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TD_EC135.pdf | Instrument Flight Rules | Avionics
TD_EC135.pdf
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Ec135 t2 Basis Flm
For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
135.06.101.01 E 1
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 shall not be disclosed. eurocopter - 01/2006
1 Foreword .......................................................................................................................................... 3
2 General characteristics..................................................................................................................... 7
2.1 External dimensions.................................................................................................................. 7
2.2 Internal dimensions................................................................................................................... 8
2.3 Possible cabin arrangement (seats & equipment as option) .................................................... 8
2.4 Weight ....................................................................................................................................... 9
2.5 Fuel Capacities ......................................................................................................................... 9
2.6 Engines ..................................................................................................................................... 9
2.7 Main transmission ratings ....................................................................................................... 10
3 Standard aircraft definition ............................................................................................................. 11
4 Basic configuration choice ............................................................................................................. 13
4.1 VFR packages (based on Avionics Solution 1)....................................................................... 16
4.2 Dual pilot IFR packages, conventional instrumentation, (based on Avionics Solution 3)....... 22
4.3 Dual pilot IFR packages, conventional instrumentation, (based on Avionics Solution 4)....... 26
4.4 Dual Pilot or Single/Dual Pilot IFR Glass Cockpit, based on Avionics Solution 7, 8 or 11..... 30
4.5 Single Pilot IFR Glass Cockpit, based on Avionics Solution 9, 10 or 12 ............................... 36
4.6 Antenna layouts ...................................................................................................................... 42
5 Cabin arrangement......................................................................................................................... 45
5.1 Passenger transport................................................................................................................ 45
5.2 EMS equipment....................................................................................................................... 52
6 Optional equipment ........................................................................................................................ 64
6.1 Shopping list............................................................................................................................ 64
6.2 Police ...................................................................................................................................... 69
6.3 Offshore .................................................................................................................................. 70
7 Table of constraints........................................................................................................................ 71
7.1 General Checklist for Incompatibilities.................................................................................... 71
7.2 Legend of the following chart .................................................................................................. 72
8 Main performance .......................................................................................................................... 74
Manufacturers notes Attention!
Eurocopters policy is one of on-going product enhancement which means that alterations in
definition, weights, dimensions or performance may be made at any time without 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 a
prior check as to its validity and prior written agreement of Eurocopter.
The operational or certification regulations, as defined by the local authorities, can make
compulsory the installation of some of the equipment or recommended solutions, listed in this
document. This list does not claim to cover the whole of the worldwide operational requirements
nor the equipment not specifically related to the helicopter (for example: life jacket) or necessary
for particular missions (for example: supplemental oxygen). The operator is responsible for
ascertaining with his local authorities that the planned configuration of the helicopter complies
with regulatory requirements for the area(s) of operations and the type(s) of mission(s)
EUROCOPTER, its logo, MARMS
and STEADYCONTROL
are trade marks of the Eurocopter
135.06.101.01 E 2
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The EC135 is a light twin-engine, multi-purpose helicopter of the 2-3 ton class with up to 8 seats for
pilot/s and passengers. Underlining its multi-role capabilities, it can even be operated single pilot IFR
as an option. The helicopter combines Eurocopters latest Technologies, like advanced cockpit design,
modern avionics, fenestron anti-torque-device and all-composite bearingless main rotor system, giving
the helicopter an outstanding maneuverability. Optimized main rotor blades with advanced tip
geometry in combination with a fenestron with unequal blade spacing make the EC135 the quietest
helicopter in its class, bringing it 6.5 dBA below the ultra-stringent ICAO limit. The built-in anti
resonance isolation system (ARIS) filters rotor-induced vibrations and thus enhances flying comfort to
a maximum. As a result, the vertical vibration level is far below 0.1g at hover with no increase with
Due to its extreme simplicity, the rotor system contributes to highest safety standards and, at the same
time, reduces maintenance to a minimum. The first scheduled maintenance is the intermediate
inspection after 400 Flh. In addition, the rotor system together with high TBO gearbox and airframe
components grant for high in-service-time of the helicopter.
Depending on the operators preferences, the EC135 can be equipped with either Arrius 2B2 or
Pratt & Whitney PW206B2 power plants - both are FADEC controlled. These powerful and reliable
engines in combination with the lifting system provide outstanding performance and vital power
reserves even in OEI scenarios.
For training purpose an OEI training mode is implemented to perform a realistic OEI training. This
training mode is based on a twin engine training concept featuring a so called TRAINING and a
TRAINING IDLE engine.
Twin-engine reliability is complemented by a tandem hydraulic and dual electrical system as well as a
redundant lubrication and cooling system for the main transmission.
Further safety aspects of the EC135 are design elements like energy absorbing fuselage and seats,
as well as the crash resistant fuel cells.
A wide range of quick interchangeable optional equipment is available for the EC135, e.g. emergency
floats, hoist, SX16 search light, single or dual cargo hook and many more. Together with its most
versatile cabin layout the EC135 is ready to operate in different missions, like police / surveillance,
passenger / VIP transport, EMS, public service, to highlight on a few.
Compared to other helicopters in its class, the EC135 offers a large cabin, featuring:
Excellent outside visibility for pilots and passengers
Roomy cabin which accommodates long or bulky freight
Unrivalled side loading (no door posts) and rear loading capability
Unobstructed and flat floor all over the cabin area with integrated airline style rails
135.06.101.01 E 4
Alternatively to a conventional cockpit, the EC135 is available with glass cockpit, which comprises
primary flight displays (PFD) and NAV displays (ND). All LCD screens are well arranged on the
instrument panel, easy to read even if viewed from an angle and feature perfect readability in any light
conditions. The unique color coding, warning and information concept helps the pilot/s to collect all
relevant parameters while suppressing presentation of non-relevant information.
Common to the conventional and the glass cockpit is the Central Panel Display System (CPDS).
Included in this CPDS there is Eurocopters unique first limit indicator (FLI) which dramatically
simplifies engine and torque monitoring. Being relieved from the instrument scan without missing vital
information, the pilot/s can dedicate more of his/their attention to the mission.
(analog instruments)
Glass Cockpit Instrumentation
(MEGHAS / FCDS)
VFR- Single Pilot
or Dual Pilot
Packages based on
Avionics Solution 1
covered by SP or DP-IFR
IFR- Dual Pilot Packages based on
Avionics Solution 3 or 4
IFR- Dual Pilot or
Single/Dual Pilot
Avionics Solution 7, 8 or 11
IFR- Single Pilot not available IFR- Single Pilot Packages based on
Avionics Solution 9, 10 or 12
Latest news / highlights:
New version EC135 P2+ or T2+ with:
Increased maximum take off weight: MTOW: 2.910 kg
Increased useful load: 1.455 kg
135.06.101.01 E 5
135.06.101.01 E 6
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* Rotor turning, controls in neutral position
135.06.101.01 E 8
2.2 Internal dimensions
Floor area Volume
Cabin & baggage compartment 4.35 m 46.83 ft 4.90 m 173.04 ft
Cockpit (pilot side) 1.15 m 12.38 ft 1.00 m 35.31 ft
Total (undivided) 5.50 m 59.21 ft 5.90 m 208.35 ft
2.3 Possible cabin arrangement (seats & equipment as option)
1 or 2 pilots + 7 or 6 passengers (6 Passenger Transport version)
1 or 2 pilots + 6 or 5 passengers (5 Passenger Transport version)
1 or 2 pilots + 6 or 5 passengers (5 Corporate Passenger Transport version)
1 or 2 pilots + 5 or 4 passengers (4 VIP Passenger Transport version)
1 pilot + 1 litter + up to 5 seats for doctor and attendants
1 pilot + 2 litters + up to 4 seats for doctor and attendant
2 pilots + 1 litter + up to 4 seats for doctor and attendants
2 pilots + 2 litters + up to 3 seats for doctor and attendant
1 pilot + 4.9 m (173.04 ft) in cabin and cargo compartment
135.06.101.01 E 9
Note : margin 1.5 % kg lb
Empty weight, wet (in standard aircraft configuration) 1,455 3,208
Useful load (for standard aircraft configuration) 1,455 3,208
Payload and / or fuel 1,375 3,031
Maximum take-off weight 2,910 6,415
2.5 Fuel Capacities
Usable Fuel Unusable Fuel
Note: Tolerance of fuel figures: 1%
Fuel density used is 0.8 kg/liter.
