SHEPHARD
SHEPHARD
IN ASSOCIATION WITH
ROTORHUB MAGAZINE
PUBLIC SERVICE AVIATION handbook 2008-09
aircraft
specifications
emergency
medical service
law enforcement
Public Service
Aviation
handbook 2008-09
search and rescue
firefighting
A Shephard Press publication
coastguard &
border patrol
guide to operators
guide to suppliers
The concise global industry guide
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Sandy Doyle sd@shephard.co.uk
Editor
Peter Donaldson pd@shephard.co.uk
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The Shephard Public Service Aviation Handbook
is published annually by The Shephard Press Ltd.
©2008 The Shephard Press
Published July 2008
ISSN 1740-9284
Member of the Periodical Publishers
Association.
Production and DTP by Clear Impressions,
High Wycombe, Bucks, UK.
Printed by Williams Press, Berkshire, UK.
Public Service Aviation
handbook 2008-09
3Introduction
Modern public service aircraft are now reaching levels of sophistication not
found in their military counterparts just a few years ago. Peter Donaldson
assesses the industry and introduces this year’s handbook.
5 R
otary- and fixed-wing specifications
Basic data for aircraft currently in production or under development and
used for public service missions.
25 Emergency medical service
Featuring information on the types of air ambulance Interiors and
Interior-related equipment available.
39 Law enforcement
Brief descriptions of the broad range of equipment available to aid aerial
law enforcement, ordered by type, then by manufacturer.
65 S
earch and rescue
Examples of equipment specifically designed to aid SAR professionals
using helicopters or fixed-wing aircraft.
75 Firefighting
Products such as under-slung fire buckets, water and foam delivery and
refill systems are described, listed by manufacturer.
81 O
perators and activity guides
Companies providing air ambulance, law enforcement, firefighting,
coastguard and border patrol, and search and rescue flight capability.
Listed in country order. Quick-reference Activity Guide starts on page 133.
139 Suppliers and product guides
anufacturers and service companies providing the tools of the trade are
M
all listed here in alphabetical order. Track down which company provides
the product or service you’re after with the Product Guide on page 181.
SHEPHARD
The Shephard Press Ltd
268 Bath Road, Slough,
Berkshire, SL1 4DX, UK
Tel: +44 (0)1753 727001
Fax: +44 (0)1753 727002
COVER: One of two AgustaWestland AW139s used by the United Arab Emirates
Air Force for search and rescue gets ready to drop a rescue diver.
(photo: agustawestland)
Peter Donaldson « INTRODUCTION
WELCOME
W
AW 109 POWER
Your solution.
As a global leader in helicopters,AgustaWestland offers you complete solutions designed specifically for you and your mission. From vertical lift
support of military and police forces to corporate and offshore transport, to the demands of disaster relief, SAR and air medical operations.
AgustaWestland tailors solutions for you.
agustawestland.com
elcome to the
2008-09 edition
of the Shephard
Public Service Aviation
Handbook.
It is intended as a handy
reference source for the
industry serving those who fly aircraft on missions of
mercy, use them to uphold the law, rescue those in distress
or protect life and property from the ravages of fire.
Inside you will find outline descriptions of aircraft and
their capabilities plus more detailed entries on the role
equipment without which their missions would not be
possible. Aircraft, particularly helicopters, are necessarily
multi-purpose machines that have to be tailored to
customer’s mission needs through the careful integration
of communication, navigation and mission management
systems, sensors of many kinds including electro-optical
and infrared devices, rescue hoists, water, foam and
retardant dispensing systems, load hooks, stretchers, sealed
floors, power and gas supplies for medical equipment and
more in an almost bewildering array of choices. Long gone
are the days when a police helicopter, for example, could
perform its mission with only a pair of eyes and a radio in
the cockpit.
Most modern public service aircraft are reaching levels
of sophistication rarely found in their military counterparts
only a few years ago. This means that the integration of
role equipment is a demanding task that requires in depth
SHEPHARD
knowledge of both aircraft and mission systems on the
part of the manufacturer or third party contractor and
the building of deep trust and understanding between
them and the customer. In this handbook you will find
organisations with decades of experience in turning aircraft
into finely honed tools for tough, complex and risky jobs in
all weathers, day and night. You will also find people who
can act as independent consultants in a ‘customer’s friend’
role, helping to bridge the cultural divides between the
aviation industry and, for example, law enforcement
professionals and the officials who hold the purse strings.
One of the most important capabilities that
technological progress has provided is the ability to see at
night. Image intensifying night vision goggles are gradually
finding their way into public service aircraft, but progress is
slow. The evidence is by now so clear that NVG make flying
at night much safer simply because with them the pilot can
see when without them he or she could not. Operating
safely with NVG demands rigorous application of the right
procedures. Companies that can impart the right
knowledge and provide training and support of the highest
quality can also be found in these pages..
This is meant to be a thoroughly useful little book.
I hope you find it so.
Peter Donaldson, Editor
pd@shephard.co.uk
Public Service Aviation Portfolio
PUBLICATIONS
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ONLINE
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14 OCTOBER 2008
www.shephard.co.uk/events
5-6 NOVEMBER 2008
www.shephard.co.uk/police
30-31 MARCH 2009
www.shephard.co.uk/sar
contact
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Tel: +44 (0)1753 727001 Fax: +44 (0)1753 727002
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SHEPHARD
3
“San Diego depends on us.
And we depend on FlightSafety.”
AIRCRAFT
SPECIFICATIONS
EMERGENCY MEDICAL
EMS Helicopter Training
SERVICE
A SERIES
LAW ENFORCEMENT
SEARCH AND RESCUE
FIREFIGHTING
guide to OPERATORS
BATTALION CHIEF BRIAN FENNESSY
Director of Air Operations for the
San Diego Fire-Rescue Department
ACTIVITY GUIDE
The air operations division provides
multimission emergency services
GUIDE TO SUPPLIERS
including aerial firefighting, emergency
medical services transportation
PRODUCT GUIDE
and rescue on both land and water.
Helicopters and crews also assist
the Lifeguard Service and Coast Guard.
SPECIFICATIONS
W
hen a call comes in, Brian Fennessy
and his crews have to be ready. To
drop firefighters into the hottest, most
dangerous part of a forest fire. To join an
offshore search and rescue. To stabilize and
transport a critically injured accident victim.
Calm, rapid response is essential. There’s only
one way to develop the kind of edge required
when lives are at stake: effective, highly
specialized training. That’s why the San Diego
Fire-Rescue Department depends on FlightSafety.
For more information on industry-specific helicopter crew training,
please contact our West Palm Beach Sikorsky Learning Center at
561.515.2900 or our Fort Worth Bell Learning Center at 817.282.2557.
“Our safety, efficiency and effectiveness
have increased significantly as a result of
our training with FlightSafety International,”
Fennessy says.
EMS training at FlightSafety addresses
the specific challenges of emergency
response. It’s designed to pull emergency
crews together and to get them working
as one. Intense FlightSafety training
pushes helicopter crews to the limit.
Fennessy wouldn’t have it any other way.
ROTARY- & FIXED-WING
AIRCRAFT
The aircraft specifications listed here are intended to provide a handy, at-a-glance reference
source for the basic parameters that describe an aircraft’s capacity and performance.
Manufacturers and their agents can supply more information on request.
The maximum and cruise speeds and the Hover In Ground Effect (HIGE) and Hover Out of
Ground Effect (HOGE) figures assume International Standard Atmosphere (ISA) conditions at
maximum gross weight unless otherwise stated.
The maximum gross weight is the highest weight at which the aircraft is permitted to fly by
regulatory authorities. Engine ratings are for take-off power. The figures in Useful Load are
derived by subtracting the empty weight from the maximum gross weight, so allowance must
be made for fuel and crew in assessing the payload capacity.
This section provides a guide to helicopters and fixed-wing aircraft in production or under
development worldwide, with the emphasis on those aircraft most commonly used in public
service operations. Aircraft built by the original manufacturers only are included; licence-built
machines such as Agusta-built Bell designs, for example, are excluded to save space.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.
SPECIFICATIONS » Rotary-wing
Rotary-wing « SPECIFICATIONS
ROTARY-WING SPECIFICATIONS
MODEL
6
ROTOR
DIAMETER
end
mgw
bf
endurance
max gross weight
blades folded
rt
sc
sl
rotors turning
service ceiling
sea level
FUSELAGE
LENGTH
OVERALL
LENGTH
POWERPLANT
EMPTY
WEIGHT
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
CABIN
WIDTH
AgustaWestland 36 ft 1 in
A109 Power
(11 m)
37 ft 6.78 in
(11.45 m)
42 ft 9.18 in
(13.035 m) rt
2 x 640 shp (477 kW)
P&WC PW 206C or 670 shp
Turbomeca Arrius 2K1
3,461 lb
(1,570 kg)
6,284 lb
(2,850 kg)
2,822 lb
(1,280 kg)
6,9 ft
(2.1 m)
5 ft 3.38 in 4.2 ft
(1.61 m) (1.28 m)
AgustaWestland 36 ft 1 in
A109K2
(11 m)
37 ft 6.39 in
(11.44 m)
42 ft 9.18 in
(13.035 m) rt
2 x 737 shp (550 kW)
Turbomeca Arriel 1K1
3,660 lb
(1,650 kg)
6,284 lb
(2,850 kg)
2,645 lb
(1,200 kg)
6,9 ft
(2.1 m)
5 ft 2.6 in
(1.59m)
AgustaWestland 35 ft 6 in
A109S Grand
(10.83 m)
38 ft 3 in
(11.65 m)
42 ft 6 in
(12.96 m)
2 x 735 shp (548 kW) P&WC 3,649 lb
PW207C turboshafts
(1,655 kg)
7,000 lb
(3,175 kg)
3,351 lb
(1,520 kg)
AgustaWestland 36 ft 1 in
A119 Koala
(10,83 m)
36 ft 3.98 in
(11.074 m)
42 ft 9.18 in
(13.035 m) rt
1 x 1,002 shp (747 kW)
P&WC PT6B-37
3,086 lb
(1,400 kg)
5,732 lb
(2,600 kg)
AgustaWestland 45.28 ft
AW 139
(13.8 m)
44.4 ft
(13.53 m)
54.64 ft
(16.65 m) rt
2 x 1,679 shp (1,252 kW)
P&WC PT6C-67C
7,227 lb
(3,300 kg)
American
21 ft
Sportscopter Intl (6.4 m)
Ultrasport 254
17 ft 8 in
(5.38 m) bf
19 ft 2 in
(5.84 m)
1 x 55 hp (41 kW) Hirth
2703 two-stroke
American
21 ft
Sportscopter Intl (6.4 m)
Ultrasport 331
17 ft 8 in
(5.38 m) bf
19 ft 2 in
(5.84 m)
American
23 ft
Sportscopter Intl (7.01 m)
Ultrasport 496
17 ft 8 in
(5.38 m) bf
Bell 206 BIII
JetRanger
33 ft 5 in
(10.16 m)
Bell 206 L4
LongRanger
max fuel
standard fuel
reserves
nr
wxl
xc
no reserves
with external load
excluding cockpit
MAX
SEATS
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
8
180.21 ft3
(5.1 m3)
inc cockpit
16,600 ft
(5,060 m)
11,800 ft
(3,600 m)
156 kt
(289 kph)
137 kt
(254 kph)
521 nm
(965 km),
st, nr
4 ft 2.39 in 8
(1.28 m)
173 ft3
(4.9 m3)
inc cockpit
17,400 ft
(5,300 m)
12,800 ft
(3,900 m)
143 kt
(265 kph)
120 kt
(226 kph)
351 nm
(583 km),
st, nr
6 ft 3.5 in NA
(1.9 m)
4 ft 2 in
(1.48 m)
8
N/A
14,270 ft
(4,350 m)
9,350 ft
(2,850 m)
155 kt
(287 kph)
NA
470 nm
(870 km)
2,845 lb
(1,290 kg)
6.9 ft
(2.1 m)
5.5 ft
(1.59 m)
4 ft 2.39
in (1.28
m)
8
175 ft3
(4.9 m3)
inc cockpit
11,000 ft
(3,350 m)
8,800 ft
(2,680 m)
140 kt
(260 kph)
115 kt
(210 kph)
330 nm
(610 km),
st, nr
13,227 lb
(6,000 kg)
6,000 lb
(2,700 kg)
8.86 ft
(2.7 m)
6.56 ft (2
m)
4.66 ft
(1.42 m)
17
283 ft3
(8 m3) inc
cockpit
N/A
12,000 ft
(3,600 m)
N/A
N/A
400 nm
(750 km),
st, nr
252 lb
(115 kg)
525 lb
(239 kg)
273 lb
(124 kg)
52 in
(1.32 m)
30 in
(76.2 cm)
59 in
(1.5 m)
1
N/A
10,800 ft
(3,292 m)
7,000 ft
(2,134 m)
63 mph
(101 kph)
63 mph (105 N/A (1.25
kph) (FAA
hrs end)
restriction)
1 x 65 hp (48 kW) Hirth
706 two-stroke
330 lb
(150 kg)
650 lb
(295 kg)
320 lb
(145 kg)
52 in
(1.32 m)
30 in
(76.2 cm)
59 in
(1.5 m)
1
N/A (single 10,800 ft
seat)
(3,292 m)
7,000 ft
(2,134 m)
104 mph
(167 kph)
65 mph
(105 kph)
150 sm
(250 km)
2.5 hrs end
19 ft 9 in
(6.020 m)
1 x 95 hp (70.3 kW) Hirth
F30 two-stroke
495 lb
(225 kg)
1085 lb
(493 kg)
590 lb
(268 kg)
53 in
48 in
(1.346 m) (1.22 m)
59 in
(1.5 m)
2
N/A
10,800 ft
(3,292 m)
7,000 ft
(2,134 m)
98 mph
(158 kph)
65 mph
(104.6 kph)
N/A (2.5
hrs end)
31 ft 2.4 in
(9.5 m)
38 ft 11.4 in
(11.82 m)
1 x 420 shp (313 kW) Allison
250-C20J turboshaft
1,678 lb
(761 kg)
3,200 lb
(1,451 kg)
1,522 lb
(690 kg)
7 ft
(2.13 m)
4 ft 2 in
(1.28 m)
4 ft 2.5 in 5
(1.28 m)
40 ft3
(1.13 m3)
12,800 ft
(3,900 m)
8,800 ft
(2,682 m)
114.5 kt
(212 kph)
114.5 kt
(212 kph)
365 nm
(676 km)
nr
37 ft
(11.28 m)
33 ft 2.4 in
(10.1 m)
42 ft 10.2 in
(13.02 m)
1 x 557 shp (415 kW) Allison
250-C30P turboshaft
2,307 lb
(1,046 kg)
4,450 lb
(2,018.5
kg)
2,143 lb
(972 kg)
9 ft
(2.74 m)
4 ft 2 in
(1.28 m)
4 ft 2.5 in 7
(1.28 m)
83 ft3
(2.35 m3)
10,000 ft
(3,048 m)
6,500 ft
(1,981 m)
110 kt
(204 kph)
110 kt
(204 kph)
321 nm
(594 km)
nr
Bell 210
48 ft (14.6
m)
41 ft 8.1 in
(12.7 m)
57 ft 3.25 in
(17.45 m)
1 x 1,800 Shp Honeywell T53-517B turboshaft
5,210 lb
(2,363 kg)
10,500 lb
(4,763 kg)
internal
5,034 lb
(2,284 kg)
internal
7 ft 8 in
(2.34 m)
8 ft (2.43
m)
4 ft 1 in
(1.24 m)
15
220 ft3
(6.23 m3)
15,012 ft
(4,576 m)
estimated
N/A
110 kt
(204 kph)
N/A
251 nm
(465 km)
Bell 212
48 ft
(14.6 m)
41 ft 8.1 in
(12.7 m)
57 ft 3.25 in
(17.45 m)
1 x 1,290 shp (961 kW)
P&WC PT6T 3P Twin Pac
6,176 lb
(2,801 kg)
11,200 lb
(5,080 kg)
5,024 lb
(2,279 kg)
7 ft 8 in
(2.34 m)
8 ft
(2.43 m)
4 ft 1 in
(1.24 m)
15
220 ft3
(6.23 m3)
4,750 ft
(1,448 m)
8400 ft
111 kt
(2,560 m) @ (206 kph)
10,000 lb
104 kt
(193 kph)
224 nm
(415 km)
nr
Bell 407
35 ft
(10.7 m)
33 ft 2.4 in
(10.1 m)
41.8 ft
(12.7 m)
1 x 791 shp (589 kW) Allison
250-C47 turboshaft
2,598 lb
(1,178 kg)
5,000 lb
(2,267 kg)
2,402 lb
(1,090 kg)
9 ft
(2.74 m)
4 ft 9 in
4 ft 2.5 in 7
(1.738 m) (1.28 m)
83 ft3
(2.35 m3)
12,200 ft
(3,719 m)
10,400 ft
(3,170 m)
128 kt
(237 kph)
115 kt
(213 kph)
312 nm
(578 km)
Bell 412 HP
46 ft
(14 m)
46 ft (14 m) 56 ft 2 in
(17.1 m)
1 x 1,800 shp (1,341 kW)
P&WC PT6T 3P Twin Pac
6,789 lb
(3,079 kg)
11,900 lb
(5,398 kg)
5,111 lb
(2,318 kg)
7 ft 8 in
(2.34 m)
8 ft
(2.43 m)
4 ft 1 in
(1.24 m)
15
220 ft3
(6.23 m3)
10,200 ft
(3,109 m)
5,200 ft
(1,585 m)
122 kt
(226 kph)
122 kt
(226 kph)
352 nm
(652 km)
Bell 427
37 ft (11.3
m)
37.9 ft
(11.55 m)
2 x 611 shp (452 kW) P&WC 3,485 lb
PW 206D turboshafts
(1,581 kg)
6,000 lb
(2,722 kg)
2,515 lb
(1,141 kg)
N/A
4 ft 11 in
(1.5 m)
N/A
8
N/A
16,200 ft
(4,938 m)
13,900 ft
(4,237 m)
136 kt
(252 kph)
126 kt
(233.5 kph)
353 nm
(654 km)
Public Service Aviation Handbook 2008-09
42.9 ft (13.06
m)
CABIN
HEIGHT
mf
sf
res
visit us at www.shephard.co.uk
SHEPHARD
7
SPECIFICATIONS » Rotary-wing
8
Rotary-wing « SPECIFICATIONS
MODEL
ROTOR
DIAMETER
FUSELAGE
LENGTH
OVERALL
LENGTH
POWERPLANT
EMPTY
WEIGHT
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
CABIN
WIDTH
CABIN
HEIGHT
MAX
SEATS
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
Bell 429i
42.3 ft
(12.9 m)
approx
39.9 ft
(12.17 m)
53.4 ft (16.28
m) rotors
turning, approx
2 x 710 shp (528 kW) Pratt
& Whitney Canada PW 207D
turboshafts
4,300 lb
(1,950 kg)
7,000 lb
(3,175 kg)
2,700 lb
(1,225 kg)
N/A
N/A
N/A
10
220 ft3
(6.23 m3)
12,000 ft
(3,658 m)
9,300 ft
(2,835 m)
142 kt
(264 kph)
N/A
350 nm
(648 km)
Bell 430
42 ft
(12.8 m)
44.1 ft
(13.4 m)
50.5 ft
(15.39 m)
2 x 770 shp (573 kW) Allison
250-C40 turboshafts
5,285 lb
(2,397 kg)
9,000 lb
(4,082 kg)
3,715 lb
(1,685 kg)
8 ft 6 in
(2.59 m)
4 ft 11 in
(1.5 m)
4 ft 9.6 in 9
(1.45 m)
158 ft3
(4.5 m3)
11,350 ft
(3,459 m)
8,750 ft
(2,667m)
135 kt
250 kph
128 kt (237
kph)
351 nm
(650 km)
Bell Agusta 609 26 ft (7.9
tilt rotor
m) each
60ft span
44 ft
(13.31 m)
44 ft
(13.31 m)
2 x 1,940 shp (1,447 kW)
P&WC PT6C-67A turboshafts
10,500 lb
(4,763 kg)
16,000 lb
(7,258 kg)
5,500 lb
(2,495 kg)
12.8 ft
(3.84 m)
(9 seats)
58.5 in
(1.48 m)
(2 seats)
56 in
(1.42 m)
9
9
25,000 ft
(7,620 m)
25,000 ft
(7,620 m)
275 kt
(509.63
kph)
250 kt
(464 kph)
750 nm
(1,390
km)
Brantly
23 ft 9 in
International Inc (7.24 m)
B2B
21 ft 1 in
(6.43 m)
28 ft
(8.53 m)
1 x 180 hp (133 kW) Textron 1,070 lb
Lycoming IVO 360 AIA fuel
(481 Kg)
injected piston engine
1,670 lb
(757 kg)
600 lb
(272 Kg)
6 ft (1.83 3 ft 11 in
m)
(1.19 m)
3 ft 3 in
(0.99 m)
2
98 ft3
(2.78 m3)
3,525 ft
(1,074 m)
N/A
78 kt (145 N/A (msl 87
kph) (75% kt, 161 kph
power)
@ SL)
174 nm
(322 km)
Dragon Fly 333 21.65 ft
(6.6 m)
18.3 ft
(5,561 m)
N/A
1 x 105 hp (78.2 kW) DF/
573 lb
F30A26AK 4-cyl 2-stroke piston (260 kg)
engine (modified Hirth)
1102 lb
(500 kg)
530 lb
(240 kg)
N/A (two
seats)
4 ft 1 in
(1.25 m)
N/A
2
N/A
6,730 ft
(2,051 m)
4,300 ft
(1,371 m)
80 kt (148 65 kt
kph) [VNE] (120.5 kph)
162 nm
(300 km)
[20 min r]
EH Industries
EH 101
61 ft
(18.6 m)
64 ft
(19.5 m)
74 ft 10 in
(22.8 m)
3 x 2,100 shp (1,554 kW) RR 19,048 lb
Turbomeca RTM 322 or 2,000 (8,640 kg)
shp (1,480 kW) GE CT7-6
32,188 lb
(14,600 kg)
13,140 lb
(5,960 kg)
21 ft 4 in
(6.5 m)
8 ft 2 in
(2.49 m)
6 ft 2 in
(1.88 m)
34
970 ft3
(27.5 m3)
8,000 ft
(2,438 m)
4,000 ft
(1,220 m)
150 kt
(278 kph)
140 kt (259
kph)
500 nm
(926 km)
Enstrom 480
32 ft
(9.8 m)
29 ft 10 in
(9.1 m)
37 ft 4.3 in
(11.39 m)
1 x 420 shp (313 kW) Allison
250-C20W turboshaft derated
to 269 shp continuous
2,850 lb
(1,293 kg)
1,175 lb
(533 kg)
7.3 ft
(2.2 m)
5.87 ft
(1.79 m)
4.25 ft
(1.3 m)
4
N/A
15,000 ft
(4,572 m)
12,000 ft
(3,719 m)
114 kt
(211 kph)
96 kt (177
kph)
369 nm
(684 km)
425 sm nr
Enstrom 480B
32 ft
(9.8 m)
29 ft 10 in
(9.1 m)
37 ft 4.3 in
(11.39 m)
1 x 420 shp Allison 250-C20W 769 kg
turboshaft derated to 305 shp
(227 kW) for t/o
1,361 kg
592 kg
7.3 ft
(2.2 m)
5.87 ft
(1.79 m)
4.25 ft
(1.3 m)
5
N/A
12,300 ft
(3,750 m)
5,400 ft
(1,645 m)
202 km/h NA
at MTOW
657 km at
3,000 ft, nr
Enstrom
F 280 FX
32 ft
(9.8 m)
28.7 ft
(8.7 m)
37 ft
(11.28 m)
1 x 225 hp (168 kW)
Lycoming HIO-360-F1AD
turbocharged piston engine
1,585 lb
(719 kg)
2,600 lb
(1,179 kg)
1,015 lb
(460 kg)
5.6 in
(1.7 m)
4 ft 11 in 4 ft (1.2
(1.498 m) m)
2
N/A
13,200 ft
8,700 ft
(4,023 m) (2,651 m)
@ 2,350 lb @ 2,350 lb
101 kt
(188 kph)
117 mph
93 kt
(172 kph)
107 mph
260 nm
(483 km)
300 sm nr
Enstrom F28F
Falcon
32 ft
(9.8 m)
28.1 ft
(8.6 m)
37 ft
(11.28 m)
1 x 225 hp (168 kW)
Lycoming HIO-360-F1AD
turbocharged piston engine
1,570 lb
(712 kg)
2,600 lb
(1,179 kg)
1,080 lb
(467 kg)
5.4 ft
(1.7 m)
5 ft 1 in
(1.55 m)
4 .2 ft
(1.3 m)
2
N/A
13,200 ft
8,700 ft
(4,023 m) (2,651 m)
@ 2,350 lb @ 2,350 lb
97 kt (180 89 kt
kph) 112 (165 kph)
mph
102 mph
240 nm
(423 km)
263 sm nr
Erickson
(Sikorsky) S64E/F Aircrane
72 ft
(21.95 m)
70 ft 3 in
(21.41 m)
88 ft 6 in
(26.97 m)
2 x 4,500 shp (3,356 kW)
19,234 lb
P&WC JTFD12-4A (S-64E) or (8,724 kg)
4,800 shp (3,579 kW)
JTFD12-5A (S-64-F) turboshafts
42,000 lb
(19,050 kg)
(S-64E)
47,000 lb
(21,319
kg) (S-64-F)
20,000 lb
(9,072 kg)
(S-64E
25,000 lb
(11,340 kg)
(S-64F)
Container N/A
pod or
firefighting
tank and
pump
system
N/A
3
N/A
10,600 ft
(3,230 m)
(S-64E)
6,900 ft
(2,103 m)
(S-64E)
104 kt
(193 kph)
N/A
230 sm
(370 km)
with 10%
reserve
Eurocopter AS
332 L1 Super
Puma
51.12 ft
(15.58 m)
53.44 ft
(16.29 m)
61.35 ft
(18.7 m)
2 x 1,820 shp (1,357 kW)
Turbomeca Makila 1A1
turboshafts
9,832 lb
(4,460 kg)
18,960 lb
(8,600 kg)
9,128 lb
(4,140 kg)
16.44 ft
(5.01 m)
at floor
5.9 ft (1.8 5.09 ft
m)
(1.55 m)
22
473.92 ft3 10,663 ft
(13.42 m3) (3,250 m)
7,546 ft
(2,300 m)
144 kt
(267 kph)
138 kt
(256 kph)
655 nm
(1,215
km)
Eurocopter AS
332 L2 Super
Puma 2
53.15 ft
(16.2 m)
55 ft
(16.79 m)
63.98 ft
(19.5 m)
2 x 1,845 shp (1,375.5 kW)
Turbomeca Makila 1A2
turboshafts
10,330 lb
(4,686 kg)
20,500 lb
(9,300 kg)
10,173 lb
(4,614 kg)
18.67 ft
(5.69 m)
at floor
5.91 ft
(1.8 m)
4.76 ft
(1.45 m)
27
547.38 ft3
(15.5 m3)
10,236 ft
(3,126 m)
6,430 ft
(1,960 m)
150 kt
(278 kph)
136 kt
(251 kph)
655 nm
(1,215
km)
Eurocopter AS
350 B2
35 ft 0.8 in
(10.69 m)
35.85 ft
(10.93 m)
42.45 ft
(12.94 m)
1 x 732 shp (546 kW)
Turbomeca Arriel 1D1
2,581 lb
(1,171 kg)
4,960 lb
(2,250 kg)
2,379 lb
(1,079 kg)
7.94 ft
(2.42 m)
at floor
5 ft 4.9
(1.65 m)
4.27 ft
(1.3 m)
7
105.94 ft3
(3 m3)
9,843 ft
(3,000 m)
7,546 ft
(2,300 m)
133 kt
(246 kph)
122 kt
(226 kph)
362 nm
(670 km)
Eurocopter AS
350 B3
35 ft 0.8 in
(10.69 m)
35.85 ft
(10.93 m)
42.45 ft
(12.94 m)
1 x 848 shp (632 kW)
Turbomeca Arriel 2B turboshaft
2,588 lb
(11,74 kg)
4,960 lb
(2,250 kg)
2,372 lb
(1,076 kg)
7.94 ft
(2.42 m)
at floor
5 ft 4.9
(1.65 m)
4.27 ft
(1.3 m)
7
105.94 ft3
(3 m3)
12,927 ft
(3,940 m)
11,549 ft
(3,520 m)
140 kt
(260 kph)
122 kt
(226 kph)
356 nm
(660 km)
Public Service Aviation Handbook 2008-09
1,675 lb
(760 kg)
visit us at www.shephard.co.uk
SHEPHARD
9
SPECIFICATIONS » Rotary-wing
10
Rotary-wing « SPECIFICATIONS
MODEL
ROTOR
DIAMETER
FUSELAGE
LENGTH
OVERALL
LENGTH
POWERPLANT
EMPTY
WEIGHT
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
CABIN
WIDTH
CABIN
HEIGHT
MAX
SEATS
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
Eurocopter AS
350 BA
35.07 ft
(10.69 m)
35.86 ft
(10.93 m)
42.45 ft
(12.94 m)
1 x 640 shp (477 kW)
Turbomeca Arriel 1B turboshaft
2,566 lb
(1,164 kg)
4,960 lb
(2,250
kg),wxl
2,064 lb
(936 kg)
7.94 ft
(2.42 m)
at floor
5.41 ft
(1.65 m)
4.27 ft
(1.3 m)
7
105.94 ft3
(3 m3)
9,154 ft
(2,790 m)
6,496 ft
(1,980 m)
126 kt
(234 kph)
123 kt
(228 kph)
394 nm
(730 km)
Eurocopter AS
355 F2
35.07 ft
(10.69 m)
35.86 ft
(10.93 m)
42.45 ft
(12.94 m)
2 x 420 shp (313 kW) Allison
250-C20F turboshafts
3,022 lb
(1,371 kg)
5,600 lb
(2,540 kg)
2,578 lb
(1,169 kg)
7.94 ft
(2.42 m)
5.41 ft
(1.65 m)
4.27 ft
(1.3 m)
7
105.94 ft3
(3 m3)
6,562 ft
(2,000 m)
4,921 ft
(1,500 m)
122 kt
(226 kph)
110 kt
(204 kph)
382 nm
(707 km)
Eurocopter AS
355 N
35.07 ft
(10.69 m)
35.86 ft
(10.93 m)
42.45 ft
(12.94 m)
2 x 456 shp (340 kW)
Turbomeca Arrius 1A
turboshafts
3,165 lb
(1,436 kg)
5,731 lb
(2,600
kg),wxl
2,567 lb
(1,164 kg )
7.94 ft
(2.42 m)
5.41 ft
(1.65 m)
4.27 ft
(1.3 m)
7
105.94 ft3
(3 m3)
6,726 ft
(2,050 m)
2,625 ft
(800 m)
121 kt
(224 kph)
116 kt
(215 kph)
386 nm
(715 km)
Eurocopter AS
365 N2
Dauphin
39.14 ft
(11.93 m)
38.16 ft
(11.63 m)
45.05 ft
(13.73m)
2 x 736 shp (550 kW)
Turbomeca Arriel 1C2
turboshafts
5,006 lb
(2,271 kg)
9,369 lb
(4,250 kg)
4,363 lb
(1,979 kg)
7.22 ft
6.30 ft
(2.2 m) at (1.92 m)
floor
4.59 ft
(1.4 m)
13
176.57 ft3
(5 m3)
6,562 ft
(2,000 m)
3,937 ft
(1,200 m)
150 kt
(277 kph)
137 kt
(254 kph)
465 nm
(861 km)
Eurocopter
AS 365 N3
Dauphin
39.14 ft
(11.93 m)
38.16 ft
(11.63 m)
45.05 ft
(13.73m)
2 x 851 shp (635 kW)
5,072 lb
Turbomeca Arriel 2C turboshafts (2,301 kg)
9,369 lb
(4,250 kg)
4,297 lb
(1,949 kg)
7.22 ft
6.30 ft
(2.2 m) at (1.92 m)
floor
4.59 ft
(1.4 m)
13
176.57 ft3
(5 m3)
6,234 ft
(1,900 m)
5,085 ft
(1,550 m)
150 kt
(277 kph)
146 kt
(271 kph)
442 nm
(819 km)
Eurocopter
BK 117 B2
36.09 ft
(11 m)
32.74 ft
(9.98 m)
42.65 ft
(13 m)
2 x 684 shp (510 kW)
AlliedSignal Lycoming LTS 101
750B turboshafts
3,869 lb
(1,755 kg)
7,385 lb
(3,350 kg)
3,516 lb
(1,595 kg)
9.91 ft
(3.02 m)
4.89 ft
(1.49 m)
4.20 ft
(1.28 m)
11
176.57 ft3
(5 m3)
5,413 ft
(1,650 m)
4,200 ft
(1,280 m)
133 kt
(247 kph)
125 kt
(231 kph)
292 nm
(540 km)
Eurocopter
BK 117 C1
36.09 ft
(11 m)
32.74 ft
(9.98 m)
42.65 ft
(13 m)
2 x 738 shp (550 kW)
Turbomeca Arriel 1E2
turboshafts
3,891 lb
(1,765 kg)
7,385 lb
(3,350 kg)
3,516 lb
(1,595 kg)
9.91 ft
(3.02 m)
4.89 ft
(1.49 m)
4.20 ft
(1.28 m)
11
176.57 ft3
(5 m3)
8,361 ft
(2,530 m)
4,856 ft
(1,460 m)
133 kt
(247 kph)
125 kt
(231 kph)
292 nm
(540 km)
Eurocopter
BO 105 CB
32.28 ft
(9.84 m)
28.08 ft
(8.56 m)
38.91 ft
(11.86 m)
2 x 420 shp (313 kW) Allison
250-C20B turboshafts
2,813 lb
(1,276 kg)
5,511 lb
(2,500 kg)
2,698 lb
(1,224 kg)
7.17 ft
(2.185
m)
4.27 ft
(1.3 m)
3.84 ft
(1.17 m)
6
73.1 ft3
(2.07 m3)
5,000 ft
(1,524 m)
1,500 ft
(457 m)
130 kt
(240 kph)
111 kt
(205 kph)
300 nm
(555 km)
Eurocopter BO 105 32.28 ft
CBS Super Five
(9.84 m)
28.9 ft
(8.81 m)
38.91 ft
(11.86 m)
2 x 420 shp (313 kW) Allison
250-C20B turboshafts
2,910 lb
(1,320 kg)
5,512 lb
(2500 kg)
2,564 lb
(1,163 kg)
7.99 ft
4.27 ft
(2.435 m) (1.3 m)
3.84 ft
(1.17 m)
6
88.29 ft3
(2.5 m3)
7,800 ft
(2,378 m)
5,397 ft
(1,645 m)
131 kt
(243 kph)
111 kt
(205 kph)
305 nm
(564 km)
Eurocopter
BO 105 LS A-3
32.28 ft
(9.84 m)
28.9 ft
(8.81 m)
38.91 ft
(11.86 m)
2 x 500 shp (373 kW) Allison
250-C28B turboshafts
2,910 lb
(1,320 kg)
5,732 lb
(2,600 kg)
3,248 lb
(1,280 kg)
7.99 ft
(2.435
m)
4.27 ft
(1.3 m)
3.84 ft
(1.17 m)
6
88.33 ft3
(2.5 m3)
11,483 ft
(3,500 m)
8,366 ft
(2,550 m)
129 kt
(239 kph)
111 kt
(205 kph)
278 nm
(515 km)
Eurocopter
EC 120 B
32.81 ft
(10 m)
31.5 ft
(9.6 m)
37.86 ft
(11.52 m)
1 x 504 shp (376 kW)
1,929 lb
Turbomeca Arrius 2F turboshaft (875 kg)
3,750 lb
