P/N: MS27508E8F98P
Meets EASA TGL-36 Requirements
Meets FAA AC 120-76B
Meets MIL-STD-461 “EMI” Standards
RTCA DO-160G: Section 7(B), 8(S), 15(A), 17(B), 18(R), 19(BCX), 20(TT), 21(MM), 25(A)
P/N: M24308/2-1F:
Installation Screws directly onto the IPS
Our STC (Supplemental Type Certificate) list for all our FAA approved modifications is constantly kept up to date and each is available to view here.
