the annualized cost threshold established in FAA Order 
    2100.14A.
        Small entities potentially affected by the final rule are small on-
    demand air tour operators in Hawaii using helicopter and fixed-wing 
    aircraft. The FAA assumes that air tour operators will elect to have 
    lifevests on board the helicopter rather than installing external 
    flotation gear because the costs are dramatically lower. The FAA 
    estimates that the annualized cost associated with acquiring lifevests 
    for all helicopter occupants is about $127 per seat. This estimate 
    incorporates the cost of purchasing the lifevests, maintenance, and the 
    associated weight penalty. Also, the FAA estimates that the annualized 
    cost of the 1,500-foot minimum altitude requirement is about $989 per 
    seat. This cost incorporates the estimated lost profits for days when 
    tour operations are prohibited due to inclement weather.
        FAA Order 2100.14A defines small on-demand operators as those 
    operating with a fleet of nine or fewer aircraft, which includes 37 (7 
    fixed-wing and 30 helicopter) of the 38 air tour operators in Hawaii. 
    The annualized cost threshold for small operators is $4,700 in 1994 
    dollars. The FAA has determined that the final rule will have a 
    significant economic effect on 6 of the 7 fixed-wing air tour operators 
    and 25 of the 30 affected helicopter air tour operators. The final rule 
    will impose costs greater than the annualized cost threshold of $4,700 
    for all affected operators except for six of the small air tour 
    operators.
        Due to the significant economic impact of the final rule on a 
    substantial number of small entities, the FAA examined an alternative 
    minimum altitude requirement for the affected operators. The FAA 
    evaluated various minimum altitude requirements including 500, 800, and 
    1,000 feet so as to reduce the annualized cost of the final rule on 
    individual operators. The FAA has determined that a minimum altitude 
    requirement of 500 feet will be necessary to lower the annualized cost 
    of the final rule below the $4,700 threshold for most air tour 
    operators. (Under Sec. 91.155, pilots conducting VFR flights more than 
    1,200 feet above the surface in class G airspace must maintain a 500-
    foot vertical clearance below the clouds. Pilots operating VFR in class 
    G airspace 1,200 feet or less above the surface must remain clear of 
    clouds.) The FAA estimates that the annualized cost of a 500-foot 
    minimum altitude requirement is about $81 per seat. Including the cost 
    of the lifevests, the FAA has determined that the combined cost of the 
    lifevests and the alternative requirement for a 500-foot minimum 
    altitude will lower the annualized cost below the $4,700 threshold for 
    all fixed-wing air tour operators and 26 of the 30 helicopter air tour 
    operators.
        The FAA has evaluated the level of safety for the 1,500-foot 
    minimum altitude requirement in the final rule and that provided by a 
    500-foot minimum altitude requirement. Although the 1,500-foot minimum 
    altitude requirement has a significant economic impact on a substantial 
    number of small entities, it provides operational safety superior to 
    that provided by a 500-foot minimum altitude and is necessary in the 
    public interest. With the 1,500-foot minimum altitude, fixed-wing 
    aircraft and helicopters have a longer power off gliding time, and the 
    pilots are better able to select a suitable landing area in the event 
    of a power failure. Hawaii's unique topography often complicates access 
    to suitable emergency landing areas. The air tour accidents in Hawaii 
    have been characterized by insufficient time for pilots to locate 
    suitable landing areas after engine power loss or other problems 
    leading to accidents. Therefore, the additional safety margins at the 
    1,500-foot minimum altitude should be provided when conducting 
    passenger flights.
    
    International Trade Impact Analysis
    
        The SFAR will not have any impact on international trade because 
    the affected operators do not compete with foreign operators. The SFAR 
    will not constitute a barrier to international trade, including the 
    export of U.S. goods and services to foreign countries and the import 
    of foreign goods and services to the United States.
    
