Avionics Requirements Sample Clauses

Avionics Requirements. 3.4.1 An intercommunications system (ICS) must be provided for the pilot, observer/copilot, and any additional required crewmember positions. ICS operation may be via either voice-activation (VOX) or push-to-talk (PTT). If PTT, the pilot’s PTT switch(es) must be mounted on the flight controls (helicopter cyclic or airplane control yoke), with cord-mounted PTT switches at any other required positions. ICS audio must mix with, but not mute, selected receiver audio. An ICS audio level control must be provided. ICS sidetone audio must be provided for the earphones corresponding with the microphone in use. The ICS audio output must be free of excessive distortion, hum, noise, and crosstalk and must be amplified sufficiently to facilitate ease of use in a noisy cockpit/cabin environment.

Avionics Requirements. Resource Reconnaissance II 3.4.1 Avionics equipment for this approval level is dependent upon the type of mission being flown and must be determined by the using bureau entity as required.

Avionics Requirements. 4.4.1 One panel- mounted global positioning system (GPS) must be permanently installed in the aircraft. The GPS must reference latitude and longitude coordinates for aircraft positioning, utilize an approved, fixed, external aircraft antenna, and be powered by the aircraft electrical system. The GPS installation must be FAA approved (or approval pending). Handheld and/or marine-type equipment is not acceptable. 4.4.2 An intercommunications system (ICS) must be provided for the pilot, observer/copilot, and all required crewmember positions. ICS audio must mix with, but not mute, selected receiver audio. ICS sidetone audio must be provided for the earphones corresponding with the microphone in use. The ICS audio output must be free of excessive distortion, hum, noise, and crosstalk and must be amplified sufficiently to facilitate ease of use in a noisy cockpit/cabin environment. 4.4.3 Microphones, PTTs, and jacks. 4.4.3.1 The system must be designed for operation with 600 ohm earphones and carbon-equivalent, noise- canceling boom-type microphones (Gentex electret type Model 5060-2, military dynamic type M-87/AIC with CE-100 TR preamplifier, or equivalent). The pilot position only may be configured for low impedance (dynamic) operation.

Avionics Requirements. The following systems shall be furnished, installed, made operable and maintained by the Vendor in each agreement aircraft in accordance with the installation and maintenance standards of this agreement.

Avionics Requirements. Resource Reconnaissance I 2.5.1 Navigational systems: One global positioning system (GPS) must be installed in the aircraft. The GPS must utilize the WGS-84 datum, reference latitude and longitude coordinates in the DM (degrees/minutes/decimal minutes) mode for aircraft positioning, and be powered by the aircraft electrical system. Panel- mounted units must utilize an approved, fixed, external aircraft antenna. Portable units must be securely mounted and must utilize an antenna which is external to the GPS unit itself.