What is a transport category rotorcraft?

What is a transport category rotorcraft?

Transport category is a category of airworthiness applicable to large civil airplanes and large civil helicopters. If an element in a transport category airplane or helicopter is not highly critical, or if its failure is relatively benign, it is possible for that element not to be duplicated.

Is the airworthiness standard for transport category airplanes?

The airworthiness standards outlined in CFR Part 25 apply to aircraft in the transport category. Transport category aircraft are designed and certified under CFR Part 25 and Part 26, while transport category helicopters fall under Part 29.

What is a Part 29 aircraft?

CFR 14 Part 29 is a section (Part) of the USA/FAA Federal Aviation Regulations (FARs) that deals with Airworthiness Standards: Transport Category Rotorcraft. Rotorcraft with more than 20,000 lb (9,100 kg) maximum takeoff weight and 10 or more passengers must be certified to Category A standards.

What is a Part 27 aircraft?

Currently, Part 27 rotorcraft are defined as those with a maximum gross weight (MGW) up to 7,000 lb (3,200 kg) with a passenger capacity of nine or less. Under the proposed policy change, that single definition would be broken down as: Single turbine engine, up to 4,000 lb (1,800 kg) MGW with five or fewer occupants.

What are the types of rotorcraft?

An Introduction to the Different Types of Rotorcraft

  • Helicopter. The most common type of rotorcraft is a helicopter.
  • Autogyro. While not as common as helicopters, autogyros are another type of rotorcraft.
  • Gyrodyne. A gyrodyne is another type of rotorcraft.
  • Roto Kite.

What are the airworthiness requirements for aircraft?

Two main factors determine if an aircraft is airworthy:

  • The aircraft conforms to its type certificate and authorized modifications; and.
  • The aircraft must be in condition for safe operation.

What are rotorcraft used for?

Rotorcraft generally include aircraft where one or more rotors provide lift throughout the entire flight, such as helicopters, autogyros, and gyrodynes. Compound rotorcraft augment the rotor with additional thrust engines, propellers, or static lifting surfaces.

What is the principle of rotorcraft?

How Does A Helicopter Work? In order to fly, an object must have “lift,” a force moving it upward. Lift is usually made by wings. Wings create lift because of a relationship called the Bernoulli Principle.

What is the principle involved in rotorcraft?

Wings create lift because of a relationship called the Bernoulli Principle. The Bernoulli Principle describes how the speed of air and the pressure in the air are related. An airplane must fly fast to move enough air over its wings to provide lift. A helicopter moves air over its rotor by spinning its blades.

What are the requirements for helicopter flight control systems?

Helicopter Flight Control Systems The certification requirements for helicopters to operate under Instrument Flight Rules (IFR) are contained in 14 CFR Part 27, Airworthiness Standards: Normal Category Rotorcraft, and 14 CFR Part 29, Airworthiness Standards: Transport Category Rotorcraft.

What are the IFR requirements for helicopters?

The certification requirements for helicopters to operate under Instrument Flight Rules (IFR) are contained in 14 CFR Part 27, Airworthiness Standards: Normal Category Rotorcraft, and 14 CFR Part 29, Airworthiness Standards: Transport Category Rotorcraft.

How much visibility reduction can helicopters do?

Helicopters flying conventional (non-Copter) SIAPs may reduce the visibility minima to not less than one half the published Category A landing visibility minima, or 1 / 4 statute mile visibility/1200 RVR, whichever is greater unless the procedure is annotated with “ Visibility Reduction by Helicopters NA .”

How complex is AFCS/AP/FD equipment installed in IFR helicopters?

Experience has shown that modern AFCS/AP/FD equipment installed in IFR helicopters can, in some cases, be very complex. This complexity requires the pilot (s) to obtain and maintain a high level of knowledge of system operation, limitations, failure indications and reversionary modes.

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