Relocation of No. 1 and No. 2 static inverters from...
Overview
Introduction
Relocation of No. 1 and No. 2 static inverters from nose to aft section of the airplane.
Textron Hawker Beechcraft Hawker 400, Beechjet 400, MU-300 Diamond I, II
€ RFQ
Product Description
Relocation of No. 1 and No. 2 static inverters from nose to aft section of the airplane.
Please contact modification supplier for further details.
STC Status: Reissued
STC Date: 26/03/07
Responsible Office: Wichita Aircraft Certification Office (ACE-115W), Tel: (316) 946-4100
Raytheon Aircraft Company
- MU-300