lb kg l lb kg
Main Tank 1038.6 471.1 588.9 7.5 3.4
Supply Tank 196.8 89.3 111.6 9.3 4.2
Total 1235.4 560.4 700.5 16.8 7.6
2 Pratt & Whitney turbine engines PW206B2
2 TURBOMECA turbine engines - ARRIUS 2B2
Thermodynamic limits per engine at SL, ISA kW ch shp
Take-Off Power (TOP) 498 677 667
Maximum Continuous Power (MCP) 457 621 612
Take-Off Power (TOP) 473 643 634
Maximum Continuous Power (MCP) 442 601 592
135.06.101.01 E 10
2.7 Main transmission ratings
Single engine operation kW ch shp
30 sec OEI-power 1 x 526 1 x 715 1 x 705
2.0 min OEI-power 1 x 513 1 x 698 1 x 687
Maximum continuous OEI-power 1 x 368 1 x 501 1 x 493
Twin engine operation
Take-Off Power (TOP) 2 x 320 2 x 435 2 x 429
Maximum Continuous Power (MCP) 2 x 283 2 x 385 2 x 380
135.06.100.01 E 11
3 Standard aircraft definition
Energy absorbing fuselage
Tail boom with fixed horizontal stabilizer and two end-
Vertical fin with faired-in fenestron
Upper deck with fittings for main gearbox, engines,
hydraulic and cooling system
Cowlings for main transmission and engines
Skid-type landing gear with skid protectors, capable of
taking ground-handling wheels
Long boarding steps, LH and RH
Maintenance built-in steps and grips
Exterior painting (single color)
COCKPIT, CABIN AND CARGO COMPARTMENT
One-level cabin and cargo compartment floor with
Two hinged cockpit doors with sliding window
Map case in pilot's door
Two wide passenger sliding doors
Two rear hinged clam-shell doors
Longitudinally adjustable energy absorbing pilot and copilot
seats with head rest and 4-point safety belts with automatic
Cabin boarding grips (LH and RH)
Interior paneling with integrated basic sound insulation
Flight controls (pilot side)
Engine controls with manual engine back-up system at
pilot's collective pitch lever
Instrument panel with extension on pilot's side and glare
Ram-air and electrical ventilating system for cockpit and
Headset holder in the cockpit
Headset holder in the cabin
Stowage net for first aid kit at the LH rear clam-shell door
4 Mobile tie-down rings
Central Panel Display System (CPDS), consisting of:
Caution Advisory Display (CAD) with indication of:
Caution and advisory information
Vehicle and Engine Management Display (VEMD) with
Engine parameters (N1-RPM (for P&W) or N1-RPM
(for TM), oil pressure, oil temperature, Turbine Outlet
Temperature (TOT), engine/FADEC rep EEC failure
and parameter code messages, self diagnoses)
FLI (First Limit Indicator) for TQ, TOT, N1 (for P&W)
or N1 (for TM) as analogue display
Main transmission parameters (oil pressure, oil temp.)
Dual ammeter (generator)
Ammeter (battery)
Parameters of optional equipment (e.g. internal long
range fuel tank)
Engine cycle counter (on flight report page)
Triple (rotor and engines) RPM-indicator (2)
Standard instruments: (single pilot) 1)
Encoding altimeter (3")
Airspeed indicator (3")
Vertical speed indicator (3")
Warning unit:
Engine fire warning with fuel emergency shut-off
Main switch panel:
Digital engine control (FADEC)
Pitot / static system with electrical heated pitot tube, pilot
Static pressure crossover system
1) If glass cockpit instrumentation is chosen as optional equipment, these standard instruments are deleted and an altimeter (2)
and an airspeed indicator (2) as back-up instruments are added.
Two PRATT & WHITNEY PW206B2 turbine engines or
Two TURBOMECA ARRIUS 2B2 turbine engines
These 2 engines are equipped with:
electronic engine control (FADEC-BOX)
chip detectors with quick-disconnect plugs
twin-engine OEI-training mode
Oil cooling and lubricating system with thermostatic valve
Crash resistant fuel system with a flexible bladder-type fuel
main tank and supply tank (split into two sections)
Automatically controlled variable rotor speed system
Fuel tank filler flap, lockable
135.06.100.01 E 12
Flat-shaped main gearbox with two stages
Chip detector system with quick-disconnect plug (main
Redundant oil cooling and lubrication system
Main gearbox attachment with Anti-Resonance Isolation
System (ARIS)
Free wheel assemblies in the engine input drives
Tail rotor gearbox with splash lubrication and oil level sight
Chip detector system with quick-disconnect plug (tail rotor
ROTOR AND FLIGHT CONTROLS
Bearingless Main Rotor system (BMR), consisting of:
Rotor head/mast in one piece
Four fiber-reinforced composite main rotor blades with
anti-erosion strips, control cuff, elastomeric lead-lag
dampers and special blade tip painting
Main rotor control system with dual hydraulic boost system
Electrical trim system (cyclic)
Basic provisions for an easy integration of a track and
Fenestron-type tail rotor with ten metal blades (asymmetric
blade spacing) and stator
Tail rotor gearbox cover
Tail rotor control system with flexball cable and single
Yaw-SAS (Stability Augmentation System)
Mast moment system
Two starter/generators (2 x 160 A, 28 VDC)
Nickel-Cadmium battery, (24 V, 17 Ah)
External power connector (STANAG 3302)
Two primary busbars
Two shedding busbars
Two essential busbars
Two high load busbars (80 A) - for optional equipment
Two high power busbars (200 A)
One utility receptacle in LH side of cargo compartment
Anti-collision warning light (red flashing)
Fixed, nose-mounted landing light (250 W)
Three position lights (red, green, white)
One utility light in the cockpit
5 spot-lights in the cabin
One light in cargo compartment RH side
GROUND HANDLING KIT
Two ground-handling wheels
Basic aircraft covers (short time)
Main rotor blade tie-down lash bags
Fuel tank drain device
Keys for cockpit doors, cabin doors, baggage compartment
doors and tank flap (one-key system)
Pilots-Checklist
CD-ROM including AMM, SDS, MSM, WDM, IPC
1) 2 3
Master Servicing Manual (MSM)
Service Bulletin Catalogue (SB)
Avionics Manual (for avionics installed by Eurocopter)
STANDARD DOCUMENTATION (contd.):
OPTIONAL DOCUMENTATION (hard copy format):
System Description Section (SDS)
Weight not included in the standard helicopter empty weight
Documents revision service included for 5 years
135.06.101.01 E 13
4 Basic configuration choice
Selection of a PINAO package
Please select your PINAO code according to your operational needs by using the following table:
Single Dual Single/Dual
* This offered equipment package is derived from JAR-OPS 3 Amendment 3. It does not
cover oxygen equipment and equipment required for over water operations. As the
national operating rule may differ from the JAR-OPS 3 Amendment 3, the operator has
to contact its national authority to assure that the planned equipment configuration is
acceptable for the intended kind of operation.
P I N A O
Use this code to find your required PINAO packages on the following pages.
As a general guidance, use the diagram on the next page
One PINAO code may lead to different PINAO packages
Avionics solutions 2, 5 and 6 are no more available.
For IFR, there is no difference between day and night. Therefore only IFR night PINAO
packages are listed.
All possible PINAO codes are listed in the following pages.
Weight margin in this chapter: 3 %
For all intercom systems, the following impedances are standard: LOW IMPEDANCE
Microphone: 5 (dynamic) / Headset: 8 (military - EUROCOPTER typical)
135.06.101.01 E 14
Use this diagram to find the appropriate Avionics Solution
based on your individual PINAO selection.
(PINAO codes x0xxx)
(PINAO codes x1xxx)
MEGHAS / FCDS
(codes 20xxx are
included in 30xxx)
(PINAO codes 21xxx)
21xxx or 31xxx
(PINAO codes 11xxx)
Avionics Solution 3
Avionics Solution 4
Avionics Solution 7
Avionics Solution 8
Avionics Solution 11
Avionics Solution 9
Avionics Solution 10
(see page 36
Avionics Solution 12
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4.1 VFR packages (based on Avionics Solution 1)
4.1.1 Instrument panel overview
A - for 2 back-up airspeed indicator (used in MEGHAS/FCDS Glass cockpit solutions)
B - for 2 standby horizon AI 804 DC
C - for 2 back-up altimeter (used in MEGHAS/FCDS Glass cockpit solutions)
D - e.g. for 3 RMI
E - e.g. for DME or ELT remote control
G - e.g. for 2nd gyro 205 1BL (GOODRICH)
M - e.g. for marker lights
R - e.g. for 3 radar altimeter indicator (KNI 416)
S - e.g. for 2nd GPS/COM/NAV GNS430 or other equipment
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4.1.2 Content of Avionics Solution 1 (basic for all VFR PINAO packages)
L2300-001-04 Avionics Solution 1, consisting of:
08-16053-A L2341-192-01 Audio/Comm. control system (pilot) AS 3100-12 (BECKER)
incl. Intercom Select Panel (ICS mode selector)
08-16053-A L2341-293-01 Intercom amplifier IC 3100-4 (BECKER)
08-22026-A L2325-092-12 Transponder (Mode S) GTX 330 (GARMIN)
08-29003-A L2480-090-01 Avionics/Radio master switches (Special ECD)
08-43018-B L3442-092-00 GPS / NAV / COM GNS 430, pilot (GARMIN)
with I-panel annunciation/switch unit MD 41 (MIDCONTINENT)
08-51012-A L3425-092-02 4" Artificial horizon GH14-391, pilot (HONEYWELL)
08-52013-A L3421-092-02 Gyro Magnetic Heading System KCS 55 A (HONEYWELL)
incl. KG-102A, KMT-112, KA-51B with HSI KI-525A, pilot
08-99000-A L0000-150-01 Avionics Solution 1 interconnection / wiring
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4.1.3 Minimum required equipment
Minimum required equipment for Avionics Solution 1 Single pilot PINAO
(margin 3 %)
05-03007-A L2562-001-00 First aid kit 1.3 2.9 X X X
05-22008-A L2621-001-00 Engine fire extinguishing system 3.6 7.9 X X X X
05-33001-A L3113-001-00 Slant panel 0.8 1.8 X X X X X X X
05-33002-A L3113-004-00 Center console 2.3 5.1 X X X X X X X
05-41004-B L2104-100-00 Bleed air heating system
6.6 14.6 X X X X X X X
05-44002-A L2122-001-00 Ventilation extruder
without copilot I-panel extension
05-61010-A L2433-003-00 Battery, type "Saft", ULM, 27 Ah,
24 V instead of standard battery
05-62010-B L2420-002-00 AC System (350VA) 3.2 7.1 X X X X X X X
05-63003-A L2432-001-00 Starter/generators
(2 x 200 A, 28 VDC), instead of
06-45023-A L3343-003-00 Landing & search light, 450 W 3.4 7.5 X X X
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX)
incl. NAV. opt.
