Product Certification Consultations and Publications

Wing Leading Edge Slats (Applicable to Boeing 737-7 / -8 / -9)

Deviate from RTCA/DO-229D 2.2.3.3.1 and provide the deviations relative to the first approach leg instead of the FAF.

Deviates from RTCA DO-283A Appendix H section H.2.7 by alerting 15 seconds instead of the minimum 30 seconds before the required vertical path change.

Deviates from RTCA DO-283A Appendix H section H.2.4.4.3 by using a different vertical guidance compatible of the vertical constraints.

Deviates from RTCA DO-283A Appendix C section C.2.2 by using a different algorithm to determine position from multiple (more than two) DME, and secured with reasonableness checks.

Deviate from RTCA DO-283A Appendix C section C.2.1 by using a different weighting-algorithm to select or exclude VOR stations, and secured with reasonableness checks.

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.