Product Certification Consultations and Publications

Deviate from ETSO-C80, Appendix 1, § 7.1.3 performing slosh test at room temperature instead of at 135°±10° F.

Deviates from ETSO-C80, Appendix 1, § 7 Slosh test, specifically from § 7.1.15, performing slosh test without including water and dye in the test fluid as required by the test procedure.

Deviate from ETSO-C80, Appendix 1, § 4.2.a, substituting the test fuel MIL-S-3136, Type III, with fuel Jet A1 for tests in the paragraphs: §7 Slosh, §8 Stand test, §10 Fluid resistance of exterior surface, and §17 Low temperature leakage.

Deviate from ETSO‐C30c by not marking the minimum lamp candle power or lamp part number for lights using non‐replaceable light‐emitting component(s).

Deviate from ETSO-C80, Appendix 1, § 11.0 Permeability, specifically from §11.1.2 Test Procedure, carrying out permeability testing at a relative humidity (RH) level of 50 +/- 5% instead of 40 +/- 5%.

Presentation of Engine Parameters on Universal 5 Panel EFIS (Applicable to BAe Systems ATP)

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.