08-00001-A L2300-001-04 Avionics Solution 1 39.7 87.5 X X X X X X X
08-21014-A L3441-090-04 Radar altimeter KRA 405B
08-21014-A L3441-092-03 Radar altimeter indicator KNI 416
08-51013-A L3425-806-51 2 std-by horizon AI 804 DC
(GOODRICH) with emergency
for VFR flights on routes not navigated by reference to visual landmarks, a 2nd GPS/NAV/COM
GNS430 (see possible add-ons) is required.
For helicopters dedicated for EMS select Bleed air heating system: EMS version L2104-003-00
(05-41004-A) (7.0 kg / 15.4 lb.)
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Minimum required equipment for Avionics Solution 1- Single/Dual pilot PINAO
05-37016-A L6701-001-00 Copilot flight controls 6.0 13.2 X X X X X X X
05-38010-A L3111-001-00 10" copilot instrument panel with glare shield 2.8 6.2 X X X X X X X
05-61010-A L2433-003-00 Battery, type "Saft", ULM, 27 Ah, 24 V instead
of standard battery
05-63003-A L2432-001-00 Starter/generators (2 x 200 A, 28 VDC),
instead of standard generators
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. opt. 3.8 8.4 X X X
08-16053-A L2341-191-01 Audio/Comm. control system (2nd station -
copilot) AS 3100-12 (BECKER)
08-21014-A L3441-090-04 Radar Altimeter KRA 405B (HONEYWELL) 4.8 10.6 X X X X
08-51012-A L3425-091-02 4" artificial horizon GH14-391, copilot
08-51013-A L3425-806-51 2 std-by horizon AI 804 DC (GOODRICH) with
08-52010-A L3421-091-02 2nd directional Gyro (3 unslaved indicator)
205 1BL on copilot side (GOODRICH)
08-54001-A L3411-001-00 Copilot pitot static system 1.4 3.1 X X X X X X X
08-60003-A L3412-002-00 Copilot 3" instruments (airspeed indicator,
altimeter, vertical speed indicator (UNITED
08-61010-A L3166-091-04 RMI KI 229, copilot (HONEYWELL) 2.3 5.1 X X X X X X X
08-61011-A L3167-091-02 CDI KI 204, copilot (HONEYWELL) 1.2 2.6 X X X X X X X
(05-41004-A) alternatively (7.0 kg / 15.4 lb.)
135.06.101.01 E 20
4.1.4 Possible add-ons
Possible add-ons for Avionics Solution 1 Single Pilot PINAO
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. opt. 3.8 8.4 X X X X
08-16053-A L2341-191-01 Audio/Comm. control system
(2nd station - copilot) AS 3100-12 (BECKER)
08-21014-A L3441-090-04
L3441-092-03
Radar altimeter KRA 405B (HONEYWELL)
Radar altimeter indicator KNI 416
08-25014-A L3455-092-03
L3169-092-02
DME KN 63
DME indicator KDI 572 (HONEYWELL)
08-26010-A L3431-092-02 Marker Beacon receiver / lights KR 21
08-51013-A L3425-806-51 2 std-by horizon AI 804 DC (GOODRICH)
incl. back-up battery
08-71002-B L2217-001-10 VFR SAS
(VFR pitch/roll Stability Augmentation System)
8.5 18.8
135.06.101.01 E 21
Possible add-ons for Avionics Solutions 1
Single - Dual pilot
08-43018-B L3442-091-00
L3167-091-01
GPS/NAV/COM GNS 430, copilot (GARMIN)
with I-panel annunciation/switch unit MD 41
(MIDCONT.)
CDI KI206 instead of CDI KI 204 (HONEYWELL)
included back-up battery
4.1.5 On request items
Multifunction display KMD 850 (HONEYWELL) for weather radar or digital map
Color weather radar RDR2000 (HONEYWELL) on KMD850 display
Moving Map EURONAV IV - RN6 (EURO AVIONICS)
4.1.6 Further avionics add-ons see chapter 6 page 64
4.2 Dual pilot IFR packages, conventional instrumentation, basic
(based on Avionics Solution 3)
4.2.1 Instrument panel overview
D - e.g. for 3 RMI or 3 CDI
S - e.g. for tactical or other optional equipment
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135.06.101.01 E 23
4.2.2 Contents of Avionics Solution 3
L2300-003-04 Avionics Solution 3, consisting of:
08-16053-A L2341-191-01 Audio/Comm. control system (2nd station - copilot) AS 3100-12
08-25014-A L3169-092-02 DME indicator KDI 572 (HONEYWELL)
08-25014-A L3455-092-03 Distance measuring equipment KN 63 (HONEYWELL)
VOR / ILS /MKR receivers
08-26010-A L3431-092-02 Marker beacon receiver / lights KR 21(HONEYWELL)
08-43018-B L3442-091-00 GPS / NAV / COM GNS 430, copilot (GARMIN)
08-51012-A L3425-091-02 4" Artificial horizon GH14-391, copilot (HONEYWELL)
08-51013-A L3425-806-51 2 Stand-by horizon AI 804 DC incl. battery (GOODRICH)
08-52014-A L3421-092-01 Gyro Magnetic Heading System C14D (HONEYWELL)
08-60003-A L3412-002-00 Copilot 3" instruments (airspeed indicator, altimeter, vertical speed
indicator (UNITED INSTRUMENTS)
08-61012-A L3165-091-01 Horizontal Situation Indicator - KPI 552, copilot (HONEYWELL)
08-61012-A L3165-092-01 Horizontal Situation Indicator - KPI 552, pilot (HONEYWELL)
08-99000-A L0000-150-03 Avionics Solution 3 interconnection / wiring
135.06.101.01 E 24
4.2.3 Minimum required equipment
Minimum required equipment for Avionics Solution 3 PINAO
05-03007-A L2562-001-00 First aid kit 1.3 2.9 X
05-22008-A L2621-001-00 Engine fire extinguishing system 3.6 7.9 X X
05-33001-A L3113-001-00 Slant panel 0.8 1.8 X X X
05-33002-A L3113-004-00 Center console 2.3 5.1 X X X
05-37016-A L6701-001-00 Copilot flight controls 6.0 13.2 X X X
05-38010-A L3111-001-00 10 copilot instrument panel with glare shield 2.8 6.2 X X X
05-39006-A L2514-003-01 Map case in copilot door 0.5 1.1 X X X
05-39007-A L3111-001-10 Map case on instrument panel glare shield 0.6 1.3
05-39008-A L3113-004-10 Illuminated chart holder for pilot side 0.9 2.0 X
6.6 14.6 X X X
05-61010-A L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V
instead of standard battery
16.8 37.0
05-62010-B L2420-003-00 Dual AC System (2 x 350VA) 6.6 14.6 X X X
instead of standard one
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. opt. 3.8 8.4 X
08-00002-A L2300-003-04 Avionics Solution 3 78.1 172.2 X X X
08-21014-A L3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 4.8 10.6 X X
205 1BL (GOODRICH) on copilot side
08-54001-A L3411-001-00 Copilot pitot static system 1.4 3.1 X X X
08-71002-B L2217-001-50 IFR pitch/roll SAS 12.2 26.9 X X X
(05-41004-A) (7.0 kg / 15.4 lb.).
