L3Harris™ DM N4-17/N Vor - Loc - Gs Balanced Loop Antenna - Blade Type - One Output
Our Part #:
SGP108005
Manufacture Part #:
DM-N4-17-N
Our Price:
$3,933.82
Price Per Each
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Approvals and Conformities
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Product Attributes
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Description
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Product Attributes
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Description
Country of Origin
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS
Approvals and Conformities
Alternate PN#s
DM N4-17/A
Product Attributes

United States
Shipping Weight
1.2 pounds
ECCN
7A994
Manufacturer P/N
DM N4-17/N
Schedule B Code
8529.10.4000
Pack Quantity
1
The DM N4-17 VOR/LOC/Glide Slope antenna is designed for general aviation, commercial, and military aircraft that operate up to Mach 1.0. The DM N4-17 is designed and qualified to provide a low-cost, lightweight, low-drag antenna for state-of-the-art avionics systems.
The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
Frequency Range:The antenna is not only T.S.O.'d, its performance parameters exceed the environmental specifications of MIL-E-5400 Class 3 equipment. Therefore, the DM N4-17 can be installed on single engine to jet engine aircraft.
The balanced loop design of the DM N4-17 assures an omnidirectional radiation pattern at the horizon to obtain the maximum signal for standard VOR and area navigation, which in turn provides more receiving distance and reliable system performance.
The standard system is the DM N4-17/N, which consists of two antenna elements (DM N4-17-1/N), two feed cables and gaskets (DM U212-1 and DM U23501 respectively), and a phasing coupler (DM N4-17-2). Dual output couplers (DM N4-17-4) are available as well.
VOR/LOC 108-118 MHz
GS 329-335.3 MHz
VSWR:
5.0:1 max
Polarization:
Horizontal
Radiation Pattern:
VOR/LOC Omnidirectional
GS:
Forward Pointing
Gain:
0 +/- 2 dB
Impedance:
50 Ohms
Lightning Protection:
dc short
Weight:
1.32 lbs
Connector:
BNC Female
Cable Length:
27 inches
Side Load:
17 psi
FAA Approval:
C34e, C36e, C40c
D0138 ENV. CAT. AA5XXXXXHDXS