ECUREUIL AS 355 N Contents Manufacturers notice Attention !

Transcription

ECUREUIL AS 355 N
Technical Data
Contents
1 - General characteristics ........................................................................... 4
2 - Standard Aircraft Definition ..................................................................... 9
3 - Optional equipment ................................................................................ 11
4 - Radio communication and radio-navigation equipment ....................... 15
5 - Incompatibility between of optional equipment ...................................... 21
6 - Main performance .................................................................................... 25
7 - Customer Service Overview .................................................................... 45
Manufacturers notice
Attention !
Eurocopter’s policy is one of on-going product enhancement which means
that alterations in definition, pictures, weights, dimensions or performance
may be made at any time without notice being included in those documents
that have already been issued.
This document cannot thus be taken as an offer or serve as an appendix to a
contract without a prior check as to its validity and prior written agreement of
EUROCOPTER.
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.
355 N 02.101.02 E
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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. ã EUROCOPTER
ECUREUIL AS 355 N
Technical Data
Blank
355 N 02.101.02 E
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ECUREUIL AS 355 N
Technical Data
Foreword
The AS 355 N twin engine version of the ECUREUIL family is powered with 2
TURBOMECA ARRIUS 1A engines of 520 shp (388 kW) each. It benefits from the
FADEC system (Full Authority Digital Engine Control) which makes piloting easier and
safer. it is the most affordable twin-engine helicopter in the market.
Thanks to its two engines and its redundant systems, the AS 355 N is able to perform
missions such as flights over water, or hostile environments by day and night.
It is compliant with the JAR OPS 3 regulation requirements. More particularly, it is totally
suited for police and MEDEVAC operations over large cities, aerial work and offshore
support operations. It is fully IFR certified. It can also be equipped with a 3 axis
autopilot.
Thanks to its single engine flight performance, the AS 355 N is able to operate from
building rooftops, to work near power lines or to ensure safe harbour pilot
transportation.
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ECUREUIL AS 355 N
Technical Data
1- General Characteristics
Lay-Out
n
Passenger-transport
l
1 pilot + 5 passengers in standard version
l
1 pilot + 4 or 5 passengers in "comfort" version
l
1 pilot + 6 passengers in "high density" version
n Casualty-evacuation
l
1 pilot + 1 or 2 stretcher patients + 2 doctors
n Cargo carrying
l
1 pilot + 3 m³ (105.9 ft³) load in cabin
Weights
kg
lb
1,437
3,168
1,163
2,600
1,134
2,600
2,564
5,732
2,500
5,732
Note : Empty weight accuracy : within ± 2 %
n
n
n
n
n
Empty weight, standard aircraft
(including engine oil and unusable fuel)
Useful load
Maximum all-up weight
Maximum cargo-swing load
Maximum all-up weight in external load configuration
Power plant
2 TURBOMECA ARRIUS 1A turbine engines
Engine ratings
kW
388
358
340
296
Thermodynamic Power, in standard atmosphere, at sea level :
n
n
n
n
Maximum emergency power (OEI 2½min.)
Intermediate emergency power (OEI 30 min.)
Take-off power
Maximum continuous power
ch
528
487
462
402
shp
520
480
456
397
kg
577
375
lb
1,272
827
Usable Fuel capacities
n
n
litres
730
475
Standard fuel tanks
Auxiliary fuel tank (option)
US gal.
193
125
355 N 02.101.02 E
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ECUREUIL AS 355 N
Technical Data
Main dimensions
Dimensions with blades folded
355 N 02.101.02 E
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ECUREUIL AS 355 N
Technical Data
Configurations
Standard lay-out
"Customized"
lay-out
355 N 02.101.02 E
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ECUREUIL AS 355 N
Technical Data
Dimensions of compartments and accesses
Cabin main dimensions
CABIN
Surface
A
Volume
2.60 m²
27.98 ft²
3.000 m³
105.94 ft³
LH HOLD
Surface
Volume
0.43 m²
4.62 ft²
0.235 m³
8.29 ft³
RH HOLD
Surface
Volume
0.35 m²
3.76 ft²
0.200 m³
7.06 ft³
REAR HOLD
Surface
Volume
0.55 m²
5.92 ft²
0.496 m³
17.50 ft³
TOTAL HOLDS
Surface
Volume
1.33 m²
14.3 ft²
0.931 m³
32.85 ft³
Cabin floor
l Pilot's safety belt attachment and freight-tie-down rings
n Passenger safety belt or freight tie-down rings
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ECUREUIL AS 355 N
Technical Data
Other characteristics
TURBOMECA ARRIUS 1A turbine engines
n
520 shp (388 kW) maximum contingency power
n
Optimized engine ratings according to outside
operations conditions thanks to electronic
governing system (FADEC)
n
Modular design
n
Fully proven and reliable
n
Standard
systems
n
Single-pilot or two-pilot possible configurations
n
3 axis autopilot with flight director coupler
IFR cockpit lay-out (on option)
redundant
hydraulic
and
electrical
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ECUREUIL AS 355 N
Technical Data
2- AS 355 N ECUREUIL - Standard Aircraft Definition
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ECUREUIL AS 355 N
Technical Data
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ECUREUIL AS 355 N
Technical Data
3- Optional equipment
Note : value of the weight breakdown is given for information and shall not be considered as contractual.
