This document is the property of EUROCOPTER; no part of it shall be ... This
document gives a technical overview of the EC135 standard sales and its
possible ...
EC 135 Technical Data
Contents
Page FOREWORD
3
GENERAL CHARACTERISTICS
5
EC 135 - STANDARD AIRCRAFT DEFINITION
9
OPTIONAL EQUIPMENT •
GENERAL OPTIONAL EQUIPMENT
15
•
VIP OUTFITS
22
•
EMS OUTFITS
26
RADIO COMMUNICATION / NAVIGATION EQUIPMENT •
SELECTION OF PINAO CODES
27
•
PACKAGES DESCRIPTIONS
30
•
HEADSETS AND HELMET
37
EQUIPMENT COMPATIBILITY
39
MAIN PERFORMANCE
45
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EC 135 Technical Data
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EC 135 Technical Data
FOREWORD
PURPOSE OF DOCUMENT This document gives a technical overview of the EC135 standard sales and its possible additional equipment. The mandatory equipment for a Cat A or JAR OPS 3 certifications is already included in the “PINAO” avionics packages. For any more in-depth technical information, please refer to the EC135 type specification (135.02.102.01 E)
PRIORITY 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.
IMPORTANT NOTES Eurocopter’s 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.
■
The data set forth in this document are general in nature and for information purposes only. They may vary with conditions. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.
■
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EC 135 Technical Data
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EC 135 Technical Data
GENERAL CHARACTERISTICS EXTERNAL DIMENSIONS
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EC 135 Technical Data
INTERNAL DIMENSIONS
Floor area
Volume
Cabin
3.15 m²
33.91 ft²
Cabin
3.80 m³
134.20 ft³
Cockpit (pilot side)
1.15 m²
12.38 ft²
Cockpit (pilot side)
1.00 m³
35.31 ft³
Baggage compartment
1.20 m²
12.92 ft²
Baggage compartment
1.10 m³
38.84 ft³
Total (undivided)
5.50 m²
59.21 ft²
Total (undivided)
5.90 m³
208.35 ft³
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EC 135 Technical Data
LAYOUT (Alternatives) Passenger transport: n Casualty evacuation: n
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) 1 pilot + 1 litter + 3 seats for doctor and attendants (2nd litter in stowed position possible) 1 Pilot + 2 litters + 2 seats for doctor and attendant 2 pilots + 1 litter + 3 seats for doctor and attendants (2nd litter in stowed position possible) 2 pilots + 2 litters + 2 seats for doctor and attendant
WEIGHTS n n n n n
Empty weight, basic version, wet Pilot Useful load Maximum take-off weight Maximum take-off weight with external load
kg 1,490 80 1,265 2,835 2,900
lb. 3,285 176 2,789 6,250 6,400
ENGINES -
2 Pratt & Whitney turbine engines: new PW206B2 with 30 sec-rating.
or - 2 Turbomeca turbine engines: new ARRIUS 2B2 with 30 sec-rating. (for deliveries after Sept. 2002) Engine ratings (thermodynamic limits per engine at SL, ISA): PW206B2 • One Engine Inoperative (OEI), 30 sec power • One Engine Inoperative (OEI), 2.0 min power • One Engine Inoperative (OEI), MCP
kW
ch
shp
609 580 528
828 789 718
816 777 708
• Take-Off Power (TOP) • Maximum Continuous Power (MCP)
463 419
630 570
621 562
ARRIUS 2B2 • One Engine Inoperative (OEI), 30 sec power • One Engine Inoperative (OEI), 2.0 min power • One Engine Inoperative (OEI), MCP
kW
ch
shp
609 580 528
828 789 718
816 777 708
• Take-Off Power (TOP) • Maximum Continuous Power (MCP)
452 426
615 579
606 571
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EC 135 Technical Data
MAIN TRANSMISSION 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 353 1 x 480 1 x 473
Twin engine operation • Take-Off Power (TOP) • Maximum Continuous Power (MCP)
2 x 308 2 x 419 2 x 413 2 x 283 2 x 385 2 x 380
FUEL CAPACITIES
Usable Fuel (lb)
(kg)
Unusable Fuel (l)
(lb.)
(kg)
Total (lb.)
(kg)
Main Tank
989.0
448.6
560.8
7.5
3.4
996.5
452.0
Supply Tank
193.6
87.8
109.8
9.3
4.2
202.8
92.0
1,182.6
536.4
670.5
16.8
7.6
1,199.3
544.0
Total
Note: • From the helicopter with S/N (Serial Number) 250 onwards, a new fuel tank version with 700 l usable fuel (i.e. 560 kg / 1,235 lb.) is due to be available. • Fuel density used is 0.8 kg/litre.
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EC 135 Technical Data
EC 135 - STANDARD AIRCRAFT DEFINITION
General Crashworthy fuselage Tail boom with fixed horizontal stabiliser and two end-plates 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 colour)
Cockpit, Cabin and Cargo Compartment One-level cabin and cargo compartment floor with integrated rails Glazed canopy Two hinged cockpit doors (with sliding window and map case in pilot's door) Two wide passenger sliding doors Two rear hinged clam-shell doors Longitudinally adjustable crash resistant pilot and copilot seats with head rest and 4-point safety belts with automatic locking system Five upholstered crash resistant passenger seats with head rests and three-point safety belts with automatic locking system (three seats facing aft and two seats facing forward) Cabin boarding grips (LH and RH) Interior panelling 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 shield Ram-air and electrical ventilating system for cockpit and cabin Headset holder in the cockpit, rotatable Headset holder in the cabin Portable fire extinguisher Stowage net for first aid kit at the LH rear clam-shell door Flash light (torch) Mobile tie-down rings (4ea)
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EC 135 Technical Data
Basic Instrumentation •
•
Central Panel Display system (CPDS), consisting of: - Caution Advisory Display (CAD) with indication of: * Caution and advisory information * Fuel quantity indication - Vehicle and Engine Management Display (VEMD) with indication of: * Torque * Engine parameters (N1-RPM, 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 temperature) * Dual ammeter (generator) * Ammeter (battery) * Dual voltmeter * Outside Air Temperature (OAT) * Parameters of optional equipment (e.g. mast moment) * Engine cycle counter (on flight report page) Clock (2”)
•
Magnetic compass
•
Triple (rotor and engines) RPM-indicator (2”)
•
Standard instruments: ** - Encoding altimeter (3") - Airspeed indicator (3") - Vertical speed indicator (3") Warning unit: - Engine fire warning with fuel emergency shut-off - Warning lights - Aural warning (for each warning, rotor RPM, fire warning) Main switch panel: - DC power control - Digital engine control (FADEC)
•
•
•
Pitot/static system with electrical heated pitot tube, pilot side
•
Static pressure crossover system.
** If “MEGHAS instrumentation” is chosen as optional equipment, these standard instruments are deleted (function included in MEGHAS) and the following back-up instruments are added: - altimeter (2”) - airspeed indicator (2”)
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EC 135 Technical Data
Power Plant Two PRATT & WHITNEY PW206B2 turbine engines or Two TURBOMECA ARRIUS 2B2 turbine engines (for deliveries after Sept. 2002) These 2 engines are equipped with: - fire detectors - electronic engine control (FADEC-BOX) - chip detectors with quick-disconnect plugs - overspeed system - twin-engine OEI-training mode Oil cooling and lubricating system with thermostatic valve Crashworthy 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
Transmission System Flat-shaped main gearbox with two stages Chip detector system with quick-disconnect plug (main gearbox) 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 drive shaft Tail rotor gearbox with splash lubrication and oil level sight gauge Chip detector system with quick-disconnect plug (tail rotor gearbox) Rotor and Flight Controls Bearingless Main Rotor system (BMR), consisting of: - Rotor head/mast in one piece - Four fibre-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 balance system 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 hydraulic booster Yaw-SAS (Stability Augmentation System)
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EC 135 Technical Data
Electrical Installation Power generation system: - Two starter/generators (2 x 160 A, 28 VDC) - Nickel-Cadmium battery, (24 V, 17 Ah) - External power connector (STANAG 3302) Power distribution system: - Two primary busbars - Two shedding busbars - Two essential busbars - Two high load busbars (80 A) - for optional equipment only - Two high power busbars (200 A) - Battery bus Lighting: - Anti-collision warning light (red flashing) - Fixed, nose-mounted landing light (250 W) - Three position lights (red, green, white) - Adjustable instrument lighting - One utility light in the cockpit - Lights in the cabin and cargo compartment Ground Handling Kit * Two ground-handling wheels Basic aircraft covers (short time) Main rotor blade tie-down lash bags Oil drain hoses Fuel tank drain device Keys for cockpit doors, cabin doors, baggage compartment doors and tank flap (one-key system) Battery key Compass compensation key Lifting points
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EC 135 Technical Data
Documentation Flight Manual ♣ Pilots-Checklist ♣ Logbook Battery Manual * Maintenance Manual ♣ * - Part 1: System Descriptions - Part 2: Maintenance Procedures Illustrated Parts Catalogue incl. type relevant Ground Support Equipment ♣ * Wiring Diagram Manual ♣ * List Of Applicable Publications (LOAP) ♣ * Service Bulletins Catalogue ♣ * Engine Documentation * including: - Maintenance Manual - Illustrated Parts Catalogue (IPC) - Service Bulletins Avionics Manual (if avionics equipment is installed by Eurocopter) *
* not included in the standard helicopter empty weight. ♣ documents revision service is available.
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EC 135 Technical Data
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EC 135 Technical Data
OPTIONAL EQUIPMENT General optional equipment Weight kg
Free Selectable Optional Equipment L2122-001-00 Ventilation extruder without copilot I-panel extension
lb.
1.5
3.3
+ 3.6
+ 7.9
L3113-001-00 Slant panel
0.7
1.5
L5232-001-00 Multifunction handle on the main gear box cowling (LH and RH)
1.2
2.6
L1111-002-00 Two-colour external painting instead of single colour painting
≈ 1.5
≈ 3.3
L1111-004-00 Multicolour external painting instead of single colour painting
≈ 5.0
≈ 11.0
0.9
2.0
L2432-001-00 Starter/generator (2 x 200 A, 28 V DC), instead of standard generator
Cockpit, Cabin and Cargo Compartment Equipment
L2512-002-02 Reversed copilot seat installation kit (position change on ground) L2512-002-11 Manual lock for safety harness of pilot seat
0.1
0.2
L2512-002-21 Manual lock for safety harness of copilot seat
0.1
0.2
L2512-003-10 Height adjustable pilot seat instead of standard pilot seat
+ 3.9
+ 8.6
L2512-003-20 Height adjustable copilot seat instead of standard copilot seat
+ 3.9
+ 8.6
+ 14.5
+ 31.9
3.0
6.6
L2512-006-00 Winch operator seat, turnable in flight instead of standard copilot seat (not usable for piloting) L2513-004-40 Quick detachable VIP carpet for passenger cabin L2513-200-00 Washable floor covering for cockpit
4.1
9.1
L2513-210-00 Washable floor covering for cargo compartment
2.9
6.4
11.8
26.0
L2513-300-00 Carpet for cockpit and cabin floor
7.0
15.4
L2513-310-00 Carpet for cockpit, cabin and cargo compartment floor
9.5
20.9
L2514-002-00 Tinted sun shades for cockpit windshield roof section
1.9
4.2
L2514-003-01 Map case in copilot door
0.5
1.1
L2515-003-10 Stowage unit behind pilots’ seats, fixed provisions
0.1
0.2
L2515-003-21 Stowage unit behind pilot’s seat, detachable parts
2.6
5.7
L2515-003-22 Stowage unit behind copilot’s seat, detachable parts L2522-004-10 Utility seats for 3 rear passengers, model eurocopter, fixed provisions
4.6 1.2
10.1 2.6
+ 8.7
+ 19.2
+ 13.8
+ 30.4
L2513-220-00 Washable floor covering for cockpit, cabin and cargo compartment
L2522-004-20 Utility seats for 3 rear passengers, model eurocopter, detachable parts (in addition to standard seat arrangement) L2522-008-00 Utility seats for 3 rear passengers, model aerolite (in addition to standard seat arrangement)
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EC 135 Technical Data
Weight Cockpit, Cabin and Cargo Compartment Equipment (contd.)
kg
lb.
L2524-001-00 Cabin / cargo compartment separation wall incl. smoke detector (avionics compartment required)
2.8
6.2
L2524-002-00 Cockpit / cabin separation curtain
4.0
8.8
L2524-021-00 Cabin / cargo compartment separation curtain incl. smoke detector (avionics compartment required)
2.3
5.1
L2524-030-10 IFR - training screen, fixed provisions
0.1
0.2
L2524-030-20 IFR - training screen, detachable parts
1.2
2.6
L2525-102-81 Executive kit comprising: • Map case in copilot door • Retractable coat hooks in the rear cabin ceiling (2ea) • Ashtrays in the cabin (if demanded) • Ashtrays in pilot’s and copilot’s door (if demanded) • Covers for sliding door fairing LH/RH • Variable tie-down web for luggage securing • Map cases on I-panel glare shield • Map case in sliding door LH/RH L2562-001-00 First aid kit
4.8
10.6
1.3
2.9
L2562-001-10 First aid kit for DGAC certification
3.0
6.6
L2566-001-00 Emergency hammer
0.2
0.4
L2576-001-00 Avionics compartment
6.2
13.7
L2581-001-00 Enhanced sound proofing kit
9.8
21.6
L2625-003-00 2nd portable fire extinguisher
2.3
5.1
L3111-001-00 10" copilot instrument panel with glare shield
2.7
5.9
L3111-001-01 11" copilot instrument panel with glare shield
3.8
8.4
L3111-001-03 7“ copilot instrument panel with glare shield
2.5
5.5
L3111-001-10 Map cases on instrument panel glare shield
0.6
1.3
L3113-004-00 Centre console
2.1
4.6
L3113-004-10 Illuminated chart holder for pilot side
0.9
2.0
L3113-004-20 Illuminated chart holder for copilot side
1.1
2.4
L5621-001-00 Tinted window in cockpit doors
0.0
0.0
L5632-001-00 Tinted windows for passenger cabin
0.0
0.0
L8514-001-00 Multipurpose attachment hardpoints integrated in the cabin
1.3
2.9
Heating and ventilation equipment L2104-003-00 Bleed air heating system: EMS-version
6.6
14.6
L2104-100-00 Bleed air heating system
6.2
13.7
L2105-001-00 Air conditioning system
58.8
129.6
L2105-001-10 Air conditioning system for tropical environment
61.6
135.8
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EC 135 Technical Data
Weight kg
lb.