135.06.101.01 E 25
4.2.4 Possible add-ons
Possible add-ons for Avionics Solution 3 PINAO
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. opt. 3.8 8.4 X X
08-24015-A L3452-092-17
L3452-092-08
ADF system DFS-43A (CHELTON/WULFSBERG)
ADF control unit CD-432B (CHELTON/WULFSBERG)
4.2.5 On request items
Multifunction display KMD 850 (HONEYWELL)for weather radar or digital map
4.2.6 Further avionics add-ons see chapter 6 page 64
4.3 Dual pilot IFR packages, conventional instrumentation,
enhanced (based on Avionics Solution 4)
4.3.1 Instrument panel overview
F - e.g. for ADF control unit (CD-432B)
P - e.g. for 3 CDI or 3 RMI
S / T - e.g. for GPS receiver or other optional equipment
135.06.101.01 E 26
135.06.101.01 E 27
4.3.2 Contents of Avionics Solution 4
L2300-004-04 Avionics Solution 4, consisting of:
08-11023-A L2313-091-03 VHF AM/COM. system, copilot KTR 908/KFS 598 A (HONEYWELL)
08-11023-A L2313-092-03 VHF AM/COM system, pilot KTR 908 / KFS 598A (HONEYWELL)
08-22027-A L2325-092-06 Transponder (Mode S) MST 67A (HONEYWELL)
08-22027-A L2325-092-15 Transponder control unit PS 578A (HONEYWELL)
08-25025-A L3455-092-01 Distance measuring equipment KDM 706 A (HONEYWELL)
08-26025-A L3432-091-03 VOR/ILS/MKR Navigation system, copilot KNR 634 A / KFS 564 A
08-26025-A L3432-092-03 VOR/ILS/MKR Navigation system, pilot KNR 634 A / KFS 564 A
08-26028-A L3431-092-01 Marker beacon lights KA 35 A (HONEYWELL)
08-99000-A L0000-150-04 Avionics Solution 4 interconnection / wiring
135.06.101.01 E 28
4.3.3 Minimum required equipment
Minimum required equipment for Avionics Solution 4 PINAO
05-34002-A L2576-001-00 Avionics compartment 4.2 9.3 X X X
05-39007-A L3111-001-10 Map case on instrument panel glare shield 0.6 1.3 X X X
instead of std one
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. opt.
(GPS receiver required)
08-00003-A L2300-004-04 Avionics Solution 4 78.3 172.6 X X X
08-21014-A L3441-092-03 Radar altimeter indicator KNI 416 (HONEYWELL) 1.2 2.6 X X
135.06.101.01 E 29
4.3.4 Possible add-ons
Possible add-ons for Avionics Solution 4 PINAO
Radar altimeter indicator KNI 416 (HONEYWELL)
ADF control unit CD-432B CHELTON/WULFSBERG
08-43017-A L3442-092-12 GPS Nav. system 2101 I/O Approach Plus
6.0 13.2
08-63009-A L3442-092-80 GPS indication on HSI (KPI 552) 2.9 6.4 X X X
4.3.5 On request items
4.3.6 Further avionics add-ons see chapter 6 page 64
4.4 Dual Pilot or Single/Dual Pilot IFR Glass Cockpit, based on
4.4.1 Instrument panel overview
Avionics Solution 7 Avionics Solution 8 Avionics Solution 11
M - Marker beacon lights for Avionics Solution 11
S - e.g. or other optional equipment
T - e.g. for autopilot (DAFCS) control unit or other optional equipment
U - for GPS annunciation / switch unit
V - for Video Radar Unit (brightness control for external video source e.g. moving map, FLIR, weather
135.06.101.01 E 30
135.06.101.01 E 31
4.4.2 Contents of Avionics Solutions 7, 8 and 11
L2300-007-04 Avionics Solution 7, consisting of
08-11023-A L2313-091-03 VHF AM/ COM. system, copilot KTR 908 / KFS 598 A (HONEYWELL)
08-16053-A L2341-191-01 Audio/Comm. control system (2nd station - copilot) AS 3100-12 (BECKER)
08-25022-A L3455-090-02 Distance measuring equipment DMS-44A (CHELTON/WULFSBERG)
VOR/ILS/MKR receivers
08-65003-A L3161-090-09 MEGHAS - Flight Control Display System (FCDS) - Dual (4xSMD45)
08-99000-A L0000-150-07 Avionics Solution 7 interconnection / wiring
135.06.101.01 E 32
L2300-008-04 Avionics Solution 8, consisting of
08-11022-A L2313-091-08 VHF AM/COM system, copilot VCS-40 A (CHELTON/WULFSBERG)
08-11022-A L2313-091-13 Control unit CD 402 B, copilot (CHELTON/WULFSBERG)
08-11022-A L2313-092-07 VHF AM/COM system, pilot VCS-40 A (CHELTON/WULFSBERG)
08-11022-A L2313-092-13 Control unit CD 402 B, pilot (CHELTON/WULFSBERG)
08-26024-A L3432-091-06 VOR/ILS/MKR Navigation system, copilot VNS-41 A
(CHELTON/WULFSBERG)
08-26024-A L3432-091-09 Control unit CD 412 B, copilot (CHELTON/WULFSBERG)
08-26024-A L3432-092-07 VOR/ILS/MKR Navigation system, pilot VNS-41 A (CHELTON/WULFSBERG)
08-26024-A L3432-092-12 Control unit CD 412 B, pilot (CHELTON/WULFSBERG)
08-99000-A L0000-150-08 Avionics Solution 8 interconnection / wiring
L2300-011-02 Avionics Solution 11, consisting of:
08-22026-A L2325-092-12 Transponder (Mode S) GTX330 (GARMIN)
08-26010-A L3431-092-02 Marker beacon receiver/lights KR 21(HONEYWELL)
08-43018-B L3442-091-07 GPS / NAV / COM GNS 430, copilot (GARMIN) interfaced with FCDS
(GPS stand-alone)
08-43018-B L3442-092-07 GPS / NAV / COM GNS 430, pilot (GARMIN) interfaced with FCDS
08-99000-A L0000-150-11 Avionics Solution 11 interconnection / wiring
- NVG friendly version of
Avionics Solutions 7, 8
- Exchange of 2x SMD45
on copilot side to one
135.06.101.01 E 33
135.06.101.01 E 34
4.4.3 Minimum required equipment
Minimum required equipment for Avionics Solution 7, 8 and 11 PINAO
05-03007-A L2562-001-00 First aid kit 1.3 2.9 X X
05-33001-A L3113-001-00 Slant panel 0.8 1.8 X X X X X X
05-33002-A L3113-004-00 Center console 2.3 5.1 X X X X X X
05-34002-A L2576-001-00 Avionics compartment 4.2 9.3 X X X X X X
05-37016-A L6701-001-00 Copilot flight controls 6.0 13.2 X X X X X X
05-38010-A L3111-001-04 7 copilot instrument panel with glare shield 2.7 6.0 X X X X X X
05-39006-A L2514-003-01 Map case in copilot door 0.5 1.1 X X X X X X
05-39007-A L3111-001-10 Map case on instrument panel glare shield 0.6 1.3 X X X X X X
05-39008-A L3113-004-10 Illuminated chart holder for pilot side 0.9 2.0 X X
6.6 14.6 X X X X X X
05-62010-B L2420-005-00 AC System (50VA)
1.9 4.2 X X X X X X
06-12008-B L3217-001-00 Reinforced rear landing gear cross tube
(standard landing gear only)
06-45023-A L3343-003-00 Landing & search light, 450 W 3.4 7.5 X X X X X X
(GPS is required)
08-00004-A
08-00005-A
08-00022-A
L2300-007-04
L2300-008-04
L2300-011-02
08-21014-A L3441-090-04 Radar Altimeter KRA 405B (HONEYWELL) 4.8 10.6 X X X X X
08-53002-B L2212-400-00 MEGHAS sensor kit 17.8 39.3 X X X X X X
08-54001-A L3411-001-00 Copilot pitot static system 1.4 3.1 X X X X X X
08-72001-B L2212-001-00 Digital Automatic Flight Contr. Syst. - DAFCS 27.0 59.6 X X X
For helicopters dedicated for EMS select Bleed air heating system:
EMS version L2104-003-00 (05-41004-A) (7.0 kg / 15.4 lb.).
Alternatively the AC system L2420-002-00 (05-62010-B) (350VA; 3.2kg) can be selected
135.06.101.01 E 35
4.4.4 Possible add-ons
Possible add-ons for Avionics Solution 7, 8 and 11 PINAO
08-21014-A L3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 4.8 10.6 X
ADF system DFS-43A CHELTON/WULFSBERG
ADF control unit CD-432B CHELTON/WULFSB.
08-31019-A L3443-090-02
L2571-001-00
Color weather radar RDR2000 (HONEYWELL)
(VRU
required) see below
Radar radome (for RDR2000)
08-31034-A L3443-004-00
L2571-002-00
Search and rescue weather radar RDR1600
(TELEPHONICS) (VRU
Radar radome (for RDR1600)
(only possible for Avionics Solutions 7 and 8)
08-46007-A L3168-090-17 Digital moving Map DKG 4 (DORNIER)
basic version without options
(VRU and GPS receiver required)
(Enhanced options and maps on request)
08-46020-B L3168-092-04 Digital moving Map EURONAV IV - RN6
(EURO AVIONICS),
8.0 17.6
08-65004-A L3443-010-00 Video Radar Unit (VRU) for weather radar or
digital moving map indication on FCDS
(SMD45/SMD68)
5.6 12.3
08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS
(Radar altimeter required)
31.0 68.3
of IFR
08-81018-A L2321-007-00
Cockpit Voice and Flight Data
Recorder (CVFDR), ground station not included
(in combination with UMS: 18.3 kg / 40.3 lb)
17.3 38.1
08-83007-A L3171-001-00
Usage Monitoring System (UMS),
ground station not included
4.4.5 Further avionics add-ons see chapter 6 page 64
Tactical mission equipment can not be certified by German Civil Aviation Authorities. Eurocopter will
ensure that the equipment is compatible with the basic helicopter and will assist the customer in
obtaining certification or acceptance approval in his country.