CI : Complete Installation
CI
CI
FP : Fixed Parts
FP
FP
kg
lb
General items of equipment
05-011
Dual controls 1
4.7
10.4
05-021
05-030
05-035
05-041
05-050
Improved side-visibility in standard front doors
Tinted window for standard and optional configuration
Bulged window on copilot front or rear doors
Hourmeter
Pilot's windshield wiper 2
2.2
0.0
0.1
0.3
2.2
4.9
0.0
0.2
0.7
4.9
05-060
Copilot's windshield wiper 2
2.2
4.9
05-073
Cabin heating installation 2
05-080
05-103
05-121
05-130
05-139
2.1
4.6
2nd battery kit 3
19.2
42.3
Air conditioning system 4
55.0
121.3
Engines flushing device without removal of cowlings
Engines fire-extinguishing system
0.7
6.2
14.5
1.5
13.7
32.0
Extras for CAA certification, V.F.R. (in production kit) 5
05-140
Extras for CAA certification, I.F.R. single pilot and/or two-pilot
(in production kit) 6
33.5
73.9
05-151
05-167
Skid landing gear, raised type with 2 footsteps on either side
Long footstep on high skid landing gear on right side or left
side 7
10.6
4.5
23.4
9.9
05-168
Short footstep on high or low skid landing gear on right side or
left side 8
2.7
6.0
05-171
05-186
Skid wearing plates
Adaptation for night-time missions with NVG
1.4
On request
3.1
1
2
3
4
5
6
7
8
Optional equipment already included in the copilot IFR kit when this configuration is purchased.
Optional item of equipment already included in the single-pilot IFR instrument kit when this configuration is
purchased.
Recommended for start-up in cold weather.
Available : cycle + 2 months.
These extras cover in particular the following items of optional equipment :
l
Engine fire-extinguishing system
l
RH landing-light (swivelling in elevation) and LH landing-light (swivelling in elevation and azimuth).
These extras cover in particular the following items of optional equipment :
l
Engine fire-extinguishing system
l
RH landing-light (swivelling in elevation) and LH landing-light (swivelling in elevation and azimuth)
nd
nd
l
2 battery / 2 altimeter.
Requires the fitment of the optional "Skid landing gear", raised type. Incompatible with the skis SURFAIR.
Short footstep incompatible with emergency floatation gear + low landing gear.
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ECUREUIL AS 355 N
Technical Data
CI
CI
FP : Fixed Parts
FP
FP
kg
lb
9.9
21.8
General items of equipment (continued)
05-191
Wire strike protection system 1
05-201
05-210
05-300
05-352
05-910
Fuel tanks self-sealing protection
High visibility main rotor blades
Tail rotor arch
Protection and markings kit
Extra-charge for customized external paint - level 1 2
05-920
Extra-charge for customized external paint - level 2 3
4.0
05-930
Extra-charge for highly customized external paint 4
On request
21.0
0.1
3.8
On request
4.0
46.3
0.2
8.4
8.8
8.8
Instruments and flying aids
06-052
06-120
06-170
2.0
4.4
0.8
1.8
Being studied
Remaining fuel flowmeter
Turn and bank indicator
Moving Map GPS
Specific mission equipment
07-013
73.3
Emergency floatation gear
161.6
5.7
12.6
07-041
SURFAIR Skis 5
27.0
59.5
07-053
Sand prevention filters, dynamic type (sand and snow
prevention)
Re-inforced sand-erosion protection strip on main rotor blades
Re-inforced sand-erosion protection strip on tail rotor blades
Ferrying tank
26.4
58.2
0.2
0.1
27.7
0.4
0.2
61.1
0.3
0.7
17.7
39.0
4.5
9.9
3.1
6.8
07-060
07-061
07-071
07-102
07-110
1
2
3
4
5
6
7
8
Cargo swing with dynamometer (1 134 kg - 2,500 lb) 6
RH side external mirror 7 - 8
This optional item has to be fitted on the production line.
Paint scheme comprising a basic shade and 2 or 3 additional shades, with straight separation lines, apart from
standard paint schemes.
Paint scheme comprising a basic shade and up to 3 additional shades, with separation lines not straight or tangled
up, with graduated shades or complicated emblem or logo to be hand-painted.
Sophisticated paint scheme with numerous shades, complex graduated shades, or complicated emblem or logo.
Incompatible with the optional 05-167 "Long footstep on high skid landing gear".
Imply the fitting of : Skid landing gear, raised type.
Recommended for sling/swing work.
The optional 07-210 RH swivellable landing light is recommended for simultaneous use.
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ECUREUIL AS 355 N
Technical Data
CI
CI
FP : Fixed Parts
FP
FP
kg
lb
16.1
35.5
Specific mission equipment (continued)
07-120
Lower casualty carrying installation with stretcher
0.3
0.7
17.6
38.8
0.2
0.4
07-131
Upper casualty carrying installation with stretcher 1
07-143
EMS kit AAT 2
Refer to AAT
07-150
Left rear sliding door 3
3.6
7.9
07-160
Right rear sliding door 3
3.6
7.9
07-165
07-166
07-171
Sliding window, on rear LH sliding door
Sliding window, on rear RH sliding door
AIR EQUIPEMENT electrical hoist
(136 kg - 300 lb, 40 m – 131 ft cable) 4
1.0
1.0
40.1
2.2
2.2
88.4
2.6
5.7
BREEZE electrical hoist
(204 kg – 450 lb, 50 m – 164 ft cable) 4
54.0
119.0
3.3
7.3
-10.0
24.7
-22.0
54.5
2.7
6.0
07-175
07-180
07-195
Drip tub (sea rescue)
SPECTROLAB SX 16 search-light
07-196
Infra Red filter for SPECTROLAB SX 16 search-light 5
07-210
RH landing-light (swivelling in elevation) 6
3.1
6.8
07-220
07-235
LH landing-light (swivelling in elevation and azimuth)
3.4
On request
7.5
4.0
8.8
07-360
07-400
07-600
07-700
Integrated hailers 7
Rappelling installation (without rope) 8
Protective lower cowlings
Protection for floatation gear in case of hoisting operation
Nose mounted FLIR installation 9
To be defined
On request
On request
On request
8.5
07-740
FLIR installation fitted on side mounted support beam 9
On request
33.0
07-780
07-790
1
2
3
4
5
6
7
8
9
Cabin console for FLIR installation
Transmission system for FLIR installation
18.7
72.8
On request
On request
Incompatible with I.F.R. instrument panel. Compatibility with the VFR instrument panel to be checked according to
the radio communication / navigation configuration.
