Vector`s STC Catalogue - Helitech International

Vector`s STC Catalogue - Helitech International
SETTING THE STANDARD OF CUSTOMER SERVICE
STC
Catalogue
SETTING THE STANDARD OF CUSTOMER SERVICE
ORDER INFORMATION
Helicopter Services - Richmond
4551 Agar Drive, Richmond
British Columbia, Canada V7B 1A4
Tel: 604.276.7600 I Fax: 604.276.7667
Helicopter Services - Alabama
22378 Billie Blackmon Road, Andalusia
Alabama, USA 36421
Tel: 334.222.1277 I Fax: 334.222.1954
Email: sales.hsna@vectoraerospace.com
Phone: 1.888.729.2276
Helicopter Services - Langley
#101B - 5947 206A Street, Langley
British Columbia, Canada V3A 8M1
Tel: 604.514.0388 I Fax: 604.514.0389
INDEX
SETTING THE STANDARD OF CUSTOMER SERVICE
S61
FAA STC SR02336AK VFR-IFR Rockwell Collins/SAGEM Electronic Display System with Dual AHRS
TCCA STC SH97-42 Replacement Avionics Shelves
FAA STC SR02335AK DC Fuel Quantity System
FAA STC SR09236RC Modular Wiring Harness
STC SRO2279AK Rockwell Collins Four (4) Display FDS Electronic Flight Instrument System Upgrade with
Dual AHRS
FAA STC SR09232RC Solid State Static Inverter
FAA STC SR09233RC Solid State Voltage Regulator
FAA STC SR00283SE Fifty Inch Section Removal from Forward Fuselage between Stations 110 and 160
FAA STC SR00427SE, TCCA STC SH98-02 External Cargo Hook Assembly Kits
FAA STC SR00814SE Reinforcement Kit - Aft Fuselage Station 493
FAA STC SR01264SE, TCCA STC SH03-27 Replacement Windshields
S76
FAA STC SRO1367SE Rockwell Collins Four (4) Display FDS Electronic Flight Instrument System FAA
Upgrade with Dual AHRS
STC SR01520SE Modularized Main DC Electrical Junction Box
FAA STC SH804NE, TCCA STC SH90-13 Exhaust Ejector
FAA STC SR02352AK AXSYS Forward Looking Infra-Red (FLIR) Imaging System or Camera
p1-2
p3
p4
p5
p6
p7
p8
p9
p10
p11
p12
p13
p14
p15
p16-17
Bell 205/Bell 212 Single
FAA STC SR03043NY, TCAA STC SH09-59 SAGEM Three (3) Display Electronic Flight Instrument System
with AHRS
p18
Bell 206
FAA STC SR02292AK, TCCA STC SH08-18 SAGEM Electronic Flight Instrument System and AHRS Upgrade
FAA STC SR02326AK Single Sagem Avionics ICDS-8 Integrated Cockpit Display System with Attitude and
Heading Reference Inputs and Garmin GNS430 NAV/COMM/GPS System
FAA STC SR01149SE, TCCA STC SH03-25 Carbon Fiber Modular Tailboom Drive Cover
p19
p20
p21
Bell 212/412
FAA STC SH767NE, TCCA STC SH90-9 Overhauled Exhaust Ejectors
p22
Bell UH-1H
FAA STC SR00767SE Spar Replacement System
FAA STC SR00267SE Vertical Tail Fin with 42° and 90° Gear Boxes and 212 Push Rod System
p23
p24
Bell 427/430
FAA SR1520NY, TCCA STC SH02-20 Bulkhead Adaptor
STC SH00-41 FSI Ultra Media II or III, or Wescam 16SS-320, 16SS-B750/725, 16SS-1000, 16DB-750
Camera and Isolation Mount
STC SR01262NY FSI Ultra Media II Camera and Isolation Mount
STC SR01451SE Nose-Mounted Tokimec/Cineflex Gyro-Stabilized E.N.G Camera
STC SR01452SE Tokimec Antenna Array
Airbus Helicopters AS332L/L1
FAA STC SR02415AK Cockpit Voice and Flight Data Recorder (CVFDR)
FAA STC SR02405AK Night Vision Goggle (NVG) Compatible Cockpit
FAA STC SR02398AK Helicopter Emergency Egress Lighting (HEEL) System
FAA STC SR02399AK Dual Garmin GNS 530WNAV/COMM/GPS
FAA STC SR02393AK Satellite Tracking System
p25
p26
p26
p27
p27
p28
p29
p30
p31
p32
SIKORSKY
S61
4
11
5
8
10
1
2
3
9
7
6
S61 SIKORSKY
1
2
Replacement Avionics Shelves
Rockwell Collins/SAGEM
Electronic Display System with
Dual AHRS
5
3
6
Rockwell Collins Four (4) Display
FDS Electronic Flight Instrument
System Upgrade with Dual AHRS
9
4
DC Fuel Quantity System
8
7
Solid State Static Inverter
10
Solid State Voltage Regulator
11
Reinforcement Kit - Aft
Fuselage Station 493
External Cargo Hook Assembly Kits
Modular Wiring Harness
Replacement Windshields
Fifty Inch Section Removal
from Forward Fuselage
between Stations 110 and
160
S61
ROCKWELL COLLINS/SAGEM ELECTRONIC DISPLAY SYSTEM with DUAL AHRS
FAA STC SR02336AK VFR-IFR
PRODUCT DESCRIPTION
Rockwell Collins/Sagem Integrated Cockpit Display System (ICDS) with Rockwell Collins Dual AHRS.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
Rockwell Collins
Two high resolution 8x10 in active matrix LCD adaptive flight displays
Composite PFD/MFD format during reversionary mode as a result of display failure in flight
NVG options available