4.5 Single Pilot IFR Glass Cockpit,
based on Avionics Solution 9, 10 or 12
4.5.1 Instrument panel overview
Avionics Solution 9 Avionics Solution 10 Avionics Solution 12
D - e.g. for radar altimeter indicator, stormscope
M - Marker beacon lights for Avionics Solution 12
S / T - e.g. for GPS or other optional equipment
V - for Video Radar Unit (brightness control for external video source e.g. moving map, FLIR,
weather radar)
135.06.101.01 E 36
135.06.101.01 E 37
4.5.2 Contents of Avionics Solution 9, 10 and 12
L2300-009-04 Avionics Solution 9, consisting of:
08-61011-A L0000-200-12 Back-up indicator CDI KI 204 (HONEYWELL),
Back-up indicator SD 442 B (CHELTON / WULFSBERG)
08-65003-A L3161-092-03 MEGHAS - Flight Control Display System (FCDS) - Single (2xSMD45)
08-99000-A L0000-150-09 Avionics Solution 9 interconnection / wiring
135.06.101.01 E 38
L2300-010-04 Avionics Solution 10, consisting of:
08-99000-A L0000-150-10 Avionics Solution 10 interconnection / wiring
135.06.101.01 E 39
L2300-012-02 Avionics Solution 12, consisting of:
08-43018-B L3442-091-07 GPS / NAV / COM GNS 430, copilot (GARMIN) interfaced with FCDS (GPS
08-99000-A L0000-150-12 Avionics Solution 12 interconnection / wiring
- NVG friendly version of Avionics Solutions 9, 10 and 12
135.06.101.01 E 40
4.5.3 Minimum required equipment
Minimum required equipment for Avionics Solution 9, 10 and 12 PINAO
05-44002-A L2122-001-00 Ventilation extruder w/o copilot I-panel extension 0.3 0.7 X X X
1.9 4.2 X X X
06-67044-A L2563-801-06 ELT C406-N HM (ARTEX) incl. NAV. Opt
08-00006-A
08-00007-A
08-00023-A
L2300-009-04
L2300-010-04
L2300-012-02
08-21014-A L3441-090-04 Radar altimeter KRA 405B (HONEYWELL) 4.8 10.6 X X X
08-53002-B L2212-400-00 MEGHAS sensor kit 17.8 39.3 X X X
08-72001-B L2212-001-00 Digital Automatic Flight Control System - DAFCS 27.0 59.6 X X X
EMS version L2104-003-00 (05-41004-A) (7.0 kg / 15.4 lb.)
135.06.101.01 E 41
4.5.4 Possible add-ons
Possible add-ons for Avionics Solutions 9, 10 and 12 PINAO
ADF control unit CD-432B (CHELTON/WULFSB.)
(FREE FLIGHT, only possible for Avionics Solutions 9, 10)
(EURO AVIONICS) basic version without options
08-65004-A L3443-010-00 Video Radar Unit (VRU) for weather radar or digital
moving map indication on FCDS (SMD45/SMD68)
(CVFDR), ground station not included
MARMS MARMS
(UMS), ground station not included
4.5.5 Further avionics add-ons see chapter 6 page 64
135.06.101.01 E 42
4.6 Antenna layouts
4.6.1 Typical VFR antenna layout
1 ELT antenna
2 ATC antenna
3 VOR antennas
4 VHF 1 antenna
5 GPS antenna
4.6.2 Typical IFR antenna layout
2 VHF2 antenna
4 VHF1 antenna
(6 ADF antenna (if required))
7 Radar altimeter antenna
8 ATC antenna
9 Marker antenna
10 DME antenna
135.06.101.01 E 43
135.06.101.01 E 44
135.06.101.01 E 45
5 Cabin arrangement
5.1 Passenger transport
5.1.1 Six (6) Passenger transport (Recommended configuration)
This installation is characterized by:
reference Title kg lb
07-27001-A L2522-001-00 Three (3) forward passenger seats, facing backwards 37.4 82.5
In combination with either
07-27004-A L2522-004-10 Utility seats for 3 rear passengers, model Eurocopter, fixed
07-27004-A L2522-004-20 Utility seats for 3 rear passengers, model Eurocopter, detachable
33.2 73.2
07-27005-A L2522-008-00 Utility seats for 3 rear passengers, model aerolite 37.0 81.6
3 forward passenger seats
Model Eurocopter model Aerolite
135.06.101.01 E 46
5.1.2 Five (5) Passenger transport (Recommended configuration)
07-27001-A L2522-001-00 Three (3) forward passenger seats, facing backwards 37.4 81.6
07-27001-A L2522-002-00 Two (2) rear passenger seats, facing forwards 22.2 49.0
07-50036-A L2514-012-00 Covers for sliding door fairing LH/RH 0.1 0.2
07-60014-A L2514-013-00 Map case in sliding doors LH/RH 1.4 3.1
07-60015-A L2514-014-00 Variable tie-down web for luggage securing 4.2 9.3
07-90006-A L2514-011-00 Retractable coat hooks (2ea) in rear cabin
(if avionics compartment is installed, only)
135.06.101.01 E 47
135.06.101.01 E 48
5.1.3 Corporate / VIP passenger transport
5.1.3.1 Five (5) corporate passenger transport (Recommended configuration)
07-81015-A L2525-101-11 VIP-pilot seat (instead of std. pilot seat) 1.1 2.4
07-81015-A L2525-101-21 VIP-copilot seat (instead of std. copilot seat) 1.1 2.4
07-81013-A L2525-102-00 4 VIP passenger seats (2 front and 2 rear) 56.1 123.7
07-81013-A L2525-202-20 1 VIP passenger seat (front, middle) 14.2 31.3
07-85003-A L2526-112-710 Rear cabinet with armrest 10.0 22.2
07-83003-A L2525-104-00 VIP carpet for cockpit, cabin and cargo compartment 16.6 36.6
07-82010-A L2525-102-62 Armrest in rear window niche LH / RH 0.8 1.8
07-86001-A L2525-100-35 Special painted interior 0.1 0.2
5.1.3.2 Four (4) VIP passenger transport (Recommended configuration)
07-85002-A L2526-212-601 Front cabinet, flat 14.5 32.0
07-86002-A L2525-112-35 Leather covered interior 13.4 29.5
07-60015-A L2514-014-00 Variable tie-down web for luggage securing 3.8 8.4
135.06.101.01 E 49
135.06.101.01 E 50
5.1.3.3 Customer specific Corporate / VIP solutions
Customer specific solutions can be defined by using the following table.
Note: Only one item per line can be selected.
VIP pilot seat
07-81015-A L2525-101-11
(1.1 kg / 2.4 lb.)
VIP pilot seat height
07-81015-A L2525-101-71
(4.8 kg / 10.6 lb.)
VIP copilot seat
07-81015-A L2525-101-21
VIP copilot seat height
07-81015-A L2525-101-76
4 VIP passenger seats
07-81013-A L2525-102-00
(56.1 kg / 123.7 lb.)
1 VIP passenger seat (front,
07-81013-A L2525-202-20
(14.2 kg / 31.3 lb.)
Front cabinet, flat
07-85002- A L2526-212-601
(14.5 kg / 32.0 lb.)
Front cabinet, middle
07-85002-A L2526-112-63
(22.5 kg / 49.6 lb.)
06-65004-A L2625-003-00
(2.8 kg / 6.2 lb.)
Table for front cabinet
07-85002-A L2526-112-61 (3.0 kg / 6.6 lb.)
Cooling box for front cabinet
07-85002-A L2526-112-62 (2.5 kg / 5.5 lb.)
Rear cabinet with Armrest
07-85003-A L2526-112-710
(10.0 kg / 22.2 lb.)
Rear cabinet, flat
07-85004-A L2526-312-701
(8.6 kg / 19.0 lb.)
Rear cabinet, high
07-85004-A L2526-112-75
(14.0 kg / 30.9 lb.)
Armrests in rear window
niche, LH/RH
07-82010-A L2525-102-62
(0.8 kg / 1.8 lb.)
135.06.101.01 E 51
Special painted interior
07-86001-A L2525-100-35
(0.1 kg / 0.2 lb.)
Leather covered interior
07-86002-A L2525-112-35
(13.0 kg / 28.7 lb.)
VIP carpet for cockpit, cabin and cargo compartment
07-83003-A L2525-104-00 (16.6 kg / 36.6 lb.)
Retractable coat hooks (2ea) in rear cabin
07-90006-A L2514-011-00 (0.1 kg / 0.2 lb.)
Map case in sliding doors LH/RH
07-60014-A L2514-013-00 (1.4 kg / 3.0 lb.)
Variable tie-down web for luggage securing
07-60015-A L2514-014-00 (4.2 kg / 9.3 lb.)
Covers for sliding door fairing LH/RH
07-50036-A L2514-012-00 (0.1 kg / 0.2 lb.)
Control covers painted in harmony with carpet
(if copilot flight controls are selected, only)
07-90008-A L2525-101-65 (-2.3 kg / -5.1 lb.)
