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KEY OWNER/USER BENEFITS Unsurpassed flexibility and crew coordination with centralized,
fully integrated system Terminal and en route ADI display modes eliminate unnecessary
information Airspeed and trend displays Integrated system architecture offers extensive reversionary
capabilities Improved integrated system diagnostic capability minimizes
the need for line test equipment Full-sky ADI and three-dimensional runway provide more realistic
view of outside world Multiple-mode EHSI provides dual course arrows, waypoints,
weather radar and sensor source selection on a single display MFD provides a shared data information window without disrupting
ADI/HSI display modes Two-, three-, four- and five-tube configurations available 4 x 4-inch display saves
console space Compatible with FCS-65 or FCS-80 and AHC-85 Compatible with EGPWS for bolt-on applications that utilize
global positioning systems and on-board global terrain databases to provide
pilots with a picture of the terrain in front of them
OVERVIEW
The EFIS-84 Electronic Flight Instrument System combines Electronic
Attitude Director Indicator/Electronic Horizontal Situation Indicators (EADI/EHSI)
with a center panel Multifunction Display (MFD) to provide a fully integrated
flight deck display system. The electronic ADI expands the horizons of a conventional
four-inch electromechanical instruments with a 50 percent larger earth/sky
representation for terminal and en route formats. The electronic HSI combines
multiple display formats with weather radar and built-in NAV source selection
for simplified coordination of all navigation and weather avoidance tasks.
The MFD augments the EADI/EHSI displays by providing the pilot and copilot
with additional navigation, weather avoidance, data management and reversionary
functions.
DESCRIPTION
The EFIS-84 system is comprised of a family of components that can be
configured to meet various flight deck display applications. The system components
are: DSP-84 Display Select Panel
The DSP-84 provides EHSI format selection, active and preset navigation
sensor selection, bearing pointer selection, NAV data selection and weather
radar on the EHSI. The DSP allows decision height to be set on the EADI. Additionally,
course, course direct to, heading and heading sync are selected from the DSP.
DPU-84 Display Processor Unit
The DPU-84 provides the necessary deflection and video signals for up
to two EFD-84 Electronic Flight Display units. It contains aircraft systems
I/O interface and provides sensor input processing and switching.
EFD-84 Electronic Flight Display
The EFD-84 provides a 4 x 4-inch multicolor
CRT instrument display of an EADI or an EHSI with a lighted inclinometer.
MFD-85B Multifunction Display
The MFD-85B provides a multicolor CRT instrument display of weather
radar, pictorial navigation map, page data, waypoint definition, display of
multiple waypoints and remote data.
MPU-84 Multifunction Processor Unit
The MPU-84 provides the necessary deflection and video signals for the
MFD. It is similar to the DPU except it has expanded I/O capability for a
second set of aircraft systems.
The EFIS-84 can be configured in two-, three-, four- or five-tube systems
depending on the flight deck application. (See tables for system totals and
equipment complement.) The EFD-84 and MFD-85B contain a CRT, deflection yoke, video and deflection
amplifiers and high-voltage power supply. The CRT is a high-resolution color
tube. The CRT has an in-line gun with shadow mask that uses a black matrix
surrounding pigmented phosphor dot trios; this provides high contrast along
with high resolution. A custom designed, multiband pass optical filter is
used to provide enhanced contrast. Both stroke and raster scanning techniques
are used to provide large area color background for weather and distinct alphanumerics
and symbols with high brightness. Mode select and display control functions
are located on the display bezel for the MFD-85B. EADI
The EADI display provides an ADI presentation that can include the following
(with defined sensor inputs):
Pitch and roll attitude Steering commands (single or dual queue) Vertical deviation (glidescope) Localizer deviation Autopilot mode annunciation (analog, digital) Radio altitude Decision height Marker beacon annunciation Fast-slow deviation Indicated airspeed Trend vector VNAV Cat II comparator logic Rising runway Microwave landing system EHSI
The EHSI display has two basic modes: full compass rose and compass
sector. The full compass mode presents compass rose similar to existing electromechanical
instruments. Information available in this mode includes the following with
defined sensors inputs:
True/magnetic heading Selected heading Selected course Navigation data source annunciation lateral deviation To/from Distance to station waypoint Ground speed, time-to-go, elapsed time Bearing pointer (VHF omnidirectional radio range, automatic
direction finder, etc.) Vertical deviation (vertical navigation or global positioning
system) Weather radar return information (four-color, path athenuation
compensation alert) Cat II comparator Wind vector Map of sector mode
OPERATION AND PERFORMANCE
The EFIS-84 system provides system operational capability in the event
of a system element failure. The following paragraphs describe this capability
with reference to any operational differences that may be required. DSP-84 Display Select Panel Failure
In the event of a DSP-84 failure, an external switch can be actuated
that allows the cross-side DSP-84 to provide control for the affected EADI
or EHSI.