Air Ambulance Technology (AAT) is responsible for the conformity, performances and certification of the
ambulance installation on the helicopter.
Improved side-visibility in the corresponding front door included in the optional equipment.
Implies the fitting of the optional "Left rear sliding door" (07-150).
The filter is not remotely controlled retractable.
Optional items of equipment already included in the single-pilot IFR instrument kit when this configuration is
purchased.
Availability : cycle + 3 months.
Implies the fitting of rear sliding door on both sides.
This equipment can be submitted to export licence.
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ECUREUIL AS 355 N
Technical Data
CI
CI
FP : Fixed Parts
FP
FP
Interior cabin layout
09-011
3 places instead of 4 places transformation kit 1
5.3
11.7
09-021
Left side two-place front bench seat (pilot on right side) 2
3.9
8.6
09-031
09-041
09-050
09-070
09-072
"Comfort" lay-out
"Comfort" lay-out with sound proofing
"EXECUTIVE" lay-out
Alternate fabrics for seats
Leather upholstery for seats 3
09-075
Velvet carpeting 3
On request
09-077
09-081
Washable floor covering
Energy-absorbing front seats
On request
8.0
30.7
67.7
43.7
96.3
64.0
141.1
On request
On request
17.6
Ground handling and picketing
10-011
Folding of main rotor blades 4
1.0
2.2
10-020
Mooring kit (ground or ships) 5
2.1
4.6
10-030
1
2
3
4
5
Marine gripping system
1.3
2.9
1.2
2.6
Including mainly 4 arm-rests and a fifth harness.
The two-place front bench is incompatible with the IFR version.
Option available for the optionals 09-031 and 09-041 "Comfort" lay-out and "Comfort" lay-out with sound proofing.
For rough weather conditions. Ground tooling 32.2 kg – 71 lb.
Recommended for transport by land, air and sea (when not in a container).
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ECUREUIL AS 355 N
Technical Data
4- Radio-communication and radio-navigation equipment
The radio/com/nav. equipment weight figures included in this chapter are average values. As the installation of those
equipment may vary from one a/c to an other, the weight of a complete configuration with multiple items may not be the
simple sum of all individual weights.
A/ Minimal installations for day and night VFR operations
for general aviation (private use and aerial work) or for JAA commercial air transportation
Designation
Gyro-instruments type 1
Stand-by gyro horizon
Solution A
Equipment
Thales H321 EHM gyro-horizon
or
AIM 1100-28-LS gyro-horizon
+
AIM 205-1 BL gyro-directional
Thales H321 EHM
or
AIM 1100-28-LS
kg
lb
4.2
9.2
3.8
8.4
VHF/AM/VOR/LOC/GLIDE
Honeywell KX 165 1 + KI206
5.4
11.9
VHF/AM Pilot
Honeywell KY 196 A 1
3.6
7.9
GPS 2
Trimble TNL 2101 Approach +
3.1
6.8
Transponder
+
Altitude encoder
Honeywell KT 76 C (mode A+C) 3 - 4
+
Shadin 8800 T
2.6
+
1.0
5.7
+
2.2
Emergency locator transmitter
Kannad 121 AF-H 5
1.5
3.3
I.C.S. (1 control box)
NAT AA95 6 - 7
2.6
5.7
Weight supplement
1
2
3
4
5
6
7
27.8
61.3
(118-136.9 MHz).
Coupling of GPS with the HSI if Type 2 Gyro-instruments are installed.
Delivered with Europe map. Subscription to be made by the customer.
If mode S is necessary, use Honeywell KT 70 instead of the Honeywell KT 76 C.
Mandatory for VFR use in France.
2 frequencies : 121.5 MHz, 243 MHz. Compliant with ED 62 and TSO C91A.
Includes the passenger interphone function.
Implies the fitting of David Clark H 10-36 headsets.
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ECUREUIL AS 355 N
Technical Data
A/ Equipment that can be added
depending on the operational needs or the requirements of the authorities in certain countries
if not included in the above minimum items of equipment
Designation
For Solution A
Equipment
kg
lb
Gyro-instruments type 2
(instead of the type 1)
Thales H140 Gyro-horizon
+
Honeywell KCS 55 A gyro-compass system
with KI 525 A Horizontal Situation Indicator
2.5
+
5.7
5.5
+
12.6
R.M.I. with 2 crossed needles
Honeywell KI 229 1 - 2
1.6
3.5
Honeywell KX 165A + KI206 3 - 4
To be defined
VHF/VOR/LOC/GLIDE GPS
Garmin GNS 430 3 - 5
To be defined
VHF/FM maritime
NAT NPX 138 3 -6
2.5
5.5
VOR/LOC/GLIDE
Honeywell KN 53 7
2.8
6.2
A.D.F.
Honeywell KR 87 + KI 227 8
5.5
12.1
Marker
Honeywell KR 21
1.0
2.2
D.M.E.
(with 1 or 2 indicators)
Honeywell KN 63
3.3
7.3
Transponder
Garmin GTX327 (mode A + C) 3 - 9
Radio altimeter
Thales AHV 16
1
2
3
4
5
6
7
8
9
To be defined
5.0
11.0
Implies the fitting of Type 2 Gyro-instruments.
Implies the fitting of 10 VA AC generation system if 250 VA AC generation is not installed.
Availability to be checked.
Instead of Honeywell KX 165 + KI206.
Instead of VHF/AM Pilot Honeywell KY 196 A and GPS Trimble TNL 2101 Approach +.
