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N4-17 Series VOR / LOC Glide Slope Antenna

The antenna is Technical Standard Order (TSO) certified and its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the N4-17 can be installed on single- to jet-engine aircraft.

The balanced loop design of the N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation. In turn, this provides more receiving distance and reliable system performance. The standard system is the N4-17/N, which consists of two antenna elements (N4-17-1/N), two feed cables and gaskets (U212-1 and U235-1 respectively) and a phasing coupler (N4-17-2). Dual output couplers (N4-17-4) are available as well.

N4-17 Series Antenna Specifications

N4-17 Series Antenna Specifications
Electrical
Frequency range  
VOC/LOC 108 – 118 MHz
Glide slope 329 – 335.3 MHz
VSWR 5.0:1 max
Gain 0 ±2 dB
Impedance 50 ohms
Polarization Horizontal
Radiation patterns  
VOC/LOC Omnidirectional
Glide slope Forward pointing
Lightning protection DC short
Power handling Receive only
Mechanical
Connector BNC female
Cable length 28 in
Side load 17 psi
Weight 1.32 lbs
Environmental
Drag See graph
FAA C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
N4-17 Specification Graph

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