Ec155 flight manual

EC B 4,kg EC B1 4,kg New Fenestron New engines New engines New engines with FADEC New Fenestron New avionics New digital 4-axis autopilot Glass cockpit Bigger cabin New engines New engines Dauphin Family Evolution SA C () AS C () Retrofit EC B to EC B1 available. COMPLEMENTARY FLIGHT MANUAL 2 FLIGHT CONTROL DISPLAYS SYSTEM GENERAL The FCDS is composed of 2 independent channels. Each channel is composed of the following equipments: r One simplex electronic module FCDM (Flight Control Displays Module), r Two independent displays: PFD (Primary Flight Display) and ND (Navigation Display). 1. Flight Manual SA C1: Flight Manual approved on 26 March by DGAC FR, or subsequent DGAC FR or EASA approved revisions (see Note 4) SA C2: Flight Manual approved on 18 February by DGAC FR or subsequent DGAC FR or EASA approved revisions (see Note 4) SA C3: Flight Manual approved on 14 January by DGAC FR.

Study the Rotorcraft Flight Manual (RFM)/Pilot's Operating Handbook (POM) so that you are thoroughly familiar with: • limitations; including rotor speeds/power settings and the HV diagram, • normal, abnormal and emergency procedures, consider your actions should you encounter abnormal or emergencies in flight. In , Life Flight is celebrating 40 years of providing lifesaving care to critically ill and injured people of Pennsylvania. As a longtime customer of Airbus Helicopters Inc., Life Flight has transported more than 75, patients over the past four decades. The modification will be integrated into the following manuals: Illustrated Parts Catalog (IPC), - Flight Manual (FLM). Revision of the documents IPC will be updated on the customer's order. The Flight Manual (FLM) will be updated as part of a future revision. 1.M. PART INTERCHANGEABILITY OR MIXABILITY Not applicable. CAUTION.

For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate docume nts. B1 CORPORATE E 9 This document is the property of EUROCOPTER ® ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER ® and its contents. COMPLEMENTARY FLIGHT MANUAL 2 FLIGHT CONTROL DISPLAYS SYSTEM GENERAL The FCDS is composed of 2 independent channels. Each channel is composed of the following equipments: r One simplex electronic module FCDM (Flight Control Displays Module), r Two independent displays: PFD (Primary Flight Display) and ND (Navigation Display). FLIGHT MANUAL. www.doorway.ru TOT limit Upon starting. C. Automatic shut off NOTE 1. C. For N1, MCP/MTOP/Transient limitations change according to Hp and OAT. NOTE 2 For torque: MTOP can be maintained for 30 min. when IAS < 40 kt (74 km/h). The max. total permissible transient is ,4% or up to % for yaw control in hover flight.