PUBLISHER’S NOTICE
PRICES REFLECTED IN THIS PRESENTATION MAY NOT INCLUDE ALL THE NECESSARY MOUNTS, HARNESSES, CONNECTORS, OR LABOR TO INSTALL. THE ITEMS PRICING SHOWN IN THIS DOCUMENT ARE SUBJECT TO CHANGE WITHOUT NOTICE.

Genesys Aerosystems is offering an avionics UPGRADE AND MODERNIZATION program to provide the  UH-1 / SW204 / SW205 / SW205T and 412HP helicopters with state-of-the-art digital avionics for primary flight, navigation, engine/systems displays, solid-state sensors, and integrated SBAS GPS navigation. The IDU-680 Avionics Suite is a complete flight and navigation system designed to seamlessly integrate into the aircraft's existing systems. The screen displays include three-dimensional, enhanced situational awareness Primary Flight Information and Multi-Function displays. Multi-Function display can be configured to show a moving map, an HSI, traffic, terrain, hover vector, weather, radio/audio control, video input, or engine displays.

The Level A certified IDU-680 EFIS utilizes ADAHRS and GPS SBAS data for precision aircraft operation including RNP and LPV approaches, and Genesys’ patented OASIS (Open Architecture System Integration Symbology) to display engine information and CAS messages. The system also integrates with select radios and weather radar and offers expansion ports supporting a path for future growth. The STC meets all IFR regulations, increasing the mission capabilities, dispatch ability, and usefulness of the aircraft. Additionally, the IDU-680 comes standard with:

  • 3D Synthetic Vision
  • Highway-In-The-Sky (HITS) navigation
  • Geo-referenced Hover Vector
  • Helicopter TAWS (HTAWS)
  • Graphical Flight Management System (FMS)
  • Digital flight recorder
  • NVIS compatibility
  • MIL-STD qualification
  • Search and Rescue patterns
  • And more

The IDU-680 can be customized (and other) airframes using the Genesys OASIS. OASIS allows low-cost integration of aircraft systems and allows for centralized EICAS (Engine Indication and Crew Alerting System) messages, simplifying the instrument scan and reducing workload in critical phases of flight.

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SAGEM has a fully certified helicopter glass cockpit which includes the following:

  • 4 each ICDS-10A Integrated Cockpit Displays
  • 2 each PFD-35A Air Data Computers
  • 2 each EMM-35H Engine Modules
  • 2 each Tach Generator Interface Units
  • 2 each Signal Interface Units
  • 1 each Fuel Quantity Signal Conditioner
  • 4 each Pressure Transducers
  • 2 each Crossbow AHRS Computers and Remote Magnetometers
  • 1 each Structural Bracket Kit
  • 1 each Wire Harness Kit
  • 1 each Instrument Panel (3 sections)
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BASIC FEATURES and will vary depending on model

  • Complies with WAAS TSO C146a
  • Terrain database for terrain awareness is standard
  • WAAS GPS receiver allows for primary navigation and vertical guidance for LPV, L/VNAV, and LNAV+V approaches
  • Combines 16 watt VHF communications transceiver, VHF navigation and UHF glideslope receivers, 12-channel GPS receiver with color moving map
  • WAAS and LAAS compatible GPS receiver 760 channel VHF comm with 25khz spacing; software configurable for 2280 channels (8.33 kHz spacing) for Europe
  • Provides both course deviation and optional roll steering outputs to aircraft flight guidance systems which will enable ARINC 424 lateral guidance procedures including IFR arrivals, departures and approaches
  • Automatically will nominate appropriate VOR and localizer frequencies for VHF navaid
  • Sends correct ATIS, approach, clearance, tower or ground control frequency to the comm radio at the touch of a button
  • 16-color, active-matrix LCD measuring approximately 2" high and 3" wide with a resolution 
    of 128 by 240 pixels
  • Cartographic database displays geopolitical boundaries, federal interstate highways, state routes, major local thoroughfares, plus railroads, rivers, coastlines and lakes
  • Can be interfaced to main indicators such as KI-202/203/204/206/208/208A/209/209A
  • Can be interface to Bendix/King RMI units such as KI-229 and KNI-582
  • Can tune most panel mount DME and remote mount DME units
  • Interfaces to ARINC 429 EFIS systems such as Sandel SN3308 and Bendix/King EFIS 40 AND 50 RS-232 and RS-422 serial ports for interfacing
  • ARINC 429 digital output (GAMA standard) for left/right analog course deviation, ng, encoded or greycode altitude, and basic fuel flow sensor links
  • Fuel Flow page configurable to allow for simultaneous display of left and right engine fuel flows
  • ARINC 429 digital output compatible with some autopilots which can accept ARINC 429 roll-steering information
  • ARINC 429 output data can be used with digital to analog adapter such as Allied Signal KA-90 to produce roll-steering signal used by autopilots systems requiring analog signal
  • Accepts RS-232 fuel flow data from external sources
  • 28 Volt or 14 Volt operation
  • TSO'd
  • Interfaces to BF Goodrich WX-500 Weather Mapping Sensor and Skywatch Traffic Advisory System for combined moving map display with nav data and weather/traffic information 
  • Interfaces to Ryan 9900B / 9900BX TCAD and Goodrich Skywatch to display traffic information
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REWIRING OF  SWFA UH-1 / SW204 / SW205 / SW205T TO CURRENT WIRE SPECIFICATIONS 

Benefits Include:

  • Instrument panel inspection, rewire, paint and placard of instrument
  • Upper Deck Harnesses included in rewire
  • Static Instrument Air System repair or replacement
  • Solid State Power Inverters
  • Solid State Voltage Regulators
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  • Designed to offer superior performance and reliability, the all solid-state Bendix King KDF 806 is the acknowledged standard in remote-mounted ADF systems. Incorporating “coherent detection” technology,  the KDF 806 is able to select weak or distant signals with a high level of  accuracy.
  • This capability helps reject interference and eliminate bearing errors, even during thunderstorms, to give you reliable ADF tracking. All ADF  frequencies, from 190 kHz to 1799 kHz (with an option to include  marine frequencies up to 2182 kHz), are generated by a digital  synthesizer.
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  • The KNR 634A digital VOR/LOC/GS/MB receiver features 200-channel  VOR/LOC, 40-channel glideslope and marker beacon with XYZ RMI.  Also includes KFS 564A frequency selector which simultaneously  displays active and standby frequencies in gas discharge numerics. The  KNR 634A accepts ARINC 429 channeling and provides ARINC 429  outputs for use with EFS 10 and ARINC 429 based systems. TSO'd.
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  • Known for its reliability, the KDM 706A all solid-state distance measuring equipment (DME) features 252 channels and 250 watts. It  accepts direct DME channeling from Bendix King serial, 2x5, and ARINC  429 serial tuning formats. It has outputs for ARINC formats 568 and  429, analog pulse pairs, and analog rate pulse, plus Bendix King Serial  Data for DME indicators.
  • Compatible with an electronic flight instrument system (EFIS), meaning that the KDM 706A's self-test sequence is on a 3 second interval as  opposed to the 1 second interval of other units.
  • Includes a KA 60 antenna, installation kit, and DME indicator.  
  • Available with KDI 572 indicator (28V or 5V) and KDI 574 indicator. 18 to 33VDC operation. TSOd.
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  • Providing superior two-way AM voice communications, these units  were specifically designed for international governmental, military and  paramilitary applications, and have already been specified for use in U.S. Air Force and U.S. Navy training programs.
  • The all-solid-state unit accesses frequencies from 225.000 to 399.975  MHz in 25 kHz increments and is specifically designed for low  maintenance and high reliability. The KTR 909 scans other frequencies  when the unit is not in use.
  • The KFS 599A control head is used as an interface for the KTR 909. The  control head features 20 user programmable channels an easy-to-read  gas-discharge display or Night Vision Goggle (NVG) compatible display.
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FEATURES