(1,700 kg)
1,655 lb
(750 kg)
7.55 ft
(2.3 m)
4.43 ft
(1.35 m)
4.10 ft
(1.25 m)
5
N/A
10,499 ft
(3,200 m)
7,999 ft
(2,438 m)
124 kt
(230 kph)
110 kt
(204 kph)
395 nm
(732 km)
Eurocopter
EC 130
35.07 ft
(10.69 m)
35.03 ft
(10.68 m)
41.47 ft
(12.64 m)
1 x 847 shp (632 kW)
Turbomeca Arriel 2B1
turboshaft
2,998 lb
(1,360 kg)
5,291 lb
(2,400 kg)
2,293 lb
(1,040 kg)
7.185 ft
(2.19 m)
6.12 ft
3.85 ft
8
(1.865 m) (1.175 m)
130.7 ft3
(3.7 m3)
10,720 ft
(3,265 ft)
8,740 ft
(2,660 m)
127 kt
(235 kph)
NA
358 nm
(662 km)
to dry tanks
Eurocopter
EC 135 P1
33.46 ft
(10.2 m)
33.33 ft
(10.16 m)
39.7 ft
(12.1 m)
2 x 621shp (463 kW) P&WC
PW 206Bs
3,174 lb
(1,440 kg)
6,000 lb
(2,720 kg)
2,734 lb
(1,240 kg)
10.04 ft
(3.06 m)
at floor
4.91ft
4.22 ft
8
(1.496 m) (1.285 m)
139.07 ft3 14,599 ft
(3.938 m3) (4,450 m)
11,401 ft
(3,600 m)
139 kt
(257 kph)
134 kt
(249 kph)
362 nm
(670 km)
Eurocopter
EC 135 T1
33.46 ft
(10.2 m)
33.33 ft
(10.16 m)
39.7 ft
(12.1 m)
2 x 732 shp (546 kW)
Turbomeca Arrius 2B1
3,148 lb
(1,428 kg)
6,000 lb
(2,720 kg)
2,767 lb
(1,255 kg)
10.04 ft
(3.06 m)
at floor
4.91 ft in 4.22 ft
(1.496 m) (1.285
m)
139.07 ft3 14,205 ft
(3.938 m3) (4,330 m)
12,139 ft
(3,475 m)
139 kt
(257 kph)
134 kt
(249 kph)
356 nm
(660 km)
Eurocopter EC
145
36,08 ft
(11 m)
33.43 ft
(10.19 m)
42.74 ft
(13.03 m)
2 x 750 shp (550 kW)
Turbomeca Arriel 1E2
turboshafts
1,742 kg
3,500 kg
1,728 kg
3.44 m,
excl
cockpit
1.57 m
max, 1.40
m in rear
1.27 m
12
max, 0.99
m in rear
5.85 m3
2,130 m
10,000 ft
(3,048 kg)
245 kph
243 kph
670 km
Eurocopter
EC 155
41.34 ft
(12.6 m)
41.76 ft
(12.73 m)
46.91 ft
(14.30 m)
2 x 851 shp (635 kW)
Turbomeca Arriel 2C1
turboshafts
N/A
10,582 lb
(4,800 kg)
4,887 lb
(2,217 kg)
incl fuel
8.2 ft
(2.5 m)
Four seats
5.18 ft
(1.58 m)
14
240 ft3
(6.8 m3)
N/A
N/A
143 kt
(266 kph)
136 kt
(252 kph)
450 nm
(831 km)
with st
Eurocopter
EC 225
53.14 ft
(16.2 m)
55 ft
(16.79 m)
63.98 ft
(19.5 m)
2 x 2,413 shp (1,800 kW)
Turbomeca Makila 1A4
turboshafts
N/A
22,930 lb
(10,400
kg) wil
11,870 lb
(5,380 kg)
wil
18.67 ft
(5.69 m)
at floor
5.91 ft
(1.8 m)
4.76 ft
(1.45 m)
27
547.38 ft3
(15.5 m3)
N/A
N/A
156 kts
N/A
783 nm
Public Service Aviation Handbook 2008-09
8
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SHEPHARD
11
SPECIFICATIONS » Rotary-wing
12
MODEL
ROTOR
DIAMETER
Euromil Mi-38
FUSELAGE
LENGTH
Rotary-wing « SPECIFICATIONS
OVERALL
LENGTH
POWERPLANT
EMPTY
WEIGHT
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
69 ft 2.75 in 65 ft 5.5 in
(21.1 m)
(19.95 m)
82 ft 8 in
(25.2 m) rt
2 x 2,500 shp (1,863 kW)
Klimov TVA-3000 or P&WC
PW-127 TS turboshafts
18,518 lb
(8400 kg)
34,392 lb
(15,600kg)
15,873 lb
(7,200 kg)
Groen Brothers
Aviation Hawk
5 Gyroplane
42 ft
(12.8 m)
24 ft
(7.32 m)
N/A
1 x 420 shp Rolls-Royce 250
C20S turboprop
1,840
lb(834 kg)
3,500 lb
(1,588 kg)
HAL Advanced
Light Helicopter
43 ft 3.7 in
(13.2 m)
42 ft 3 in
(12.89 m)
52 ft
(15.87 m)
2 x 1,000 shp (746 kW) Turbomeca 6,172.9 lb
TM-333 2B or 2 x 1,200 shp (895 (2,800 kg)
kW) LHTEC CTS 800 turboshafts
HAL CHEETAH
36.2 ft
(11.02 m)
33.62 ft
(10.236 m)
42.4 ft
(12.92 m)
1 x 870 shp (649 kW) HALbuilt Turbomeca Artouste IIIB
turboshaft
HAL CHETAK
36 ft 1.75 in 33 ft 4.5 in
(11.02 m) (10.17 m)
42 ft 1.5 in
(12.84 m)
1 x 870 shp (649 kW) HALbuilt Turbomeca Artouste IIIB
turboshaft
Kaman K-1200
K-MAX
48 ft 4 in
(14.68 m)
41 ft 9 in
(12.72 m)
Kamov Ka 126
42.65 ft
(13 m)
25.5 ft
(7.775 m)
Kamov Ka 226
42.65 ft
(13 m)
Kamov Ka 32
CABIN
HEIGHT
MAX
SEATS
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
35ft 1.25 7 ft 8 in
in(10.7m) (2.34 m)
6 ft
(1.85 m)
30
approx
1,041 ft3
(29.5 m3)
N/A
8,203 ft
(2,500 m)
148 kt
(275 kph)
135 kt
(250 kph)
701 nm
(1,300
km)
1,525 lb
(692 kg)
6.25 ft
(1.9 m)
Hawk 4
6.78 ft
(2.07 m)
5
N/A
Canot hover
Cannot hover 140 kt
(256 kph)
VNE
122 kt
(223 kph)
508 sm
(818 km)
nr
12,125.3 lb
(5,500 kg)
5,952.4 lb
(2,700 kg)
10 ft 11.9 6 ft 5.5 in 4 ft 8 in
in
(1.968 m) (1.42 m)
(3.35 m)
14
258.9 ft3
(7.33 m3)
9,850 ft
(3,000 m)
N/A
157 kt
(290 kph)
132 kt
(245 kph)
432 nm
(800 km)
(20 min r)
2,425 lb
(1,100 kg)
4,300 lb
(1,950 kg)
1,870 lb
(850 kg)
6.43 ft
(1.96 m)
4.36 ft
(1.33 m)
4.36 ft
(1.33 m)
5
109.7 ft3
16,565 ft
(5,050 m)
15,100 ft
(4,600 m)
113 kt
(209 kph)
103 kt (192
kph) at sl
302.3 nm
(560 km)
2,711 lb
(1,230 kg)
4,850 lb
(2,200 kg)
2,134 lb
(970 kg)
5 ft 11.64 6 ft 1.2 in
in (1.82 (1.86 m)
m)
4.36 ft
(1.33 m)
7
122.4 ft3
(3.47 m3)
9,350 ft
(2,850 m)
4,920 ft
(1,500 m)
113 kt
(209 kph)
100 kt (185
kph) at sl
270 nm
(500 km)
52 ft
(15.85 m)
1 x derated 1,800 shp (1,343 5,100 lb
kW) AlliedSignal Lycoming
(2,491 kg)
T53-17A-1
6,500 lb
(2,949 kg)
wxl
6,000 lb
(2,722 kg)
5 ft (1.52 3.17 ft
m)
(0.97 m)
4.17 ft
(1.27 m)
1
48.5 ft3
(1.37 m3)
29,120 ft
(8,876 m)
at mgw
26,300 ft
(8,016 m)
at mgw
100 kt
(185.2
kph)
85 kt
(157 kph)
270 nm
(500 km)
42.65 ft
(13m)
1 x 720 shp (530 kW) Mars
TV-O-100 turboshaft
4,222 lb
(1,915 kg)
7,165 lb
(3,250 kg)
2,943 lb
(1,335 kg)
6.69 ft
(2.04 m)
4.1 ft
(1.25 m)
4.5 ft
(1.40 m)
10
113 ft3
(3.2 m3)
3,182 ft
(970 m)
262 ft (80
m)
100 kt
(180 kph)
88.9 kt
(160 kph)
384.73 nm
(713 km)
sf
26.57 ft (8.1 42.65 ft
m)
(13m)
2 x 450 shp (331 kW) Allison
250-C20R1 turboshafts
4,303 lb
(1,952 kg)
7,496 lb
(3,400 kg)
3,190 lb
(1,448 kg)
7.71 ft
(2.35 m)
5.5 ft
(1.54 m)
4.52 ft
(1.40 m)
10
160.3 ft3
(4.54 m3)
10,330 ft
(3,150 m)
8,100 ft
(2,470 m)
118 kt
(214 kph)
108 kt
(194 kph)
341 nm
(620 km)
52 ft 2 in
(15.9 m)
37 ft 1 in
(11.22 m)
52 ft 2 in
(15.9 m) RT
2 x 2,200 shp (1,619 kW)
Klimov TV3-117VMA
turboshafts
14,990 lb
(6,800 kg)
24,250 lb
(11,000
kg)
11,000 lb
(5,000 kg)
on hook
14 ft 10
in (4.52
m)
4 ft 3 in
(1.3 m)
4 ft 4 in
(1.24 m)
18
257.8 ft3
(7.3 m3)
14,107 ft
(4,300 m)
12,140 ft
(3,700 m)
144 kt
(260 kph)
126 kt
(230 kph)
350 nm
(650 km)
sf, nr
Kamov Ka-62
44.3 ft
(13.5 m)
43.47 ft
(13.25 m)
51.84 ft
(15.80 m) RT
2 x 1,300 shp (970 kW)
RKBM Rybinsk RD-600
turboshafts
8,223 lb
(3,730 kg)
13,779 lb
(6,250 kg)
4,409 lb
(2,000 kg)
7.49 ft
(2.28 m)
5.83 ft
(1.78 m)
4.26 ft
(1.30 m)
18
264.85 ft3
(7.5 m3)
9,514 ft
(2,900 m)
6,890 ft
(2,100 m)
167 kt
(300 kph)
144 kt
(260 kph)
378 nm
(700 km)
sf, nr
Kazan Aktai
32 ft 9.75 in 27 ft 4.75 in
(10 m)
(8.35 m)
35 ft 8.25 in
(10.88 m)
1 x 240 hp (179 kW) RPD
VAZ 4265 rotary engine
1,334 lb
(605 kg)
2,535 lb
(1,150 kg)
1,201 lb
(535 kg)
3 ft 11.75 5 ft 7 in
in (1.2 m) (1.7 m)
N/A
3 or 4
N/A
7,550 ft
(2,300 m)
4,265 ft
(1,300 m)
103 kt
(190 kph)
84 kt
(155 kph)
324 nm
(600 km)
Kazan Ansat
37.75 ft
(11.5 m)
37.9 ft
(11.538 m)
45 ft
(13.77 m)
2 x Pratt & Whitney/Klimov
PK 206C turboshafts
N/A
7,275 lb
(3,300 kg)
3,637 lb
(1,650 kg)
N/A
N/A
N/A
9
N/A
N/A
5,900 ft
(1,800 m)
128 kt
(238 kph)
75.5 kt
(140 kph)
281 nm
(520 km)
MD Helicopters
MD 500E
26.4 ft
(8.05 m)
24.6 ft (7.49 30 ft 10 in
m)
(9.4 m)
1 x 420 shp (313 kW) Allison
250-C20B turboshaft
1,481 lb
(672 kg)
3,000 lb
(1,361 kg)
1,519 lb
(689 kg)
8 ft
(2.44 m)
4 ft 3.5 in
(1.31 m)
5 ft
(1.52 m)
5
N/A
8,500 ft
(2,590 m)
6,000 ft
(1,830 m)
134 kt
(248 kph)
129 kt
(239 kph)
264 nm
(488 km)
MD Helicopters
MD 520N
27.4 ft
(8.34 m)
25 ft 6 in
(7.8 m)
28 ft 6 in
(8.7 m)
1 x 450 shp (317 kW) Allison
250-C20R turboshaft
1,586 lb
(719 kg)
3,350 lb
(1,519 kg)
1,764 lb
(800 kg)
8 ft (
2.44 m)
4 ft 3.5 in
(1.31 m)
5 ft
(1.52 m)
5
N/A
9,300 ft
(2,835 m)
5,600 ft
(1,707 m)
124 kt
(230 kph)
N/A
201 nm
(389 km)
MD Helicopters
MD 530F
27.4 ft
(8.34 m)
24.6 ft (7.5
m)
32 ft 1 in
(9.78 m)
1 x 650 shp (484 kW) Allison
250-C30 turboshaft
1,509 lb
(684 kg)
3,100 lb
(1,406 kg)
1,591 lb
(722 kg)
8 ft
(2.44 m)
4 ft 3.5 in
(1.31 m)
5 ft
(1.52 m)
5
N/A
16,000 ft
(4,877 m)
14,400 ft
(4,389 m)
133 kt
(246 kph)
131 kt
(243 kph)
232 nm
(430 km)
MD Helicopters
MD 600N
27.5 ft
(8.4 m)
30.5 ft (9.3
m)
36.9 ft
(11.2 m)
1 x 808 shp (603 kW) Allison
250-C47 turboshaft
1,930 lb
(875 kg)
4,100 lb
(1,860 kg)
2,120 lb
(961 kg)
10.5 ft
(3.2 m)
4.6 ft
(1.4 m)
5 ft
(1.52 m)
8
40 ft3, 1.132 11,100 ft
m3 front, 96 ft3, (3,383 m)
2.716 m3 aft
6,000 ft
(1,828m)
136 kt
(252 kph)
125 kt
(231 kph)
380 nm
(704 km)
MD Helicopters
MD Explorer
33 ft 10 in
(10.32 m)
32.4 ft (9.9
m)
38 ft 3 in
(11.7 m)
2 x 710 shp (529 kW) P&WC 3,375 lb
PW 207E turboshafts
(1,531 kg)
6,500 lb
(2,948 kg)
3,125 lb
(1,599 kg)
6 ft 3 in
(1.91 m)
4 ft 9 in
(1.45 m)
4 ft 7 in
(1.4 m)
8
172.5 ft3
(4.89 m3)
12,200 ft
(3,719 m)
10,000 ft
(3,048 m)
135 kt
(250 kph)
123 kt
(158kph)
293 nm
(543 km)
Public Service Aviation Handbook 2008-09
CABIN
WIDTH
4.5 ft
(1.37 m)
Hawk 4
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SHEPHARD
13
SPECIFICATIONS » Rotary-wing
MODEL
14
ROTOR
DIAMETER
FUSELAGE
LENGTH
Rotary-wing « SPECIFICATIONS
OVERALL
LENGTH
POWERPLANT
Mil (Kazan)
69 ft 10.5 in 60 ft 5.75 in
Mi-17 / Mi-172 (21.29 m) (18.42 m)
83 ft 2 in
(25.35 m)
Mil (Ulan Ude)
Mi-171
69 ft 10.5 in 60 ft 5.75 in
(21.29 m) (18.42 m)
Mil Mi-26T
105 ft
(32 m)
Mil Mi-34C
32 ft 10 in
(10 m)
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
2 x 2000 shp (1470 kW)
15,653 lb
Klimov TV3 117MT turboshafts (7,100 kg)
28,660 lb
(13,000kg)
13,007 lb
(5,900 kg)
17.51 ft 7 ft 8.25 in 5 ft 10.25 24
(5.37 m ) (2.34 m) in (1.8 m)
812 ft3
(23m3)
7,213 ft
(2,200 m)
5,775 ft
(1,760 m)
134.9 kt
(250 kph)
130 kt
(240 kph)
318 nm
(590 km)
83 ft 2 in
(2.535 m)
2 x 2,070 shp (1,545 kW)
15,653 lb
Klimov TV3 117VM turboshafts (7,100 kg)
28,660 lb
(13,000kg)
13,007 lb
(5,900 kg)
20.85 ft
(6.36 m)
812 ft3
(23m3)
N/A
5,775 ft
(1,760 m)
113 kt
(210 kph)
N/A
307 nm
(570 km)
110 ft 8 in
(33.3 m)
131 ft 3.75 in
(40.03 m)
2 x 10,000 (7352 kW) ZMKB 63,134 lb
123,458 lb
Progress D-136 turboshafts
(28,600 kg) (56,000 kg)
60,486 lb
39 ft 4.25 10 ft 6 in
(27,400 kg) in (12 m) (3.2 m)
10 ft 4.25 85
in (3.17 m)
4,273 ft3
(121 m3)
8,852 ft
(2,700 m)
5,574 ft
(1,700 m)
159 kt
(295 kph)
137 kt
(255 kph)
383 nm
(710 km)
29 ft (8.85
m)
37.4 ft
(11.71 m)
1 x 325 hp (239 kW) M14
V26 radial piston engine
2,252 lb
(1,020 kg)
3,201 lb
(1,450 kg)
949 lb (430 2.1 ft (0.96 4 ft
kg)
m) xc
(1.23 m)
4.13 ft
(1.26 m)
4
53 ft3
(1.5m3)
N/A
2,950 ft
(900 m)
116 kt
(215 kph)
92 kt
(170 kph)
194 nm
(360 km)
Mil (Ulan Ude)
Mi-8T
69 ft 10.25 60.80 ft
in (21.29 m) (18.547 m)
82 ft 10 in
(25.24 m)
2 x 1500 shp (1103 kW)
Klimov TV2 117A turboshafts
15,382 lb
(6,968 kg)
26,455 lb
(12,000 kg)
11,108 lb
(5,032 kg)
17.51 ft
(5.37 m)
7 ft 8.25 in 5 ft 11 in
(2.34 m) (1.8 m)
30
812 ft3 (23 6,235 ft
(1,900 m)
m3)
2,625 ft
(800 m)
134.9 kt
(250 kph)
118.7 kt
(220 kph)
288.7 nm
(535 km)
Mitsubishi
MH2000A
24.4 m
12.2 m
14 m
2 x 876 shp Mitsubishi MG5110 turboshafts
2,500 kg
(5,510 lb)
4,500 kg
(9,920 lb)
2,000 kg
(4,410 lb)
2.1 m
2.0 m
1.4 m
10
5.8 m3
2,700 m
(8,860 ft)
@ MTOW
1,650 m
(5,400 ft)
@ MTOW
250 kph
(135 kt)
228 kph
(123 kt)
780 km
(420 nm)
MK Helicopter 30.57 ft
GmbH Light
(9.32 m)
Helicopter MkIII
25.8 ft
(7.863 m)
34 ft 9 in
(10.6 m)
1 x 230 ps SMA SR-305 jet
fuel piston engine
1,540 lb
(700 kg)
2,600 lb
(1,182 kg)
2,337 lb
(1,060 kg)
5.9 ft
(1.8 m)
4.26 ft
(1.3 m)
4.26 ft
(1.3 m)
2
N/A (two
seats )
14,763 ft
(4,500 m)
9,842 ft
(3,000 m)
108 kt
(200 kph)
97 kt (180
kph)
Approx 431
nm (800
km)
PZL Kania
47.8 ft
(14.56 m)
39.47 ft
(12.03 m)
57.07 ft
(17.4 m)
2 x 426 shp (313 kW) Allison
250-C20B turboshafts
4,320 lb
(1,960 kg)
7,826 lb
(3,550 kg)
3,505 lb
(1,590 kg)
13.35 ft
(4.07 m)
4.92 ft
(1.5 m)
4.95 ft
(1.51 m)
14
275.62 ft3
(7.8 m3)
8,202 ft
(2,500 m)
4,511 ft
(1,375 m)
113 kt
(210 kph)
103 kt (190
kph)
479 nm
(886 km)
PZL Mi-2
47.8 ft
(14.56 m)
39.2 ft
(11.94 m)
57.4 ft
(17.42 m)
2 x 425 shp (312 kW) GTD
350 turboshafts
5,313 lb
(2,410 kg)
7,826 lb
(3,550 kg)
2,513 lb
(1,140 kg)
7.44 ft
(2.27 m)
4.92 ft
(1.5 m)
4.6 ft
(1.4 m)
average
10
219 ft3
(6.2 m3)
5,167 ft
(1,575 m)
2,870 ft
(875 m)
105 kt
(190 kph)
99.5 kt (180 315 nm
kph)
(580 km)
PZL SW-4
29.5 ft
(9 m)
27 ft
(8.25 m)
29.7 ft
(9.07 m)
1 x 450 shp (336 kW) Allison
250-C20R /2 (SP) turboshaft
2,094 lb
(950 kg)
3,968 lb
(1,800 kg)
1,874 lb
(850 kg)
7.67 ft
(2.34 m)
4.92 ft
(1.5 m)
4.3 ft
(1.31 m)
5
109.5 ft3
(3.1 m3)
7,544 ft
(2,300 m)
5,412 ft
(1,650 m)
125.4 kt
(232 kph)
108.1 kt
(200 kph)
468.9 nm
(860 km)
PZL W-3A Sokol 51.5 ft
(15.7 m)
46.6 ft
(14.2 m)
61.65 ft
(18.79 m)
2 x 900 shp (662 kW) PZL 10W turboshafts
8,487 lb
(3,850 kg)
14,110 lb
(6,400 kg)
5,623 lb
(2,550 kg)
10 ft 6 in
(3.2 m)
5.08 ft
(1.55 m)
4 ft 8 in
(1.4 m)
14
247.35 ft3
(7m3)
9,906 ft
(3,020 m)
6,232 ft
(1,900 m)
127 kt
(235 kph)
120 kt (222
kph)
672 nm
(1,244 km)
Robinson R22
Beta II
25.2 ft
(7.67 m)
20.7 ft
(6.3 m)
28.7 ft
(8.76 m)
1 x 131 hp (94.3 kW) Textron 845 lb
Lycoming O-360-J2A piston eng (384 kg)
1,370 lb
(621 kg)
525 lb
(239 kg)
4.3 ft
(1.31 m)
3.6 ft
(1.1 m)
4 ft
(1.22 m)
2
N/A
9,400 ft
(2,865 m)
N/A
96 kt (177 83 kt (154
kph)
kph)
319 nm
(592 km)
Robinson R44
33 ft
(10.05 m)
29.7 ft
(9.07 m)
38.6 ft
(11.76 m)
1 x 225 hp (167 kW) Textron 1,424 lb
Lycoming O-540-F1B5 piston eng (645 kg)
2,400 lb
(1,089 kg)
976 lb
(443 kg)
6.9 ft
(2.09 m)
4.2 ft
(1.27 m)
4.3 ft
(1.31 m)
4
N/A
6,400 ft
(1,950 m)
5,100 ft @
2,200 lb
113 kt
(209 kph)
100 kt
(185.2 kph)
347 nm
(643 km)
Rotorway EXEC
162 F
25 ft
(7.62 m)
22 ft
(6.705 m)
N/A
1 x 150 hp (111 kW) 4-cyl,
162 in3 RI 162F four-stroke
1,500 lb
(680.4 kg)
525 lb
N/A (two
(238.14 kg) seats)
N/A (two
seats)
N/A (two
seats)
2
N/A (two
seats)
7,000 ft
(2,134 m)
5,000 ft
(1,524 m)
100 kt
(185 kph)
115 mph
95 mph
(152.9 kph)
180 sm
(289.67
km)
Schweizer
300C
26.8 ft
(8.2 m)
22.19 ft
(6.76 m)
30.8 ft
(9.39 m)
1 x 190 hp (141 kW)
1,100 lb
AlliedSignal Lycoming HIO-360- (499 kg)
D1A piston engine
2,050 lb
(930 kg)
950 lb
(431 kg)
4.1 ft
(1.25 m)
4.7 ft
(1.43 m)
4.2 ft
(1.28 m)
3
N/A
10,800 ft
(3,292 m)
at 1,700 lb
8,600 ft
(2,612 m)
at 1,700 lb
86 kt (159 64 kt (118
194 nm
kph)
kph) VNE is 95 (360 km)
kt (176 kph)
Schweizer
300CB
26.8 ft
(8.2 m)
22.19 ft
(6.76 m)
30.8 ft
(9.39 m)
1 x 180 hp (134 kW) AlliedSignal 1,088 lb
Lycoming HO-360-C1A piston eng (493.5 kg)
1,750 lb
(793.8 kg)
662 lb
(300.3 kg)
4.1 ft
(1.25 m)
4.7 ft
(1.43 m)
4.2 ft
(1.28 m)
3
N/A
7,000 ft
(2,133 m)
4,800 ft
(1,463 m)
Schweizer 333
27.51 ft
(8.39 m)
22.38 ft
(6.82 m)
31.17 ft
(9.51 m)
1 x derated 420 shp (313
kW) Allison 250-C20W
turboshaft
1,250 lb
(567 kg)
2,550 lb
(1,1257
kg)
1,300 lb
(590 kg)
6.5 ft
(1.98 m)
5.7 ft
(1.73 m)
4.4 ft
(1.34 m)
4
N/A
11,900 ft
(3,627 m)
at 2,300 lb
8,500 ft
(2,591 m)
at 2,300 lb
105 kt
(192 kph)
95 kt
(176 kph)
310 nm
(574 km)
Schweizer 434
27.51 ft
(8.39 m)
22.38 ft
(6.82 m)
31.17 ft
(9.51 m)
1 x 253 hp (186 kW)
Rolls-Royce 250-C20W engine
1,250 lb
(567 kg)
2,550 lb
(1,1257
kg)
3,200 lb
(1,454 kg)
6.5 ft
(1.98 m)
5.7 ft
(1.73 m)
4.4 ft
(1.34 m)
4
N/A
13,100 ft
12,500 ft
(3,993 m) (3,810 m)
at 2,300 lb)
105 kt
(192 kph)
95 kt
(176 kph)
310 nm
(574 km)
Public Service Aviation Handbook 2008-09
EMPTY
WEIGHT
975 lb
(442.2 kg)
CABIN
WIDTH
CABIN
HEIGHT
MAX
SEATS
7 ft 8.25 in 5 ft 10.25 24
(2.34 m) in (1.8 m)
85 kt (157 72 kt (133
kph) VNE 94 kt kph) at gw
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240 nm or
440 nm
SHEPHARD
15
SPECIFICATIONS » Rotary-wing
Rotary-wing « SPECIFICATIONS
MODEL
ROTOR
DIAMETER
FUSELAGE
LENGTH
OVERALL
LENGTH
POWERPLANT
Sikorsky
S-76B
44 ft
(13.41 m)
43 ft 4 in
(13.22 m)
52 ft 6 in
(16 m)
Sikorsky
S-76C+
44 ft
(13.41 m)
43 ft 4 in
(13.22 m)
Sikorsky
S-76C++
44 ft
(13.41 m)
Sikorsky
S-92
MAX T/O
WEIGHT
USEFUL
LOAD
CABIN
LENGTH
CABIN
WIDTH
CABIN
HEIGHT
MAX
SEATS
CABIN
VOLUME
HIGE
HOGE
MAX
CRUISE
ECONOMIC
CRUISE
RANGE
2 x 981 shp (731 kW) P&WC 8,620 lb
PT6B-36B turboshafts
(3,909 kg)
11,700 lb
(5,306 kg)
3,080 lb
(1,395 kg)
8 ft 1 in
(2.46 m)
6 ft 4 in
(1.93 m)
4 ft 5 in
(1.35 m)
14
204 ft3
(5.78 m3)
8,000 ft
(2,438 m)
3,750 ft
(1,143 m)
155 kt
(287 kph)
139 kt (257
kph)
350 nm
(649 km)
52 ft 6 in
(16 m)
2 x 856 shp (638 kW)
Turbomeca Arriel 2S1
turboshafts
8,138 lb
(3,691 kg)
11,700 lb
(5,306 kg)
3,562 lb
(1,616 kg)
8 ft 1 in
(2.46 m)
6 ft 4 in
(1.93 m)
4 ft 5 in
(1.35 m)
14
204 ft3
(5.78 m3)
5,650 ft
(1,722 m)
1,800 ft
(549 m)
155 kt
(287 kph)
140 kt (260
kph)
439 nm
(813 km)
43 ft 4 in
(13.22 m)
52 ft 6 in
(16 m)
2 x 923 shp (688 kW)
Turbomeca Arriel 2S2
turboshafts
7,005 lb
(3,177 kg)
in utlility con
11,700 lb
(5,306 kg)
4,695 lb
(2,129 kg)
in utility con
8 ft 1 in
(2.46 m)
6 ft 4 in
(1.93 m)
4 ft 5 in
(1.35 m)
14
204 ft3
(5.78 m3)
7,050 ft
(2,149 m)
@ take-off
3,300 ft
(1,006 m)
15 kt
(287 kph)
137 kt
(254 kph)
345 nm
(639 km)
30 min res
57 ft 5 in
(17.50 m)
68 ft 6 in
(20.67 m)
68 ft 6 in
(20.87 m)
including rotors
2 x 2,520 shp (1,879 kW)
General Electric CT7-8
turboshafts
15700 lb
(7,030 kg)
26,150 lb
wil, 28,300
lb wxl
N/A
20 ft 0 in
(6.10 m)
6 ft 7 in
(2.00 m)
6 ft (1.83 22
m)
10,700 ft
140 ft3
(3.96 m3) (3,261 m)
baggage area
6,370 ft
(1,942 m)
151 kt
(283 kph)
137 kt (254
kph)
538 nm
(997km)
(19 pax, nr
Tridair Gemini st 37 ft
(11.28 m)
33 ft 2.4 in
(10.1 m)
42 ft 10.2 in
(13.02 m)
2 x 450 shp (335 kW) Allison
250-C20R turboshafts
2,913 lb
(1,321 kg)
4,550 lb
(2,064 kg)
1,637 lb
(742 kg)
9 ft
(2.74 m)
4 ft 2 in
(1.28 m)
4 ft 2.5 in 7
(1.28 m)
7
10,000 ft
(3,048 m)
6,900 ft
(2,130 m)
106 kts
(196.3
kph)
106 kts
(196.3 kph)
260 nm
(482 km)
nr
Vertical Aviation 33 ft
Technologies
(10.05 m)
Hummingbird
30.5 ft
(9.296 m)
39.75 ft
(12.115 m)
1 x 260 hp (193.96 kW),
401 cu in (6,571 cc) V8 fourstroke piston engine
1,800 lb
(816.5 kg)
2,700 lb
(1,224.72
kg)
900 lb
9 ft 9in
(408.24 kg) (2.97 m)
5 ft (1.52
m)
5 ft (1.52 4
m)
N/A
N/A
N/A
(VNE 110
mph (177
kph)
90 mph
(144.8 kph)
400 sm
(643.72
km)
SHEPHARD
EMPTY
WEIGHT
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SHEPHARD
16
Public Service Aviation Handbook 2008-09
Ritz Carlton, Tysons Corner,
Washington, DC, USA
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SHEPHARD
17
SPECIFICATIONS » Fixed-wing
Fixed-wing « SPECIFICATIONS
FIXED-WING SPECIFICATIONS
Model
Overall
length
Height
Span
Powerplant
BAE Jetstream 31/32EP 14.36m
(47.12ft)
5.38m
(17.66ft)
15.85m (52ft)
Bombardier Dash 8-200
22.25m
(73.00ft)
7.49m
(24.58ft)
Bombardier
Challenger 604
20.85m
(68.42ft)
Bombardier Learjet 31A
Max take-off weight
Useful load
Cabin Length
CABIN Width
CABIN Height Max
seaTS
MAX CRUISE
ECONOMIC
CRUISE
RANGE
2x940shp Honeywell TPE331-10 (J31) 7,059kg (15,562lb) (J31);
2 x 1,020shp TPE331-12 (J32EP)
7,350kg (16,204lb) J32EP
1,860kg (J31);
2,042kg (J32EP)
7.39m (24.25ft )
1.85m (6.08ft)
1.80m (5.96ft)
19
255kt (J31);
265kt (J32EP)
N/A
324nm (J31 18 pax);
494nm (J32EP 19 pax)
25.91m
(85.00ft)
2 x 2,150shp Pratt & Whitney
PW123C/PW123D
16,465kg (36,300lb)
4,262kg
(9,396lb)
9.14m (30.00ft)
2.49m (8.16ft)
1.95m (6.42ft)
39 in
cabin
290kt
N/A
925nm
6.30m
(20.66ft)
19.61m
(64.33ft)
2 x 8,729lb General Electric CF34-3B
21,591kg (47,600lb)
2,436kg
(5,370lb)
8.66m (28.5ft)
2.49m (8.17ft)
1.85m (6.08ft)
19 in
cabin
470kt
425 kt
(787 kph)
3,769nm
14.8m
(48ft 8.4in)
3.75m
(12ft 3.6in)
13.4m (43ft
9.6in)
2 x 3,500lb AlliedSignal TFE731-2
7,711kg (17,000lb)
1042kg (2,297lb) 5.2m (17.08ft)
1.5m (4.92ft)
1.3m (4.42ft)
N/A
463kt
M0.73
1,448nm
Bombardier Learjet
35A/36A
14.83.
(48.75 ft)
3.73 m
(12.24 ft)
12.04 m
(39.5 ft)
2 x 3,500 lb Honeywell TFE731-2-2B
8,300 kg (18,300 lb)
1,534 kg
(3,381 lb)
35A 5.21 m
35A 1.5 m
35A 1.32 m
N/A
(17.08 ft), 36A
(4.92 ft), 36A
(4.33 ft), 36A
4.06 m (13.33 ft) 1.5 m (4.92 ft ) 1.32 m (4.33ft)
460 kt
N/A
35A 2,196 nm,
36A 2,522 nm
Britten Norman
Islander BN2T
35 ft 7.75 in
(10.97 m)
13 ft 8.75 in
(3.78 m)
49 ft (14.93
m)
2 x 420 shp (313 kW) Allison 2506,600 lb (3,175 kg)
B17C turboprops flat rated at 320 shp
(238.5 kW)
N/A
Incl baggage bay:
15 ft 2 in (4.63
m)
3 ft 7 in (1.09
m)
4 ft 2 in (1.27
m)
8 pax
2 crew
170 kt
(315 kph)
150 kt
(278 kph)
590 nm
(1093 km)
Britten Norman Defender 40 ft 4 in
4000 BN2T4S
(12.2 m)
14 ft 3 in
(4.3 m)
53 ft (16.15
m)
2 x Allison 250-B17F turboprops flat
rated at 400 shp (298 kW)
8,500 lb (3,855 kg)
3,600 lb
(1,632 kg)
Incl baggage bay:
17 ft 8 in (5.39
m)
3 ft 7 in (1.09
m)
4 ft 2 in (1.27
m)
12 pax
176 kt
(326 kph)
150 kt
(278 kph)
891 nm
(1595 km)
Cessna 172R/172S
Skyhawks
(172R) 26 ft 11
in (8.204 m)
(172R) 8 ft 11 (172R) 36 ft 1
in (2.718 m), in (11 m)
(172R) 1 x 160 hp Textron Lycoming
IO-360 L2A piston engine driving a
McCauley 2-bladed, fixed-pitch
propeller
(172R) 2,457 lb
(1,114.5 kg)
(172R) 857 lb
(389 kg)
(172R) 142 in
(3.61 m),
(172R) 39.5 in
(1 m),
(172R) 48 in
(1.22 m),
4
122 kts (226
kph)
104 kt
(192.7 kph)
687nm (1,272 km)
Cessna 182T/T182T
Skylanes
(182S) 29 ft
(8.8 m)
(182S) 9 ft 4
in (2.84 m)
(182S) 36 ft
(10.973 m)
(182S) 1 x 230 hp Textron Lycoming (182S) 3,110 lb
IO-540 AB1A5 piston engine
(1,410.7 kg)
(182S) 1,200 lb
(544 kg)
(182S) 134 in
(3.4 m)
(182S) 42 in
(1.07 m)
(182S) 48.5 in
(1.23 m)
4
145 kts (268
kph)
120.2 kt
(222.7 kph)
968nm (1,793 km)
Cessna 208-675/208B 41 ft 8 in
Grand Caravan
(12.7 m)
15 ft 5.5 in
(4.7 m)
52 ft 2 in
(15.9 m)
1 x 502 kW (675 shp) Pratt &
(208-675) 7,800 lb (3,538
Whitney Canada PT6A-114A turboprop kg), (208B) 8,500 lb
(3,856 kg)
4,500 lb
(2,041 kg)
16.7 ft (5.1 m)
5 ft 3 in (1.6 m) 4 ft 3 in
(1.2 m)
14
184 kt (341
km)
N/A
907 nm (1,679 km)
Cessna Citation CJ1
12.98m
(42.6ft)
4.20m
(13.8ft)
14.26m
(46.8ft)
2 x 1,900lb Williams/Rolls-Royce
FJ44-1A
4,853kg (10,600lb)
1,923kg
(4,240lb)
4.85m (15.9ft)
1.49m (4.9ft)
1.45m (4.8ft)
5 pax
380kt (704kph) 346 kt
(640 kph)
1,475nm (2,732km) with
full fuel
Cessna Citation CJ2
47 ft 8 in
(14.53 m)
13 ft 11 in
(4.24 m)
47 ft 8 in
(14.53 m)
2x 2,400 lbs (10.67 kN) WilliamsRolls FJ44-2C
12,375 lbs (5,613 kg)
1,600 lb (726 kg) 18 ft 8 in
(5.69 m)
4 ft 9 in
(1.45 m)
4 ft 9 in
(1.45 m)
8 pax
410 KTAS (759 N/A
km/hr), 33,000
ft, 10,300 lbs
N/A
Cessna Citation CJ3
51 ft 2 in
(15.61 m)
15 ft 2 in
(4.62 m)
52 ft 11 in
(16.13 m)
2 x 2,780 lbs Williams-Rolls FJ44-3A
13,870 lbs (6,291 kg)
1,950 lb (884 kg) 20 ft 10 in
(6.35 m)
4 ft 8 in (1.43
m)
4 ft 9 in (1.45
m)
10 pax
417 KTAS (772 367 KTAS @ 1,900 nautical miles
km/hr), 33,000 45,000 ft
(3,518 km) VFR with 45ft (10,058 m)
minute reserve
Cessna Citation Bravo
14.39m
(47.2ft)
4.57m (15.0ft) 15.90m
(52.2ft)
2 x 2,885lb Pratt & Whitney
PW530-A
6,712kg (14,800lb)
2,812kg
(6,200lb)
6.37m (20.9ft)
1.49m (4.9ft)
1.43m (4.7ft)
7 pax
402kt
359 KTAS @ 2,000nm
43,000 ft
Cessna Citation
Encore Ultra
14.90m (48.9ft)
4.57m (15ft)
2 x 3,360lb Pratt & Whitney
PW535-A
7,543kg (16,630lb)
6.89m (22.6ft)
1.49m (4.9ft)
1.43m (4.7ft)
8 pax
430kt
407 KTAS @ 1,970nm
45,000 ft
Cessna Citation Excel
15.78m (51.8ft) 5.24m (17.2ft) 17.1m (55.7ft) 2 x 3,804lb Pratt & Whitney
PW 545-A
9,072kg (20,000lb)
7.00m (23ft)
1.74m (5.57ft)
1.77m (5.67ft)
N/A
430kt
N/A
18
15.90m
(54.1ft)
Public Service Aviation Handbook 2008-09
N/A
visit us at www.shephard.co.uk
2,080nm
SHEPHARD
19
SPECIFICATIONS » Fixed-wing
Model
Overall
length
Height
Span
Cessna Citation X
22.1m (72.3ft)
5.8m (19.2ft)
Dassault Falcon 7X
76 ft 8 in
(23.19 m)
Dassault Falcon 10
Fixed-wing « SPECIFICATIONS
Max take-off weight
Useful load
Cabin Length
CABIN Width
CABIN Height Max
seaTS
MAX CRUISE
ECONOMIC
CRUISE
RANGE
19.4m (63.9ft) 2 x 6,400lb Rolls-Royce Allison
AE 3007C
16,375kg (36,100lb)
1362 lb with full
fuel
8.6m (28.3ft)
1.7m (5.57ft)
1.7m (5.57ft)
12 pax
M0.91
483 kt @
47,000 ft
3,390 nm
25 ft 6 in
(7.77 m)
82 ft 5 in
(25.13 m)
3 x P&WC PW 307A
69,000 lb (31,297 kg)
N/A
39 ft 1 in
(11.91 m)
7 ft 8 in
(2.34 m)
6 ft 2 in
(1.85 m)
19 pax
Mach 0.80
N/A
5,950 nm (11,026 km)
40 ft (12 m)
15 ft (4.5 m)
42 ft (12.8 m)
2 x 3,230 lb Honeywell TFE 731-2-1C 18,740 lb (8,518 kg)
turbofans
7,540 lb (3,427
kg)
16 ft (4.8 m)
4.9 ft (1.5 m)
4 ft (1.2 m)
7 in
cabin
470 kt
N/A
1,600 nm with 5 pax @M
0.78
Dassault Falcon 50EX
18.52m
(60.75ft)
6.98m
(22.92ft)
18.86m
(61.83ft)
3 x 3,700lb Honeywell TFE731-40
18,008kg (39,700lb)
1,710kg
(3,770lb)
7.16m (24.42ft)
1.86m (7.16ft)
1.80m (6.25ft)
19 in
cabin
370 kt
N/A
3,025nm/ 8 pax/ M.80
Dassault Falcon
900C/900EX
20.21m
(66.33ft)
7.55m
(24.75ft)
19.33m
(63.42ft)
3 x 4,750lb Honeywell TFE731-5B
(900C); 3 x 5,000lb Honeywell
TFE731-60 (900EX)
20,640kg (45,000lb)
(900C); 21,900 kg
(48,300lb) (900EX)
1,968kg (4,340lb) 10.11m
(900C); 2,796kg (33.17ft)
(6,165lb) (900EX)
2.34m (7.66ft)
1.88m (6.17ft)
19-22
370 kt
M0.75
4,000nm (900C)/5 pax/
M.75; 4,500nm
(900EX)/8 pax/LRC
Dassault Falcon 2000
20.21m
(66.33ft)
7.06m
(23.17ft)
19.33m
(63.42ft)
2 x 5,918lb CFM CFE738-1-1B
16,238kg (35,800lb)
3,270kg
(7,210lb)
7.98m (26.17ft)
2.34m (7.66ft)
1.88m (6.17ft)
14 in
cabin
370 kt
M0.8
3,000nm/ 8 pax/M.80
EADS PZL-104MA
Wilga 2000
28.28 ft
(8.62 m)
8.46 ft
(2.58 m)
37 ft
(11.28 m)
1 x 300 hp Textron Lycoming IO-540K1J5D or K1D5 or K1B5 six-cylinder
3,307 lb
(1,500 kg)
1184 lb
(537 kg)
N/A
N/A
N/A
4
223 kph
211 kph
1,500 km
Grob SPn
48 ft 7 in
(14.81 m)
16 ft 10 in
(5.12 m)
48 ft 9 in
(14.86 m)
2 x Williams FADEC controlled
turbofans
13,889 lb (6,300 kg)
N/A
16 ft 9 in
(5.10 m)
5 ft (152.4 cm)
5 ft 5 in
(164 cm)
8 pax
Mach 0.70
463 mph
(402 kt)
1,800 nm (3,334 km)
Piaggio P180
47.28ft
13.06ft
46.03ft
2 x 850 shp Pratt & Whitney PT6A-66 11,550lb
4,100lb (incl.
