REVISION HISTORY
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DESCRIPTION
DATE (YR-MO-DY)
-
Product Baseline Release. RA 05-0421
05-11-09
A
Shts 18,19 & 25 revised. ECO 05-0544
05-12-12
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B
All sheets revised. ECO 06-0202
06-05-02
D.C
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APPROVED
CMC Electronics Inc.
Montreal, Quebec, Canada
CONTRACTOR
ORIGINATOR
PILOTVIEW™
CLASS 2 EFB
TECHNICAL DESCRIPTION
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TABLE OF CONTENTS
1.
OVERVIEW ........................................................................................................................................ 3
2.
2.1
2.2
PILOTVIEW™ ELECTRONIC FLIGHT BAG (EFB).......................................................................... 4
PilotView™ Electronic Display Unit (EDU)......................................................................................... 4
PilotView™ EFB Specifications.......................................................................................................... 5
2.2.1
EDU Characteristics ................................................................................................................ 5
2.2.2
EMU and Enhanced EMU (EEMU) Characteristics ................................................................ 8
2.2.3
EDU and EMU Installation..................................................................................................... 10
2.3
Aircraft Mounts ................................................................................................................................. 12
2.3.1
Side Mounts........................................................................................................................... 12
2.3.2
Yoke Mount ........................................................................................................................... 12
2.4
System Configuration ....................................................................................................................... 13
2.5
“CMC-Approved” Peripherals........................................................................................................... 14
3.
3.1
3.2
3.3
INSTALLATION ............................................................................................................................... 14
Qualification...................................................................................................................................... 14
PilotView™ MTBF / MTBUR ............................................................................................................ 14
PilotView™ Warranty ....................................................................................................................... 14
4.
4.1
4.2
4.3
4.4
4.5
4.6
APPLICATION ENVIRONMENT ..................................................................................................... 15
Standard Software Applications ....................................................................................................... 15
PilotView™ Master Menu Software.................................................................................................. 15
PilotView™ Note Taker .................................................................................................................... 16
PlotView™ Setup and Test Tools .................................................................................................... 16
Adobe® Reader® ............................................................................................................................... 16
Operator-Specific Applications......................................................................................................... 17
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1.
OVERVIEW
The PilotView™ EFB bridges the gap between low-end off-the-shelf PC tablets and high-end
Class 3 EFBs, by offering an avionics-grade hardware package and certification to DO-160D.
Many of the features found only in Class 3 EFBs, such as FMS-style line select keys, a very
high- resolution, fully dimmable display, integrated communication capabilities and DO-160D
certification make the PilotView™ EFB an ideal system to meet the varied requirements of
the air transport and regional airline market.
In addition to line select keys, the PilotView™ offers a “film-onglass” touch-sensitive screen providing pilots with a choice when
accessing or navigating through EFB software applications. An
optional feature unique to the PilotView™ also enables a pilot to
immediately view what is on the other pilot’s display through the
touch of a single key.
Also unique to the PilotView™ is a one-touch video key
(standard feature) that enables the pilot to toggle between the
current application and video images from video surveillance
systems.
Multiple interfaces including integrated WLAN (802.11),
PCMCIA, USB 2.0, 10/100BaseT Ethernet, RS232, RS422
(optional), and ARINC 429 (optional) provide the operator with a
variety of methods for communications and updating of
PilotView™ data such as electronic charts and documents.
Optional discrete support is also provided to enhance
applications.
CMC, formerly known as Canadian Marconi Company, celebrated 100 years of innovation in
2003. As a world leader in high-technology products for the aerospace market, CMC has
installed over 17,000 various avionics units with over 100 airlines in more than 50 countries
around the world.
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2.
PILOTVIEW™ ELECTRONIC FLIGHT BAG (EFB)
The PilotView™ EFB is an avionics grade Class 21 Commercial-Off-The-Shelf (COTS) EFB
system specifically designed for flight deck environments to bring up-to-date Information
Technology-related advantages to the pilot.
The PilotView™ EFB consists of 2 LRUs: a lightweight, compact and self-contained
Electronic Display Unit (EDU); and a companion Expansion Module Unit (EMU).
Figure 1. EDU and EMU
(Enhanced EMU-EEMU with ARINC429 and video options shown)
2.1
PilotView™ Electronic Display Unit (EDU)
The EDU boasts an extremely high-quality, fully dimmable display that provides exceptional
readability in all cockpit lighting conditions. A “film-on-glass” touch-sensitive screen
complements the backlit “FMS-style” line select keys providing the user quick access to
specific functions such as:
Approach, airport or en-route electronic charts;
Checklists;
Electronic documents;
Performance calculations;
Surveillance and/or EVS video.