L3215-001-10 Emergency floats, fixed provisions
+ 8.8
+ 19.4
L3215-001-21 Emergency floats, detachable parts
49.6
109.3
+ 29.2
+ 64.4
L3217-001-10 Reinforced rear landing gear cross tube
1.1
2.4
L3272-001-10 Snow skids, fixed provisions
0.1
0.2
L3272-001-20 Snow skids, detachable parts
19.4
42.8
8.3
18.3
Landing Gear and Associated Equipment
L3216-001-10 High landing gear instead of standard landing gear
L3273-001-00 Lengthened skids L3274-001-10 Settling protectors, fixed provisions
2.1
4.6
L3274-001-20 Settling protectors, detachable parts
10.2
22.5
L3322-001-00 Boarding step illumination
0.2
0.4
L3343-003-00 Landing & search light, 450 W
3.4
7.5
L3343-006-00 Landing & search light, 400/200 W, NVG compatible
4.3
9.5
L3344-001-00 Strobe lights (white flash lights)
1.4
3.1
L3346-100-10 Search light SX16, front installation, fixed provisions
7.9
17.4
L3346-100-20 Search light SX16, front installation, detachable parts (without vendor parts)
4.8
10.6
L3346-300-10 Search light SX16, LH multi function step mounted, fixed provisions
3.8
8.4
L3346-300-20 Search light SX16, LH multi function step mounted, detachable parts, (without vendor parts)
9.1
20.1
L3346-500-10 Search light SX16, vendor parts
20.4
45.0
L3346-500-20 Search light SX16, with infrared filter, vendor parts
27.6
60.8
L3353-005-00 Emergency lights (boarding step illumination and illuminated exit signs)
3.0
6.6
L3353-006-20 Illuminated signs "NO SMOKING/FASTEN SEAT BELT"
0.3
0.7
L3353-007-00 Illuminated sign "SWITCH-OFF MOBILE PHONE"
0.2
0.4
Landing and Search Lights incl. Illumination Equipment
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EC 135 Technical Data
Weight General Mission Equipment
kg
lb.
L2212-001-00 Digital Automatic Flight Control System (DAFCS)
38.5
84.9
L2212-300-00 MEGHAS sensor kit, consisting of: • AHRS (1st and 2nd system) • Air Data System (1st and 2nd system) • “Pelican” rack L2217-001-10 VFR SAS (VFR pitch/roll Stability Augmentation System)
22.1
48.7
8.5
18.7
L2217-001-50 IFR SAS (IFR pitch/roll Stability Augmentation System)
12.2
26.9
L2420-002-00 AC (Alternating Current) system
3.2
7.1
L2420-003-00 Dual AC (Alternating Current) system
4.3
9.5
L2433-001-00 Battery, type “Varta”, 25 Ah, 24 V instead of standard battery
+ 8.0
+ 17.6
L2433-002-00 Battery, type "Saft", 26 Ah, 24 V instead of standard battery
+ 9.0
+ 19.8
L2433-005-00 Battery, type “Varta”, 40 Ah, 24 V instead of standard battery
+ 19.4
+ 42.8
L2551-003-00 Additional 4 tie-down fittings for airline attachment rails
0.6
1.3
L2621-001-00 Engine fire extinguishing system
3.8
8.4
L2812-001-00 Self sealing fuel supply tanks
4.2
9.3
L2818-100-10 Internal long range fuel tank system, fixed provisions
3.2
7.1
30.3
66.8
L3042-001-00 Windshield wiper system
4.9
10.8
L3043-001-00 Windshield wiper system with windscreen washing device
8.8
19.4
L2818-100-20 Internal long range fuel tank, detachable parts
L3411-001-00 Copilot pitot static system (electrically heated)
1.3
2.6
L5211-001-00 Sliding window in copilot door
0.1
0.2
L5211-002-00 Sliding windows in sliding doors
0.2
0.4
L5211-004-10 Securing device for complete opening of pilot door
0.8
1.8
L5211-004-20 Securing device for complete opening of copilot door
0.8
1.8
L5213-001-11 Sliding door fastener, intermediate and max. position, LH
1.0
2.2
L5213-001-12 Sliding door fastener max. position, LH
0.4
0.9
L5213-001-21 Sliding door fastener, intermediate and max. position, RH
1.1
2.4
L5213-001-22 Sliding door fastener max. position, RH
0.4
0.9
L5231-001-00 One-hand latching system for clam-shell doors
1.5
3.3
L5231-002-00 Extended opening fasteners for clam-shell doors
0.2
0.4
L5633-001-10 Window in clam-shell door, LH
0.6
1.3
L5633-001-20 Window in clam-shell door, RH
0.6
1.3
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EC 135 Technical Data
Weight kg
General Mission Equipment (contd. 1)
lb.
L6201-001-30 Accelerometers (for track and balancing system)
0.0
0.0
L6201-002-10 Optical tracker (Chadwick Helmuth), fixed provisions
0.1
0.2
L6201-002-20 Optical tracker (Chadwick Helmuth), detachable parts
0.6
1.3
L6344-001-00 Mast moment system
1.0
2.2
L6351-001-00 Rotor brake system
4.8
10.6
L6701-001-00 Copilot flight controls
7.1
15.7
L6721-001-00 Covers for copilot flight controls
0.5
1.1
37.1
81.8
L7165-002-00 Engine compressor washing device
1.8
4.0
L7924-001-00 Fuzz burners for engines
1.0
2.2
L8511-001-10 Cargo hook system, fixed provisions
2.9
6.4
L8511-001-30 Cargo hook system, detachable parts
16.2
35.7
L8511-002-10 Cargo hook mirrors, fixed provisions
0.7
1.5
L8511-002-20 Cargo hook mirrors, detachable parts
4.2
9.3
L8512-001-10 External hoist, fixed provisions
9.6
21.2
L8512-001-20 External hoist, detachable parts, (incl. 1 week winch operator training)
62.8
138.5
L8521-301-00 Folding stretcher Ferno / aerolite-type, model 12-2/16G modified
14.0
30.9
7.0
15.4
L7161-001-00 Sand filter system
L8521-301-20 Installation device for one stretcher type Ferno / aerolite-type (model 12-2/16G modified) in full or half length L8521-431-10 Two attachment rails for universal apparatus in sliding door post
3.5
7.7
L8521-432-10 Two airline attachment rails in LH passenger cabin ceiling
1.0
2.2
12.1
26.7
L8522-350-00 Installation device for one stretcher type Bucher-Leichtbau (16 G) in full only
5.0
11.0
L8522-720-01 EMS stowage box
9.7
21.4
11.0
24.3
L8532-002-30 Multifunction step LH for standard landing gear (instead of boarding step)
+ 6.7
+14.8
L8532-002-40 Multifunction step RH for standard landing gear (instead of boarding step)
+ 3.7
+ 8.2
L8541-001-10 Wire strike protection system, fixed provisions
3.3
7.3
L8541-001-20 Wire strike protection system, detachable parts
8.2
18.1
GSE
GSE
L8522-320-00 Folding stretcher type Bucher-Leichtbau (16 G)
L8531-001-00 External loudspeaker system with siren
Handling and Picketing Equipment L1321-001-00
Tie-down and covering kit (long-term outside helicopter parking)
L6611-001-10
Main rotor blade folding: basic kit
1.3
2.9
L6611-001-20
Main rotor blade folding: fixed provisions for ground handling kit
0.7
1.5
L6611-001-30
Main rotor blade folding: ground handling kit
GSE
GSE
L8544-001-00
Lashing points (wind speeds up to 40 kts)
3.8
8.4
L8544-002-00
Lashing points (wind speeds up to 100 kts) (weight of GSE: 24.9 kg)
0.7
1.5
135.02.101.01.E
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EC 135 Technical Data The following listed items can be offered at customer’s request but are not necessarily kept on stock. Availability, certification status and compatibility with other equipment items must be checked individually. Weight kg
Customer Request Equipment
lb.
L1111-005-00 Special detail paintings (markings, letters, logos)
on request
L1111-006-00 Matching painting of externally installed optional equipment
on request
TM
17.3
38.1
TM
18.3
40.4
L3171-001-00 M’ARMS Usage Monitoring System (UMS), JAR OPS III compliant, (ground station not included)
TM
5.3
11.7
L8503-001-10 Fire extinguishing bucket attachment (Bambi Bucket), fixed provisions (cargo hook system required)
0.7
1.5
L8534-000-11 Rope-down device for 2 persons, fixed provisions LH
3.4
7.5
8.5
18.7
3.4
7.5
8.5
18.7
1.0
2.2
127.0
280.0
L2321-007-00 M’ARMS Cockpit Voice and Flight Data Recorder (CVFDR), JAR OPS III compliant L2321-009-00 M’ARMS Cockpit Voice and Flight Data Recorder (CVFDR) and Usage Monitoring System (UMS), JAR OPS III compliant (ground station not included)
L8534-000-12 Rope-down device for 2 persons, detachable parts LH
1)
L8534-000-21 Rope-down device for 2 persons, fixed provisions RH L8534-000-22 Rope-down device for 2 persons, detachable parts RH
1)
L8551-001-10 Light armour protection kit, cockpit and cabin, fixed provisions L8551-001-20 Light armour protection kit, cockpit and cabin, detachable parts 1)
operation cannot be civil certified.
Broadcast, Thermal Imaging and TV Surveillance Equipment Several systems are available on request.
135.02.101.01.E
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EC 135 Technical Data
Weight kg
NVG Compatible Equipment
lb.
L2524-003-00 Cockpit / cabin separation curtain, NVG version
4.0
8.8
L3111-002-21 NVG painting for cabin and cargo compartment
0.2
0.4
L3312-003-00 NVG compatible standard cockpit layout
0.2
0.4
L3347-002-00 Additional NVG friendly external lighting kit, comprising position and anti-collision lights L5213-003-00 Curtains for cabin windows (grey)
0.4
0.9
1.5
3.3
Note: For NVG compatible landing and searchlights, refer to § 5.1 Landing and search lights.
General remarks about NVG If NVG flights are requested, three important factors must be considered: • The switching-off of non-NVG compatible lights and instrumentation (crash risks). • The non-compliance with local civil regulations (NVG flights may be forbidden). • The different level of vision provided by NVG compatible lighting.
Requirements and checklist for building up a NVG compatible configuration • General compatibility requirements A NVG compatible cockpit is possible only with a MEGHAS avionics solution and only with filtered goggles. • Checklist for NVG compatible configuration The following points must be checked and fulfilled: ü The cockpit must be fully NVG compatible, which means − The avionics solution must be NVG compatible, − The NVG compatible cockpit layout (option L3312-003-00) is required, − The customer must be advised about NVG compatibility status of its BFE (Buyer Furnished Equipment). ü The cabin lighting must not negatively affect NVG compatibility, which means − The NVG compatible cockpit/cabin separation curtain (option L2524-003-00) is required. Otherwise, the customer must be advised that all cabin lighting must be switched off during NVG flights. ü The external lights must be fully NVG compatible, which means − The additional NVG compatible external lighting kit (option L3347-002-00) is required. Otherwise, the customer must be advised that all non-NVG compatible lighting must be switched off during NVG flights. ü If the customer lands in NVG mode, the NVG compatible landing & searchlight, 400/200 W (option L3343-006-00) is required. ü If the customer needs a NVG compatible SX16 searchlight, the SX16 with infrared filter (option L3346-500-20) is required.
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EC 135 Technical Data
VIP Outfits
1. VIP Package 1 (Basic Package; 5 seat arrangement) L2526-100-01 Weight of the complete package 1: + 54.3 kg / + 119.7 lb. This installation offers corporate comfort and is characterised by: - Five passenger seats fitted with leather or combination of leather and fabric (three rearward facing and two forward facing), - Cabinet with armrest (wood and leather finish), between the two rear passenger seats - Pilot and copilot seats co-ordinated with passenger seats, - Cockpit, cabin and cargo compartment floors fitted with a VIP carpet, - Special colour of the interior outfit (painted). Sold as complete package, only. To meet individual requirements a customer specific VIP package can be created using the VIP table shown in paragraph 3.
2. VIP Package 2 (Advanced Package; 4 seat arrangement) L2526-200-00 Weight of the complete package 2: + 69.3 kg / + 152.8 lb. This installation offers first class comfort and is characterised by: - Four passenger seats upholstered with leather or combination of leather and fabric (two rearward facing and two forward facing), - Cabinet (wood and leather finish), between the two front passenger seats, - Cabinet with armrest (wood and leather finish), between the two rear passenger seats, - Pilot and copilot seats co-ordinated with passenger seats, - Cockpit, cabin and cargo compartment floors fitted with a VIP carpet, - Cockpit and cabin panels and doors upholstered in leather. Sold as complete package, only. To meet individual requirements a customer specific VIP package can be created using the VIP table shown in paragraph 3.