Displays support TAWS, weather radar, TCAS, lightning detection and other advanced features
•
•
•
•
Sagem Electronic Display System
•
•
•
•
•
•
•
•
•
Improved situational awareness
Improved system reliability and maintainability
Enhanced information management
Reduced pilot workload
Reduced operational costs
Aircraft weight reduction
NVG options available
Replaces all analog gyros, instruments, including engine instruments
Two year factory warranty
TECHNICAL INFORMATION - Rockwell Collins Display System
Screen
LCD
Size
10 in (25.4 cm)
Environmental
DO-160D
Software specifications
DO-178B level A
Weight
12.9 lb (5 kg)
Operational temperature
-20°C to 70°C (-4°F to 158°F)
Input voltage
27.5 Vdc nominal
Inputs/outputs
32 discretes, multiple arinc I/O and one ethernet interface
Part/model number
Rockwell Collins AFD-3010E PFD
Approvals
FAA STC SR02336AK
1
TECHNICAL INFORMATION - Sagem Electronic Display System
Screen
LCD
Size
6.4 in and 10.4 in (16.2 cm and 26.4 cm) landscape and portrait mode
Power supply
10 - 35 VDC
Wattage (max)
50 watts, 14 - 28 volts
Operational limitations
-20°C to 70°C (-4°F to 158°F) operating temperature
Operating temperature
-20°C to 80°C (-4°F to 176°F)
Serial input/output
4 RS-232/4 22
Inputs
8 discrete, NTSC option, external brightness control, external push buttons, external
keyboard
Outputs
16 discrete, audio output
MTBF
5000 hrs
Part/model number
Sagem ICDS-10A (EMS & MFD) and ICDS-6A (CAS MFD)
Approvals
FAA STC SR02336AK
2
S61
REPLACEMENT AVIONICS SHELVES
TCCA STC SH97-42
PRODUCT DESCRIPTION
Installation of new honeycomb avionics shelving in the nose ebay of a Sikorsky S61.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Made of light weight honeycomb material
• Single piece shelf
• New anchors for installing equipment that can be customized for layout
TECHNICAL INFORMATION
Material
Light weight aluminum honeycomb core
Operational limitations
Equivalent to original shelf
Part/model number
SH S61-53-001
Approvals
Transport Canada STC - SH97- 42
Before
3
After
S61
DC FUEL QUANTITY SYSTEM
FAA STC SR02335AK
PRODUCT DESCRIPTION
Designed to replace the existing AC fuel quantity system in the Sikorsky S61. The DC Fuel Quantity System allows
for the display of fuel quantity data in modern glass cockpit flight decks and solves all issues associated with
procurement of legacy probes. This STC utilizes original fuel bladders, requiring only minor modifications to accept
the new system.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Readily procurable modern system components
TECHNICAL INFORMATION
Tank profiling
•
•
•
•
•
•
•
Temperature range
19°C to 70°C (67°F to 158°F)
Weight
• Probes: 0.28 lb (127 g)
• Signal conditioner: 1.7 lb (771 g)
Moment arm (m)
Varies
Required STC
SR02336AK
Approvals
FAA STC SR02335AK
Fuel type compensation
Digital filtering to suppress sloshing
Attitude compensation
Low level detection
Pump and valve control
Built-in-test and system monitoring
ARINC 429, RS232
4
S61
MODULAR WIRING HARNESS
FAA STC SR09236RC
PRODUCT DESCRIPTION
Modular wiring harnesses with latest wire technology to replace existing old/damaged harnesses.
Modular Harness
•
•
•
•
•
•
•
•
•
•
•
•
•
Instrument panel electrical
#1 and #2 AC generator
Fuel transfer bay
#1 and #2 engine anti-ice
LH and RH airframe sponsons (if installed)
Landing gear pump
Tail pylon harness with disconnect
Main transmission
LH and RH aft transmission
#1 and #2 engine
#1 and #2 vee deck
Main landing gear and intermediate sponsons
Modularized AC and DC circuit breaker panels
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
Provides superior wire identification without fading
More durable
Lighter weight
Upgraded connector technology - easier maintenance
Replaces old/damaged harnesses with MIL-W-22759/43 wire with laser marking technology
•
•
•
•
•
TECHNICAL INFORMATION
Specifications
MIL-W-22759/43 specification, high temp wire harnesses
Material
Silver coated copper wire
Operational limitations
200°C (392°F) operational limit FAA STC SR09236RC
Part/model number
61-91-00-105
Approvals
FAA STC SR09236RC
5
S61
ROCKWELL COLLINS FOUR (4) DISPLAY FDS ELECTRONIC FLIGHT INSTRUMENT
SYSTEM UPGRADE and DUAL AHRS
STC SR02279AK
PRODUCT DESCRIPTION
Rockwell Collins FDS-2000 Instrument Display System (IDS).