  • The light-weight NXT-800 transmits ADS-B Out data from your aircraft to other nearby aircraft and Air Traffic Control (ATC)
  • DO-260B compliant to meet FAA/EASA NextGen mandates, while transmitting a more precise position, speed and intent data
  • Meets Air Transport, Business Jet and Helicopter demands with 3 size options that are form factor replacements for the XS-950 (4 MCU)
  • RCZ-852 and ¼ ATR Short
  • Elementary & Enhanced Mode S surveillance compliant
  • Maximum reliability with built-in test and self-test capabilities
  • Compatible with all ARINC 735B/735A/735 TCAS II systems, including ACSS TCAS 3000SP,TCAS 2000, T2, CAS® and T3 CAS
  • AC or DC power options
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  • Setting a new standard in value and performance, the RDR 2100 Digital  Weather Radar provides a vertical picture of a pilot-selected cross-  section of the storm, offering the best view available to general  aviation. The simple press of a button allows you to analyze a storm  segment vertically, giving you the information you need to determine  the scope of the storm.
  • You can examine the angle of the cell's leading edge to determine  direction of movement, monitor the tops of cells to see how quickly a  storm is building, and easily distinguish between ground and weather  returns. The system is fully stabilized to +/- 30° combined pitch and  roll, and antenna stabilization keeps your screen clear of ground  returns during moderate aircraft maneuvers. You can choose between  two antennas, a 10-inch or 12-inch, to fit a wide variety of airframe  applications
  • The RDR 2100 uses intuitive colors (green, yellow, red, magenta), and  six ranges (10 nm to 320 nm) to depict the weather intensity, creating  a clear picture of the weather and making it easy for you to avoid  danger. The horizontal scan provides an angle of 120°; the vertical scan  an angle of 60°. Using Sensitivity Time Logic, the system can correlate  target distance with intensity, and its attenuation compensation  reduces shadowing.
  • The system is fully Electronic Flight Instrument System (EFIS) compatible using ARINC 429 and ARINC 453 data busses. It also  features a Multi-Function Display (MFD) interface, fault annunciation,  TILT readout on display, and independent dual indicator operation.
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With its advanced solid-state transmitter design eliminating the need for life limited magnetron tubes, the GWX 70 — and GWX 70H that's been made more rugged for helicopter operations — comprises the very latest and most reliable technology in onboard weather radar. 

  • Scan with Doppler Accuracy

Bringing full-color storm cell tracking to your compatible Garmin multifunction display, this Doppler-capable weather avoidance tool combines excellent range and adjustable scanning profiles with precision target definition — for accurate, easy-to-interpret, weather analysis in the cockpit. With pilot-adjustable horizontal scan angles of up to 120°, you can easily focus scanning on the areas you want to watch, while vertical scanning lets you focus on storm tops, gradients and cell buildup at various altitudes. Plus, Weather Attenuated Color Highlight (WATCH™) can identify areas beyond the radar's capability that may contain even more hazardous areas of precipitation.

  • Reduce Pilot Workload

On compatible displays, altitude compensated tilt in the GWX 70 reduces your workload by needing to manually adjust the radar’s tilt; simply set it once to the tilt angle you want, and it will automatically adjust with any change in altitude. Also, when interfaced with your aircraft’s analog gyro or AHRS system, the GWX 70 offers full radar stabilization to 30 degrees of pitch and roll. The GWX 70 also has a ground mapping mode that can assist in a number of applications -- including navigation. Ground mapping mode provides a real-time depiction of the terrain below you.

  • Experience Solid-State Reliability

With its digital design, the GWX 70 provides reduced power consumption and extended life when compared to previous generations of magnetron-based radars. While magnetron tubes degrade or burn out over time, the solid-state technology in the GWX 70 maintains a consistent weather picture its entire lifecycle – all while only using 40 W of power. What’s more, the all-in-one antenna/receiver/transmitter unit is available in 10", 12" and 18" radomes, so it easily installed on a wide variety of aircraft configurations.

  • Upgrade to Advanced Features

The GWX 70 you buy today is prepared for the technologies you might need tomorrow. You can unlock a wealth of new functionality in your GWX 70, such as ground clutter suppression*, which identifies radar ground returns and removes them from the display – taking the guesswork out of interpreting what's on your screen. And optional turbulence detection* can determine areas of turbulence that might contain particulate, like rain or hail. These capabilities are available through simple software upgrades, eliminating the need to purchase new hardware in the future.

The Lynx® MultiLink Surveillance Systems (MSS) is a single box avionics solution packed full of ADS-B benefits. The Lynx family includes four models, ranging from an ADS-B Out only unit with WiFi display options for Persona Electronic Devices (PED) as well as models for display of ADS-B information to dedicated cockpit displays (MFDs). The most notable model is the Lynx NGT-9000 - an intuitive touch screen display that is a form-factor replacement for existing transponders. The NGT-9000 offers an extensive features list and is the most logical choice for pilot’s looking to take full advantage of the ADS-B NextGen flight environment.
The Lynx NGT-9000 series provide 1090ES (Mode S Extended Squitter) ADS-B Out as well as 1090Mhz and 978Mhz (UAT) ADS-B In. This provides ADS-B traffic (ADS-B, ADS-R and TIS-B) and FIS-B input. L-3 NextGen Active Traffic® and/or ADS-B antenna diversity is an available option. Panel mount (NGT-9000) and remote mount (NGT9000R) versions are available. All systems provide 14 CFR 91.227 compliance. A WiFi interface module is available for connectivity to iPad® and AndroidTM devices with applications such as WingX Pro and SkyRadar (other apps pending). All Lynx MSS models incorporate a rule compliant position source (WAAS GPS) requiring no external GPS connections.

One of the primary benefits of the ADS-B environment is the traffic information it provides. The Lynx NGT-9000 offers flexibility to display traffic on the unit itself, as well as other panel mounted avionics that use the popular ARINC 429, RS-232 or RS-422 protocols. The NGT-9000 model features an option for an in-line WiFi transmitter, enabling pilots to view ADS-B traffic on their PED (iPad) using a compatible app. Since the Lynx NGT-9000 receives simultaneously on both 1090Mhz and 978Mhz, pilots will receive ADS-B traffic regardless of altitude or geographic location.