(138-173.9 MHz)
With indicator Honeywell KI 204 or Honeywell KI 206 + converter Honeywell KN 72 if Honeywell KI 206 already
fitted or Honeywell KI 229 if already fitted.
Replaced by Honeywell KI 229 if installed.
Instead of transponder Honeywell KT 76 C (mode A + C).
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ECUREUIL AS 355 N
Technical Data
A/ Equipment that can be added (continued)
if not included in the above minimum items of equipment
Designation
For Solution A
Equipment
kg
lb
Kannad 406 AF-H 1 - 2
0.0
0.0
Three-axis autopilot
with failure passivation unit
SFIM 85 T 31 3
33.6
74.1
Flight director coupler
SFIM CDV 85 T3
4.9
10.8
Electrical generation
250 VA AC generation system 4
4.8
10.6
Electrical generation
10 VA AC generation system
1.2
2.6
I.C.S. (1 control box)
NAT AMS 43 TSO instead of NAT AA95 5 - 6
0.0
0.0
kg
lb
A/ Headsets and helmets
Designation
For Solution A
Equipment
Headsets
David Clark H 10-36
0.5
1.1
Headset electrical extension
-
0.2
0.4
Helmets
To be defined
1
2
3
4
5
6
To be defined
3 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.
Instead of ELT 2 frequencies.
Implies the mandatory fitting of the 250 VA AC generation system and Type 2 Gyro-instruments.
Mandatory for autopilot
Includes the passenger interphone function.
Implies the fitting of David Clark H 10-36 headsets.
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ECUREUIL AS 355 N
Technical Data
B/ Minimum items of equipment - single pilot IFR
Solution B
Equipment
Designation
kg
lb
29.7
65.4
n
Special IFR instrument panel
in place of the standard one
n
Second anemo-barometric circuit
n
Thales H 140 flight director gyro-horizon
n
with KI 525 A Horizontal situation indicator
Single pilot IFR
instrument and equipment kit
n
Thales H 140 stand-by gyro-horizon
n
Rate-of-climb indicator with setter
in place of the standard one
n
Honeywell KNI 582 R.M.I. with two needles
and twin switching
n
Pilot’s and copilot’s windshield wipers
n
Landing-light swivellable in elevation
(in place of the fixed RH one)
n
Cabin heating system
Pilot
Honeywell KX 165
5.4
11.9
Copilot
Honeywell KX 165
5.4
11.9
A.D.F.
Honeywell KR 87
5.5
12.1
Marker
Honeywell KR 21
1.0
2.2
Transponder
+
Altitude encoder
Honeywell KT 76 C (mode A+C) 1
+
Shadin 8800 T
2.6
+
1.0
5.7
+
2.2
Radio altimeter (1 indicator)
Thales AHV 16
5.0
11.0
Three-axis autopilot
with failure passivation unit
+
Flight director coupler
SFIM 85 T 31 2
+
SFIM CDV 85 T3
33.6
+
4.9
74.1
+
10.8
Electrical generations
1st and 2nd 250 VA AC generation systems 3
9.0
19.8
Kannad 121 AF-H 4
1.5
3.3
I.C.S. (2 control boxes)
Team TB 39
3.8
8.4
Passenger interphone
Team BA 1816
1.6
3.5
110.0
242.5
Weight supplement
1
2
3
4
If mode S is necessary, use Honeywell KT 70 instead of the Honeywell KT 76 C.
Implies the mandatory fitting of the 250 VA AC generation system.
Mandatory for autopilot
2 frequencies : 121.5 MHz, 243 MHz. Compliant with ED 62 and TSO C91A.
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ECUREUIL AS 355 N
Technical Data
B/ Additional equipment for two-pilot IFR
Solution B
Equipment
Designation
Additional instrument and
equipment kit for two-pilot IFR
kg
lb
18.9
41.7
n
n
n
n
n
n
Altimeter
Airspeed indicator
Rate-of-climb indicator
Rotor tachometer
Autopilot indicating panel
with KI 525 A Horizontal Situation indicator
n Thales H 140 gyro-horizon
n Dual controls
Weight supplement
B/ Equipment that can be added for single pilot or two-pilot IFR
Designation
For Solution B
Equipment
kg
lb
VHF/FM maritime
NAT NPX 138 1 - 2
2.5
5.5
VHF/AM Copilot
Honeywell KY 196 A 3
3.6
7.9
HF/SSB
Honeywell KHF 950
14.4
31.7
D.M.E. (with 1 or 2 indicators)
Honeywell KN 63
3.3
7.3
2nd indicator for Radio altimeter
2nd indicator for Thales AHV 16
0.9
2.0
Transponder
Honeywell KT 70 (mode S)
2.6
5.7
GPS 4
(interfaced with HSI pilot)
Trimble TNL 2101 Approach +
3.1
6.8
18.5
40.8
Weather radar
(color version)
Telephonics RDR 1400 E
or
Honeywell RDR 2000 5
Stormscope
BF Goodrich WX 1000 5
6.1
13.5
Kannad 406 AF-H 6 - 7
0.0
0.0
1
2
3
4
5
6
7
(138-173.9 MHz)
Availability to be checked.
Instead of VHF/AM/VOR/LOC/GLIDE copilot Honeywell KX 165. (118-136.9 MHz).
Coupling of GPS with the HSI if Type 2 Gyro-instruments are installed.
Delivered with Europe map. Subscription to be made by the customer.
Availability : cycle + 2 months.
3 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.
Instead of ELT 2 frequencies.