BENEFITS
•
•
•
•
•
•
•
•
•
•
•
Improved situational awareness
Enhanced information management
Improved system reliability and maintainability
Reduced pilot workload
Aircraft weight reduction
Optional NVG compliant displays
Five inch Liquid Crystal Displays (LCD)
Advanced graphics capabilities that support the display terrain
Weather radar and traffic collision avoidance information
Flight management system maps and other advanced information on the Horizontal Situation Indicator (HSI)
AHRS feature a digital quartz sensor, significantly improving accuracy and reliability while reducing volume, weight,
power consumption and cost of ownership
TECHNICAL INFORMATION
Part/model number
Rockwell Collins FDS 2000 EFIS, AHS 3000 AHRS
Approvals
FAA STC SR02279AK
6
S61
SOLID STATE STATIC INVERTER
FAA STC SR09232RC
PRODUCT DESCRIPTION
Direct replacement for the Sikorsky S61L/N rotary inverter. DC to AC airborne static electrical power inverter. Silicon
solid state 300 VA 3/1 phase, class B, multi-purpose with remote turn on circuitry.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Quiet operation
• Solid state with no moving parts
• MTBF 5000 hours
TECHNICAL INFORMATION
Electrical output
AC 3/1 phase
Voltage
• 115/200 VAC ±5% (24 to 30 VDC input)
• No load to full load, over temp/alt operating range
Current
•
•
•
•
Power
• 300 VA continuous duty
• 300 watts (1 pf) continuous duty
Frequency
• 400 Hz ±1%, no load to full load, over temp/alt operating range
(frequency is maintained to < 10 VDC input)
Weight
2.4 lb - 5.3 lb (1 kg - 2 kg)
Operational limitations
None
Part/model number
AA1020-24-450-CS
Approvals
FAA STC SR09232RC
7
0.87 ampere - 115/200 VAC
Three phase wye 1.51 ampere - 115 VAC
Three phase delta 2.61 ampere - 115 VAC
Single phase
S61
SOLID STATE VOLTAGE REGULATOR
FAA STC SR09233RC
PRODUCT DESCRIPTION
Direct replacement for the Sikorsky S61L/N carbon pile voltage regulator.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Solid state unit
• Direct replacement of carbon pile voltage regulators
• Reduced weight
TECHNICAL INFORMATION
Duty
Continuous, unattended
Temperature rise
15°C (59°F) max
Cooling
Self cooled by convection
Ambient temperature range
-85°C to 85°C (-121°F to 185°F)
Max operating altitude
100,000 ft (3048 m)
Electrical
Regulated DC voltage range: 27.5 VDC to 29.5 VDC no load to full load over
generator speed and temp/alt operating range
Field current
(continuous) 14 amperes (minimum)
Part/model number
AA-1020-24-450CS
Approvals
FAA STC SR09233RC
8
S61
FIFTY INCH SECTION REMOVAL from FORWARD FUSELAGE between STATIONS 110 and 160
FAA STC SR00283SE
PRODUCT DESCRIPTION
Removal of a fifty inch section from the forward fuselage between stations 110 and 160 and reinstallation of forward
cabin with associated fabricated parts (S6, S61n transport category only).
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Transforms the S61 into a shorter helicopter; yielding a lower empty weight and resulting in increased external lifting capacity and enhanced flight performance
TECHNICAL INFORMATION
Weight
Recommend reweigh A/C
Moment arm (m)
Recommend reweigh A/C
Material
See MDL
Operational limitations
See RFMS
Retrofit information
Special training and tooling required
Approvals
FAA STC SR00283SE
9
S61
EXTERNAL CARGO HOOK ASSEMBLY KITS
FAA STC SR00427SE, TCCA STC SH98-02
PRODUCT DESCRIPTION
Fabrication and installation of a Helipro model H9661N01-01, -03, -05, -07, -51, - 53, -55, -57, -59 or -61 logging utility
system.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61N
BENEFITS
• Provides lifting capabilities to 11,000 lb with External Cargo Hook Assembly Kit or without with load cell provisions
• Kit options may be installed in an aircraft separate from a cargo sling system as a stand-alone installation
TECHNICAL INFORMATION
Weight
57.5 lb (26 kg)
Moment arm (m)
267 in (recommend reweigh A/C)
Material
See MDL
Operational limitations
Increases lift capability to 11,000 lb see RFMS HCI-RMS No1
Part/model number
H9661N01-XX
Approvals
FAA SR00427SE, TCCA STC SH98-02
10
S61
REINFORCEMENT KIT - AFT FUSELAGE STATION 493
FAA STC SR00814SE
PRODUCT DESCRIPTION
Fabrication of Reinforcement Kit - Aft Fuselage Station 493.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61NM
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
H2EA
Sikorsky Aircraft Corporation
S61A (USAF CH-3B)
BENEFITS
• Improves structural integrity of a known cracking area
TECHNICAL INFORMATION
Weight
Recommend reweigh A/C
Moment arm (m)
STA 493
Material
7075-T6
Operational limitations
No change
Part/model number
H61070
Approvals
FAA STC SR00814SE
11
S61
REPLACEMENT WINDSHIELDS
FAA STC SR01264SE, TCCA STC SH03-27
PRODUCT DESCRIPTION
Fabrication of Helipro Replacement Windshields.
Type Certificate Number
Make
Model
1H15
Sikorsky Aircraft Corporation
S61L
1H15
Sikorsky Aircraft Corporation
S61N
1H15
Sikorsky Aircraft Corporation
S61NM
BENEFITS
• Lighter and considerably less expensive than laminated glass heated windshields
TECHNICAL INFORMATION
Weight
LH windshield -11 lb (5 kg), RH windshield -11 lb (5 kg)
Moment arm (m)
-572 x 2 = -1148
Material
Acrylic plastic
Operational limitations
No change
Retrofit information
Installation instruction No. HCI-030523
Part/model number
H6120-61228-01 and -02
Approvals
FAA STC SR01264SE, TCCA STC SH03-27
12
SIKORSKY
S76
3
1
2
4
S76 SIKORSKY
1
2
Rockwell Collins Four (4) Display FDS Electronic
Flight Instrument System Upgrade with Dual AHRS
3
Modularized Main DC Electrical Junction
Box
4
Exhaust Ejector
AXSYS Forward Looking Infra-Red (FLIR)
S76
ROCKWELL COLLINS FOUR (4) DISPLAY FDS ELECTRONIC FLIGHT INSTRUMENT
SYSTEM UPGRADE and DUAL AHRS
FAA STC SR01367SE
PRODUCT DESCRIPTION
Rockwell Collins FDS-2000 Instrument Display System (IDS) with Dual Rockwell Collins AHRS.