While ADS-B traffic is comprehensive, there are limitations to the service including line of sight to station, non-equipped areas, GPS signal integrity and non-participating aircraft. The Lynx NGT-9000 has the option to be equipped with the L-3 NextGen Active Traffic® system. This enablement blends ADS-B with active traffic data, providing an uninterrupted display of aircraft equipped with Mode A, C and S transponders. Adding NextGen Active Traffic also enables extended aural alerting of intruder aircraft position such as “Traffic, 1 O’clock High, 2 Miles.” Existing SkyWatch® owners can opt to re-use the system’s antenna and cables. The L-3 NextGen Active Traffic enablement is built into the NGT-9000+, eliminating the need for an external box, saving weight and installation costs.

The Lynx NGT-9000 includes subscription-free weather data such as METARs, AIRMETs, SIGMETs and NEXRAD information overlaid on a moving map. A second map page shows Winds and Temps Aloft data. This arrangement allows the pilot to quickly page through graphical weather screens, viewing large amounts of data without overloading a single page. A touch of the finger on the graphical weather map brings up corresponding textual data of the highlighted station or weather icon. A settings page allows the pilot to further customize the weather data pages in both detail and range.

With the Lynx family of ADS-B products, you will receive up to the minute broadcast information regarding airports, Notice to Airmen (NOTAMs) and Temporary Flight Restrictions (TFR) in graphical and textual form. Similar to the weather map, touching an airport or zone icon on the graphical side of NGT-9000 map brings up its corresponding textual data. This data is useful in all phases of flight, aiding the pilot in planning proper routes and informing them about their departing and destination airports.

LYNX NGT-9000 FEATURES

  • Mode S Extended Squitter (ES) transponder with intuitive touch screen interface
  • Dual Mode 1090ES ADS-B Out plus 1090 and 978 ADS-B In
  • Designed for 14V and 28V installations
  • Patented Lynx Tail provides Flight ID, aircraft type and ground speed data of other ADS-B traffic
  • Internal rule compliant position source (WAAS-GPS)
  • Moving map including TFRs, airport databases and NOTAMs
  • Subscription-free ADS-B graphical and textual weather including NEXRAD, METARs, Winds & Temps Aloft, AIRMETs and SIGMETs
  • Customizable layouts and information per pilot preference
  • Faceplate data port for maintenance personnel access to setup menus, software updates and option enablements via laptop
  • Options available for internal L-3 NextGen Active Traffic, Antenna Diversity, PED (iPad) WiFi connectivity and Remote Mount models
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Description

TTR-4100 Traffic Alert and Collision Avoidance System (TCAS II) traffic computer for helicopters Give your commercial helicopter  pilots better traffic-threat awareness for safer operations with the TTR-4100. It's the first TCAS II system certified by the  European Aviation Safety Agency and the Federal Aviation Administration for use in commercial helicopter operations.

More than 30 years of traffic surveillance product experience goes into every TTR-4100. The system enhances crew awareness of traffic threats by detecting, displaying and automatically computing avoidance maneuvers. These are aurally and visually  presented to pilots for ease of execution.

TTR-4100 TCAS II

Features & benefits

  • TCAS II Version 7.1 compliant, meets latest mandates for traffic advisory and resolution systems 30 to 40 NMI traffic surveillance range, improves pilot
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Honeywell's Enhanced Ground Proximity Warning Systems (EGPWS):

The state-of-the-art MK XXII EGPWS is a full-featured HTAWS system with highly advanced safety functions for IFR-equipped helicopters with a radio altimeter. This system exceeds the FAA TSO-C194 requirements. In addition to HTAWS required modes, it includes several GPWS modes and unique callouts for excessive bank angle, tail strike protection, and autorotation.

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(IF EQUIPPED)

The  SWFA UH-1 / SW204 / SW205 / SW205T utilizes the Honeywell SPZ-7600 digital Automatic Flight Control System (AFCS), providing 3-axis or 4-axis flight director capability. The  SWFA UH-1 / SW204 / SW205 / SW205T readily allows upgrade to 4-axis which provides the additional features of yaw trim, altitude pre-select, simultaneous vertical and speed coupling, automatically decelerating approaches, radar altitude hover hold, and hover velocity assist. 

  • AeroCorder 100 Flight Data Recorder (FDR), commonly referred to as a "black box", extends the standard features of existing FDRs with a new approach to capturing, storage, and protection of flight information from flight instruments along with cockpit voice recordings. Using a patent- pending innovative memory insulation technique, AeroCorder 100 offers a smaller size, lower weight, and less power consumption than traditional FDRs in a modular and flexible architecture.
  • These features combine to make it the lightest and lowest volume TSO’d FDR on the market. The “software free” recorder allows for aircraft specific configurations as well as the addition of creative and useful expansion capabilities. AeroCorder 100 can also be flange mounted in any orientation where space is at a premium.
  • AeroCorder 100 FDR includes an ARINC 717 interface for data collection in today’s digital cockpits. To expand AeroCorder’s 100 capabilities, a data acquisition module is available from Flight Data Systems (FDS). The Modular Acquisition Unit (MAU) converts AeroCorder 100 into a Data Acquisition and Crash Recorder System. By using MAUs you can pull in a variety of inputs into AeroCorder 100, making it the ideal option for Flight Operational Quality Assurance (FOQA) and Safety Management.
  • AeroCorder 100 comes standard with a TSO 121b Underwater Locator Beacon (ULB), and provides for two different mounting locations for greater installation flexibility
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  • The Cockpit Voice and Flight Data Recorder (CV/FDR) is an “on-condition,” line-replaceable unit that simultaneously records both cockpit voice and flight data. This CV/FDR is capable of recording a minimum of 25 hours of flight data and two hours of audio.  Audio inputs are provided from three separate channels. The CVR simultaneously records all three channels, converts the audio  into a digital format and stores the data in solid-state memory. Flight data is recorded in flash memory and segregated from the  cockpit voice data. Flight data may be downloaded to ground station equipment in approximately five minutes. A ground support  equipment interface connector is provided and easily accessible. A pedestal mounted cockpit control unit enables CV/FDR test  and recorded audio monitoring. The recorder is JAR-OPS 3 approved.
  • Installation requires additional specialized test equipment (which is NOT included in this kit) in order to comply with the installation requirements. This equipment can either be purchased or leased. Contact an Aeronautical Accessories Brand Sales  Representative for details.
  • Note: 412EPI CV/FDR Kit (412-635-001) includes a Recorder Independent Power Supply (RIPS) that provides 10 +/- minutes of  power to CV/FDR after loss of aircraft electrical power.
  • Recorder Independent Power Supply (RIPS) (412-634-007) can be installed with the 412EP CV/FDR (412-634-009) Kit and will provide 10 +/- minutes of power to CV/FDR after loss of aircraft electrical power.
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The HUMS Kit provides the Helicopter a comprehensive airframe, rotor, engine and drive system vibration monitoring capability, and aircraft data recording supports customer flight data monitoring (FDM) programs. The HUMS Kit is designed to conduct routine vibration management functions, with no changes required in the mandatory maintenance functions of the Maintenance Manual. The system utilizes its vibration monitoring capability to make discretionary rotor and balance adjustments. No pilot interface is required during flight operations. Data downloads are manually commanded by pressing the LED array switch located on the PBA panel in the center pedestal.

The GPMS Foresight MX Remote Monitoring Health and Usage Monitoring System (HUMS) is the most advanced health and condition monitoring system on the market today, combining data acquisition, transfer, analysis, and display.