1
For a full description of Class 1, Class 2 and Class 3 Electronic Flight Bags and software applications, please refer to the FAA
Advisory Circular: AC No. 120-76A. This document can be downloaded from the Internet at the following site:
http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/B5DE2A1CAC2E1F7B86256CED00786888?
OpenDocument
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The PilotView™ EFB integrates several communication capabilities that provide flexibility for
operators to introduce applications as their cockpit information management requirements
evolve. It is truly a mobile cockpit information management tool offering the flexibility to be
used as installed cockpit avionics or as a PC “tablet”.
Please refer to Appendix 1 for an overview of communications capabilities.
2.2
PilotView™ EFB Specifications
2.2.1
EDU Characteristics
The EDU integrates a high-end display, processing capabilities and the user interfaces of the
PilotView™ EFB which include a touch screen as well as backlit bezel keys.
Several bezel keys are pre-defined to facilitate user navigation across applications.’Main’
provides a shortcut to the Master Menu application (see para. 4.2), ‘Apps’ lists active
applications. ‘Video’ launches CMC View if installed, a ‘Hot-Key’ button is also available and
user configurable.
In addition, and as shown in the photograph below, the display portion of the EDU slides up
to reveal an “FMS-style” alphanumeric keyboard with backlit keys.
Figure 2. PilotView™ EDU shown with keyboard extended
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Size
Weight
Casing
Battery
Display
8.5” H x 6.1” W x 1.5” D (216mm H x 155mm W x 40mm D);
3.5 lbs (1.6kg) including batteries
Machined Aircraft grade aluminium alloy.
Lithium Ion rechargeable (2 battery packs inside unit).
Active Matrix Liquid Crystal Display (AMLCD)
“Film-on-glass” touch-sensitive screen
Custom, Cold Cathode Fluorescent Lamp (CCFL) backlight
Low Voltage Differential Swing (LVDS) interface.
8.4”(214 mm) diagonal screen.
Resolution 1024 x 768 (XGA);
262,144 colors;
Fully dimmable from 800 nits to 1 nit;
Viewing Characteristics:
Vertical: +40°, -50°
Horizontal: +60°, -60°
The EDU display has very low reflectance and is readable in direct sunlight. An integrated ambient light
sensor automatically adjusts brightness levels.
In addition, at any time, the brightness level can also be easily adjusted using the controls in the upper
right corner of the EDU.
Memory
The EDU provides 512 Mbytes of Error Correcting Code (ECC) RAM (standard configuration).
ECC encoding protects the processing environment from electrical field interference, in particular, at
high altitudes.
As an option 1Gbytes of ECC RAM can be installed on the EDU.
Storage
The EDU has two internal interfaces that accommodate solid-state Compact Flash cards (providing a
storage capacity of up to 8 Gbytes) that provide high performance and reliability particularly in high
vibration environments.
Processing
Platform
The EDU is designed around the latest Centrino Mobile family Pentium-M® and employs a 1.1GHz
processor.
It includes a 400MHz system bus and Enhanced SpeedStep® power management.
The chipset integrates an Intel® Graphics and Memory Controller HUB (GMCH) as well a 3D graphics
engine that supports Intel’s Extreme Graphics 2 suite of graphics drivers.
EDU Power
Interfaces
EDU
Communication
Interfaces
In the aircraft, during normal operation, the PilotView™ EFB is powered by the EMU-EDU interface.
Battery backup in the EDU provides 40 minutes or more of independent power in the event of aircraft
power failure.
When used outside of the aircraft in a portable manner, the EDU is powered by an optional 110220Vac (50-60Hz) Power Adapter that is similar to a laptop computer power supply.
The EDU communicates with aircraft systems via the EMU and the EDU-EMU cable.
The EDU also provides an integrated IEEE 802.11 a/b/g wireless LAN communications capability.
Dual antennas are integrated in the EDU case for optimum performance.
This feature can be optionally removed.
For additional i/o communications, the EDU incorporates a single channel PCMCIA/Card Bus interface
on the motherboard through a TI PCI1510 Card Bus controller.
Two (2) USB 2.0 ports are available externally, one on each side, of the EDU to interface to external
devices such as USB memory stick or CD/DVD ROM.
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Integrated IEEE 802.11 a/b/g
Wireless LAN with dual
antenna.