Type Certificate Number
Make
Model
H1NE
Sikorsky Aircraft Corporation
S76A
H1NE
Sikorsky Aircraft Corporation
S76B
H1NE
Sikorsky Aircraft Corporation
S76C
BENEFITS
•
•
•
•
•
•
•
•
•
•
Improved situational awareness
Enhanced information management
Improved system reliability and maintainability
Reduced pilot workload
Aircraft weight reduction
Optional NVG compliant displays
Five inch liquid crystal displays
Advanced graphics capabilities that support the display terrain
Weather radar and traffic collision avoidance information
Flight management system maps and other advanced information on the horizontal situation indicator or
multi-function display
• AHRS feature a digital quartz sensor, significantly improving accuracy and reliability while reducing volume, weight,
power consumption, and cost of ownership
TECHNICAL INFORMATION
Part/model number
76-24-51-101
Approvals
FAA STC SRO1367SE
13
S76
MODULARIZED MAIN DC ELECTRICAL JUNCTION BOX
FAA STC SR01520SE
PRODUCT DESCRIPTION
S76 main DC electrical junction box rewire to incorporate modular design.
Type Certificate Number
Make
Model
H1NE
Sikorsky Aircraft Corporation
S76A, S76B, S76C
BENEFITS
• Simplified maintenance: the DC junction box can be disconnected and removed from the aircraft by disengaging the five electrical connectors
• Less solder connectors - improved reliability
• Exchange assembly program available
TECHNICAL INFORMATION
Operational limitations
Aircraft specific
Part/model number
76-24-51-101
Approvals
SR01520SE Sikorsky S76 A/B/C Aircraft specific
14
S76
EXHAUST EJECTOR
FAA STC SH804NE, TCCA STC SH90-13
PRODUCT DESCRIPTION
Installation of replacement S76 Exhaust Ejectors
Type Certificate Number
Make
Model
H1NE
Sikorsky Aircraft Corporation
S76A
BENEFITS
• Extends ejector life by applying a different construction method and increasing the material thickness in areas previously subject to cracking
• Provides a more durable unit that can be removed, installed and repaired in an identical manner to that of the standard OEM unit
• AHGS can also replace damaged piece parts
TECHNICAL INFORMATION
Weight
Negligible
Moment arm (m)
Negligible
Material
See MDL
Operational limitations
No change
Retrofit information
Direct replacement
Part/model number
99-104-112-001 Ejector assembly, 99-104-112-103 Interior vane sub assembly
Approvals
FAA STC SH804NE, TCCA STC SH90-12
15
S76
AXSYS FORWARD LOOKING INFRA-RED CAMERA SYSTEM (FLIR)
FAA STC SR02352AK
PRODUCT DESCRIPTION
Camera and equipment system consists of four major assemblies
A. Gimbal/turret mounted on the exterior of aircraft nose containing camera and lens. The turret unit contains a set
of gyro stabilized gimbals that provide four axis of line of sight stability for the multi sensor platform that features
both electro-optical (EO) and infrared (IR) cameras. The unit houses control motors and mechanical systems, and
the necessary electronics, gyroscopes, encoders and circuitry for control of system features.
B. Hand controller located in the aircraft is used to operate the camera and position the gimbal/turret. The V9 MS
hand control unit is the user interface component for operating the AXSYS V9 MS CAMERA SYSTEM. The unit is
NVG compatible and ergonomically designed for comfortable and flexible operation. It provides movement control
of the turret unit, and operates the cameras and other system features. The control system has provisions to
control third party accessories such as an external search light or automatic target tracker and can interface with a
moving map system.
C. The V9 MS auxiliary junction unit contains the necessary circuitry required to execute the camera control
commands. The unit houses the video distribution amplifier, signal converters, IC boards and cooling fan, and
supplies clean power and connectivity for the system.
