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Reservoir with sight gauge
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Back-up accumulator
2.1.3
2.1.4
2.1.5
2.1.6
Communications equipment
1.
KMA 24H Audio Control/Voice activated intercom connected to both crew seats and six cabin positions.
2.
Dual Bose noise-cancelling aircraft powered pilot and co-pilot headsets.
3.
Sat Talk II Satellite Telephone System comprising L Band Antenna, Audio Control Unit, Power and Data cables, and Iridium 9505A Portable Handset (including Cradle Mount).
Navigation and guidance equipment
1.
Dual AM 250 Digital Encoding Altimeter/Air Data Computers
2.
Dual Garmin GNS 530A Nav/Comms Global Positioning System, able to be upgraded to C146, C146a and WAAS, and capable of integration with Automatic Dependent Surveillance-Broadcast (ADS-B) In and Out (subject to regulatory directive from CASA and final definition of standards).
3.
Dual KT73 ATC Mode S Transponders
4.
KCS 55A
5.
KI 204 Standby Nav Indicator
6.
KN 63 DME with Nav.1 / Nav.2 / Hold
7.
Dual KNI 582 RMI
8.
KR 21 Marker Beacon
9.
KR 87 Automatic Direction Finder
10.
KRA 405B Radar Altimeter
11.
KRG 332 Yaw Rate Gyro
12.
Litef AHRS – LCR 93
13.
RDR 2000 Weather Radar
14.
WX 500 Stormscope
15.
KMD850 Multi Function Display
16.
Electronic Flight Bag, including Jeppview software
17.
Becker SAR-DF-517 Search and Rescue Direction Finder with 3” Display and RS232 output.
Electronic flight controls
1.
Pilot EFIS 50 Electronic Flight System comprising Dual ED462 EAS Tube EADI/EHSI, SG465 EFIS Symbol Generator, and CP468 EFIS Control Panel
2.
KFC325 Autopilot System comprising KDC220 A/P Computer, KDC222 Air Data Computer, KTA33C Pitch Trim Adapter, Triple KSA372 Servos, KAS297C Altitude Pre-Selector, and KMC321 Mode Controller.
Flight controls
The aircraft shall be fitted with pilot and co-pilot flight instruments and controls:
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Dual pilot static system
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Airspeed indicator
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Vertical speed indicator
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Clock/stopwatch
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Standby magnetic compass
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Standby attitude indicator
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Standby altimeter
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Flap position indicator
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Triple trim indicator
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Cabin rate of climb indicator
.
Cabin altitude and differential pressure indicator
.
Landing gear position lights
The aircraft shall be fitted with:
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All mechanical primary flight controls
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