Note: The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight difference compared to the standard aircraft.
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EC 135 Technical Data
3 Creation of a specific VIP package Only 1 Item per line can be selected. The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight difference compared to the standard aircraft. For information:
the items included in package 1 are noticed with: the items included in package 2 are noticed with:
COCKPIT
only 1 Item can be selected per line
VIP copilot seat (L2525-101-21) +1.2 kg / + 2.6 lb.
VIP-seat)
* (each front cabinet is installed in place of or instead of the front middle
only 1 Item can be selected per line
VIP copilot seat height adjustable (L2525-101-76) + 4.3 kg / + 9.5 lb.
VIP carpet (L2525-101-50) 5,7 kg / 12,6 lb.
FWD. PAX CABIN
135.02.101.01.E
VIP pilot seat height adjustable (L2525-101-71) + 4.3 kg / + 9.5 lb.
VIP pilot seat (L2525-101-11) +1.2 kg / + 2.6 lb.
2 VIP passenger seats, front (L2525-202-13) + 7.7 kg / + 17 lb.
3 VIP passenger
Front Cabinet, flat * (L2526-212-601) 14,4 kg / 31,7 lb.
Front Cabinet, middle incl. nd 2 fire extinguisher
Front Cabinet, high incl. nd 2 fire extinguisher for cabin and illuminated
for cabin * (L2526-212-601 + L2526-112-63 + L2625-003-50) 23,4 kg / 51,7 lb.
signs * (L2526-212-601 + L2526-112-64 + L2625-003-50 + L3353-006-20) 29,4 kg / 64,9 lb.
seats, front* (L2525-102-13) + 8.9 kg / + 19.6 lb.
Table for front cabinet (L2526-112-61) 3,0 kg / 6,6 lb. Cooling box for front cabinet (L2526-112-62) 2,5 kg / 5,5 lb. Illumination system for front cabinet, middle / high (L2526-112-10) 2,0 kg / 6,6 lb. VIP carpet (L2525-102-50) 5,6 kg / 12,3 lb.
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EC 135 Technical Data
only 1 Item can be selected per line
REAR PAX CABIN
2 VIP seats, rear (L2525-102-23) + 4.9 kg / + 10.8 lb. Rear cabinet with Armrest (L2526-112-710) 14,0 kg / 30,8 lb.
VIP carpet (L2525-103-10) 5,1 kg / 11,2 lb.
GENERAL INTERIOR
Special painted interior (L2525-100-35) 1,5 kg / 3,3 lb.
only 1 Item can be selected per line
Rear cabinet, high (L2526-312-701 + L2526-112-75) 14,5 kg / 32,0 lb.
Armrests in rear window niche, LH/RH (L2525-102-62) 0,8 kg / 1,8 lb.
CARGO COMPARTMENT
GROUND SUPPORT EQUIPMENT
Rear cabinet, flat (L2526-312-701) 12,5 kg / 27,5 lb.
Leather covered interior (L2525-112-35) 16,1 kg / 35,5 lb.
Executive kit (L2525-102-81) 5,4 kg / 11,9 lb. Copilot controls covers (painted in harmony with carpet) (L6721-001-00 + L2525-101-65) 0,7 kg / 1,5 lb. Cabin entertainment system (on request) Fabric protection cover for 1 VIP pilot seat (L2525-111-50) Fabric protection cover for 1 VIP pax seat (L2525-112-91) Plastic protection cover for cockpit carpet (L2525-111-60) Plastic protection cover for cabin carpet (L2525-112-92)
Note: The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight difference compared to the standard aircraft.
135.02.101.01.E
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EC 135 Technical Data
only 1 Item can be selected per line
HIGHLY RECOMMENDED ITEMS
Air conditioning system (L2105-001-00) 58,0 kg / 127,9 lb.
Air conditioning system for tropical environment + Special ducting for front passenger seats (L2105-001-10 + L2525-112-46) 63,0 kg / 138,7 lb.
Enhanced sound proofing kit (L2581-001-00) 9,8 kg / 21,6 lb. Pax / cargo compartment separation wall + Avionics compartment (L2524-001-00 + L2576-001-00) 10,0 kg / 22,1 lb.
Note: The VIP seats are installed and delivered instead of the standard seats. The given weights represent the weight difference compared to the standard aircraft.
135.02.101.01.E
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EC 135 Technical Data
EMS Outfits For further information as well as description of the content of the different packages please refer to the EC135 EMS-Brochure (135 EMS 02.101.01 E). 2)
Weight kg lb. L8524-000-03 --L8523-000-03 --L8522-000-03 --L8521-000-04 --L8521-000-05 ---
EMS Outfit Package I
83.0
Additional Suitable EMS Equipment and Apparatus for Individual Choice
refer to EMSBrochure
EMS Outfit Package II
150.0
Additional Suitable EMS Equipment and Apparatus for Individual Choice EMS Outfit Package III
EMS Outfit Package IV
EMS Outfit Package V
287.0
refer to EMSBrochure 132.0
Additional Suitable EMS Equipment and Apparatus for Individual Choice
335.0
refer to EMSBrochure 130.0
Additional Suitable EMS Equipment and Apparatus for Individual Choice
331.0
refer to EMSBrochure 152.0
Additional Suitable EMS Equipment and Apparatus for Individual Choice
183.0
291.0
refer to EMSBrochure
2) for all EMS-packages the complete standard passenger seating weight (60.5 kg / 133.4 lb.) has to be subtracted.
Note: The EMS seats are installed and delivered instead of the standard seats.
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EC 135 Technical Data
RADIO COMMUNICATION / NAVIGATION EQUIPMENT
1. Selection of an avionics package function of operational needs (PINAO code) A/
Asses your operational needs and corresponding PINAO code, with the help of the following table Pilot (single/dual)
P
VFR/IFR
I
Day/night
N
Cat A
A
JAR OPS 3
O
P
B/
one 1 VFR 0 day 0 yes 1 yes 1
two 2 IFR 1 night 1 no 0 no 0
one/two 3
I
N
A
O
With this code you will find the required avionics package in the following table. One PINAO code may lead to different avionics solutions. Key words and package weights are indicated in the following table to simplify the selection.
C/
A reference to the page corresponding to the chosen solution is also given for selection of possible additional equipment.
NOTE - “VFR day” is included in all solutions. - NVG compatible MEGHAS versions can be offered on request. - Others requested additional equipment for JAR OPS 3 above 10,000 ft and over water are not covered by the PINAO code. - For more details about the different avionics solutions (contents and layout) please refer to the brochure “EC 135 AVIONICS Mission Packages” (135 AVIONICS 02.101.01 E).
135.02.101.01.E
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EC 135 Technical Data
COMPLETE Based on solution CODE number 10000 10001 10010 10011 10100 10101 10110 10111 11000 11001 11010 11011 11100 11101 11110 11111 20000 20001 20010 20011 20100 20101 20110 20111 21000
21001
21010
135.02.101.01.E
Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 9 Solution 10 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8
Key words Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability st
Glass cockpit, SPIFR 1 step Glass cockpit, SPIFR upper end, NMS capability Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability
Complete Complete see weight weight page (kg) (lbs)
29,8 33,1 46,6 49,9 29,8 46,1 46,6 51,2 169,3 176,8 172,6 180,1 173,1 180,6 176,4 183,9 169,3 176,8 172,6 180,1 173,1 180,6 176,4 183,9 47,9 51,2 64,7 68,0 47,9 61,9 64,7 71,3 111,1 122,7 154,6 162,2 116,4 128,0 157,9 165,5 121,2 132,8 161,0 168,6
65,8 73,1 103,0 110,3 65,8 101,9 103,0 113,1 374,1 390,6 381,4 397,9 382,5 399,0 389,7 406,3 374,1 390,6 381,4 397,9 382,5 399,0 389,7 406,3 105,8 113,1 143,0 150,2 105,8 136,8 143,0 157,5 245,5 271,1 341,6 358,4 257,2 282,8 348,9 365,7 267,8 293,4 355,7 372,5
27 27 27 27 27 27 27 27 32 33 32 33 32 33 32 33 32 33 32 33 32 33 32 33 27 27 27 27 27 27 27 27 28 29 30 31 28 29 30 31 28 29 30 31
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EC 135 Technical Data
COMPLETE Based on Solution CODE number
21011
21100
21101
21110
21111 30000 30001 30010 30011 30100 30101 30110 30111 31000 31001 31010 31011 31100 31101 31110 31111
135.02.101.01.E
Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8 Solution 3 Solution 4 Solution 7 Solution 8 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 1 Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS Solution 7 with AFCS Solution 8 with AFCS
Key words Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Conventional, few extensions possible Conventional, upper end Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Basic conventional Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability Glass cockpit, 1st step Glass cockpit, upper end, NMS capability
Complete Complete see weight weight page (kg) (lbs)
124,5 136,1 164,3 171,9 111,1 122,7 154,6 162,2 116,4 128,0 157,9 165,5 121,2 132,8 161,0 168,6 124,5 136,1 164,3 171,9 47,9 51,2 61,5 64,8 47,9 61,9 64,7 71,3 185,7 193,3 189,0 196,6 189,5 197,1 192,8 200,4 185,7 193,3 189,0 196,6 189,5 197,1 192,8 200,4
275,1 300,7 363,0 379,8 245,5 271,1 341,6 358,4 257,2 282,8 348,9 365,7 267,8 293,4 355,7 372,5 275,1 300,7 363,0 379,8 105,8 113,1 135,9 143,2 105,8 136,8 143,0 157,5 410,3 427,1 417,6 434,4 418,7 435,5 426,0 442,8 410,3 427,1 417,6 434,4 418,7 435,5 426,0 442,8
28 29 30 31 28 29 30 31 28 29 30 31 28 29 30 31 28 29 30 31 27 27 27 27 27 27 27 27 30 31 30 31 30 31 30 31 30 31 30 31 30 31 30 31
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EC 135 Technical Data
2. Packages descriptions (NB: All packages with PINAO 30xxx are identical to those with PINAO 20xxx of this page) 10101
10110
10111
20000
20001
20010
20011
20100
X
X
X
X
X
X
X
X
X
X
X
X X
X
7,1
X
X
X
X
X
X
X
X
X
X
X
X
X
X X
X
1,5
X
X
X
X
X
X
X
X
X
X
X
X
X
X X
X
X
X
X
X
X
X
X
X X
X
X
X
X
X
X
X
X
X
X
L2420-002-00
3,2
Slant panel
L3113-001-00
0,7
2” std-by horizon AI 804 DC with battery
L3425-802-52
5,5
12,2
Radar Altimeter KRA 405B / KNI 416
L3441-002-00
4,3
9,5 X
X
X
X
X
X
20111
10100
X
20110
10011
57,2
20101
10001
25,9
AC System
10010
10000
L2300-001-02
Weight (lbs)
Avionics solution 1
PINAO code based on avionics solution 1
Weight (kg)
Minimum required equipment
X X
ELT C406-2 HM (ARTEX) 3 frequencies
L2563-090-05
2,0
4,4
Dual controls copilot
L6701-001-00
7,1
15,7
X
X
X
X
X
X
X
X
Copilot I-Panel extension 10" (*)
L3111-001-00
3,0
6,6
X
X
X
X
X
X
X
X
4" Artificial Horizon, 2nd Sys.GH 14 - 391
L3425-091-02
2,5
5,5
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
RMI / CDI, KI 229 / KI 204
L3166-091-04 L3167-091-02
3,0
6,6
X
2nd indicators System packages 3" instruments:(UNITED INSTRUMENTS)
L3412-002-00
2,5
5,5
X
2nd directional Gyro (3” unslaved indic. 205 1BL
L3421-091-02
2,0
4,4
X
Copilot static system
L3411-001-00
1,3
2,9
X
Search & Landing light (450 W)
L3343-003-00
3,2
7,1
First aid kit
L2562-001-00
1,3
2,6
Engine fire extinguishing
L2621-001-00
3,8
8,4
X X X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X X X
X
X
X
X
(*) or enlarged version if combination of other optional equipment requires it Possible add-ons 2” std-by horizon AI 804 DC with battery Radar Altimeter KRA 405B / KNI 416 2” std-by altimeter (instead of Radar altimeter KRA 405B / KNI 416) 2nd indicators System packages 2" instruments (instead of 3" indicator System) Comm. Control Sys. 2nd st AS 3100-XX (BECKER) Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in passenger cabin) HF Com.syst. F 990/KFS 594 Tactical FM Radio Teledux 9 (AEG) 2m or 4m Tactical FM Radio GM 900 (MOTOROLA) Tactical FM Radio MCS 2000 (MOTOROLA) Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF VHF / UHF - AM / FM Transceiver ARC 210 DME KN 63 / KDI 572 (HONEYWELL) Marker Beacon KR 21 (HONEYWELL) Direction Finder Chelton DF931 (stand alone) Stand alone SAR DF 517 (BECKER) VHF NAV/COM/GPS with annunciation/switch 2nd sys. GNS 430 (GARMIN)/ MD 41 Stormscope WX 1000 + (GOODRICH) Colour weather radar RDR2000 (HONEYWELL) (radome included) Colour weather radar RDR2100 (HONEYWELL) (radome included) Colour weather search radar Moving map DKG3 (Dornier, basic version) Stand alone Moving Map System Euro Nav III (Euro Avionics): ELT 100 HM (ARTEX) ELT C406-2 HM (ARTEX) 3 frequencies
L3425-802-52 L3441-002-00 L3111-100-00
6,4 4,3 0,7
14,1 9,5 1,5
X X
X X
X X
X X
X X
L3412-003-00
1,6
3,5
ON REQUEST ON REQUEST
1,6 2,9
3,5 6,4
X X
X X
X X
X X
X X
X X
X X
L2313-008-00
12,5
27,6
X
X
X
X
X
X
ON REQUEST ON REQUEST ON REQUEST ON REQUEST
5,0 4,0 3,5 TBC
11,0 X 8,8 X 7,7 X TBC X
X X X X
X X X X
X X X X
X X X X
X X X X
ON REQUEST L3455-092-03/ L3169-092-02 L3431-092-02 ON REQUEST
10,0 3,6
22,1 8,0
X X
X X
X X
X X
X X
0,9 7,7
2,0 17,0
X X
X X
X X
X X
L2313-010-03 L3442-092-00
2,8 7,8
6,2 17,2
X X
X X
X X
L3443-090-04 L3443-090-02/ L2571-001-00 L3443-090-06/ L2571-001-00 ON REQUEST L3168-090-01 L3168-092-03
6,2 14,0
13,7 30,9
14,0
30,9
X X 3) X 3)
X X 3) X 3)
X X 3) X 3)
TBC 3,2 10,0
TBC 7,1 22,1
X X
X X
X X
L2563-801-02 L2563-090-05
2,0 2,1
4,4 4,6
X X
or
X X
X X
X
X
X
X
X
X
X
X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X
X
X
X
X
X
X
X
X
X
4) 5)
X X X X
X X X X
X X X X
X X X X
X X X X
X X X X
X X X X
X X X X
X X X X
X X X X
3) 4) 5) 14)
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
4) 5) 14)
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
9) 14)
X X 3) X 3) 9) X X
X X 3) X 3)
X X 3) X 3)
X X 3) X 3)
X X 3) X 3)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
X X 7) X 7)
9) 8) 9)
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
14) 4) 5) 9) 14)
or
X X
or
X X
or
X X
or
X X
or
X X
or
X X
or
X
ELT C406-2 HM (ARTEX) 3 frequenc Nav. Option
L2563-821-52
2,1
4,6
X
or
X
or
X
or
X
or
X
or
X
or
X
or
X
or
ELT JE 290 (JOLLIET)
L2563-808-01
2,1
4,6
X
or
X
or
X
or
X
or
X
or
X
or
X
or
X
or
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 3) LH instrument panel extension has to be checked. 4) Requirement of avionics compartment has to be checked 5) Requirement of centre console has to be checked 7) Copilot altimeter, airspeed indicator and vertical speed indicator required size 2” instead of 3”.