Can be used for broadband
content upload and download
PCMCIA Type II Card Slot
Can be used for GSM/GPRS
card or Mass Storage
Brightness Sensor
Manual Dimming control
Two USB 2.0 slots are onboard.
Supporting CD/DVD reader
updates or USB memory stick.
Bezel keys provide efficient
access to applications
including zoom in/out, video
button and configurable ‘hot’
button
Locking mechanism for
integrated keyboard open/close
control.
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2.2.2
EMU and Enhanced EMU (EEMU) Characteristics
The Expansion Module Unit (EMU) provides certified aircraft power to the EDU protecting applications
from aircraft power spurious and short term interruptions.
The Basic EMU provides, as standard, the following interfaces between aircraft systems and the EDU:
RS232 (DB9).
Used for Weather data
inputs or GPS when
required.
2 x USB 2.0 ports.
High speed
communication and
USB power.
Aircraft Power Interface
10Base T Ethernet
EDU-EMU interface.
Delivers power and high
speed communications to
EDU
The Enhanced EMU provides the above interfaces as well as ARINC 429, RS422, discrete support and/or RS170 Video interface. Specific versions of the Enhanced EMU can be configured to satisfy specific aircraft
installation requirements.
ARINC429, RS422,
Discrete Support (DB26)
RS170/NTSC Video Input
EVS head down display and
secure camera
RS232 (DB9).
2 x USB 2.0 ports.
Aircraft Power Interface
EDU-EMU interface.
10/100Base T Ethernet
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The EMU is easily installed in any convenient, accessible location within 15’ (4.5 m) of the EDU (2).
Characteristics for the EMU and EEMU are listed below.
Power Conditioning
22-30Vdc, nominal 28Vdc
The EEMU provides power conditioning of the aircraft power and supplies 18Vdc to the EDU.
Input power interruptions of up to 200 milliseconds will not affect power output of the EDU.
Size
Base EMU:
6.86” L x 5.22” W x 1.0” D (174mm H x 133mm W x 25mm D)
Enhanced EMU : 6.88” L x 5.10” W x 1.87” D (175mm H x 130 mm W x 48mm D)
Weight
(Base and Enhanced EMU share mounting holes)
Base EMU:
1.0 lbs (470g max)
Enhanced EMU: 1.7 lbs (750g max)
Power Consumption
The EMU consumes 52W typical, 82W maximum (including EDU consumption)
The EEMU consumes 60W typical, 95W maximum (including EDU consumption).
The EDU consumes 45W typical, 75W maximum.
Standard Interfaces
Standard interfaces are provided by both the base EMU and Enhanced EMU:
Two (2) USB 2.0 interfaces
One (1) 10/100Base T RJ-45 interfaces
One (1) RS232 (DB9)
EDU-EMU interface
Optional Interfaces
Optional Interfaces available with the Enhanced EMU include:
Video Interface. Analog signal inputs can be RS170, NTSC or PAL.
Arinc429 which can be set for high or low speed with a choice of 1RX or 1RX +1
RX/TX configurations
Up to two optional RS422 interfaces
4 discrete inputs and 2 discrete outputs
The above optional interfaces can be configured based on customer requirements. CMC
provides a set of APIs for these interfaces and for development of Windows XP applications on
the EDU.
2
For installations requiring a longer distance between the EDU and EMU, an EECE unit can be used. Please refer to
the relevant section of this document for additional information.
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2.2.3
EDU and EMU Installation
As illustrated in the picture below, a typical installation of the PilotView™ EFB requires the
following elements:
Docking mount with latching device which holds the EDU to the mount and provides
power and high speed interface to the unit
EDU-EMU cable
Mount to aircraft which can vary depending on aircraft configuration and operators’
preference including side mounting, yoke mounting, or knee mount.
5’’ Mount Design
Latching Device
EDU-EMU Cable
Latching Device
The EDU accepts a docking mount that provides mounting, with a physical latch of the
system to the articulating mounting arm and hard-wired connections.
The associated I/O connections include power and USB 2.0. The pins in the connector
are hooded and the sockets protrude (similar to ARINC 600 connectors).
Hot-docking
The EDU is hot-pluggable and can be docked and undocked while active. There are no
impacts on applications provided appropriate actions are taken by the user to disable any
USB devices active across the USB ports.
Interconnect Cable
The interface cable between the EDU Docking Mount and (E) EMU is installation
dependent. The Interconnect Cable is a shielded, high flex (high strand count),
impedance controlled cable suitable for power and USB 2.0 transmission.