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ECUREUIL AS 355 N
Technical Data
B/ Headsets and helmets
For Solution B
Equipment
kg
lb
Headsets
Silec 4449-1
0.5
1.1
Headset electrical extension
-
0.2
0.4
Helmets
To be defined
Designation
To be defined
355 N 02.101.02 E
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ECUREUIL AS 355 N
Technical Data
5- Incompatibility between of optional equipment
n Impossibility of simultaneous fitment of the fixed parts of 2 items of equipment
▲ Total or partial incompatibility of simultaneous fitment of the removal parts of two items of equipment
l Possibility of simultaneous fitment on the same aircraft, but impossible to use simultaneously
Note:
This table indicates the compatibility restrictions existing between the installations. The consultation of EUROCOPTER is necessary for the definitive Equipment
Compatibility clearance of a configuration.
Reference
Optional
Nature of the incompatibility
Installation
■
▲
●
General items of equipment
05-011
Dual controls
07-120 07-131
07-143 09-021
05-021
Improved side-visibility in standard front doors
07-150 07-160
05-060
Copilot's windshield wiper
05-103
05-103
Air conditioning system
05-060
05-167
Long footstep on high skid landing gear,
on RH side or LH side
07-041
05-168
Short footstep on high or low skid landing gear,
on RH side or LH side
07-013 1
05-186
Adaptation for night time missions with NVG
Being studied
05-352
Protection and markings kit
07-120 07-131
07-143
Being studied
Being studied
07-180
Instruments and flying aids
06-120
Turn and bank indicator
Being studied
Being studied
Being studied
05-168 1
07-041
07-171 2
05-167
07-013
Specific mission equipment
07-013
Emergency floatation gear
07-041
SURFAIR skis
07-071
Ferrying tank
1
2
07-175 2
07-360
07-120
07-143
09-021
09-041
07-131
09-011
09-031
09-050
07-102 07-171
07-175
The short footstep is incompatible with emergency floatation gear + low landing gear.
Hoisting remains possible when the floats are folded.
355 N 02.101.02 E
21
ECUREUIL AS 355 N
Technical Data
Reference
Optional
Installation
■
▲
●
07-102
Cargo swing with dynamometer
(1134 kg - 2,500 lb)
07-195
07-071
07-131
07-171
07-360
07-120
Lower casualty-carrying installation
with stretcher
05-011 05-103
07-071 07-143
07-180 09-011
09-021
07-102 07-171
07-175
07-131
Upper casualty-carrying installation
with stretcher 1
05-011 05-103
07-071 07-143
07-180 09-011
09-021
07-102 07-171
07-175
07-143
EMS kit AAT
05-011
07-071
07-131
09-011
09-031
09-050
07-102 07-171
07-175
07-150
Left rear sliding door
05-021
07-160
Right rear sliding door
05-021
07-171
AIR EQUIPEMENT electrical hoist
(136 kg - 300 lb, 40 m - 131 ft cable)
07-175 2
07-013 3
07-071 07-102
07-120 07-131
07-143 07-360
09-011 09-021
07-175
BREEZE electrical hoist
(204 kg - 450 lb, 50 m - 164 ft cable)
07-171 2
07-013 3
07-071 07-102
07-120 07-131
07-143 07-360
09-011 09-021
07-180
Drip tub (sea rescue)
07-120 07-131
07-143 09-011
09-031 09-041
09-050
07-195
SPECTROLAB SX 16 searchlight
07-102
07-235
Integrated hailers
07-360
Rappelling installation 4
1
2
3
4
Being studied
05-103
07-120
07-180
09-021
09-041
Being studied
07-120
07-143
07-175
09-021
05-352
Being studied
07-013 07-102
07-171 07-175
Incompatible with I.F.R. instrument panel. Compatibility with the VFR instrument panel to be checked according to
the radio communication / navigation configuration.
Only the structural supplies for the 07-175 BREEZE electrical hoist are compatible with the 07-170 AIR
EQUIPMENT electrical hoist installation.
Hoisting remains possible when the floats are folded.
Implies the fitting of rear sliding door on both sides.
355 N 02.101.02 E
22
ECUREUIL AS 355 N
Technical Data
Reference
Optional
Installation
■
▲
●
07-700
Nose mounted FLIR installation
Being studied
Being studied
Being studied
07-740
FLIR installation fitted on side mounted support
beam
Being studied
Being studied
Being studied
07-780
Cabin console for FLIR installation
Being studied
Being studied
Being studied
07-790
Transmission system for FLIR installation
Being studied
Being studied
Being studied
Interior arrangement
09-011
3 places instead of 4 places transformation kit
07-071 07-120
07-131 07-143
07-180
07-171 07-175
09-021
Left side two-place front bench seat (pilot on RH
side)
05-011 07-071
07-120 07-131
07-143
07-102 07-171
07-175
09-031
"Comfort" lay-out
09-041 09-050
07-071 07-143
07-180
09-041
"Comfort" lay-out with sound-proofing
09-031 09-050
07-071 07-143
07-180
09-050
"Executive" lay-out
09-031 09-041
07-071 07-143
07-180
09-081
Energy-absorbing front seats
Being studied
Being studied
Being studied
355 N 02.101.02 E
23
ECUREUIL AS 355 N
Technical Data
Blank
355 N 02.101.02 E
24
ECUREUIL AS 355 N
Technical Data
6- Main performance
The following performance values and figures refer to an AS 355 N, equipped with a new 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.