Continuously monitor your fleet from any device and from anywhere, through our proprietary cloud-based software. Foresight MX’s smart sensors uncover when components are starting to wear and our prognostic algorithms display when maintenance may be required.

The Foresight MX combines mechanical machine condition monitoring (MCM), rotor track and balancing (RTB), and helicopter flight data monitoring (HDFM) all in one solution with a STC'd weight of 3.36 kg.

SWFA UH-1 / SW204 / SW205 / SW205T UPGRADE AND MODERNIZATION
SWFA UH-1 / SW204 / SW205 / SW205T UPGRADE AND MODERNIZATION

Foresight MX combines onboard sensor and avionics data, automated data transfer via WiFi/cellular, and powerful algorithms in the cloud. The result is a predictive dashboard available from any browser. 

  • Optimize Rotor Track & Balance
  • Flight Data  + Exceeding Monitoring
  • Engine + Drivetrain Health Monitoring
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FORESIGHT FEATURES, ATTRIBUTES, & SPECIFICATIONS -  SWFA UH-1 / SW204 / SW205 / SW205T/412

 

CORE FEATURES

Machine Condition Component vibration monitoring

Monitoring Engine performance monitoring
               Dashboard of component and engine Health Indicators
               Diagnostic capability via Condition Indicator drilldown
               Prognostic capability providing RUL for trending components
               Fault validation capability via raw sensor data
Flight Data Monitoring Data from avionics via ARINC 429 or analog interface
               Track & graph missions on 37+ parameters; 60+ on download
               Automatic digital capture of OEM exceedances
               Automatic capture operator defined exceedances
               All data exportable into X-Plane
               AC 135-14B HEMS HFDM compliant
Rotor Track & Balance Automatic in-flight regime recognition and acquisitions
              Optimized RTB adjustment (WGTS, PCRS, TABS) available postflight
              Adjustments can be modified, constrained, or overridden
              Main and tail rotor balancing
              1/rev and 2/rev

 

SYSTEM-WIDE ATTRIBUTES

 

Accessibility Interpretability  Data Transfer Updatability Certifications

Software Integrations  Data Export

Alerting

Aircraft Support

 

 Any-device, Anywhere access via cloud + browser architecture

By maintainer (not dedicated expert) via intuitive dashboards
Automatic postflight upon cooldown via cellular or WiFi
HW updates over the air, SW updates in cloud
STC
Yes via API’S
Yes, via export buttons
Yes, via Email or SMS
Digital or Analog

 

Feature Honeywell GPMS Why It Matters
System Architecture Ground Station + Aggregation Server Cloud-Based Remote and faster access from any browser-enabled device and any location
Data Transfer Manual via usb stick Automated via onboard wifi/cell Regime detection + WiFi and LTE capabilities for quicker and automatic remote access
Usability Specialized Interpreter needed All Members of your team Intuitive, modern UI dashboard for all users
Accuracy Data Processing in the main signal processing unit (MSPU) Data Processing at sensor level, onboard control unit (OBCU), and in the cloud Distributed processing for faster acquisitions and more data, resulting in improved data accuracy
Updates Static Future Proof Secure, over-the-air updating capabilities keep the system up-to-date and modern.
Weight ~9.07kg 6.52kg Bused architecture uses less wire + lightweight sensors, providing weight savings

GPMS UH-1 / SW204 / SW205 / SW205T Foresight MX Differentiators

Competitors are years behind with legacy products lagging in accuracy, usability, weight, and cost.

Intelligence Suite is an adaptive system for high definition imaging sensors that reduces operator fatigue while improving crew effectiveness. Features let operators stay sharply focused on assessing small targets that can be easily overlooked in the flood of information provided by HD thermal imagery. 

The FLIR provides superior image stabilization, ultra long-range imaging performance, and true metadata embedded in digital video, all with laser designation (LD) and rangefinder. The FLIR also provides the ability to operate continuously in all conditions even while sitting on the tarmac with no airflow. The world’s most widely deployed single LRU for ISR&T missions, the FLIR provides HD multi-spectral imaging, accurate target location, and laser spot positioning.

NIGHTSUN SEARCHLIGHT

  • The SX-16 is designed with the intent of providing a mobile, high-intensity light source for a variety of applications. It has been used on over 30 different airframes over the course of its lifetime.
  • Thanks to the valued customers, the SX-16 enjoys the distinction of being chosen as the number one helicopter Searchlight for law enforcement entities, border patrol agencies, Emergency Medical Services (EMS) and several other public service organizations.
  • The SX-16 Nightsun® is the benchmark for high-intensity Searchlights the world over due to its capacity to provide a powerful light source wherever it is needed and doing so under some of the worst environmental scenarios imaginable.

Helicopter has partnered with BLR Aerospace to provide its  performance, safety and efficiency-enhancing FastFin® system as a  standard feature on new  SWFA UH-1 / SW204 / SW205 / SW205T aircraft orders. The system  incorporates two parallel stall strips along the tail boom and a  reshaped vertical fin. These modifications combine to optimize airflow  around the tail boom, improving the handling, stability and lifting  capacity of the  SWFA UH-1 / SW204 / SW205 / SW205T in all environments, especially high and hot  conditions.

The FastFin® system is a combination of two separate modifications,  one to the vertical fin and the other to the tailboom. For clarity, the  term FastFin® refers to the BLR modification that changes the shape  and contour of the vertical fin. The term FastFin® System refers to the  combined FastFin® and Dual Tail Boom Strake installation.

  • Upgrade Provide A Dramatic Increase In Tail Rotor Authority With A Decrease In The Power It Takes To Maintain Directional Control 
  • This Means More Available Power To The Main Rotor, Which Increases The Altitude And High Temperature Performance Of The Aircraft
  • These Benefits Are Accomplished Without Modifying The Original Drivetrain or Gearboxes In Any Way
  • The WSPS™ Wire Strike Protection System™ provides a measure of protection for helicopters in the event of inadvertent flight into  horizontally strung mechanical, electrical transmission, or communication wires or cables. The WSPS™ is designed to reduce the  possibility of wires entering into the cockpit area, reduce the possibility of flight control damage during a wire strike, and decrease  the possibility of wires becoming entangled in the landing gear.
  • It is the original helicopter wire cutting system with over 20,000 kits delivered worldwide. In actual cases, this system was effective  against multiple wire strikes. The typical WSPS™ consists of an upper cutter/deflector, a windshield deflector and lower  cutter/deflector. Each cutter is equipped with high tensile steel cutting blades. Kits come complete with the necessary hardware to  accommodate high or low skid gear and fixed or pop-out floats.

The Ballistic Protection System (BPS) was developed by LifePort or AOA. LifePort or AOA’s BPS is manufactured from High Performance Polyethylene (HPPE) fiber and ballistic steel offering the lightest weight technology in composite armor solutions and maximizing crew comfort and ballistic coverage. The BPS is certified in accordance with National Institute of Justice (NIJ) Level III Standard 018.01  providing a multi-hit ballistic solution defeating the 7.62 mm full metal jacket (U.S. military designation M80) ball round. The BPS is  encapsulated with LifeGard, a protective coating that seals and protects the composite armor. The coating increases the life and  durability of the system as well as providing a slip resistant surface.