crew)
14.60ft
6.07ft
5.74ft
9 in
cabin
395kt (TAS)
N/A
1,750nm (@ 39,000ft)
Pilatus PC6/B2-H4
Turbo Porter
35 ft 11 in
(10.9 m)
10 ft 6 in
(3.2 m)
52 ft 1 in
(15.87 m)
1 x 410 kW (550 shp) Pratt &
Whitney Canada PT6A-27 turboprop
6,173 lb (2,800 kg)/
5,864 lb (2,660 kg)
N/A
4 ft 2.5 in (1.28 11
m)
125 KTAS
116 KTAS
500 nm
Raytheon Beech
King Air C90B
10.82 m
(35.60 ft)
4.36 m
(14.3 ft)
15.33 m (50.3
ft)
2 x 550 shp Pratt & Whitney Canada
PT6A-21
4,581 kg (10,100 lb)
1,429 kg
(3,150 lb)
3.94 m (12.7 ft)
1.37 m (4.6 ft)
1.45 m (4.9 ft)
6 incl
pilot
249 kt
196 kt
(363 kph)
1,390 nm (2,574 km)
Raytheon Beech
King Air B200
13.35 m
(43.9 ft)
4.61 m (15 ft)
16.61 m (54.6
ft)
2 x 850 shp Pratt & Whitney Canada
PT6A-42
5,670 kg (12,500 lb)
1,828 kg
(4,030 lb)
5,08 m (16.8 ft)
1.37 m (4.6 ft)
1.45 m (4.9 ft)
8 incl
pilot
249 kt (541
kph)
221 kt
(409 kph)
1,975 nm (3,660 km)
Raytheon Beech
King Air 350
14.23 m
(46.8 ft)
4.36 m
(14.4 ft)
17.65 m
(57.11 ft)
2 x 1,050 shp Pratt & Whitney
Canada PT6A-60A
6,804 kg (15,000 lb)
2,476 kg
(5,460 lb)
5.94 m (19.6 ft)
1.37 m (4.6 ft)
1.45 m (4.9 ft)
10 incl
pilot
315 kt
237 kt
(439 kph)
1,994 nm (3,693 km)
Raytheon Beechjet 400A 14.76m
(48.5 ft)
4.24 m
(13.11 ft)
13.26 m
(43.6 ft)
2 x 2,965 lb Pratt & Whitney Canada
JT15D-5 turbofans
7,303 kg (16,000 lb)
2,472 kg
(5,450 lb)
4.72 m (15.6 ft)
1.5 m (4.11 ft)
1.45 m (4.9 ft)
8 pax
468 kt (867
kph)
445 kt
(824 kph)
1,577 nm (2,920 km)
Raytheon Hawker
800XP
14.76 m
(48.5 ft)
4.24 m
(13.11 ft)
15.66 m
(51.4 ft)
2 x 4,660 lb Honeywell TFE 731-5BR
12,700 kg (28,000 lb)
5,375 kg
(11,850 lb)
6.49 m (21.4 ft)
1.83 m
(6.00 ft)
1.75 m (5.9 ft)
8+
466 kt (863
kph)
401 kt
(745 kph)
2,619 nm (4,850 km)
Raytheon Hawker
900XP
51 ft 2 in
(15.6 m)
18 ft 1 in
(5.5 m)
54 ft 43 in
(16.5 m)
2 x Honeywell TFE731-50BR
28,000 lb (12,701 kg)
N/A
21 ft 4 in (8.5 m) 6 ft (1.83 m)
5 ft 9 in
(1.75 m)
13 pax
514 mph
(448 kt)
463 mph
(402 kt)
2,642 nm (4,893 km)
Raytheon Hawker 4000 69 ft 9 in
(21.1 m)
19 ft 2 in
(6 m)
61 ft 9 in
(18.8 m)
2 x P&WC PW308A
37,500 lb (17,010 kg)
N/A
7.62 m
77.5 in
(1.97 m)
72 in (1.83 m)
12 pax
541 mph
(470 kt)
495 mph
(430 kph)
3,400 nm (6,300 km)
Reims Aviation F406
4.008 m
15.088 m
2 x 500 shp Pratt & Whitney Canada
PT6A-112
4,468 kg (9,850 lb)
2,219 kg
5.712 m
1.422 m
1.306 m
14
246 KCAS @
15,000 ft
202 KTAS @ 1,027 nm
20
11.893 m
Public Service Aviation Handbook 2008-09
Powerplant
(including cockpit): 3 ft 10 in (1.16
12 ft 1.7 in (3.7 m) m)
visit us at www.shephard.co.uk
SHEPHARD
21
SPECIFICATIONS » Firefighting & SAR amphibians
Firefighting & SAR amphibians « SPECIFICATIONS
FIREFIGHTING & SAR AMPHIBIANS
FIREFIGHTING & SAR AMPHIBIANS
Model
Overall
length
Height
Span
Powerplant
Max take-off weight
Useful load
Cabin Length
CABIN Width
CABIN Height Max
seaTS
MAX CRUISE
ECONOMIC
CRUISE
RANGE
Beriev Be-200
31.429 m
8.9 m
32.76 m
2 x 7,500 kgf Ivchenko/ProgressD436 TP turbofans
43,000 kg
12,000 kg water
18.7 m
2.5 m
1.895 m
61
710 kph
550 kph
1,700 km (7 tonnes
cargo)
Beriev Be-12P-200
26.51 m
9.1 m
29.84 m
2 x 5,180 shp Ivchenko Progress AI20D turboprops
36,000 kg
6,000 kg water
N/A
N/A
N/A
N/A
473 kph
N/A
1,500 km with 5,000 kg
load
Bombardier CL-415
19.82 m
8.98 m
28.6 m
2 x2,380 shp Pratt & Whitney Canada 19,890 kg
PW123AF turboprops
6,123 kg
9.38 m
2.39 m
1.9 m
11
375 kph
@10,000 ft
278 kph
2,427 km (ferry)
DEDICATED FIREFIGHTING CONVERSIONSDEDICATED FIREFIGHTING CONVERSIONS
Model
Overall
length
Height
Span
Powerplant
Air Tractor AT-802F
35.7 ft
12.75 ft
58 ft
1 x 1350 shp Pratt & Whitney Canada 16,000 lb
PT6A-67AG turboprop
17.7 m
1 x 1,000 hp Asz-62IRM18 radial aircooled piston engine
PZL M-18B Dromader
Max take-off weight
Useful load
4,200 kG or 5300 kG
(under CAM8)
Cabin Length
CABIN Width
CABIN Height
Max
seaTS
MAX CRUISE
ECONOMIC
CRUISE
RANGE
9,190 lb (820 gals N/A
water, 18 gals foam
N/A
N/’A
1
N/A
N/A
N/A
2,200 kg
N/A
N/A
1
N/A
N/A
Shephard Civil Helicopter 0707 v3 color Luminator.ai
170 to 200 1,000 km
11:42:18 AM
kph
6/11/2007
C
SHEPHARD
M
Y
HELICOPTER FIREFIGHTING
TECHNOLOGY AND TECHNIQUES
CM
MY
CY
Conference
CMY
14 October 2008
K
Hotel Quinta da Marinha, Estoril,
Nr Airport Cascais, Portugal
I D S
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22
Public Service Aviation Handbook 2007-08
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Information Display Systems
SHEPHARD
23
wave.ch
AIRCRAFT
SPECIFICATIONS
EMERGENCY MEDICAL
SERVICE
LAW ENFORCEMENT
SEARCH AND RESCUE
FIREFIGHTING
guide to OPERATORS
ACTIVITY GUIDE
GUIDE TO SUPPLIERS
Medical Interiors for Aircraft
and Helicopters
Tailor-made
Medical interiors that
fit your mission
PRODUCT GUIDE
EQUIPMENT
EMERGENCY MEDICAL
SERVICE
The equipment featured in this section is divided into:
Performance
Lightweight equipment and
excellent handling
Flexibility
Quick change capabilities for
different missions
aerolite
Turnkey solutions
From design to completion
Aerolite Max Bucher AG | Aumühlestr. 10 | 6373 Ennetbürgen | Switzerland | Phone +41 41 624 58 58 | www.aerolite.ch
Aerolite America LLC | 145 Mills Lane | Fort Mill | SC 29708 | USA | Phone +1 425 931 73 81 | www.aerolite.aero
±Air Ambulance interiors
±Interior-related equipment
Medical interiors generally represent the fixed infrastructure that
supports patient monitoring and intervention equipment but not such
equipment itself. This section is designed to present examples of
companies that can convert helicopters and aircraft to an air
ambulance configuration, or which supply major items of medical and
other equipment. As all interiors feature essentially the same
components, many of which are often available as separate items, we
have tried to show the breadth of capability of the companies, rather
than focus on particular products. Contact the companies concerned
for full details.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.
EMS VIEW » Tom Withington
EMS patient transfer « EMS VIEW
that they have been called to. Satellite technology not only
allows EMS operations to get aircraft location information
but can also be used for voice and text communications
between crews and their bases.
EXPANSION OF UK SERVICES
» The AgustaWestland A109 Power provides a good baseline airframe for specialist EMS conversions.
HIGH SPEED, LONG DISTANCE
PATIENT TRANSFER
By Tom Withington
As specialist health care provision moves increasingly to centres of national excellence, EMS
service providers in Europe and North America are being called upon to transport patients
from their local hospitals to these facilities.
E
urope is witnessing a drive to increase Emergency
Medical Services (EMS) safety with operators
widening their use of Night Vision Systems (NVS) for
air ambulance work and increasing their reliance on
advanced simulator technology to train EMS pilots. In
Europe, the concentration of specialist medical centres as
‘poles of excellence’ offering specific care such as cancer
treatment, is underpinning a general increase in EMS
aviation. Air ambulances are increasingly being called upon
to provide a rapid means by which seriously ill patients can
be moved to these specialist facilities, which may
sometimes be hundreds of miles from their local hospital.
26
Public Service Aviation Handbook 2008-09
This is increasing air ambulance flight hours, along with
training and safety demands on EMS crews.
EUROPEAN SATELLITE TECHNOLOGY
To cope with this demand, Europe-wide EMS operators
such as DRF (German Air Rescue) are expanding their
operations out of their homeland. DRF already has a fleet
of 50 aircraft and operates more than 40 bases across the
continent. Along with increasing the use of NVS, some
European operators are also looking at satellite tracking
systems to give service providers a precise view of where
their aircraft are located and their proximity to the incident
East Anglian Air Ambulance Services in the UK has
expanded its catchment area to cover Norfolk, Suffolk,
Cambridgeshire and Bedfordshire. EMS services have also
begun from East Midlands International Airport using an
AgustaWestland A-109 Power for air ambulance provision
across Derbyshire, Leicestershire and Rutland in the central
UK. The aircraft can reach the borders of its operating area
within 15 minutes flight time from its base near
Nottingham. The aircraft can perform night operations and
be configured to fly with either one or two stretchers.
Sloane Helicopters provides the service seven days a week.
Further south, Sussex Air Ambulance and the South
East Coast Ambulance Service National Health Service
trust have joined forces with Sussex Police to outfit the
helicopter operated by the latter with EMS equipment. The
use of the police helicopter, an MD-902 Explorer, for EMS
allows the provision of night time air ambulance services to
people living on the south coast of England.
Meanwhile in the Republic of Ireland, the country’s Air
Corps has been drafted by the government to provide EMS
nationwide. One of the key areas that the new scheme will
serve is the transfer of patients from one hospital to
another, as well as rapidly airlifting road accident patients
for medical treatment.
NORTH AMERICAN ORDERS
In North America, California Shock Trauma Air Rescue
(CALSTAR) has placed an order for four MD Helicopters
MD-902 aircraft to operate from its Lake Tahoe airport
base. The aircraft have been ordered as a replacement
for the previous Eurocopter BO-105 machines that
CALSTAR operated. The company has also placed an order
for the new Bell 429. Bell has used significant input from
the EMS community to maximise the 429’s suitability for
this role and the company is confident of healthy sales for
its new model.
The helicopter features a large cabin, side or rear
loading doors and also a cockpit layout which has drawn
appreciative comments from pilots. To this end, Air
Methods will receive an aircraft in June to begin the design
process for the helicopter’s dedicated medical interior. The
launch customer for Air Methods first EMS-configured Bell
429 is expected to be Mercy Hospital, IA, which will receive
its new aircraft in 2009.
Meanwhile, Med-Trans of Dallas, TX, has ordered eight
Eurocopter EC 135 aircraft for EMS operations, along with
» EMS helicopters are proving their worth for transfer of
chronically ill patients to specialist centres, as well as critical
patients who need fast transportation. (eurocopter)
options for further aircraft in the future. This is in addition
to the 11 Bell 407s that the company has on order.
Deliveries of the EC 135s are expected to span one
helicopter per quarter while the 407s will enter service
between 2009 and 2011.
The orders come at a time when Med-Trans is
significantly expanding its business, operating EMS
services across Arizona, California, Colorado, Kentucky,
North Dakota, South Dakota, South Carolina and
Tennessee; in addition to the services it operates in Texas.
Med-Trans Corporation has also announced that it has
added an extra Bell 407 to its fleet for EMS operations
around Texas and south-eastern New Mexico. MD
Helicopters reported delivering a single MD 902 Explorer to
Cox Air Care, a company that provides EMS services in
south-east Missouri and northern Arkansas.
MIDDLE AND FAR EAST TRANSPORT
Looking towards the Middle East, Russia’s Ulan Ude
company sold five Mi-17 helicopters to the Iranian Red
Crescent Society for EMS provision in 2007. Meanwhile,
Thailand’s first ever EMS service was inaugurated in the
same year, with Dusit Medical Services which operates four
large hospitals in the Bangkok area, contracting Siam Land
Flying and Bangkok Airways to provide patient transport
services. The company will use a Eurocopter EC 145 aircraft
for this new EMS service.
Finally, in South Africa, Netcare 911, an EMS provider
in the Eastern Cape region, revealed that it would begin
providing an air ambulance service from Port Elizabeth
from spring 2008 using a Eurocopter AS 350 for
emergency air transfer work. The company already has
significant experience providing these services in other
parts of South Africa where patients often have to be
transported over long distances to obtain medical care. ±
visit us at www.shephard.co.uk
SHEPHARD
27
EMS » Interiors
Interiors « EMS
EMS EQUIPMENT SPECIFICATIONS
INTERIORS
» AERO-MEDICAL PRODUCTS MFG INC
Aero-Medical Products Mfg, Inc has been manufacturing medical
interior equipment and supplying medical items for both
fixed-wing aircraft and rotorcraft since 1979. The company
has STC/PMA and EASA approvals for over 405 different makes
and models of business and commercial aircraft. and also
manufactures custom seats, divans and cabinets. » AEROLITE MAX BUCHER AG
MEDICAL INTERIOR FOR AGUSTAWESTLAND A109 GRAND
Advanced Life Support Interior: based on a modular concept
with various components for scene rescue, intensive care,
neonatal missions and search and rescue; features: single or
dual or neonatal patient configurations, up to four med crew
members, oxygen supply, power system with 12/14 VDC and 23
VAC, EASA STC EASA.R.S.01144
MEDICAL INTERIOR FOR AGUSTAWESTLAND AW 139
Basic Life Support Interior: designed for Medevac Missions
with quick change capabilities from utility to medical
configuration; features: one intensive care patient and two
slightly injured patients, up to six med crew seats, oxygen
supply of 4,000 litres (4x5lt / 200 bar), power systems with
12/14 VDC and 24/28 VDC supply and 230/115 VAC power, EASA
STC.R.S.01403 Advanced Life Support Interior: based on a
modular concept with various components for scene rescue,
intensive care, neonatal missions and search and rescue;
features: single or dual or neonatal patient configurations, up to
5 med crew seats, oxygen supply of 4,000 litres (4 x 5 lt/200
bar) and med air supply, rails/provisions for med devices and IV
bags, med storage cabinet, baggage net for loose equipment,
power system with 12/14 VDC and 24/28 VDC supply and 230/115
VAC power, EASA STC.R.S.01448 / EASA STC.R.S.01474
MEDICAL INTERIOR FOR EUROCOPTER EC 135
Basic Life Support Interior: designed for medevac missions
with quick change capabilities from utility to medical
configuration; features: single or dual patient configurations, up
to three med crew seats, oxygen supply 600 litres (1x3lt / 200
bar), stowage shell with equipment rails for med devices, EASA
STC R.S. 01406. Advanced Life Support Interior: based on a
modular concept with various components for scene rescue,
intensive care, neonatal missions and search and rescue;
features: single or dual or neonatal patient configurations, up to
three med crew seats, oxygen supply 1,800 litres (3x3lt / 200
bar) and med air supply, rails/provisions for med devices and IV
bags, med storage cabinet, tie down web for loose equipment,
power system with 12/14 VDC and 24/28 VDC supply and 230 /
115 VAC power, EASA STCR.S.01286
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Public Service Aviation Handbook 2008-09
MEDICAL INTERIOR FOR EUROCOPTER EC 145
Basic Life Support Interior: designed for medevac missions with
quick change capabilities from utility to medical configuration;
features: single or dual patient configurations, up to three med
crew seats, oxygen supply 1,200 litres (2x3lt / 200 bar), FOCA
Z29.20.75. Advanced Life Support Interior: based on a modular
concept with various components for scene rescue, intensive
care, neonatal missions and search and rescue; features: single or
dual patient configurations, up to three med crew seats, oxygen
supply 2,400 litres (4x3lt / 200 bar) or lox system and med air
supply, rails/provisions for med devices and IV bags, med storage
cabinet, tie down web for loose equipment, power system with
12/14 VDC and 24/28 VDC supply and 230 / 115 VAC power, EASA
(FOCA) STC Z25-20-96 / EASA.R.S.01241, FAA SR00006RD
MEDICAL INTERIOR FOR BELL 429
Advanced Life Support Interior: based on a modular concept
with various components for scene rescue, intensive care,
neonatal missions and search and rescue; features: single or
dual patient configurations, up to three med crew seats, oxygen
supply and med air supply, rails/provisions for med devices and
IV bags, med storage cabinet, tie down web for loose equipment,
power system with 12/14 VDC and 24/28 VDC supply and 230 or
110 VAC power, certification planned for 2009
MEDICAL INTERIOR FOR GATES LEAR JET 35A
Advanced Life Support Interior: designed for medevac
missions of one or two critically ill patients. Quick change
capability to switch from a medical to a corporate configuration;
features: single or dual patient configurations, up to four med
crew seats, power system with 12/14 VDC and 24/28 VDC and
230 VAC; EASA.IM.AS.01800
MEDICAL INTERIOR FOR BEECHCRAFT KING AIR 200
Advanced Life Support Interior: designed for medevac missions
of one or two critically ill patients; features: single or dual or
neonatal patient configurations, up to four med crew seats,
oxygen supply of 3,000 litres and med air, power system with 12/14
VDC and 230 VAC, EASA certification planned by end of 2008
MEDICAL INTERIOR FOR GROB SPN
Advanced Life Support Interior: designed for medevac
missions of one or two critically ill patients; features: single or
dual or neonatal patient configurations; features: single or dual
patient configurations, up to four med crew seats, oxygen
supply of 4,000 litres (2x 10 lt. / 200 bar), power system with
12/14 VDC and 230 VAC
» AIR AMBULANCE TECHNOLOGY GESMBH
AIR AMBULANCE EQUIPMENT EC 135
Intended use: rescue, disaster, intensive-care and neonatal
equipment. Transport capability: one patient in rescue,
intensive-care or neonatal, two patients for disaster
configuration. Design features: interchangeable air ambulance
equipment, installation and conversion in minutes, no
modification to the helicopter. Side- and aft-stretcher loading/
unloading. Module parts as floor, carrier, cabinet, oxygen station,
additional equipment at customer’s request. Crew: 1 doctor, 1-2
paramedic, 2 flight crew.
AIR AMBULANCE EQUIPMENT EC 145/BK 117 SERIES
Intended use: rescue, disaster, intensive-care and neonatal
equipment. Transport capability: one or two patient in rescue,
intensive care; Design features: interchangeable air ambulance
equipment, installation and conversion in minutes, no
modification to the helicopter. Easy aft-stretcher loading/
unloading with loading system and undercarriage stretcher.
Module parts as floor, rescue stretcher, carrier, cabinets, oxygen
station, storage box, ceiling panel with light and infusion holder.
Crew: 1 doctor, 1-2 paramedic, 1-2 relatives, 2 flight crew.
AIR AMBULANCE EQUIPMENT EC 155/AS 365 SERIES
Rescue, intensive care and neonatal air medical missions;
one or two patient rescue, ambulance, disaster; interchangeable
equipment in different configurations, no modification to
helicopter structure; one or two stretchers; Module parts
as floor, carrier, mid-level stretcher, storage box. Crew: doctor,
paramedic and relatives seating on PAX seat or medical
crew seat.
EQUIPMENT FOR BELL/AGUSTA BELL AB 205/212/412
Rescue, intensive care and neonatal air medical missions; one or
two patient rescue; interchangeable equipment, no modification
to helicopter structure, different configurations; one or two
stretchers in low loading height; medical equipment located in
holders. Module parts as floor, carrier, cabinet. Crew: doctor,
paramedic and relatives seating on medical crew seat or PAX
seat. Air ambulance equipment is also available for AS350/355,
AS332, Sikorsky and Mi-8.
CESSNA CITATION V AND ULTRA, LEARJET,
JETSTREAM, CHALLENGER, BEECH 1900
Air ambulance/intensive care equipment for patient transfer;
one patient; basic unit: stretcher in longitudinal position to
flight direction, drawers for medical equipment and materials,
waste bin; medical tower; oxygen/air station. Crew: doctor
and paramedics.
FLYING INTENSIVE STATION DORNIER 328/
ANTONOV 74
Intended use: intensive care stations for patient transfer.
Transport capability: 1 to 3 intensive patients. Design features:
interchangeable air medical interior, installation and conversion
in minutes, no modification to the aircraft. The module includes
cabinets, comfort stretcher, medical equipment carrier with
holders for medical devices such as ECG monitor system,
ventilation, suction unit and syringe pumps, holder for
compressed infusion bags and oxygen system, located
conveniently and easily removable from the holders at the
medical equipment carrier. Options: non-intensive care station
(NICS) RH to carry 2 patients, NICS LH to carry one patient,
NICS LH/S for one intensive patient, paediatric intensive care
unit (PICU) for an intensive care infant, incubator. Crew: 1 doctor,
1-2 paramedic, 1 flight attendant, 2 pilots.
» AIR METHODS CORPORATION
Dedicated medical interiors for Bell 206L, 222, 230, 407, 427,
430, 212, 412; MD Explorer; Eurocopter BK 117; Multi-Mission
Medevac System for US Army Sikorsky UH-60Q Black Hawk.
BELL 407 INTERIOR
Modular Medical Cabinet (MMC) is two modules: medical
services and hat rack, holds medical systems allowing for easy
access and operation in a high stress environment. Both
modules together weigh 38.5 kg (85 lb) and can be removed or
installed by one person in less than 20 minutes; secures in cargo
area thereby maximising cabin real estate. Installation of
interior retrofit takes two weeks. Articulating Patient Loading
System (APLS): weighs 18 kg (40 lb), swivel arm utilised during
heavy patient loading, 20 kg (44 lb) in travel allows medical
attendants to sit behind patient’s head.
BELL 430 INTERIOR
Modular Medical Cabinet (MMC) is located directly behind the
cockpit, emergency shut-off easily accessed by pilot. Two
patients treated by two attendants. Weighs 32 kg (70 lb).
Removed or installed by one person in 15 minutes. Combined
with the O2 system (gas or LOX) it weighs 45 kg (100 lb); 25 cm x
33 cm x 122 cm (10 in x 13 in x 48-in). Two connections, one for
power and the other for oxygen; auxiliary station on top for
storage, a lock box for narcotics, an IV warmer or an
air-to-ground ICS transmitter; installation of interior retrofit
takes two weeks; Multi-Function Floor (MFF), features a
multi-track, multi-directional matrix system; 100% machined
aluminium, contamination proof; Articulating Patient Loading
System (APLS) weighs 14 kg (60 lb) and has a 360 deg swivel
ability; 18 kg (40 lb) in travel and 0-15 deg incline/decline
capability allowing below-the-waist loading; 9 kg (20 lb) load
assistance eases loading of heavy patients.
MD EXPLORER INTERIOR
Modular Medical Cabinet: single location for all systems, one
person removal in under 20 minutes, 25 cm x 76 cm (10 x 30 in),
32 kg (70 lb). Articulating Patient Loading System: 27 kg (60 lb),
shock/antishock capability +15 deg, 18 kg (40 lb) travel for
below-waist loading from outside, 9 kg (20 lb) load assistance,
saves space. Contamination-proof aluminium flooring: replaces
existing floor, 27 kg (60 lb) net weight, increased utility and
durability, ten integral seat tracks, no abutments or blood traps,
contains spilt fluid, uses existing hardware, preserves
maintenance access. Flexible seating and storage options. LOX
or gaseous O2 installations available; upgradeable interior
systems.
PAULEY PAK IV INTERIOR FOR EUROCOPTER BK 117
Up to three patients, four attendants and one or two pilots.
Primary/secondary platforms (secondary converts to two seats).
Pauley Lift system on primary articulates to heights and
positions including Trendelenburg and reverse Trendelenburg.
Primary may support one patient on Pauley Lift and one on
secondary module. Third on floor. Dual vac/suction. Dual 115 V
inverters. Dual medical air systems 8,600 l pressurised LOX.
High intensity lighting. Medical console between aft-facing
seats. IV warmer/cooler; external power; heart monitor and
defib mounts. Doppler jacks for vein/artery monitors; blackout
curtain; provision for extras (eg, neonatal isolette) and storage.
visit us at www.shephard.co.uk
SHEPHARD
29
EMS » Interiors
» AIRTECH CANADA AVIATION SERVICES LTD
AGUSTA 109
Dual patient/incubator capability; load assist systems; medical
O2 systems; medical air; medical suction. EMS control panel (O2,
suction, air and electrical); storage cabinets; storable loading
system; inverter (110 V to 220 V); high-intensity cabin lighting;
interior panels; soft storage systems. EMS/ambulance
installations for: Piper PA-31 series and PA-42, Cessna 400 and
Citation series, Raytheon Beech King Air and 1900 series,
Mitsubishi MU-2 series, Lear Jets, Commander 700, Swearingen
SA26AT and Pilatus PC12.
Utility flooring, pivoting litter system using Ferno model 1402
stretcher, aft-facing attendant seat folds down for loading of a
patient and then up for the attendant. The seat also features a
large storage drawer and locking draft drug box, soft pocket
storage, respiratory gas system supplied by liquid oxygen or
light weight Kevlar wrapped aviation oxygen cylinders and
single or dual vacuum pumps, and medical air supplied by
cylinder or 28VDC pumps, IV hooks, emergency medical radios,
electrical support package with high-intensity dimmer lights,
lightweight AV inverter and 110 VAC outlets and 28 VDC outlets;
and blackout curtain.
SIKORSKY S-76 HELICOPTER INTERIOR
BELL 206L
FIXED-WING INTERIORS
Dual patient/incubator capability; up to four attendant positions,
two forward-facing, two aft-facing (tilt-back and full swivelling);
four point attendant seat belts; load assist uses Ferno 35A Aero;
dual medical O2 systems (under floor); dual medical air; dual
medical suction. EMS control panel (O2 , suction, air, lighting
and electrical); multiple stretcher positions in cabin; storage
cabins; storage loading system; hard storage systems; black-out
curtain; search light; inverter (110 and 220 V); EMS
communications panels; cabin/cockpit climate control systems;
interior panels (sides, floor, ceiling); high-intensity cabin lighting.
» BUCHER LEICHTBAU AG
Dedicated medical interiors for the Eurocopter BO 105, BK 117C2,
EC 135 and EC 155; dedicated medical interior for the Pilatus
PC-12; new generation stretcher system (in cooperation with
SAS Components).
B0105 AC31
Rescue conversion system for Eurocopter B0 105 helicopter;
components include wall-mounted medical equipment panel,
crew seating and oxygen, suction and electrical supply systems;
components have to be functional, light and very robust.
EC 135 EMS INTERIOR SYSTEM
Developed in co-operation with ADAC Luftrettung. Modular
units, easy-to-maintain construction and low weight. Floor:
integrated drain channels, liquid barrier and anti skid sections.
Fixed doctor seat and swivelling and tracking medical attendant
seat, both with full harness system. Primary and secondary
stretcher capability. Loading table allows for patients weighing
up to 220 kg (485 lb), maximum pointload on end of stretcher
table of up to 150 kg (330 lb). Universal box; medical panel; left
and right-hand side cabinets.
» CUSTOM AIRCRAFT COMPLETIONS INC
Dedicated medical interiors for the Sikorsky S-76.
» HELI-ONE INC
Dedicated medical interior for the Bell 206/407, 212/412,
222/230, 430; Agusta 109; Eurocopter AS 350/355, BK 117, EC
135, SA 365N and MD Helicopters MD-900 patient litter systems;
lightweight ground/air intensive care litter; medical flight crew
seating.
Moulded slip-resistant flooring; equipment panel attaches to
same rail system as positionable seats; mounts can be
customised for attachment of Life Pack 5/10, IV, pumps,
ventilators, etc; respiratory gas system; IV track assembly;
electrical support package; soft pocket storage; blackout
curtain; primary and secondary litters; defibrillator cabinet;
storage compartment (drug box and second monitor); aft
medical cabinet; Siemens Mini Med #3 IV pump.
BELL 212/412
Dual pivoting litter (litter base and mobile litter carriage);
high-intensity cabin lighting; centre attendant seat (pivots 360
deg); outboard/aft facing jump seats (two each); liquid oxygen
system; compressed air system; two suction systems; locking
drug box; pylon-mounted life support panel with medical
equipment brackets; overhead storage cabinet; forward medical
cabinets; soft storage pockets; bulkhead with blackout curtain;
EMS control panel; IV rails with hooks; other equipment includes
stowable six-place litter kit requiring six stowable stretchers and
two stowable stretcher support stanchions. New IV warmer/
cooler features: built in power converter; light weight and
compact fibreglass construction; powerful 140 Watt heating
capacity; standard 50 watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for four ampoules or medicine vials.
BELL 222/230/430
Dual pivoting litter system (with co-pilot seat removed or
installed); sliding pivoting attendant seat (quick change);
pivoting seat (secondary); medical flooring; respiratory gas
system; intravenous hooks; EMS radios; litter system life
support/storage base; rear medical cabinet; pylon life support
panel; electrical support; medical control panel; customised
mounts; high intensity cabin lighting. New IV warmer/cooler
features: built in power converter; light weight and compact
fibreglass construction; powerful 140 Watt heating capacity;
standard 50 Watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for 4 ampoules or medicine vials.
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Wh ich M ay E xpl ai n Why We’re Suc h G ood L i st e ne rs
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We listen when they tell us they
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fast and reliable OEM-authorized
When they say they want flexible
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pricing. When they ask us for
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more options. Maybe we’re
ask the owners of the thousands
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A fully authorized Pratt & Whitney Canada Distributor and Designated Overhaul Facility.
Call 888.769.0999 or visit www.atlanticturbines.com
30
Public Service Aviation Handbook 2008-09
EMS » Interiors
BK 117 EMERGENCY MEDICAL INTERIOR
Ferno # 30 multi-level lift in cot; secondary stretcher, when
folded in half, stores between the attendant and pilot seats on
the left and right hand side of the aircraft and is secured by a
Heli-Dyne Systems fabricated restraint system. High-intensity
cabin lighting; three-place, side facing seat for attendants, in
bench-style design. It can be quickly converted into a raised
litter platform to accommodate and secure the installation of a
secondary stretcher. One aft-facing medical attendant seat with
manual flip-up seat bottom, adjustable lumbar spine support and
integrated four point restraint system. The secondary medical
attendant seat serves as the mounting location for the LidePac
10 ECG/defibrillator, with its carrying case and accessory bag.
Medical utility floor; liquid oxygen converter system;
supplemental oxygen clamps; suction system; locking drug
system; left hand window medical life support panel; blackout
curtain; soft storage pockets; EMS control panel; IV with hooks
(four each pans/two each hooks); IV warmer/cooler. New IV
warmer/cooler features: Built in power converter; light weight
and compact fibreglass construction; Powerful 140 Watt heating
capacity; standard 50 Watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for four ampoules or medicine vials.
EPIC COT AND PATIENT LOADING SYSTEM FOR EC
135 AND EC 145
Interiors « EMS
EUROCOPTER SA 365N EMERGENCY MEDICAL
INTERIOR
Dual pivoting litter (litter base and mobile carriage litter) with
integral medical flooring; high-intensity cabin lighting; medical
crew seating includes centre attendant seat, side-facing
attendant seat and forward-facing jump seats (two each); liquid
oxygen system; compressed air or pump air system(s); suction
system; locking drug box; side-cabin mounted life support panel
with medical equipment brackets and aft storage cabinet;
bulkhead with blackout curtain; soft storage pockets; EMS
control panel; IV hooks; EMS communications console. New IV
warmer/cooler features: built in power converter; light weight
and compact fibreglass construction; powerful 140 Watt heating
capacity; standard 50 Watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for four ampoules or medicine vials.
Litter Kit
Heli-One Six-Place Litter Kit is designed to provide modular and
lightweight high density rescue and medical evacuation system
that can be quickly fielded for emergency response. The system
is certified (FAA STC No. SR09162RC) for Bell 212 and 412
helicopters.
MD 900 AIR MEDICAL INTERIOR SYSTEM (AMIS)
Hard-anodized aircraft-grade aluminium tubing provides
unsurpassed strength and rigidity in a lightweight design. The
hard-anodized coating eliminates abrasion and oxidation and
ensures quick and easy decontamination. The roll in loading
system with actuated folding-legs design, along with other
standard features including one-hand release fold-down side-rails
for use in restricted space and lift-assist pneumatic backrest
approved for all phases of flight, support actual one-person
operation and free the medical staff to perform life saving tasks.
The EPIC 272 kg (600 lb) capacity easily accommodates larger
patients while optimizing the space between patient and operator.
The oversized wheels (6x2) with sealed caster and roller bearings
provide stability and ease of mobility on all types of terrain and
standard locks prevent an unoccupied cot from rolling.
Dual pivoting litter system; secondary stretcher; medical utility
floor; high intensity cabin lighting; high g crash attenuating
medical crew seating; liquid O2 system; supplemental O2
clamps; compressed air system; suction system; locking drug
box; aft bulkhead mounted life support panel with medical
equipment cabinet and brackets; overhead storage cabinet; R/H
forward cabinets; soft storage pockets; blackout curtain; EMS
control panel; IV with hooks - four each pans/two each hooks;
EMS communications console; optional stowable litter kit; IV
warmer/cooler; SX-16 Nightsun searchlight. new IV warmer/
cooler features: built in power converter; light weight and
compact fibreglass construction; powerful 140 Watt heating
capacity; standard 50 Watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for four ampoules or medicine vials.
EUROCOPTER AS 350/AS 355
RAMS
Dual pivoting litter system; pivoting/tracking attendant seat;
utility flooring; positionable attendant seats; equipment panel;
respiratory gas system; IV track assembly; electrical support
package; soft pocket storage; blackout curtain.
Heli-One Roof Accessory Mounting System (RAMS) is designed
to provide modular installation provisions for the Goodrich
600lbs hoist system with superior cabin loading ergonomics
and minimal airframe modifications. The system is certified
(FAA STC No.SH8476SW) for Bell 412 helicopters.
EUROCOPTER EC 135 and EC 145 EMERGENCY
MEDICAL INTERIOR
Rappelling Kit
New primary patient loading system (EPIC PLS1); secondary
patient folding stretcher (EPIC PFS1); side/rear loading dual
pivoting litter system (EPIC DPL2); integral medical floor
assembly; RH tracking swivelling medical attendant seat 30 cm
x 38 cm (12/15 inch) options; LH/ RH aft facing attendant seat
provisions 30 cm x 38 cm (12/15 inch); fold-up stowable medical
attendant seat; blackout curtain; high intensity cabin lighting;
medical equipment rails; medical services panel; electrical
support package; soft pocket storage; respiratory gas system; IV
hooks; emergency medical system radios and overhead console;
center cabin medical cabinets; Heli-Dyne Systems, Inc new IV
warmer/cooler features: built in power converter; light weight
and compact fibreglass construction; powerful 140 Watt heating
capacity; standard 50 Watt cooling capacity; optional 140 Watt
thermoelectric heat pump; digital temperature controller; built
in storage slots for four ampoules or medicine vials.
32
Public Service Aviation Handbook 2008-09
» KAZAN HELICOPTERS JSC
MIL MI-17 FLYING HOSPITAL INTERIOR
‘Flying clinic’ for deployment to remote, austere locations; can
land at up to 4,000 m (13,123 ft) above sea level; APU ensures
autonomous operation/engine start; cargo compartment
converted to heated, sound insulated operating room;
mop-clean wall panels; two portable generators for independent
power supply on the ground; medical equipment voltage 220
VAC/24 VDC; EV 801 ventilator; Titus respiratory/anaesthetic
apparatus; Oxyshuttle pulse oxymeter; Cardiolog 2000
defibrillator; PM8014 monitor; other equipment present.
» KEYSTONE HELICOPTER CORPORATION
Medical interior kits (installation assistance available): Bell 206L
Quick Change Kit; Eurocopter AS365N; Eurocopter BO105
Medical; Sikorsky S-76. Accessories: IV hook system; litter
retention system; SX-16 Searchlight side-mount kit for BK117;
SX-5 Searchlight side-mount kit for S-76; liquid oxygen (LOX);
engineering, design and FAA/JAA certification services.
206L/407 EMS QUICK CHANGE KIT
Provides a solution to rapid mission profile changes; facilitates a
five-minute conversion from executive or utility to medical
configuration; STC and PMA-qualified for application on Bell
206L helicopters; fits under standard Bell litter kit between
existing forward and aft seats; lightweight carbon fibre kit has
provisions for basic life support equipment including oxygen,
suction, 110 VAC power and miscellaneous storage; provisions
for three E or D cylinders; plumbing for two outlets; oxygen and/
or air in any combination (oxygen regulated to 50 psi at outlet);
options include suction pump, additional power sources.
QUICK CHANGE LONGRANGER INTERIOR
Quick-change kit; self-contained; designed for installation under
the standard Bell litter arrangement; unit can be installed or
removed in ten minutes. Standard features include: three class E
cylinder hook-ups for oxygen; two Ohio Medical outlets; 28 V
wiring and hardware; storage for Lifepak 5 or equivalent; 250
ml suction bottle storage; 28 V suction pump plumbed into the
medical suction outlet.
S-76 HELICOPTER EMS INTERIOR
Configuration features a primary patient litter mounted on a
base that provides rotational (360 deg) and longitudinal (litter
axis) movement; a secondary fixed litter is located adjacent to
the primary just off the aircraft centre line; primary seating
consists of two full-size, aft-facing seats; secondary seating
features two seats facing forward on the aft bench; secondary
seats have hinged storage compartments in the backs; the
helicopter has the capacity to carry two adult patients and up to
four medical crew members; full body access; complete patient
monitoring; medical equipment includes: isolettes, nitre-aortic
balloon pump.
» LIFEPORT INC
Designs, manufactures and certifies air ambulance, law
enforcement and utility equipment for both fixed-wing and
rotary-wing aircraft. Offers a premium option for long range VIP
medical transport, mass evacuation/repatriation equipment,
high-density seating options and ballistic protection. The
medical interiors of LifePort’s medical helicopter interiors are
built around the MedDeck patient handling platform, MedPak
advanced life support module, AeroSled stretcher, and receiving
deck. The MedPak consists of an oxygen, vacuum and
compressed air system and electrical inverter.
Heli-One rappelling kit is designed to provide secure and modular
attachment points for Search and Rescue and tactical insertion
operations. The system is certified (FAA STC No.SH3886SW) for
the Bell Helicopter Textron aircraft models 205, 212 and 412
» HILLAERO MODIFICATION CENTER
Dedicated and quick change medical interiors for fixed-wing
aircraft including custom medical cabinetry, loading lights, door
kickstand, aft-baggage net, intubation seat, and aft-ramp
storage cabinet.
visit us at www.shephard.co.uk
SHEPHARD
33
EMS » Interiors
» SPECTRUM AEROMED INC
Patient Transport Container, self-contained medical unit for
airline use.
BELL 407 INTERIOR
» METRO AVIATION
BO 105 TWIN JET III EMS KIT
Wheelen PA/siren with one speaker; four fixed landing lights;
custom two litter tracking and floor system; external oxygen
system with two outlets; one outlet suction system; 110 V AC
inverter; 12 V DC converter; medical storage pouches; aft
medical wall; Lifepac V bracket; blood pressure monitor bracket;
IV rack; aft facing attendant seat; pilot isolation barrier; side
facing attendant seat with shoulder harness; stainless steel
leak-proof floor with blood dam; optional third attendant seat
and shoulder harness; patient examination lighting; FAA STC
number 3663SW.