Performance on 2 engines
n
Maximum speed, VNE
km/hr
kts
1,800
3,968
278
150
n
Fast cruise speed (at MCP)
km/hr
kts
250
135
244
132
237
128
230
124
222
120
n
Recommended cruise speed
km/hr
kts
244
132
237
128
231
124
223
120
215
116
n
Fuel consumption at recommended cruise
speed
kg/hr
Ib/h
183
403
183
403
183
403
183
403
183
403
n
Rate-of-climb at MCP
m/sec
ft/min
10.9
2,146
9.9
1,949
8.9
1,752
7.7
1,516
6.4
1,260
n
Hover ceiling IGE (at TOP, height 5 ft)
Gross Weight
n
kg
lb
2,000
4,409
278
150
2,200
4,850
278
150
2,400
5,291
278
150
2,600
5,732
278
150
l
ISA
m
ft
6,000
19,685
5,100
16,732
4,250
13,944
3,400
11,155
2,000
6,560
l
ISA + 20°C
m
ft
5,300
17,388
4,300
14,108
3,400
11,155
2,550
8,366
1,400
4,590
Hover ceiling OGE (at TOP)
l
ISA
m
ft
5,700
18,701
4,700
15,420
3,850
12,631
2,850
9,350
750
2,460
l
ISA + 20°C
m
ft
4,850
15,912
3,900
12,795
2,950
9,378
2,100
6,890
150
490
>6,096
>20,000
>6,096
>20,000
5,335
17,500
4,525
14,846
3,800
12,470
428
231
693
374
760
410
740
400
713
385
2h53
4h38
5h05
4h55
4h45
n
Service ceiling (1 m/s, 200 ft/min)
m
ft
n
Range
(without reserve, at recommended cruise
speed)
km
nm
n
Endurance
(without reserve, at 100 km/hr – 54kts)
hr : min
355 N 02.101.02 E
25
ECUREUIL AS 355 N
Technical Data
Performance on 1engine
kg
lb
Gross Weight
n
Rate of climb at intermediate contingency
power
n
m/sec
ft/min
1,800
3,968
7.0
1,378
2,000
4,409
6.1
1,201
2,200
4,850
4.9
965
2,400
5,291
3.8
748
2,600
5,732
2.6
500
Service ceiling (1 m/sec., 200 ft/min.)
l
ISA
m
ft
4,850
15,912
3,900
12,795
3,050
10,007
2,250
7,382
1,450
4,757
l
ISA + 20°C
m
ft
4,050
13,287
3,050
10,007
2,100
6,890
1,200
3,937
250
820
n
Maximum Temperature for CAT A take-off
from clear heliport, at SL
°C
>50
>50
>50
47.5
36
n
Maximum Temperature for CAT A take-off
from helipad, at SL
°C
>50
>50
49
38
-
Operating limitations
The helicopter is cleared to be operated within the following altitude and temperature limitations
(according to Flight Manual). For complementary information, refer to Flight Manual.
n
Maximum altitude :
6,096 m - 20,000 ft (PA)
n
Maximum temperature
ISA + 35°C limited to + 50°C
n
Minimum temperature
– 40°C
Abbreviations
AEO :
IGE :
ISA :
MCP :
OEI :
OGE :
All Engines Operative
In Ground Effect
International Standard Atmosphere
Maximum Continuous Power
One Engine Inoperative
Out of Ground Effect
PA :
SL :
TAS
TOP :
VNE :
Vz :
Pressure Altitude
Sea Level
True Air Speed
Take-Off Power
Never Exceed Speed
Rate-of-climb
Units
nm :
kts:
ft/min :
m/sec :
°C:
nautical miles
knots
feet/minute
meters per seconds
degrees Celsius
hr:min :
kg :
lb :
km :
hours:minutes
kilogramms
pounds
kilometers
355 N 02.101.02 E
26
ECUREUIL AS 355 N
Technical Data
Performance charts
The performance charts presented hereafter apply to an aircraft as per the standard definition.
n
Take-off weight in hover IGE, AEO
(height 5 ft, Maximum TOP, no wind)
Page 28
n
Take-off weight in hover OGE, AEO
(Maximum TOP, no wind)
Page 29
n
Take-off weight in hover IGE, OEI
(Maximum contingency power, no wind)
Page 30
n
Take-off weight in hover OGE, OEI
(Maximum contingency power, no wind)
Page 31
n
Take-off weight CAT A, clear heliport
(Intermediate contingency power)
Page 32
n
Take-off weight CAT A, helipad
(Maximum contingency power)
Page 33
n
Fast cruise speed
(ISA)
Page 34
n
Fast cruise speed
(ISA+ 20°C)
Page 35
n
(ISA)
Page 36
n
(ISA + 20°C)
Page 37
n
Rate of climb in oblique flight
(AEO, ISA, MCP)
Page 38
n
(AEO, ISA +20°C, MCP)
Page 39
n
(OEI, ISA, Intermediate contingency power)
Page 40
n
(OEI, ISA +20°C, Intermediate contingency power)
Page 41
n
Hourly fuel consumption at fast cruise speed
(ISA, ISA + 20°C, ISA +35°C)
Page 42
n
Hourly fuel consumption at recommended cruise speed
(ISA, ISA + 20°C, ISA +35°C)
Page 43
n
Payload/Range
(ISA, SL, recommended cruise speed, without reserve)
Page 44
355 N 02.101.02 E
27
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS IN HOVER IGE
on two engines at maximum TOP
(Height 5 ft)
(ft)
Pressure Altitude (m)
180
6000
190
0
0
5000
200
0
210
0
ISO-Weight (kg)
170
16
00
0
220
0
23
00
15000
240
0
4000
250
0
25
40
10000
26
00
3000
2000
5000
1000
0
10
5
-10
0
-20
+3
+2
-30
S td
S td
0
-40
Std
0
20
30
40
50
T (°C)
Note : Guaranteed performances as long as the engines meet the power check criteria, as defined in the Flight Manual.