D. Monitor and keyboard located in LH side of instrument panel and/or the passenger cabin.
Type Certificate Number
Make
Model
H1NE
Sikorsky Aircraft Corporation
S76B
BENEFITS
•
•
•
•
•
•
•
•
•
Four-axis gyro stabilization
Mid-wave cooled thermal sensor
Two high-definition cameras
Continuous optical zoom illuminator
Searchlight interface
Moving map interface
High-definition overlay
Digital video processing
Compact design
TECHNICAL INFORMATION
Thermal imager
•
•
•
•
•
•
•
•
Sensor type 640 x 480 HgCdTe FPA
Wave length 3 - 5 µm
Field of view type continuous
Focal length 25 - 300 mm
Field of view 17.5° to 1.5°
Digital zoom 2x
Effective focal length 600 mm
Zoom ratio 12x optical, 24x overall
16
TECHNICAL INFORMATION CONTINUED
Daylight imager
•
•
•
•
•
•
•
Laser illuminator
• Laser class (class Illb)
• Wave length 830 mm
• Output power 30 mW
System specifications
•
•
•
•
Dimensions (HxWxD)
• Turret 12.1 in x 10.25 in (30.7 cm x 26 cm)
• Auxiliary unit 8 in x 9.5 in x 15.6 in (20.3 cm x 24.1 cm x 39.6 cm)
Weight
•
•
•
•
Power
• Input voltage 28 VDC +/- 10%
• Continuous 132W/5A
• Maximum 450W/16A
System interfaces
•
•
•
•
Operational limitations
• The aircraft is limited to VFR use only when forward display and keyboard are
mounted in the co-pilot position on instrument panel
• The pilot is not permitted to use this equipment
Part/model number
AXSYS V9 System
Approvals
FAA STC SR02352AK, Transport Canada accepted NAPA# P-10-0227
17
Sensor type 1/3 in CMOS 1920 x 1080
Field of view type continuous
Focal length 5.1 - 153 mm
Optical field of view 50.4° to 1.8°
Digital zoom 4x
Effective focal length 612 mm
Zoom ratio 30x optical, 120x overall
System type 4-axis gyro-stabilized multi-sensor
Azimuth coverage 360° continuous
Elevation coverage 57° to -188°
Slew rate 0° -60°/sec
Turret 27.5 lb (12 kg)
Auxiliary unit 20 lb (9 kg)
Control unit 1.5 lb (680 g)
System 58 lb (26 kg) with standard cables
Digital video HD-SDI, HDMI
Analog video NTSC/PAL
Control RS232, RS422
Data RS232, RS422
BELL
205/212
SINGLE
1
BELL 205/212 SINGLE
1
SAGEM Three (3) Display Electronic Flight Instrument System with AHRS System
BELL 205/BELL 212 SINGLE
SAGEM THREE (3) DISPLAY ELECTRONIC FLIGHT INSTRUMENT SYSTEM and
AHRS SYSTEM
FAA STC SR03043NY, TCAA STC SH09-59
PRODUCT DESCRIPTION
Sagem ICDS three (3) display Integrated Cockpit Display System (ICDS) and AHRS system.
Type Certificate Number
Make
Model
H105
Bell Helicopter Textron
205B
H86
Bell Helicopter Textron
212
H1SW
Bell Helicopter Textron
205A, 206A-1
BENEFITS
• Replaces standard instrumentation including critical engine parameter monitoring instruments with a light weight cost effective solution
• Offers better situational awareness with a significantly reduced pilot workload
Screen
LCD
Size
10.4 in (26.4 cm) landscape or portrait mode
Power supply
10 - 35 VDC
Wattage (max)
50 watts, 14 - 28 volts
Operating temperature
-20°C to 70°C (-4°F to 158°F)
Storage temperature
-40°C to 80°C (-40°F to 176°F)
Serial input/output
4 RS-232/422
Inputs
8 discrete, NTSC option, external brightness control, external push buttons, external
keyboard
Outputs
16 discrete, audio output
MTBF
5000 hrs
Weight
Variable
Moment arm (m)
Variable
Material
See TSOs
Operational limitations
Aircraft specific
Part number
Multi levelled
Approvals
FAA STC SR03043NY, TCCA STC SH09-59
18
BELL
206
3
2
1
BELL 206
2
1
SAGEM Electronic Flight Instrument
System and AHRS Upgrade
3
Single Sagem Avionics ICDS-8 Integrated
Cockpit Display System with Attitude and
Heading Reference Inputs and a Garmin
GNS430 NAV/COMM/GPS System
Carbon Fiber Modular Tailboom
Drive Cover
BELL 206
SAGEM ELECTRONIC FLIGHT INSTRUMENT SYSTEM and AHRS UPGRADE
FAA STC SR02292AK, TCCA STC SH08-18
PRODUCT DESCRIPTION
The installation of Sagem Electronic Flight Instrument System and Upgrade includes Sagem integrated cockpit
displays with one, two or three screen options. It has Garmin GNS-430/530W GPS/NAV/Com system options and
Crossbow or Sagem Att/Hdg reference system options. A two inch standby instrument package is available and
includes a panel allowing for remote adjustment of HDG, CRS and BARO.
Type Certificate Number
Make
Model
H2SW
Bell Helicopter Textron (Canada)
206, 206A
H2SW
Bell Helicopter Textron (Canada)
206A-1 (OH-58A)
H2SW
Bell Helicopter Textron (Canada)
206B, 206B-1
H2SW
Bell Helicopter Textron (Canada)
206L-1, 206L-3, 206L-4
BENEFITS
• Replaces standard instrumentation with a light weight cost effective advantage
• Integrated engine display replaces all mechanical indicators
• Offers better situational awareness with significantly reduced pilot workload
TECHNICAL INFORMATION
Screen
LCD
Size
8.4 in or 10.4 in (21.3 cm or 26.4 cm) landscape or portrait mode
Power supply
10 - 35 VDC
Wattage (max)
50 watts, 14 - 28 volts
Operating temperature
-20°C to 70°C (-4°F to 158°F)
Storage temperature
-40°C to 80°C (-40°F to 176°F)
Serial input/output
4 RS-232/422
Inputs
8 discrete, NTSC option, external brightness control, external push buttons, external
keyboard
Outputs
16 discrete, audio output
MTBF
5000 hrs
Retrofit information
FAA STC#: SR02292AK, Transport Canada STC: SH08-18, EASA IM.R.S. 01369
Part/model number
Sagem Avionics ICDS-8
Approvals
FAA STC SR02292AK, TCCA STC SH08-18, EASA STC EASA.IM.R.S.01369
19
BELL 206
SINGLE SAGEM AVIONICS ICDS-8 INTEGRATED COCKPIT DISPLAY SYSTEM with
ATTITUDE and HEADING REFERENCE INPUTS and a GARMIN GNS430
NAV/COMM/GPS SYSTEM
FAA STC SR02326AK
PRODUCT DESCRIPTION
Sagem single display Integrated Cockpit Display System (ICDS) and AHRS system.
