Product Certification Consultations and Publications

High Wall Mini-Suite (Applicable to Airbus A380 / Boeing 777)

Post Certification Actions to Verify the Continued Integrity of Safety Critical Parts

Deviate from ED‐73E by not performing explosion test for these equipment limited to installation in nonexplosive atmosphere.

for limited Icing Clearances Applicable to Large Rotorcraft, CS 29 or equivalent

To replace every reference to SAE AS 407C by a reference to SAE AS 407D to demonstrate compliance for Fuel Flowmeters.

To replace every reference to SAE AS 405C by a reference to SAE AS 405D to demonstrate compliance for Fuel and Oil Quantity Instruments.

To replace every reference to SAE AS 405C by a reference to SAE AS 405D to demonstrate compliance for Fuel and Oil Quantity Instruments.

for the certification of an ADS-B Out Extended Squitter & ELS installation (Major Change) and its compliance to CS-ACNS

Bird strike and Ingestion

Use of Magnesium Alloys for Passenger Seat Components (Applicable to Airbus A350-941)

Deviates from AS8031 paragraph 12.1.3, with light transmission being approximately 80%, slightly less than the Z87.1 standard required value of 89%.

Deviates from AS8031 paragraph 8.1(k) Optical Quality, as is impossible for the Applicant to meet because of the nature of the product design: i.e., a flexible hood rather than a rigid face piece or goggles.