Fabric protection cover for 1 VIP pilot seat
07-90007-A L2525-111-50 (GSE)
Fabric protection cover for 1 VIP pax seat
07-90007-A L2525-112-91 (GSE)
Plastic protection cover for cockpit carpet
07-90007-A L2525-111-60 (GSE)
Plastic protection cover for cabin carpet
07-90007-A L2525-112-92 (GSE)
05-42019-A L2105-001-00
(58.7 kg / 129.4 lb.)
Air conditioning system for tropical
environment + Special ducting for
front pax. seats
05-42020-A
L2105-001-10 + L2525-112-46
(63.0 kg / 138.6 lb.)
Enhanced sound proofing kit
07-30012-A L2581-001-00
(6.0 kg / 13.2 lb.)
Pax / cargo compartment separation wall
(requires Avionics compartment)
07-30012-A L2524-001-00
(3.9 kg / 8.6 lb.) +
05-34002-A L2576-001-00
(4.2 kg / 9.3 lb.)
135.06.101.01 E 52
5.2 EMS equipment
5.2.1 Single stretchers
07-74011-A L8522-320-00 Folding stretcher (16 G) - Bucher-Leichtbau (STC) 12.0 26.5
07-74011-A L8522-350-00 Installation device for one stretcher (16 G) in full length only -
Bucher-Leichtbau (STC)
07-74032-A AL2013-009-10 Stretcher LH - Cirrus 1000 (three-piece), fixed provisions
Aerolite (STC)
07-74032-A AL2013-009-20 Stretcher LH - Cirrus 1000 (three-piece), detachable parts
5.2.2 Packages from Aerolite
5.2.2.1 Quick change EMS kit Aerolite (STC)
5.2.2.1.1 Content:
07-70028-A AL2035-001 Quick change EMS kit Aerolite (STC) consisting of: 33.5 73.9
1 Life support module oxygen
1 Stretcher LH - Cirrus 2000 (foldable), detachable parts
1 Stretcher LH - Cirrus 2000 (foldable), fixed provisions
1 Tie down web
5.2.2.1.2 Minimum required equipment:
Middle seat (11 kg / 24.3 lb.) has to be removed.
5.2.2.1.3 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
5.2.2.1.4 Optional equipment:
07-27008-A L2522-160-00 One (1) rear RH passenger seat in FWD 11.1 24.4
135.06.101.01 E 53
5.2.2.2 Rescue EMS kit Aerolite (STC)
5.2.2.2.1 Content:
07-70029-A AL2035-002 Rescue EMS Kit Aerolite (STC) consisting of: 100.0 220.5
1 Ceiling rails LH
1 DC power and lighting System
1 Integral floor, detachable parts
1 Integral Floor, fixed provisions
1 Life support panel LH
1 Med oxygen system 3x3 Lt., detachable parts
1 Med oxygen system 3x3 Lt., fixed provisions
1 Med rack rear LH, detachable parts
1 Med rack rear LH - fixed provisions
1 Med suction system, detachable parts
1 Med suction system, fixed provisions
1 Pax seat cover - fixed provisions
1 Pax seat cover, detachable parts
1 Stationary seat FWD RH, detachable parts
1 Stationary seat FWD RH, fixed provisions
1 Stretcher LH - Cirrus 2000, detachable parts
1 Stretcher LH - Cirrus 2000, fixed provisions
5.2.2.2.2 Minimum required equipment:
07-77001-A L8521-001-00 EMS main switch in overhead console for Aerolite installation 0.2 0.4
5.2.2.2.3 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 54
5.2.2.3 Intensive Care EMS kit Aerolite (STC)
5.2.2.3.1 Content:
07-70030-A AL2035-003 Intensive Care EMS Kit Aerolite (STC) consisting of: 151.5 334.0
1 IV Hook LH
1 Medium height med cabinet, detachable parts
1 Medium height med cabinet, fixed provisions
1 Rear door stowage RH
1 Slide & swivel seat FWD RH, detachable parts
1 Slide & swivel seat FWD RH, fixed provisions
1 Stretcher LH - Cirrus 2000 with stretcher platform,
1 Stretcher LH - Cirrus 2000 with stretcher platform, fix
1 Window stowage shell RH
5.2.2.3.2 Minimum required equipment:
5.2.2.3.3 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 55
5.2.3 Packages from Air Ambulance Technology (AAT)
5.2.3.1 EMS / Law enforcement kit AAT (STC)
5.2.3.1.1 Content:
07-70021-A 135-25-20-5000-515 EMS / Law enforcement kit AAT (STC) consisting of: 31.9 70.0
1 Belt system, Emergency Belts, Storage Case
1 Medical floor LH with locker system
5.2.3.1.2 Minimum required equipment:
07-27001-A L2522-002-00 Two (2) rear passenger seats, facing forward 22.2 49.0
5.2.3.1.3 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 56
5.2.3.2 EMS Standard kit AAT (STC)
5.2.3.2.1 Content:
07-70022-A 135-25-20-5000-605 EMS Standard Kit AAT (STC) consisting of: 126.4 278.0
1 Medical cabinet
2 Medical crew seat adjustable
1 Medical equipment carrier
1 Medical floor with locker system
1 Oxygen air station incl. 4x oxygen bottles
5.2.3.2.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 57
5.2.3.3 EMS Advanced kit AAT (STC)
5.2.3.3.1 Content:
07-70023-A 135-25-20-5000-603 EMS Advanced Kit AAT (STC) consisting of: 142.1 313.0
1 Adapter floor
1 Medical cabinet - AFT
2 Medical crew seat swiveling
5.2.3.3.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 58
5.2.4 Packages from Bucher Leichtbau
5.2.4.1 EMS basic kit, rear loading Bucher Leichtbau (STC)
5.2.4.1.1 Content:
07-70025-A ARA-EC135-AC65-B EMS basic kit, rear loading Bucher Leichtbau (STC)
102.0 224.9
1 409 Wheel stretcher
1 Centre light
1 Electrical supply system
1 Integral floor
1 Medical wall
1 Stretcher loading platform and retainer AFT
1 Stretcher retainer FWD
2 Tie down (LH & RH)
5.2.4.1.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 59
5.2.4.2 EMS high sophisticated kit, rear loading Bucher Leichtbau (STC)
5.2.4.2.1 Content:
Title kg lb
07-70024-A ARA-EC135-AC65-HS
EMS high sophisticated kit, rear loading Bucher
Leichtbau (STC) consisting of:
1 12 V outlet FWD
1 12-2 foldable stretcher 16g
1 12-2 Stowage provision
1 Attachment plate AFT RH Zarges box
1 Center cabinet
1 Electrical charger & battery
1 EMS GPU-connector
1 Infusion hook
1 Light AFT
1 Light FWD
1 Medical attendant seat type A
2 Medical attendant seat type B (swiveling)
1 Modification kit front rail 409 stretcher
1 Oxygen bottle rack
3 Oxygen supply hose
1 Rear door stowage unit
1 Reversible copilot seat (modification)
1 Roof rail
1 Stretcher retainer AFT
2 Stretcher retainer FWD
1 Suction unit in side cabinet LH
1 Tie down LH
1 Tie down RH
5.2.4.2.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 60
5.2.4.3 EMS basic kit, side and rear loading Bucher Leichtbau (STC)
5.2.4.3.1 Content:
07-70027-A ARA-EC135-AC61-B EMS basic kit, side and rear loading Bucher Leichtbau
(STC) consisting of:
101.2 223.1
1 Side- and rear-load stretcher
5.2.4.3.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 61
5.2.4.4 EMS high sophisticated kit, side and rear loading Bucher Leichtbau (STC)
5.2.4.4.1 Content:
07-70026-A ARA-EC135-AC61-HS
EMS high sophisticated kit, side and rear loading
Bucher Leichtbau (STC) consisting of:
189.0 416.7
1 Medical attendant seat type B (swiveling)
1 Side cabinet RH
5.2.4.4.2 Recommended optional equipment for EMS packages see chapter 5.2.4 page 63
135.06.101.01 E 62
135.06.101.01 E 63
5.2.5 Recommended optional equipment for EMS packages:
07-50026-A L5231-001-00 One-hand latching system for clam-shell doors 1.0 2.2
07-50027-A L5231-002-00 Extended opening fasteners for clam-shell doors 0.3 0.9
07-50025-A L5211-004-10 Securing device for complete opening of copilot door
(copilot pitot / static system required)
05-31027-A L5633-001-10 Window in clam-shell door, LH 0.6 1.3
135.06.101.01 E 64
6 Optional equipment
6.1 Shopping list
05-02016-A L1111-002-00 Two-color external painting instead of single color painting 1.5 3.3
05-02016-A L1111-004-00 Multicolor external painting instead of single color painting 2.0 4.4
05-03007-A L2562-001-00 First aid kit 1.3 2.9
05-03008-A L2562-001-10 First aid kit for DGAC certification 2.8 6.2
05-12001-A L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH) 0.6 1.3
05-12002-A L2551-003-00 Additional 4 tie-down fittings for airline attachment rails 0.6 1.3
05-21015-A L8541-001-10 Wire strike protection system, fixed provisions 3.3 7.3
05-21015-A L8541-001-20 Wire strike protection system, detachable parts 8.2 18.1
05-22014-A L5371-001-00 Engine outlet heat protection 1.2 2.7
05-22013-B L7100-001-00 Automatic in flight power check 0.0 0.0
05-22007-A L7924-001-00 Fuzz burners for engines 1.2 2.6
05-22008-A L2621-001-00 Engine fire extinguishing system 3.6 7.9
05-23006-A L7165-002-00 Engine compressor washing device 3.2 7.1
05-24017-A L6211-014-00 Sand erosion protection kit for rotor blades 0.9 2.0
05-25016-A L7161-001-10 Sand filter system, fixed provisions 10.1 22.3
05-25016-A L7161-001-20 Sand filter system, detachable parts 26.2 57.8
05-26012-A L1241-001-00 Anti-corrosion protection for high corrosive environment 2.0 4.4
05-31025-A L5211-002-00 Sliding window in sliding doors 0.9 2.0
05-31026-B L2514-002-00 Tinted sun shades for cockpit windshield roof section 1.9 4.2
05-31026-B L5621-001-00 Tinted window for cockpit doors 0.0 0.0
05-31026-B L5632-001-00 Tinted windows for passenger cabin
(incl. sliding window for sliding doors)
05-31027-A L5633-001-20 Window in clam-shell door, RH 0.6 1.3
05-31028-A L2524-030-10 IFR training screen, fixed provisions 0.1 0.2
05-31028-A L2524-030-20 IFR training screen, detachable parts 1.6 3.5
05-31045-A L5211-001-11 Lockable sliding window in copilots' door 0.2 0.4
05-31045-A L5211-001-12 Lockable sliding window in pilots' door 0.2 0.4
05-32007-A L3042-001-00 Windshield wiper system 4.9 10.8
05-34003-A L2576-002-00 Dampers for avionics compartment
(avionics compartment required)
05-37016-A L6701-001-00 Copilot flight controls 6.0 13.2
135.06.101.01 E 65
General Equipment (contd.)