Type Certificate Number
Make
Model
H2SW
Bell Helicopter Textron (Canada)
206, 206A
H2SW
Bell Helicopter Textron (Canada)
206A-1 (OH-58A)
H2SW
Bell Helicopter Textron (Canada)
206B, 206B-1
H2SW
Bell Helicopter Textron (Canada)
206L-1, 206L-3, 206L-4
BENEFITS
• Replaces standard instrumentation with a light weight cost effective advantage and offers better situational awareness with significantly reduced pilot workload
TECHNICAL INFORMATION
Screen
LCD
Size
8.4 in (21.3 cm) portrait orientation
Power supply
10 - 35 VDC
Wattage (max)
50 watts, 14 - 28 volts
Operating temperature
-20°C to 70°C (-4°F to 158°F)
Storage temperature
-40°C to 80°C (-40°F to 176°F)
Serial input/output
4 RS-232/422
Inputs
8 discrete, NTSC option, external brightness control, external push buttons, external
keyboard
Outputs
16 discrete, audio output
MTBF
5000 hrs
Part/model number
Sagem Avionics ICDS-8, Garmin GNS430
Approvals
FAA STC SR02326AK
20
BELL 206
CARBON FIBER MODULAR TAILBOOM DRIVE COVER
FAA STC SR01149SE, TCCA STC SH03-25
PRODUCT DESCRIPTION
Alternate tailboom drive cover.
Type Certificate Number
Make
Model
H2SW
Bell Helicopter Textron Canada Limited
206B
BENEFITS
• Lighter, stronger, dent resistant, and two-piece modular for easier installation and shipping
TECHNICAL INFORMATION
Weight
Negligible
Moment arm (m)
Negligible
Material
Carbon fiber
Operational limitations
No change
Retrofit information
Some special drills and tooling required to install
Part/model number
H206-031-462
Approvals
FAA STC SR01149SE, TCCA STC SH03-25
21
BELL
212/412
1
BELL 212/412
1
Overhauled Exhaust Ejectors
BELL 212/412
OVERHAULED EXHAUST EJECTORS
FAA STC SH767NE, TCCA STC SH90-9
PRODUCT DESCRIPTION
Bell 212/412 overhauled exhaust ejectors.
Type Certificate Number
Make
Model
H4SW
Bell Helicopter Textron
212, 412
H-86
Bell Helicopter Textron
212, 412
BENEFITS
• Cost effective: exhaust ejectors can be repaired/overhauled instead of having to purchase replacements
TECHNICAL INFORMATION
Part/model number
89-104-004, 212-061-201 and 212-061-216
Approvals
FAA STC SH767NE,TCCA STC SH90-9
22
BELL
UH-1H
1
2
BELL UH-1H
1
2
Spar Replacement System
Vertical Tail Fin with 42° and 90° Gearboxes and 212
Push Rod System
BELL UH-1H
SPAR REPLACEMENT SYSTEM
FAA STC SR00767SE
PRODUCT DESCRIPTION
Fabrication and installation of Helipro Spar Replacement System.
Type Certificate Number
Make
Model
H11SW
AST, Inc
UH-1F
H12NM
Rotorcraft Development Corp
UH-1F
H12NM
Rotorcraft Development Corp
TH-1F
H12NM
Rotorcraft Development Corp
UH-1P
H13WE
Rotorcraft Development Corp
UH-1B
H13WE
Rotorcraft Development Corp
UH-1H
H15NM
Hagglund Helicopters
UH-1H
H1RM
San Joaquin Helicopters
UH-1H
H1SW
Bell Helicopter Textron
204B
H3SO
Richards Heavylift Helo, Inc
UH-1H
H7NE
Tamarack Helicopters, Inc
UH-1F
H7SO
OAS Parts LLC
UH-1H
BENEFITS
• Unlimited life and is approved AMOC for AD 99-25-12
TECHNICAL INFORMATION
Weight
Recommend reweigh of A/C
Moment arm (m)
Recommend reweigh of A/C
Material
See STC approved model list
Operational limitations
No change
Retrofit information
Requires special training and UH-1H tailboom fixture
Part/model number
See Approved Model List (AML)
Approvals
FAA STC SR00767SE
23
BELL UH-1H
VERTICAL TAIL FIN with 42° and 90° GEARBOXES and 212 PUSH ROD SYSTEM
FAA STC SR00267SE
PRODUCT DESCRIPTION
Fabrication and installation of a 212 Vertical Tail Fin and Rotor, 42° and 90° Gearboxes, and 212 push rod and antitorque control system. (UH 1H) restricted category rotor craft.
Type Certificate Number
Make
Model
H15NM
Bell Helicopter Textron
UH-1H
H7SO
OAS Parts LLC
UH-1H
R00004RC
JJASPP/Vector
UH-1H
BENEFITS
Increased MTBF, improved maintenance procedures, and improved operating performance. This STC also eliminates
requirement for AD 99-25-12.
