Product Certification Consultations and Publications

To deviate from RTCA DO-260B Test 2.4.6.1.2 – Step 2 and to test the equipment with regard to bursts only to the actual behavior of a current (year 2015) TIS-B implementation in the US and to limit the use of the TIS function to the US.

Emergency Exit Access – Applicable to Large Aeroplanes

Applicable to Large Aeroplane category

Certification of airborne systems using Light Amplification by Stimulated Emission of Radiation (LASER) with high energy

Certification of Auto-Throttle Function in CS-23 Aircraft

Equipment, Systems and Installations in Small Remotely Piloted Unmanned Systems (RPAS)

Clarification on the limited validity of equation (A-22) and (A-22a) proposed by DO-229(A,B,C,D) for the ionospheric pierce point location computation and provision of a formula which does not have that limitation.

Determination of an Unsafe Condition for Risk of Rotorcraft Engine In-Flight Shut-Down (IFSD) and Power Loss

Usable Fuel Capacity Marking

Fire protection of flight controls, engine mounts, and other flight structure (Applicable to Boeing 737-7 / -8 / -9)

Fan blade loss - effects at aircraft level - Applicable to Airbus A-320 Neo (equipped with CFN LEAP-1A engines)

Rotor Drive System - Gearbox TBO Development