COMANT
CI 119 VHF Communications
Part No: CI-119
DESCRIPTION
CI 119 VHF Communications
Designed for large single or twin-engine aircraft. The antenna assembly is enclosed in an aerodynamically shaped, injection molded polyester glass shell with internal components foamed in place for mechanical integrity. Reduced height convenient for mounting to the underside of an aircraft. The CI 119 has been re-tested and upgraded to the new RTCA DO-160D environmental requirements and offers the 118 to 137 MHz frequency associated with DO-186 MOPS.
Comant’s four internal hole mount blade style VHF communication antenna with offset BNC port. Equivalent to the CI 138, CI 139 and CI 196 expect for variations to BNC location and hold pattern. Suitable for either top or bottom mounting with both light and heavy fixed wing single / multiengine and helicopter aircraft.
Applications
Single and twin engine piston aircraft for applications. This antenna design features an offset connector. Consult your FBO or installation shop for best application information.
The antenna assembly enclosed in an aerodynamically shaped, injection molded polyester glass shell with internal components foamed in place for mechanical integrity. Reduced height convenient for mounting to the underside of an aircraft. The 119 has been re-tested and upgraded to the new RTCA DO-160D environmental requirements and offers the 118 to 137 MHz frequency associated with DO-186A MOPS.
Frequencies Covered 118 - 137 MHz
Specifications
Electrical :
FREQUENCY | 118 - 137 MHz |
VSWR | 2.5:1 Maximum |
POLARIZATION | Vertical |
RADIATION PATTERN | Omnidirectional |
IMPEDANCE | 50 Ohms |
POWER | 25 Watts |
Mechanical :
WEIGHT | 1.25 lb. Maximum |
HEIGHT | 13.0 in. Maximum |
MATERIAL | Valoz 420 |
FINISH | White Polyurethane Enamel |
CONNECTOR | BNC |
GASKET | C12704 Cork Neoprene |
Environmental :
TEMPERATURE | -55°C to +85°C |
ALTITUDE | 35,000 ft. |
AIR SPEED | 350 Knots TAS @ 25,000 ft. |
Federal Specifications :
RTCA ENVIRONMENTAL | DO-160D |
ENVIRONMENTAL CATEGORY | [D2X]ACB[R(C,C1)U(F,F1)] XWFDXSXXXXX[XX]X[XXXX]XAX |
FAA TSO | C37d, C38d |
RTCA MOPS | DO-186A |