TECHNICAL INFORMATION
Weight
Recommend reweigh of A/C
Moment arm (m)
Recommend reweigh of A/C
Material
See MDL
Operational limitations
RFMS section II torque available. Maximum time for operation exceeding 47.5 psi is
5 min
Retrofit information
“D” level major modification. Requires UH-1H/205/212 tailboom fixture and special
training
Part/model number
MDL DM9405-3
Approvals
FAA STC SR00267SE
24
BELL
427/430
1
3 2
BELL 427/430
1
2
Bulkhead Adapter
3
- Nose-Mounted Tokimec/Cineflex Gyro Stabilizer E.N.G Camera
- Tokimec Atenna Array
- FSI Ultra Media II or III, or Wescam 16SS-320, 16SS-B750/725,
16SS-1000, 16DB-750 Camera and Isolation Mount
- FSI Ultra Media II Camera and Isolation Mount
BELL 427/430
BULKHEAD ADAPTOR
FAA STC SR00267SE
PRODUCT DESCRIPTION
Bulkhead installation that is easily installed behind the rear seats against the rear wall to move seating forward.
Type Certificate Number
Make
Model
R00001RC
Bell Helicopter Textron (Canada)
427
H-103
Bell Helicopter Textron
427
BENEFITS
• Clear view from main cabin windows
• Improves rear passenger photography capability
TECHNICAL INFORMATION
Part/model number
HP42725-11-801-001
Approvals
FAA STC SR1520NY, TCCA STC SH02-20
25
BELL 427/430
FSI ULTRA MEDIA II OR III, or WESCAM 16SS-320, 16SS- B750/725, 16SS-1000,
16DB-750 CAMERA and ISOLATION MOUNT, FSI ULTRA MEDIA II CAMERA and
ISOLATION MOUNT
STC SH00-41, STC SR01262NY
PRODUCT DESCRIPTION
Installation of a camera system with an “in house” designed isolation mounting system to meet customer installation
and usage requirements.
Type Certificate Number
Make
Model
R00001RC
Bell Helicopter Textron (Canada)
427
H-103
Bell Helicopter Textron
427
BENEFITS
• Light weight, high strength materials are used to manufacture the isolation mount that can be adapted to mount with a number of camera systems
• If another type of camera system or a newer system/mounting is required, it can be developed “in house” to meet customer requirements
• Internal turret design for unprecedented stability
• High magnification
• Outstanding image quality
• Five axis microprocessor controlled gyro stabilization technology
TECHNICAL INFORMATION
Operational limitations
-20°C to 45°C (-4°F to 113°F)
Part/model number
FSI Ultra Media II, III or Wescam 16SS-320, 16SS-B750/725, 16SS-1000, 16DB750
Approvals
FAA STC SR01262NY, TCCA STC SH00-41
26
BELL 427/430
NOSE-MOUNTED TOKIMEC/CINEFLEX GYRO-STABILIZED E.N.G CAMERA STC SR01451SE
TOKIMEC ANTENNA ARRAY
STC SR01452SE
PRODUCT DESCRIPTION
Installation of camera system with antenna array for live broadcasting.
Type Certificate Number
Make
Model
H9SW
Bell Helicopter Textron (Canada)
430
BENEFITS
• Complete all in one system installation
• Includes camera system and the installation of antennas required for live broadcasting of images/video for news or sporting events to a ground station
TECHNICAL INFORMATION
Part/model number
Cineflex HDV14, 430-23-00-101
Approvals
FAA SR01451SE, Approvals FAA STC SR01452SE
27
AIRBUS HELICOPTERS
AS332L/L1
SUPER PUMA
5
1
2
4
3
AIRBUS HELICOPTERS
1
AS332L -
3
2
CVFDR
4
Night Vision Goggle Compatible
Cockpit
5
Dual Garmin NAV/COMM/GPS
Super Puma
Satellite Tracking System
Helicopter Emergency Egress
Lighting (HEEL) System
AS332L
COCKPIT VOICE and FLIGHT DATA RECORDER (CVFDR)
FAA STC SR02415AK
PRODUCT DESCRIPTION
The CVFDR retrofit package features a light-weight solid, low power consumption state of the art Cockpit Voice and
Flight Data Recorder (CVFDR) with an underwater acoustic beacon and a six year battery-life warranty. A digital flight
data acquisition unit is also included as part of the system. The system is capable of recording over 25 flight data
parameters with integrated optional Recorder Independent Power Supply (RIPS), requiring no additional wiring.
Type Certificate Number
Make
Model
H4EU
Airbus Helicopters France
AS332C
H4EU
Airbus Helicopters France
AS332L, AS332L1
BENEFITS
• The only FAA approved CVFDR retrofit solution available on the market
• Further enhances the mission capability profile of the venerable AS332L helicopter
• Minimal downtime for retrofit
TECHNICAL INFORMATION
Operating temperature
-55°C to 70°C (-67°F to 158°F)
Part/model number
L3 Com FA5001 CVFDR
Approvals
FAA STC SR02415AK
28
AS332L
NIGHT VISION GOGGLE (NVG) COMPATIBLE COCKPIT
FAA STC SR02405AK
PRODUCT DESCRIPTION
Replaces existing system internal lighting with a circumferential bezel floodlight, external lighting with covert lighting
and cabin lighting with NVG compliant lighting.
Type Certificate Number
Make
Model
H4EU
Airbus Helicopters France
AS332C, AS332L
BENEFITS
• Night vision goggles operate by sensing smallest amount of natural and artificial light
• NVGs allow air crews to view terrain, avoid obstacles and observe changing weather conditions usually hidden by darkness
• Day/night readable without NVG goggles
• Compatible with ITT 4949 series and L3 M949 series NVG goggles meeting class B operational requirements
• STC meets commercial standards of RTCA/DO-275/268, TSO-C164 and meets the military specifications
MIL-L-85762A and MIL-STD-3009
TECHNICAL INFORMATION
Mil specs
MIL-L-86762A Lighting, Aircraft, Interior, Night Vision Imaging System (NVIS)
Compatible, MIL-STD-3009 Lighting, Aircraft, Night Vision Imaging System (NVIS)
Compatible
Part/model number
Compatible models include ITT F4949 Series, Litton/Northrop-Grumman/L3 M949
systems.