Two externally mounted Kevlar® fuel tanks providing an additional 140 gallons of usable fuel, extending endurance by 1.5 hours. This system is compatible with internal auxiliary fuel system for military and commercial aircraft and is compatible with OEM float systems. Complete utilization of 13 passenger seats, or all cabin volume for cargo.

Helicopter owners seeking superior performance, reliability and capability – as well as low cost of ownership – can count on Collins Aerospace’s Goodrich rescue hoist. Internally mounted, electrically powered rescue hoist model 42305 utilizes the Collins Aerospace proprietary translating drum cable management system. The hoist design also incorporates a Weston-style load brake for added safety. The lubricated cable extends cable life and helps arrest corrosion of the cable. 

KEY BENEFITS/FEATURES • Capable of high fleet angle allowing hoist operation in high winds or other circumstances requiring an off-angle lift • Single point payout reduces potential for hoist-induced load swings • Continuous operational duty cycles allow for multiple victim rescues without a cool-down period • Worldwide field engineering services available

DESIGN FEATURES • Boom rotates 205 degrees for easy deployment and recovery of a stretcher • Cable extension meter on control pendant • Hour meter logs total hoisting time • NVG compatible (42305-3 and -5) • Secondary hoist controls for pilot • Emergency cable cut with press-to-test feature • Redundant limit and decel switches

The Breeze Eastern externally mounted 600 lbs. rated 28 VDC electrically driven hoist incorporates all of the safety, self-sensing and redundancy features, as well as the cable management system present in all other Breeze Eastern category one hoist designs. These features enhance operational safety and unit reliability and extend the service life of the hoist assembly. The hoist is normally operated by a crew-person  through a variable speed control in a hand-held control pendant assembly or control box. A second set  of controls for the hoist is located on the helicopter cyclic stick. These controls are operated by the  pilot and have priority over the crew-person controls.

DESIGN FEATURES:

  • External, electric hoist
  • 30º fleet angle
  • Continuous duty cycle
  • Lubricated cable extends cable life and resists corrosion on internal metal components
  • Event meter logs total cycles (hour meter available on some models)
  • Emergency cable cut
  • Down limit override for quick cable changes
  • Redundant limit and “decel” switches
  • Dynamic braking available on some models
  • Night vision compatible controls
  • Cable length display on operator’s pendant
  • Searchlight or hover control pendant
  • 2 position Intercom switch on pendant
  • Pendant lighting includes “Overtemp” or “Caution” indicators
  • Priority hoist controls for pilot

Cargo hook external load equipment includes many technological improvements over the original  equipment. They offer reduced maintenance costs while improving utility and safety. 

Overall Benefits:

  • Extended Shelf & Service Life: Recent product design update and extensive airworthiness analysis now allows for a combined shelf/service life of up to 10 years for products manufactured after February 1, 2020. For products manufactured before February 1, 2020, please refer to shelf and service life information on the product ID tag.
  • Protective End Covers: Provide abrasion resistance at both ends of the longline (top and bottom). Reflective cinch strap promotes high visibility.
  • Compliances: Supported by Airworthiness Analysis to FAA CFR Title 14, Parts 27 & 29.
  • Proof-loading: Proof-loaded to working load limit (WLL).
  • Comes With: Permanent ID tag, Certificate of Compliance (COC), transport/storage bag, and user instructions manual.
  • Optional Accessories: Contact us to request custom line lengths or hardware (such as a non-electric swivel hook for bottom end), weighted bottom end-covers (for increased load stability and velocity without load), or other accessories.
  • Longlines
  • Longline kits for HEC missions include many essential components for properly rigging your aircraft to carry human external cargo, including the Y-Rope, a rigging plate, longline, weight bag, lanyard, and carabiners.
  • Rigging Plate
  • HEC Rigging Plate helps you manage distribution of up to five separate loads for connecting multiple lanyards during your mission. Four of the holes are rated up to 310 lbs.. each, while the center lug is rated for up to 800 lbs.. Any combination of loads may be applied through the lower five holes as long as the 310 lbs.. load is not exceeded when using each of the side holes and the 800 lbs.. overall limit is not exceeded.
  • Slip-Ring Kit
  • Tangled wires and complicated operations with suspended auxiliary equipment are things of the past when you install the Onboard Systems Multi-Channel Slip-Ring Kit. Our Slip-Ring Kit supplies electrical power and control signals to accessory equipment suspended from the rotating cargo hook. Equipment suspended from rotating hooks receive full, direct power, while the hook itself is allowed to rotate freely, unhindered by snagged power cables coming from other parts of the aircraft.

Cargo Hook Retention System - The Cargo Hook Retention System was designed for  205, SWFA UH-1 / SW204 / SW205 / SW205T and 412 operators who need to be able to temporarily keep the cargo hook assembly from rotating during certain types of external load missions. This certified upgrade kit provides a restraining arm that is coupled to the cargo hook assembly and supported by a bracket that is attached to the airframe. It can be quickly enabled or disabled as needed via a quick release ball lock pin.

Benefits

  • Stops Cargo Hook Rotation: Length of rod allows for full fore/aft and full lateral movement without hook rotation. Rod is supported by a Teflon® lined bracket that lets the pole smoothly swing forward and back.
  • Supports Complex Missions: An elegant solution for situations where you don't want the hook to spin due to multiple cable connections, use of seeding buckets, cone harvesters, portable saws, hydraulic shears, Sacksafoam™, hydraulic pumps, etc.
  • Quick & Easy to Use: Once the kit is installed, you can leave it on the aircraft and enable/disable it as needed for each mission via a quick release pin.
  • Simple Yet Robust System: Requires minimal maintenance. Service on condition.

Cargo hook kit includes many technological improvements over the original  equipment. They offer reduced maintenance costs while improving utility and safety. Our cargo hook kits include TALON MC Keeperless Cargo Hook, which has significantly more safety features than other hooks available. Note: 5VDC back lighting system for C-39 indicator 

Benefits

  • 30% Lighter than Original  System: Lighter, stronger alloys and parts allow the system to haul maximum weight, while adding minimum load to the airframe.
  • Improved Yoke Design: We've eliminated cracking problems by distributing load stress across multiple parts.
  • High-Impact Bumper Ring: Crack-resistant, 2-piece polymer ring protects both hook and airframe from the stresses of swinging loads.
  • Nickel Plated Carbon Steel Load Beam: We've upgraded the load beam material from stainless steel to nickel plated carbon steel for greater durability. The new load beam is harder and resists wear and tear from frequent use for heavy loads.
  • Power for Suspended Equipment: The 8-channel slip ring supplies power to your suspended equipment.
  • Integrated Onboard Weighing System: Allows pilots to instantly know the exact weight of the cargo on the hook. Reduces the risk of overload airframe stress and helps the pilot make more informed aircraft loading decisions.
  • Keeperless Hook: The keeperless hook handles a wide variety of load ring sizes and styles while eliminating the possibility of losing a load that inadvertently gets past the keeper.
  • The Onboard Advantage: Our cargo hook kits can be installed on new or existing aircraft using standard hand tools. Time between overhauls is five years or 1,000 operating hours for all cargo hooks. And because Onboard Systems maintains a large inventory of cargo hook kits and spare parts, we can usually ship your order out quickly.
  • Increase productivity, safety and accurate external load weight reporting with a digitally-accurate weighing system from Onboard Systems. This load weigh system is designed to integrate seamlessly with cargo hook system for your 204, 205, SWFA UH-1 / SW204 / SW205 / SW205T or 412 helicopter. Lift with confidence every time while safely increasing your average loads and improving operational efficiency.

