Product Certification Consultations and Publications

Deviates from RTCA DO-283A section 2.2.4.1.2 by scaling the approach deviation against RNP value (full scale deviation – 2 dots) instead of the discrete scale value defined in table 2-2.

Deviate from RTCA DO-283A section 2.2.4.1.2 by providing angular deviations for the analog approach deviation output.

Deviate from RTCA DO-283A sections 2.2.2.12.2 by not supporting the RNP RNAV type coded in the navigation data base for the area.

Deviate from RTCA DO-283A sections 2.2.2.7, 2.2.2.9, and 2.4.3.4 by not implementing fixed-radius transitions.

Deviate from RTCA DO-283A section 2.2.2.7 by cancelling the offset mode after proceeding from a manually defined (present position) hold.

Limited Icing Clearances Applicable to Large Rotorcraft, CS-29 or equivalent.

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)