DPU-84 Display Processor Unit Failure
In the event of a DPU-84 failure, an external switch can be actuated
that allows the cross-side DPU-84 to provide inputs to the affected EADI and
EHSI. The cross-side DSP-84 controls the EADI and EHSI displays.
EFD-84 Electronic Flight Display Failure
In the event of an EFD-84 failure, an external switch can be actuated
to cause either the EADI display to transfer to the EHSI in composite format
or the EHSI to transfer to the EADI to form the same composite format. An
optional strap allows the EADI and the EHSI to be transferred unchanged to
the cross-side EADI and EHSI.
MFD-85B Multifunction Display Failure
In the event of an MFD-85B failure, there is no backup capability for
the display. The NAV and weather modes are available for display on the EHSI
when operating in SECTOR or RDR modes. Checklist and remote data functions
are lost.
MPU-84 Multifunction Processor Unit Failure
In the event the single MPU-84 fails, external switching of the digital
bus lines is required to maintain cross-side data on either side EADI or EHSI.
Backup drive capability to the EADI and EHSI is lost as well as the MFD-85B
display. The weather radar modes are still available on the EHSI.
EFIS-84 SYSTEM CERTIFICATIONS Beech 200 | Beech 1900D | Cessna 441 | Fairchild
Metro 23 | Lockheed 1329 |
TYPICAL SYSTEMS DSP-84 | 1 | Display Select Panel | 622-9683-001 | DPU-84 | 1 | Data Processing Unit | 622-9682-002 | EFD-84 | 2 | Electronic Flight Display | 622-9681-001 |
DSP-84 | 1 | Display Select Panel | 622-9683-001 | DPU-84 | 1 | Data Processing Unit | 622-9682-002 | EFD-84 | 2 | Electronic Flight Display | 622-9681-001 | MFD-85B | 1 | Multifunction Display | 622-7876-011 | MPU-84 | 1 | Multifunction Processor
Unit | 622-9684-002 |
DSP-84 | 2 | Display Select Panel | 622-9683-001 | DPU-84 | 2 | Data Processing Unit | 622-9682-002 | EFD-84 | 4 | Electronic Flight Display | 622-9681-001 |
DSP-84 | 2 | Display Select Panel | 622-9683-001 | DPU-84 | 2 | Data Processing Unit | 622-9682-002 | EFD-84 | 4 | Electronic Flight Display | 622-9681-001 | MFD-85B | 1 | Multifunction Display | 622-7876-011 | MPU-84 | 1 | Multifunction Processor
Unit | 622-9684-002 | Note(s): | See Installation Hardware table for mounts and connectors |
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SPECIFICATIONS FAA TSO | C6c, C52a | C3b, C4c, C6c, C34c, C36c, C40b, C52a | Environmental | DO-160A D1/B/PKS/XXXXXXAZAAA | DO-160A D1/A/PKS/XXXXXXAZAAA | EUROCAE | ED-14A | ED-14A |
Height | 47.62
mm (1.875 in) | 106.04 mm (4.175 in) | Width | 146.1 mm (5.75 in) | 106.04 mm (4.175 in) | Length | 203.2
mm (8.00 in) | 259.08 mm (10.2 in) | Weight | 1.31 kg (2.9 lb) | 2.3 kg (5.0 lb) | Mounting Information | Dzus | Panel-mounted |
Temperature | -20 to 55°C | -20 to 55°C | Altitude | 50,000 ft | 50,000
ft |
Input Power | 28
V DC, 5.5 W | 28 V DC, 55 W | Lighting | 5 V AC/DC, 7.7 W 28 V DC, 4.1 W | 5 V AC/DC, 1.4 W 28 V DC, 1.2 W |
FAA TSO | C6c, C63b | C3b, C4c, C6c, C34c, C36c,
C40b, C52a | C3b, C4c,
C6c, C34c, C36c, C40b, C52a | Environmental | DO-160A D1/A/PKS/XXXXXX
AZAAA | DO-160A F2/A/MNO/XXXXXX ZAAAA | DO-160A F2/A/MNO/XXXXXX
ZAAAA | EUROCAE | ED-14A | ED-14A | ED-14A |
Height | 120.14
mm (4.730 in) | 194.8
mm (7.67 in) | 195.6 mm (7.70 in) | Width | 159.5 mm (6.28 in) | 128-9 mm (5.08 in) | 128.9 mm (5.085 in) | Length | 314.5
mm (12.38 in) | 372.1
mm (14.65 in) | 372.1 mm (14.65 in) | Weight | 4.36 kb (9.6 lb) | 6.4 kg (14.1 lb) | 7.7 kg (17.0 lb) | Mounting Information | Panel mounted | UMT-14, UMT-14A, UMT-14B | UMT-15, UMT-15A, UMT-15B |
Temperature | -55
to 70°C | -55
to 70°C | -55 to 70°C | Altitude | 55,000 ft | 55,000