    Good Cause for Immediate Adoption
    
        The FAA is implementing this emergency final rule due to the recent 
    escalation of fatal air tour accidents. Despite voluntary measures, the 
    cooperation of the Hawaii air tour operators, and the FAA's 
    inspections, the accident data show that voluntary measures and 
    existing regulations are insufficient to ensure safe air tour 
    operations in Hawaii. The recent accidents discussed above indicate an 
    urgent safety problem that cannot be adequately addressed solely by 
    enforcement of existing regulations. For this reason, I find that 
    notice and public procedure are impracticable and contrary to the 
    public interest. However, interested persons are invited to submit such 
    comments as they desire regarding this SFAR. Communications should 
    identify the docket number and be submitted in triplicate to the Rules 
    Docket address noted above. All communications received on or before 
    the close of the comment period will be considered by the 
    Administrator, and this SFAR may be changed in light of the comments 
    received. All comments will be available, both before and after the 
    closing dates for comments, in the Rules Docket for examination by 
    interested parties.
    
    International Civil Aviation Organization and Joint Aviation 
    Regulations
    
        In keeping with U.S. obligations under the Convention on 
    International Civil Aviation, it is FAA policy to comply with the 
    Standards and Recommended Practices of the International Civil Aviation 
    Organization to the maximum extent practicable. The FAA is not aware of 
    any differences that this amendment will present.
    
    Federalism Implications
    
        The regulations adopted herein will not have substantial direct 
    effects on the States, on the relationship between the national 
    government and the States, or on the distribution of power and 
    responsibilities among the various levels of government. Therefore, in 
    accordance with Executive Order 12612, it is determined that this 
    regulation will not have sufficient federalism implications to warrant 
    the preparation of a Federalism Assessment.
    
    Conclusion
    
        For the reasons discussed in the preamble, and based on the 
    findings in the Regulatory Flexibility Determination and the 
    International Trade Impact Analysis, the FAA has determined that this 
    regulation is a significant regulatory action under Executive Order 
    12866. In addition, the FAA certifies that this regulation will have a 
    significant economic impact on a substantial number of small entities 
    under the criteria of the Regulatory Flexibility Act. This regulation 
    is considered significant under DOT Regulatory Policies and Procedures. 
    A final regulatory evaluation of the regulation, including a Regulatory 
    Flexibility Determination and Trade Impact Analysis, has been placed in 
    the docket. A copy may be obtained by contacting the person identified 
    under ``FOR FURTHER INFORMATION CONTACT.''
    
    List of Subjects
    
    14 CFR Part 91
    
        Aircraft, Airmen, Aviation safety.
    
    14 CFR Part 135
    
        Air taxi, Aircraft, Airmen, Aviation safety.
    
    The Amendment
    
        In consideration of the foregoing, the Federal Aviation 
    Administration amends parts 91 and 135 of the Federal Aviation 
    Regulations (14 CFR parts 91 and 135) as follows:
    
    PART 91--GENERAL OPERATING AND FLIGHT RULES
    
        1. The authority citation for part 91 continues to read as follows:
    
        Authority: 49 U.S.C. app. 1301(7), 1303, 1344, 1348, 1352 
    through 1355, 1401, 1421 through 1431, 1471, 1472, 1502, 1510, 1522, 
    and 2121 through 2125; Articles 12, 29, 31, and 32(a) of the 
    Convention on International Civil Aviation (61 stat. 1180); 42 
    U.S.C. 4321 et seq.; E.O. 11514, 35 FR 4247, 3 CFR, 1966-1970 Comp., 
    p. 902; 49 U.S.C. 106(g).
    
    PART 135--AIR TAXI OPERATORS AND COMMERCIAL OPERATORS
    
        2. The authority citation for part 135 continues to read as 
    follows:
    
        Authority: 49 U.S.C. app. 1354(a), 1355(a), 1421 through 1431, 
    and 1502; 49 U.S.C. 106(g).
    