135.02.101.01.E
3) 5) 14) 3) 5) 14) 4) 5) 14)
9) 14)
8) 9)
8) Requires RVG 801 E for antenna stabilisation if no SAS is installed 9) Stand alone system; physical integration has to be checked 14) 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.
30
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
EC 135
21010
21011
21100
21101
21110
21111
PINAO code based on avionics solution 3 21001
Minimum requirement equipment
Weight (lbs) 21000
Weight (kg)
Technical Data
Avionics solution 3
L2300-003-02
55,4
122,4
X
Dual controls, copilot
L6701-001-00
7,1
15,7
X
X X
X X
X X
X X
X X
X X
X X
Copilot I-panel extension 10“ (*)
L3111-001-00
3,0
6,6
X
X
X
X
X
X
X
X
Slant panel
L3113-001-00
0,7
1,5
X
X
X
X
X
X
X
X
Copilot static system
L3411-001-00
1,3
2,9
X
X
X
X
X
X
X
X
Bleed air heating (**)
L2104-100-00
6,6
14,6
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
Search & Landing light (450W)
L3343-003-00
3,2
7,1
X
Sliding window in copilot door
L5211-001-00
0,1
0,2
X
X
X
X
X
X
X
X
Windshield wiper
L3042-001-00
4,9
10,8
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
25 Ah battery (*)
L2433-001-00
8,0
17,7
X
200 A starter generators
L2432-001-00
3,6
8,0
X
X
X
X
X
X
X
X
Dual AC System
L2420-003-00
6,3
13,9
X
X
X
X
X
X
X
X
IFR pitch/roll SAS
L2217-001-50
10,0
22,1
X
X
X
X
X
X
X
Map case on I-Panel glare shield
L3111-001-10
0,4
0,9
X
X
X
X
X
X
X
X
Map case in copilot door
L2514-003-01
0,5
1,1
X
X
X
X
X
X
X
X
Radar Altimeter KRA 405B / KNI 416 (HONEYWELL)
L3441-002-00
4,3
9,5
X
X
ELT C406-2 HM (ARTEX) 3 frequencies
L2563-090-05
2,0
4,4
X
2nd directional Gyro (3” unslaved indicator) 205 1BL (Goodrich) First aid kit
L3421-091-02
2,0
4,4
X
L2562-001-00
X X X X 2,9 X X X X 3,8 8,4 (**) Select L2104-003-00 instead for EMS helicopters
Engine fire extinguishing
L2621-001-00 (*) or enlarged version if combination of other optional equipment requires it
X
X
X
X
X
X
X X
X
X
1,3
Possible add-ons Radar Altimeter KRA 405B / KNI 416 (HONEYWELL)
L3441-002-00
4,3
9,5
X
X
X
X
X
X
X
X
X
X
X
Exchange of KI206/KI229 to KPI552 HSI on copilot side ON REQUEST
+1,0
+2,2
X
Comm. Control Syst., 3rd station AS 3100-XX (BECKER) (in passenger cabin) HF Communication system KHF 990/KFS 594 (HONEYWELL) Tactical FM Radio Teledux 9 (AEG) 2m or 4m
ON REQUEST
2,9
6,4
X
X
X
X
X
X
X
X
L2313-008-00
12,5
27,6
X
X
X
X
X
X
X
X 4) 5)
ON REQUEST
5,0
11,0
X
X
X
X
X
X
X
X 3) 4) 5) 14)
Tactical FM Radio GM 900 (MOTOROLA) Tactical FM Radio MCS 2000 (MOTOROLA) Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins) Not civil certified
ON REQUEST
4,0
8,8
X
X
X
X
X
X
X
X 3) 5) 14)
ON REQUEST
3,5
7,7
X
X
X
X
X
X
X
X 3) 5) 14)
X
X
X
X
X
X
X 4) 5) 14)
ON REQUEST
TBC
TBC
X
ON REQUEST
10,0
22,1
X
X
X
X
X
X
X
X 4) 5) 14)
ADF / ADF Adapter (KR 87/KDA 692) Direction Finder Chelton DF931 stand alone Stand alone SAR DF 517 (BECKER)
ON REQUEST
4,7
10,4
X
X
X
X
X
X
X
X 15)
ON REQUEST
7,7
17,0
X
X
X
X
X
X
X
X 9) 14)
L2313-010-03
2,8
6,2
X
X
X
X
X
X
X 9) 14)
Stormscope WX 1000 + (GOODRICH)
L3443-090-04
6,2
13,7
X
X
X
X
X
X
X 9)
Moving Map Kneeboard DKG 3 (Dornier, basic version) L3168-090-01
3,2
7,1
X
X
X
X
X
X
X
X 14)
Stand alone Moving Map System Euro Nav III (Euro Avionics)
L3168-092-03
10,0
22,1
X
X
X
X
X
X
X
X 4) 5) 9) 14)
ELT 100 HM (ARTEX) ELT C406-2 HM (ARTEX) 3 frequencies ELT C406-2 HM (ARTEX) 3 freque Nav. Option ELT JE 290 (JOLLIET)
L2563-801-02
2,0
4,4
X
or
X
or
X
or
X
or
L2563-090-05
2,1
4,6
X
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 3) BFE required 4) Requirement of avionics compartment has to be checked 5) Requirement of centre console has to be checked 9) Stand alone system; physical integration has to be checked
135.02.101.01.E
X
X
X
L2563-821-52
2,1
4,6
X
or
X
or
X
or
X
or
L2563-808-01
2,1
4,6
X
or
X
or
X
or
X
or
14) 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. 15) should be checked with customer airport landing requirements
31
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
EC 135
(*) or enlarged version if combination of other optional equipment requires it Possible add-ons Radar Altimeter KRA 405B / KNI 416 Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in cabin) HF Communication system KHF 990/KFS 594
Tactical FM Radio Teledux 9 (AEG) 2m or 4m Tactical FM Radio GM 900 (MOTOROLA) Tactical FM Radio MCS 2000 (MOTOROLA) Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins) Not civil certified ADF KDF 806 (incl. KFS 586A) Direction Finder Chelton DF931 (stand alone) Stand alone SAR DF 517 (BECKER) GPS Course Deviatio Ind. 802100 (ETS / DAC) GPS indication on HSI KPI 552 pilot GPS Nav Syst. 2101 Approach plus (TRIMBLE) Stormscope WX 1000 + (GOODRICH) Colour weather radar RDR2000 (HONEYWELL) (radome included) Colour weather radar RDR2100 (HONEYWELL) (radome included) Colour weather search radar
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X
X X
X
X
X X
X
X X X
X
21111
2,6 8,4
21110
1,3 3,8
21101
L2562-001-00 L2621-001-00
21100
134,3 15,7 6,6 13,7 1,5 2,9 14,6 7,1 0,2 10,8 17,7 8,0 13,9 22,1 0,9 1,1 9,5 4,4 4,4
21011
60,8 7,1 3,0 6,2 0,7 1,3 6,6 3,2 0,1 4,9 8,0 3,6 6,3 10,0 0,4 0,5 4,3 2,0 2,0
21010
Avionics solution 4 Dual controls copilot Copilot I-Panel extension 10" (*) Avionics compartment Slant panel Copilot static system Bleed air heating (**) Search & Landing light (450W) Copilot door sliding window Windshield wiper 25 Ah battery (*) 200 A starter generators Dual AC System IFR pitch/roll SAS Map case on I-Panel glare shield Map case in copilot door Radar Altimeter KRA 405B / KNI 416 ELT C406-2 HM (ARTEX) 3 frequencies 2nd directional Gyro (3” unslaved indicator) 205 1BL (BFGoodrich) First aid kit Engine fire extinguishing
21001
Weight (lbs)
L2300-004-02 L6701-001-00 L3111-001-00 L2576-001-00 L3113-001-00 L3411-001-00 L2104-100-00 L3343-003-00 L5211-001-00 L3042-001-00 L2433-001-00 L2432-001-00 L2420-003-00 L2217-001-50 L3111-001-10 L2514-003-01 L3441-002-00 L2563-090-05 L3421-091-02
Minimum requirement equipment
PINAO code based on avionics solution 4 21000
Weight (kg)
Technical Data
X X
(**) Select L2104-003-00 instead for EMS helicopters
L3441-002-00
4,3
9,5
X
X
X
X
ON REQUEST
2,9
6,4
X
X
X
X
X
X
X
X
L2313-008-00
12,5
27,6
X
X
X
X
X
X
X
X 4) 5)
11,0 8,8
X
X
X
X
X
X
X
X 3) 4) 5) 14)
X
X
X
X
X
X
X
X 3) 5) 14)
ON REQUEST ON REQUEST
5,0 4,0
ON REQUEST
3,5
7,7
X
X
X
X
X
X
X
X 3) 5) 14)
ON REQUEST
TBC
TBC
X
X
X
X
X
X
X
X 4) 5) 14)
ON REQUEST
10,0
22,1
X
X
X
X
X
X
X
X 4) 5) 14)
L3452-092-03
5,8
12,8
X
X
X
X
X
X
X
X 15)
ON REQUEST
7,7
17,0
L2313-010-03
2,8
6,2
X
X
X
X
X
X
X
X 9) 14)
L3167-092-02
0,4
0,9
X
X
X
X
X
X
X
ON REQUEST
2,9
6,4
X
X
X
X
X
X
X
X TRIMBLE required
L3442-092-14
2,3
5,1
X
X
X
X
X
X
X
X
L3443-090-04
6,2
13,7
X
X
X
X
X
X
X
X 9)
L3443-090-02/ L2571-001-00
14,0
30,9
X
X
X
X
X
X
X
X 9) In console
L3443-090-06/ L2571-001-00
14,0
30,9
X
X
X
X
X
X
X
X 9) In console
ON REQUEST
TBC
TBC X
X
X
X
X
X
X 11) 14)
9) 14)
TBC
9) In console
Moving Map DKG 3 (Dornier, basic version)
L3168-090-01
3,2
7,1
X
Stand alone Moving Map Euro Nav III (Euro Avionics):
L3168-092-03
10,0
22,1
X
X
X
X
X
X
X
X 4) 5) 9) 14)
ELT 100 HM (ARTEX) ELT C406-2 HM (ARTEX) 3 frequencies
L2563-801-02
2,0
4,4
X
or
X
or
X
or
X
or
L2563-090-05
2,1
4,6
X or
X
or
X
or
X
or 13)
or
X
or
X
or
X
or
ELT C406-2 HM (ARTEX) 3 frequencies Nav. Option
L2563-821-52
2,1
4,6
X
ELT JE 290 (JOLLIET)
L2563-808-01
2,1
4,6
X
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 3) BFE required 4) Requirement of avionics compartment has to be checked 5) Requirement of centre console has to be checked 9) Stand alone system; physical integration has to be checked
135.02.101.01.E
X
X
X
11) GPS required 13) ARINC 429 GPS required 14) 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. 15) should be checked with customer airport landing requirements
32
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
EC 135
31101
31110
31111
X X
31100
X
X X
X
X
31011
X
31010
X X X X X X X X X X X X X X X X X
31001
X X X X X X X X X X X X X X X X X
31000
X X
X X X X X X X X X X X X X X X X X X X X
21111
X
X X X X X X X X X X X X X X X X X X
21110
X X X X X X X X X X X X X X X X X
21101
(lbs) 21000 X X X X X X X X X X X X X X X X X
21100
L3441-090-04 L2563-090-05 L2217-001-50 L2212-001-00 L2562-001-00 L2621-001-00
147,6 15,7 6,0 13,7 1,5 1,5 2,9 14,6 7,1 0,2 10,8 42,8 8,0 7,1 0,9 1,1 35,1 7,1 4,4 22,1 85,1 2,6 8,4
21011
Radar Altimeter KRA 405B ELT C406-2 HM (ARTEX) 3 frequency IFR pitch/roll SAS Digital AFCS (DAFCS) First aid kit Engine fire extinguishing
66,8 7,1 2,7 6,2 0,7 2,1 1,3 6,6 3,2 0,1 4,9 19,4 3,6 3,2 0,4 0,5 15,9 3,2 2,0 10,0 38,5 1,3 3,8
21010
L2300-007-02 L6701-001-00 L3111-001-03 L2576-001-00 L3113-001-00 L3113-004-00 L3411-001-00 L2104-100-00 L3343-003-00 L5211-001-00 L3042-001-00 L2433-005-00 L2432-001-00 L2420-002-00 L3111-001-10 L2514-003-01 L2212-300-00
PINAO code based on avionics solution 7 21001
Avionics solution 7 Dual controls copilot Copilot I-Panel extension 7" Avionics compartment Slant panel Centre console Copilot static system Bleed air heating (**) Search & Landing light (450W) Copilot door sliding window Windshield wiper 40 Ah battery 200 A starter generator AC System Map case on I-Panel glare shield Map case in copilot door MEGHAS sensor kit
(kg)
Minimum requirement equipment
Weight
Weight
Technical Data
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X X
X
X X X X X X X X X X X X X X X X X X X X
X
X X
X
X
X X
X
X X X
X
X X
X
X X X
X
X
(**) Select L2104-003-00 instead for EMS helicopters Possible add-ons Radar Altimeter KRA 405B (HONEYWELL) Radar Altimeter AHV16 (THALES) Exchange of 2 SMD45 screens to one SMD68 on copilot side Digital AFCS (DAFCS)
L3441-090-04 L3441-090-06 ON REQUEST
3,2 4,0 +1,1
7,1 8,8 +2,4
L2212-001-00
38,5
85,1
Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in cabin) HF Communication system KHF 990/KFS 594 (HONEYWELL) Tactical FM Radio Teledux 9 (AEG) 2m or 4m BFE required Tactical FM Radio GM 900 (MOTOROLA) BFE required Tactical FM Radio MCS 2000 (MOTOROLA) BFE required Tactical FM Radio Tac / Com II (NAT) VHFlow, VHF-high, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins Automatic Direction Finder DFS 43 DF Chelton DF931(stand alone) Stand alone SAR DF517 (BECKER) GPS Nav System 2101 I/O Approach + Stormscope WX 1000 429E (GOODRICH) Colour weather radar RDR2000 (HONEYWELL) (radome included) Colour weather search radar Moving Map DKG 3 (Dornier, basic version) Moving Map System DKG 4 (Dornier) Map generator control unit + options Moving Map system Euro Nav III ELT 100 HM (ARTEX) ELT C406-2 HM (ARTEX) 3 frequencies ELT C406-2 HM (ARTEX) 3 freq Nav. Option ELT JE 290 (JOLLIET)
ON REQUEST
2,9
6,4
L2313-008-00
12,5
27,6
ON REQUEST
5,0
ON REQUEST
X X X
or or X X
X X X
X X X
or or X X
or or or or or or or or X X X X X X X X
instead of pitch/roll SAS (Rad. Alt. required) X X X X X X X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
11,0
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 14)
4,0
8,8
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 14)
ON REQUEST
3,5
7,7
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 14)
ON REQUEST
