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
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Approvals and Conformities

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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

Approvals and Conformities

Alternate PN#s
DM N4-17/A

Product Attributes

Country of Origin
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:
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