        3. In parts 91 and 135, Special Federal Aviation Regulation No. 71, 
    the text of which will appear at the beginning of part 91, is added to 
    read as follows:
    
    SFAR No. 71--Special Operating Rules for Air Tour Operators in the 
    State of Hawaii
    
        Section 1. Applicability. This Special Federal Aviation Regulation 
    prescribes operating rules for airplane and helicopter visual flight 
    rules air tour flights conducted in the State of Hawaii under parts 91 
    and 135 of the Federal Aviation Regulations. This rule does not apply 
    to flights conducted in gliders or hot air balloons.
        Section 2. Definitions. For the purposes of this SFAR:
        ``Air tour'' means any sightseeing flight conducted under visual 
    flight rules in an airplane or helicopter for compensation or hire.
        ``Air tour operator'' means any person who conducts an air tour.
        Section 3. Helicopter flotation equipment. No person may conduct an 
    air tour in Hawaii in a single-engine helicopter beyond the shore of 
    any island, regardless of whether the helicopter is within gliding 
    distance of the shore, unless:
        (a) The helicopter is amphibious or is equipped with floats 
    adequate to accomplish a safe emergency ditching and approved flotation 
    gear is easily accessible for each occupant; or
        (b) Each person on board the helicopter is wearing approved 
    flotation gear.
        Section 4. Helicopter performance plan. Each operator must complete 
    a performance plan before each helicopter air tour flight. The 
    performance plan must be based on the information in the Rotorcraft 
    Flight Manual (RFM), considering the maximum density altitude for which 
    the operation is planned for the flight to determine the following:
        (a) Maximum gross weight and center of gravity (CG) limitations for 
    hovering in ground effect;
        (b) Maximum gross weight and CG limitations for hovering out of 
    ground effect; and,
        (c) Maximum combination of weight, altitude, and temperature for 
    which height-velocity information in the RFM. is valid.
        The pilot in command (PIC) must comply with the performance plan.
        Section 5. Helicopter operating limitations. Except for approach to 
    and transition from a hover, the PIC shall operate the helicopter at a 
    combination of height and forward speed (including hover) that would 
    permit a safe landing in event of engine power loss, in accordance with 
    the height-speed envelope for that helicopter under current weight and 
    aircraft altitude.
        Section 6. Minimum flight altitudes. Except when necessary for 
    takeoff and landing, or operating in compliance with an air traffic 
    control clearance, or as otherwise authorized by the Administrator, no 
    person may conduct an air tour in Hawaii:
        (a) Below an altitude of 1,500 feet above the surface over all 
    areas of the State of Hawaii, and,
        (b) Closer than 1,500 feet to any person or property; or,
        (c) Below any altitude prescribed by federal statute or regulation.
        Section 7. Passenger briefing. Before takeoff, each PIC of an air 
    tour flight of Hawaii with a flight segment beyond the ocean shore of 
    any island shall ensure that each passenger has been briefed on the 
    following, in addition to requirements set forth in Sec. 91.107 or 
    135.117:
        (a) Water ditching procedures;
        (b) Use of required flotation equipment; and
        (c) Emergency egress from the aircraft in event of a water 
    landing.'
        Section 8. Termination date. This Special Federal Aviation 
    Regulation expires on October 26, 1997.
    
        Issued in Washington, DC, on September 22, 1994.
    David R. Hinson,
    Administrator.
    [FR Doc. 94-23840 Filed 9-22-94; 11:42 am]
    BILLING CODE 4910-13-M
    
    
    

Document Information

Effective Date:
10/26/1994
Published:
09/26/1994
Entry Type:
Uncategorized Document
Action:
Final rule; request for comments.
Document Number:
94-23840
Dates:
This final rule is effective October 26, 1994. Comments must be received on or before December 27, 1994.
Pages:
0-0 (1 pages)
Docket Numbers:
Federal Register: September 26, 1994