TBC
TBC
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 14)
ON REQUEST
10,0
22,1
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 14)
L3452-092-05 ON REQUEST L2313-010-03 L3442-092-12 L3443-090-07 L3443-090-02/ L2571-001-00 ON REQUEST L3168-090-01 L2444-002-10
7,0 7,7 2,8 2,3 6,2 10,0
15,5 17,0 6,2 5,1 13,7 22,1
X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
X X X X X X
TBC 3,2 3,4
TBC 7,1 7,5
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
X X X
L3168-090-08 L2563-801-02 L2563-090-05 L2563-821-52 L2563-808-01
9,0 2,0 2,1 2,1 2,1
19,9 4,4 4,6 4,6 4,6
X X X X X
X or
X X X X X
X or
X X X X X
X or
X X X X X
X or
X X X X X
X or
X X X X X
X or
X X X X X
X or
X X X X X
X 10) X 11) 14) X 10) 11) 14) X 10) 11) 14) or
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required
135.02.101.01.E
X X X
or or
or or
or or
or or
or or
or or
or or
15) 9) 14) 9) 14) 9) 10)
or 13) or
13) ARINC 429 GPS required 14) 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. 15) should be checked with customer airport landing requirements
33
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
EC 135
21001
21010
21011
21100
21101
21110
21111
31000
31001
31010
31011
31100
31101
31110
31111
PINAO code based on avionics solution 8 21000
(lbs)
Weight
(kg)
Weight
Technical Data
L2300-008-02
74,4
164,3
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
L6701-001-00 L3111-001-03 L2576-001-00 L3113-001-00 L3113-004-00 L3411-001-00 L2104-100-00 L3343-003-00 L5211-001-00 L3042-001-00 L2433-005-00 L2432-001-00 AC System L2420-002-00 Map case on I-Panel glare shield L3111-001-10 Map case in copilot door L2514-003-01 MEGHAS sensor kit L2212-300-00 Radar Altimeter KRA 405B (HONEYWELL) L3441-090-04 ELT C406-2 HM (ARTEX) 3 frequencies L2563-090-05 IFR pitch/roll SAS L2217-001-50 Digital AFCS (DAFCS) L2212-001-00 First aid kit L2562-001-00 Engine fire extinguishing L2621-001-00 (**) Select L2104-003-00 instead for EMS helicopters
7,1 2,7 6,2 0,7 2,1 1,3 6,6 3,2 0,1 4,9 19,4 3,6 3,2 0,4 0,5 15,9 3,2 2,0 10,0 38,5 1,3 3,8
15,7 6,0 13,7 1,5 1,5 2,9 14,6 7,1 0,2 10,8 42,8 8,0 7,1 0,9 1,1 35,1 7,1 4,4 22,1 85,1 2,6 8,4
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X
X
X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X X
X
X X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X
X
X X X X X X X X X X X X X X X X X X X
X
X X
X
X
X
X X X
X
X X
X X
X
X X
X X X
Minimum requirement equipment Avionics solution 8 Dual controls copilot Copilot I-Panel extension 7" Avionics compartment Slant panel Centre console Copilot static system Bleed air heating (**) Search & Landing light (450W) Copilot door sliding window Windshield wiper 40 Ah battery 200 A starter generators
X
X
X
X
Possible add-ons Radar Altimeter KRA 405B (HONEYWELL) Radar Altimeter AHV16 (THALES) Digital AFCS (DAFCS)
L3441-090-04 3,2 L3441-090-06 4,0 L2212-001-00 38,5
7,1 8,8 85,1
Exchange of 2 SMD45 screens to one SMD68 on copilot side Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in passenger cabin) HF Communication system KHF 990/KFS 594 Tactical FM Radio Teledux 9 (AEG) 2m or 4m Tactical FM Radio GM 900 (MOTOROLA) Tactical FM Radio MCS 2000 (MOTOROLA) Tactical FM Radio Tac / Com II (NAT) VHF-low, VHF-high, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins) Not civil certified
ON REQUEST
+1,1
+2,4
X X X X or or X X or or instead of pitch/roll SAS (Rad. Alt. required) X X X X X X X X
ON REQUEST
2,9
6,4
X
X
X
X
X
X
X
L2313-008-00 12,5 ON REQUEST 5,0 ON REQUEST 4,0 ON REQUEST 3,5 ON REQUEST TBC
27,6 11,0 8,8 7,7 TBC
X X X X X
X X X X
X X X X X
X X X X X
X X X X X
X X X X X
ON REQUEST
10,0
22,1
X
X
X
X
X
Automatic Direction Finder DFS 43 (incl. CD 432B) L3452-092-05
X X
or or or or or or or or
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X X X X X
X
X
X
X
X
X
X
X
X
X
X 14)
3) 14) 3) 14) 3) 14) 14)
7,0
15,5
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 15)
Direction Finder Chelton DF931 stand alone Stand alone SAR DF (BECKER)
ON REQUEST
7,7
17,0
L2313-010-03
2,8
6,2
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X X
X 9) 14) X 9) 14)
FMS/Radio management with GPS Canadian Marconi (CMA3000 + CMA 3012)
ON REQUEST
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
9,3
20,5 X
GPS Nav System 2101 I/O Approach + (TRIMBLE) L3442-092-12
2,1
4,6
X
X
X
X
X
X
X
X
X
X
X
Stormscope WX 1000 429E (GOODRICH)
L3443-090-07
6,2
13,7
X
X
X
X
X
X
X
X
X
X
X
Colour weather radar RDR2000 (HONEYWELL) (radome included)
L3443-090-02/ 10,0 L2571-001-00
22,1
X
X
X
X
X
X
X
X
X
X
X
Colour weather search radar
ON REQUEST
TBC
TBC
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 10)
Moving Map DKG 3 (Dornier, basic version)
L3168-090-01
3,2
7,1
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 11) 14)
Moving Map System DKG 4 (Dornier) Map generator control unit + options
L2444-002-10
3,4
7,5
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X 10) 11) 14)
Moving Map System Euro Nav III
L3168-090-08
9,0
19,9
ELT 100 HM (ARTEX)
L2563-801-02
2,0
4,4
X X
X or
X X
X or
X X
X or
X X
X or
X X
X or
X X
X or
X X
X or
X X
X 10) 11) 14) or
ELT C406-2 HM (ARTEX) 3 frequencies
L2563-090-05
2,1
4,6
X or
X
or
X
or
X
or
X
or
X
or
X
or
X
or 13)
or
X
or
X
or
X
or
X
or
X
or
X
or
X
or
ELT C406-2 HM (ARTEX) 3 freque Nav. Option
L2563-821-52
2,1
4,6
X
ELT JE 290 (JOLLIET)
L2563-808-01
2,1
4,6
X
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 3) BFE required 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required
135.02.101.01.E
X
X
X
X
X
X
X
X
X
X
X
X
X
X 9)
X
X
X
X 10)
X
X
13) ARINC 429 GPS required 14) 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. 15) should be checked with customer airport landing requirements
34
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
EC 135
Avionics solution 9 Avionics compartment Slant panel Centre console Copilot static system Bleed air heating (**) Search & Landing light (450W) Windshield wiper 40 Ah battery 200 A starter generators AC System Map case on I-Panel glare shield MEGHAS sensor kit Digital AFCS (DAFCS) ELT C406-2 HM (ARTEX) 3 frequencies First aid kit Engine fire extinguishing
L2300-009-02 L2576-001-00 L3113-001-00 L3113-004-00 L3411-001-00 L2104-100-00 L3343-003-00 L3042-001-00 L2433-005-00 L2432-001-00 L2420-002-00 L3111-001-10 L2212-300-00 L2212-001-00 L2563-090-05 L2562-001-00 L2621-001-00 (**) Select L2104-003-00 instead for EMS helicopters
11111
11110
11101
11100
11011
11010
11001
PINAO code based on avionics solution 9 11000
Minimum requirement equipment
Weight (lbs)
Weight (kg)
Technical Data
63,4 140,1 X X X X X X X X 6,2 13,7 X X X X X X X X 0,7 1,5 X X X X X X X X 2,1 1,5 X X X X X X X X 1,3 2,9 X X X X X X X X 6,6 14,6 X X X X X X X X 3,2 7,1 X X X X X X X X 4,9 10,8 X X X X X X X X 19,4 42,8 X X X X X X X X 3,6 8,0 X X X X X X X X 3,2 7,1 X X X X X X X X 0,4 0,9 X X X X X X X X 15,9 35,1 X X X X X X X X 38,5 85,1 X X X X X X X X X X X X 2,0 4,4 X X X X 1,3 2,6 X X X X 3,8 8,4
Possible add-ons Radar Altimeter AHV16 (THALES) Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in passenger cabin) HF Communication system KHF 990/KFS 594 (HONEYWELL) Tactical FM Radio Teledux 9 (AEG) 2m or 4m Tactical FM Radio GM 900 (MOTOROLA) Tactical FM Radio MCS 2000 (MOTOROLA Tactical FM Radio Tac / Com II (NAT) VHF-low, VHFhigh, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins) Not civil certified ADF DFS 43 (incl. CD 432B) Direction Finder Chelton DF931(stand alone) Stand alone SAR DF517 (BECKER) GPS Nav System 2101 I/O Approach + (TRIMBLE) Stormscope WX 1000 429E (GOODRICH) Colour weather radar RDR2000 (HONEYWELL) (radome included)
L3441-090-06
4,0 2,9
8,8 6,4
or or or or or or or or X X X X X X X X
L2313-008-00 12,5
27,6
X X X X X X X X
ON REQUEST
ON REQUEST ON REQUEST ON REQUEST ON REQUEST
5,0 11,0 4,0 8,8 3,5 7,7 TBC TBC
X X X X
ON REQUEST
10,0
22,1
X X X X X X X X 14)
L3452-092-05
7,0 7,7 2,8 2,1 6,2
15,5 17,0 6,2 4,6 13,7
L3443-090-02 10,0 L2571-001-00
22,1
X X X X X X
ON REQUEST
L2313-010-03 L3442-092-12 L3443-090-07
X X X X
X X X X X
X X X X
X X X X X X
X X X X
X X X X X X
X X X X
X X X X
X X X X X X X X X X X
X X X X
X X X X X X
X X X X
X X X X X X
3) 14) 3) 14) 3) 14) 14)
15) 9) 14) 9) 14) 9) 10)
TBC TBC X X X X X X X X 10) 3,2 7,1 X X X X X X X X 11) 14)
Colour weather search radar
ON REQUEST
Moving Map Kneeboard DKG 3 (Dornier, basic version)
L3168-090-01
Moving Map System DKG 4 (Dornier) Map generator control unit + options Moving Map System Euro Nav III (Euro Avionics)
L2444-002-10
3,4
7,5
L3168-090-08
9,0
19,9
X X X X X X X X 10) 11) 14) X X X X X X X X 10) 11) 14)
ELT 100 HM (ARTEX)
L2563-801-02
1,9
4,2
X or X or X or X or
ELT C406-2 HM (ARTEX) 3 frequencies
L2563-090-05
2,1
4,6
X
ELT C406-2 HM (ARTEX) 3 frequencies Nav. Option
L2563-821-52
2,1
4,6
X or X or X or X or 13)
ELT JE 290 (JOLLIET)
L2563-808-01
2,1
4,6
X or X or X or X or
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 3) BFE required 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required
135.02.101.01.E
X
X
X
13) ARINC 429 GPS required 14) 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. 15) should be checked with customer airport landing requirements
35
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
EC 135
11101
11110
X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X
X X X X X X X X X X X X X X X X
X X X X X X X X X X X X X X
11111
11100
11010
11011
11001
Avionics solution 10 Avionics compartment Slant panel Centre console Copilot static system Bleed air heating (**) Search & Landing light (450W) Windshield wiper 40 Ah battery 200 A starter generators AC System Map case on I-Panel glare shield MEGHAS sensor kit Digital AFCS (DAFCS) ELT C406-2 HM (ARTEX) 3 frequencies First aid kit Engine fire extinguishing (**) Select L2104-003-00 instead for EMS helicopters
PINAO code based on avionics solution 10 11000
Minimum requirement equipment
Weight (lbs)
Weight (kg)
Technical Data
L2300-010-02 L2576-001-00 L3113-001-00 L3113-004-00 L3411-001-00 L2104-100-00 L3343-003-00 L3042-001-00 L2433-005-00 L2432-001-00 L2420-002-00 L3111-001-10 L2212-300-00 L2212-001-00 L2563-090-05 L2562-001-00 L2621-001-00
70,9 6,2 0,7 2,1 1,3 6,6 3,2 4,9 19,4 3,6 3,2 0,4 15,9 38,5 2,0 1,3 3,8
156,7 13,7 1,5 1,5 2,9 14,6 7,1 10,8 42,8 8,0 7,1 0,9 35,1 85,1 4,4 2,6 8,4
X X X X X X X X X X X X X X X X X X
L3441-090-06 ON REQUEST
3,6 2,9
12,0 or or or or or or or or 6,4 X X X X X X X X
L2313-008-00
12,5
27,6
X
X X X X X X X
ON REQUEST
5,0
11,0
X
X X X X X X X 14)
ON REQUEST
4,0
8,8
X
X X X X X X X 14)
ON REQUEST
3,5
7,7
X
X X X X X X X 14)
ON REQUEST
TBC
TBC
X
X X X X X X X 14)
ON REQUEST
10,0
22,1
X
X X X X X X X 14)
L3452-092-05 ON REQUEST L2313-010-03 ON REQUEST
7,0 7,7 2,8 9,3
15,5 17,0 6,2 20,5
X X X X
X X X X
