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Контакты
Головной Офис Объединенные Арабские Эмираты Международный Аэропорт Шарджа
тел.: +971 6 5570710
факс: +971 6 5570495
По вопросам продаж: sales@trast-aero.com
Series III VHF Navigation Receiver designed for regional air carriers and corporate aviation aircraft
Standard glideslope and marker beacon receivers
Digital VOR/LOC and glideslope converters
ARINC 429 Input/Output for compatibility with EFIS and digital FMS
Special heat sink and cooling fin design dissipates heat with max efficiency
Converts VOR/LOC and glideslope signals from three independent receiver modules to digital format virtually eliminating CDI needle oscillations
Automatic calibration of VOR converter ensures nav guidance accuracy despite passage of time or temperature changes
Digital tone filters in LOC and GS converters eliminate need for periodic system realignment
Additional filtering virtually eliminates needle oscillations from rotor modulation in helicopter installations
Compatible with most HSIs, CDIs, RMIs, and conventional marker beacon displays
Models available with ICAO Annex 10 Modification for FM immunity for use in Europe (see table below)
Models available that measure azimuth in VOR mode as Bearing TO or Radial FROM VOR ground stations (see table below)
Models available with 10 or 40 MW audio output (see table below)
Compatible with GNS-XLS Navigation Systems
Used with CD-412B or CD-413B digital control units
Характеристики
Dimensions: 4.10"W x 4.0"H x 13.33"D
Temperature: -55 to 70C
Freq Range: 108.00-117.95 MHz
Channel Spacing: 50 kHz
LOC Channels: 40
OBS: course resolver EZ'd at 300 deg. with 400Hz
VOR/RMI Outputs: 4-wire 400Hz Sine/Cos or 4-wire DC Sine/Cos
TSO: (VOR) C40b, DO-153A (LOC) C36c, DO-131A, Class E RTCA Env. Cat. F2A/MNO/XXXXXXABABA
GS TSO: C34c, DO-132A, Class D, RTCA Env. Cat. F2A/MNO/XXXXXXABABA
Marker TSO: C35d, DO-143, Class A, RTCA DO-160A Env. Cat. F2A/MNO/XXXXXXABABA
ARINC 429 Interfaces: VOR deviation, VOR flag, LOC deviation, LOC flag, GS deviation, GS flag, marker passage, RMI data and DME tuning provided as outputs, ADF data from DFS 43 ADF system accepted as input data. Dedicated input bus for FMS such as KNS-660/GNS-XLS
Weight: 6.26 lbs.
Altitude: to 55000 ft.
Power Requirements: 18-33 VDC, 0.8A max
VOR Channels: 160
VOR Accuracy: +/-1 deg.
LOC Accuracy: +/-5.0 mV
RMI Accuracy: =/-1.5 deg. typical
Glideslope Channels: 40
Eurocae (GS): 1/WG.5/66 Env. ED-14A
Eurocae (MB): 1/WG.7/70 Env. ED-14A
Модификации
Чертежный номер
Описание
066-1101-00
10MW audio, Bearing TO display
066-1101-01
Fokker model, 10MW audio, Radial FROM display
066-1101-10
BAE model, 10MW audio, Bearing TO display
066-1101-20
Lear model, 40MW audio, Bearing TO display
066-1101-30
Fokker model, 10MW audio, Radial FROM display, ICAO Annex 10
066-1101-40
BAE model, 10MW audio, Bearing TO display, ICAO Annex 10
066-1101-50
Lear model, 40MW audio, Bearing TO display, ICAO Annex 10