EC 135 HELICOPTER EMS SYSTEM
One/two primary litters feature one-person loading and include
single-point post-lock system; two aft-facing, positionable
attendant seats with three-point restraint system; leak-proof
impact-absorbing composite floor with blood dam; external
transfill oxygen system; options include: stowable secondary
litter with posi-lock, stowable forward-facing high-g third
attendant seat with four-point restraint system, 360 degree
rotating attendant/observer seat with four-point restraint
system, modular avionics and medical control panel, 110 V AC
inverter (12 V DC converter), built in suction, left and right
mission-adaptable storage pods, medical cabinets, D or E
cylinder storage, LOX system, Tac-comm systems, mounting
options for isolette, balloon pump, examination lighting, etc,
custom paint, avionics options to custom specifications,
environmental control option.
EUROCOPTER ASTAR/TWIN STAR EMS KIT
PA/siren with one speaker; night scanner search light; single
litter on tracking carriage; transfill oxygen system with two
outlets; built in suction system; 110 volt AC inverter (12 volt DC
converter); medical storage pouches; aft medical wall or
modular cabinet for outlets and controls; various configurations
for carry-on medical equipment; IV rack; one tracking/pivoting
attendant seat; one or two positionable attendants’ seats; pilot
isolator barrier; all seating has four-point restraint system;
leak-proof composite floor with blood dam; patient examination
lighting; easily changeable to other configurations; avionics
options to custom specifications; aircraft options include high
skids, custom paint, DeVore lights, air conditioning.
» PHI AEROMEDICAL SERVICES
Dedicated medical interior for the Eurocopter BO 105, BK117.
» PREMIER AVIATION INC
Dedicated medical interior for the Bell 206L and 407; energy
attenuating crew seats.
» SIKORSKY AIRCRAFT CORPORATION
S-76 HELICOPTER EMS INTERIOR
Sikorsky Aircraft Corporation is a world leader in the design,
manufacture and service of advanced helicopters for
multi-mission applications. Sikorsky’s S-76C++ features a large
cabin area to support the multi-mission role and maintains a
99.9 percent dispatch reliability rate. The S-76 can be found
around the world in public service, police, SAR and EMS missions.
34
Public Service Aviation Handbook 2008-09
Quick change modular system; allows reconfiguration from
executive seating to air ambulance in less than ten minutes;
component box contains a vacuum pump, air compressor, inverter,
pneumatic and electrical outlets below the stretcher; 2,350 litre
(621 US gal.) oxygen tank located in cargo area; medical panel
features pneumatic outlet for oxygen and gauge; stretcher locks
into place, with locking and unlocking on either side.
WHEN LAW ENFORCERS
DEPEND ON IT,
WE’RE RIGHT ALONGSIDE.
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» LUFTHANSA TECHNIK AG
DUAL PATIENT DEDICATED SYSTEMS FOR KING AIR 200 & LEARJET 31/35
Designed to transport two adults, two incubators or a
combination of each; forward two storage drawers, one for
defibrillator the other for medical equipment or supplies; aft
section houses 7,000 litres (1,849 US gal.) of oxygen, two 1,000
Watt inverters, three air pumps and two vacuum pumps;
overhead compartment has pneumatic and electrical outlets,
built in suction regulators, patient monitoring mounts and
optional radio bays; system has a Patient Loading System with
pneumatic assist, allowing the loading of a 159 kg (350 lb)
patient or incubator.
» TEXAS AVIATION SERVICES
Customer service facility for Emergency Medical Systems (EMS),
Airborne Law Enforcement (ALE), Corporate/VIP, Maintenance,
Repair and Overhaul (MRO), Special Mission, Search and Rescue
(SAR), Military Retrofit and Paint for Agusta, Bell, Eurocopter
and Sikorsky helicopters.
INTERIOR-RELATED EQUIPMENT
» AERO-DIENST
AMBULANCE EQUIPMENT
Two additional components are needed for completion of the
Aero-Dienst ambulance equipment: the GOX bottle container,
which carries three oxygen bottles and the Intensive Rack; both
units in combination provide electrical power, oxygen and air
supply to the medical equipment (respirator, vacuum pump,
reanimator, etc); all necessary emergency and intensive care
equipment that the medical personnel require can be brought
onboard the aircraft, stowed securely and used in flight.
INTEGRATED LOADING DEVICE (ILD)
Designed for business/executive aircraft and helicopters;
stress-free loading/unloading of patients with minimum effort
by flight and medical crew; low weight; quick, easy installation
and removal; safe, easy storage in small area; no modifications
to existing aircraft door areas or special access needed; max of
two people required for installation and use; patient remains
horizontal during loading/unloading; stretcher loading/support
rail needs only two fixing points in aircraft cabin, folding support
strut on ground; fits any aircraft/helicopter; couplings and
connectors standardised.
Good news for all law enforcement operators.
Whatever platforms you use for your search
and rescue, Goodrich has a hoist that’s ready
and available.
Whether you operate AS350s, EC145s or A109s,
there’s a Goodrich hoist you can rely on to provide
the perfect solution.
Goodrich is unique in providing the translating
drum technology, which has the highest reliability
in the industry and no fleet angle restrictions.
And Goodrich has the lowest life cycle costs.
So whichever platforms fly your missions, depend
on Goodrich to be right there with you.
For more information about Goodrich rescue hoists,
email sis@goodrich.com
right attitude/right approach/right alongside
www.goodrich.com
EMS » Interior-related equipment
» AEROLITE MAX BUCHER AG
AEROLITE C3 - INTENSIVE CARE TRANSPORT SYSTEM
Bed size 195 cm x 55 cm (78 in x 22-in); basic weight 30 kg (66
lb); payload 220 kg (485 lb); internal battery power; internal
oxygen and air supply; external DC and AC power connection;
external oxygen and air connection; adjustable IV mast;
detachable folding trolley; respiratory and monitoring
equipment; vacuum mattress; miscellaneous pouches.
» AEROLITE MAX BUCHER AG/FISCHER &
ENTWICKLUNGEN
HELICOPTER SEATS
Modular, all-in-one seating concept; medical attendant;
observer/instructor; combi seat (for co-pilot, attendant or hoist
operator); cabin seat. Basic seat: 9.5 kg (21 lb); SRP height 23 cm
(9 in); energy absorbing design - System Fischer; forward/rear
facing; MS 33601 A seat track mounting; recline fixed at four;
adjustable headrest; inertia reel four-point harness; detachable
upholstery. Options: swivelling and sliding unit; adaptor for
fixed seat both increase SRP height to 25 cm (10 in); panel
mount fittings; quick release track fittings (MS 33601 A);
adjustable recline; manual harness lock/unlock; combi seat kit
tailored to individual helicopter; custom finish.
» AIR AMBULANCE TECHNOLOGY SELF
CONTAINED MEDICAL UNIT (SCMU)
Critical care-equipment for uninterrupted patient transfer;
transport capability - one patient in critical care configuration.
Includes comfort stretcher; IV pole; medical devices in holders;
ECG monitor/defibrillator; respirator; suction unit and syringe;
oxygen system and medical power distribution unit; lifting
device (battery powered) for loading and unloading.
» AIR METHODS
ARTICULATING PATIENT PLATFORM
Lightweight platform secures into aircraft seat tracks; head/
spinal adjustment integrated into litter; 1 m (40 in) longitudinal
travel 51 cm (20 in) either side of centreline); 360 deg swivel;
decline/incline to 15 deg; adjustable loading heights; weight
approximately 34.02 kg (75 lb) with litter; height 26.03 cm
(10.25 in); width 40.64 cm (16 in); length 1.27 m (50 in).
EMS LIGHTWEIGHT 2001 PATIENT LITTER
Designed to be secured to Air Methods’ articulated patient
loading system (APLS), or directly to the aircraft floor;
perimeter tubing provides easily accessible handholds; integral
spinal angulator provides patient support – from 15 deg to 85
deg – and can be used in take-off and landing without returning
the patient to a horizontal position; patient restraint system
features disposable webbing belts and a four-point harness,
adjustable to patient size; closed cell foam pad, upholstered
with a tough, non-absorbent material.
MULTI-FUNCTION MEDICAL CABINET
Converts an aircraft into a medical transport vehicle without
needing airframe modifications; locates aft of cockpit, between
two aft facing attendant seats; delivers oxygen, vacuum and
electrical requirements to two patients; height 117 cm (46 in);
width 39 cm (15 in); depth 42 cm (17 in). Standard features:
medical storage; medical suction cabinet; medical cabinet
36
Public Service Aviation Handbook 2008-09
Interior-related equipment « EMS
lighting; pilot medical control panel; LOX or gaseous O2
systems, 110 V AC/220 V AC electrical system. Options:
equipment rail; medical air system; upholstered pouches;
vacutron suction system; intercommunication system.
FOLDING TRANSPORT SYSTEM (FTS)
LAW & EMERGENCY MEDICAL SYSTEM (LEMS)
» BAE SYSTEMS INC.
HD/Ferno FTS designed to provide users of side loading medical
helicopters ease in patient movement; offers lightweight (approx
14 kg/30 lb) and compact size for transport in the helicopter
baggage compartment; eliminates gurney requirement; wheel
locks; 158 kg (350 lb) capacity.
SIMULA ENERGY-ABSORBING MEDICAL
ATTENDANT SEAT
MODEL 5 ADVANCED LIFE SUPPORT UNIT FOR
BELL 212/412
Fits AS350/AS355; litter system; quick change copilot seat;
pilot isolation barrier; leak-proof composite floor with blood
dam; transfill O2 system; one or two positionable attendant
seats; all seats have four-point restraints; conversion to either
law or EMS configuration in under 1 minute; 110 V AC inverter
or 12 V DC converter; built in suction; tactical communications;
SX-16 Night Sun; SFIM autopilot; Freon air con; custom paint; all
Eurocopter factory options; avionics to customer spec; Wheelen
PA/Siren; other options include high skids, wire strike
protection, DeVore lights.
The energy-absorbing swivel seat was the first seat of its kind
certified to the new energy-absorbing requirement; full
360-degree swivel; lock positions every 15 degrees; folding seat
back; tracking adjustments can be made on fore/aft or lateral
tracks; four-point restraint system with an automatic locking
inertia reel; three seat back positions; seat can face the forward
or aft directions for taxi, take-off and landing operations;
maximum seat weight is 40 kg (58 lb); meets structural
requirements of the FAA’s TSO-C127 Type B for FAR Part 27 and
29 rotorcraft applications.
» DART AEROSPACE
Design and manufacture Skidtubes (using Round-I-Beam
technology), crosstubes, lightweight steps, bearpaws,
emergency stretcher kits, shoulder harnesses, aircraft disabling
devices, baskets, mirrors, spacedoors, vertical reference
windows, fuel purge canister.
» DOCTOR DOWN
RESCUE WRAP
A self-contained bedding system to maintain patient body
temperature. This patented three-part system can be easily
modified for use in many climates and accommodates
patients up to 181.4 kg (400 lb). It is a warm, compact,
lightweight and waterproof barrier to the elements with a
disposable liner system to contain body fluids. Velcro
straps secure fluid bags, monitors and pumps in place, and 2
large internal pockets hold reusable heat packs (included) for
patient warming. Kit weight is 14 lb (6.35 kg).
» FERNO AVIATION Inc.
AERO ORB LIQUID OXYGEN SYSTEMS
The Model 526 Liquid Oxygen Component System and the
Model 526-RTI (Ready-To-Install) Liquid Oxygen System have
proven reliable and safe in over 150 FAA approved aeromedical
installations and in over 30,000 military installations. The Liquid
LOX System requires 75% less space and is 75% lighter than
high-pressure systems. The 10 Litre LOX System can hold the
equivalent of 8,600 litres (2,271 US gal.) of gaseous oxygen. At
a flow of 5 lpm (1 Us gal pm), the 10 Litre (2.6 US gal) LOX
system can provide gaseous oxygen for 28 hours of flight time.
The Model 526-RTI includes all required system components in a
pre-engineered enclosure with mounting hard-points, access
door, and quick-disconnect external connections for oxygen,
electrical supply, supply vent, and quantity monitoring. The
dimensions of the Model 526-RTI are 41 cm (16 in) height x 36
cm (14 in) width x 46 cm (18 in) depth.
FAA APPROVED PATIENT RESTRAINTS
A complete line of FAA Approved Patient Restraints including
the lap belts and shoulder harness assemblies. The units have
sewn loops at the ends for easy attachment and removal from
stretchers and patient loading chairs. The lap belts meet FAA
TSO C22g and the shoulder harnesses meet FAA TSO C114
Converts standard Bell 212/412 in under 7 minutes; selfcontained; no aircraft modification; complies with FAA
TSO 39b; compatible with all medium and larger aircraft;
interchangeable between types; custom base adaptors;
portable cardiac monitor/defibrillator; portable suction; portable
ventilator; O2 for 1.5 hrs on ventilator or 2.75 hrs of O2 therapy;
light stretcher with folding IV stand; storage drawers and
compartments; swing-out instrument tray; tie-down rings;
fold-out handles with base interlock; quick attach points for
optional equipment; optional pulse oximeters, infusion pumps,
transport isolettes, custom seats.
MODEL 46 PASSENGER LOADING CHAIR
Designed to conveniently transport a person through narrow
passageways, including most commercial aircraft aisles, and
other areas where space is limited. It has a sturdy light-weight
aluminium frame with a heavy-duty vinyl coated nylon cover
and seat pad. The loading chair comes with two upper body
restraints and one leg restraint. The unit is 132 cm (52 in) high x
38 cm (15 in) wide, and 86 cm (34 in) deep. It weighs 8 kg (17 lb).
» LENOIR AVIATION
AIR PORTABLE HOSPITAL
Self-contained unit designed for transport by Hercules C-130,
L-100 or Transall C-160 aircraft; the only mobile hospital unit in
which a successful kidney transplant has been made, according
to the company; able to operate 48 hours on its own power
generator and with its own water supply; circa 15 minutes to
load unit into aircraft (via its Remlift screw jacks handling
system); once the aircraft has landed, the unit is delivered to
site by truck, semi-trailer or towed on its own wheels. Units are
then operational within the hour; self-contained oxygen tanks,
water tanks, vacuum and air-conditioning service; modules
include a surgical care unit and intensive care unit; additional
mobile unit for production of injectable aqueous solution;
engineer training included; overnight delivery of spare parts, if
needed; service contracts available.
» METRO AVIATION CUSTOM OXYGEN SYSTEM
Developed for MBB BK117 ‘Spaceship’ and MBB BO 105 Twin Jet
III aircraft. BK117 system features are: Scott Aviation 2.16 cu m
(76.5 cu ft) oxygen bottle and regulator assembly; under-floor
bottle mounting; emergency electrical shut-off valve for low
pressure oxygen supply; emergency shut-off accessible to pilot
and crew; single point system filling; all stainless steel lines and
fittings; dual contents gauges. B0 105 system features:
externally mounted Scott Aviation bottle and regulator
assembly; streamlined fibreglass weather-proof bottle fairing;
single point system filling; cable-actuated emergency low
pressure shut-off accessible to pilot and crew; stainless steel
lines and fittings; installation approved under FAA STC
#3663SW.
» NOORDUYN
NNAL527 AIRBORNE STRETCHER
Stretcher system suitable for L-1011, B-747/767/727/757, DC9,
Airbus A320 and de Havilland Dash 8 aircraft; sloping outboard
legs allow installation close to the aircraft side, over the top of
the window row; reversible, to permit location at left or right
hand side of aircraft; accessories include two-track adaptor
assemblies, setting bar, curtain assembly, foam rubber mattress
and fabric carrying case.
» SOS LTD
HYPERLITE FOLDING PORTABLE HYPERBARIC
CHAMBER
Supplied as fully operational unit, except for air and oxygen
cylinders; pressurised on site and then transferred under
pressure to any therapeutic facility; other items include
dome edge protection rings, medical lock, wheeled internal
stretcher, lifting slings, additional pneumatic and/or electrical
connections, air and oxygen cylinders, air and/or oxygen
adapters, oxygen and/or carbon dioxide monitors, thermometer/
gygrometer, remote air inlet tube and silencer, exhaled gases
hose assembly, back-up pressure gauge in chamber, absolute
pressure gauge, activated carbon filter for scuba air, folded
dry zipped storage bags, folding equipment trolleys, silicone
rubber repair kit.
» SPECTRUM AEROMED
500-LP LOW PROFILE
Modular; dual position overhead pneumatics; dual supply
outlets: O2, air, vacuum; stretcher with expandable arm rests;
four IV mounts; wiring harness; master panel breaker (relay
optional); bench length 72 in; width 17 in; height 10 in to top of
bench; base unit 118 lb; overhead console 14 lb; air pump 11 l/min
@ 50 psi; vacuum pump 14 l/min @ 14 in Hg; 2 x 115 VAC outlets,
1 x 28 VDC outlet; O2 3,500 l or 7,500 l. Options: infant
transport deck, patient loading system, dual vacuum and air
pumps, O2 interface, IV pole, auxiliary equipment table, unit
loader, dual, large capacity, or 230 VAC, 50 Hz inverters, mobile
overhead console.
SHORTBOX 2000
Compact design allows aft portion of stretcher to cantilever
over the back of the divan, giving crew more forward space;
self-contained, featuring dual pneumatic outlets, 3,500 litre
oxygen capacity, inverter, dual air pumps, vacuum pump and
electrical outlets; accessories include: equipment tables, IV pole,
patient loading and incubator decks.
visit us at www.shephard.co.uk
SHEPHARD
37
www.cobham.com
© McAlpine Helicopters
AIRCRAFT
SPECIFICATIONS
EMERGENCY MEDICAL
Chelton Ltd, Fourth Avenue, Marlow, Bucks, UK, SL7 1TF
CDUs are NVIS Green A, Type l/ll, Class B
compatible
Remote CDU for operation in rear cabin
Standard Dzus-mount CDU
ARINC 600 transceiver chassis
Designed to DO160 D/E environmental
requirements
TEA 1,2,3 and 4
HPSC
Air-interface and End-to-End (E2E) encryption
High level of interoperability with all
network infrastructures
Proven core TETRA radio
In-service worldwide
Single and multiple radio solutions
Airborne TETRA
Radio Systems
Telephone: +44 (0) 1628 472072
Email: mkt@chelton.co.uk
SERVICE
LAW ENFORCEMENT
SEARCH AND RESCUE
FIREFIGHTING
guide to OPERATORS
ACTIVITY GUIDE
GUIDE TO SUPPLIERS
PRODUCT GUIDE
EQUIPMENT
law enforcement
The equipment featured in this section is divided into:
±Electro-optical pods
±Microwave links and antennas
±Helmet-mounted systems
±Night vision goggles
±Searchlights
±Obstacle warning systems
±Voice communications
±Mission management systems / moving map displays
The section begins with an article highlighting major activities in the
growing worldwide police aviation market.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.
LAW VIEW » Tom Withington
Investment versus rationalisation « LAW VIEW
sPENDING SPREES AND BELT
TIGHTENING FOR 2008?
By Tom Withington
North America is seeing increased investment into helicopters for law enforcement while
in the United Kingdom in particular, police helicopter assets are undergoing a period of
rationalisation and restructuring.
T
he past year has witnessed purchases of new law
enforcement helicopters in Europe, North America,
Asia and Africa. At the same time, budgetary
concerns, particularly in the UK and North America, have
caused some Police Air Support (PAS) units to fall under
scrutiny and restructuring in a bid to reduce their operating
costs. At the manufacturer’s level, Eurocopter,
AgustaWestland and MD Helicopters continue to enjoy
healthy sales of their law enforcement products.
In Europe, London’s Metropolitan Police disposed of
three Eurocopter AS 355N machines, which have been in
storage since 2007, to a French aircraft chartering company.
This follows the acquisition of Eurocopter EC 145 machines
by the force in 2006. Further north, in January 2008
Greater Manchester Police took delivery of a new MD 900
Explorer, which will replace the existing helicopter of the
same type that the force already operates towards the
second half of the year. The aircraft that this new
helicopter replaces has already amassed over 7,000
» French paramilitary police officers descend from a
Eurocopter BK 117 helicoopter.
40
Public Service Aviation Handbook 2008-09
service hours since it began operations in 2001.
Greater Manchester’s neighbouring force, Lancashire
Police, has performed a major upgrade of its Eurocopter
EC 135 helicopters with new cameras. The upgrade had
been financed, in part, by the Proceeds of Crime Act, UK
legislation that allows seized criminal assets to be used to
pay for law enforcement improvements. That said, the
North East Air Support Unit was fighting for its future
in February with senior police officers deciding the fate
of the two EC 135s which cover Cleveland, Durham and
Northumberland in northern England.
Current plans call for the fleet size to be reduced to
one aircraft. However, further south in a bid to improve
police helicopter coverage, Essex Police agreed to provide
air support to the county of Kent, giving both counties up
to 20 hours of coverage per day, seven days a week.
On the continent, Austrian police are due to receive a
single Eurocopter EC 135 this year as an addition to the
four similar aircraft which arrived in 2009. It was expected
to support law enforcement operations for the 2008
European soccer championships, which were taking place
in Austria and Switzerland at press time. The deliveries are
part of an eight-helicopter order which the
Austrian Ministry of the Interior signed with
Eurocopter in 2007. In France the Groupement
des Formations Aériennes de la Gendarmerie
Nationale (National Gendarme Aviation Group)
is performing a wholesale revitalization of the
service’s helicopter fleet, ordering a total of 15
Eurocopter EC-145s to be delivered in their
entirety by 2013 plus 37 EC 135s which will
replace the force’s Eurocopter Alouette III
and AS 350 helicopters. To the north, the
Netherlands Police Agency has ordered a pair
of AgustaWestland AW 139 helicopters for law
enforcement operations.
NORTH AMERICAN MARKET
In the US, the San Bernardino Police
Department in California was looking hard
at its finances in Spring 2008 to see if it
could continue to operate its Robinson R44
helicopter, which is operated by a private
company under a contract. San Bernardino
was not the only American city looking at its
helicopter operations. Staying in California,
Sonoma County is to operate a single Bell 407
under contract from Aviation Specialists
Unlimited of Idaho to provide air support to the
County Sheriff.
In Texas, the city of Austin is considering
whether the local police helicopter is giving value for
money. However, some voices in the city are actually calling
for the police department’s PAS unit of one aircraft to be
increased, given the conurbation’s size. Meanwhile it was
announced in April 2008 that Houston, TX, would receive
new aircraft to supplement the existing four MD-500E
Explorers and two Schweizer 333 machines.
City officials in Columbus, OH, have given the go-ahead
for the construction of a new heliport to support the
Columbus police department as a base for the force’s five
MD-500E aircraft. The state of Delaware received a new
Bell 412 helicopter which is configured for SAR as well as
law enforcement. The helicopter is equipped with floats to
allow it to perform rescues on water during flooding.
Finally, the state of Maryland is looking to replace its
Eurocopter AS 365 aircraft, announcing a solicitation for
bids with the Sikorsky S-76, Eurocopter EC 135 and EC 145
in the running to fulfil the requirement to provide a new
aircraft for state police.
Looking towards the Caribbean, police in the Cayman
Islands are looking forward to their Eurocopter EC 135
entering service in 2008, which will replace the private
service that the force currently buys from Cayman
» Law enforcement aircraft are increasingly being called
upon to support SAR and EMS operations. (eurocopter)
Helicopters for air support. Furthermore, police in
Edmonton, Canada, have decided to purchase a second
Eurocopter EC 120 to supplement the force’s existing
aircraft, which will allow the police to provide air support
for 24 hours per day.
Looking at the rest of the world, 2007 saw the Abu
Dhabi Police Air Wing celebrate its tenth anniversary.
The force deploys six Agusta AB 412 and three Eurocopter
BK 117 helicopters. The Police Air Wing provides a range
of functions in addition to its law enforcement duties,
including SAR, VIP transport and Emergency Medical
Services. In Asia, Tokyo Metropolitan Police placed an order
for a second AW-139 in May 2008, which will join the first of
the type which was delivered in March 2006.
Other orders for helicopters by the Tokyo force are
expected as the service performs a wholesale fleet
modernisation. In China, Beijing Police received an
AgustaWestland AW-109 for the Beijing Municipal Public
Services Bureau. This order follows a 2004 delivery of an
AW-109 to Shenzhen Police. ±
visit us at www.shephard.co.uk
SHEPHARD
41
LAW » Electro-optical pods
Electro-optical pods « LAW
LAW ENFORCEMENT EQUIPMENT
ELECTRO-OPTICAL PODS
» CONTROP PRECISION TECHNOLOGIES LTD
DSP-1 Payload
» AXSYS TECHNOLOGIES
CINEFLEX V14 HD
High-definition five-axis gyro-stabilised turret system with an
integrated high-definition daylight camera and a laptop
controller. Light and compact, it is designed for surveillance and
security as well as cinema and news gathering operations. The
V14 HD relies on an extremely accurate gimbal system that
provides sharp, stable performance and comprehensive control
of azimuth, elevation, and roll. Its flexible high-definition daylight
camera accepts multiple lens configurations with optical zoom
capacities extending from short range wide fields of view to long
range narrow fields of view. Features: extremely accurate gimbal
system; automatic and steerable field of view; continuous 360º
pan (azimuth); +20º to-195º tilt (elevation); +/- 45º roll; Sony HDC
1500 high-definition TV camera with 1,920 x 1,080 effective
pixels; f/1.4 prism system; multiple lens options; full digital servo
control system; choice of ergonomic laptop control units. Weight:
45 to 68 lb depending on lens. Dimensions: 19.5 x 14.5 x 19.5 in.
CINEFLEX V14MS II
Designed for 24-hour surveillance applications, can be configured
to accommodate multiple payload instruments in a compact
package. Payloads include: high-definition day/night camera, wide
field of view camera, three field of view thermal imaging camera,
laser rangefinder, laser illuminator/designator. System
specifications: System type 5-axis gyro-stabilized multi-sensor.
Turret size (H x W x L) 19.5˝ x 14.5˝ x 19˝. Turret weight <80 lbs.
Azimuth coverage 360° continuous. Elevation coverage +36° to
-188°. Roll coverage +/- 20° (HD sensor only). Slew rate >55° /sec.
Thermal imager: Sensor type 640 x 512 15μm pitch focal plane
array. Wavelength cooled 3-5 μm InSb. Output NTSC/PAL. Fields
of view: 3 (FOVs) 31.5° x 24.0°, 9.10° x 6.90°, 2.70° x 2.06°. HD daylight imager: Camera Sony HDC-1500. Imaging device 3-CCD
2/3˝. Effective pixels 1920(H) x 1080(V). Aspect ratio 16:9. Frame
rates 1080/50i, 60i, 30P, 25P, 24P, 720/60P, 50P. Video Output
HDSDI (BNC-2) test out (BNC-1). Minimum illumination 10 lux
(.9290 foot-candles). Zoom ratio 25x (16.5mm to 413mm). Optical
extender 2x (825mm) Digital extender 2x (1650mm). Field of view
32.25° x 18.33° (16.5mm) to 0.4° x 0.2° (825mm). Laser
rangefinder option: Laser type erbium-glass. Wavelength 1.54
microns pulse rate 12 PPM (1-Hz optional). Range resolution +/- 5
m (optional +/- 2 m). Min/max range 50 metres / 20 Km. Receiver
aperture 40 mm. Detector (INGAAS TYPE) APD. Beam divergence
1.0 mrad (standard) 0.5 mrad (optional). Laser illuminator
option: Output power 1W or 2W options. Classification class 4.
Beam divergence 1° x 1°. Laser pointer option: Type NVG
compatible – target pointing. Emission Wavelength 830 μm.
Classification class llb beam divergence 0.2 mrad, 2 - 1 aspect
ratio. Output power 5 – 40 mW. Options: Auto tracker, radar and
navigation interface, NightSun interface, digital zoom (1x to
4x-continuous), DVR (continuous loop recording/H.264 encoding),
geo-pointing, video fusion (HD daylight and IR), frame grab w/cab
accessible SD card drive (USB), moving map.
42
Public Service Aviation Handbook 2008-09
Compact dual sensor day/night observation system for
helicopters, light reconnaissance aircraft, UAVs and marine
patrol boats. Highly stabilised platform: four gimbals stabilise
the turret in azimuth and elevation to better than 20
microradians RMS. Pointing accuracy is 0.5°. Field of regard:
+70° to -115° in elevation, unlimited in azimuth. IR sensor FOX
450: 3-5 micron indium antimonide (InSb), 320 x 256 element
focal plane array with up to x22.5 continuous optical zoom lens.
Fields of view are 27° x 20.6° (wide) continuous to 1.2° x 0.9°
(narrow), 0.6° x 0.45° (electronic zoom). Daylight channel:
High-resolution colour CCD camera with 768 x 494 element chip
and x20 continuous zoom lens. Fields of view are 13.6° x 10.2°
(wide) and 0.7° x 0.52°. Gain control is automatic. Turret
Weight: 22.5 kg ( electronics box: 3.5 kg). Dimensions: diameter
330 mm x height 483 mm. Temperature limits: -20° to +50°C.
Vibration Endurance: 2.5 grms, 5 to 2,000 Hz. Electrical
Interface: voltage is 28 VDC, power consumption is 110 W, video
output is NTSC or PAL. Options: FOX 720, x36 continuous IR
zoom lens, Narrowest FOV 0.76° x 0.59°, extended maritime
environment, low temperature, laser pointer (LP), x1.5 extender
for TV zoom lens, eye-safe laser rangefinder (LRF), dual parallel
output (TV, IR), GPS interface, 1553 and ARINC 429 interfaces.
Truck detection: 25 km (day TV), 25 km (IR). Truck recognition:
10 km (day TV), 7.5 km (IR). High ratio performance to weight.
MSSP-3 Payload
Three-sensor day/night observation system designed for
maritime patrol applications on helicopters, fixed-wing aircraft
and boats. Stabilised platform: Four gimbals stabilise the line
of sight to better than 25 microradians with a pointing accuracy
of 3 milliradians. Field of regard: +35 to -110° in elevation,
unlimited in azimuth. IR Sensor: 3-5 micron indium antimonide
(InSb), 320 x 256 element focal plane array with up to x22.5
continuous zoom lens. Fields of view are 27° x 20.6° (wide), 1.21°
x 0.91° (narrow). Daylight channel: High-resolution black and
white CCD camera with x15 zoom lens. Fields of view are 18° x
13° (wide) and 1.2° x 0.9°. Gain control is automatic or manual.
Eye-safe laser rangefinder (optional): 1.54 micron laser accurate
to +/- 5m out to 20 km capable of 10 pulses per minute in 1 pps
bursts. Turret Weight: 38 kg. Control unit Weight: 4.5 kg.
Joystick Weight: 1.5 kg. Dimensions: 400 mm diameter x 570
mm high. Temperature limits: -20° to +50°C. Vibration
Endurance: 2.5 g RMS, 5 to 2,000 Hz. Electrical Interface:
voltage is 28 VDC, power consumption is 200 W, video output is
CCIR or RS-170. Options: colour CCD, intensified CCD, laser
rangefinder (eye-safe or non eye-safe), 35x continuous optical
IR zoom lens for InSb thermal imager, GPS interface, 1553
databus interface, lower operating temperatures.
STAMP Mini Payloads
FOX-450Z and FOX-450ZE Thermal Cameras
Stabilised miniature payload for use on board small UAVs,
VTOLs, small manned aircraft, aerostats and balloons, manned
and unmanned ground and maritime vehicles. Payload
configurations including Gyro mechanical stabilization sub
system, CCD camera for day-time use, or Uncooled IR camera,
or Low Light Level CCD for night-time operation. Variety of
Mounting options for this compact, lightweight mini payload.
Modes of Operation: Control in ‘observation mode’ is via joystick
rate command, ‘point-to-coordinate’, ‘target tracking’ and
optional ‘scan’ modes. Stabilised platform: three(3) gimbals
mechanical Gyro stabilising the payload with a pointing
accuracy of 1° relative to platform. Field of regard: +70 to -40°
in pitch, in roll//yaw +/- 170 °. Sensors configurations: a)¼ inch
high-resolution colour CCD TV camera with x10 continuous
optical zoom lens offering 48x38° (widest) and 5.2x4.2°
(narrowest) fields of view and up to x4 electronic zoom and
NTSC or PAL output. B) Uncooled IR camera for night-time
operation with continuous optical zoom lens. Weight: from 750
g. Dimensions: Mounting 4”, diameter 125 mm, height 160 mm.
Temperature limits: -10 to +45°C. Altitude: limited by vehicle.
Electrical Interface: 24 and 12 VDC, 9W. Comms Interface:
RS232 standard, RS422 optional. Options: Inertial Navigational
System, GPS, high resolution panoramic scan and panoramic
picture display mode, alternative mountings, wide roll angular
dynamic range.
Thermal imaging cameras with continuous zoom lens. Main
Features: high quality IR picture for night and day use; unique IR
continuous zoom lens; 3rd generation InSb FPA (320 x 256
pixels) standard; highly sensitive in the 3-5 micron spectral
range; operating with proprietary high power continuous optical
zoom lenses; auto-focus through zoom; analogue (CCIR/RS170)
or 14 bit digital output. Special software for image
enchancement and unique algorithms. Options: fixed CG
through zoom, micro scanning for improved resolution, other
FPA formats. Video from Fox family cameras video can be seen
on a remote monitor and are operated by an external control
panel or by means of an RS422A communication channel. The
cameras can be supplied with an enclosure (FOX-450ZE) or
without an enclosure (FOX-450Z). Sensor Type: MWIR InSb 3rd
Gen FPA. Spectral Range: 3-5 microns. Number of pixels:
320x256. Lens Type: continuous optical zoom. WFOV to NFOV /
Max Magnification: 27º x 20.2º to 1.2º x 0.9º / X22.5 (FOX-450Z
and FOX-450ZE). 2-axis scan: optional for 450Z/ZE. Zoom
change: remotely controlled. Focus: automatic adjustment
through zoom. Focus adjustment: remotely controlled.
Uniformity calibration: internal or external 1 or 2 points. Video
format: CCIR or RS-170 or 14 BIT digital. Cooling: closed-cycle
Stirling cooler. Cooldown time: 8 minutes (nominal).
Communication: RS-422A. Polarity: black or white hot. Gain/
level control: automatic or manual or local AGC™. Reports:
zoom position, calibration and BIT status. Power requirements:
28VDC, 30 Watt (nominal). Weight: 4.9 kg (FOX-450Z), 10.5 kg
(FOX-450ZE). Dimensions in mm, W x H x L: 148 x 213 x 243
(FOX-450Z), 184 x 243 x 292 (FOX-450ZE).
FOX-250Z and FOX-250ZE Thermal Cameras
Thermal imaging cameras with continuous zoom lens. Main
Features: high quality IR picture for night and day use; unique IR
continuous zoom lens; 3rd generation InSb FPA (320 x 256
pixels) standard; highly sensitive in the 3-5 micron spectral
range; operating with proprietary high power continuous optical
zoom lenses; auto-focus through zoom; analogue (CCIR/RS170)
or 14 bit digital output. Special software for image
enchancement and unique algorithms. Options: fixed CG
through zoom, micro scanning for improved resolution, other
FPA formats. Video from Fox family cameras video can be seen
on a remote monitor and are operated by an external control
panel or by means of an RS422A communication channel. The
cameras can be supplied with an enclosure (FOX-250ZE) or
without an enclosure (FOX-250Z). Sensor Type: MWIR InSb 3rd
Gen FPA. Spectral Range: 3-5 microns. Number of pixels:
320x256. Lens Type: continuous optical zoom. WFOV to NFOV /
Max Magnification: 27º x 20.2º to 2.2º x 1.7º / X12.5 (FOX-250Z
and FOX-250ZE). Zoom change: remotely controlled. Focus:
automatic adjustment through zoom. Focus adjustment:
remotely controlled. Uniformity calibration: internal or external 1
or 2 points. Video format: CCIR or RS-170 or 14 BIT digital.
Cooling: closed-cycle Stirling cooler. Cooldown time: 8 minutes
(nominal). Communication: RS-422A. Polarity: black or white
hot. Gain/level control: automatic or manual or local AGC™.
Reports: zoom position, calibration and BIT status. Power
requirements: 28VDC, 30 Watt (nominal). Weight: 2.5 kg
(FOX-250Z), 5.5 kg (FOX-250ZE). Dimensions in mm, W x H x L:
95 x 110 x 240 (FOX-250Z), 150 x 147 x 367 (FOX-250ZE).
FOX-720Z and FOX720ZE Thermal Cameras
Thermal imaging cameras with continuous zoom lens. Main
Features: high quality IR picture for night and day use; unique IR
continuous zoom lens; 3rd generation InSb FPA (320 x 256
pixels) standard; highly sensitive in the 3-5 micron spectral
range; operating with proprietary high power continuous optical
zoom lenses; auto-focus through zoom; analogue (CCIR/RS170)
or 14 bit digital output. Special software for image
enchancement and unique algorithms. Options: fixed CG
through zoom, micro scanning for improved resolution, other
FPA formats. Video from Fox family cameras video can be seen
on a remote monitor and are operated by an external control
panel or by means of an RS422A communication channel. The
cameras can be supplied with an enclosure (FOX-720ZE) or
without an enclosure (FOX-720Z). Sensor Type: MWIR InSb 3rd
Gen FPA. Spectral Range: 3-5 microns. Number of pixels:
320x256. Lens Type: continuous optical zoom. WFOV to NFOV /
Max Magnification: 27º x 20.2º to 0.76º x 0.59º / X36
(FOX-720Z and FOX-720ZE). 2-axis scan: optional for FOX-720Z
and FOX-720ZE. Zoom change: remotely controlled. Focus:
automatic adjustment through zoom. Focus adjustment:
remotely controlled. Uniformity calibration: internal or external 1
or 2 points. Video format: CCIR or RS-170 or 14 BIT digital.
Cooling: closed-cycle Stirling cooler. Cooldown time: 8 minutes
(nominal). Communication: RS-422A. Polarity: black or white
hot. Gain/level control: automatic or manual or local AGC™.
Reports: zoom position, calibration and BIT status. Power
requirements: 28VDC, 30 Watt (nominal). Weight: 4.9 kg
(FOX-720Z), 10.5 kg (FOX-720ZE). Dimensions in mm, W x H x L:
148 x 213 x 243 (FOX-720Z), 184 x 243 x 292 (FOX-720ZE).
visit us at www.shephard.co.uk
SHEPHARD
43
LAW » Electro-optical pods
CEDAR
Electro-optical “radar” panoramic intruder detection system
which automatically detects moving targets in motion in a wide
panoramic view. Panoramic IR scan and panoramic IR image
display. Field of regard: horizontal: ± 160°, vertical: ± 25°.
Angular Velocity: up to 1 rad/sec. Thermal Sensor: InSb, 3-5 µm.
Image format: 320 x 240. Optics: Continuous Zoom Lens from
WFOV: 27° x 21 to NFOV 2.2° x 1.6°. Laser rangefinder (option):
Wavelength: 1.54 µm (Eyesafe) Range: 10,000 m. Range
accuracy: ±5 m. Weight (Pan & Tilt unit): 13 kg. Dimensions:
400H x 380W x 250 D mm.
SPIDER
The Stabilised Panoramic Automatic Intruder Detection and
Recognition (SPIDER) system is a sophisticated wide area,
passive, real time, electro-optical system which automatically
detects motion in a wide panoramic view and may be installed
on a mobile platform and/or high mast. It incorporates a
Thermal Imaging Camera with a 22. 5x zoom lens, a Daylight TV
Camera and an Eyesafe Laser Rangefinder. Field of regard:
Horizontal: 360° x n (continuous), Vertical: ±40° (nominal).
Angular Velocity: Up to 1rad/sec. Scanning Sector: Up to 360°.
Dimensions: 617mm (w), 607mm (h), 325mm (d). Weight:
Gimbal assembly: 28 kg, Optronic payload: 17 kg.
FPD-1
High-brightness, flat-panel display developed for helicopters and
fixed-wing aircraft that can also be used in marine and ground
applications. Ruggedised to Mil Std 810. Screen: flat panel
colour LCD 26.4 cm (10.4 in) across the diagonal. Resolution:
640 x 480 pixels. Brightness: 1,000 cd/m2. Voltage supply: 18
to 32 VDC. Video inputs: PAL, NTSC. Options: 800 x 600
resolution, serial communication links, other monitor sizes, Y/C
or VGA video inputs.
