Product Certification Consultations and Publications

Fuselage doors (Applicable to Airbus A350-941)

If RTCA/DO-181E is used as an equivalent document for EUROCAE ED-73E to deviate from RTCA/DO-181E Section 2.2.22.h to not interface with FAA TSO-C119a (RTCA/DO- 185 compatible) TCAS units.

Single Event Effects (SEE) Caused by Atmospheric Radiation

Passenger sleeping compartments (Applicable to Airbus A380)

Installation of side facing seats (Applicable to Large Aeroplanes fitted with VIP or Executive interior)

Soft Go-around Mode (Applicable to Airbus A350-941)

CS-AWO 300(b), 321(b)(3), 364 and 365 – CAT 3 Operations - Super Fail Passive Anomalies (Applicable to Airbus A350-941)

Installation of non-smoking signs (Applicable to Large Aeroplanes fitted with VIP or Executive interior)

Improved passenger oxygen mask deployment system (Applicable to Airbus A350-941)

Pitot Heat Indication Systems (Applicable to Airbus A350-941)

Deviate from ETSO-C30c 3.1.1 and use SAE document AS 8037C instead of AS 8037 as the minimum requirement standard. Deviate from ETSO-C96a 3.1.1 and use SAE document AS 8017C instead of AS 8017A as the minimum requirement standard.

Emergency Exit Access - Applicable to Large Aeroplanes