Benefits

  • Highly Accurate: Digital technology in the weighing systems ensures consistently reliable measurements
  • Safely Lift Higher Average Loads: Ramp up productivity by eliminating guessing games about the weight of your load. When the pilot knows the exact weight being carried, there's no need to err on the side of caution.
  • Includes All Hardware: All necessary hardware for a full installation is included. Comes with the load cell, cockpit indicator, and wiring harness.
  • Improve Customer Relations: Eliminates disputes over weight promised or weight transported. You can report accurate statistics to your customer right away.
  • Reduce Maintenance Costs: Never make load weight miscalculations again. Your pilots will know the load weight every time and greatly reduce repairs from airframe overstress and overload.
  • Digital Readouts in the Cockpit: Provides a clear, backlit, easy-to-read digital weight readout in pounds or kilograms. Easy to operate without increasing pilot workload.
  • Scaleable Analog Output: Built-in 0-5 volt output can be used to feed data to a variety of Helicopter Flight Data Monitoring (HFDM) devices (such as a Hobbs meter, Latitude, or Flightcell data recorder, etc.). Signal can be used to alert the pilot if a load is on the hook, or provide load weight information to a data tracking or GPS system.
  • NVG Backlighting Option: 

The HPASOS system has been specifically designed to meet the needs of unpressurised airframes flying at altitudes in excess of 10,000ft providing the pilots and aircrew with protection against the effects of hypoxia.

It is the most efficient and easy to use system available, not batteries required.

The Oronasal Mask Assembly has been designed in conjunction with the POD Unit, again as a key component of the HPASOS system. The mask comes with a fully integrated communications suite allowing voice communications over the existing aircraft network. The mask also benefits from a fully adjustable helmet interface which allows the user to quickly and easily drop the mask off the face when the aircraft is flying at an altitude where oxygen is not required, below 10,000ft.

The Pneumatic Oxygen Delivery Unit is one of the key components of the Helicopter Pilot and Aircrew Supplementary Oxygen System (HPASOS). The system has been designed specifically for the pilots and aircrew of unpressurised rotary wing aircraft, giving them protection against the effects of hypoxia when flying at altitudes in excess of 10,000ft.

Kit includes Fwd, Mid & Aft Tri-Bag floats with integrated liferaft in the Mid floats. Requires installation of 412-630-033/-034 Steps. Price is for complete float with liferaft system. 

KEY FEATURES

  • Exchange program available 
  • Available with integrated liferaft (10-man)
  •  Requires installation of 412-630-033/-034 Steps
  •  Hoist compatible configuration available
  •  Installs on high gear

KEY BENEFITS

• Lighter than OEM 
• Includes 10-man integrated liferaft 
• No life limit on inflatables (Floats & Liferafts) 
• Best in the industry lead time 
• Increased safety with electrical/mechanical & water sensor activation system 
• Reduced maintenance cost (longer maintenance intervals) 
• Tri-Bag technology allows for: 
- Significant weight reduction (smaller reservoir & less gas usage) 
- Increased stability 
• Can install on OEM compatible skidtubes 
• Liferafts will be compliant with EASA OPS requirements

1 Patient Kit
2 Patient Kit
1 Patient Kit with Stryker Stretcher

Air Ambulance Technology GmbH designs and manufactures interiors for, and with its customers. The medical carrier of the rotorcraft can be designed with either new medical devices or already owned medical devices. The interior can be transformed from a 1 patient to a 2 patient configuration within minutes

The installation time for the 2 patient full EMS configuration for the rotorcraft is approximately 20 minutes. There are three possible configurations. 1 patient, 2 patient and SAR. Not only are Air Ambulance Technology GmbH's aircraft interiors exceptionally quick to install and remove, the modular system also allows the operator to change between a full EMS and a Search and Rescue mission within a very short time.

EMS – AEROMED

AeroMed designs and manufactures interiors for, and with its customers. The medical carrier of the 412 can be designed with either new medical devices or already owned medical devices. The interior can be transformed from a 1 patient to a 2 patient configuration within minutes

The installation time for the 2 patient full EMS configuration for the 412 is approximately 20 minutes. There are three possible configurations. 1 patient, 2 patient and SAR. Not only are AeroMed's aircraft interiors exceptionally quick to install and remove, the modular system also allows the operator to change between a full EMS and a Search and Rescue mission within a very short time.

TACTICAL MISSION-FAST ROPE SYSTEM
The Fast Rope Insertion/Extraction System provides aft cabin mounted hardware consisting of a quick deployable tube and support assembly designed to allow rapid insertion of special operations personnel from both sides of the aircraft utilizing a specially designed rope. The Fast Rope System incorporates an innovative telescoping feature to allow quick retraction of the tube ends into the cabin to allow operation of the aircraft with cargo doors closed. The kit also includes an innovative quick release rope retention mechanism allowing crew to release the rope in the event of an emergency. The system allows four personnel per side simultaneous deployment.

SPACEDOORS®
If installed, you can increase visibility and add 8-12 inches of usable space in your cabin area. The Spacedoor™ allows you to have a variety of possible interior configurations to meet your needs — whatever they are. This is a great accessory for multi-mission aircraft. Designed to replace the standard OEM sliding door, the Spacedoor™ utilizes a lightweight composite technology. It’s easy to install and does not create additional operating limitations. Here’s another bonus: The Spacedoor™ comes with one of our other products, the Cabin Door Roller Kit, which makes opening and closing the door a breeze.

HEEL

Helicopter Emergency Egress Lighting Systems (HEELS) identifies emergency escape hatches, exits and push-out windows by illuminating their perimeter to guide you to safety during emergency situations.

Automatic illumination occurs if aircraft power is lost or when the lighting system water sensor becomes immersed in water. HEELS can also be manually illuminated using a three mode ON, OFF, ARMED cockpit switch. HEELS is also a battery-operated independent lighting system. A typical HEELS installation consists of an array of light emitting diodes on substrate placed around escape hatches or doors. The system has two water sensors, each of which will activate lighting  upon immersion. An optional aircraft Permanent Magnet Generator (PMG) interface unit monitors rotor rpm and interfaces the HEELS to the aircraft. The system is activated upon signal loss. When the rotors fall below a threshold rpm, the HEELS will automatically illuminate. The Control Unit consists of an electronic module with a removable battery pack, which automatically recharges during flight 

53 AMP BATTERY

  • 53 AMP-hour Ni-Cad Battery with increased amperage than the standard 40 Amp battery. 
  • 53 AMP-hour Battery Kit
  • Dual Battery Provision are accommodated
  • Battery-driven engine starts with the standard 40 Amp-Hour battery are limited to aircraft cold-soak temperatures above 0 °C (32 °F) For battery-driven engine starts down to aircraft cold-soak temperatures of -25 °C (-13 °F) a 53 Amp-Hour battery is required. If configured, the 53 Amp-Hour Battery kit must be installed prior to, or concurrently with the installation of the SW-Series certification.

