6.3 a) Large airplanes that have a U.S. original type certificate issued on or before 30 September 1969, which are certificated for operations above 25,000 feet altitude or are turbine.engine powered must have one or more flight data recorders that record data from which time, altitude, airspeed, vertical acceleration, heading and the time of each radio transmission either to or from air traffic control (ATC) can be determined. b) Large airplanes that have a U.S. original type certificate issued after 30 September 1969, which are certificated for operations above 25,000 feet altitude or are turbine.engined powered must have one or more flight data recorders that record data from which the following information may be determined: time, altitude, airspeed, vertical acceleration, heading, time of each radio transmission either to or from ATC, pitch attitude, roll attitude, sideslip angle or lateral acceleration, pitch trim position, control column or pitch control surface position, control wheel or lateral control surface position, rudder pedal or yaw control surface position, thrust of each engine, position of each thrust reverser, trailing edge flap or cockpit flap control position, and leading edge flap or cockpit flap control position.
6.3.1.1 Pursuant with above paragraph a), recorders do not record engine power, configuration, or operation. Pursuant with paragraph b), recorders do not record operation.
6.3.1.2 Pursuant with above paragraph a), recorders do not record engine power or configuration of lift and drag devices.
6.3.5.1 The U.S. does not require such equipage for all aircraft which meet this weight criterion. U.S. regulations (14 CFR 135.152) only require that multi.engine, turbine.powered airplanes or rotorcraft with 10.19 seats that are brought onto the U.S. register after 11 October 1991, be equipped with the flight data recorder specified in this standard.
6.4 Although the U.S. does provide air traffic control services to aircraft operating under VFR, it does not specifically provide for en route ‘‘controlled VFR flights’’ in the ICAO context. The U.S. does not, therefore, have specific requirements or regulations regarding airman certification or aircraft minimum equipment for ‘‘controlled VFR flights.’’
6.5.1 a), c) The U.S. Federal Aviation Regulations do not require all seaplanes for all flights to be equipped with: a) equipment for making the sound signals prescribed in the International Regulations for Preventing Collisions at Sea; or b) one sea anchor (drogue).
6.5.3.1 The U.S. defines extended over water operations for aircraft other than helicopters as an operation over water at a horizontal distance of more than 50 nautical miles from the nearest shoreline.
6.7.5 U.S. regulations require that oxygen dispensing units capable of being automatically presented to the passengers and cabin attendants (before the cabin pressure altitude exceeds 15,000 feet) be installed, in all transport category aircraft approved to operate above 30,000 feet, type certificated on or after 1 September 1977.
6.9.2 The U.S. Federal Aviation Regulations state ‘‘weight’’ and express weight in pounds.
6.12 The U.S. Federal Aviation Regulations do not require airplanes operated above 15,000 meters (49,000 feet) to carry equipment to measure and indicate continuously the dose rate of total cosmic radiation being received and the cumulative dose on each flight.
6.15.1, 6.15.2 The U.S. Federal Aviation Regulations state ‘‘weight’’ and express weight in pounds.
6.17.1 The U.S. only requires one automatic.type, emergency locator transmitter in operable condition that meets the requirement of TSO.C91. However, installations of emergency locator transmitters which occur after 21 June 1995 must meet the requirements of TSO.C91A.
6.17.2 Emergency locator transmitters are not required for: turbojet.powered aircraft, aircraft while engaged in scheduled flights by scheduled air carriers, or aircraft while used to show compliance with regulators or crew training.
6.18.1 U.S. regulations do not require such airplanes to be equipped with an airborne collision avoidance system (ACAS II). U.S. regulations only require equipage with TCAS II which is not equivalent to ACAS II.
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