355 N 02.101.02 E
28
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS IN HOVER OGE
on two engines
at maximum TOP
(ft)
6000
18
00
ISO-Weight (kg)
17
00
16
00
19
00
15
00
20
00
5000
15000
21
00
22
00
23
00
4000
24
10000
3000
25
25
2000
00
00
40
26
00
5000
1000
-30
-20
-10
0
10
20
30
35
d+
St
0
+2
Std
0
-40
d
St
0
40
50
T (°C)
355 N 02.101.02 E
29
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS IN HOVER IGE
on 1 engine
at maximum contingency power
(O.E.I. 2½ min)
(ft)
0
150
0
35
d+
St
15000
140
20
d+
St
5000
ISO-Weight (kg)
d
St
6000
160
0
4000
170
0
180
0
10000
190
0
3000
200
210
2000
1000
0
220
0
230
5000
0
0
23
50
24
00
24
50
0
0
-40
-30
-20
-10
0
10
20
30
40
50
T (°C)
355 N 02.101.02 E
30
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS IN HOVER OGE
on 1 engine
(O.E.I. 2½ min)
(ft)
35
d+
St
20
d+
St
5000
ISO-Weight (kg)
d
St
6000
140
0
15000
150
0
4000
10000
3000
2000
160
0
170
0
180
0
190
0
200
0
210
0
215
0
5000
220
0
1000
0
0
-40
-30
-20
-10
0
10
20
30
40
50
T (°C)
355 N 02.101.02 E
31
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS FROM A CLEAR HELIPORT (CAT. A)
at intermediate contingency power
(O.E.I. 30 min)
(ft)
ISO-Weight (kg)
2500
8000
25
2000
26
22
00
23
00
00
00
20
25
00
00
21
24
40
00
6000
1500
4000
1000
2000
500
0
10
20
30
+35
+20
-10
St d
St d
0
-20
Std
0
40
50
T (°C)
355 N 02.101.02 E
32
ECUREUIL AS 355 N
Technical Data
TAKE-OFF WEIGHTS FROM A HELIPAD (CAT. A)
(O.E.I. 2½ min)
(ft)
ISO-Weight (kg)
18
2500
8000
20
00
21
00
19
00
00
22
00
2000
6000
23
00
1500
24
00
4000
25
00
25
40
1000
26
00
2000
500
0
0
10
20
30
+35
Std
+20
Std
Std
0
40
50
T (°C)
Height / speed limit
355 N 02.101.02 E
33
ECUREUIL AS 355 N
Technical Data
FAST CRUISE SPEED
ISA
(ft)
ISO-Weight (kg)
6000
00
00
20
00
14
16
18
00
5000
22
00
15000
4000
24
00
10000
3000
25
40
26
00
2000
5000
1000
0
0
180
190
200
210
220
230
240
250
260
270
280
True airspeed (km/h)
105
115
125
135
145
(kt)
Note : Typical performance with clean standard aircraft.
355 N 02.101.02 E
34
ECUREUIL AS 355 N
Technical Data
FAST CRUISE SPEED
ISA + 20°C
(ft)
ISO-Weight (kg)
6000
14
16
00
00
18
00
5000
20
00
15000
4000
10000
3000
2000
22
00
24
00
25
4
26 0
00
5000
1000
0
0
180
200
220
240
260
280
True Airspeed (km/h)
105
115
125
135
145
(kt)
355 N 02.101.02 E
35
ECUREUIL AS 355 N
Technical Data
RECOMMENDED CRUISE SPEED
ISA
(ft)
ISO-Weight (kg)
6000
00
14
00
16
18
00
20
00
5000
22
00
15000
4000
10000
3000
24
00
25
40
26
00
2000
5000
1000
0
0
180
200
220
240
260
100
110
120
130
140
(kt)
355 N 02.101.02 E
36
ECUREUIL AS 355 N
Technical Data
RECOMMENDED CRUISE SPEED
ISA + 20°C
(ft)
ISO-Weight (kg)
6000
200
00
5000
14
16
00
18
00
0
15000
22
00
4000
24
10000
3000
00
25
40
26
00
2000
5000
1000
0
0
180
200
220
240
260
100
110
120
130
140
(kt)
355 N 02.101.02 E
37
ECUREUIL AS 355 N
Technical Data
RATE OF CLIMB IN OBLIQUE FLIGHT
on 2 engines at MCP
ISA
(ft)
6000
00
16
00
18
00
00
14
20
22
ISO-Weight (kg)
00
5000
24
0
15000
25
4
26 0
00
4000
10000
0
3000
2000
5000
1000
0
0
0
10
Vz (m/s)
0
500
1000
1500
2000
2500
(ft/mn)
355 N 02.101.02 E
38
ECUREUIL AS 355 N
Technical Data
on 2 engines at MCP
ISA + 20°C
(ft)
6000
16
00
00
14
20
00
18
00
ISO-Weight (kg)
5000
22
00
15000
4000
24
00
25
10000
4
26 0
00
3000
2000
5000
1000
0
0
0
10
Vz (m/s)
0
500
1000
1500
2000
2500
(ft/mn)
355 N 02.101.02 E
39
ECUREUIL AS 355 N
Technical Data
on 1 engine
at intermediate contingency power (O.E.I. 30 min)
ISA
(ft)
6000
14
00
16
00
18
5000
ISO-Weight (kg)
00
15000
20
00
4000
10000
22
0
3000
0
24
00
25
4
26 0
00
2000
5000
1000
0
0
0
2
4
6
8
10
Vz (m/s)
0
500
1000
1500
(ft/mn)
355 N 02.101.02 E
40
ECUREUIL AS 355 N
Technical Data
on 1 engine
at intermediate contingency power (O.E.I. 30 min)
ISA + 20°C
(ft)
ISO-Weight (kg)
6000
16
00
14
00
5000
15000
18
00
4000
20
00
10000
3000
22
00
2000
24
00
5000
25
4
26 0
00
1000
0
0
0
2
4
6
8
10
Vz (m/s)
0
500
1000
1500
(ft/mn)
355 N 02.101.02 E
41
ECUREUIL AS 355 N
Technical Data
HOURLY FUEL CONSUMPTION
at fast cruise speed
ISA, ISA + 20°C, ISA + 35°C
(ft)
ISO-(%)
6000
5000
15000
4000
0
+2
td
S
3000
S
10000
td
5
td
S
+3
2000
5000
1000
0
0
100
120
140
160
180
200
Hourly Fuel Consumption (kg/h)
Note : Typical consumption with clean standard aircraft and new engines.