AIR CONDITIONING

This innovative, lightweight and compact design uses the latest technology to create smaller and lighter components while still providing the same performance and reliability. All the major components of the system are located on the transmission deck for ease of maintenance, increased cooling efficiency, and to help reduce weight. An electric motor allows the AC to be run from external power. The Air Conditioning System consists of a compressor and electric motor attached to the helicopter’s transmission, a condenser and evaporator unit attached to the transmission deck, and the necessary parts and hardware to complete the kit installation. The Air Conditioning System is powered by a drive pulley attached to the  Transmission or during ground operations, the AC system can be run from external power. The system reduces weight by having a single evaporator and condenser on the transmission deck in close proximity of each other. The A/C system also has multiple speed output control and fresh air ventilation.

  • Lightweight
  • Compact design
  • Cools down before take off

 

IR/EO CAMERA SYSTEM
Low-altitude Tactical Surveillance & Target Acquisition and Designation missions requiring low-weight installation flexibility.
Product Features Benefits

  • Compact Solution
  • 43 lbs../19.5 kg turret
  • 15 in. turret height for better ground clearance
  • Multi-Sensor Imaging/Lasing Payload Options
  • Currently supports up to six sensors simultaneously
  • Superior HD imaging resolution from Electro-Optical (EO) camera
  • Laser rangefinder, illuminator, designator
  • Latest Enhancements – 2020 – 
  • WESCAM Advanced Video Engine (WAVE)
  • High Sensitivity Color Camera
  • High-Definition (HD) IR
  • Pseudo-Colour IR
  • Advanced Video Tracker (AVT)
  • Embedded MTI
  • Enhanced Local Area Processing (ELAP)
  • Real-time image enhancement for EO day, EO night & Infrared
  • High-Performance IMU & MX-GEO Software Suite
  • IMU & MX-GEO work to create accurate target location
  • MX-GEO automatically aligns to the aircraft
  • Robust automatic image focus
  • Uncompromised Stabilization
  • Four-axis gimbal with internal IMU
  • All payloads are fully stabilized

LOUD SPEAKERS

The AA21-400 Cabin PA control unit provides centralized control for an aircraft’s internal and external PA systems. The integrated 25W amplifier drives an 8W speaker arrangement for internal cabin paging. The AA21-400 provides excellent high quality sound, a very important feature when the audio is to be amplified by an external, high power PA system.

The LSA Series is newest Loud Speaker Amplifier. This high end ‘Class D’ amplifier will outperform any comparable system on the market today. Using the latest technology allows for a lighter weight PA that processes and optimizes the audio signal to get the best output using much less power compared to its predecessor. Newer generation parts and automated electronic assembly also allows for a better price point, reducing the cost to the end user. The LSA Series of amplifiers incorporates a ‘smart power supply’ that modifies the amplifier output to meet the output load demand. These amplifiers deliver up to 1200 watts of audio output power to the speakers.

The TS95-16DS is a 6 , high power speaker with a steel chassis that provides magnetic shielding. Fitted with AEM’s updated high power speaker drivers, the TS95 series speakers provide much better conversion of electrical power (Watts) to sound pressure (SPL). Designed from the same mechanical configuration as the TS9x series speakers, the TS95 can be installed into existing PA installations with only minor mechanical modifications to the aircraft speaker mount.

SW204HP SKD KIT WITH OVERHAULED MAJOR COMPONENTS

Item# Type Mod Benefit
1 DT&RS Overhauled 212 Main Rotor Hub & 212 Main Rotor System Improved lift to 9,500 lbs. / 5,080 kg internal; 9,500 lbs. / 5,080 kg external GW
2 DT&RS Overhauled 212/412 Main Rotor Transmission Increased horsepower to 1,370 HP
3 DT&RS Overhauled Swashplate Assembly Improved lift to 9,500 lbs. / 4,309 kg internal; 9,500 lbs. / 4,309 kg external GW
4 DT&RS Overhauled 212 Main and Tail Rotor drive shaft and coupling Increased horsepower to 1,370 HP
5 DT&RS Overhauled 212 Tail Rotor & 212 Tail Rotor System Additional tail rotor authority and efficiency at higher altitudes
6 DT&RS Overhauled 212 90° gearbox Additional tail rotor authority and efficiency at higher altitudes
7 DT&RS Overhauled 212 42° gearbox Increased horsepower to 1,370 HP
8 DT&RS Overhauled hydraulics system Improves cyclic control by raising the operating pressure to 1,500 PSI
9 DT&RS Single T53-L-703 engines install Increased horsepower with increased efficiency at higher altitudes, increased to 5,000 TBO
10 Airframe Overhauled oil cooler and blower Improved cooling for T53-L-703 engine
11 Airframe Overhauled airframe Increased strength for 1,370 HP and 56.5 PSI torque
12 Airframe Overhauled lift beam and main beam and pylon Increased strength for 1,370 HP and 5,000 lbs. / 2,268 kg cargo hook capacity
13 Airframe Overhauled cross tube tunnel Increased strength and fatigue capabilities for 9,500 lbs. / 4,309 kg internal GW
14 Tailboom Overhauled tailboom for additional torque requirements Increased strength for 1,370 HP and 56.5 PSI torque
15 Tailboom 412 vertical fin Reduced flight loads and better crosswind performance
16 Tailboom Boundary Layer Research Inc. tailboom mods Improves cyclic control
17 Electrical Avionics Optional electrical and avionics Options include electrical rewire, glass cockpit STC and avionics suites
*Optional Instrument Full Glass Cockpit Display Enhance Ground Situational Awareness Considerably

SW205 SKD KIT WITH OVERHAULED MAJOR COMPONENTS

Item# Type Mod Benefit
1 DT&RS Overhauled 212 Main Rotor Hub & 212 Main Rotor System Improved lift to 11,200 lbs. / 5,080 kg internal; 11,200 lbs. / 5,080 kg external GW
2 DT&RS Overhauled 212/412 Main Rotor Transmission Increased horsepower to 1,370 HP
3 DT&RS Overhauled Swashplate Assembly Improved lift to 11,200 lbs. / 5,080 kg internal; 11,200 lbs. / 5,080 kg external GW
4 DT&RS Overhauled 212 Main and Tail Rotor drive shaft and coupling Increased horsepower to 1,370 HP
5 DT&RS Overhauled 212 Tail Rotor & 212 Tail Rotor System Additional tail rotor authority and efficiency at higher altitudes
6 DT&RS Overhauled 212 90° gearbox Additional tail rotor authority and efficiency at higher altitudes
7 DT&RS Overhauled 212 42° gearbox Increased horsepower to 1,370 HP
8 DT&RS Overhauled hydraulics system Improves cyclic control by raising the operating pressure to 1,500 PSI
9 DT&RS Single T53-L-703 engines install Increased horsepower with increased efficiency at higher altitudes, increased to 5,000 TBO
10 Airframe Overhauled oil cooler and blower Improved cooling for T53-L-703 engine
11 Airframe Overhauled airframe Increased strength for 1,370 HP and 56.5 PSI torque
12 Airframe Overhauled lift beam and main beam and pylon Increased strength for 1,370 HP and 5,000 lbs. / 2,268 kg cargo hook capacity
13 Airframe Overhauled cross tube tunnel Increased strength and fatigue capabilities for 11,200 lbs. / 5,080 kg internal GW
14 Tailboom Overhauled tailboom for additional torque requirements Increased strength for 1,370 HP and 56.5 PSI torque
15 Tailboom 412 vertical fin Reduced flight loads and better crosswind performance
16 Tailboom Boundary Layer Research Inc. tailboom mods Improves cyclic control
17 Electrical Avionics Optional electrical and avionics Options include electrical rewire, glass cockpit STC and avionics suites
*Optional Instrument Full Glass Cockpit Display Enhance Ground Situational Awareness Considerably