FPD-2
NVG-compatible, high-brightness, flat-panel display developed
for helicopters and fixed-wing aircraft that can also be used in
marine and ground applications. Ruggedised to Mil Std 810.
Screen: LCD active matrix (TFT) 21.4 cm (8.4 in) across the
diagonal. Resolution: 800 x 600 pixels. Brightness: 1,400 cd/
m2. Voltage supply: 18 to 32 VDC. Video inputs: composite PAL
or composite NTSC. Options: serial communication links, other
monitor sizes, Y/C or Super VGA video inputs, high altitude
6,096 m (20,000 ft), customised mounting.
» CARL ZEISS OPTRONICS (FORMERLY DENEL
OPTRONICS)
LEO-II A1/A2/A3/A5
Gyro-stabilised platform containing a thermal imager and TV
camera for police, paramilitary, SAR and civil/military
applications Stabilised platform: Diameter 400 mm, 2-axis
stabilisation to less than 12 microradians RMS Field of regard: n
x 360 deg in azimuth, +20 deg to -100 deg in elevation Thermal
imager: Agema 8-12 micron thermal imager with dual 20 deg/5
deg lens (or dual 12 deg/3 deg lens on LEO-II A2), 8x zoom and
pseudo colour isotherm alarms (A3 is fitted with 3-5 micron FPA
FLIR, with 18 deg and 3 deg FoVs) TV camera: 3-CCD broadcast
colour TV camera with 32x zoom (extended daytime operation
to 0.002 lux on A3) Mass complete: 35 kg (77 lb) (basic system)
Options: GPS interface, (search radar interface for A3)
44
Public Service Aviation Handbook 2008-09
embedded video autotracker, microwave downlinks, aircraft
mounting kits. A5 features a latest generation QWIP thermal
imaging sensor, 3-CCD 38x zoom TV, plus either a spot TV (0.35
deg FoV) or a laser rangefinder
» FLIR SYSTEMS INC
BRITE Star DP
Offers a field-of-view to match any mission, providing excellent
situational awareness and the greatest stand-off range in its
class. Enhances daylight missions and target identification;
maintains operator orientation when switching between
sensors. Offers continuous duty cycle, high reliability, and
long-range performance; compatible with US and NATO
laser-guided munitions, including Hellfire missiles. Provides an
air-to-ground tactical advantage. Reduces preflight prep, allows
for fast switching between aircraft, and allows the system to be
boresighted by the operator at any time. Reduces workload and
facilitates target hand-off. Supports precision pointing and
delivers smooth steering at extreme zoom levels. Reduces
operator workload. FLIR controls the critical technology inside
every Star class gimbal ensuring the fastest service and
worldwide support, 4 field-of-view (FOV), large format thermal
imager, 3 FOV, high-resolution, 3-chip colour daylight camera
with monochrome mode and matched fields of view to the
thermal imager. Diode Pumped Laser Designator/Rangefinder
(DPLDR). Laser pointer (LP). Automatic in-flight boresighting
capability. Laser spot tracker (LST) option. Internal
Measurement Unit (IMU) and navigation processor inside.
Automatic target tracker.
Star SAFIRE HD
Complete digital architecture provides maximum image clarity,
precise system control, and a flexible upgrade path Megapixel
resolution significantly improves scene detail and increases
identification range High-magnification optics extend detection
range to the horizon without sacrificing wide FOV situational
awareness. Patented electro-mechanical design keeps payloads
stable for clear viewing during extreme aircraft manoeuvres.
Direct digital connection enables long-distance remote control
and preserves the high-definition imagery critical for detailed
viewing and post-processing. Analogue video installations will
benefit from the HD’s high-resolution digital sensors and
high-quality optics. View and track ground locations using the
fully-embedded IMU; follow moving targets with the multi-mode
Autotracker. Covertly illuminate wide areas, point out distant
targets to other forces, and determine target distance and
location. Total cable compatibility allows operators to upgrade
existing .SAFIRE-family installations to High-Definition with
plug-and-play. Simplicity. All-weather design is qualified to the
most demanding requirements of MIL-STD-810 & 461. All digital
performance, High-definition IR, colour, and low-light cameras:
120x zoom ratio 5 micro-radian stability, Fibre optic or
SMPTE-292M.
LAW » Electro-optical pods
Electro-optical pods « LAW
Star SAFIRE III
SeaFLIR III
Can be used in applications as diverse as land force protection,
shipboard open ocean and littoral patrol, and long-range
airborne reconnaissance. Extends identification range
performance by providing maximum detail from covert stand-off
distances. All cameras feature multiple FOV’s maintaining
situational awareness while also achieving long range
performance and enabling. Image Blending. Brings true all day /
all night capability in multiple wavebands, and forms the basis
for Image Blending. Combine critical spectral information from
IR imager with Image Intensified. Low-Light camera or
long-range Spotter Scope. High MTBF and proven combat
survivability in demanding arctic and desert environments. View
and track ground locations using the fully-embedded IMU; follow
moving targets with the multi-mode. Autotracker. Covertly
illuminate wide areas, point out distant targets to other forces,
and determine target distance and location. Total cable
compatibility allows operators to upgrade existing SAFIRE family
installations with plug-and-play simplicity. All-weather design is
qualified to the most demanding requirements of MIL-STD-810 &
461. Multi-mission capable. High-resolution colour spotter scope.
Matched multi-FOV optics. Image Intensified lowlight camera.
Image blending. Reliable 24/7 operation. Optimized usability.
Multiple laser payloads. Maintain SAFIRE-family compatibility.
Commercially developed/MIL qualified.
Powerful, sensitive thermal imaging delivers crisp imagery
through total darkness and most obscurants with detection
capability beyond 10km. Assists in reading ship registration
numbers and multitude of daytime surveillance missions. The
low-light camera allows operation into dawn and dusk, and can
see the laser pointer. Eye-safe laser rangefinder works in
conjunction with GPS/INS/IMU/DMC to calculate target lat/long,
elevation, range and bearing. Provides stable imagery in rough
seas, or on aircraft in flight, critical for long-range imaging.
Allows operator to “lock” onto targets and reduces fatiguecritical for long missions. Optional laser pinpoints targets for
observers using night vision equipment, while remaining
invisible to others. Engineered to withstand the harsh conditions
of maritime and military environments. SeaFLIR III incorporates
a comprehensive BIT which confirms operation of critical
functions and performs fault isolation to simplify logistics.
SeaFLIR III can communicate with a variety of command and
control systems, GPS /INS/IMU devices, radar, moving map and
searchlight systems for improved mission effectiveness. Support
of both output types maximizes compatibility with platform
monitors and recording devices. Digital capability optimizes
video resolution and provides greater data transmission/
manipulation flexibility. Mid or large format midwave IR with up
to 450mm of continuous zoom. Daylight/Low-light TV with 40x
zoom. Precision target geopositioning. Gyro stabilization.
Multi-mode autotracker. Laser pointer. Rugged marinizationexceeds Mil-standards. Built in test (BIT). Flexible integration
capability. Digital and analogue video outputs
Star SAFIRE QWIP
Complete digital architecture provides maximum image clarity,
precise system control, and a flexible upgrade path. Provides
crisp imagery through total darkness, fog, smoke, dust and
many other obscurants. 1280x720 resolution significantly
improves scene detail and increases identification range.
High-magnification optics extend detection range to the
horizon without sacrificing wide FOV situational awareness.
Patented electro-mechanical design keeps payloads stable for
clear viewing during extreme aircraft manoeuvres. Direct digital
connection enables long-distance remote control and preserves
the high-definition imagery critical for detailed viewing and
post-processing. Analogue video installations will benefit from
HD’s high-resolution digital sensors and high-quality optics.
View and track ground locations using the fully-embedded IMU;
follow moving targets with the multi-mode Autotracker.
Covertly illuminate wide areas, point out distant targets to
other forces, and determine target distance and location. Total
cable compatibility allows operators to upgrade existing
SAFIRE-family installations to High-Definition with plug-andplay simplicity. All-weather design is qualified to the most
demanding requirements of MIL-STD-810 & 461. All digital
performance. Long-wave QWIP thermal imager. High-definition
IR, Colour, and low-light cameras. Long-range telescopes 5
micro-radian stability. Fibre optic or SMPTE-292M. Enhanced
standard definition video. Optimized usability. Multiple laser
payloads. Maintain SAFIRE-family compatibility. Commercially
developed/MIL qualified.
46
Public Service Aviation Handbook 2008-09
SeaFLIR II
Powerful, sensitive thermal imager detects targets at distances
greater than 10km and delivers crisp imagery in total darkness
and through heavy atmospheric obscurants. The daylight TV
imager can be used in a variety of surveillance roles, as well as
having a low-light capability that extends its utility well into the
twilight hours. Provides stable imagery in rough seas, or on
aircraft in flight – critical for long range imaging. Allows
operator to “lock” onto targets and reduces fatigue on long
missions. Optional laser pinpoints targets for observers using
night vision equipment while remaining invisible to others.
Engineered to withstand the harsh maritime environments
encountered by military operators, SeaFLIR II can communicate
with a variety of command and control systems including GPS
receivers, radars, moving map and searchlight systems for
expanded mission effectiveness. Mid-wave IR with up to 450
mm of continuous zoom. Daylight/Lowlight TV with 40x zoom.
Gyro-stabilization. Multi-mode autotracker. Laser pointer.
Rugged marinization – exceeds Mil-standards. Flexible
integration capability.
TALON
Can be installed on wide range of platforms with low profile and
low drag. The most payloads available in a system of this type:
infrared, CCD-TV, low light EMCCD-TV, Laser Rangefinder, Laser
Pointer or Laser Illuminator, IMU. Large format, 640 x 480
infrared camera with 10x continuous optical zoom (18x overall),
plus continuous optical zoom color CCD and low-light EMCCD
cameras deliver crisp, detailed images day or night. Talon
provides SMPTE digital video for all channels, ensuring the
highest image fidelity and resolution. Analogue video outputs
also provided. Embedded, self-contained capability that provides
target geolocation, geo-pointing and full tactical targeting
coordination. Stealth capabilities that pinpoint targets and
illuminate scenes for observers using night vision equipment
and maximize sensor performance in extreme low-light
conditions. Talon’s program-based pedigree for reliable
operation in extreme environments is unsurpassed, with
beyond-MIL SPEC environmental design. Compact, light weight.
Penta-sensor configuration. State-of-the-art imaging. Digital and
analogue video. Embedded IMU and LRF Laser Pointer or
Illuminator. Military qualified and field proven.
Ultra8500
Compact 23 cm (9 in) military-qualified, stabilised turret with
triple-payload capability. Optimised for light to medium fixed
and rotary wing aircraft operation, it includes a high resolution
GEN III thermal imager with auto focus and continuous zoom IR
lens (Focal length: 25-250 mm), a colour CCDTV with Autofocus
and lowlight TV mode, and an optional IR laser pointer. The
system provides real-time automatic image optimisation, an
embedded multi-mode autotracker, and an intuitive, icon-based
colour graphical overlay. Designed for law enforcement, search
and rescue, and surveillance missions, it provides powerful
imaging capabilities in a small and lightweight (29 lb) gimbal
package. Thermal imager: 320 x 240 InSb FPA 3-5 µm. IR
Continuous zoom Telescope with 10x magnification; Field of
View Range: 22º x 16.5º (WFOV) to 2.2º x 1.65º (NFOV); PAL or
NTSC Video Output. IFOV: 0.12 milliradians (NFOV) TV: 752 H x
582 V (PAL) 768 x 494 (NTSC) Continuous zoom Telescope with
18x magnification and integral 4x electronic zoom; Maximum
Magnification: 72x Field of View Range: 48 deg x 32 deg
(WFOV) to 2.7 deg x 2.2 deg (0.67deg x 0.55 deg using E-Zoom)
(NFOV) Low Light Mode: Operational down to 0.2 Lux.
Resolution: 460 TV Lines (PAL), 470 TV Lines (NTSC) Laser
Pointer: visible with night vision goggles. Optional features: RS
422/232, ARINC interface, RS-232 serial GPS interface, Search
Light Slave (SLASS) interface, PIP monitor, Terse Binary
Protocol (TBP) for Remote and UAV control functions, compact
electronics control box for UAV applications
UltraForce 275
Reduces weight for increased mission range. Large format 640
x 512 infrared camera allows for positive target analysis at safe
stand-off ranges in all weather conditions. Maximises stand-off
range and target acquisition during daytime surveillance
missions, the low light function extends operation into dawn or
dusk. Provides stable imagery by compensating for aircraft
movement and vibration critical for long-range imaging. The
system can be delivered with EASA Form 1 certification. Single
LRU configuration, embedded digital communication for remote
control of gimbal and sensors. FLIR controls the entire supply
chain for the critical technology inside its Ultra class gimbals,
ensuring fast service and long-term support. Lightweight high
stiffness composite body. Multiple FOV’s thermal imagers.
Daylight colour camera with 26x zoom. Four axis active
stabilisation. EASA Certified installations. UAV applications.
UltraForce 350
Reduces weight for increased mission range. Large format 640
x 512 infrared camera allows for positive target analysis at safe
stand-off ranges in all weather conditions. Maximises stand-off
range and target acquisition during daytime surveillance
missions; the low light function extends operations into dawn or
dusk. Provides stable imagery by compensating for aircraft
movement and vibration, critical for long range imaging. The
system can be delivered with EASA from 1 certification. FLIR
controls the entire supply chain for the critical technology
inside its Ultra class gimbals, ensuring fast service and
long-term support. Lightweight high stiffness composite body.
Multiple FOV’s, thermal imagers. Daylight colour camera with
26x zoom. 4 axis active stabilisation. EASA Certified
installations.
» GALILEO AVIONICA SPA
GALIFLIR ASTRO
Application: Police/paramilitary Military standard surveillance
and remote observation FLIR installed on a four-axis
gyro-stabilised platform. The wide FoV is used for detection, the
narrow one for identification of targets TV: Optional colour
daylight or low light level TV Weight complete basic system:
49.5 kg (109 lb) Options: Video tracker
» GYROCAM SYSTEMS, INC
GYROCAM DNV (DAY/NIGHT VISION)
A long lens, high altitude surveillance system that combines a
three-chip high resolution colour camera with NextGen
NightVision. The infrared laser illuminator allows covert
surveillance in no light conditions. Invisible to the unaided eye,
the laser acts as a searchlight with NightVision optics, providing
illumination from 914 m (3000 ft). The camera produces 800
lines of horizontal resolution and the NextGen NightVision
optics has a low light lux rating of .00001. Both colour and
NightVision video can be viewed simultaneously.
GYROCAM HD CAMERA SYSTEM
High-definition colour camera system fully integrated with
1000-line HD camera and Fujinon zoom lens with 2 x extender
yielding over 1000 lines of resolution. System can be outfitted
with a variety of lens and colour camera options. Fully
integrated package with built-in down converter, which converts
HDTV signal into NTSC or PAL and provides three simultaneous
outputs.
GYROCAM IR (DUAL SENSOR IR/COLOUR)
The dual sensor features a thermal imager in addition to the
daylight colour camera. Specifications for platform, thermal
imager and daylight colour camera: as per the Triple Sensor
(over).
GYROCAM MP (MARINE PATROL SURVEILLANCE
SYSTEM)
The same gyrostabilised technology used on helicopters and
aeroplanes is now available for marine patrol units, providing
steady pictures even in the roughest seas. The GyroCam MP is a
valuable resource in navigation, search and rescue and harbour
security and surveillance. Any one of our GyroCam Systems can
be manufactured into a Marine Patrol System.
visit us at www.shephard.co.uk
SHEPHARD
47
LAW » Electro-optical pods
GYROCAM TS (TRIPLE SENSOR)
MiniPOP
A multi-mission camera system that combines high resolution
colour, NextGen NightVision (with a laser illuminator), advanced
thermal imaging and a laser range finder in a single, lightweight
gimbal. The heart of the Gyrocam TS is our patent pending optics
system that allows one lens to be utilized for both the
NightVision and colour camera. The NextGen NightVision optics
has a low light lux rating of .00001 and the high resolution colour
camera produces 800 lines of resolution. In addition, the
integrated 3-5 micron thermal imager offers a 1.7 to 20 cm (0.6-8
in) optical lens or an optional 6 to 40 cm (2.4-16 in) optical lens.
Miniaturized dual axis, gyro-stabilized payload. The system is
built on a one line replaceable unit (LRU) open architecture and
carries a variety of sensors. The payload has a continuous zoom
colour day camera, a thermal imaging camera and a laser
pointer. An automatic television tracker can also be installed.
Size: 21 cm (8 in) Weight: 6-7 kg (13-15 lb) dependent upon
specifications Field of regard: Elevation: +40 deg to -110 deg,
Azimuth: n X 360 deg Thermal imager: InSb 3-5 micron, 2
Fields of View (FOV) or continuous zoom Day Colour Camera:
CCD with Near IR (NIR) capability, zoom x 22.5, Fields of View 2
deg- 45 deg Laser Pointer (optional): Applications: Day and
night observation and surveillance on board small aircraft and
helicopters for SAR, law enforcement and crime prevention
» TAMAM DIVISION – IAI
HELICOPTER MULTI-MISSION OPTRONIC
STABILISED PAYLOAD (HMOSP)
Very small dual axis gyro-stabilized payload is built on a one line
replaceable unit (LRU) carrying a single sensor that can be
switched in minutes. Sensors contain either a “day” continuous
zoom color camera or a “night” uncooled thermal imaging
camera. Dimensions: Diameter 10 cm (4 in), Height 17 cm (6.8
in) Weight: 1 kg (2.2 lb) Thermal imager: Uncooled 8-12 µm, 320
x 240 pixels, 1 FOV of 7 deg (option for 2 Fields of View) Day
Colour Camera: Continuous zoom x 10 (4 deg to 46 deg)
Applications: Day and night observation and surveillance on
very small airborne platforms for law enforcement and crime
prevention, crowd monitoring and forest fire detection
POP 200
MX SERIES
Plug-in Optronic Payload (POP) carries sensors in field
interchangeable slice Turret Dimensions: Diameter 26 cm (10
in), height 38 cm (14 in), weight 14-16 kg (30-35 lb) depending on
sensor type Sensor slices: 3-5 micron focal plane array (FPA) IR
and colour CCD TV; IR FPA & LRF IR sensors: Narrow FoV of 5
deg x 3.7 deg and wide FoV of 25 deg x 18.7 deg. POP 100 has
narrow FoV of 1.7 deg x 1.3 deg and wide FoV of 22 deg x 16 deg.
3-5 micron InSb sensors TV cameras: Colour with continuous
zoom lenses Automatic Video tracker Video output: PAL or
NTSC. Built-in test Power: 120 W @ 28 VDC to Mil Std 704D
Interface: RS-422 Accessories: Monitor, VCR, datalink, hand
control unit Applications: Day and night observation and
surveillance, SAR, law enforcement and crime prevention, crowd
monitoring, smuggling interdiction, fishery patrol, forest fire
detection, power cable surveillance.
WESCAM’s MX-Series™ is the industry’s only modular family of
gyro-stabilized turreted EO/IR/Laser surveillance systems.
Addressing mission requirements, program cost targets and
aircraft installation constraints, the MX-15i, MX-15 True HD,
MX-20, and MX-20 True HD surveillance turrets incorporate
superior gyro-stabilization, advanced EO/IR technology, and
precision optics to provide high-performance visual intelligence
from and airborne and ground-based platforms. Continuing with
aggressive research, development, and investment, WESCAM
maintains its position at the forefront of the imaging market by
incorporating leading performance features into the MX-Series
line of imaging turrets.
Advanced Plug-in Optronic Payload (POP) carries sensors in field
interchangeable slice Turret Dimensions: Diameter 26 cm (10.2 in),
height 38 cm (15 in), weight 15-16 kg (33-35 lb) depending on sensor
type Sensor slices: Large Format Focal plane array (FPA) IR and
colour CCD TV with Laser pointer; Large Format 3-5 micron FPA IR
and colour CCD TV with LRF IR sensors: Narrow FoV of 2.35 deg x
1.7 deg and wide FoV of 29 deg x 22 deg. TV cameras: Colour, with
Near IR capability and continuous zoom lenses Automatic Video
tracker Video output: PAL or NTSC. Built-in test Power: 120 W @ 28
VDC to Mil Std 704D Interface: RS-422 Accessories: Monitor, VCR,
datalink, hand control unit Applications: Day and night
observation and surveillance, SAR, law enforcement and crime
prevention, crowd monitoring, smuggling interdiction, fishery
patrol, forest fire detection, power cable surveillance
48
Public Service Aviation Handbook 2008-09
AGUSTA A109K2
HS-29700
EUROCOPTER AS-350B3
AGUSTA BELL 212/412
HS-20200
AGUSTA BELL AB139
MDHI MD902
HS-20200
AGUSTAWESTLAND 109E
SIKORSKY CH53
HS-10300
BOEING CH 46/47
AGUSTAWESTLAND EH-101
HS-10300
EUROCOPTER AS365(HH65)
SIKORSKY UH-60Q
HS-29900
AGUSTAWESTLAND EH101
MicroPOP
Helicopter optimised family of four-gimbal stabilised EO
payloads. Dual, triple or quadruple sensor configuration for day
and night observation and targeting. Automatic day and night
target tracking. Fixed-focus or zoom optics TV channel: three
colour CCD FLIR channel: 3-5 micron large format FPA (InSb) or
8-12 micron scanning sensors Optics: Up to 900 mm. Additional
channels: Spotter, Laser pointer, Laser rangefinder (LRF) or
Laser designator/rangefinder (LDRF). Diameter 38 cm (15 in),
height 50 cm (20 in), weight 26 to 36 kg (57 to 79 lb) (varies
with sensors carried). Field of regard +15 deg to -105 deg
elevation, n x 360 deg (unlimited) azimuth. Consumes 280 W @
28 VDC Applications: Day and night observation and
surveillance, SAR, CSAR, targeting.
POP 300
BREEZE-EASTERN
» WESCAM (L3 COMMUNICATIONS)
1080p HD Imaging from EO Zoom and
Spotter Payloads WESCAM’s MX-15 and MX-20 1080p True HD turrets are the only
turrets in the industry capable of outputting True 1080p, 720p
and analogue video formats. This sought after feature makes
these turrets compatible with both new and legacy platforms.
Furthermore, the 1080p capability produces longer-range,
higher-resolution and more detail than competitive turrets
offering only 720p HD.
Enhanced Local Area Processing
Providing higher resolution and enhanced imaging performance,
WESCAM’s 1080p HD technology is augmented by Enhanced
Local Area Processing (ELAP). ELAP enables increased standoff
range, improved feature recognition and maximum haze
penetration in long-range surveillance missions.
HELICOPTER RESCUE HOISTS
700 Liberty Avenue, Union NJ 07083, USA
Telephone: (908)686-4000 Fax: (908)686-9292 Web Site: www.breeze-eastern.com
LAW » Electro-optical pods
Microwave links / antennas « LAW
Integrated MCU – 25% lighter
BRIEFCASE RECEIVER
The integrated MCU feature provides an installed weight saving
on rotary-wing platforms of up to 50 lbs. This lightweight EO/IR
imaging is made possible through the integration of, what once
were considered, external control electronics into the top of the
turret.
Fully self-contained microwave video receiver, monitor, antenna,
battery pack, optional tape deck. Frequency Range: 1.7 to 6.5
GHz in bands. Range: Up to 25 miles. Dimensions: 39 x 22 x 14
cm (15.5 x 8.5 x 5.5 in). Power: Internal batteries, 12 VDC vehicle
adapter or AC battery charger. GCA-4 Directional airborne high
gain antenna system that automatically points to receive site
via GPS steering. Frequency: L, S, C bands. Weight: 8 kg (18 lb).
Range: more than 160 km (100 miles) line of sight. Directional
and continuous rotation Antenna Gain: 15 dBi Dimensions: 17 in
diameter x 8 in high Power: 24-32 VDC @ 2 amps (S-Band
specifications typical).
Charge multiplied CCD MX Night spotter &
Laser illuminated Night spotter Together, WESCAM’s Charge multiplied CCD MX Night Spotter &
Laser illuminated Night Spotter create 24/7 EO imaging. The
technology offers a 20% improvement in IR range, compared to
older image intensified technology. With 2 times superior
imaging resolution and greater than 10 times mean-time
between failure, this technology allows for long-range ID in
low-light conditions. A laser illuminated night spotter in the
configuration gives the longest ID range in total darkness - with
4 times the range performance of older-generation illumination
technology.
Digital imaging technology for Zoom and
Spotter Cameras
WESCAM has incorporated state-of-the-art digital imaging
technology for Zoom and Spotter Cameras within MX-Series
turrets. With a megapixel focal plane with 12-bit digitization for
higher resolution & dynamic range, and 12-bit histogram image
processing for enhanced video quality in difficult imaging
conditions, incorporating this technology provides users with
superior performance compared to NTSC & PAL camera
technology.
Improved Digital IR Camera
The Improved Digital IR Camera offered within the MX-Series
boasts superior imaging capability through increased resolution
and uniformity. With a 20% increase in IR range magnification
and resolution, missions unfolding at night or in less than ideal
weather conditions will now result in a higher subject ID success
rate. By integrating an MX-Series Turrets with WISARD™, a
breakthrough series of digital and analogue transmission and
reception equipment, WESCAM provides a complete situational
awareness solution – providing personnel with real-time
intelligence captured from above to support operational
decision-making on the ground.
MICROWAVE LINKS/
ANTENNAS
» BROADCAST MICROWAVE SERVICES INC
BMA-O-SERIES
Omni-directional microwave antennas for data links. Frequency:
L, S, C Bands: 4% to 20% bandwidth Antenna Gain: 2, 6, 9, 11 dBi
BMA-7000
High gain antenna central receive site for long range operation.
Frequency: 1.7 to 7.2 GHz in bands. Range: more than 160 km
(100 miles) line of sight. Directional and continuous rotation.
50
Public Service Aviation Handbook 2008-09
LONG RANGE MICROWAVE VIDEO DOWNLINK
High gain GPS steered aircraft transmit and ground-based
receive sites for microwave video downlinks Frequency: 1 to 13
GHz in bands. Range: more than 160 km (100 miles) line of sight.
Radiation pattern: Directional 15 deg azimuth, 25 deg elevation.
Antenna Gain: 15 dBi Power: 28 VDC amps (S-Band
specifications typical).
MEDIUM RANGE MICROWAVE VIDEO DOWNLINK
Omni to high gain antenna systems with optional GPS steering
on receive site. Frequency: 1 to 13 GHz in bands. Range: 1.6 to
80 km (1 to 50 miles) Radiation pattern: Omni on aircraft, high
gain on receive (S-Band specifications typical).
SHORT RANGE MICROWAVE VIDEO DOWNLINK
Aircraft mounted transmitter with omni antenna and portable
briefcase receive site with omni or patch antenna. Frequency: 1
to 6.5 GHz in bands. Range: 1.6 to 8 km (1 to 5 miles) line of sight.
Omni-directional Antenna Gain: 0 to 6 dBi Power: DC or AC
PORTABLE HAND HELD VIDEO DIGITAL
DOWNLINK
Weighs less than 1.8 kg (4 lbs), provides live video, includes
hi-res colour video monitor. 1.7 to 6.55 GHz in bands, two hour
battery life, up to 8 km (5 miles) coverage. Applications: SAR,
fire, SWAT, crowd control, emergency management.
TAA-101
Skid-mounted antenna actuator deploys omni-directional
antennas below aircraft for 360 deg azimuth coverage. Weight:
2.2 kg (5 lb) Dimensions: 23 x 10 x 5 cm (9 x 4 x 2 in) Power: 28
VDC @ 1 amp. Models available for all aircrafts.
Diversity Receivers
2, 4, and 6-way Diversity Receivers for COFDM Digital Microwave
reception. Simplified operation and installation. Can use a wide
variety and mixture of antennas.
Video Downlinks
High Definition Video Downlinks provide the finest detail to
ground-based units. BMS can provide an all-new digital HD
datalink or assist with retrofitting an existing system.
» ENTERPRISE CONTROL SYSTEMS LTD
MSA5-24L/233-GPS
GPS antenna tracking system Helicopter equipment: GPS video
encoder, Weight: 1 kg (2.2 lb), Dimensions: 15 x 25 x 4 cm (6 x
10 x 2 in) Antenna: 5 sector solid state antenna with integral
LNA and controller, Weight: 3 kg (6.6 lb), Dimensions: 15.5 cm
(6 in) diameter x 65 cm (25 in) long Control rack: 1U x 48 cm (19
in) rack with LCD read-outs of antenna GPS data.
VLR 15-16-1
Video downlink receiver Frequency Range: 2.1 to 2.7 GHz
Sensitivity: -88 dBm Signal to noise ratio: 55 dB typically
Dimensions: 1U x 19 in rack
VLR 31/B10 BRIEFCASE
Portable video receiver with monitor Frequency Range: 2.1 to
2.7 GHz Sensitivity: -87 dBm Display: 26 cm (10.4 in) TFT colour
LCD monitor Battery life: 1.5 hours Weight: 7 kg (15 lb)
Dimensions: 44 x 26 x 17 cm (17 x 10 x 7 in)
VLT 15-10-6
16 channel video transmitter for helicopter downlink use
Frequency Range: 2.31 to 2.47 GHz Weight: 3 kg (6.6 lb) Range:
Typically 48 km (30 miles) @ 304 m (1,000 ft) or 80 km (50 miles)
@ 609 m (2,000 ft Dimensions: 26 x 6.6 x 15 cm (10 x 3 x 6 in)
» MICROWAVE RADIO COMMUNICATIONS (MRC)
MRC GPS AUTO-POD (AIRBORNE)
Auto-tracking selectable array antenna system Frequency
Range: 1.7 GHz to 7.1 GHz Radiation pattern: 45 deg lateral/35
deg vertical Antenna Gain: 11 dBi Range: Up to 200 km+ (124
mile+) dependent on operational requirement Options: Manual/
auto/omni antenna modes, custom airborne system design/
planning/installation/commissioning.
MRC GPS AUTO-POD (GROUND BASED)
Auto-tracking electronically steerable array antenna system (no
moving parts) Frequency Range: 1.7 GHz to 7.1 GHz Radiation
pattern: 25 deg lateral/20 deg vertical Antenna Gain: 16 dBi
Range: Up to 200 km+ (124 mile+) dependent on operational
requirement Options: Manual/auto/omni antenna modes,
customised system design/planning/installation/commissioning
MRC STRATA SERIES (ANALOGUE)
Manually tracking portable receive terminals Frequency Range:
1.7 to 13.5 GHz Radiation patterns: 3 deg to 90 deg directional
options Antenna Gain: Options for 5-36 dBi Range: 1 km to 200
km+ 91.6 to 124 mile+) dependent on operational requirement
Options: Low profile/hand held/parabolic antennas, manual and
autotrack options, lightweight/heavy duty mechanics/portable/
semi-portable configuration
MRC STRATA SERIES (COFDM DIGITAL)
MRC SERIES STRATA
Manually tracking portable analog/COFDM transmitters and
receivers Frequency Range: 2 to 13.5 GHz Radiation patterns:
Omni-directional, mounts directly to Reporter Antenna Gain:
Options for 4-36 dBi Range: 30 m - 200 km+ (98 ft to 31 mile+)
dependent upon operational requirement Options: High power, 1
or 2 Box TX or RX, omnidirectional/low profile/hand held/
parabolic antennas, manual and autotrack options, lightweight/
heavy duty mechanics/portable/semi-portable configuration,
motorcycle transmit and helicopter repeater formats
Diversity Tactical Receiver Case The Diversity Tactical Receiver Case eliminates the distortion
and signal loss found with conventional analogue systems,
which struggle when line of sight communication isn’t possible.
Ideal for terrestrial urban operations, it’s simple to use and
enables you to extend the range of digital downlinks from omni
antenna mounted aircraft without the increased cost and
complexity of GPS tracking antenna systems. Airborne
surveillance applications in need of extended range will
immediately benefit from the portable receiver’s increased
threshold. By using COFDM (Coded Orthogonal Frequency
Division Multiplexing) technology to transmit a compressed
video signal by dividing it up over thousands of different
carriers, the TRC dramatically reduces fade and multipath loss.
And for maximum mission performance, the TRC incorporates
an integrated weatherproof, waterproof 10G shock rated 12” TFT
LCD 700 daylight readable color monitor and a rugged,
military-grade 2590 rechargeable battery. Maximum Ratio
Combining DVB-T COFDM Diversity Receiver with MPEG
Decoder. Compatible with MRC’s HS Series STRATA-HS and
MCR-HS Transmitters. Rugged daylight readable 700 nit TFT
LCD Flat Screen Monitor in NEMA. 6P/IP68 outdoor housing.
-Housed in a MIL-STD 810F Hardigg Storm im2720 Case.
User-friendly simple ergonomic front panel control. Military
grade 2590 Lithium ION rechargeable battery with AC/DC shore
power connectors. -AES 32 Key Decryption: Headphone set for
audio monitoring. Two 3dBi Flexible Omni Antennae included.
DRS6000-HS
Advanced Digital Receiver designed specifically for Public
Sector and Homeland Security Applications: Multiple frequency
receiver that supports: L, S, and C Bands. Additional antenna
inputs support high gain overlapping antenna installations for
maximum system range. Ideal for Mobile Command Van
applications and Airborne Digital Downlink. Strategic Receive
Sites. User friendly ergonomic “real time monitoring “ front
panel control with. programmable “presets”. BISS, BISS-E and
AES 128 bit decryption support with support for 6, 7, & 8. MHz
COFDM pedestals. Maximal Ratio Combining (MaxRC) diversity
receive technology. Compatible with MRC’s HS Series
STRATA-HS, MCR-HS, and DTX Transmitters. Compatible with
both MRC / LINK Block Down Converters
Omnidirectional/manually tracking portable receive terminals
Frequency Range: 1.7 to 13.5 GHz Radiation patterns: 3 deg to
90 deg directional options, 360 deg omnidirectional Antenna
Gain: Options for 5-36 dBi Range: 1 km to 200 km+ (1.6 to 124
mile+) dependent on operational requirement Options:
Omnidirectional/low profile/hand held/parabolic antennas,
manual and autotrack options, lightweight/heavy duty
mechanics/portable/semi-portable configuration
visit us at www.shephard.co.uk
SHEPHARD
51
LAW » Microwave links / antennas
QuikVUE
The smallest handheld COFDM/MPEG receiver/decoder in the
industry, featuring a high resolution 6.4” LCD colour video
screen for active monitoring from a portable transmitter for
reconnaissance and crowd control. Weighing in at mere 6.8lbs.
(3.08kg), and consuming less than 30 watts, the QuikVue HS can
be easily concealed for covert operations and will interface with
standard digital or analogue monitors and recorders for
enhanced operator flexibility. It features independent video, SDI,
and ASI outputs as well as two audio sub-carrier demodulators,
which are accessible via XLR connectors. Furthermore, a 1/4”
headphone jack connector is supplied for operator convenience.
The QuikVue features a vacuum florescent display indicating
receiver carrier level (RCL), menu functions, system status, and
a new feature exclusive to MRC called Link Quality (LQ). LQ
measures signal strength of the COFDM transmission and allows
operators to monitor its “cliff effect”, thereby minimizing the
sudden dropouts associated with digital microwave operations.
Helmet-mounted systems « LAW
» sagem
STERN
» NAVTECH SYSTEMS LTD
A digital video transmission system, based on COFDM encoding.
This technology overcomes the propagation and interference
problems that normally plague outside broadcasts and image
acquisition in difficult environments (urban, hilly, etc.)
Frequency Range: 2.3 to 2.7 GHz and 1.9 to 2.5 GHz in steps of
0.5 Mhz. Frequencies: 9 (programmable). Data rate: 2 to 10
Mbits/s. RF bandwidth: 8 Mhz. Channel encoding: Reed Solomon,
convolutional encoding, special time and frequency interleaving.
Rugged: vibration and shock qualified Transmitter: DVB-ASI
input 75; clock + data input 75; 70 MHz IF output (option);
programmable via RS 232 port; separate 2 to 10 W power
amplifier Power supply: 18/32 VDC, 45 W Dimensions: 31 x 24 x
16 cm (12 x 9.4 x 6.2 in) Weight: <6.5 kg (14.3 lb) Receiver:
DVB-ASI output 75; clock + data output 75; 70 MHz IF input
(option); programmable via RS 232 port; sensitivity -95 dBm
Power supply: 18/32 VDC, 45 W Dimensions: 31 x 24 x 16 cm (12
x 9.4 x 6.2 in) Weight: <7 kg (15 lb)
CAMNAV
» SKYQUEST AVIATION LTD
Synchronised GPS data with video signal to camcorders or
VCRs. Uses audio channel to carry encoded GPS data.
MICROWAVE LINK EQUIPMENT
The latest ‘State of the Art’ digital transmission systems using
MPEG 2, 4 or JPEG2000 compression and modulation
techniques. Receiving systems use multi channel Diversity
Reception for long range links without the use of GPS or
azimuth tracking. Ranges in excess of 160Km (100miles) are
achievable. Low cost COFDM links for security and mobile links
from a variety of host camera systems
Specialist equipment for airborne surveillance missions.
Skyquest supply a wide range of multi-function mission displays,
digital video recorders, video distribution systems and
microwave link systems for airborne surveillance aircraft. The
Skyquest VMS (video management system) is fitted to most UK
Police helicopters and integrates several items of role
equipment into a touch screen man-machine interface. Skyquest
also provide a range of High Definition video displays for use
with the latest generation of HD airborne camera systems.
MOBILE COMMAND POST SYSTEMS
» WESCAM (L3 COMMUNICATIONS)
COFDM Digital Video links
Mobile versions of the MicroSector and multi-channel Diversity
systems, used on command vehicles. Can act as either primary
or secondary receive site. Range: In excess of 75 miles
Frequency: L Band, S Band and C Band.
GPS APPLICATIONS
Bespoke designs of GPS (GNSS) based positioning and location
techniques for a variety of security applications.
GPS COMPASS
GPS derived heading from static or mobile kinematic carrier
phase measurements to yield true heading.
GRAB ‘N’ GO RECEIVE CASE
Rapid deployment video downlink receive system with receiver,
15 cm (10 in) display, video distribution, accepts hand held or
tripod mounted receive antenna. Analogue FM and COFDM
versions Frequency: L Band, S band and C Band.
TELENAV
Invisible GPS encoding of a video signal for precise location of
camera for onward transmission or recording.
TRANSMISSION SYSTEMS
Variety of systems available to suit all applications, both
analogue FM and digital COFDM. Power: Up to 40 dB (10 watts)
Frequency: L Band, S Band and C Band.
52
Public Service Aviation Handbook 2008-09
HELMET-MOUNTED SYSTEMS
AZTRACK ANTENNA AND RECEIVER
A rugged and completely portable digital receiver. It provides a
key component to tactical command centres. The solid state
antenna and tripod is designed to be mounted at a temporary
tactical command site. The 4-sector antenna, includes a built-in
computer, GPS receiver and integral compass. The antenna,
using NAVTRACK data, automatically finds and tracks the
airborne system by activating the sector that is pointing
towards the SkyPOD transmitter.
WISARD
The WISARD (Wireless Information for Situation Awareness and
Real-time Decisions) Hand Held is a rugged, lightweight and
completely portable digital receiver. The 1.9 to 2.7 GHz receiver is
designed to be person-carried or mounted in vehicles, providing
high quality ‘real time’ images. Features include menu driven
controls, operator selected preset channels. In concert with an
encryption capability in the SkyPod, it can be equipped with a
decryption option, ensuring completely secure image transmission.
» AERO SOLUTIONS
AEROVISION
HMD interchangeable with ANVIS NVGs, fits goggle mount on
Gentex helmet for example. High res LCDs can accept up to four
video sources including colour TV and FLIR. See-through display
claimed distortion free. Provides 30 deg FoV for each eye with
100% overlap and focused at 3.3 m (11 ft) to minimise eye strain,
needs no interpupil adjustment and can be worn with glasses.
Light output is NVG compatible so will not interfere with other
crew members’ goggles. Manufacturer says it can replace
instrument panel MFDs. Weight: Less than 226.8 g (8 oz).
Resolution: 180,000 pixels per LCD panel. Power supply: 28
VDC input, 6 VDC output. Power consumption: 2.5 W. Input:
Multi-NTSC channel, field sequential. Video Interface:
Multichannel BNC input.
