Stage: Final Publications

Regulatory Agency Final Publications

FAA Order 8110.56B Restricted Category Type Certification

This order prescribes how to issue type certificates (TC), supplemental type certificates (STC), and other design approvals in restricted category pursuant to Title 14 of the Code of Federal Regulations (14 CFR). This order supplements the procedures in FAA Order 8110.4, Type Certification, and other orders such as those covering the changed product rule (CPR), certification project notification (CPN), issue papers, instructions for continued airworthiness (ICA), and compliance statements. Contact the Aircraft Certification Service (AIR) Design, Manufacturing, & Airworthiness Division (AIR-100) if you have any questions.

EASA ED Decision 2017/017/R AMC/GM for Aerodromes – Amendment 2

The objective of this Decision is to maintain a high level of safety for aerodrome and flight operations.
This Decision amends AMC/GM to Part – ADR.OPS and, more specifically,:
 includes the publication of information by the aerodrome operator concerning the installation of an arresting
system;
 transfers from CS-ADR-DSN to Part-ADR.OPS the provisions related to temporary runway and taxiway closures; and
 revises runway surface evenness criteria.
The amendments are expected to maintain a high level of safety and ensure alignment with ICAO Amendment 13 to
Annex 14 Volume I. Aerodrome operators are mainly affected, however, the proposed changes are considered to have a
minimal impact because the cost of their implementation is negligible.

FAA PS-ASW-27-TBD Safety Continuum for Part 27 Normal Category Rotorcraft Systems and Equipment

This policy establishes a safety continuum for certificating systems and equipment installed on
normal category (14 Code of Federal Regulations (CFR) Part 27) rotorcraft. The policy sets
classes of normal category rotorcraft used for establishing a graduated scale for the certification
standards for systems and equipment. These classes are based on aircraft weight, engine type and
count, and occupant capacity for rotorcraft weighing up to 7,000 pounds. The purpose of the
safety continuum concept established by this policy is to facilitate a more rapid incorporation of
advances in technology for systems and equipment by recognizing a balanced approach between
the risk and safety benefits for installing such technology.