Approvals
FAA STC SR02405AK
29
AS332L
HELICOPTER EMERGENCY EGRESS LIGHTING (HEEL) SYSTEM
FAA STC SR02398AK
PRODUCT DESCRIPTION
The HEEL system is a supplemental lighting system and is a pre-requisite to have the original OEM emergency
lighting system installed.
Type Certificate Number
Make
Model
H4EU
Airbus Helicopters France
AS332C
H4EU
Airbus Helicopters France
AS332L, AS332L1
BENEFITS
• Can be activated by emergency events such as loss of helicopter power, water, and impact
• Following a ditching or crash the HEEL system identifies emergency escape hatches, push out windows and emergency exits by illuminating their perimeter
• Mandatory for off shore operations
• Watertight up to 50 feet for 20 minutes
TECHNICAL INFORMATION
Weight
7.85 lb (3 kg)
Part/model number
Luminescent System Inc, HEEL System
Approvals
FAA STC SR02399AK, EASA STC 10047200
30
AS332L
DUAL GARMIN NAV/COMM/GPS
FAA STC SR02399AK
PRODUCT DESCRIPTION
Installation of a Dual Garmin GNS 530W system on an AS332 L1 rotorcraft. The GNS 530W is fully coupled to the
autopilot.
Type Certificate Number
Make
Model
H4EU
Airbus Helicopters France
AS332C
H4EU
Airbus Helicopters France
AS332L, AS332L1
BENEFITS
•
•
•
•
•
•
•
•
•
•
Combined NAV/Comm/GPS unit mounted in the console
Eliminates need for multiple remote boxes to save space and reduce weight
Dual units for redundancy
Approved for IFR operations and for LPV approaches
Meets FAA TSO C146a standards for WAAS “sole means” navigation
Enhances situational awareness
Class-B TAWS capable
Jeppesen navigation database provides magnitude of flight information
Capable of displaying XM weather information, NEXRAD weather graphics, METARs
Capable of integration with TCAD, WX Radar, Transponder, XM Satellite Datalink
TECHNICAL INFORMATION
Unit dimensions (WxHxD)
6.25 in W x 4.60 in H x 11.0 in D (15.9 cm x 11.7 cm x 27.9 cm)
Display size (WxHxD)
4.0 in W x 3.0 in H (10.2 cm x 7.6 cm)
Display resolution (WxH)
320 x 234 pixels
Display type
8 color TFT LCD; sunlight readable
Weight
9.5 lb (4.3 kg)
Voltage range
14 -28
Built-in VHF Comm
Yes, 8.33/25 kHz channel spacing
Transmit power
10 watts minimum; 16 watts minimum (GNS 530A)
Built-in VOR/Loc/Glideslope
Yes, ICAO annex 10 FM compliant
SBAS/WAAS receiver
15 channel
IFR or VFR
IFR
Part/model number
GNS530W
Approvals
FAA STC SR02399AK
31
AS332L
SATELLITE TRACKING SYSTEM
FAA STC SR02393AK
PRODUCT DESCRIPTION
Installation of a SkyTrac ISAT model 100 or model 200, flight following satellite communication system. Unit offers
two-way voice communication between aircraft and ground. System flight following enables aircraft tracking and flight
mapping.
Type Certificate Number
Make
Model
H4EU
Airbus Helicopters France
AS332C
H4EU
Airbus Helicopters France
AS332L
H4EU
Airbus Helicopters France
AS332L1, AS332L2
H4EU
Airbus Helicopters France
EC225LP
BENEFITS
• Global flight following, voice, messaging and data transfer
• Easily integrates with other on-board equipment
• Automatic operation - no pilot interaction required
Hardware Features
•
•
•
•
•
•
Single TSO GPS and iridium dual antenna
Smart tray installation with field replaceable transceiver
Two-way voice communication
SD card interface for quick data download and firmware upgrades
Supports Wi-Fi or Bluetooth interface for additional onboard connection options
Internal field replaceable battery to enable emergency mode in case of aircraft power loss, as well as the sending of a final “power off” event which provides more accurate flight times for billing and maintenance purposes
Cockpit Interface (Dialer and Display)
•
•
•
•
Send/receive pre-configured, editable field or free-form messages
Send/receive satellite phone calls
Emergency switch
Tag flight number of pilot log to each position report
TECHNICAL INFORMATION
Part/model number
ISAT-100/ ISAT-200
Approvals
FAA STC SR02393AK
32
SETTING THE STANDARD OF CUSTOMER SERVICE
ORDER INFORMATION
Helicopter Services - Richmond
4551 Agar Drive, Richmond
British Columbia, Canada V7B 1A4
Tel: 604.276.7600 I Fax: 604.276.7667
Helicopter Services - Langley
#101B - 5947 206A Street, Langley
British Columbia, Canada V3A 8M1
Tel: 604.514.0388 I Fax: 604.514.0389
Helicopter Services - Alabama
22378 Billie Blackmon Road, Andalusia
Alabama, USA 36421
Tel: 334.222.1277 I Fax: 334.222.1954
Email: sales.hsna@vectoraerospace.com
Phone: 1.888.729.2276
www.vectoraerospace.com
SETTING THE STANDARD OF CUSTOMER SERVICE
August 2014
www.vectoraerospace.com
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