» CARL ZEISS OPTRONICS
SCOUT
Combines helmet mounted display and observation systems
technologies to provide a cueing and observation system for
application in the police, civil and SAR markets. An optical
helmet tracker, an aiming reticle and a ‘capture’ switch are used
to cue a helicopter observation turret directly towards an area
of interest to provide immediate acquisition and tracking of any
moving or stationary item, significantly reducing the observer’s
workload and acquisition time.
» ELBIT SYSTEMS LTD
ANVIS/HUD
Device that projects flight symbology into night vision goggles.
Selected by US Army (designated AN/AVS-7 and co-produced by
Tracor) and Israeli forces. Allows pilot to fly nap-of-the-earth
missions at night without having to look inside the cockpit.
Operational in more than 10 helicopter types, over 3,000
systems ordered and supplied so far. Features: aiming sight level
resolution, quick mount on any NVG, independent pilot and
copilot/gunner displays, low weight and flexibility (no fibreoptic
cables). Field of view: 34 deg. Display types: Stroke. Resolution:
512 x 512 pixels. Power: 28 VDC, <5 amps, Mil Std 704A.
Interfaces: Mil Std 1553B, ARINC 429m RS 422, analogue,
discrete and synchro. Operating temperature: -32 to +52 deg C.
Environment: Mil Std 810C. NVG compatibility: Mil L 85762A.
MTBF: >1,000 hours.
MIDASH
Modular Integrated Display Advanced Sight Helmet designed to
provide helicopter pilots with binocular imagery, symbology and
head tracking (LOS) for both day and night operation. The
system includes a standard shell helmet with a personal fitting
device, helicopter retained optical units and a vest mounted
unit. A stand alone mode allows operation outside helicopter.
Display is based on two image intensifiers and a single CRT tube
for symbology, both projected on see-through combiners. Well
balanced helmet system with a minimal neck fatigue.
Successfully filed operational on PUMA & Armed BlackHawk.
Night image FOV: 50° x 40°. Daytime FOV: 120° x 70°.
Symbology FOV: 30°. Weight: a total of 2.2 kg (4.8 lb). Eye
relief: 5 cm (1.9 in). Adjustments: none needed prior to flight, all
done once to personal fitting device. Exit pupil: 1.4 cm (0.5 in)
on axis. Symbology readability: readable in 10,000 fc ambient.
M142 Integrated Helmet And Display Sight System
IHADSS is a monocular system used in all current variants of
Apache and Mangusta attack helicopters. CRT based Helmed
Display Unit attaches to the side of the helmet and feeds
pilotage, navigation and weapon aiming symbology and imagery
from the nose-mounted infrared camera to the crewmember’s
left eye via a half mirror optical combiner. Can be coupled to
pilotage and targeting sensors, turret guns and air-to-air missile
seekers. Former Honeywell product supplied by EFW (US
subsidiary of Elbit). With the NVG HUD add-on module, the same
flight information combines the standard Night Vision Goggles
(NVG) displayed for alternate night use as well. US plans call for
IHADSS-21 to upgrade the entire system performance
» ELOP - ELECTRO-OPTICS INDUSTRIES LTD
HELMET MOUNTED DISPLAY DEVICE (HMDD)
HMDD puts symbology within the pilot’s field of view. Head
assembly which can be fitted to ANVIS/6 or similar NVGs with
an adapter. The system contains a miniature display, an optical
sub-assembly and unit that interfaces with the aircraft symbol
generator. Features: Stroke and/or raster type display
compatible with existing display source; adjustable with
NVG-type controls; removable from the helmet; foldable while
on the helmet; compatible with aviator glasses and gas masks;
transferable to allow use of dominant eye. Option: Two HMDDs
can be used together as a binocular display. Field of view:
Horizontal 28 deg, vertical 20 deg. Exit pupil: 1.5 cm (0.6 in).
Eye relief: 2.5 cm (0.9 in). Weight: Helmet mounted element 110
g (0.2 lb) interface unit 290 g (0.4 lb).
» LITEYE MICRODISPLAY SYSTEMS LLC
LITEYE HEAD MOUNTED DISPLAYS
Lightweight displays that can be fitted to flight helmets, combat
helmets, David Clark headsets, hard hats, and even a baseball
cap. The units can also be sold with a stand-alone headset
similar to those used with hands-free phone systems. Designed
to work with NTSC or SVGA signals. Specifications: Liteye is a
800 x 600 pixel, transmissive, OLED, colour sequential display
designed for showing graphics and video. Power is less than
100mW. Liteye HMDs are being utilized in military and industrial
areas world wide.
visit us at www.shephard.co.uk
SHEPHARD
53
LAW » Night vision goggles
NIGHT VISION GOGGLES
» Aselsan
M929/M930 FINE
Aviator’s night vision goggles. Licence-built version of NG Litton
product. Image intensifier: Advanced Gen III, Inverting.
Magnification: 1x. Field of view: 40 deg. Distortion: Less than
4%. Resolution, on Axis (min) 1.28. Photocathode Sensitivity
(min) 2856 K, µA/lm: 1,800. Tube resolution, lp/mm (min): 64.0.
Signal to Noise Ratio (min): 21.0. Brightness Gain @ 2 deg 10-6
fc: 45.000-65.000. Output Brightness @ 1 and 20 fc: 2.0-4.0
» Geophyzika
GEO-NVG-III
Russian Gen 3 goggles said to be in use in Russian helicopters.
Image intensifier: Gen 3 (with gallium arsenide photocathode).
Luminous sensitivity at 2,856 deg K: 1,200 microamps per
lumen. Radiant sensitivity at 830 nanometres: 120 microamps
per Watt. Field of view: 40 deg. Objective lens: 25 mm, F1.1.
Eyepiece lens: 2.5 cm (0.9 in) Eye relief: 4.3 mm. Diopter
adjustment: +/-4. Exit pupil: 10 mm. Ambient light Range: 10-5
to 10 lx. Power supply: 2 AA batteries. Weight: 780 g.
» ITT NIGHT VISION
AN/AVS-6 (F4210)
Spectral response: Visible to 0.90 µm (IR). Field of view: 40
deg. Magnification: Unity. Resolution: 1.3 cy/mr (cycles per
miliradian) minimum. Brightness Gain: 5,500 fl/fl minimum.
Diopter adjustment: +2 to -6 diopters. Interpupillary
adjustment: 51 to 72 mm. Fore and aft adjustment: 27 mm
range. Tilt adjustment: 10 deg minimum. Exit pupil/eye relief
On-axis: 14 mm @ 25 mm distance. Full-field: 6 mm @ 25 mm
distance. Automatic breakaway: 11 to 15 g. Operating
Endurance: Nominally 30 hours under standard conditions.
Batteries: 2 x AA size alkaline. Clip-on power source option
allows hand-held use. Weight of binocular: 590 g maximum
(525 g typical). Operating temperature range: -32 deg C to +52
deg C. Standard mounting: SPH-4B, SPH-4AF, HGU-56P helmets,
Alpha and CGF optional.
AN/AVS-9 (F4949 SERIES)
Spectral response: Visible to 0.90 µm (IR). Field of view: 40
deg nominal. Magnification: Unity. Resolution: 1.30 cy/mr
minimum (1.36 typical). Brightness Gain: 5,500 fl/fl minimum.
Diopter adjustment: minimum range +2.0 to -6.0.
Interpupillary adjustment: Independent, 51 to 72 mm total.
Vertical adjustment: 25 mm range. Fore and aft adjustment:
27 mm range. Tilt adjustment: 10 deg range. Eyepiece exit pupil/
eye relief On-axis: 14 mm @ 25 mm distance. Full-field: 6 mm @
25 mm distance. Automatic breakaway: 11 to 15 g. Batteries:
Fixed wing: 2 x ½ AA size, lithium. Rotary wing: 4 x AA size,
alkaline. Weight of binocular: 550 g (max). Weight of mount:
Fixed wing: 250 grams. Rotary wing: 330 grams. Operating
temperature range: -32 deg C to +52 deg C.
54
Public Service Aviation Handbook 2008-09
Searchlights « LAW
» NEW NOGA LIGHT (2000) LTD
» SAGEM
NL-93 ANVIS GOGGLES
CN2H/CN2H-AA PILOT NIGHT VISION GOGGLES
Aviator goggles for both helicopter and fixed-wing pilots. In
service with Israeli forces and export customers. Available with
a wide range of image tubes. Field of view: 40 deg.
Magnification: 1 +/-5%. Resolution (minimum): 0.77 cy/mr with
36 lp/mm Gen II+ tubes, 0.96 cy/mr with 45 lp/mm Super Gen II
tubes, 1.2 cy/mr with 55 lp/mm XD-4 tubes, 1.3 cy/mr with 64 lp/
mm Gen III tubes. Brightness gain (minimum): 2,200 fl/fl (Gen
II+), 2,600 fl/fl (Super Gen II), 3,200 fl/fl (XD-4), 3,600 fl/fl (Gen
III). Exit pupil: 6mm. Eye relief: 25 mm. Automatic breakaway:
10-15 G. Binocular Weight: = 570 g. Mount Weight: = 150 g.
Power source: AA alkaline or lithium batteries.
CN2H designed for use by helicopter or transport aircraft pilots,
CN2H-AA ejection compatible for fast jets. They can fit a variety
of helmets (Guenau 459, Helmets Ltd Mk 4, Alpha, Gentex SPH4,
SPH5, etc). Image intensifier tubes: SuperGen or Gen 3.
Performance depends on image intensifier tubes. Gain: >2,700
(3rd generation tubes). Gain match: <50%. Resolution: 0.86 cy/
mrad (standard resolution tubes), 1.0 cy/mrad (high resolution
tubes). Fov: 40 deg or 50 deg. Magnification: x1. Weight:
goggles only 550 g (CN2H), 590 g (CN2H-AA), power pack 170 g,
helmet set 190 g. Eye relief: 20 mm. Power supply module:
mounted at the rear of the helmet to balance the goggles, 1.5 V
AA batteries, 3 V or 3.5 V lithium batteries, or aircraft 28 V
supply. An internal filter can be coated on the goggle optics to
ensure compatibility with aircraft lighting.
» OIP SENSOR SYSTEMS
HELIMUN
High performance night vision system for helicopter pilots,
available with 40 deg and super-wide 60 deg field of view.
Features new XD-4 or XR-5 image intensifiers. Magnification:
unity. Resolution: 0.8 mrad/lp or better for 40 deg goggle, 1.1
for 60 deg goggle. Diopter adjustment: -6 to +2 for 40 deg
goggle, -6 to +3 for 60 deg goggle. Interpupil adjustment: 47 to
76 mm. Tilt adjustment: 5 deg minimum. Exit pupil: min. 10 mm.
Eye relief: 25 mm for 40 deg goggle, 19 mm for 60 deg goggle.
Focal Range: 25 cm to infinity. Flip-up/Switch-off. IR LED
incorporated. Minus blue filters. Batteries: 2 x AA alkaline. Can
be adapted to all pilots’ helmets
» PCO SA
PNL-1 AVIATOR’S NIGHT VISION GOGGLES
Polish-manufactured NVGs designed for helicopter aircrew.
Features include full adjustment range for different face shapes,
automatic separation in event of crash, sufficient eye relief to
enable pilot to read instruments underneath. Image intensifier:
Gen II+ or Super Gen. Magnification: 1x. Field of view: min. 38
deg. Diopter adjustment: +2 to -4. Power supply: 3.6V (R6/AA)
lithium battery x 1. Temperature tolerance: -20 deg C to +45 deg
C. Total Weight: 1.5 kg (3.3 lb).
PNL-2/PNL-2A AVIATOR’S NIGHT VISION
GOGGLES
Polish-manufactured NVGs designed for helicopter aircrew.
PNL-2 A is simplified, single-tube version. Features include full
adjustment range for different face shapes, automatic
separation in event of crash, sufficient eye relief to enable pilot
to read instruments underneath. Also marketed for ground use.
Magnification: 0.95x. Field of view: 38 deg. Exit pupil: 8 mm.
Eye relief: 22 mm. Power supply: Lithium battery AA 3.6 V or
2xAA 1.5 V. Endurance: >50 hrs/>100 hrs. Component weights:
goggles 420 g/210 g, mounting 190 g, power supply and
counterweight 615 g/395 g. Total Weight: 1,250 g/1,035 g.
CN2H-AA Mk II PILOT NIGHT VISION GOGGLES
The latest version of the CN2H, designed for use by both
helicopter and aircraft pilots. It can fit a very wide variety of
helmets (OS 458 & 459, Gallet LH 250, Alpha, Gentex HGU-55,
SPH5, ZSh-5, etc). Quick manual disconnecting system. Image
intensifier tubes: Gen 3, XD-4, XR-5 or XH-72. Resolution: >1.36
cy/mrad. Fov: 40 deg. Magnification: x1. Eye relief: 20 mm.
Weight: goggles only 590 g (1.3 lb), power pack 150 g (0.3 lb),
helmet mount 100 g (0.2 lb). Power supply module: mounted at
the rear of the helmet to balance the goggles, 1.5 V AA
batteries, 3 V or 3.5 V lithium batteries, or aircraft 28 V supply.
Cockpit compatibility: internal filters (coating) available.
» VECTOP LTD
NIGHT WITNESS
Debriefing camera integrated into NVG with video output.
Features: No look-through visibility loss. Integrates into left or
right eyepiece of NVG. Easily adaptable to F4949, and most other
NVGs. VCE unit fits standard avionics racks. Stand-alone portable
model available for easy installation to helicopters and other
aircraft with no ejection seat. Quick disconnects on cable. Full
Military standard and SOF approved. Components: 1.2 cm (0.5 in)
CCD detector with sensitivity down to starlight (0.001 Lux);
Multi-prism optic eyepiece; video control and enhancement (VCE)
unit for image processing capability; Cable (up to 6 m/19 ft length)
between the eyepiece and the VCE; ‘Cyclop’ - Optional miniature
day-helmet-camera attaches to the system for day missions.
SEARCHLIGHTS
» BOEING SPECTROLAB
NIGHTSUN II
Lamp type: 1,300 Watt short arc xenon. Peak beam intensity:
30 million candlepower. Beam width: 4 - 20°. Focus control:
bi-directional remote control. Performance: Typical Range: 1 km
(3,300 ft). Target ID Range: 1.6 km (1 mile). Peak illuminance: 32
lux (2.9 ft-cd) @ 1 km. Diameter at 10% of peak illuminance: 70
m @ 1 km (230 ft @ 3,300 ft). Azimuth rotation: 360°
continuous. Elevation Range: +12° to –72° (+/- 3°). Elevation/
azimuth slew rate: 0 - 60° per second. Mechanical specs:
Searchlight/gimbal: max height 60 cm (23.9 in), min height 50
cm (19.4 in), max width 56 cm (22.0 in), min width 30 cm (12 in),
max weight 24.5 kg (54 lb). Junction box: dimensions 15.2 x 17.8
x 12.7 cm (6 x 7 x 5 in), Weight: 2.8 kg (6.1 lb). Hand controller:
dimensions 10.2 x 22.9 x 10.2 cm (4 x 9 x 4 in), weight 0.68 kg
(1.5 lb). Electrical specs: Input voltage: 28 volts nominal
(26.5-29.0 vdc). Input current: 65 amps nominal (75 amps max).
Start time: less than 1 second typical. Recycle time: none
required. Slave-ready for thermal imaging systems using the
RS422 interface. Options/accessories: interface translator kits
- provide slaving communication to non-RS422 thermal imaging
systems. Cyclic or collective controller kits. Dual or parallel
controller kits. Sidecar adapters to fit many Wescam and FSI
hand controllers. Infrared version due soon.
SX-5 STARBURST
Lamp type: 500 Watt short arc xenon. Peak beam intensity: 15
million candlepower (min). Beam width: 2-10° (remote control
focus). Performance: Typical Range: 500 m (1,650 ft). Peak
illuminance at 500 m: 40 lux (3.7 ft-cd). Diameter at 10% of
peak illuminance: 44 m (143 ft) at 500 m. Electrical specs:
Input voltage: 28 vdc nominal. Input current: 25-30 amps. Start
time: 3-5 seconds. Recycle time: none required. Searchlight
power requirements are compatible with standard aircraft type
dc generators. Accessory power converters are available from
other primary power sources from 117-480 vac, 50-400 Hz.
Mechanical specs: Searchlight: cylindrical 190 mm (7.5 in) OD x
460 mm (11.25 in) long, weight 4.5 kg (10.0 lb). Internal cooling
fan with filtered air intake. Lamp max life expectancy 1,000 hrs,
2 years’ operation. Junction box: 21.6 x 15.9 x 13.3 cm (8.5 x 6.25
x 5.25 in), weight 2.9 kg (6.3 lb). Gimbal: two-axis remote
electrical control, weight 3.8 kg (8.5 lb), slew rate 9° per second
standard. Control box: 12.7 cm x 5.7 cm x 4.4 cm (5 x 2.25 x 1.75
in), weight 6 ounces. Total system weight (typical): with
installation, hardware, cable assemblies, 13.6 kg (30 lb).
SX-16 NIGHTSUN
Lamp type: 1,600 Watt short arc xenon. Peak beam intensity:
30 million candlepower. Beam width: 4-20° (remote control
focus). Performance: Typical Range: 1 km (3,300 ft). Useful
range for target ID: 1 mile. Peak illuminance @ 1 km: 32 lux (2.9
ft-cd). Diameter at 10% of peak illuminance: 70 m (230 ft) at 1
km. Electrical specs: Input voltage: 28 volts dc nominal. Input
current: 55-67 amps. Start time: 3-5 seconds. Recycle time:
none required. Mechanical specs: Searchlight: cylindrical 280
mm (11 in) OD x 460 mm (18 in) long, weight 11.4 kg (25 lb).
Internal cooling fan with filtered air intake. Lamp max life
expectancy 1,000 hrs, 2 years’ operation. Junction box:
visit us at www.shephard.co.uk
SHEPHARD
55
LAW » Searchlights
dimensions 26.7 x 15.9 x 14 cm (10.5 x 6.25 x 5.5 in), weight 3.2
kg (7 lb). Gimbal (standard or high air speed) type: two-axis
remote electrical control, weight 4.1 kg (9 lb) or 6.8 kg (15 lb),
slew rate 9° per second standard, others available. Control box:
12.7 x 5.7 x 4.4 cm (5 x 2.25 x 1.75 in), weight 6 ounces. Total
system Weight: typical with installation, hardware, cable
assemblies, 25-30 kg (55-64 lb). Version with in-flight infrared
changeover available.
Voice communications « LAW
OBSTACLE WARNING
SYSTEMS
VOICE COMMUNICATIONS
» ICX (FORMERLY AMPHITECH)
AEROPHONE
OASYS
» LUMINATOR
Radar-based obstacle warning system (OWS) for helicopters.
Transmits thousands of pulses per second through four
multiplexed radar beams at a frequency of 35 GHz. These radar
beams are narrow and the pulses extremely short in duration,
enabling OASYS to detect objects with a very high degree of
resolution. Specifications: antenna 28 cm (11 in). Very low
sidelobes. Scan rate: 150 deg per second. Stabilisation: better
than 0.15 deg in +/- 30 deg (azimuth/elevation) window. Scan
volume: +/- 30 deg (azimuth) x +/- 11 deg (elevation) adaptable
to the speed, flight path and altitude. The scan volume is
centred about the flight vector of the aircraft and not about the
heading axis (above 5 kt), or centred on heading at less than 5
kt. Maximum limit of scan volume: +/- 90 deg (azimuth) -85 deg
to +25 deg (elevation) referenced to mounting. RF power
transmitted: 2.5W (average-maximum). Power consumption @28
VDC: 75 W (standby), 250 W (operating). Range accuracy: 2
metres. System warm-up time: 70 seconds (above -8 deg C) to 5
minutes (at -40 deg C). Operating temperature: -40 deg C to
+60 deg C. Environmental conditions: DO-160B. Software
certification: DO-178B level C. Dimensions: Radar: Height: 39.3
cm (15.48 in). Width: 42.6 cm (16.78 in). Depth: 57 cm (22.4 in).
Control panel: Height: 4.75 cm (1.87 in). Width: 14.6 cm (5.75 in).
Depth: 14.33 cm (5.64 in). Display: Height: 2.03 cm (0.80 in).
Width: 16.8 cm (6.60 in). Depth: 3.6 cm (1.41 in).
DUAL MODE WHITE LIGHT/IR SEARCHLIGHT
» EADS DORNIER GMBH
SX-16P PATROL AIRCRAFT SEARCHLIGHT
Lamp type: 1,600 Watt short arc xenon. Peak beam intensity:
80-100 million candlepower. Beam width: 1-10° (remote control
focus). Performance: Typical Range: 2-4 km (1-2.5 miles). Peak
illuminance: 80 lux at 1 km, 20 lux at 2 km, 5 lux at 4 km.
Diameter at 10% of peak illuminance: 35 m at 1 km, 70 m at 2
km, 140 m at 4 km. Adaptable to pod configured, fixed-wing
aircraft such as Twin Otter, F-27, Bandeirante, S-2 tracker.
Electrical specs: Input voltage: 28 vdc nominal. Input current:
55-67 amps. Start time: 3-5 seconds. Recycle time: none
required. Searchlight power requirements are compatible with
standard aircraft type dc generators. Mechanical specs:
Searchlight: tapered cylinder, 381 mm (15”) OD x 407 mm (16”)
long, weight 13 kg (28 lb). Internal cooling fan with filtered air
intake. Lamp max life expectancy 1,000 hrs, 2 years’ operation.
Junction box: 267 mm x 159 mm x 140 mm (10.5” l x 6.25” w x
5.5” h), weight 3.2 kg (7 lb). Gimbal: two-axis remote electrical
control, weight 6.8 kg (15 lb), slew rate 9° per second, standard.
Control box: 127 mm x 57 mm x 44 mm (5” l x 2.25” w x 1.75” h),
weight 6 ounces. Total system weight (typical): with installation
hardware, cable assemblies, 29.5-31.7 kg (65-70 lb).
Described as the most powerful searchlight on the market
which fits into the MIL-L81174/2B-2 helicopter searchlight
envelope, this product has an HID lamp providing over 3,000
powered hours of white light, 40 times longer than the life of a
standard halogen cycle lamp, says the company. The switching
process from HID to IR mode is instantaneous, says Luminator,
with no down time when switching light sources. The ballast has
an instant start and hot re-strike capability in less than 2
seconds, full light output in 5-10 seconds. The current design fits
the MIL-L81174/2B-2 helicopter searchlight envelope. In addition
to the longer life, the HID/IR LED Dual Mode Searchlight has a
lower power draw on the helicopter than traditional dual mode
searchlights. The HID lamp draws only 55 watts, and the IR LED
draws a mere 20 watts. The circuitry, including motors, draws a
maximum of 100 watts. Every helicopter manufacturer is
concerned with reducing power consumption and weight.
Voltage: 28. Power: 155 Watts max. Approximate initial
maximum candle Power: 7,000.
HELLAS HELICOPTER OBSTACLE WARNING SYSTEM
Imaging eye-safe laser radar (ladar) warning system for
helicopters flying nap-of-the-earth and other low-altitude military
and civil missions. Designed to detect and display obstacles such
as towers, masts, buildings, terrain features and especially wires
and cables at up to 1,000 m (3,280 ft) range. Probability of
detection: > 99.5%. Depending on customer requirements,
warning can be shown on a dedicated indicator (modes: day,
night, NVG) or a helicopter display unit (MFD, HUD, HMSD).
Acoustic alarm sounds if safety threshold ignored by the pilot.
Electrical and mechanical interfaces: ARINC, STANAG, Mil1553.
» AERODATA AG
Airborne voice communication and data transfer at low entry
and operating cost. Provides worldwide communication
capabilities using the Iridium satellite network. Key Features:
Low system installation and operation cost; easy and flexible
operation; capability for full duplex voice and data
communication; direct internet or dial-up data services via PC/
laptop; easy installation into small fixed-wing aircraft and
helicopters; interface to primary aircraft intercom system;
certified according to the National Technical Standards by the
German Airworthiness Authority (Luftfahrt-Bundesamt);
optional interface to Aerodata’s navigation and mission
management system AeroNav, and Aerodata’s fleet
management system.
ACS 300A DUAL AUDIO MIXER PANEL
Full support for pilot and copilot; PTT and hot ICS modes; 5
transmit positions plus PA; 5 receive audio selections;
emergency mode operation; internal interface for non-aircraft
radios; 14 or 28 VDC operation; custom panel legends;
connector installation kit (crimp) included; one-year warranty
Options: ICS support for 6 passengers (2 of 6 will have ICS and
TX support), VOX ICS, NVG lighting; 250 mW power output, 500
mA @ 28 VDC Weight: 0.99 kg (2.2 lb (0.99 kg) Dimensions:
2.62 in high, 6.312 in wide (5.5 in behind face plate), 6,78 in
deep, allow up to 2.5 in for connector and cable clearance.
ACS 300B DUAL AUDIO MIXER PANEL
Specifications as for ACS 300A except for standard VOX mode
in addition to PTT and hot ICS; 6 transmit positions plus PA; 6
Quick Adjust receive audios; options include private ICS bus
Weight: 1.3 kg (2.9 lb).
ACS 700-3 INTERCOM EXPANSION UNIT
» AIR COMM SYSTEMS INC
Specifications as ACS 179 except for OCS and receive audio
support for three passengers (no transmit audio capability).
ACS 1278 SINGLE AUDIO MIXER PANEL
ACS 775 A-SL SINGLE AUDIO MIXER PANEL
Specifications as ACS 2010 except for up to 11 transmit
positions; 13 receive audio selections; standard rather than
optional private ICS bus; toggle switches standard; quick
adjustment optional for receive audios Weight: 2.2 lb (0.99 kg)
Dimensions: 2.6 in high, 5.75 in wide (4.95 in wide behind face
plate) 6.78 in deep.
Specifications as ACS 2010 except for 6 transmit positions plus
PA; 8 receive audio selections; toggle switches instead of Quick
Adjust receive audio controls Weight: 0.68 kg (1.5 lb).
ACS 179 INTERCOM EXPANSION UNIT
ICS and TX support for 2 passengers; compatible with all
AirComm audio panels; compact size - Dzus or remote mount; 14
or 28 VDC operation; connector installation kit (crimp) included;
one-year warranty; approved for use on USFS contracts; 500 mW
power output; 400 mA @ 28 VDC Weight: 0.75 lb (0.34 kg)
Dimensions: 1.875 in high, 5.75 in wide (4.95 in behind face plate),
2.875 in deep, allow 2.5 in for connector and cable clearance.
ACS 2010 SINGLE AUDIO MIXER PANEL
Dzus mounting; PTT and hot ICS modes; 5 transmit positions
plus PA; 5 receive audio selections; Quick Adjust receive audio;
ICS bus/RX audio for passenger expansion; emergency mode
operation; internal interface for non-aircraft radios; 14 or 28 VDC
operation; custom panel legends; colour-coded knobs and toggle
switches; connector installation kit (crimp) included; one-year
warranty; approved for use on USFS contracts; optional VOX;
NVG lighting private ICS bus; circular connector for quick
disconnect; 250 mW power output; 500 mA @ 28 VDC; lighting
MIL-P-7788 Type 3/5 Weight: 1.25 lb (0.56 kg) Dimensions: 1.5 in
high x 5.75 in wide (4.95 in wide behind face plate), 5.031 in deep
(allow 2.5 in for connector and cable clearance).
ACS 775SL SINGLE AUDIO MIXER PANEL
Specifications as ACS 2010 except for toggle switches instead of
Quick Adjust receive audio controls.
ACS PA100D PA/SIREN SYSTEM
Specifications as ACS PA100F except for: 200 W output,
remotely mounted dual amplifier, amplifier weight 6 lb (2.7 kg)
Dimensions: (amplifier) 5.1 in high, 4.9 in wide, 0.68 in deep.
ACS PA100F PA/SIREN SYSTEM
Can be used with any of the external loudspeakers offered by Air
Comm Systems - TS100, TS200Y and CP100V modified; 100 W
output; manual, wail and yelp siren modes; PA and radio
transmission modes; clean, clear audio output; Dzus mounted
control unit; remotely mounted amplifier; 14 or 28 VDC
operation; colour coded knobs and switches; lighting MIL-P-7788
Type 3; connector installation kit (crimp) included; defined
features; 500 mA @ 28 VDC (manual); approved for USFS
contracts; control weight 0.45 kg (1 lb); amp weight 1.58 kg (3.5
lb) Dimensions: (control panel) 1.875 in high, 5.75 in wide (4.95
in behind face plate), 4.55 in deep, allow 2.5 in for connector and
cable clearance, (amplifier) 4.9 in wide, 5.1 in high, 7.5 in deep.
ACS 296 RECEIVE AUDIO INDICATOR PANEL
Compact Dzus mount – 2.8 cm (1.125 in) high; 6 receive audio
LED indicators; LEDs with fresnel lens for max light distribution;
automatic LED dimming using photoelectric cell; 28 VDC
operation; custom panel legends; horizontal or vertical layout;
connector installation kit (crimp) included; lighting - MIL-P-7738
E Type 5, indicators - high efficiency green LED, 5 VDC; one-year
warranty Weight: 0.45 kg (1 lb).
56
Public Service Aviation Handbook 2008-09
visit us at www.shephard.co.uk
SHEPHARD
57
LAW » Voice communications
» HONEYWELL CABIN MANAGEMENT, SYSTEMS
AND SERVICES
M5055 AUDIO CONTROL SYSTEM
Self-contained audio control panel, provides pilot and co-pilot or
observer full control of transmitter, receiver, intercom and
paging functions, amplifier offers automatic levelling on
headphone and speaker, white-tipped buttons select all
functions, colours are available as options, push ‘on’, push ‘off’
switches select receivers, also serve other functions such as
Mask microphone selection and cockpit intercom ‘hot mic’ (on
the mask or boom microphone), cockpit intercom connects the
pilot with the co-pilot or observer, using mask or boom
microphone whenever either crew member selects a transceiver
mike, button marked ‘CABIN’ enables communication between
cockpit and rear cabin passengers and crew, emergency
circuitry allows normal use of transmit and receive functions
with or without power to the system using the cockpit hand
microphone and headset, optionally boom mike can operate in
an emergency mode as UK CAA requires, 27.5 DC, 2 A max
Weight: 3.6 lb (1.63 kg) Dimensions: (panel) 5.75 in wide, 3.37 in
high, (box) 5 in wide, 3.37 in high, 5.475 in deep.
» NORTHERN AIRBORNE TECHNOLOGY LTD
AA95
User customisable with control for up to 6 transceivers with an
individual volume control, support for 5 navaids, separate RX
and ICS volume controls, direct audio input, ICS supports pilot,
co-pilot and four passengers, 3 ICS modes - LIVE, KEYED, VOX,
single VOX level adjustments, high power output 500 mW,
optional tone alert generators, ICS tie line for multi-control
operation; low or high impedance, optional NVG, Dzus mount,
UK CAA and Home Office approved for police applications,
requires 28 VDC, draws 0.25 A Weight: 0.95 kg (2.1 lb)
Dimensions: height 4.7 cm (1.8 in).
AMS43
ICS supports pilot, co-pilot and four passengers; support for 5
transceiver positions plus PA support. Five navaids; separate RX
and ICS volume controls; direct audio input; 3 built-in-alert tone
generators; colour coded toggle switches; 3 ICS modes - LIVE,
KEYED, VOX; VOX level adjustment; Active Noise Filter - ANF for
enhanced noise isolation; high power output 500 mW; ICS tie
line for multi-control operation; emergency mode operation;
available in TSO’d version; Dzus mount; requires 28 VDC, draws
0.25 A Weight: 0.95 kg (2.1 lb) Dimensions: 4.7 cm (1.8 in).
AMS44 MULTI-USER DUAL CHANNEL AUDIO
CONTROLLER
Two audio panels in the space of one; LH or RH pilot
configuration; support for 5 transceiver positions, PA and
navaids; individual RX and ICS volume control; direct audio
inputs; colour coded toggle switches; ICS support pilot, co-pilot
and five passengers; 3 ICS modes - LIVE, KEYED, VOX; single
VOX level adjustment; high power output (400 mW/channel);
ICS tie line for multi-control operation; emergency mode
operation; optional NVG lighting; Dzus mount; needs 28 VDC
power, draws 0.35 A Weight: 1.04 kg (2.3 lb) Dimensions: height
4.7 cm (1.8 in).
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Public Service Aviation Handbook 2008-09
Voice communications « LAW
AMS50 STEREO AUDIO PANEL WITH MARKER BEACON
Full function TSO’d audio panel w/wo built-in Marker Beacon
receiver; 6 place stereo intercom; ALL, CREW, and PILOT ISO
modes; true ‘split com’ operation; expandable; transmit select
with true ‘split’; PTT ICS; Pilot/Crew/All modes; patented
Independent Microphone Circuits (Gating); Active Noise Filtering
(ANF); adjustable music mute; emergency fail-safe. Requires
11-33 VDC; draws 3.0 A max Weight: 0.9 kg (2 lb) Dimensions:
height 3.5 cm (1.38 in).
CC450 RELAY/SIMULCAST CONTROLLER
Compact controller for adding relay and/or simulcast operation
to existing FM transceivers; up to four radios; simple operation;
60 sec voice storage for remote relay operation on same radio;
less than 1 in Dzus height; optional NVG compatible lighting;
requires 28 VDC; draws 0.6 A Weight: 0.5 kg (1.1 lb).
PA/SIRENS
Internal and external applications; auto chime functions;
multiple siren modes; 100-850 Watt systems; lightweight high
efficient speaker arrays; airborne and ground vehicle
applications.
PTA12-100 AIRBORNE TELEPHONE DIALER/ADAPTER
New compact Dzus mounted telephone interface; full function
touch-tone keypad with display; 16 number memory; 2-wire POTS
(tip/ring) interface; standard DTMF encoder (Dual Tone Multi
Frequency) dialling capabilities; interface with cellular, Aero M/
Aero I, Globalstar and Iridium; LED backlighting; field adjustable
settings; Hook, Hold, Redial, Flash, Volume functions; multiple
ringer outputs. Requires 27.5 VDC; draws 500 mA Weight: 0.22
kg (0.5 lb) Dimensions: height 2.8 cm (1.13 in).
N301A SINGLE-USER AUDIO CONTROLLER
STX100 AIRBORNE SATELLITE COMMUNICATION
SYSTEM
Replacement for A301-6 series; user customisable for up to 6
transceivers with individual volume control (or 5 plus PA);
support for 6 navaids; ICS supports pilot; separate RX and ICS
volume controls; 3 ICS modes - LIVE, KEYED, VOX; VOX level
adjustment; direct audio input dual ICS tie line for multi-control
operation; low or high impedance; CVR output; optional NVG
lighting Dzus mount; TSO’d; UK CAA and Home Office approved
for police applications; requires 28 VDC; draws 0.17A Weight:
0.79 kg (1.75 lb) Dimensions: height 6/7 cm (2.65 in).
Certified airborne communication system capable of voice and
data operations; utilises Globalstar satellite network. System
consists of STX100-000, PTA12-100 and Globalstar antenna.
STX100 is compact, lightweight, tray mounted; has touch-tone
keypad standard DTMF encoder (Dual Tone Multi Frequency)
dialling capability; precision crystal controlled tones; reverse
polarity protection; RF filtering; LED backlighting; solid state
switching. Requires 27.5 VDC; draws 2.5 A (transmit) Weight:
3.8 kg (8.4 lb) Dimensions: height 18 cm (7.24 in).
N335 SINGLE CHANNEL DUAL-USER AUDIO CONTROLLER
TAC/COM NPX138N PANEL MOUNTED FM TRANSCEIVER
Self-contained; solid state modular plug-in construction; support
for 2 operators; backup emergency circuits; high crosstalk
filtering; supports high or low impedance headset systems;
individually adjustable mic outputs; constant loading regardless
of selection; 3 ICS modes LIVE/KEYED/VOX; separate PTT
keyline; up to 14 adjustable level controls; 8 position transmit
select; NORM/EMER switch; CVR output; TX LED; ICS Call LED;
emergency LED; composite output of all selected receive
channels; sidetone input for PA system; optional 28 VDC
standard blue/white or NVG compatible/compliant lighting; Dzus
mount; requires 24.8 - 32 VDC; draws 0.27 A Weight: 1.3 k g (2
lb) – 7 coms; 1.6 kg (3.5 lb) – 7 coms/7 navs Dimensions: height
6.7 cm (2.62 in) – 7 coms; 8.5 cm (3.37 in) - 7 coms/7 navs.
Agile self-contained panel mount transceiver 138-174 MHz;
multiple scanning modes; optional guard receiver; simultaneous
monitoring on main and guard channels; CTCSS supported;
simplex or semi-duplex; 1 or 10 Watt; encryption option; compact
size and weight; wide or narrow band; high duty cycles; requires
28 VDC; draws 0.5 - 3.0 A Weight: 1.35 kg (3 lb).
NTA01 MOTOROLA ASTRO OR SPECTRA RADIO
CONVERSION KIT
All required interface functions and ATR mounting hardware for
Motorola ASTRO or SPECTRA Radio Conversion. Voltage is
converted through a switching regulator with over voltage, over
current and thermal protection; speaker and mic levels are
converted for connection to standard aircraft audio system; kit
produces artificial side tone. Programming access is maintained
with external 15 pin connector for use with Motorola RSS
software (Motorola RIB or SRIB box required). To complete the
system, interface to NAT Tac/Com II control can simultaneously
operate up to four separate FM transceivers; supports ASTRO
functions: Modes, Zones, Scanning. Requires 27.5 VDC; draws
2.5 A (transmit) Weight: 3.67 kg (8.1 lb) (with radio) Dimensions:
height 18 cm (7.24 in).
TAC/COM TACTICAL FM CONTROLS
2, 3 or 4 FM radio control head system; supports NAT and most
other airborne FM transceivers; compatible with Motorola
Spectra Trunking radios; simultaneous operation of up to 4
transceivers; alpha-numeric channel labelling; on-screen help;
allows simultaneous monitoring on main and guard channels;
remote channel selection; master and slave control heads;
retrofits for Wulfsberg controls; CTCSS, DPL and DES supported,
CTCSS tone look-up table; optional NVG compatible lighting;
encryption options; DTMF keypads; Dzus mount; UK CAA and
Home Office approved for police applications; requires 28 VDC;
draws 0.25 - 0.45 A Weight: 0.9 - 1.3 kg (2 - 2.9 lb)
» RACAL ACOUSTICS LTD
B691 STATION BOX
Selection and control of audio input signals; processing and
routing of microphone signals; adaptable electrical
configuration; custom panel legends; seven toggle switches and
a potentiometer control receiver audio; combined switch/
potentiometer for intercom, four-position rotary switch for
transmitter selection (up to four Txs); optional use toggle switch;
Normal/Fail switch routes one receiver audio direct to earphone
in ‘Fail’ position; can use EM/Dynamic or carbon microphones;
12 audio inputs (9 switched, 3 unswitched); 4 transmitter
outputs plus intercom; integral panel illumination; operates
between -40 and +70 deg C; needs 28 VDC Weight: 520 g
Dimensions: 146 mm wide, 48 mm high, 64 mm deep.
B692 STATION BOX
Specification as for B691 except for 13 toggle switches; facility
for connection to a cockpit voice recorder (CVR) with automatic
routing of RX and TX audio signals to the CVR; 18 audio inputs
(15 switched and 3 unswitched) including system intercom
facilities Weight: 720 g Dimensions: 146 mm wide, 67 mm high,
64 mm deep.
B693 STATION BOX
Designed for use with headsets with electromagnetic
microphones; selection and control of audio input signals;
processing and routing of microphone signals; custom panel
legends; two intercom services (IC/1 and IC/2); IC/1 has option of
hot mic or PTT, 12 receiver inputs (4 switched, 8 unswitched)
plus intercom facilities; 8 transmitter options (four position
rotary switch); Normal/Fail switch; operates between -40 and
+70 deg C Weight: 850 g Dimensions 146 mm wide, 58 mm
high, 89 mm deep.
B694 STATION BOX
Complete two-crew aircraft communication management
system in a single unit; low cost; simple; provision for four
carbon mic inputs; rocker switch selects either earphones or
cockpit speaker; automatic switching in case of phone amplifier
failure; transmitter selection by six-position rotary switch; 10
audio inputs; outputs for six transmitters including passenger
address or ramp hail; integral intercom for up to four crew; 28
VDC; operating temperatures -10 to +70 deg C Weight: 680 g
Dimensions: 146 mm wide, 48 mm high, 118 mm deep.
