| 摘要 |
A system (10) for mounting aircraft system components (28, 58) in the crown area of an aircraft comprises a first longitudinal carrier element (12), a second longitudinal carrier element (14) and a bridging element (16) which connects said first longitudinal carrier element (12) to said second longitudinal carrier element (14). The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier element (12, 14) extend substantially parallel to the longitudinal axis (L) of the aircraft. A plurality of cable ducts (26) for accommodating electrical lines (28) is provided on the first and/or the second longitudinal carrier element (12, 14). |