SW205T SKD KIT WITH OVERHAULED MAJOR COMPONENTS

Item# Type Mod Benefit
1 DT&RS Overhauled 212 Main Rotor Hub & 212 Main Rotor System Improved lift to 12,500 lbs. / 5,669 kg internal; 12,500 lbs. / 5,669 kg external GW
2 DT&RS Overhauled 212/412 Main Rotor Transmission Increased horsepower to 1,370 HP
3 DT&RS Overhauled Swashplate Assembly Improved lift to 12,500 lbs. / 5,669 kg internal; 12,500 lbs. / 5,669 kg external GW
4 DT&RS Overhauled 212 Main and Tail Rotor drive shaft and coupling Increased horsepower to 1,370 HP
5 DT&RS Overhauled 212 Tail Rotor & 212 Tail Rotor System Additional tail rotor authority and efficiency at higher altitudes
6 DT&RS Overhauled 212 90° gearbox Additional tail rotor authority and efficiency at higher altitudes
7 DT&RS Overhauled 212 42° gearbox Increased horsepower to 1,370 HP
8 DT&RS Overhauled hydraulics system Improves cyclic control by raising the operating pressure to 1,500 PSI
9 DT&RS Twin T53-L-13B engines install Increased horsepower with increased efficiency at higher altitudes, increased to 5,000 TBO
10 Airframe Overhauled oil cooler and blower Improved cooling for T53-L-13B engine
11 Airframe Overhauled airframe Increased strength for 1,370 HP and 56.5 PSI torque
12 Airframe Overhauled lift beam and main beam and pylon Increased strength for 1,370 HP and 5,000 lbs. / 2,268 kg cargo hook capacity
13 Airframe Overhauled cross tube tunnel Increased strength and fatigue capabilities for 12,500 lbs. / 5,669 kg internal GW
14 Tailboom Overhauled tailboom for additional torque requirements Increased strength for 1,370 HP and 56.5 PSI torque
15 Tailboom 412 vertical fin Reduced flight loads and better crosswind performance
16 Tailboom Boundary Layer Research Inc. tailboom mods Improves cyclic control
17 Electrical Avionics Optional electrical and avionics Options include electrical rewire, glass cockpit STC and avionics suites
*18 Instrument Full Glass Cockpit Display-Included Enhance Ground Situational Awareness Considerably

Replacement of the BHTI Vertical Fin Web/Spar with the New 412 Helicopter Vertical Fin Web/Spar Assembly is considered by the Federal Aviation Administration (FAA) a major repair and therefore requires “competent and experienced” personnel. SWFA holds Federal Aviation Administration (FAA) approval under its Repair Station Certificate for the replacement of the fin spar/web on the following aircraft: UH-1B, UH-1H, UH-1L, UH-1F, UH-1P, 204B, 205A-1, UH-1 / SW204 / SW205 / SW205T, and 412. This modification is a Federal Aviation Administration (FAA) - Means of Compliance (MOC) approved terminating action for the spar Airworthiness Directive (AD 99-25-12, AD 93-02-07).

VERTICAL FIN

This allows for significantly improved transitional displacement of stress loads encountered by the tailboom under high load conditions. Upper skins are also upgraded to meet higher heat demands from the exhaust output in hover conditions.

Improved vertical fin skins are manufactured by SWFA and are made as replacement items to the original 412. The replacement longeron fitting is made of aluminum and is hot bonded to three aluminum splices.

  • Item 1 Replacement spar: this spar uses the current New 412 spar cap
  • Item 2 Replacement bulkhead: canted bulkhead (2 parts) was 0.015 to 0.025 thick each and is replaced by 0.032 thick bulkheads
  • Item 3 Replacement shear tie: this replaces the previous shear tie that was 0.063 thick and is now 0.080 thick
  • Item 4 Replacement skin: this replaces the previous skin that was 0.025 thick, and is now 0.032 thick
  • Item 5 Replacement doublers: the left side is 0.032 thick and the right side is 0.040 thick, these doublers replace the previous 0.025 thick doublers
  • Item 6 Skin: replaces the existing skin with skin and clips similar to the current 412
  • Item 7 Replaces the existing doubler with doubler similar to the current 412
  • Item 8 Replacement stringers: these stringers replace the previous 0.025 thick stringer (now 0.032 thick)
  • Item 9 Added doubler (left side only): this additional doubler has been added to the left side only and is 0.040 thick
  • Item 10 Added doubler: This doubler is 0.050 thick
  • Item 11 Replacement doubler .050 thick

PROTECTIVE TRIM

Protective Trim Kits feature stainless steel doublers that protect aircraft skin and structures in often damaged areas. Door Sill Protective Trim Kit is designed to protect the crew door sills from damage. Step Protective Trim Kit consists of two stainless steel doublers that install around the RH post steps between the crew and hinge panel doors to protect the edges of the aircraft skin from damage. Fuel Panel Protective Trim Kit consists of a stainless steel doubler that protects the aircraft skin below the aircraft fuel cap from fuel cap damage during refueling.

CREW DOOR STRUTS

  • The Automatic Door Opener Kits modify the hinge panel (quarter) doors with a durable gas spring that assists in opening the door and keeps it open while occupants are entering the aircraft.
  • Reliable gas spring
  • Gas Spring does not force the door to travel past its normal open position
  • Prevents door from swinging closed as passengers enter or exit the aircraft
  • Compatible on aluminum and Spacepod™ doors

PILOT WINDOW GUARD

The pilot window guard protects the green house window from accidental breakage when maintenance crew climb onto the roof deck.

LED STROBE LIGHTS

71080 Series beacons are FAA TSO compliant self-contained LED Anti-Collision lights (Ref. Class I - 150 effective candlepower). They are designed to replace a range of products. Refer to models and descriptions below.

Models -01, -04, -05, -14, -15, -20, -51, -55: Ship with 12” Flying Leads. Models -07, -17, -08, -18: MS3102R10SL-3P Connector. Models -04, -14, -08, -18: designed to replace existing beacons using 5-Hole mounting pattern on a 4.656 dia. bolt circle (Whelen 70285 series/7090501 series or 70900 with A440 adapter). Models -05, -15, -07, -17: 3 ¾” opening designed to fit inside an A440 mounting adapter, mounting holes to fit in place of rotating beacons, Whelen Model HRCFA, or 7090004, -05 series LED beacons.

WE THANK YOU FOR ALLOWING US TO PROVIDE OUR UPGRADE AND MODERNIZATION PRESENTATION FOR THE UH-1 / SW204 / SW205 / SW205T