355 N 02.101.02 E
42
ECUREUIL AS 355 N
Technical Data
HOURLY FUEL CONSUMPTION
at recommended cruise speed
ISA, ISA + 20°C, ISA + 35°C
(ft)
ISO-Atm (°C)
6000
5000
15000
4000
0
+2
td td
S
S
5
+3
td
S
10000
3000
2000
5000
1000
0
0
100
120
140
160
180
200
Hourly Fuel Consumption (kg/h)
Note : Typical consumption with clean standard aircraft and new engines.
355 N 02.101.02 E
43
ECUREUIL AS 355 N
Technical Data
PAYLOAD / RANGE
ISA
Empty weight equipped a/c + 1 pilot : 1,545 kg - 3,406 lb
(lb)
(kg)
1000
2000
800
15
24
m
1500
600
-5
0
0 00 f
m
t
-0
ft
1000
400
500
0
200
0
0
200
400
600
800
Range (km)
0
100
200
300
400
(nm)
Note : Typical mission without reserve, with clean aircraft and new engines.
355 N 02.101.02 E
44
ECUREUIL AS 355 N
Technical Data
7- Customer Service Overview
Maintenance and maintainability data
"Scheduled" and "unscheduled" maintenance are considered in labour figures given hereafter. 1
"On helicopter" maintenance
Scheduled maintenance
Before the first flight
n
Daily checks
In between flights
Pilot task
After the last flight
or 10 flight hours
n
Complementary
inspection
Every 100 flight hours
« S » inspection
2.1 hrs for 100 flight hours
0.021 MH/FH 2
n
Basic inspection
Every 500 flight hours
« T » inspection
or
every 24 months
« A » inspection
80.5 hrs for 500 flight hours
0.161 MH/FH
n
Calendar
inspection
every 12 years inspection 335 hrs for 7200 flight hours
0.046 MH/FH
Unscheduled maintenance
n
Repairs, removal, unusual
on-condition maintenance, …
Experience
shows
that
1,550 hrs are devoted to
inspections, unscheduled maintenance for
5000 flight hours
1,550 hrs for 5000 flight
hours
0.31 MH/FH
Average man hour between two calendar inspections
n
Assumptions :
2 hours 30 min Flight Hours per day in 2 flights
600 Flight Hours per year
0.310 hour of unscheduled maintenance per flying hour
2 engine cycles / hour operation.
l
l
l
l
n
1
2
Average maintenance man-hours per flying hour in above conditions :
l
0.539 hour
including calendar inspection
l
0.492 hour
without calendar inspection.
Data are given with hypothesis of 2001.
MH / FH : Man Hour per Flight Hour
355 N 02.101.02 E
45
ECUREUIL AS 355 N
Technical Data
Time Between Overhaul (TBO)
TBO of Major assemblies
n
FH
l
l
l
l
Main Gearbox (MGB)
Epicyclic reduction gear
Bevel gear
Oil pump
Combiner gearbox
3000
3000
3000
3000
l
l
l
Engine
Module 1 : Gearbox
Module 2 : Generator
Complete engine
2000
2000
2000
n
Tail Gearbox (TGB)
2700
n
Main servo-unit
3000
n
Tail servo-unit
3000
n
Main assemblies replacement times
The aircraft maintenance could be performed either in the workshop or in the field using a specially designed
portable crane.
Replacement Times
ASSEMBLIES
In the Workshop
Main blades (Qty : 3)
Main rotor head (MRH)
MRH + Mast
Mast (bare)
MGB
Engine (equipped)
TGB
Tail rotor
Tail drive shaft
MGB-engine coupling shaft
*
0 hr 18
1 hr 35
1 hr 50
3 hrs 30
3 hrs 30
1 hr 50
0 hr 30
0 hr 12
0 hr 18
1 hr 48
In the field
0 hr 25
1 hr 48
2 hrs 07
3 hrs 55
4 hrs 00
2 hr 30
0 hr 30
0 hr 12
0 hr 18
2 hr 00
Men
*
*
*
*
*
*
*
2
2
2
2
2
2
1
1
2
1
add crane installation/removal time = 0 hr 10
Note : The given times were obtained for replacements carried out during demonstrations with qualified personnel, and
adequate tools and means on the repair site.
The operator is advised to multiply these times by a coefficient of correction depending on personnel qualification,
work station preparation, available means.
355 N 02.101.02 E
46
ECUREUIL AS 355 N
Technical Data
Documentation
Following technical documents are supplied by default with newly purchased helicopters, associated with
corresponding subscriptions :
On paper :
l
l
l
l
Flight Manual (PMV)
Master servicing recommendation (PRE)
Service Bulletins (SBT), issued since last CD-ROM release
Equipment (“O” and “I” maintenance levels) (MCM)
On CD-ROM :
(Free unlimited update twice a year)
l
Operating
Master servicing recommendation (PRE)
t
l
Maintenance
Circuits and Schemas (MCS)
Description and operations (MDF)
Maintenance sheets (MET)
Fault isolation (MFI)
Storage (MST)
Repair (MRR)
Standard practices (MTC)
t
t
t
t
t
t
t
l
Identification
Spares parts (IPC)
Tools (ICO)
t
t
l
Specific
Service Bulletins (SBT)
Index of Modifications (SIM).
t
t
Note : The whole documentation on paper is available as an optional, on request.
355 N 02.101.02 E
47
ECUREUIL AS 355 N
Technical Data
Blank
355 N 02.101.02 E
48

ECUREUIL AS 355 N Contents Manufacturers notice Attention !

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