B696 STATION BOX
Specifications as for B694 except for three-position toggle
switches provide selection of eight receiver audio services to
either loudspeakers or earphones; further two unswitchable
receiver inputs for warning tones, etc; integral illumination of
panel legends; 10 audio inputs (2 unswitched); output for 4
transmitters inc passenger address or ramp hail; operating
temperatures -25 to +55 deg C Weight: 1,250 g Dimensions: 149
mm wide, 48 mm high, 200 mm deep.
S693 AUDIO SELECTOR PANEL
Can be used alone, but intended for use with station box to form
a control station in a communication control system; provides
selection and control of up to 4 additional receivers; 4 switch/
potentiometers on front panel; 28 VDC; 4 receiver inputs;
integral panel illumination; operating temperature -40 to +70
deg C Weight: 260 g Dimensions: 146 mm wide, 38 mm high,
38.5 mm deep.
» SIGTRONICS CORP
PA-1 PUBLIC ADDRESS SYSTEM
Designed to interface with the SAMS 1000 (or other audio
systems); 200 W system incorporates horn and yelp functions;
requires 28 VDC; draws 10 A max Weight: 2.5 lb (PA module),
17.7 lb (speaker) Dimensions: width 6.25 in, height 2.5 in, depth
8.6 in.
visit us at www.shephard.co.uk
SHEPHARD
59
LAW » Voice communications
Voice communications « LAW
SAMS 1000 DUAL AUDIO PANEL
TFM-500 MULTI-BAND TRANSCEIVER
Provides pilot and observer with full control of up to 6 radios
and 5 nav receivers; individual switches control intercom and PA
functions; hot mic and PTT intercom modes standard; voice
activation optional; each operator can independently monitor
any or all receivers; 8 audio adjustments controlled by 4
push-pull volume controls; two rotary switches allow crew to
talk independently on any of the transceivers; 3 alarm inputs;
PAS-IC switch allows passengers to talk to front seaters and
hear what the observer hears; intercom can support up to 6
passengers; switches for RAMP-PA; yelp and horn tones
included; can run on 12 or 24 VDC (must specify); accepts
standard general aviation mics and headphones including noise
cancelling types Weight: 1.25 lb Dimensions: 6.25 in wide, 1.7 in
high, 4 in deep.
UHF (403 to 512 MHz) and VHF (138 to 174 MHz). 96 character
LED matrix display (red or green). Top line displays all data
relating to UHF module. Second line displays info relating to the
VHF module. Third line presents operating info on 2-channel,
synthesised guard. Fourth line presents transceiver status
information. Can be configured as single multi-band transceiver
or installed as FM1 and FM2 for simultaneous UHF and VHF
operation. Supports cross band repeat. 400 channels of pre-set
memory. Built-in thermally controlled cooling. All data entry via
enhanced tactile keyboard or download from PC.
SPCC PORTABLE COMMUNICATIONS
CONTROLLERS
Eliminates installation costs; aimed at units which rent or lease
aircraft; dual audio panel capability for pilot and observer; quick
disconnect; VOX intercom; 2 headset positions; SPCC-2 model
connects to aircraft VHF radio and 1 FM radio, can monitor a
third; SPCC-3 connects to aircraft radio and 2 VHF sets; ‘+2’
option allows 2 rear headset positions to transmit on radio;
satellite unit on cable can be placed on back seat; input voltage
11-34 VDC Master Unit Weight: 22 oz Dimensions: 3.75 x 6.25 x
2.5 in, aircraft interface cord length 4 ft, satellite unit 2.9 x 4 x 2
in, satellite cord length 4 ft.
» TECHNISONIC INDUSTRIES LTD
A710 AND A711 ACCESS/A COCKPIT AUDIO
CONTROLLER
Support for up to 8 users per station, plus expansion bus.
Supports six transceivers plus PA (which can be 7th TX).
Supports all headset impedance from 8 to 600 Ohms. Delivers
1,500 mW total headset audio output power. Supports built-in
CVR amplifier. Transformer isolated, floating inputs and outputs
provide exceptional RFI, cross talk and ground loop noise
rejection. Voice alerting for critical airframe warnings. Individual
transceiver transmit status enunciation. User defined and field
replaceable lexan panel legends. Supports simulcast operation
for up to three transceivers.
TFM-30, TFM-138, TFM-403 AIRBORNE FM
TRANSCEIVERS
TFM-30 covers 30 to 50 MHz, TFM-138 covers the 138 to 174
MHz, TFM-403 covers 403 to 512 MHz. Top line of display
provides information on main transmitter and receiver. Bottom
line displays info on the two-channel synthesised guard receiver.
Displayed simultaneously for main and guard is information
relating to channel number, alpha-numeric label, narrow or wide
band operating mode, scan status, operating frequency and
status of tones or digital squelch codes. Dzus panel mounted.
Self contained (no remote R/T). TX power 1 W or 10 W, front
panel selectable Weight: 1.4 kg (3.1 lb).
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Public Service Aviation Handbook 2008-09
TFM-520 FM/AM MULTI-MODE, VHF/UHF
MULTI-BAND TRANSCEIVER
Supports AM or FM mode operation on VHF band (138 to 174
MHz) and AM FM communications in the UHF band (403 to 512
MHz). Operating frequencies and related data are presented on
a 96 character, 4 line LED matrix display. Top line shows VHF
operating channel information, the second line shows UHF
operating channel data, the third line indicates operating mode
(VHF AM or VHF FM) while the fourth provides status
information. This transceiver supports narrow and wide band
operation, and features 400 pre-set memory positions
(channels) each of which can be programmed with a receive
frequency, transmit frequency, alpha-numeric label, CTCSS tone
or DPL/DCS code and instructions to operate in wide or narrow
band on a channel by channel basis. The TFM-520 can be
installed in single mode in which case it operates on one band at
a time, or can be installed in dual mode enabling simultaneous
operation on both bands from different positions in the aircraft.
Transmit power is 1 W or 10 W (VHF/FM), 1 W or 6 W (VHF/AM)
and 100 mW or 1 W (UHF/FM). This light panel mounted
transceiver was designed specifically to support police aviation
activities in the UK and is presently available only in the UK.
TFM-550 TRI BAND VHF/UHF AIRBORNE FM
TRANSCEIVER
This compact, panel mounted three band airborne FM
transceiver is entirely self contained (no remote box) and
weighs just 5.1 lb. Coverage is 30 to 50 MHz (VHF Lo Band), 138
to 174 MHz (VHF Hi Band) and 403 to 512 MHz (UHF). This
transceiver can be installed in Dual Mode as FM1 and FM2
allowing for simultaneous operation on VHF and UHF from
different positions in the aircraft. Technisonic offers an optional
slaved remote control head (RC-550) allowing frequency change
and frequency management from a remote position. This
transceiver features 600 memory positions (channels) and
displays operating data on a 96 character, four line LED matrix
display. Each non volatile memory position is capable of storing
a receive frequency, a transmit frequency, an alpha-numeric
label, and a CTCSS tone or digital squelch code. Information
concerning scan and wide or narrow band operation is also
stored during programming. Data entry is via a front panel
keypad or download from a PC. Top line of the display shows
VHF operating data, second line shows UHF operating
information, the third line presents VHF Lo Band operating data
and the fourth line is a status enunciator. DTMF signalling
during transmit is supported by an internal encoder. Transmit
power is 10 W or 1 W on all bands
» WULFSBERG ELECTRONICS
C-5000 COMMUNICATIONS MANAGEMENT
CONTROL
Successor to C-1000 controller; controls up to three R/T
systems (up to nine radios) including RT-5000, RT-9600F/
RT-7200; simultaneous monitoring of main, guard or both
receivers; transmission on main channel displayed or guard; 350
programmable pre-set channel; simultaneous use of two radios
from one control; external ‘take control’ switch; three
independent voice recorders for quick playback from any of the
radio systems; enhanced operation modes including simulcast,
cross band relay, relay/simulcast, repeater, cross band full
duplex, programmable channel memory; supports encryption
systems, scan functions; alphanumeric channel identification;
two-line display screen; back-lit key pad; NVG compatibility
optional; digital squelch protocols can be added; coffee
resistant; requires 27.5 VDC aircraft power, nominal (17-33 VDC);
tolerates -30 to +60 deg C Dimensions: 3.75 in high, 5.75 in
wide (5 in behind face plate), 6.484 in deep (excluding face plate
and connectors, wires)
FLEXCOMM II/RT-5000
One-box 29.7 MHz to 960 MHz transceiver; controlled through
C-5000 unit; 688,640 channels available; covers every discrete
AM or FM channel assigned to the public safety, industrial
forestry, business, military, air traffic control or federal agency
operation between these frequencies; covers nearly every
discrete comms channel used world-wide including 12.5 kHz
channels; high speed scanning; two-level priority and multiple
pre-selector filters; triple conversion AM/FM design; five
selectivity bandwidths; supports narrowband voice; digitally
encrypted voice or data; voice on ATC channels; digital signal
processor to boost voice quality and squelch control; analogue
CTCSS squelch control; digital coded squelch control; support
for automatic number identification; voice scrambler; voice
encryption; requires 27.5 VDC (+/-20%) Weight: 15 lb (6.81 kg)
Dimensions: 4.88 in wide, 7.64 in high, 14 in deep.
FLITEFONE VI AIRBORNE TELEPHONE SYSTEM
Automated AGRAS operation; 1+, 0+, 01+, 011+ calls; office
phone operating environment; all solid-state design,
microprocessor-based logic design, modular construction; small
size, light weight; low power consumption; burnout resistant
transmitter; high receiver sensitivity; high inherent MTBF;
exceptionally high frequency stability.
RT-138F FLEXCOMM TRANSCEIVER
138 to 174 MHz 4,400 channel VHF-FM transceiver; no band
spread limitation from 138 to 173.9975 MHz; other specifications
as for RT-30; ready for encryption (optional); provides interface
for popular digital voice encryption systems.
RT-30 FLEXCOMM TRANSCEIVER
One-box 29.7 to 50 MHz 2,030 channel low-band VHF-FM
transceiver; controlled through C-5000 or earlier C-1000
controller; push-to-talk (PTT) duplex operation; automatic RF
tuning; no crystals to change; no band spread limitation; 32
synthesised sub-audible CTCSS tones; all solid state; plug-in
modular construction with gold card-edge connectors; glassfibre
printed circuit boards with post coating for humidity and dust
protection; burn-out resistant transmitter; automatic
signal-to-noise squelch with manual override; separate audio
input and output; operates on 28 VDC power; audio side tone
exists when transmitter is producing RF power; options include
single channel guard receiver module, guard receiver CTCSS
decoder; programmable tone Weight: 7.5 lb (3.41 kg) or 8.3 lb
(3.76 kg) with guard receiver Dimensions: 4.38 in wide, 10.5 in
long, 5 in high.
RT-406F FLEXCOMM TRANSCEIVER
406-512 MHz; 8,480 channel UHF-FM transceiver; no band
spread limitation from 406 to 511.9875 MHz; other specifications
as for RT-30.
SERIES III COM/NAV SYSTEMS
VCS-40A VHF Communications System - 20 W solid-state
transmitter, continuous self-test and built-in diagnostics, built-in
SELCAL and ACARS capability, ARINC 429 serial data bus tuning
capability; VNS-41A VHF Navigation System - 200 channel
microprocessor based navigation receiving system that
combines VOR/LOC, glideslope and marker beacon reception in
the same unit; TRS-42A ATC Transponder System - dual
transmitter output devices, encoding altimeter readout, dual
transponder control from a single Control Display Unit, full-time
automatic and pilot-selected self-test, ARINC 420 serial bus
control capability; DFS-43A automatic direction finder system low-frequency navigational aids and AM broadcast stations in
the 190.0 - 1860 kHz frequency; DMS-44A Distance Measuring
System - provides data from 3 DME stations simultaneously;
RMS-555 Radio Management System - single display/control
unit and remote-mounted data adapter.
visit us at www.shephard.co.uk
SHEPHARD
61
LAW » Mission management / moving maps
MISSION MANAGEMENT
SYSTEMS/MOVING MAP
DISPLAYS
» AERODATA AG
AERONAV
Navigation and mission management system specifically
designed to support special mission operations by itself and/or
in close cooperation with ground support. Key features: IFR
(including NPA) certified GPS navigation (TSO C129a), B-RNAV;
interfaces to autopilot, moving map systems, (E)HSI, air data
computer; mission management for enhanced operation
efficiency; navigation with position and attitude information;
data communication and fleet management using Aerodata’s
AeroPhone system; capability for fleet management using
Aerodata’s AeroTrack system; customised solutions available,
such as DGPS; various interfaces for mission related equipment
(FLIR, Direction Finder, etc)
» BECKER FLUGFUNKWERK GMBH
MODE-S TRANSPONDER
The single block Class 1, Level 2, Mode S transponder, BXP
6401-1-(01) in 2 ¼ standard panel cut out format, will be
introduced, dedicated especially for General Aviation purposes.
This unit is interfaces to various blind encoders and air data
computers. The 250 watt model will be complemented by a 150
Watt model with extremely low power consumption especially
suited for glider aircraft. The BXP 6401-2-(01) Class 2, Level 2,
Mode S transponder can be optionally equipped with a digital
encoding altimeter as a separate unit attached to the
transponder. This latest concept combines individual customer
requirements with facilitated maintenance / calibration routines
in optimized form. Based on their form compatibility both of
these BXP 6401 models can be used to replace Becker’s
previous Mode A/C transponder ATC 4401.
» EUROAVIONICS NAVIGATIONSSYSTEME
EURONAV IV DIGITAL NAVIGATION AND TASK
MANAGEMENT SYSTEM
Intended for police, EMS, military and special helicopter
operators, the RN6 is the successor of the popular RN5 and has
a 12-channel differential GPS, 14-key Dzus keypad and a variety
of LCD screens (5”-10”). Modular software offers variable
options such as Digital Terrain Elevation Data, Search and
Customisable Vector Charts, Airspace Structure, Raster Charts,
Satellite and Photo Maps, etc. The RN6 can be linked to a wide
range of hardware components, including an existing FMS. With
its capability of mission planning, flight recording, traffic
collision avoidance, obstacle warning, message management
etc. the system offers variable mission support capabilties and
is adapted to the needs of the customer.
62
Public Service Aviation Handbook 2008-09
» FLIGHT COMPONENTS AG
TIMEARC VISUALISER
Multi-function digital display system with a large, flat panel, full
colour and high resolution active matrix (TFT) LCD driven by the
digital map display generator (LRU) offers pilots a variety of
navigation capabilities. Topographic raster and vector graphic
maps, displayed in multiple windows, with Video (FLIR or TV
camera imagery) and GPS Nav Data, real time and simultaneous,
all combined in one screen. Obstacle and area warning and
terrain clearance checker module warns the pilot visually and/or
audibly if there is a conflict between the helicopter obstacle
warning zone and an object in the obstacle area database.
Display of FLIR or video camera position if interfaced with a
gyro-stabilised camera system. Real View dramatically increases
situational awareness by flying through digital terrain in 3D.
Real View overlays images from aeronautical charts or from
satellites on elevation data.
» sagem Défense Sécurité
ICDS (Integrated Cockpit Display System)
A multi-function digital display system available in three
different sizes 10.4”, 8.4” and 6.4”. It is a fully sun-readable,
colour Active Matrix Liquid Crystal Displays (AMLCD) flat panel
displays with optional embedded Night Vision Imaging System.
Associated with different other devices it can offer various
on-board functions: Weather service: (requires Sagem
RCOM-100 satellite receiver) weather data may be uploaded to
the ICDS. Weather reports are obtained on a request/reply basis.
Aviation weather products include NEXRAD, METAR, TAF,
AIRMET, SIGMET, CATMET, NOTAM, Winds Aloft, Significant
Weather graphical and text reports. Moving map Display:
(requires Sagem Mercator) offers pilots further navigation data:
geographical maps with mission related overlays, terrain
elevation, etc. The typical geographic coverage is 3,000,000
km2. Tracking function: (requires a GPS receiver but no
transponder) only available when the corresponding
ground-based infrastructure is available. This function gives the
aircraft or helicopter crew information with Traffic Alert and
Collision System (TCAS) and Terrain Awareness Warning System
(TAWS via ARINC 708 or video inputs. Multi function Display:
The ICDS also features a composite Map /video mode via RS170,
PAL or NTSC. The ICDS screens have been chosen to modernize
several helicopters: EC120, AS350 Ecureuil, Bell 206, Bell 407,
S-64 Skycrane, R44. In the US the ICDS screens will equip the 14
LAPD’s helicopters as part of a modernization program awarded
to Sagem Avionics Inc (Grand Prairie Texas). ICDS equip also the
EMB-121 Xingu of the French Air Force and Navy.
Mission management / moving maps « LAW
APIRS
An attitude and heading reference unit designed for all
new-generation aircraft (fixed and rotary-wing), as well as
modernization programs. The APIRS system calls on
state-of-the-art technologies, such as fibre-optic gyros and
silicon accelerometers. APIRS offers very high reliability, even in
the harshest operating environments. APIRS has been selected
for the following aircraft: NH90, EC135/635, EC145, EC155,
EC225/725, ALH.
» SKYFORCE AVIONICS LTD, A HONEYWELL
COMPANY
OBSERVER MK III
The current generation of autopilots is the APM 2000 family,
fitted on all Eurocopter helicopters. The APM 2000 is based on
a highly integrated digital computer, reflecting the “new
avionics” concept now being applied throughout the aviation
sector. The APM 2000 module is certified on the Eurocopter
EC135/635, EC145 (BK177 C2) and EC155 in IFR (Instrument
Flight Rules) single-pilot configuration, and has also been
chosen for the EC225/725 heavy helicopter. Sagem Défense
Sécurité’s automatic pilot equipment equip Eurocopter, HAL,
Agusta, Bell, Denel, Mitsubishi and Sikorsky helicopters.
A high resolution, intuitive to use mapping system that can provide
highly detailed mapping for the corporate or EMS/paramilitary user
in the VFR environment. In addition, as a task management system
it is capable of creating a paperless cockpit for an airborne observer
in the military, police, emergency or utility environment through the
use of user-defined databases. This facility allows text and picture
images to be stored and retrieved at the touch of a button, whether
the information be details of helicopter landing sites, daily orders or
operational procedures. With a built in flight logging capability for
post flight analysis, Observer is a management tool that can be
used to ensure the cost efficient use of an aircraft resource. Future
upgrades will include an AIS shipping transponder interface and
Military Grid Reference System (MGRS) co-ordinate input. Observer
MkIII is approved to ETSO C113/EASA.210.423. No other mission
management system is as highly specified or qualified as Observer
MkIII says the company. London Metropolitan Police’s three new
Eurocopter EC145s will have Observer MkIII.
HelIpsYs
SENTINEL
As a mission preparation and debriefing system for helicopters,
Helipsys offers all the services necessary for preparing and debriefing
missions. Helypsis relies on the know-how Sagem Défense Sécurité
has acquired from numerous mission preparation systems it has
developed for aircraft, e.g. the MPME mission preparation module for
helicopter crews for ALAT (French Army Aviation).
Sentinel is a new Multi-Functional Display (MFD) targeted at the
helicopter market which expands the flexibility, reach and
affordability of Skyforce’s mission system family of products.
Sentinel, provides flight planning, maps, charts, relative terrain,
traffic information and FMS flight plan following; planned
feature growth will include plates, weather, satcom and
checklists. Sentinel has been designed to support all mission
roles from day VFR though night NVG operations, fixed-wing or
rotary, single or multi-crew. Sentinel has been designed to put
the pilot’s information needs first and foremost. It is being
offered in a variety of form factors, including a full NVG
compliant MFD and remote processor for avionics bay mounting
to couple to suitable displays. It can also operate as a stand
alone panel MFD or as an integral element of the Observer MKIII
Mission System. Lead customers include HEMS and police
operators, plus a number of private customer installations,
certification is expected in the third quarter of 2007 and
shipments will commence in the fourth quarter.
APM 2000
MFDAU (Miscellaneous flight data acquisition unit)
Interface with a flight data recorder, MFDAU records mandatory
parameters, according to airframe manufacturer’s
specifications. (data frame rate 64 or 128 words/sec.). Interface
with a data transfer unit. It brings data frame dedicated to
maintenance purpose. MFDAU equip EC A35, EC 145 and EC 155
helicopters: Dimensions: (LRM) = 37.6 x 183 x 306.7 mm, Weight
= 2 kg, Power supply = 28 VDC / 28 W
OLOSP
OLOSP is a gyrostabilized platform that enables observation and
targeting both day and night independently of the carrier’s
movements. Its flexible design allows for bi- or tri-sensor versions
so as to meet all the requirements of observation missions. OLOSP
sensors are used in several countries on UAVs, helicopters,
observation balloons, patrol and maritime surveillance planes,
surface ships and in fixed stations. It has just been ordered by
Eurocopter for the NH 90 of Oman (TTH version) and for the
modernization programme of the French Navy Panther helicopters.
» TRACKER NETWORK (UK) LTD
TRACKER STOLEN VEHICLE RECOVERY SYSTEM
The Tracker unit is a radio transponder. When the vehicle is
reported stolen and the theft is confirmed with the police,
Tracker activates the unit. It transmits a unique reply code,
which can be detected and decoded by police tracking
computers fitted in cars, helicopters and fixed land sites. It can
be covertly fitted to any vehicle or plant equipment. The unit is
tested remotely at the time of installation, with a customer
signature required to verify the test. The system currently only
operates in the UK. The presence of the Tracker unit is not
disclosed to the thief thus giving a greater likelihood of rapid
recovery and minimal damage. To assist in tracking, a revision
to the equipment fitted to aircraft includes an audible system
linked to the air observer in addition to the visual display unit.
This new equipment is lighter and smaller than the original.
Dimensions - display head: length 134 mm, width 40 mm, height
65 mm, weight 160 g processor: length 212 mm, width 142 mm,
height 53 mm, weight 860 g.
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63
AIRCRAFT
SPECIFICATIONS
ROTORHUB magazine is THE new International business information source for the civil,
corporate and public service rotorcraft markets. ROTORHUB magazine is founded on the
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SEARCH AND RESCUE
All products listed in this section come under the heading:
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±Search and rescue equipment
Search and rescue and emergency medical service operations are different
but related, particularly where helicopters are concerned. The medical
equipment fit of an SAR helicopter may be very similar to its EMS cousin,
but it needs much additional hardware. This section contains examples of
some essential items for SAR helicopters and fixed-wing aircraft.
Note: Items listed in this section are examples from each manufacturer’s
product range. Contact the companies concerned for full details.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.
SAR VIEW » Tom Withington
Public-private partnerships « SAR VIEW
UP AND AWAY IN EUROPE
AND ASIA
Iceland joining the project and the two countries closely
coordinating their purchases. In November 2007 CHC
helicopters announced that its contract with Statoilhydro
ASA, a Norwegian energy company, for the provision of
North Sea SAR operations with a single EC 225 helicopter
had been renewed. This renewal was in addition to a June
2007 contract that CHC Helicopters won to provide a pair of
EC 225 machines for SAR operations in the Oseberg oil field.
The November contract will see the solitary Eurocopter AS
332 aircraft, which CHC Helicopters already uses for SAR
provisions in the oil field, replaced by the EC 225.
ASIAN SUCCESS FOR EUROCOPTER
By Tom Withington
Public-private partnerships are increasing in
popularity in the United Kingdom as a means
to provide national search and rescue services.
Will the rest of the world now follow suit?
T
he competition to replace the UK’s Royal Air Force
and Royal Navy Sea King HAR3/3A/5, and CHC
Helicopter’s Sikorsky S-92 and AgustaWestland
AW-139 search and rescue (SAR) helicopters gained
momentum in January 2008 with AgustaWestland joining
Serco, FB Heliservices and Bristow Helicopters in the UK
Air Rescue consortium to provide SAR services around the
UK over a contractual period that could run for up to 30
years. UK Air Rescue Team will compete against two other
companies, namely the AirKnight consortium which
includes VT Aerospace and Lockheed Martin, and the
Soteria team which includes Thales and CHC Helicopters.
Staying in the UK, FB Heliservices signed a contract
with AgustaWestland for the provision of two AW139
machines to enter service in 2009 for the provision of joint
SAR training services for the UK Ministry of Defence. These
aircraft will be operated from RAF Valley in North Wales
and are fully equipped for over-land and water SAR
operations. They will join the two AW139 aircraft operated
by the UK’s Maritime and Coastguard Agency (MCA) which
66
Public Service Aviation Handbook 2008-09
entered service in 2008. These aircraft are flown by CHC
Helicopters on behalf of the MCA and are based at
Lee-on-Solent and Portland in southern England. CHC
Helicopters will manage the contract until 2012.
AgustaWestland have also enjoyed success in Spain
over the last year, selling three AW139 machines to the
Spanish Marine Safety Agency (SMSA). These aircraft,
eight of which are in service, are configured for SAR as well
as pollution control. Estonia will join Spain in operating
AW139s following the delivery of two to the Estonian
Government in October 2007. As well as performing SAR
missions, these aircraft will also perform border
surveillance operations.
Finally, in February 2008, Italy’s coast guard finalised
a contract with AgustaWestland for the provision of two
AW139 machines with an option for a third aircraft. These
helicopters are to be purchased as replacement aircraft for
the AgustaBell 412s that the service currently operates.
Norway and Iceland have jointly announced that they
will perform a bilateral procurement of aircraft for SAR
operations. Norway is in the market for up to twelve new
helicopters to replace the Royal Norwegian Air Force’s Mk
43A/B Sea Kings which will enter service by 2015.
Iceland also wants to buy three aircraft for SAR
provision. To this end, Norway has launched an initiative
known as NAWSARH for the helicopter purchase, with
In Asia, Eurocopter scored success in Japan, supplying the
Coast Guard with two EC 225 SAR aircraft. These
helicopters are also earmarked to provide coastal and
maritime patrol services and will supplement the four
Eurocopter AS 332 aircraft which the agency already
operates. In the Republic of Korea, the Korean Coast
Guard announced that it has purchased two AW139 aircraft
which will enter service in 2009 for the provision of SAR
support. The aircraft will also be tasked with air ambulance
and maritime patrol missions.
Eurocopter announced the delivery in December 2007
of the first two EC 225 SAR aircraft to be operated by the
China Ministry of Communications Rescue and Salvage
Bureau. This delivery brings the total helicopter fleet
operated by the Bureau to ten aircraft.
Officials at Sikorsky were celebrating in November
2007 following the conclusion of a major contract with
Saudi Arabia for the provision of S-92 and S-76 machines;
16 and 15 of which will be delivered respectively from March
2008. Search and Rescue will be a key mission for these
aircraft, alongside fire-fighting assistance, and emergency
medical services. The purchase accompanies a decision by
the country’s Ministry of Interior Affairs to perform a
significant expansion of bases for helicopter operations.
Staying in the Middle East, in August 2007 the US
Congress was notified of a deal between Sikorsky and
Bahrain for the latter to purchase the UH-60M Black Hawk
aircraft for SAR operations. Moreover, in North Africa,
AgustaWestland had reason to celebrate after it secured a
sale of six AW-101 machines, along with four Super Lynx
aircraft to Algeria for SAR, border security and general
utility tasks.
Finally, in Africa Nigeria’s National Emergency
Management Agency (NEMA) announced in January 2008
that it is to purchase an undisclosed number of helicopters
which are to be deployed across six bases throughout the
country. The aircraft, the type of which has yet to be
decided, are to be purchased so that the NEMA can reduce
its dependence on the air force for SAR provision. ±
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SHEPHARD
67
SAR » Search and rescue
Search and rescue « SAR
SEARCH AND RESCUE EQUIPMENT
» AEROLITE MAX BUCHER AG
» BEAUFORT AIR-SEA EQUIPMENT LTD
COMBI-STRETCHER TYPE AEROLITE
SINGLE SEAT LIFERAFT
Designed to be used as normal stretcher or as scoop-stretcher;
weighs 8.5 kg (19.7 lb) with safety harness fitted; stretcher frame
constructed with aluminium tubing; two locking points at head
and foot; two fixing pins at the head and foot allowing easy
installation in helicopter; carbon fibre material bed of stretcher is
shovel formed; backrest length 75 cm (29.5 in) and has a range of
adjustments from 0 - 75 degrees with four intermediate settings.
Buoyancy chamber and inner floor - 2-ply butyl-proofed nylon
fabric; outer floor and canopy - single texture polyurethane
proofed nylon fabric; CO2 cylinder; inflated buoyancy (excluding
canopy and floor) 116.12 kg (256 lb); inflated dimensions: length
169 cm (66.5in) (external) and 127 cm (50 in) (internal); width 93
cm (36 in) (external) and 49 cm (19 in) (internal); approx weight
(excluding inflation equipment): 1.87 kg (4.12 lbs) (models: B1, C1
and D1); 2.65 kg (5.84 lb) (B2 and D2); 2.72 kg (5.9 lb) (C2 - Mk 10).
CIRRUS SERIES
Modular stretcher System for different helicopters (Agusta
Grand, AW139, EC 135, EC145 etc). Flexibility in length and width,
foldable, with/ without adjustable backrest, primary and
secondary stretcher.
» AGUSTAWESTLAND
AW101 SAR MISSION EQUIPMENT
Multi-mission SAR configuration: maritime, overland, mountain;
30 m3 (1,059 cu ft) usable internal volume; up to 16 casualties on
stretchers; all weather operation with full ice protection for
rotor system; primary (hydraulic) and secondary rescue hoists;
SAR communications; advanced flight management avionics
(automated approach to and departure from hover, automatic
search patterns); Doppler and GPS navigation; rear ramp door;
three engines; auxiliary power unit; proven reliability and
maintainability; custom integrated logistic support;
computerised fleet management system; low pilot/crew
workload; NVG compatible EFIS; off the shelf.
» AIR CRUISERS CO
MULTI-PERSON LIFE RAFT (MPLR)
Thermobonded seams; lightweight closed inflation system; 8, 12,
20 person capacity (based on 0.41 sq m/4.5 sq ft/person and
average weight of 68 kg/200 lb); overload 150%; self-erecting
canopy providing occupant protection; removable radar and light
reflective strips; foam floor providing insulation; ballasting system;
auto-inflating boarding stations provide easy entry to raft.
» BCB INTERNATIONAL LTD
SOLAR STILL
Distils fresh water from salt water; constructed of PVC with a
high visibility buoyancy tube and clear dome; approx dimensions
33 x 24 x 4.5 cm (13 x 9.4 x 1.7 in) when packed; inflates to a
diameter/height of 75/58 cm (29.5 x 23 in)
68
Public Service Aviation Handbook 2008-09
» BECKER FLUGFUNKWERK GMBH
MR510 PERSONAL LOCATOR BEACON
More than 30,000 Personal Locator Beacons (PLB), are
operated successfully in more than 27 countries under
environmentally harsh conditions. The enhanced MR 510 PLB,
with GPS capability, significantly improves rescue efficiency.
Based on the well known MR 509 beacon with its rugged design,
variety of activation methods and ease of maintenance, it gives
low life cycle costs and provides full compatibility with the
complete Becker SAR system range covering Beacon, Direction
Finder SAR DF 517 and full accessories. 406 MHz COSPAS
SARSAT capability guarantees investment protection even after
the termination of satellite processing of 121.5 MHz and 243.0
MHz beacon transmissions in February 2009.
» BREEZE-EASTERN
HS-20200 RESCUE HOIST
Works with 28 VDC electric current, lightweight variable speed,
continuous duty, fail-safe break, 272 kg (600 lb) rated load, 43 kg
(95 lb) system weight, 76 m (250 ft) cable length, up/down
variable speed operator control, up/down fixed speed pilot control,
speed @ 272 kg (600 lb) 0-0/76 m/s), speed @ 136 kg (300 lb)
0-1.27 m/s. Display features digital cable payout, power-on, motor
hot, slow speed and cycle counter indication. Safety features
include electronic overload protection, redundant limit switches,
mechanical fail-safe brake, cable foul sensor, safety clutch,
bi-directional cable tension control. Options include various hook
designs, various control pendant displays, pilot cable payout
display, hover trim four-way switch, NVG compatible display.
HS-29900 RESCUE HOIST
272 kg (600-lb) rated load, speed @ 272 kg is 0-1.78-m/s, 90 m
(295 ft) cable length, 50 kg (110 lb) system weight; 115 VAC, 3ph,
400 Hz voltage; 24A/Phase electric current, 28 VDC, 5A control
power, 28 VDC, 5A pulse cable cutter. Operation up/down variable
speed hoist control, pilot up/down fixed speed hoist control.
Displays include digital cable payout, motor hot, full-in/full-out,
cycle counter. Safety features include electronic overload
protection, safety clutch, redundant limit switches, mechanical
fail-safe brake, bi-directional cable tension control, automatic
slowdown at travel ends, redundant cable cut switches, cable foul
sensor. Optional features include various control pendant and
hook designs, various control station designs, hover trim/search
light control, NVG-compatible displays.
HS-10300 RESCUE HOIST
272 kg (600 lb) rated load, speed @ 272 kg is 0/1.52 m/s, 90 m
(295 ft) cable length, 22-25 kg (49-56 lb) hoist weight, 152-206
bar (2,200-3,000 psi) hydraulic pressure, 10.2-22.7 l/min (2.7-6
gpm), 26 VDC 5A control, 28 VDC 5A pulse cable cutter. Variable
speed operator controller output, constant speed back up
controller output for operator and pilot. Safety features include
overload clutch, redundant limit switches, mechanical or
hydraulic fail-safe brake, bidirectional cable tension control,
automatic slowdown at travel ends. Optional features include
cycle counter, cable payout display, NVG display; various hook,
control pendant and controller designs.
BL-27100 RESCUE HOIST
272 kg (600 lb) rated load, 0-1/25 m/s reel-in speed, 91.4 m (300
ft) maximum cable length, 41.8 kg (92 lb) system weight, 206
bar (3000 psi) hydraulic pressure, 22.68 l//min (6 gpm). Up/
down variable speed normal operator interface, up/down fixed
speed back-up operator interface. Displays for normal power,
emergency power, hoist up/down, hydraulic overheat. Safety
features include overload clutch, redundant limit switches,
dynamic hydraulic braking, back-up mechanical fail-safe brake.
Options include NVG displays, cycles counter, cable payout
display, remote control pendant.
HS-29700 RESCUE HOIST
205 kg (450 lb) rated load, speed @ 295 kg is 0-0.8 m/s, 50 m
(165 ft) cable length, 31 kg (68 lb) system weight, 28 VDC
voltage, 100A max electric current, 28 VDC 5A pulse cable
cutter. Operator up/down variable speed hoist control, pilot up/
down variable speed hoist control. Displays include digital cable
payout, power on, motor hot, cycle counter. Safety features
include electronic overload protection, redundant limit switches,
mechanical fail-safe brake, cable foul sensor, crushable bumper.
Options include variable hook designs, fixed/moveable control
pendant, pivot cable payout display, NVG compatible displays.
HS-16600 RESCUE HOIST
Rated load 136 kg (300 lb); speed @ 600 lb: 0.25 m/s (50 ft/
min); cable length 34 m (110 ft); system weight 13.2 kg (29 lb);
power: voltage 28 VDC, electric current 35 A and cable cutter
28 VDC and 5 A pulse; options: quick connect/disconnect,
carrying case, control pendant and a variety of hook designs;
operated on: Agusta A109 and A119, Bell 206 and 222, and
MD500.
SkyHook ERD Manual Backup Hoist
2.2 to 1 and 6 to 1 gear ratio, 13.5 to 1 and 40 to 1 torque ratio,
261 x 66 x 6 (24 x 26 x 0.25 in) base plate dimensions (ERD-100).
Component weights for hoist 12.7 kg (28 lbs), 100 ft rope 3.2 kg
(7 lbs), rappel bar and anchoring access 1.6 kg (3.5 lbs). Lift
capacity 135 kg (300 lbs) rated load. Accessories include
composite floating handle, stainless steel carabiner with 3,533
kg (7,790 lb) strength, Prusik winding pulley, tandem Prusik or
cam-driven anchor system, 30-60 m (100-200 ft) 1.27 cm
(0.5-in) composite rope 4,082 kg (9,000 lb strength), storage
bag for composite rope.
» CANAM AEROSPACE
C45 CARGO HOOK
Lightweight 6.8 kg (15 lb) long-line hook; lift capacity 204 kg
(450 lb); toggle mechanism assures the positive lock of the
hook, and an amplification of opening forces; adjustable clock
spring allows the load beam to be returned automatically;
stainless steel spring fully protected by a tapered cap fastened
on by four screws; tension increased or decreased as required;
standard load beam with oversized throat will accommodate up
to 8 eye chokers, 5/8 inches in diameter; throat opening is 0.35
cm (1.4 in); removable solenoid; load releasing performed
manually (manual release knob), or electrically (solenoid); not
certified as a primary or belly hook attached to the helicopter.
» CEIS TM - ELTA
A06 COSPAS-SARSAT EMERGENCY LOCATOR
TRANSMITTER RANGE
Packaged in an emergency orange container; transmitter
includes 3-position switch; red high-intensity light and buzzer;
antenna connector (whip or aircraft skin antenna); remote
control; activation is automatic by G-switch (A06); transmission
is on 406 MHz COSPAS-SARSAT frequency at 5 W power and on
the 121.5 & 243 MHz international distress frequency at 100 mW
power; remote control unit option available for Airbus cockpit
fit, and a custom option for other aircraft types; transmitter
weight 2.8 lb (1.3 kg).
» DOCTOR DOWN
RESCUE WRAP
A self-contained bedding system to maintain patient body
temperature. This patented three-part system can be easily
modified for use in many climates and accommodates
patients up to 181.4 kg (400 lb). It is a warm, compact,
lightweight and waterproof barrier to the elements with a
disposable liner system to contain body fluids. Velcro
straps secure fluid bags, monitors and pumps in place, and 2
large internal pockets hold reusable heat packs (included) for
patient warming. Kit weight is 14 lb (6.35 kg).
» EASTERN AERO MARINE (EAM)
MARINE TRIUMPH 6 LIFE RAFTS
Twin-tube self-inflating raft; inflates in 15 seconds with canopy
up; two door openings in the high visibility canopy for air
circulation; easy entry ramp, water ballasts increase stability;
stowable soft valise pack automatically opens on inflation; hard
pack, fibre-glass, weatherproof container; low profile on deck
mounting for easy access; nylon fabric, neoprene coated inside
and outside, meets military specifications (MIL-C 17415F, Type 16,
Class AA); six-person raft weighs approximately 39 kg (87 lb);
buoyancy per person is 95 kg (210 lb); with approximately four
square feet of deck area per person; freeboard height exceeds
40 cm (16 in) with full capacity load.
ILLUMINATED RESCUE HOOK BUMPER
Three-year shelf life, 200 hours battery life. Water-proof, impact
resistant, easily attaches to Breeze-Eastern Corporation Hook
Assemblies.
visit us at www.shephard.co.uk
SHEPHARD
69
SAR » Search and rescue
» FERNO (UK) LIMITED
SCOOP 65 EXL STRETCHER
Designed to be placed underneath the casualty without the
need for lifting or logrolling; contoured surface supports and
immobilises patient; lightweight alloy structure designed with
built-in handholds; extension of positive stop foot section allows
it to be adapted to fit various sizes of casualty; spinal column
can be x-rayed while patient is on Scoop; when not in use
stretcher can be folded in half for easy stowage; weight 8 kg
(17.6 lb); max load capacity 159 kg (351 lb).
» GOODRICH HOISTS & WINCHES
42305 INTERNAL ELECTRIC RESCUE HOIST
131.85 cm (51.91 in) hoist height, 934.29 cm (13.50 in) hoist
height, 85.29 cm (35.38 in) hoist length. Weights: PHP, PN
42305-1 81.65 kg (180 lb), HPH, PN 42305-2 79.83 kg (176 lb).
Boom rotation: HPH, PN 42305-1 205 degrees, HPH, PN 42305-2
90 degrees. Cable usable length 76 m (250 ft). Cable diameter:
4.775 to 4.928 mm (0.188 to 0.194 in). Rated speed: 76 mpm
(250 fpm) with 136.08 kg (300 lbs) load 38.1 mpm (125 fpm) with
272 kg (600 lbs) load.
