Maximum Continuous Power (MCP) 2 x 283 2 x 385 2 x 380.
Maximum continuous OEI-power 1 x 353 1 x 480 1 x 473.Maximum Continuous Power (MCP) 426 579 571ġ35.02.101.01.E 8This 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 shall not be disclosed.Maximum Continuous Power (MCP) 419 570 562.One Engine Inoperative (OEI), MCP 528 718 708.One Engine Inoperative (OEI), 2.0 min power 580 789 777.One Engine Inoperative (OEI), 30 sec power 609 828 816.2002)Įngine ratings (thermodynamic limits per engine at SL, ISA): 2 Turbomeca turbine engines: new ARRIUS 2B2 with 30 sec-rating.(for deliveries after Sept. 2 Pratt & Whitney turbine engines: new PW206B2 with 30 sec-rating.or � Empty weight, basic version, wet 1,490 3,285� Pilot 80 176� Useful load 1,265 2,789� Maximum take-off weight 2,835 6,250� Maximum take-off weight with external load 2,900 6,400 (2nd litter in stowed position possible)� 2 pilots + 2 litters + 2 seats for doctor and attendant � 1 Pilot + 2 litters + 2 seats for doctor and attendant� 2 pilots + 1 litter + 3 seats for doctor and attendants � Casualty evacuation: � 1 pilot + 1 litter + 3 seats for doctor and attendants(2nd litter in stowed position possible)
� Passenger transport: � 1 or 2 pilots + 6 or 5 passengers (standard version)� 1 or 2 pilots + 5 or 4 passengers (VIP advanced package-version)� 1 or 2 pilots + 7 or 6 passengers (option)
#Tecnical data pcc135w painnt manual#
For performance data and operatinglimitations, reference must be made to the approved flight manual and all appropriatedocuments.ġ35.02.101.01.E 7This 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 shall not be disclosed. ■■■■ The data set forth in this document are general in nature and for informationpurposes only. ■■■■ Eurocopter’s policy is one of on-going product enhancement which means thatalterations in definition, weights, dimensions or performance may be made at any timewithout notice being included in those documents that have already been issued. This document cannot thus be taken as an offer or serve as an appendix to a contract without aprior check as to its validity and prior written agreement of EUROCOPTER. For any more in-depth technical information, please refer to theEC135 type specification (135.02.102.01 E) The mandatory equipment for a Cat A or JAR OPS 3 certifications is already included inthe “PINAO” avionics packages. This document gives a technical overview of the EC135 standard sales and its possible additionalequipment. 135.02.101.01.E 3This 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 shall not be disclosed.
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