The cable can be up to 15” in length
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EECE
When the installation requires, the EDU to EMU Cable Extension (EECE) enables longer
distances between the EDU and EMU. Up to two EECE and associated cables can be
used to install the EDU up to 45” away from the
(E)EMU.
The EECE is self powered and
has the following characteristics:
Dimensions:
08’’ x 3.08’’ x 1.71’’
Weight :
0.2 lbs (90g)
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2.3
Aircraft Mounts
PilotView™ EFB is a Class 2 system. Associated installation requirements are as per AC12076a which mandate the use of a suitable mount. CMC has experience in yoke mounted,
side mounted EFB configurations as well as knee mounts where cockpit constraints or
operators preference mandate this option.
A physical survey of the aircraft is required to enable CMC to recommend the most costeffective, certified mounting solution. Such physical survey may cover the following
considerations:
Re-use of existing clip board location where applicable
Does not obstruct cockpit instrument panel viewing
Placed where pilot and co-pilot usually look for similar data
No obstruction to pilot entering seat
2.3.1
Side Mounts
CMC offers Side Mount in both 5” and 3”
design. Each mount is tested for cockpit
environment and crashworthiness.
CMC side mounts provide the following
benefits:
Single handed operation and
adjustment.
Pilot selectable positioning and viewing
angles
Hot-pluggable latching mount releases EDU for mobile use
Fully tested for use during all phases of flight
Simple design and operation
Robust hardware
When attached to the articulating arm, the EDU can be readily positioned, with one hand, for
optimal viewing by the pilot. In addition, since the EDU is “hot-pluggable”, it can be easily
removed for use in a portable fashion.
2.3.2
Yoke Mount
For some aircraft, yoke mounting will be a
preferred choice. CMC offers a yoke mount
which provides the same level of compliance to
cockpit environment as the Side Mounts.
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2.4
System Configuration
Depending on the choice of applications to be used, the PilotView™ EFB system can be
configured to operate with aircraft or third party systems including FMS, GPS units, Weather
transceiver data sources, communication systems such as Iridium or Satcom units, and
printers.
The EMU can interface with a GPS receiver to enable geo-centered moving maps (or “own
ship” position on moving maps when permitted). A cockpit printer, if so desired, can be
connected to one of the EMU’s USB ports. Optionally, the EMU can provide connectivity to
an on-board file server or video surveillance camera interface unit via the integrated
10/100BaseT interface.
Appendix –1- provides an overview of possible communication options.
In a standard dual configuration, each EDU is installed with its own EMU. Additional EDUs
can be installed in the cabin or galley if desired (bulk head configuration). The EDU/EMUs
can be linked together via a cross talk cable providing easy updating of documents for a
specific aircraft type or aircraft fleet.
CMC can provide reference installation documentation for interfacing of the PilotView™ EFB
with external systems such as Arinc429 FMS or GPS unit, RS232 GPS and weather units,
RS-422 weather units.
EDU - EMU cable
EMU to EMU cable
(10/100BaseT)
GPS
Printer
Weather
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2.5
“CMC-Approved” Peripherals
CMC has tested a variety of “cockpit-ready” printers, CD-ROM drives, File Servers, “memory
sticks” and other peripheral devices to ensure complete compatibility with the PilotView™
EFB. Please contact us for a list of approved devices.
3.
INSTALLATION
The PilotView™ EFB Installation Manual (available upon request: P/N 929-600040-000)
contains information regarding installation in the aircraft.
3.1
Qualification
The PilotView™ EFB meets the FAA AC 120-76A requirements for Electronic Flight Bags
(class 2), and is qualified to RTCA DO160-D. Please contact CMC for a copy of CMC’s DO160D qualification report.
3.2
PilotView™ MTBF / MTBUR
The predicted Mean Time Between Failure (MTBF) and Mean Time Between Un-scheduled
Repair (MTBUR) expressed in aircraft operating hours are defined as follows:
Table 1
Description
MTBF (1)
MTBUR (2)
PilotView™ EFB System(*)
6,000 hrs
5,100 hrs
(1) System comprised of EDU, EMU and associated EDU-EMU cable.
(2) MTBUR estimated at 85% of projected MTBF. May vary depending on operators’
definition for MTBUR.
3.3
PilotView™ Warranty
The PilotView™ EFB system is offered with a standard 24 months warranty. Longer term
warranty provisions can be offered depending on operators’ requirements.
Full details of the PilotView™ warranty are contained in the CMC’s “General Terms &
Conditions of Sale and Product Support Provisions” document, which also details after
warranty support and warranty available for repaired items.
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4.