ft | 55,000 ft |
Input Power | 28
V DC, 42 W | 28 V
DC, 66 W | 28 V DC, 143 W | Lighting | 5 V AC/DC, 5.8 W 28 V DC, 4.6 W | | |
ALT-50/55, AL-101 | DC analog | ADC-80
and ADA-85 | CSDB | ADC-82/85/86 | CSDB | VIR-30A | AC
sin/cos | VIR-31 | Three-wire synchro | VIR-32 | CSDB | VIR-432 | ARINC 429 LS | DME-40 | ARINC 568 | DME-42 | CSDB | DME-442 | ARINC 429 LS | TCN-40/42 | Analog, ARINC
568 | TCN-118 | ARINC 582 (six-wire) | TCN-500 | ARINC 429 LS | ADF-60A | Three-wire
synchro | ADF-60B | DC sin/cos | ADF-462 | ARINC 429 LS | 332D-11 | Three-wire synchro | MC-103/MCS-65 | Three-wire
synchro | FCS-65 | AC/DC analog, discretes, CSDB | FCS-80 | AC/DC
analog, discretes | APS-85 | CSDB | FMS-90,
VLF, INS, LRN | ARINC 429 HS, ARINC 561 or CSDB output | RNV | ARINC 429 LS | AHC-85 | CSDB | AHC-85E | ARINC 429 HS | WXP-85C/D,
WXP-850A/B | Serial digital | ASI-80D/F, MSI-80C/D/E | DC analog | AOA
or FAST/SLOW | DC analog | MLS | ARINC 429 LS | DF-301E | AC
synchro |
Roll angle | ADF bearing | Pitch
angle | Radio
altitude | Heading | Roll steering | VOR/TCN
bearing | Pitch
steering | ADF bearing | Localizer deviation | | | Glideslope
deviation | | | AOA or F/S deviation |
ADC data | To/from | DME
data | Sensor
valids | VLF/INS/RNV/LRN/FMS/LNV
data | Sensor modes | DSP
data | EFIS
and I/O straps | Cross-side data | FCS modes | WXR
data | CAT
II request | MLS glidepath and azimuth | Localizer tuned | FCS
modes and data | DG mode | Attitude/heading/acceleration | Master warn reset | ADF
data | Comparator
reset | VOR data | Marker beacons | TCN
data | |
Heading error | Lateral deviation | DSP control | To/from | Course
datum error | Vertical deviation | FMS waypoint
load | Back
course | | | | FCS
data | Modes/status/valids | | | | Cross-side
data | Master
warn | | | | | Comparator warns | | | | | CAT
II amber | | | | | CAT II green | | | | | High
temperature warn | | | | | DH out | | | | | RA
test | | | | | Excessive deviation | | | | | Excessive
attitude |
SELECTION GUIDE DSP-84 | | X | DPU-84 | 622-9683-001 | | | X | | DPU-84 | 622-9683-002 |
DPU-84 | | | X | X | X | X | X | 622-9682-002 | Note(s): | Full sky or racetrack available |
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EFD-84 | X | | | | X | | X | 622-9681-001 | | | X | | | | X | X | | 622-9681-002 |
MFD-85A | | | | X | 622-7236-011 | | | | | X | | 622-7236-012 | MFD-85B | X | | | X | 622-7876-011 | | | X | | X | | 622-7876-012 |
MPU-84 | | | X | X | X | X | X | 622-9684-002 | Note(s): | Both full sky and racetrack ADI displays available |
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INSTALLATION HARDWARE | | 1 or | Mating Connector, J1, 25
pin, Crimp style | 1 | 371-0213-030 | | | 1 | Mating Connector, J1, 25 pin Solder style | 1 | 371-0221-000 | | | 1 or | Mating Connector, J2, 50
pin, Crimp style | 1 | 371-0213-050 | | | 1 | Mating Connector, J2, 50 pin, Solder style | 1 | 371-0181-000 | | | 75 | Contact Pins, Crimp | 2 | 371-0213-110 | | | 1 | Keying Kit (2 per kit) | | 629-8381-001 | | | 1 | Screw Lock Assembly Kit, J1 | | 371-0040-010 | | | 1 | Screw Lock Assembly Kit, J2 | | 371-0040-040 | | | 1 | Cable Clamp, J1 | | 371-0146-000 | | | 1 | Cable Clamp, J2 | | 371-0148-000 | Note(s): | Choose crimp or solder style Order pins, as required, with crimp style connector
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UMT-14 | 1 | Mount, 1/2 ATR short, full
height | 1,
2 | 622-6171-001 | or | | | | | UMT-14A | 1 | Similar to UMT-14 with built-in 115V/400 Hz fan | | 622-6901-001 | or | | | | | UMT-14B | 1 | Similar to UMT-14 with
built-in 28 V DC fan | | 622-7265-001 | or | | | | | 390R-23 | 1 | Mount, 1/2
ATR short, full height, use UMT-14 where
