AIRBUS H135 — Systems Description
1 systems description reference for the AIRBUS H135.
Overview
H135 Technical Description · 2020
The document provides a technical description of the Airbus H135 helicopter, detailing its systems, components, and features. It serves as a general reference for understanding the aircraft's design and operational capabilities.
- Energy absorbing fuselage design
- Two turbine engines: Pratt & Whitney Canada PW206B3 or Safran ARRIUS 2B2
- Bearingless Main Rotor system for improved dynamics
- Fenestron-type tail rotor with ten blades
- Advanced cockpit with multifunction displays
- Crash resistant fuel system
- Digital 3-axis Stability Augmentation System
- Comprehensive electrical installation with multiple busbars
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
1 document
AIRBUS H135 — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the AIRBUS H135?
Sprinkle has 1 Systems Description document on file for the AIRBUS H135.
What year is the AIRBUS H135 Systems Description?
The AIRBUS H135 Systems Description on file is dated 2020.