Search and rescue « SAR
76360-200 HYDRAULIC HOIST
272 kg (600 lb) force capacity, 50 m (164 ft) usable cable length,
30 m (100 ft/m rated speed), 25 kg (54.2 lb) weight, unlimited
duty cycle, 27 V.de electrical power. Safety features include self
clamping brake, automatic end limit stops, additional stop at
3.92 m (13 ft) before upper limit, cartridge operations
emergency cable cutter.
76363-200 HYDRAULIC HOIST
272 kg (600 lb) force capacity, 50 m (164 ft) usable cable length,
30 m (100 ft/min rated speed), 32.4 kg (71.6 lb) weight, unlimited
duty cycle, 27 V.de electrical power. Safety features include
self-clamping carbon brake, automatic end limit stops, cartridge
operated emergency cable cutter protected against EMI,
universal hook assembly.
76368-500 HYDRAULIC HOIST
272 kg (600 lb) force capacity, 75 m (246 ft) usable cable length,
0-54 m (0-180 ft/min rated speed), 32.4 kg (71.60 lb) weight,
unlimited duty cycle, 27 V.de electrical power. Safety features
include self-clamping carbon brake, automatic end limit stops,
cartridge operated emergency cable cutter protected against
EMI, automatic slow down near cable end.
42315 EXTERNAL HYDRAULIC RESCUE HOIST
76370-130 ELECTRIC HOIST
Hoist height 31.14 cm (12.26 in). Hoist width: 80.65 cm (8.75 in).
Weight 44 kg (97.6 lb) max. Cable usable length 61 m (200 ft).
Cable diameter 4.775 to 4.928 mm (0.188 to 0.194 in). Rated
speed 61 mpm (250 fpm) nominal; 30 mpm (100 fpm) primary,
26 mpm (85 fpm) secondary. Hydraulic fluid: Mil-H-83282. Rated
flow 20.4-21.1 ltr (5.4 to 5.6 US gallon/min). Supply pressure
2,750 psi max. Return pressure 50 psi normal.
136 kg (300 lb) force capacity, 40 m (132 ft) usable cable length,
30 m (100 ft/min rated speed), 15.8 kg (35 lb) weight, 27 V.de
electrical power. Safety features include self-clamping brake,
automatic end limit stops, cartridge-operated emergency cable
cutter protected against EMI.
42325 EXTERNAL RESCUE HOIST
Input power: electric 28v DC to 125 amps; control power 28 VDC
to 3 amps; load limit 816.4 kg (1,800 lb); ultimate load 1224 kg
(2,700 lb); useable cable length to 88 m (290 ft); cable
over-tension clutch provides overload relief; payout swivels to
accommodate non-vertical loads to 30 deg from centre; typical
application: Bell 212/412/430/UH1, Sikorsky S-76, Lynx, Agusta
A109 and Kawasaki BK117.
44301 EXTERNAL ELECTRIC RESCUE HOIST
Hoist height 31.3 cm (12.3 in), hoist width 22.22 mm (8.75 in).
Weight for 44301-10-5 system 37.70 kg (83 lbs), weight for
44301-10-4 system is 41.80 kg (92.11 lbs). Cable usable length for
44301-10-5 system is 50 m (164 ft), cable usable length for
44301-10-4 system is 90 m (300 ft). Rated speed (nominal)
60.96 mpm (200 fpm) at 136.08 kg (300 lb) load; 36.1 mpm (150
fpm) with 45.72 kg (100.79 lb) load. Cable diameter 0.47 to 0.49
cm (0.188 to 0.194 in).
76300-200 PNEUMATIC HOIST
227 kg (500 lb) force capacity; 24 m (80 ft) usable cable length,
80 ft/m rated speed, 18 kg (40 lb) weight, 27 V.de electrical
power. Safety features include limit travel stops up and down,
cable cutting cartridge.
70
Public Service Aviation Handbook 2008-09
76378-200 ELECTRIC HOIST
272 kg (600 lb) force capacity, 91 m (297 ft) usable cable length,
0-0-45.7 m (0-150 ft/min rated speed), 44.7 kg (98.6 lb) weight,
unlimited number of consecutive lifts under max load and over
max length., 27 V.de electrical power. Safety features include
self-clamping carbon brake, automatic end limit stops, cartridgeoperated emergency cable cutter protected against EMI,
automatic slow down near cable ends, temperature monitoring,
cable length indicator, cycle totalizer.
» TECHTEST LTD (PART OF THE HR SMITH
GROUP OF COMPANIES)
An established supplier of quality emergency distress
transmitters and homing-locating systems, Techtest Ltd offers
one of the most comprehensive portfolios of Search and Rescue
equipment available today. Ranging from lightweight portable
beacons to fixed and deployable emergency transmitters,
Techtest products operate on the 406 MHz SARSAT frequency
to ensure the fastest possible satellite detection times and
accurate identification and locating. An integral GPS option
provides added improvements in locating time and accuracy,
further enhancing survival and rescue prospects. In addition, all
transmitters provide a homing signal on standard distress
frequencies.
SERIES 503 EMERGENCY LOCATOR
TRANSMITTER
The Techtest Series 503 Emergency Locator Transmitter (ELT)
and the deployable Crash Position Indicator (CPI) offer added
capability by rapidly pinpointing and broadcasting the location
of an emergency without any action from the crew. Activated
automatically in the event of an accident, these systems
transmit the aircraft’s last known GPS position as part the 406
satellite message. The CPI also deploys automatically from the
aircraft and its buoyant design ensures that it continues to
transmit the precise location of the crash site, long after the
aircraft has submerged and regardless of any subsequent tidal
drift.
SERIES 500-27 GPS
Crew members equipped with the Series 500-27 GPS personal
beacon can be separately identified and located by satellite,
thereby giving rescue forces precise information on individual
survivors. A two-way speech capability also provides an
essential voice link for use when the rescue team is within sight. SERiES 406 HOMER-DECODER SYSTEM
Techtest delivers major capability improvements for Search &
Rescue operations with its range of Series 406 Homer-decoder
systems. By decoding and displaying real-time 406 MHz
message data, including the latitude and longitude of
location-protocol emergency transmitters, the stand-alone
system can simultaneously track up to 10 beacons, thereby
facilitating a rapid transit directly to the site of an incident. A
portable, carry-on airborne 406 decoder is also available.
» LIFESAVING SYSTEMS CORP (LSC)
HELICOPTER RESCUE & SURVIVAL EQUIPMENT
Products include helicopter hoist hook, hoistable litters and
baskets fabricated of titanium or stainless tubular components,
flotation kits, hoistable rescue swimmer/crew harness, rescue
strops, and personnel life support equipment including
inflatable flotation collars, emergency egress devices and
signalling equipment.
» LITE FLITE ApS
ESCAPE RESCUE PLATFORM
Escape is a folding rescue platform designed for fast evacuation
of people from situations in which the helicopter cannot land.
The platform attaches to a helicopter’s belly hook via a load
strop and can carry a number of people up to 1,500 kg (3,306
lb). The company says that the helicopter can deploy the basket,
allow the people to board and fly away within seconds.
HOIST HARNESS SYSTEM
Harnesses in use with several military and civilian rescue
services has ‘unique’ features for maximum comfort and
effectiveness during a rescue. All adjusters, lugs and rings are
maintenance-free stainless steel. It has a guideline ring and
strap for swim-fins, and a unique elastic suspension to facilitate
swimming and walking.
QUICK RELEASE BOX
The LF Mk-2 quick-release box is almost maintenance-free
and corrosion treated stainless steel and is able to open
under tension.
RESCUE SLING
Rescue sling is made from MIL-W-4088 Type 7 nylon webbing,
with a tensile strength of 2,700 kgp. Hardware is stainless steel.
It features a unique self securing hand grip device as well as an
extra safety strap and a towing grip. Colour is fluo-orange with
three silver reflex stripes. Buoyant padding makes the sling float
for easy handling.
GUNNER BELT
Secures the winch man in the open door.
» MULTIFABS SURVIVAL LTD
SAR RESCUE SWIMMER SUIT
Suit manufactured with colour break in the sleeves and
retro-reflective tapes to increase visibility with extended neck
yoke with mesh drainage and grip patches to secure a neoprene
hood. The suit is fitted with an expandable lycra back panel to
increase comfort and is tailored for use in water.
» PRECISION LIFT, INC
HELI-BASKET
Ready to fly with multi-purpose spreader bar, tie-down straps,
safety net and cabling - for supply of medicine and first-aid
supplies, rescue tools and hazmat tools or for transporting
injured victims and responders; dimensions 137 x 259 cm (4.5 x
8.5 ft); empty weight 250 kg (550 lb); payload 2,045 kg (4,500
lb); gross weight 2,295 kg (5,050 lb); corrosion protection;
powder-coat, baked-on paint finish on all aluminium surfaces;
welding in accordance with MIL-W-8604 or MIL-W-8611 as
applicable to the materials being joined and the welding process
being employed.
» PZL SWIDNIK
W-3RM ANACONDA SAR MISSION EQUIPMENT
Two pilots, two rescue crew members, physician; up to eight
survivors; emergency flotation gear; electric hoist with 164 ft
(50 m) cable, 272 kg (599 lb) capacity, lift rate 0.75 m/sec (2.4
ft/sec); external cargo sling for loads up to 2,100 kg (4,629 lb);
SX-16 Night Sun; observation system (TV + FLIR) with ground
datalink subsystem for FLIR; inflatable 10-person raft; rescue
belts, rescue basket for two people or folding stretchers for
hoisting survivors aboard; weather radar; GPS navigation; EFIS;
provides a solution to rapid mission profile changes.
» RED UK LTD (RESCUE, EXPLORATION &
DIVING UK LTD)
AEROHAWK HELICOPTER STRETCHER SYSTEM
Lightweight carbon fibre composite; four independent casualty
restraints; accept vacuum mattresses and other spinal splints
without repackaging of patient; aerodynamic design reduces
spinning motion during winching.
visit us at www.shephard.co.uk
SHEPHARD
71
» SURVIVAL PRODUCTS INC
EPIRB
BASIC LIFE RAFT
Class B miniature personal EPIRB (emergency position
indicating radio beacon) homing beacon; lightweight, powered
by standard 9V Lithium batteries; black rubber loop antenna,
designed to be worn around the neck; antenna can be
disconnected at one side of the casing to extend the antenna if
required; frequency is 121.5 MHz; activated manually by pressing
the large button or automatically after the unit is armed and
immersed in water for approximately 20 seconds.
Comprised of a buoyancy tube, deck, life lines, boarding handles,
CO2 automatic inflation system, retaining line, hand pump, bailing
bucket, sea anchor and valise; Four-man (Bulkhead) Basic RAF1104-101 and Eight-man (Bulkhead) Basic -RAF1108-101; FAA
TSO approved and have been manufactured for commercial and/or
private aviation purposes. Dimensions: Four-man (packaged) 10.16 x
33 x 10 cm (4 x 13 x 16 in), weight 7.3 kg (16.2 lb); Eight-man 12 x 33
x 41 cm (5 x 13 x 16 in) weight 10 kg (21.2 lb). Rafts obtained with
canopy only or with FAR 91, 121, 135/125 survival equipment kits.
» SEARCH & RESCUE PTY LTD
PRECISION AERIAL DELIVERY SYSTEM (PADS)
Deployable over land and sea; canister is of moulded
polyethylene measuring 82 cm (32 in) height x 45 cm (17.7 in)
(diameter); PADS unit includes canister, towing/release
mechanism, flotation layers, 330 m (1.082 ft) trail line, skirt
(durable cover), control band and rubber bands; maintenance
performed at intervals not exceeding 90 days.
» SEMS AEROSAFE
LIFE JACKET
Slim-fit lifejacket designed for light aircraft crew and
passengers; blue protective cover prevents chafe and damage
to the inflatable stole which provides approximately 18 kg (40
lb/175 Newtons) of buoyancy; worn ready to use, no unfolding or
tying of tapes is required; self-righting; oral top-up valve is
fitted; leg strap eliminates the jacket riding up on the wearer
whilst in the water; bright orange, fitted with strips of
retro-reflective tape, a whistle and a light; adjustable to fit most
sizes of adults and is suitable for children down to 135 cm (53 in)
height and 61 lb (28 kg) weight. Optional: spray-hood and
waistbelt pouches.
» SKEDCO INC
SKED STRETCHER
Performs the functions of a stokes and basket type stretcher;
dimensions: rolled in cordura pack 23 cm (9 in) diameter x 91.44
cm (36 in) length, laid flat 91 cm (3 ft) x 243 cm (8 ft); weight
8.6 kg (19 lb); material - low density E-Z glide polyethylene
plastic; temperature range - begins to melt 450 deg F to 500
deg F (usability to -120 deg F without becoming brittle);
horizontal lift slings - webbing tensile strength 4,535 kg (10,000
lb); vertical lift sling - rope tensile strength 2,630 kg (5,800 lb).
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Public Service Aviation Handbook 2008-09
» SWITLIK PARACHUTE CO INC
HELICOPTER CREW VEST (HV-35C)
Breathable mesh back; integral side pockets for strobe, radio,
flares, whistle, etc; may be worn with shoulder and lap safety
belts; buoyancy 17.24 kg (38 lb); inflation system two each 18 g
(0.03 lb) CO2 cylinders; weight 1.3 kg (2 lb 15 oz) approx.
» TADIRAN SPECTRALINK LTD
ASARS-G AIRBORNE SEARCH AND RESCUE
SYSTEM
Latest generation Combat SAR System with GPS. ASARS-G
consists of the ARS-700 Airborne Interrogator and Guidance
System (AIGS), with over-the-horizon pinpointing capability (via
airborne relay support), and the PRC-434G/SV Personal Survival
Radio, with embedded GPS receiver and navigational
capabilities combined in a single compact unit; large position
location display with user-friendly interface; frequency range
225-229.975 MHz; 3,000 channels; battery life 15 hr @ 1:10 T/R
ratio, 24 hr @ 121.5 MHz; operating temp -40 deg C to 55 deg C;
encrypted data channel at all available frequencies for
transmission, reception and relaying of present position, route
and waypoints; long life battery.
DDU-700 DIGITAL DATA UNIT
Compact airborne CSAR system for integration into all types of
military aircraft, providing them with SAR functionality. Using covert
data messages and unique ID codes, the DDU-700 can interrogate
survivor’s Personal Survival Radio and extract GPS location data, for
display on the unit’s wide display panel or on existing onboard MFD.
system. Modes of operation include: test, interrogation (single/
continuous), messaging, and erase (on an emergency, the Erase
mode enables erasing all critical parameters stored in memory).
Size: 100x127x130 mm (HxWxD); Weight: approx. 2 kg (4.4 lb).
( 631) 752-12 4 0
( 631) 752-12 4 2
w w w. t r ans ae r oinc.com
M AI N :
FAX:
W EB :
» SEA MARSHALL RESCUE SYSTEMS LTD
35 M ELV I LLE PAR K R OA D
SUI T E 100
M ELV I LLE, NY, U. S . A . 1 1 7 4 7
Fits Bell Helicopter UH-1, 204, 205, 212 and 412; mounted either
on the ceiling or the floor of all five models; 2-speed hand
operated self-tailing winch with Harken speed grip aluminium
handle, or Titan floating handle; gear ratio 2.2 to 1 and 6 to base
plate 24” x 26” x 1/4” thick 6061, T-6511 anodized alloy
aluminium; weight: 0.79 kg (28 lb) hoist 30 m (100 foot) 1.27 cm
(0.5 in) Static Kernmantle rope and all necessary hardware is
supplied. Rappelling Bar; is available through SkyHook: The
Rappell Bar completes the manual hoist as an above the door
attachment point and doubles as a rappelling hardpoint.
With locations worldwide Transaero
can offer sales support and technical
assistance, in real-time to many
overseas customers.
SkyHook Helicopter Rope Manual Hoist system.
Mechanically deployable liferaft system for helicopters and
fixed-wing aircraft; 15 second inflation time; design approved for
150% overload accommodation; fully reversible ensuring
upright inflation; automatic inflation of canopy supports; canopy
design provides low profile reducing wind effect; exposure
protection; canopy speedily laid flat for rescue; buoyancy tubes
constructed from ultra-lightweight PU (polyurethane) coated
fabric; short and long mooring lines enabling dry shod boarding;
reversible ramps; internal and external stowage of raft; eight
models available - CAA and/or FAA approved - capacity (rated)
from seven to 18 persons.
Flight Helmets
Ballistic Ground Helmets
Parachutists Helmets
Oxygen Breathing Equipment
Helicopter Escape Breathing Devices
Night Vision Goggles
Night Vision Goggles Testing Equipment
Wireless Radio Systems
Air Crew Personal Hygiene Products
Military Clothing
Rescue Beacons
Communication Equipment
Immersion Suits
Chemical Defense Protective Gear
Hoists
Anti-Exposure Clothing
Safety Belts
Harnesses
HELIRAFT
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
•
» SKYHOOK RESCUE SYSTEMS INC
Some of the many products offered by Transaero,
include but are not limited to:
» RFD BEAUFORT LTD
Transaero offers a wide range of safety and survival equipment for
Airborne, Marine and Ground Troops, as well as many vehicle applications.
SAR » Search and rescue
FIREFIGHTING » Equipment
PRC-434G/SV “ALL-IN-ONE” PSR
Cospas/Sarsat-enabled Personal Survival Radio (PSR) for
combat and non-combat SAR operations, based on softwaredefined radio (SDR). Advanced features include GPS geolocation
response to interrogations from the airborne system or another
PSR, secured two-way messaging, navigation along dozens of
pre-programmed waypoints, and battery life up to 96 hours in
“Sleep” mode. The PRC-434G/CS is fitted for operation at the
406.025 MHz frequency of the Cospas-Sarsat emergency
satellite constellation, thus effectively substituting for an
Emergency Locator Transmitter (ELT). A Thermal Beacon can be
added to this PSR to further facilitate survivor pinpointing and
final approach for first-pass pick up.
» TRANSAERO INCORPORATED
Headquartered in Melville, New York, Transaero Incorporated
has traded for over fifty years as a major supplier of a range of
aerospace products, including subsystems specifically related to
the emergency medical services and search and rescue worlds.
During this time, the company has built its reputation as a firm
dedicated to the efficient sale and distribution of aerospacerelated material. The company keeps in excess of $20 million in
its inventory and can perform off-the-shelf delivery thanks to
computerised inventory control. Fax quotations and same day
shipments can also be supplied to customers. The company has
a truly global presence in Australia, Dubai, UK, Germany, India,
Israel, Italy, Malaysia, USA, Singapore, South America, Sweden
and Taiwan.
» TYPHOON INTERNATIONAL LTD
OVERWATER FLIGHT SUIT (OFS)
Immersion suit that keeps wearer 100% dry in the unlikely event
of ditching. The fabric, Taslan, produced by WL Gore and
Associates, has a special breathable membrane; back stretch
panel allowing a comfortable forward leaning position; pre-bent
knees prevent fabric buckling; chafing patches protect neck seal
from harness straps; neck seal is trimmable should it be
necessary to fit a larger neck. Includes: cuff seal cover; thigh
pocket; pocket with donning instruments; pencil pocket; fabric
socks and elasticated waist section. Sizes: extra small 84 to 91
cm (33 to 36 in) to extra large 107 to 114 cm (42 to 45 in) (chest)
and extra small 158 cm (5 ft 2 in) to 168 cm (5 ft 5 in) to extra
large 189 cm (6 ft 2 in) to 198 cm (6 ft 5 in) height.
AIRCRAFT
SPECIFICATIONS
EMERGENCY MEDICAL
SERVICE
LAW ENFORCEMENT
» VIKING LIFE-SAVING EQUIPMENT
SEARCH AND RESCUE
IMMERSION SUIT (M5002)
Allows the wearer to turn from a face-down position to face-up
within five seconds; ensures that the body’s core temperature
does not fall more than 2 deg C after a period of six hours in
water with a temperature of between 0-2 deg C.
FIREFIGHTING
guide to OPERATORS
VIKING 1 SOLAS LIFEJACKET (M9308)
Twin-chamber; high visibility in low light conditions; red cover,
orange buoyancy chamber; fitted with retro-reflective trim;
emergency light; whistle; buddy line; lifting bucket and crutch
strap; dimensions (l x w x h) 28 x 59 x 8 cm (11 x 23 x 3 in);
weight 1.75 kg (3.8 lb) ; buoyancy 180 Newton.
ACTIVITY GUIDE
GUIDE TO SUPPLIERS
PRODUCT GUIDE
EQUIPMENT
FIREFIGHTING
SHEPHARD
HELICOPTER FIREFIGHTING
TECHNOLOGY AND TECHNIQUES
Conference
This covers products such as under-slung fire buckets, water and foam
delivery and refill systems for helicopters and fixed-wing aircraft.
14 October 2008
The section begins with an article on the steps being taken by the
European Union to combat the increased risk of wildfires in member
countries across the continent.
Hotel Quinta da Marinha, Estoril,
Nr Airport Cascais, Portugal
www.shephard.co.uk/AerialFire
74
Public Service Aviation Handbook 2008-09
All products listed in this section come under the heading of
Firefighting Equipment.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.
VIEW » Tom Withington
Fire-fighting infrastructures « VIEW
HOT TIMES IN THE
MEDITERRANEAN
By Tom Withington
Savage forest fires in southern Europe in 2007 has prompted the European Union to look
afresh at developing a continent-wide aerial fire-fighting infrastructure.
E
rickson Sky Crane recently signed a contract with
the Italian government for the continued provision
of four S-64 Aircrane aircraft, based in Italy for
fire-fighting and disaster relief work. The lease of the S-64
aircraft began in 1999 with a single Helitanker based on the
island of Sardinia. Since then, the Italian fleet has grown in
size and the provision of the four aircraft will continue until
2016 under the terms of the June 2008 contract.
Fire departments around the US are continuing their
investment in helicopters to assist with the coordination of
fire-fighting efforts in their catchment areas. The Chicago
Fire Department has purchased a Bell 412 which joins an
existing type already in service to perform fire-fighting
command and control duties as well as search and rescue
(SAR) operations around the Lake Michigan area.
Meanwhile, the San Diego fire department has also
invested in a Bell 412, which will join the city’s Bell 212
aircraft to assist with SAR and fire-fighting, as well as
medical evacuation. The purchase of the Bell aircraft
» Eurocopter’s EC 225/725 could have a bright future in
firefighting as Europe’s wildfire seasons get hotter.
76
Public Service Aviation Handbook 2008-09
represents a departure for the city’s fire department which
had previously contracted fire-fighting helicopter support
services from a private firm. However, this changed in
2005 when the organisation decided to purchase its own
dedicated aircraft. The purchase was also made to
pre-empt the arrival of the Santa Ana winds which usually
begin in August and which can help the spread of
devastating wildfires.
CALIFORNIAN INVESTMENT
Furthermore, Bell 412 aircraft have been purchased by
Orange County in San Diego to assist the County Fire
Authority. The purchase of the four aircraft represents a
significant investment following the Santiago fire in 2007
which caused widespread destruction around California’s
Santiago Canyon.
Other Californian fire departments which have invested
in their aviation support over the past twelve months include
Los Angeles City Fire Department that has purchased a
single Bell 412 to supplement its fleet of three Sikorsky S-70
Firehawks, six Bell 412 aircraft plus a single Bell 206. The Bell
412 is equipped to perform
night-time water drops on
wildfires. However, a single aircraft
from the fire department’s existing
Bell 412 fleet will be sold off once
the new aircraft is delivered.
Another country wracked by
serious wildfires is Australia and,
in December 2007, a specially
converted Sikorsky S-61 began
duty supporting fire-fighters in
the west of the country. The
aircraft had undergone a
comprehensive upgrade by
Carson Helicopters with the
installation of new composite
rotor blades, which increased the
aircraft’s maximum take-off
weight, together with the addition of a belly
tank for fire suppressant materials. The
aircraft can also carry up to 15 fire fighters to
give a ‘rapid response’ capability.
Following the devastating fires which
ravaged Greece in 2007, the European
Union (EU) was working to develop an
integrated mechanism for a coordinated
continental response to the problem of
wildfires. The European Commission’s
Civil Protection Mechanism, the EU
body which helps coordinate the EU’s
disaster response, is working to
establish groups of personnel and
aircraft around the EU which can be
organised into a common system of
rapid response fire-fighting means
for the suppression of forest fires
before they develop into larger
conflagrations. Aircraft had to
be drafted in from Russia and
also from air forces across
Europe to help contain the
Greek fires.
One solution being touted
is the development of a
European water-bomber
fleet as the destructive
effect of forest fires can be
seriously mitigated if they
are discovered early;
hence aircraft armed
with water-bombing equipment, whether
fixed-wing or helicopters, can have a
major effect.
Meanwhile, Eurocopter has touted
the potential of its EC 225 aircraft as a
fire-fighting platform deploying it to
Corsica in 2007 as an on-site asset
ready to deal with wild fires. The
helicopter, which is routinely used
for search-and-rescue work, was
provided on loan from the French
Air Force to the country’s Sécurité
Civile civil protection organization.
However, the trial was judged to
be a success and Eurocopter will
now deliver an EC 225 configured
for fire-fighting to the
Mediterranean island in summer
2008. Spain has also invested
in fire-fighting aircraft, buying
five Eurocopter AS 532
helicopters and a pair of EC 135
aircraft to assist in fire-fighting
operations. Together with Italy,
Spain and Portugal, France is
already involved in a
unified fire-fighting force
called ‘FireFour’ which
has been raised to provide
coordinated fire-fighting
and earthquake
response. ±
visit us at www.shephard.co.uk
SHEPHARD
77
FIREFIGHTING » Equipment
Equipment « FIREFIGHTING
FIREFIGHTING EQUIPMENT
» AERO UNION
AIRBORNE FIRE FIGHTING SYSTEM
(For C-130 Hercules) AFFS is a fire fighting system for the C-130
developed for the USDA Forest Service with the help of
Lockheed Martin and the US Air National Guard. AFFS is set to
replace MAFFS used on Air National Guard C-130s. Delivers up to
15,141 litres (4,000 US gal) of retardant or water/foam using a
variety of drop profiles required to attack various fire
conditions. Delivers coverage up to level Eight (30 litres/eight
gallons of fire fighting fluid per nine square metres/hundred
square feet), which is the maximum level required by the Forest
Service and double that of the older MAFFS. New features
include an integral compressor that permits in-flight recharging
of pneumatic supply and a discharge scheme that avoids
contaminating the aircraft’s surfaces during a drop.
AFFS-equipped C-130s can fly fully pressurised to and from the
fire site and remain pressurised during the drop. Extensive use
of composite materials saves weight and eliminates corrosion.
AFFS weighs about 227 kg (500.5 lb) empty, roughly half the
weight of an equivalent MAFFS.
MODULAR AIRBORNE FIRE FIGHTING SYSTEM
(For C-130 Hercules) MAFFS is a roll-on, roll-off fire fighting
system designed for rapid conversion of Hercs equipped with
USAF 463L cargo handling equipment. This self-contained,
reusable 11,356 litres (3,000 US gal) aerial fluid dispersal system
is also adaptable to a wide variety of rear-loading heavy
transport aircraft. Pneumatically powered, it consists of tank
modules, a control module and a dissemination module.
Electrical power is provided by the aircraft or by a 24 volt
battery on the control module. MAFFS permits variable quantity
drops, with volume and flow rate pre-selected at the control
module, depending on the method of attack selected. At
maximum flow rate, it can discharge its entire load in under five
seconds. The water/retardant discharges alternately from a
series of tanks to ensure that the centre of gravity remains
within limits.
RADS III FIREHAWK
(For the S-70A/UH-60L Black Hawk) 3,785 litres (1,000 US gal)
water tank for Sikorsky Black Hawk. Equipped with a 113 litres
(30 US gal) foam tank, a 3,785 litres (1,000 US gal) per minute
snorkel and computer-controlled doors. The Firehawk can pick
up 15 fire-fighters, deliver them close to the fire and then
commence dropping water/foam. Using the snorkel hose, the
tank can be filled in approximately 60 seconds from a variety of
water sources. A Kit (fixed provisions): Water tank fuselage
attachment lugs; wiring associated with cockpit control panel
and civilian radios; landing gear extension fitting; B Kit
(removable provisions): water tank 3,785 litres (1,000 US gal);
water pump-snorkel 3,785 litres ((1,000 gal) per minute;
extended landing gear; cockpit control panel, civilian radios;
pilot lower rear-view mirror; installation/removal of water tank
takes around four hours.
78
Public Service Aviation Handbook 2008-09
RETARDANT AERIAL DELIVERY SYSTEM I
(For C-130 Hercules) RADS I uses a computer-controlled door
system that offers flow rate combinations selected by the flight
crew. The 11,356 litres (3,000 US gal) tank provides flexibility in
line lengths and coverage levels. The tank is a two part
installation. Weighing 226 kg (500 lb), the lower tank and
operating mechanisms are permanently installed in the aircraft.
The upper tank attaches at the floor line and can be removed to
convert the aircraft back to the cargo configuration. RADS is
designed to provide a continuous and uniform drop pattern with
no overlapping or gaps. It is certified by the FAA under FAR
21.25.
RETARDANT AERIAL DELIVERY SYSTEM II
(For the P-3 Orion/L-188 Electra) The RADS II constant flow,
11,356 litres (3,000 US gal) belly tank is available for both the
Lockheed P-3 Orion and the L-188. The RADS II system employs
a patented, computer-controlled door system that offers flow
rate combinations selected by the flight crew. The capacity tank
provides flexibility in available line lengths and coverage levels.
This computerised digital control logic enables the pilot to
select and control coverage level and quantity to produce the
desired drop pattern. It is certified by both the FAA and
Transport Canada, has been flight tested by the US Forest
Service and is Interagency Airtanker Board (IAB) approved.
» ERICKSON AIR-CRANE INCORPORATED
FIRE FIGHTING EQUIPMENT
(For S-64 Helitanker) Water tank: 10,000 litre (2,650 US gal)
tank drops water, retardant or foam mix. Microprocessor
controlled tank doors offer eight individual coverage level
options. Refill pump/ram scoop: Flexible hose snorkel features a
high pressure impeller and can draw water from any water
source 45 cm (18 in) or deeper as fast as 45 seconds. A ram
scoop hydrofoil allows the Helitanker to refill from fresh water
and sea water sources in less than 45 seconds. Water cannon:
Optional 1,136 litre (300 US gal) per minute water cannon
certified, intended for wild land, urban interface and high rise
structure fire suppression.
» Isolair Helicopter Systems
Eliminator II model 4600
Water and foam dispensing tank with hover fill pump system for
a range of Bell, Eurocopter and PZL Swidnik helicopters.
Eliminator II Specifications for Bell Model 205A-1, 212, 412 and
412EP Helicopters: tank assembly height 35.5 cm (14 in); tank
assembly width 223.5 cm (88 in); tank assembly length 228.5
cm (90 in); net weight 190 kg (418 lb); gross weight 1,467 kg
(3342 lb); system capacity 1,223 litres (323 US gal)); chemical
capacity 103 litres (27 US gal); power requirements 24 vdc, 90
amps; hover fill rate, maximum 1,022 litres per minute (270 US
gal p/m).
» SEI INDUSTRIES
» SIMPLEX MANUFACTURING COMPANY
BAMBI BUCKET
BIG DIPPER SERIES
Foam compatible bucket system includes an outward opening
dump valve which allows a solid column of water or foam to be
dropped. Variable fill capability, fast fill and shallow water
capability. Pilot controlled dump patterns. Eighteen sizes
available: 275 to 9,480 litres (72 to 2,600 US gal). The resulting
column of water generated allows the pilot to drop from a
higher altitude thereby reducing downwash and pilot risk. The
Instant Deployment System (IDS) ensures rapid set up; the
Bambi Bucket is deployed simply by removing it from the
carrying bag, attaching the control head to the cargo hook and
attaching power. As soon as the weight of the Bambi Bucket is
taken by the suspension lines, it instantly deploys.
Under-slung bucket system for helicopters ranging from light to
heavy cargo helicopters Capacities: 379, 530, 947, 1,514, 2,271,
2,839, 3,785, 7,571 litres (100, 140, 250, 400, 600, 750, 1,000
and 2,000 US gal). Standard cable lengths: 12 ft (378 and 529
litres/100 and 140 US gal), 18 ft (947, 1,514 and 2,271 litres/250,
400 and 600 gal), 25 ft (2,839 and 3,785 litres/750 and 1,000
US gal), 45 ft (7,571 litres/2,000 US gal); custom lengths
available. Empty weights: 48, 56, 90, 139, 161, 259, 277 and 363
kg (106, 123, 198, 308, 356, 570, 610 and 800 lb).
FIRESOCK
Water and foam dispersal accessory for Bambi Bucket range.
Designed to increase uniformity, length and width of drop
pattern by spreading water or foam over a wider area with
greater consistency.
HEAVY LIFT BAMBI BUCKET
Re-engineered for greater durability, these buckets are offered
for Black Hawk and Chinook class helicopters in six sizes from
2,500 to 9,480 litres (660 to 2,600 US gal). New features
include: 2,500% more durable fabric reinforced polyurethane
shell; solid ballast modules outside bucket as extra abrasion
barrier; laterally reinforced battens are stronger, more
split-resistant; cast Instant Deployment System hub, stronger
spokes; stainless steel triangle rings to reduce abrasion on more
durable suspension system M-straps; FCAS cinch strap now
made from heavy duty cargo webbing with stainless steel
hardware and moved outside bucket; larger mounting brackets
for better IDS support; stainless steel wear plates on bucket
bottom; thicker bottom cable.
SACKSAFOAM
Foam injection systems for Bambi Buckets. Sacksafoam I for
smaller buckets has foam dispensing unit inside bucket and
control unit in cockpit. Sacksafoam II will carry two 19 litres (5
US gal) cans of foam concentrate inside the helicopter and
pump a predetermined amount of foam concentrate down to a
Bambi Bucket. The control box is included, for remote mounting
on or near the helicopters’ dashboard. Sacksafoam III designed
for bucket models 5566 to HL9800. Carries up to 94 litres (25
US gal) of concentrate. Control box built into lid.
TWIN HEAVY LIFT BAMBI BUCKET
Two-bucket system designed for Mi-26 heavy lift helicopter.
Three twin-bucket packages offered: 5,000 litres (1,320 US gal)
HL5000 buckets, 7,570 litres (2,000 US gal) HL7600 buckets
and 9,840 litres (2,600 US gal) HL 9800 buckets. All include 1 x
control system (Mi-26), 2 x trouble shooter kits, 1 x spreader bar
and friction swivel.
HELI TORCH
Used world-wide for aerial ignition of forest slash, backfires,
habitat improvement and oil spills. Designed to operate under
any helicopter with a cargo hook and 28 VDC power. Used with a
fire boom, it can ignite and burn off approximately 600 barrels
of oil or approximately 100 tons of spilled oil in 1 hour. Propane
ignition system supplies reliable, uniform ignition to produce a
consistent stream of fire. Model 5400 includes two 208 litres
(55 US gal) drums and single point suspension as standard
equipment. Optional equipment: Drum transfer kit, trailer, mix
transfer system, fan tip, Sure Fire (Gelling fuels) Net weight: 86
kg (190 lb) Capacity: 208 litres (55 US gal).
MODEL 301 FIRE ATTACK
Belly tank/refill hose system for Eurocopter AS365 series Net
weight: 136 kg (300 lb) Gross weight: 1,036 kg (2,286 lb) Water
capacity: 900 litres (238 US gal) Retardant capacity: 90 litres
(24 US gal) Hover refill pump rate: 1,212 litres per minute (320
US gal p/m) VNE: 140 KIAS
MODEL 304 FIRE ATTACK
Belly tank/refill hose system for Bell UH-1H, 205, 212, 412 series
Net weight: 163 kg (360 lb) Gross weight: 1,582 kg (3,487 lb)
Water capacity: 1,420 litres (375 US gal) Retardant capacity:
143.1 litres (36 US gal) Hover refill pump rate: 1,212 litres per
minute (320 US gal p/m) VNE: 110 KIAS
MODEL 308 FIRE ATTACK
Belly tank/refill hose system for Bell 407 Net weight: 136 kg
(300 lb) Gross weight: 1,036 kg (2,286 lb) Water capacity: 900
litres (238 US gal) Retardant capacity: 90 litres (24 US gal)
Hover refill pump rate: 1,212 litres per minute (320 US gal p/m)
VNE: 140 KIAS
MODEL 310 FIRE ATTACK
Belly tank/refill hose system for Eurocopter AS350, 355 series
Net weight: 115 kg (254 lb) Gross weight: 1,115 kg (2,458 lb) Water
capacity: 900 litres (238 US gal), 1,100 litres (291 US gal) and
1,200 litres (317 US gal) Retardant capacity: 100 litres (26 US
gal) Hover refill pump rate: 1,212 litres per minute (320 US gal
p/m) VNE: 120 KIAS
visit us at www.shephard.co.uk
SHEPHARD
79
FIREFIGHTING » Equipment
MODEL 328 FIRE ATTACK
Belly tank/refill hose system for Kamov Ka 32 Net weight: 598
kg (1,298 lb) Gross weight: 3,692 kg (8,139 lb) Water capacity:
2,952 litres (780 US gal) Retardant capacity: 151 litres (40 US
gal) Hover refill pump rate: 3,028 litres per minute (800 US gal
p/m)
MODEL 311 FIRE ATTACK
Belly tank/refill hose system for Eurocopter Kawasaki BK 117 Net
weight: 130 kg (268 lb) Gross weight: 799 kg (1,762 lb) Water
capacity: 620 litres (177 US gal) Retardant capacity: 78 litres (20
US gal) Hover refill pump rate: 1,212 litres per minute (320 US
gal per minute)
MODEL 326 FIRE ATTACK SYSTEM
Production of a new tank for AW139 helicopter operated by Los
Angeles City Fire Department. Due to enter service shortly.
Flight test complete.
SMARRT
» SPEGEL
SEMAT FIRE BUCKETS
A range of helicopter fire buckets available in versions suitable
for liquid, gel, powder and pulverised media of various types in
capacities from 550 up to 10,000 litres (145 up to 2,642 US gal).
Types: F is for fluid media and gel based polymers; FPG is for
fluid, dry pulverised and granulate media (such as oil absorber).
All SEMAT buckets work on the patented lifting-case principle,
proven for over 20 years, in which the case lifts off the base to
release the contents. The gap controls the flow rate: dump
position opens a 16 cm (6.2 in) gap and empties the bucket in 3
seconds; spray position uses a gap of 0.5-1.5 cm (0.19-06in)
providing 15-30 sec of spray time. Remote control by cable with
30 bar display or radio with seven channels on ISM or NOE
frequencies (120-960 MHz only for export). The electricpneumatic control system is independent of helicopter sources.
The pneumatic reservoir can complete more than 150 cycles
before recharging.
AIRCRAFT
SPECIFICATIONS
EMERGENCY MEDICAL
SERVICE
LAW ENFORCEMENT
SEARCH AND RESCUE
FIREFIGHTING
SMAART (Simplex Manufactured Aerial Residue Removal
Technology) is a new system designed for the cleaning of power
line insulators. Currently being flight tested for FAA
certification.
guide to OPERATORS
ACTIVITY GUIDE
GUIDE TO SUPPLIERS
PRODUCT GUIDE
Conference and Exhibition
SHEPHARD
5 - 6 November 2008
Olympia Conference Centre, London, UK
DIRECTORY
GUIDE TO OPERATORS
This section gives fleet and contact details for public service aviation operators
around the world. Companies are listed alphabetically in country order.
Entries include:
± Company name
± Address
± Telephone and fax numbers
± Email addresses
± Website urls
± Contact names
± Company activity
WORKING TOGETHER:
DEVELOPING NATIONAL AND INTERNATIONAL
CROSS-BORDER COOPERATION
SHEPHARD
Untitled-3 1
80
Public Service Aviation Handbook 2008-09
The Activity Guide on page 133 lists all operators by area of activity.
www.shephard.co.uk/police
17/06/2008 16:53:59
To update an entry or submit information for publication in the next handbook or
online directory, go to www.shephard.info/hbr.htm and complete the electronic
registration form. Alternatively, fax Mohan Sadasivan on +44 (1628) 669789 or
send an email to directory@shephard.co.uk specifying Public Service Aviation
Handbook as the subject.
While every effort has been made to
provide accurate information, the
publishers cannot be held responsible
for errors or omissions. If you have any
comments, additions or corrections you
would like to be made please contact
the editor.