APPLICATION ENVIRONMENT
4.1
Standard Software Applications
The PilotView™ EFB comes with a software application environment that includes the
following as standard:
PilotView™ Master Menu Software (user-configurable)
PilotView™ Note Taker
PilotView™ Setup and Test Tools
Adobe® Acrobat Reader® for .pdf documents
Microsoft® Windows® XP Professional Operating System (OS)
4.2
PilotView™ Master Menu Software
CMC offers a suite of industry leading applications to
satisfy the operational requirements for a wide range of
business jet and air-transport aircraft types.
The PilotView™ EFB application environment is
supported by a CMC-controlled Windows XP Operating
System and BIOS.
Depending on Operator’s requirements, CMC’s Master
Menu software provides a configurable environment for
rapid and consistent access to applications during
Flight Preparation, In-Flight and after the flight is
complete.
It provides the following key benefits:
Automatic launch at power. Operates as a shell
from the Windows XP environment simplifying user
navigation from application to application;
The Human Machine Interface is designed specifically to satisfy cockpit operations with
the use of large buttons, suitable colour-coding, and reduced steps to get to each
application rapidly at any time;
Applications operate in their native Windows environment without any requirement for
change or the need for software integration on the platform. Some application
enhancements may be required to fully leverage the Bezel and Line-Select key
capabilities provided with the PilotView™ EFB.
Configuration tools allow for changes to the Main Menu configurations while ensuring the
overall integrity of the EFB system.
A password protected access to native functions of the Windows XP environment is possible
at all times, should this be required.
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4.3
PilotView™ Note Taker
Included with the PilotView™ EFB is a “Note Taker”
application that provides up to ten (10) full pages of free
text.
These pages can be saved and retrieved at any time
during flight.
Each page allows entry of notes via the touch screen with
either a finger or “PDA-type” stylus to keep important data
such as clearances, waypoints, or other information close
at hand.
4.4
PlotView™ Setup and Test Tools
The EFB setup and test tools application provides the means to control the configuration of
applications by providing the capability for the customer to:
Specify user preferences including appearance and behavior of the EFB applications;
Set preferred security options via the SETUP application;
Choose which software application links are displayed on the Master Menu Screen as
well as the physical positioning of the links;
Set passwords to restrict access to protected areas, such as the Operating System
Customize the links to the e-Docs as well as modify the physical position of the links on
the main menu;
Specify the application that is launched when the “Hot-Key” button is pressed;
4.5
Adobe® Reader®
The PilotView™ EFB is shipped with an integrated document browser (Adobe® Acrobat
Reader®) that provides access to user-defined documents that are stored safely on its solidstate mass storage devices. Document links are gathered by topic, into three distinct
Categories: OPS (operational), MAINT (maintenance), REGS (regulatory). Each Category
allows up to 12 user configurable e-Docs links.
Amongst a range of optional applications which can be installed on the PilotView™ EFB,
CMC offers an enhanced version of a Document Viewer integrated with the EFB Content
Manager (ECM) software suite. This optional package offers enhanced browsing and
presentation support for PDF,XML, HTML based documents and an automatic means of
maintaining and updating the e-Docs configured on the PilotView™ EFB.
Please refer to the PilotView® Website for additional information on these CMC EFB
applications at www.cmcelectronics.ca.
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4.6
Operator-Specific Applications
The PilotView™ EFB will support any operator-specific applications that are compatible with
the Microsoft® Windows® XP environment. The standard “EFB Setup and Test Tools”
application (see paragraph 4.4) enables the user to modify the Main Menu to include
operator-specific applications.
CMC also provides installation recommendations for a large number of third party
applications including installation pre-requisites, recommended system configurations, and
suggested setup options. This information is provided as part of the Question and Answer
(Q&A) reference material.
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Appendix –1- Communications Capabilities
GPRS
IEEE 802.11a/bg
IEEE 802.11a/b/g
CWLU
(ARINC 763)
- access to file
server
- wireless printing
- cabin wireless
PilotView™
EDU
PilotView™
EMU
FMS
GPS
Units
Ethernet
Network File Server (ARINC 763)
Ethernet
VHF
or
VDL
ACARS* CMU
ARINC
724B/758
TWLU
GATELINK
(ARINC 763)
VPN Access
IP-Intranet
Video Converter
or
Video Surveillance
System
SATCOM
VPN access
IP-Intranet
VPN Access
IP-Intranet
SATCOM
ARINC 740
Printer*
Cameras
*Requires ACARS
s/w application in the
PilotView™ EFB
Figure 3
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