05-37017-A L6721-001-00 Covers for copilot flight controls
-2.5 -5.5
05-39006-A L2514-003-01 Map case in copilot door 0.5 1.1
05-39007-A L3111-001-10 Map cases on instrument panel glare shield 0.6 1.3
05-39008-A L3113-004-10 Illuminated chart holder for pilot side 0.9 2.0
05-39008-A L3113-004-20 Illuminated chart holder for copilot side 0.9 2.0
05-42019-A L2105-001-00 Air conditioning system 58.7 129.4
05-42020-A L2105-001-10 Air conditioning system for tropical environment 61.9 136.5
05-61010-A L2433-003-00 Battery, type "Saft", ULM, 27 Ah, 24 V instead of standard battery 8.2 18.1
05-61010-A L2433-006-00 Battery, type "Saft", ULM, 40 Ah, 24 V instead of standard battery 16.8 37.0
05-71001-A L6351-001-00 Rotor brake system 6.3 13.9
05-81032-A L2818-100-10 Internal long range fuel tank system, fixed provisions 3.8 8.4
05-81032-A L2818-100-20 Internal long range fuel tank system, detachable parts 35.2 77.6
05-81033-A L2812-001-00 Self sealing fuel supply tanks 4.5 9.9
05-85008-A L2843-001-00 Fuel management system (Fuel flow meters) 1.0 2.2
05-92009-A L6611-001-10 Main rotor blade folding: basic kit 1.3 2.9
05-92009-A L6611-001-20 Main rotor blade folding: fixed provisions for ground handling kit
(basic kit required)
05-92009-A L6611-001-30 Main rotor blade folding: ground handling kit GSE GSE
05-93007-A L8544-002-00 Lashing points (wind speeds up to 100 kts) (weight GSE: 24.9 kg) 0.7 1.5
05-93008-A L8544-001-00 Lashing points (wind speeds up to 40 kts) 2.4 5.3
05-95001-A L1321-001-00 Tie-down and covering kit (long-term outside helicopter parking) GSE GSE
05-97001-B L6201-001-30 Accelerometers (for Track & Balance system) 0.0 0.0
05-97002-B L6201-002-10 Optical tracker, fixed provisions 0.1 0.2
05-97002-B L6201-002-20 Optical tracker, detachable parts 0.7 1.5
05-97004-A L6201-001-00 VMS II (Track & Balance system) 2.7 6.0
06-11021-A L3274-001-10 Settling protectors, fixed provisions 1.9 4.2
06-11021-A L3274-001-20 Settling protectors, detachable parts 7.6 16.8
06-11022-A L3272-001-10 Snow skids, fixed provisions 0.9 2.0
06-11022-A L3272-001-20 Snow skids, detachable parts 20.8 45.9
06-12007-A L3273-001-00 Lengthened skids (standard landing gear only) 8.3 18.3
06-12009-A L3216-001-10 High landing gear (instead of standard landing gear) 26.0 57.3
Stick, Pitch and Pedals have to be removed - thus negative delta weight
135.06.101.01 E 66
Specific Mission Equipment (contd.)
06-21017-A L8512-001-10 External hoist, fixed provisions
8.6 19.0
06-21017-A L8512-001-20 External hoist 50m, detachable parts,
(incl. 1 week winch operator training)
58.8 129.6
06-21017-A L8512-001-21 External hoist 90m, detachable parts,
62.7 138.2
06-26011-A L8511-002-10 Cargo hook mirrors, fixed provisions 0.8 1.8
06-26011-A L8511-002-20 Cargo hook mirrors, detachable parts 3.9 8.6
06-27019-A L8511-001-10 Cargo hook system, fixed provisions 3.2 7.1
06-27019-A L8511-001-30 Cargo hook system, detachable parts (cargo hook mirrors
16.5 36.4
06-27022-A L8511-005-10 Double cargo hook system, fixed provisions 4.3 9.5
06-27022-A L8511-005-20 Double cargo hook system, detachable parts 22.1 48.7
06-45023-A L3343-003-00 Landing & search light, 450 W 3.4 7.5
06-46001-A L3344-001-00 Strobe lights, white 1.4 3.1
06-61015-A L3215-001-10 Emergency floats, fixed provisions (standard landing gear only) 7.8 17.2
06-61015-A L3215-001-21 Emergency floats, detachable parts (standard landing gear only) 64.6 142.4
06-65002-A L2566-001-00 Emergency hammer 0.2 0.4
06-65004-A L2625-003-00 2nd portable fire extinguisher 2.8 6.2
06-66008-A L3353-005-00 Emergency lights (boarding step illumination and illuminated exit
06-66009-A L3322-001-00 Boarding step illumination 0.2 0.4
06-66010-A L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT" 0.3 0.7
06-66017-A L3353-010-00
HEEL System (Helicopter Emergency Egress Lighting)
(Emergency lights required)
06-67037-A L2563-005-00 Underwater Locator Beacon, ELP-362D 0.5 1.1
06-67047-A L2563-812-00 Automatic Deployable ELT 9.1 20.1
06-69005-A L2341-006-61 Voice alert generator 611-014 (NAT) 0.5 1.1
06-81009-A L8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), fixed
provisions (cargo hook or double cargo hook system required)
Communication via copilot audio / comm. control unit
135.06.101.01 E 67
07-15016-A L2512-003-10 Height adjustable pilot seat (instead of standard pilot seat) 3.7 8.1
07-15016-A L2512-003-20 Height adjustable copilot seat (instead of standard copilot seat) 3.7 8.1
07-30012-A L2581-001-00 Enhanced sound proofing kit 6.0 13.2
07-30013-A L2524-002-00 Separation curtain for cockpit / cabin 2.0 4.4
07-30014-A L2524-021-00 Separation curtain for cabin / cargo compartment incl. smoke
detector in cargo compartment (avionics compartment required)
07-30015-A L2524-001-00 Separation wall for cabin / cargo compartment incl. smoke
07-30018-A L5213-003-00 Curtains for cabin windows (grey) 1.5 3.3
07-40005-A L2513-200-00 Washable floor covering for cockpit 4.1 9.1
07-40005-A L2513-210-00 Washable floor covering for cargo compartment 3.0 6.4
07-40005-A L2513-220-00 Washable floor covering for cockpit, cabin and cargo
11.8 26.0
07-40006-A L2513-300-00 Carpet for cockpit and cabin 7.0 15.4
07-40006-A L2513-310-00 Carpet for cockpit, cabin and cargo compartment 11.0 24.3
07-50028-A L5213-001-11 Sliding door fastener, intermediate and max. position, LH 1.0 2.2
07-50028-A L5213-001-12 Sliding door fastener, max. position, LH 0.4 0.9
07-50028-A L5213-001-21 Sliding door fastener, intermediate and max. position, RH 1.1 2.4
07-50028-A L5213-001-22 Sliding door fastener, max. position, RH 0.4 0.9
07-50034-A L5212-001-00 Jettisonable cockpit doors 1.2 2.6
07-50039-A L5211-010-00 Pre catch system for pilots' doors 0.2 0.4
07-50039-A L5211-011-00 Pre catch system for sliding doors 0.2 0.4
07-83006-A L2513-004-40 Quick detachable VIP carpet for passenger cabin 3.0 6.6
135.06.101.01 E 68
08-15028-A L2319-002-41 Fixed provisions for GSM phone
(antenna, 28VDC, interfacing to ICS)
08-15507-B L2315-092-00 IRIDIUM satellite phone AEROPHONE (AERODATA) 4.6 10.1
08-16053-A L2341-193-01 Audio/Comm. control system (3rd station - PAX)
AS 3100-12 (BECKER) in cabin ceiling (LH)
08-17032-A L2331-003-00 Cabin loudspeaker 2.5 5.5
08-18018-A L2315-001-10 Headset H 10-76 (DAVID CLARK),
Low Impedance Spiral Wire
08-18018-A L2315-001-14 Headset H10-76 ANR/ENC (DAVID CLARK), Low Impedance
08-35007-A L2327-001-01 Traffic Advisory System TAS 9900BX
with 3" indicator (RYAN)
08-46006-A L3168-090-01 Digital moving Map DKG 3 (DORNIER),
08-53004-A L3424-000-00
AHRS Free Steering Mode
08-83021-A L3172-001-00
(Track, Balance and Vibration recording
Different solutions can be offered on request
Some avionics solutions can be NVG modified
NVG compatible cabin and cargo compartment lighting
NVG friendly external lighting kit, comprising position and anti-
Landing & search light 400/200 W, NVG compatible
Fixed provisions can be offered on request
Broadcast, Thermal Imaging and Video Surveillance Equipment
Ultraforce II (FLIR Systems) on request
Different equipment can be offered on request:
SP / DP IFR with FMS / NMS
SMD68 on copilots side (6 x 8 display)
NVG compatible cockpit
NVG friendly external lighting
FLIR with Operator Console and Digital Video
SX16 with IFCO, Laserpointer and slaving unit
Spoiler position for cockpit doors
Rappelling devices for 2+2 persons
Tactical direction finder, etc.
