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CNX80
 

 Specifications

 GPS/WAAS receiver performance   

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Number of channels: 15 (12 GPS and 3 GPS/WAAS/SBAS)

Frequency: 1575.42 MHz L1, C/A code

Sensitivity (acquisition):

-116 dBm to -134.5 dBm GPS

-116 dBm to -135.5 dBm WAAS

Sensitivity (drop lock): -144 dBm

Dynamic range: > 20 dB

Lat/Long position accuracy: <1 meter RMS typical with WAAS (horizontal/vertical

Velocity: 1000 knots maximum (above 60,000 ft)

TTFF (time to first fix): 1:45 min. typical

Reacquisition: 10 seconds typical

Position update interval: 0.2 sec (5 Hz)

1 pps (pulse per second): ±275 nsec of UTC second

Datum: WGS-84

SATCOM compatibility: Compatible on SATCOM-equipped aircraft

 

  VHF Comm transmitter performance   

Class: 4

Output power: 8 watts minimum carrier at >12 Vdc input

Frequency range: 118.000 to 136.975 MHz, 760 channels

Stuck mic time-out: 35 second time-out, reverts to receive

 

 VHF Comm receiver performance 

Class: D

Frequency range: 118.000 to 136.975 MHz, 760 channels

Sensitivity: 1 µV (2µV hard) for 6 dB S+N/N with 30% modulation at 1000 Hz

Selectivity: < 6 dB variation at ± 7 kHz, > 60 dB at ± 22 kHz

Squelch control: Automatic squelch with manual override

 

 VHF Nav receiver performance   

VOR

Frequency range: 108.00 to 117.95 MHz in 50-kHz increments

Receiver sensitivity:

  • 108 MHz –115 dBm typical
  • 117 MHz –117 dBm typical

Course accuracy: RTCA DO-196 two sigma limit: 3°

Localizer

Frequency range: 108.00 to 111.95 MHz

Receiver sensitivity: 115 dBm typical

Centering error: RTCA DO-195 two sigma limit: 6.6% of full scale

GNS 480 performance: less than 1.0% typical (1.5 mV)

GNS 480 performance: less than 0.5 typical

Glideslope

Frequency range: 329.150 to 335.00 MHz

Receiver sensitivity: 95 dBm typical

Centering error: RTCA DO-195 two sigma limit: 6.7% of full scale

GNS 480 performance: less than 2.0% typical (3.0 mV)

 

 TSO authorization   

Comm

TSO-C37d, DO-186a Class 4, Txr 100 nm range/TSO-2C37e

TSO-C38d, DO-186a Class D, Rxr 25 kHz channels/TSO-2C38e

TSO-C128, DO-207, Stuck Mic/TSO-2C128

VOR/ILS

TSO-C34e, DO-192 Cat B, Glideslope/TSO-C34e

TSO-C36e, DO-195 Cat B, Class A, Localizer/TSO-C36e

TSO-C40c, DO-196 Cat B, VHF Omni Range/TSO-2C40

GPS/WAAS

TSO-C146a, DO-229C, Class Gamma 1, 2, 3 (LPV)/TSO-C146

MFD

TSO-C113, DO-257, Display System/TSO-C113

 

 Electrical

Input voltage: 10 Vdc to 36 Vdc

Input current (Main input):

1.4 A typical, 2.2 A max (heater off) at 14 Vdc
2.4 A typical, 3.2 A max (heater on) at 14 Vdc
0.7 A typical, 1.1 A max (heater off) at 28 Vdc
1.2 A typical, 1.6 A max (heater on) at 28 Vdc

Note: Backlight heater turns on when internal unit temperature is below approximately 42°C.

Input current (VHF Nav input):

450 mA typical, 700 mA max at 14 Vdc
200 mA typical, 350 mA max at 28 Vdc

Input current (Comm input):

270 mA typical, 1.8 A max at 14 Vdc, receive
130 mA typical, 900 mA max at 28 Vdc, receive
2.1 A typical, 3.2 A max at 14 Vdc, transmit
1.0 A typical, 1.6 A max at 28 Vdc, transmit

Note: Receive max at full receive audio, transmit max at 90% modulation at 1000 Hz.

 

 Physical   

Height: 3.3 inches (84 mm)

Width: 6.25 inches (158.75 mm)

Depth (behind faceplate): 11.7 inches (297 mm) includes mounting frame and connectors

Weight:

5.8 lbs. (2.6 kg) unit only
0.7 lbs. (0.3 kg) mounting tube

 

 Environmental 

The GNS 480 unit is designed and tested to meet appropriate categories of DO-106D.

Operating temp.: -20°C to +55°C

Storage temp.: -55°C to +85°C

Temp. variation: 2°C per minute

Humidity: 95% at 50°C

Maximum altitude: 55,000 feet

Cooling: None required (provided internal fans are unobstructed and operating)

Vibration: Fixed Wing and Helicopter

 

 Interfaces 

ARINC 429, Aviation RS-232, CDI/HSI, RMI (digital; clock/data); Superflag Out, Altitude (interface allows baro correction potentiometer to be connected directly to the GNS 480); Synchro heading input (five-wire XYZ); Message Audio output to provide audible alerts to the pilot; Infrared Interface (currently not enabled, but will be used in the future to send and receive flight plan, TFR, and user waypoint information through PDA with infrared capabilities). Skywatch, GTX33, GTX32 for TIS-A traffic display. FADC, AHRS.

Specifications are subject to change without notice.

 

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