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The system provides a digital data (data link) mode that uses a discrete VHF frequency of 131.55. ACARS will automatically record and transmit aircraft OUT, OFF, ON, and IN event times in GMT time. In addition, fuel load information and other necessary data can be manually entered and transmitted.
A voice mode can be selected for conducting normal VHF voice communications. Desired frequencies for VHF voice communications are selected on the VHF-2 (VHF-3 on some aircraft) COMM panel.
The ACARS equipment installed in the aircraft includes a control unit (CU) and management unit (MU).  A clock is also included in the ACARS to provide time in GMT.
The CU is located on the pedestal and provides controls and alpha-numeric display for selecting and displaying data before entering the data into the MU. Controls are also provided on the CU to enter data into the MU and to send the data. Status annunciator lights are provided on the CU to indicate failure of the CU or MU and to indicate temporary delays of ACARS operation.
The MU and GMT clock are located in the avionics compartment.  ACARS is interfaced with the SELCAL decoder, engine oil pressure switches, forward and aft passenger doors and cargo doors proximity switches, parking brake switch, FDAU, and VHF-2 (VHF-3 some aircraft) communication system. Data that is manually or automatically entered into the MU for processing and memory storage is distributed automatically, or when manually called up, as applicable. The system provides for automatic updating of GMT time.

COMMUNICATIONS – CONTROLS AND INDICATORS
ACARS

Continental
Rev. 12/01/00 #29 Flight Manual

COMMUNICATIONS – CONTROLS AND INDICATORS
ACARS

COMMUNICATIONS – CONTROLS AND INDICATORS
ACARS

Continental
Rev. 12/01/00 #29 Flight Manual

COMMUNICATIONS – CONTROLS AND INDICATORS
ACARS

COMMUNICATIONS – CONTROLS AND INDICATORS
ACARS

MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
PITOT / STATIC SYSTEMS

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
PITOT / STATIC SYSTEMS

MD-80
Continental
Rev. 12/01/00 #29 Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
PITOT / STATIC SYSTEMS

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
PITOT / STATIC SYSTEMS

MD-80 Rev. 12/01/00  #29 Continental Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
COMMUNICATIONS

COMMUNICATIONS – CONTROLS & INDICATORS
MD-80 Rev. 12/01/00  #29 Continental Flight Manual

COMMUNICATIONS – CONTROLS & INDICATORS COMMUNICATIONS – CONTROLS & INDICATORS

MD-80 Rev. 12/01/00  #29 Continental Flight Manual

COMMUNICATIONS – CONTROLS & INDICATORS

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
NAVIGATION SYSTEMS

MD-80 Rev. 12/01/00  #29 Continental Flight Manual

INSTRUMENTATION AND NAVIGATION – CONTROLS AND INDICATIONS
NAVIGATION SYSTEMS

INSTRUMENTATION AND NAVIGATION – CONTROLS AND INDICATIONS
NAVIGATION SYSTEMS

MD-80 Rev. 12/01/00  #29 Continental Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
NAVIGATION SYSTEMS

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
NAVIGATION SYSTEMS

MD-80 Rev. 12/01/00  #29 Continental Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
NAVIGATION SYSTEMS

MD-80 Sec. 16 Page 55
Flight Manual Continental Rev. 12/01/00  #29

 

 

 

 

 

 

 

 

MD801625
INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS

NAVIGATION SYSTEMS
MD-80 Rev. 12/01/00  #29 Continental Flight Manual

INSTRUMENTATION AND NAVIGATION - CONTROLS AND INDICATORS
NAVIGATION SYSTEMS

MD-80 Sec. 16 Page 57
Flight Manual Continental Rev. 12/01/00  #29

 

Function Selector
OFF - Removes power from transponder.
STBY -Supplies power to transponder but does not allow tran-sponder to reply to interrogation signals.
NOTE
on the ground, tran-sponder is in standby operation when func- tion selector is in either STBY or ON. ground control relays keep transponder in standby operation  until liftoff, when func- tion selector is ON. At liftoff, function selector in ON, ground control relays automatically switch transponder from standby operation to on operation. At touchdown, function selector is ON, ground control relays automatically switch transponder to standby operation.
　
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