Possible add-ons Radar Altimeter AHV16 (THALES) Comm. Control Syst.,3rd station AS 3100-XX (BECKER) (in passenger cabin) HF Communication system KHF 990/KFS 594 (HONEYWELL) Tactical FM Radio Teledux 9 (AEG) 2m or 4m BFE required Tactical FM Radio GM 900 (MOTOROLA) BFE required Tactical FM Radio MCS 2000 (MOTOROLA) BFE required Tactical FM Radio Tac / Com II (NAT) VHF-low, VHFhigh, UHF VHF / UHF - AM / FM Transceiver ARC 210 (Rockwell & Collins) Not civil certified Automatic Direction Finder DFS 43 (incl. CD 432B) Direction Finder Chelton DF931 stand alone Stand alone SAR DF (BECKER) FMS/Radio management with GPS Canadian Marconi (CMA3000 + CMA 3012) GPS Nav System 2101 I/O Approach plus (TRIMBLE)
X X X X
X X X X
X X X X
X X X X
X X X X
X 15) X 9) 14) X 9) 14) X
L3442-092-12
2,1
4,6
X
X X X X X X X
Stormscope WX 1000 429E (GOODRICH)
L3443-090-07
6,2
13,7
X
X X X X X X X 9)
Colour weather radar RDR2000 (HONEYWELL) (radome included) Colour weather search radar Moving Map Kneeboard DKG 3 Dornier, basic version
L3443-090-02/ L2571-001-00 ON REQUEST L3168-090-01
10,0
22,1
X
X X X X X X X 10)
TBC 3,2
TBC 7,1
X X
X X X X X X 10) X X X X X X X 11) 14)
Moving Map System DKG 4 (Dornier) Map generator control unit + options Moving Map System Euro Nav III (Euro Avionics): ELT 100 HM (ARTEX) ELT C406-2 HM (ARTEX) 3 frequencies
L2444-002-10
3,4
7,5
X
X X X X X X X 10) 11) 14)
L3168-090-08 L2563-801-02 L2563-090-05
9,0 2,0 2,1
19,9 4,4 4,6
X X X X X X X X 10) 11) 14) X or X or X or X or X X X X
ELT C406-2 HM (ARTEX) 3 frequencies Nav. Option
L2563-821-52
2,1
4,6
X or X or X or X or 13)
ELT JE 290 (JOLLIET)
L2563-808-01
2,1
4,6
X or X or X or X or
or) can be selected instead of the corresponding equipment installed within minimum PINAO package 9) Stand alone system; physical integration has to be checked 10) VRU (3ET) required 11) GPS required
135.02.101.01.E
13) ARINC 429 GPS required 14) 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. 15) should be checked with customer airport landing requirements
36
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
EC 135 Technical Data
3. Optional headsets and helmet The equipment listed below apply to any package/solution Manufacturer/Type
Linear Wire
Spiral Wire
HOLMBERG
90-04-0802210
•
HOLMBERG
90-04-0602510
•
DAVID CLARK
H 10-76
•
DAVID CLARK
H 10-56
•
SENNHEISER
HMEC 222 III
•
Low Imp.
High Imp.
ANR*
• • • • •
•
Reference
Weight kg
Weight lb.
L2315-001-60
0.7
1.5
L2315-001-61
0.7
1.5
L2315-001-10
0.5
1.1
L2315-001-11
0.5
1.1
L2315-001-52
0.4
0.9
* ANR: Active Noise Reduction Headsets
Manufacturer/Type GENTEX Helmet
SPH 5
Linear Wire
•
Spiral Wire
Low Imp.
•
High Imp.
ANR*
Reference L2315-002-10
Weight kg
Weight lb.
1.3
2.4
* ANR: Active Noise Reduction Headsets
135.02.101.01.E
37
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EC 135 Technical Data
Intentionally left blank
135.02.101.01.E
38
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EC 135 Technical Data
EQUIPMENT COMPATIBILITY This chart concisely states the nature of the incompatibility:
n
Impossibility of simultaneous fitment (hence impossible to sell the 2 items of equipment of the same helicopter) – (“totally incompatible fitment”)
u
Impossibility of simultaneous fitment but possible to sell on the same aircraft (removable parts of one of the items must be delivered, packed) – (“no simultaneous fitment”)
l
Possibility of simultaneous fitment on the same aircraft, but impossible to use simultaneously – (“no simultaneous use”)
Reference Optional
L1111-002-00 L1111-004-00 L2104-003-00 L2104-200-00 L2105-001-00
Key-words
Two-colour external painting Multicolour external painting EMS Bleed air heating system Bleed air heating system Air conditioning system
L2105-001-10 Air conditioning for tropical environment
L2212-001-00 DAFCS.
L-2212-300-00 MEGHAS sensor kit
L2217-001-10 VFR Pitch/Roll SAS L2217-001-50 IFR Pitch/Roll SAS L2300-001-02 Avionics solution 1 L2300-003-02 Avionics solution 3 L2300-004-02 Avionics solution 4 L2300-007-02 Avionics solution 7 L2300-008-02 Avionics solution 8 L2300-009-02 Avionics solution 9 L2300-010-02 Avionics solution 10 L2420-002-00 AC system L2420-003-00 Dual AC system L2433-001-00 Battery, "type Varta", (25Ah, 24V) L2433-002-00 Battery, type "Saft", 26Ah L2433-005-00 Battery, "type Varta", 40 Ah L2512-002-11 Pilot seat safety harness with manual lock L2512-002-02 Reversed copilot seat installation kit (position change on ground)
L2512-002-21 Manual lock for copilot seat
135.02.101.01.E
n
u
l
Key-words "totally "no "no incompatible simultaneous simultaneous fitment" fitment" use" L1111-004-00 Multicolour external painting L1111-002-00 Two-colour external painting L2104-200-00 Bleed air heating system L2104-003-00 Bleed air heating system: EMS-version L2105-001-10 Air conditioning system for tropical environment L8512-001-20 External hoist, detachable parts std.Start./Gen L8551-001-20 Light armour protection kit, detachable parts L2105-001-00 Air conditioning system L8512-001-20 External hoist, detachable parts std.Start./Gen L8551-001-20 Light armour protection kit, detachable parts std.Start./Gen L2217-001-10 VFR Pitch/Roll SAS L2217-001-50 IFR Pitch/Roll SAS L2300-001-02 Avionics solution 1 L2300-003-02 Avionics solution 3 L2300-004-02 Avionics solution 4 L2212-001-00 Digital Automatic Flight Control System L2217-001-50 IFR Pitch / Roll SAS L2212-001-00 Digital Automatic Flight Control System L2217-001-10 VFR Pitch / Roll SAS L2212-300-00 MEGHAS sensors kit L3111-001-03 Copilot instrument panel extension 7" L2212-300-00 MEGHAS sensors kit L3111-001-03 Copilot instrument panel extension 7" L2212-300-00 MEGHAS sensors kit L3111-001-03 Copilot instrument panel extension 7" L3111-001-00 Copilot instrument panel extension 10" L3111-001-01 Copilot instrument panel extension 11" L3111-001-00 Copilot instrument panel extension 10" L3111-001-01 Copilot instrument panel extension 11" L3111-001-00 Copilot instrument panel extension 10" L3111-001-01 Copilot instrument panel extension 11" L3111-001-00 Copilot instrument panel extension 10" L3111-001-01 Copilot instrument panel extension 11" L2420-003-00 Dual AC system L2420-002-00 AC system L2433-002-00 Battery, type "Saft", 26Ah L2433-005-00 Battery, "type Varta", 40 Ah L2433-001-00 Battery, type "Varta", 25Ah L2433-005-00 Battery, "type Varta", 40 Ah L2433-001-00 Battery, type "Varta", 25Ah L2433-002-00 Battery, type "Saft", 26Ah L2512-003-10 Pilot seat with height setting capability L2512-003-20 Copilot seat with height setting capability L2512-006-00 Winch operator seat L2525-101-76 VIP copilot's seat std copil. seat EMS-Equip L8551-001-20 Light armour protection kit, detachable parts L6701-001-00 Copilot flight controls L2512-003-20 Copilot seat with height setting capability L2512-006-00 Winch operator seat
39
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EC 135 Technical Data
Reference Optional
Key-words
L2512-003-10 Pilot seat with height setting capability
L2512-003-20 Copilot seat height adjustable
L2512-006-00 Winch operator seat turnable in flight
L2513-004-40 Floor covering, cabin with quick detachable VIP carpet
L2513-200-00 Floor covering, cockpit, washable
L2513-210-00 Floor covering, cargo compartment, washable L2513-220-00 Floor covering, cockpit, cabin and cargo compartment, washable
L2513-300-00 Floor covering, cockpit and cabin with carpet
L2513-310-00 Floor covering, cockpit, cabin and cargo compartment with carpet
L2514-003-01 Map case, integrated in copilot door L2522-004-10 Utility seat arrangement for 3 rear passengers, fixed provisions L2522-004-20 Utility seats for 3 rear pax, detachable parts (in addition to the standard seats)
135.02.101.01.E
n
u
l
Key-words "totally "no "no incompatible simultaneous simultaneous fitment" fitment" use" L2525-101-71 VIP pilot's seat std. pilot seat L2512-002-11 Pilot seat safety harness with manual lock L2512-002-20 Reversed copilot seat installation kit std. copil. seat L2512-002-21 Copilot seat safety harness with manual lock L2512-006-00 Winch operator seat L2525-101-76 VIP copilot's seat L2512-002-20 Reversed copilot seat installation kit L2512-002-21 Copilot seat safety harness with manual lock L2512-003-20 Copilot seat height adjustable L2513-004-40 Quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Floor covering with carpet complete L6701-001-00 Dual controls, copilot EMS-equip std. copil. seat L2525-101-76 VIP copilot's seat L8551-001-20 Light armour protection kit, detachable parts L2512-006-00 Winch operator seat turnable in flight L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Floor covering with carpet complete L2522-004-20 Utility seats det. parts model Eurocopter EMS-equip. L8522-320-00 Stretcher (16G), type Bucher L8522-350-00 Installation device for one Bucher stretcher L8525-002-20 Inst. device for 1 FERNO/aerolite litter L8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modified L8551-001-20 Light armour protection kit, detachable parts L2513-220-00 Floor washable complete L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Floor covering with carpet complete L2513-220-00 Floor washable complete L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Floor covering with carpet complete L2513-200-00 Floor covering, cockpit, washable L2513-210-00 Floor covering, cargo compartment, washable L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Floor covering with carpet complete L2512-006-00 Winch operator seat turnable in flight L2513-004-40 Quick detachable VIP carpet for cabin L2513-200-00 Floor covering, cockpit, washable L2513-210-00 Floor covering, cargo compartment, washable L2513-220-00 Floor covering washable, complete L8522-320-00 Stretcher (16G), type Bucher L8522-350-00 Installation device for one Bucher stretcher L8525-002-20 Inst. device for 1 FERNO/aerolite litter L8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modified L2513-310-00 Floor covering with carpet complete L8551-001-20 Light armour protection kit, detachable parts EMS-Equip. L2512-006-00 Winch operator seat L2513-004-40 Quick detachable VIP carpet for cabin L2513-200-00 Floor covering, cockpit, washable L2513-210-00 Floor covering, cargo compartment, washable L2513-220-00 Floor covering washable, complete L8522-320-00 Stretcher (16G), type Bucher L8522-350-00 Installation device for one Bucher stretcher L8525-002-20 Inst. device for 1 FERNO/aerolite litter L8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modified L2513-300-00 Floor covering, cockpit and cabin with carpet L8551-001-20 Light armour protection kit, detachable parts EMS-Equip. L2525-102-81 Executive kit L2524-001-00 cabin / cargo compartment separation wall L8551-001-20 Light armour protection kit, detachable parts L2513-004-40 Quick detachable VIP carpet for cabin L2524-001-00 Cabin / cargo compartment separation wall rear seats L2524-021-00 Cabin/cargo compartment separation curtain L8522-320-00 Stretcher (16 G), type Bucher L8522-350-00 Installation device for one Bucher stretcher L8525-002-20 Inst. device for 1 FERNO/aerolite litter EMS & VIP Equi L8525-003-00 FERNO/Aerolite litter, SRFW 12-2/16G modified L8551-001-20 Light armour protection kit, detachable parts
40
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
EC 135 Technical Data
Reference Optional
Key-words
L2524-001-00 Cabin / cargo compartment separation wall