135.06.101.01 E 69
135.06.101.01 E 70
Radar altimeter with voice warning
Cockpit door jettison
HEELS (Helicopter Emergency Egress Lighting Syst.)
Traffic Advisory System TAS 9900BX
Cabin loudspeaker / Passenger address system
Vibration recording system
Corrosion prevention treatment for offshore operation
Rear window with push-out (escape window)
135.06.101.01 E 71
7 Table of constraints
7.1 General Checklist for Incompatibilities
Detachable parts require the related fixed provisions.
All recommended configurations in Chapter 4 exclude each other. Mixed Configurations are
possible but have to be individually checked.
Separation between cabin and cargo compartment can not be selected for utility seat
Quick detachable VIP carpet for passenger cabin can only be combined with 5 Passenger
Transport layout and washable floor covering.
In the following category, only one item can be selected:
sliding door fastener (for each side of the helicopter)
separation between cabin and cargo compartment
External Hoist has priority over (NSU - respective systems will be deactivated):
L8511-002-20
Cargo hook mirrors,
L2571-001-00 Radar radome
L2327-001-01
TAS 9900BX
L3216-001-10 High landing gear
L8541-001-20
System, (WSPS)
degraded in
FLIR / SX16 installation
135.06.101.01 E 72
7.2 Legend of the following chart
EXL Impossibility of simultaneous fitment of the fixed parts of 2 items of equipment
NSF Total or partial incompatibility of simultaneous fitment of the removal parts of two items of equipment
- - Recommended EMS configurations x
L2818-100-20
Internal long range fuel tank system,
05-81032-A
Recommended EMS configurations
L2105-001-10
Recommended EMS configurations X
L2331-003-00
Pure single pilot cockpits (w/o
copilot extension)
L3113-004-20
Illuminated chart holder for copilot side 05-39008-A
08-35007-A
Traffic Advisory System TAS
9900BX
L7161-001-10
Sand filter system, fixed provisions 05-31025-A
9900BX X
Lower cutter of the
Wire strike protection system,
05-21015-A
07-40006-A
L2513-310-00
Carpet for cockpit, cabin and cargo
07-83003-A
L2525-104-00
VIP carpet for cockpit, cabin and
L2818-100-10 /
Internal long range fuel tank system 05-81032-A
08-83021-A
L3172-001-00
(Track,
Balance and Vibration recording
L6201-001-00
VM II 05-97004-A
L6201-002-10
Accelerometers 05-97001-B
06-61015-A
L3215-001-21
Emergency floats, detachable parts
L3273-001-00
Lengthened skids (standard landing
06-12007-A
L8511-005-20
Double cargo hook system, detachable
06-27022-A
06-12009-A
L3216-001-10
High landing gear instead of
L3217-001-00
Reinforced rear landing gear cross
06-12008-A
06-11022-A
L3272-001-20
Snow skids, detachable parts X
L3274-001-20
Settling protectors, detachable parts 06-11021-A
06-66010-A
L3353-006-20
Illuminated signs "NO
SMOKING/FASTEN SEAT BELT"
Recommended EMS configurations -
05-31025-A
L5211-002-00
Sliding window in sliding doors
L5632-001-00
Tinted windows for passenger cabin
(dark grey) incl. sliding window for
05-31026-B
07-50028-A
L5213-001-12
Sliding door fastener, max. position,
L8512-001-10
External hoist, fixed provisions 06-21017-A
05-31027-A
L5633-001-20
Window in clam-shell door, RH X
05-97001-B
Accelerometers x
VMS II 05-97004-A
135.06.101.01 E 73
135.06.101.01 E 74
8 Main performance
The following performance values and figures refer to an EC135, equipped with average production
Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in
International Standard Atmosphere (ISA) and zero wind condition.
Performance on 2 engines (AEO) Pratt & Whitney PW206B2
Maximum speed (V
Maximum cruising speed (V
Fuel consumption at fast cruise speed
at economical cruising speed
Fuel consumption at 65 KIAS
Rate of climb, TOP, SL, ISA
Hover ceiling IGE (4 ft AGL), TOP,
no wind or headwind, ISA
no wind or headwind, ISA + 20C
Hover ceiling OGE, TOP, ISA
Hover ceiling OGE, TOP, ISA + 20C
Service ceiling, MCP,
(climb reserve 200 ft/min), ISA
Maximum range (without fuel reserve at
economical cruise speed)
standard fuel tank configuration (560 kg)
long range fuel tank configuration (730 kg)
Maximum endurance (without fuel reserve at
1) 15,000 ft density altitude certification limit
2) 12,000 ft pressure altitude certification limit
3) 10,000 ft pressure altitude certification limit
135.06.101.01 E 75
Performance on 1 engine (OEI) Pratt & Whitney PW206B2
Service ceiling with 100 ft/min climb reserve,
MCP OEI-power, ISA
MCP OEI-power, ISA + 20C
Rate of climb, MCP OEI-power, SL
Max. temperature for CAT A, take-off from
clear heliport at SL
C + 50 + 50 + 50 + 46 + 43
Max. gross weight hover IGE (4ft AGL), SL,
ISA, no wind, 2 min OEI power
ISA + 20C, no wind, 2 min OEI power
Max. gross weight hover OGE, SL,
ISA, no wind, 30 sec OEI power
ISA + 20C, no wind, 30 sec OEI power
Max. gross weight CAT A, VTOL, SL,
ISA / ISA + 20C
135.06.101.01 E 76
Performance on 2 engines (AEO) Turbomeca Arrius 2B2
135.06.101.01 E 77
Performance on 1 engine (OEI) Turbomeca Arrius 2B2
C + 50 + 50 + 50 + 47 + 43.5
OPERATING LIMITATIONS (valid for both versions, EC135 P2+ and EC135 T2+)
The helicopter can be operated within the following altitude and temperature limitations (according to
the Flight Manual):
6,415 lb.
6,095 m PA
12,000 ft PA
3,045 m PA
10,000 ft PA
Maximum operating altitude for hover in
4,570 m DA
15,000 ft DA
Minimum temperature -35C (-31F)
ISA + 39C
(max. + 50C / + 122F)
AGL Above Ground Level OGE Out Of Ground Effect
DA Density Altitude PA Pressure Altitude
IGE In Ground Effect SL Sea Level
ISA International Standard Atmosphere TOP Take-Off Power
MCP Maximum Continuous Power VNE Never-Exceed Speed
OEI One Engine Inoperative VTOL Vertical Take-Off and Landing
135.06.101.01 E 78
Hover In Ground Effect (HIGE, TOP, no wind)
with two PW206B2 engines
135.06.101.01 E 79
with two ARRIUS 2B2 engines
135.06.101.01 E 80
Hover Out Of Ground Effect (HOGE, TOP)
135.06.101.01 E 81
135.06.101.01 E 82
135.06.101.01 E 83
Hover Out Of Ground Effect (HOGE, 30 sec OEI-power)
with one PW206B2 engine
135.06.101.01 E 84
Hover Out Of Ground Effect (HOGE, 2.0 min OEI-power)
135.06.101.01 E 85
with one ARRIUS 2B2 engine
135.06.101.01 E 86
135.06.101.01 E 87
135.06.101.01 E 88
135.06.101.01 E 89
Maximum Rate Of Climb, TOP
with two PW206B2 engines,
135.06.101.01 E 90
with two ARRIUS 2B2 engines,
135.06.101.01 E 91
135.06.101.01 E 92
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