possible | | 622-6548-001 | | | 1 | UMT-14( ) grounding bracket | | 634-2626-001 | | | 2 | Mating connector kit, 4 row, full height, Collins
Thin Line, 160 pin | | 634-1020-001 | | | 320 | Contact pins, up to 0.050 dia. over insulation | 3 | 372-2514-110 | | | or | | | | | | 320 | Contact pins, 0.050-0.080 dia. over insulation | | 372-2514-180 | | | 1 | Blower (Rotron) | 4, 5 | 009-1965-030 | Note(s): | Choose one UMT-14 includes openings for cooling air and is the preferred
mount The 390R-23 is approximately 0.25 inches shorter
in height than the UMT-14 Choose as required for total quantity/unit Uses one per DPU or MPU where other means of cooling is not
provided Uses optional Rotron monitor (VPN 034358)
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| | 2 | 25 pin Cannon D Subminiature | | 371-0213-030 | | | 50 | Contacts (pins) | | 371-0213-110 | | | 2 | Connector Hood | | 371-0146-000 | | | 2 | Screw Lock Assembly Kit | | 371-0040-010 | | | 2 | Polarization Plugs Kit | | 629-8381-001 | | | 1 | Inclinometer, black, lighted, 5
V DC or AC | 1, 2 | 634-4320-001 | | | or | | | | | | 1 | Inclinometer, gray, lighted, 5
V DC or AC | | 634-4320-002 | | | or | | | | | | 1 | Inclinometer, black, lighted, 28
V DC or AC | | 634-4320-003 | | | or | | | | | | 1 | Inclinometer, gray, lighted, 28
V DC or AC | | 634-4320-004 | | | or | | | | | | 1 | Inclinometer, black, lighted, 5
V DC or AC | 3 | 634-4320-005 | | | 4 | Machine screw (8-32 UNC-2A) | | Customer-supplied | Note(s): | Choose one Used for ADI position only NVIS compatible
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UMT-15 | 1 | Mount, 3/4
ATR short, full height | 1, 2, 3 | 622-6172-001 | or | | | | | UMT-15A | 1 | Similar to UMT-15 with built-in 115 V/400 Hz blower | | 622-6902-001 | or | | | | | UMT-15B | 1 | Similar to UMT-15 with built-in 28 V DC fan | | 622-7266-001 | or | | | | | 390R-24 | 1 | Mount, 3/4
ATR short, full height, use UMT-15 where possible | | 622-6549-001 | | | 1 | UMT-15( ) grounding bracket | | 634-2627-001 | | | 3 | Mating connector kit, 160 pin, 4 row, full height,
Collins Thin Line | | 634-1020-001 | | | 480 | Contact pin, up to 0.050 dia. over insulation | 4 | 372-2514-110 | | | or | | | | | | 480 | Contact pin, 0.050 to 0.080 dia. over insulation | | 372-2514-180 | | | 1 | Blower (Rotron) | 5 | 009-1965-030 | Note(s): | Choose one UMT-15 includes openings for cooling air and is the preferred
mount The 390R-24 is approximately 0.25 inches shorter
in height than the UMT-15 Cooling air is required Use fan specified if other means of cooling is not provided Choose as required for total quantity/unit Uses optional Rotron monitor (VPN 034358)
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IMT-300 | 1 | Mount | 1 | 622-4333-001 | or | | | | | IMT-85 | 1 | Combined mount for MFD and
WXP | | 622-6878-001 | | | 1 | Mating connector, 55 pin, high density, circular crimp
removable contacts | 1 | 359-0635-180 | | | or | | | | | | 1 | Mating connector, 55 pin, high density with grounding
fingers and crimp removable contacts | | 359-0645-170 | | | 1 | Clamp, strain relief, straight | 1 | 859-6604-140 | | | or | | | | | | 1 | Clamp, strain relief, 90° | | 359-0637-150 | | | 1 | Blower (Rotron) | 2 | 009-1965-030 | Note(s): | Choose one Cooling air is required for MFD
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Two-Tube EFIS-84 | 12.3
kg (27.1 lb) | 181.5
W | 6.5/10.5 | Three-Tube
EFIS-84 | 24.4 kg (53.6 lb) | 366.5
W | 11.1/16.3 | Four-Tube
EFIS-84 | 24.6 kg (54.2 lb) | 363
W | 13/21 | Five-Tube
EFIS-84 | 36.7 kg (80.7 lb) | 548
W | 17.6/26.8 |
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