L2524-002-00 Cockpit/cabin separating curtain L2524-003-00 NVG cockpit/ cabin separation curtain, L2524-021-00 Cabin/cargo separation curtain, compatible with avionics rack (including smoke detector)
L2525-101-71 VIP pilot’s seat L2525-101-76 VIP copilot’s seat
L2525-102-81 Executive kit L2562-001-00 First aid kit L2562-001-10 First aid kit for DGAC certification L2818-100-20 Internal long range fuel system, det. parts
L3042-001-00 Windshield wiper system L3043-001-00 Windshield wiper system with washing sys L3111-001-00 Copilot instrument panel extension 10"
L3111-001-01 Copilot instrument panel extension 11"
L3111-001-03 Copilot instrument panel extension 7"
L3111-001-10 Map cases on instrument panel L3215-001-21 Emergency floats, detachable parts,
L3216-001-10 High skid landing gear L3272-001-20 Snow skids, detachable parts
L3273-001-00 Lengthened skids L3274-001-20 L3312-003-00 L3322-001-00 L3343-003-00
Settling protectors, detachable parts NVG compatible standard cockpit layout Boarding step illumination Landing & searchlight 450 W
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u
"totally "no incompatible simultaneous fitment" fitment" L2522-004-20 L2522-004-30 L2524-021-00 EMS-Equip L8522-320-00 L8522-350-00 L8525-002-20 L8525-003-00 L8551-001-20 L2524-003-00 L3312-003-00 L2524-002-00 L2522-004-20 L2522-004-30 L2524-001-00 . EMS-Equip L8522-320-00 L8522-350-00 L8525-002-20 L8525-003-00 L8551-001-20 L2512-003-10 std pilot’s seat L2512-002-02 L2512-003-20 L2512-006-00 std copil. seat L2514-003-01 L3111-001-10 L2562-001-10 L2562-001-00 EMS & VIP Equip. L2513-310-00 L3043-001-00 L3042-001-00 L3111-001-01 L3111-001-03 L2300-007-02 L2300-008-02 L2300-009-02 L2300-010-02 L3111-001-00 L3111-001-03 L2300-007-02 L2300-008-02 L2300-009-02 L2300-010-02 L3111-001-00 L3111-001-01 L2300-001-02 L2300-003-02 L2300-004-02 L2525-102-81 L3273-001-00 L3216-001-10 L3272-001-20 L3215-001-21 L3215-001-21 L3216-001-10 L3274-001-20 L3215-001-21 L3216-001-10 L3272-001-20 L2524-002-00 L3353-005-00 L3343-006-00
l
Utility seat arrangement for 3 rear passengers Utility seat arrangement for 3 rear passengers Cabin/cargo compartment curtain Stretcher (16 G), type Bucher Installation device for one Bucher stretcher Inst. device for 1 FERNO/aerolite litter FERNO/Aerolite litter, SRFW 12-2/16G modified Light armour protection kit, detachable parts NVG compatible cockpit/cabin separation curtain NVG-compatible std cockpit layout Cockpit/cabin separation curtain Utility seat arrangement for 3 rear passengers Utility seat arrangement for 3 rear passengers Cabin/cargo compartment separation wall Stretcher (16 G), type Bucher Installation device for one Bucher stretcher Inst. device for 1 FERNO/aerolite litter FERNO/Aerolite litter, SRFW 12-2/16G modified Light armour protection kit, detachable parts Height adjustable pilot’s seat Reversed copilot’s seat installation kit Height adjustable copilot’s seat Winch operator seat turnable in flight Map case integrated in copilot door Map case on instrument panel glare shield First aid kit for DGAC certification First aid kit
L8511-002-20 L3343-006-00 Landing & searchlight 400 W/200W NVG compatible L3346-100-10 SX16, front installation fixed provisions
135.02.101.01.E
L3343-003-00 L8511-002-20 L2571-001-00 L3346-300-10 L3346-400-20
Key-words
"no simultaneous use"
Carpet for cockpit, cabin & cargo compartment Windshield wiper with washing device Windshield wiper system Copilot instrument panel extension 11" Copilot instrument panel extension 7" Avionics solution 7 Avionics solution 8 Avionics solution 9 Avionics solution 10 Copilot instrument panel extension 10" Copilot instrument panel extension 7" Avionics solution 7 Avionics solution 8 Avionics solution 9 Avionics solution 10 Copilot instrument panel extension 10" Copilot instrument panel extension 11" Avionics solution 1 Avionics solution 3 Avionics solution 4 Executive kit Lengthened skids High skid landing gear Snow skids, detachable parts Emergency floats, detachable parts Emergency floats, detachable parts High skid landing gear Settling protectors, detachable parts Emergency floats, detachable parts High skid landing gear Snow skids, detachable parts Cockpit/cabin separating curtain Emergency lights Landing & searchlight 400/200W NVG Cargo hook mirrors detachable parts Landing & searchlight 450 W Cargo hook mirrors detachable parts Radar radom SX16, LH, MFS mounted, fixed provisions SX16, LH, MFS mounted, detachable parts
41
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
EC 135 Technical Data
Reference Optional
Key-words
L3346-100-20 SX16, front installation, detachable parts, (without vendor parts) L3346-300-10 Search light SX 16 fixed provisions LH MFS mounted L3346-400-20 SX16 MFS mounted detachable parts, without vendor parts L3353-005-00 Emergency lights L5213-001-11 Int. and max. posi. sliding door fastener LH L5213-001-12 Sliding door fastener, max. position, LH L5213-001-21 Inter&max. position sliding door fastener RH L5213-001-22 Sliding door fastener, max. position, RH L6701-001-00 Dual controls L6721-001-00 Copilot flight controls cover L7161-001-00 Sand filter system L8511-002-20 Cargo hook mirrors detachable parts L8512-001-10 External hoist, fixed provisions L8512-001-20 External hoist, detachable part
L8514-001-00 Multipurpose attachment hardpoints
L8522-320-00 Folding stretcher (16 G), type Bucher
L8522-350-00 Stretcher retainer system for one Bucher-type folding stretcher (16G)
L8525-002-20 Litter installation device for one Ferno/Aerolite-type litter, model SRFW 12-2/16 G modified
L8525-003-00 FERNO/Aerolite-type foldable litter, model SRFW 12-2 / 16G modified
135.02.101.01.E
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Key-words "totally "no "no incompatible simultaneous simultaneous fitment" fitment" use" L2571-001-00 Radar radom L3346-300-10 SX16, LH, MFS mounted, fixed provisions L3346-400-20 SX16, LH, MFS mounted, detachable parts L3346-100-10 SX16, front installation, fixed provisions L3346-100-20 SX16, front installation, detachable parts, L3346-100-10 SX16, front installation, fixed provisions L3346-100-20 SX16, front installation, detachable parts, L3322-001-00 Boarding step illumination L5213-001-12 Sliding door fastener, max. position, LH L5213-001-11 Interme&max. position sliding. door fastener, LH L5213-001-22 Sliding door fastener, max. position, RH L5213-001-21 Interme&max. position sliding. door fastener, LH L2512-006-00 Winch operator seat instead of copilot seat, L6721-001-00 Copilot controls cover L6701-001-00 Copilot flight controls L8512-001-20 External hoist, detachable parts std.Start./Gen L3343-003-00 Landing & searchlight 450 W L3343-006-00 Landing & searchlight 400/200 W NVG L8534-000-11 Rope-down device, LH, fixed provisions L2105-001-00 Air conditioning/cooling system (Vapour cycle) L2105-001-10 Air conditioning for tropical environment std.Start./Gen L8544-002-00 Lashing points for high wind speeds L7161-001-00 Sand filter system L8534-000-12 Rope down device for 2 persons, det. parts, LH L8512-001-10 External hoist, fixed provisions L8534-00-11 Rope-down device, fixed provisions LH L8534-00-21 Rope-down device, fixed provisions RH L2513-004-40 quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Carpet for cockpit, cabin and cargo compartment L2522-004-20 Utility seats for 3 rear passengers, det.parts L2522-004-30 Utility seats for 3 rear passengers, det. parts L2524-001-00 Cabin / cargo compartment separation wall L2524-020-00 Cabin/cargo compartment separation curtain L8525-002-20 Installation device for one FERNO/Aerolite-type 1 std rear seat L8525-003-00 FERNO/Aerolite-type litter, 12-2/16G modified L8551-001-20 Armour protection kit, detachable parts L2513-004-40 Quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Carpet for cockpit, cabin and cargo compartment L2522-004-20 Utility seats for 3 rear passengers, det. parts L2522-004-30 Utility seats for 3 rear passengers, det. part L2524-001-00 Cabin / cargo compartment separation wall L2524-020-00 Cabin/cargo compartment separation curtain L8525-002-20 Installation device for one FERNO/Aerolite-type 1 std rear seat L8525-003-00 FERNO/Aerolite-type litter, 12-2/16G modified L8551-001-20 Armour protection kit, detachable parts L2513-004-40 Quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Carpet for cockpit, cabin and cargo compartment L2522-004-20 Utility seat for 3 rear passengers, det. parts L2522-004-30 Utility seat for 3 rear passengers, det. part L2524-001-00 Cabin / cargo compartment separation wall L2524-020-00 Cabin/cargo compartment separation curtain L8522-320-00 Folding stretcher (16 G), type Bucher 1 std rear seat L8522-350-00 Stretcher retainer for one Bucher- stretcher L8551-001-20 Armour protection kit, detachable parts L2513-004-40 Quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Carpet for cockpit, cabin and cargo compartment L2522-004-20 Utility seats for 3 rear passengers, det. parts L2522-004-30 Utility seats for 3 rear passengers, det. part L2524-001-00 Pax/cargo compartment separation wall L2524-020-00 Cabin/cargo compartment separation curtain L8522-320-00 Folding stretcher (16 G), type Bucher L8522-350-00 Stretcher retainer for one Bucher- stretcher 1 std rear seat L8551-001-20 Armour protection kit, detachable parts
42
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
EC 135 Technical Data
Reference Optional
Key-words
L8534-000-11 Rope-down device fixed provisions, LH L8534-000-12 Rope-down device for two persons, detachable parts, LH L8544-002-00 Lashing points for high wind speeds L8551-001-20 Light armour protection kit, cockpit and cabin, detachable parts
135.02.101.01.E
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Key-words "totally "no "no incompatible simultaneous simultaneous fitment" fitment" use" L8512-001-10 External hoist, fixed provisions L8512-001-20 External hoist, detachable parts L8544-002-00 Lashing points for high wind speeds L8512-001-20 External hoist, detachable part L8534-000-12 Rope-down device, detachable parts, LH L2105-001-00 Air conditioning system L2105-001-10 Air conditioning system for tropical environment L2512-002-20 Reversed copilot seat, installation kit L2512-006-00 Winch operator seat L2513-004-40 Quick detachable VIP carpet for cabin L2513-300-00 Floor covering, cockpit and cabin with carpet L2513-310-00 Carpet for cockpit, cabin and cargo compartment L2522-004-20 Utility seat for 3 passengers, det. parts L2524-001-00 Cabin/cargo compartment separation wall L8522-320-00 Folding stretcher (16 G), type Bucher L8522-350-00 Stretcher retainer for one Bucher-type stretcher L8525-002-20 Installation device for one FERNO/Aerolite-type
43
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
EC 135 Technical Data
Intentionally left blank
135.02.101.01.E
44
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
EC 135 Technical Data
MAIN PERFORMANCE The following performance values and figures refer to an EC135, equipped with average production engines. 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.
The EC135 P2 will be certified over the complete envelope and for the increased OEI power levels for the end of march 2002, and therefore some performance data have to be considered as preliminary (OEI hover/climb) or are not available yet (Cat. A) PERFORMANCE ON 2 ENGINES Pratt & Whitney PW206B2 Gross Weight
kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
§
Maximum speed VNE
km/h kts
287 155
278 150
278 150
278 150
259 140
§
Maximum cruising speed
km/h kts
262 141
261 141
259 140
257 139
256 138
§
Fuel consumption at fast cruise speed
kg/h lb/h
232.5 512.5
232.5 512.5
232.5 512.5
232.5 512.5
232.5 512.5
§
Economical cruising speed
km/h kts
220 119
224 121
226 122
228 123
229 124
§
Fuel consumption at economical cruising speed
kg/h lb/h
187.5 413.5
193 425.5
198 436.5
201 443
205 452
§
Fuel consumption at 65 KIAS
kg/h lb/h
143.5 316.5
148.5 327.5
155 342
157.5 347.2
161 355
§
Rate of climb (TOP)
m/s ft/min
11.7 2300
10.4 2050
8.9 1750
8.4 1,650
7.6 1,500
§
Hover ceiling IGE (TOP), no wind or headwind (4 ft AGL), ISA
m ft
4,570 1) 15,000
1)
4,570 1) 15,000
1)
4,450 14,600
4,140 13,600
3,045 2) 10,000
§
Hover ceiling IGE (TOP), no wind (4 ft AGL), ISA + 20°C
m ft
3,880 1) 12,750
1)
3,880 1) 12,750
1)
3,230 10,600
2,830 9,300
2,315 7,600
§
Hover ceiling OGE (TOP), ISA
m ft
4,570 1) 15,000
1)
4,420 14,500
3,580 11,750
3,260 10,700
2,190 7,200
§
Hover ceiling OGE (TOP), ISA + 20°C
m ft
3,880 1) 12,750
1)
3,155 10,350
2,075 6,800
1,640 5,400
1,100 3,600
§
Service ceiling, MCP, (climb reserve 200 ft/min), ISA
m ft
4,572 3) 15,000
3)
4,572 3) 15,000
1)
2) 3)
3)
3)
4,572 3) 15,000
3)
4,572 3) 15,000
2)
15,000 ft density altitude certification limit 10,000 ft pressure altitude certification limit this limitation may be suppressed during the year 2002.
135.02.101.01.E
2)
3,045 2) 10,000
45
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
EC 135 Technical Data
PERFORMANCE ON 2 ENGINES Pratt & Whitney PW206B2 kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
km nm km nm
640 345 835 451
635 343 825 445
625 337 815 440
620 335 810 437
615 332 805 434
km nm km nm
670 362 863 466
660 356 853 460
655 353 843 455
651 351 838 452
646 349 833 450
• standard tank configuration (536 kg) • long rang tank configuration
h:min h:min
3:54 5:06
3:45 4:57
3:36 4:48
3:33 4:42
3:30 4:36
• standard tank configuration (560 kg*) • long rang tank configuration
h:min h:min
4:05 5:17
4:56 5:08
3:48 4:56
3:45 4:53
3:39 4:47
Gross Weight
§
Maximum range (without fuel reserve at economical cruise speed) • standard tank configuration (536 kg) • long rang tank configuration • standard tank configuration (560 kg*) • long rang tank configuration
§
Maximum endurance (without fuel reserve at 65 KIAS
*only available from the helicopter with the S/N (Serial Number) 250 onwards. PERFORMANCE ON 1 ENGINE Pratt & Whitney PW206B2 Gross Weight
kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
§
Service ceiling w. 100 ft/min climb reserve (MCP OEI-power) at ISA
m ft
4,890 16,050
4,265 14,000
3,550 11,650
3,275 10,750
2,925 9,600
§
Service ceiling w. 100 ft/min climb reserve (MCP OEI-power) at ISA + 20°C
m ft
4,210 13,800
3,505 11,500
2,695 8,850
2,375 7,800
1,965 6,450
§
Rate of climb (MCP OEI-power at SL)
m/s ft/min
4.0 785
3.0 585
1.9 380
1.5 300
1.1 215
§
Max. temperature for CAT A take-off from clear heliport at SL
°C
+ 50
+ 50
+ 50
+ 50
+ 45
§
Max. gross weight hover ceiling OGE, SL, ISA, OEI, no wind (30-sec-power)
kg lb
2,665 5,875
§
Max. gross weight hover ceiling OGE, SL, ISA + 20°C, OEI, no wind (30-sec-power)
kg lb
2,550 5,622
§
Max. gross weight hover ceiling IGE, SL, 4ft ISA, OEI, no wind (2-min-power)
kg lb
2,835 6,250
§
Max. gross weight hover ceiling IGE, SL, 4ft ISA + 20°C, OEI, no wind (2-min-power)
kg lb
2,630 5,798
§
Max. gross weight CAT A, VTOL, SL, (ISA / ISA + 10°C)
kg lb
2,835 6,250
135.02.101.01.E
46
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EC 135 Technical Data
The EC135T2 will be certified over the complete flight envelope for mid. 2002, and therefore performance data have to be considered as preliminary (OEI hover/climb, Cat A)
PERFORMANCE ON 2 ENGINES Turbomeca Arrius 2B2 Gross Weight
kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
§
Maximum speed VNE
km/h kts
287 155
278 150
278 150
278 150
259 140
§
Maximum cruising speed
km/h kts
262 141
261 141
259 140
257 139
256 138
§
Fuel consumption at fast cruise speed
kg/h lb/h
237 522
237 522
237 522
237 522
237 522
§
Economical cruising speed
km/h kts
231 125
233 126
235 127
237 128
239 129
§
Fuel consumption at economical cruising speed
kg/h lb/h
204 450
208.5 460.0
213 470
215.5 475.0
219 483
§
Fuel consumption at 65 KIAS
kg/h lb/h
155.5 343.0
160 353
166 366
168.5 371.5
171.5 378.0
§
Rate of climb (TOP)
m/s ft/min
11.7 2,300
10.4 2,050
8.9 1,650
8.4 1,650
7.6 1,500
§
Hover ceiling IGE (TOP), no wind or headwind (4 ft AGL), ISA
m ft
4,570 1) 15,000
1)
4,570 1) 15,000
1)
4,320 14,150
4,040 13,250
3,045 2) 10,000
§
Hover ceiling IGE (TOP), no wind (4 ft AGL), ISA + 20°C
m ft
3,880 1) 12,750
1)
3,880 1) 12,750
1)
3,100 10,150
2,740 9,000
2,255 7,400
§
Hover ceiling OGE (TOP), ISA
m ft
4,570 1) 15,000
1)
4,290 14,050
3,480 11,400
3,100 10,200
2,190 7,200
§
Hover ceiling OGE (TOP), ISA + 20°C
m ft
3,880 1) 12,750
1)
3,050 10,000
1,955 6,400
1,525 5,000
1,005 3,300
§
Service ceiling, MCP, (climb reserve 200 ft/min), ISA
m ft
6,095 20,000
6,095 20,000
5,480 18,000
5,225 17,150
3,045 2) 10,000
1) 2)
2)
15,000 ft density altitude certification limit 10,000 ft pressure altitude certification limit
135.02.101.01.E
47
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
2)
EC 135 Technical Data
PERFORMANCE ON 2 ENGINES Turbomeca Arrius 2B2 kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
km nm km nm
610 329 795 429
605 326 790 426
600 324 785 424
598 322 780 421
595 321 775 418
km nm km nm
641 346 823 444
636 343 818 441
626 338 808 436
625 337 804 434
621 335 799 431
• standard tank configuration (536 kg) • long rang tank configuration
h:min h:min
3:33 4:39
3:27 4:33
3:21 4:24
3:18 4:21
3:15 4:15
• standard tank configuration (560 kg*) • long rang tank configuration
h:min h:min
3:45 4:50
3:39 4:42
3:30 4:32
3:27 4:29
3:24 4:26
Gross Weight
§
Maximum range (without fuel reserve at economical cruise speed) • standard tank configuration (536 kg) • long rang tank configuration • standard tank configuration (560 kg*) • long rang tank configuration
§
Maximum endurance (without fuel reserve at 65 KIAS
*only available from the helicopter with the S/N (Serial Number) 250 onwards. PERFORMANCE ON 1 ENGINE Turbomeca Arrius 2B2 Gross Weight
kg
2,200
2,400
2,630
2,720
2,835
lb
4,850
5,290
5,800
6,000
6,250
§
Service ceiling w. 100 ft/min climb reserve (MCP OEI-power) at ISA
m ft
5,150 16,900
4,510 14,800
3,790 12,450
3,520 11,500
3,045 2) 10,000
§
Service ceiling w. 100 ft/min climb reserve (MCP OEI-power) at ISA + 20°C
m ft
4,510 14,800
3,730 12,250
2,830 9,300
2,500 8,200
2,070 6,800
§
Rate of climb (MCP OEI-power at SL)
m/s ft/min
4.0 785
3.0 585
1.9 380
1.5 300
1.1 215
§
Max. temperature for CAT A take-off from clear heliport at SL
°C
+ 50
+ 50
+ 50
+ 50
+ 46
§
Max. gross weight hover ceiling OGE, SL, ISA, OEI, no wind (30-sec-power)
kg lb
2,665 5,875
§
Max. gross weight hover ceiling OGE, SL, ISA + 20°C, OEI, no wind (30-sec-power)
kg lb
2,615 5,765
§
Max. gross weight hover ceiling IGE, SL, 4ft ISA, OEI, no wind (2-min-power)
kg lb
2,835 6,250
§
Max. gross weight hover ceiling IGE, SL, 4ft ISA + 20°C, OEI, no wind (2-min-power)
kg lb
2,690 5,930
§
Max. gross weight CAT A, VTOL, SL, (ISA / ISA + 10°C)
kg lb
2,835 6,250
2)
10,000 ft pressure altitude certification limit
135.02.101.01.E
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EC 135 Technical Data
OPERATING LIMITATIONS The helicopter can be operated within the following altitude limitations (according to the Flight Manual):
Gross Weight
2,720 kg 6,000 lb
2,835 kg 6,250 lb
§ Maximum operating altitude
6,100 m PA 20,000 ft PA
3,048 m PA 10,000 ft PA
§ Maximum operating altitude for hover in ground effect, takeoff and landing
4,570 m DA 15,000 ft DA
3,048 m PA 10,000 ft PA
§ Minimum temperature
- 35°C (- 31°F)
§ Maximum temperature
ISA + 39°C (max. + 50°C/ + 122°F)
ABBREVIATIONS AGL DA IGE ISA MCP OEI
: : : : : :
Above Ground Level Density Altitude In Ground Effect International Standard Atmosphere Maximum Continuous Power One Engine Inoperative
135.02.101.01.E
OGE : Out Of Ground Effect PA : Pressure Altitude SL : Sea Level TOP : Take-Off Power VNE : Never-Exceed Speed VTOL: Vertical Take-Off and Landing
49
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EC 135 Technical Data
Hover In Ground Effect (HIGE, TOP, no wind) with two PW206B2 engines
135.02.101.01.E
50
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EC 135 Technical Data
Hover In Ground Effect (HIGE, TOP, no wind) with two ARRIUS 2B2 engines
135.02.101.01.E
51
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EC 135 Technical Data
Hover Out Of Ground effect (HOGE, TOP) with two PW206B2 engines
135.02.101.01.E
52
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EC 135 Technical Data
Hover Out Of Ground Effect (HOGE, TOP) with two ARRIUS 2B2 engines
135.02.101.01.E
53
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EC 135 Technical Data
Hover Out Of Ground effect (HOGE, OEI, 30 sec-power) with one PW206B2 engine
135.02.101.01.E
54
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EC 135 Technical Data
Hover Out Of Ground effect (HOGE, OEI, 2.0 min-power) with one PW206B2 engine
135.02.101.01.E
55
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EC 135 Technical Data
Hover Out Of Ground Effect (HOGE, OEI, 30 sec-power) with one ARRIUS 2B2 engine
135.02.101.01.E
56
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EC 135 Technical Data
Hover Out Of Ground effect (HOGE, OEI, 2.0 min-power) with one ARRIUS 2B2 engine
135.02.101.01.E
57
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EC 135 Technical Data
Maximum Cruising Speed with two PW206B2 engines
135.02.101.01.E
58
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EC 135 Technical Data
Maximum Cruising Speed with two ARRIUS 2B2 engines
135.02.101.01.E
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EC 135 Technical Data
Maximum Rate Of Climb, TOP with two PW206B2 engines, MTOW: 2835 kg
135.02.101.01.E
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EC 135 Technical Data
Maximum Rate Of Climb, TOP with two ARRIUS 2B2 engines, MTOW: 2835 kg
135.02.101.01.E
61
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EC 135 Technical Data
Payload/Range with two PW206B2 engines
135.02.101.01.E
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EC 135 Technical Data
Payload/Range with two ARRIUS 2B2 engines
135.02.101.01.E
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EC 135 Technical Data
Intentionally left blank
135.02.101.01.E
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