AIR TRANSPORT INTERNATIONAL MAINTENANCE INFORMATION LETTER MIL 23-01 R2 Date: April 12, 2012 Revised May20, 2015 Revised July 24, 2015 To: All Maintenance and Inspection Personnel From: Bryan A. Sherby, Manager of Maintenance Training Re: B767 Flyht, AFIRS (Automated Flight Information Reporting System) Familiarization Training A. Air Transport International is actively modifying the B767 aircraft that it operates with the Flyht AFIRS system, certified under STC ST02523NY. Operating and Testing of the AFIRS Global Messaging System must be performed by personnel familiar with the aircraft and systems. B. Following is a comprehensive outline of the AFIRS system. This information is covered in more detail in the ATI 767 Supplemental Maintenance Manual, Section 23.01, and includes the following detailed information on this system: 1. Description. 2. Operation. 3. Troubleshooting. 4. Maintenance practices. 5. Removal/Installation. 6. Operational Tests. 7. Functional Test. C. The ATI 767 Sup. MM section also provides a general description with references to the applicable CMM/OHM supplements concerning AFIRS Global Voice and Messaging systems and also provides reference to the AFIRS Antenna detailed inspection job card. For the purpose of this familiarization training, it is not necessary to read these additional references; however an awareness of this material for future requirement is considered essential. FLYHT AFIRS SYSTEM (STC ST02523NY) (Ref. ATI 767 Supplemental Maintenance Manual, Section 23.01) NOTE: The AFIRS System is a non-essential, non-critical avionics system. The system is not required for operation of the aircraft. NOTE: This section contains excerpts from Flyht AFIRS System MM Supplement. For the complete MM Supplement, refer to the ATI issued Boeing 767 Component Maintenance Manual (CMM/OHM) (D634T101) disc. 1 AIR TRANSPORT INTERNATIONAL MAINTENANCE INFORMATION LETTER MIL 23-01 R2 1. Description A. AFIRS Unit (1) The AFIRS (Automated Flight Information Reporting System) is the avionics unit that collects data automatically on board an aircraft. Data summary files are transmitted through an onboard satellite modem for immediate analysis and generation of various reports. The complete raw data is stored on the built-in, removable, Compact Flash memory card, herein referred to as the flash (memory) card. Thus, the AFIRS unit is a Quick Access Recorder (QAR). The raw data is periodically uploaded to the UpTime Flight Data Center. (2) The front panel has an access door that allows access to the internal flash memory card and two LED lights. An external maintenance port is also located on the front panel. (3) The AFIRS rear connector is an ARINC 404B connector plug and provides the following connectivity: (a) 28 VDC Power and ground connection (b) AFIRS Indicator Panel Interface (c) ARINC 573/717 and ARINC 429 inputs (d) RS-422 interfaces (e) Discrete sensor inputs (f) Discrete outputs (g) Iridium antenna connection (h) GPS antenna connection (i) AFIRS Keypad interface (j) 2 wire phone connection 2 AIR TRANSPORT INTERNATIONAL MAINTENANCE INFORMATION LETTER MIL 23-01 R2 (4) Each AFIRS unit is identified by a data placard located on the front panel of the AFIRS unit. The data placard contains the part number of the unit as well as a unique serial number. The configuration, modification status and firmware version are also on the placard. The configuration, in general, refers to a unique customer and/or aircraft set-up for the unit. The modification status, in general, refers to hardware upgrades to the unit. B. AFIRS Antenna - The AFIRS Antenna is a Sensor Systems S67-1575-163 low profile dual-band active antenna which provides GPS input to the AFIRS unit and also provides continues Tx/Rx Iridium band coverage. The antenna is installed between STA 478 and STA 522 on the top of the fuselage crown between STR 1L and STR 1R. C. AFIRS Indicator Panel - The AFIRS Indicator Panel is located in the flight compartment P8 center pedestal (preferred location) or in the P5 overhead panel (alternate location). D. Aircraft Identification Enclosure Assembly - The Aircraft Identification Enclosure Assembly (ACID) is installed on the upper level of the AFIRS mounting tray located on shelf E2-2 of the avionics rack in the aircraft forward equipment center. The Aircraft Identification Enclosure Assembly provides a unique aircraft identified to the AFIRS unit. It is pre-programmed and is not operator maintainable. Complete the Certificate of Maintenance Training Form (M-011) and return the Training Certificate to ILN MX Training Department. (Scan/email or mail) 3 AIR TRANSPORT INTERNATIONAL MAINTENANCE INFORMATION LETTER MIL 23-01 R2 CERTIFICATE OF MAINTENANCE TRAINING (FORM M-011) AIR TRANSPORT INTERNATIONAL NAME OF TRAINEE EMP. NR. JOB TITLE DATE(S): FROM TO AIRCRAFT/ENGINE TYPE HOURS: B767 0.5 OJT LOCATION CLASSROOM Trainee named above has received instruction as described below: MIL 23-01 R2 B767 FLYHT, AFIRS (Automated Flight Information Reporting System) Familiarization Training MAINTENANCE MANUAL REFERENCE(s): This Study Guide INSTRUCTOR'S COMMENTS: NO FURTHER TRAINING REQUIRED INSTRUCTOR NAME: EMP. NR. (PRINT) SIGNATURES: (INSTRUCTOR) (TRAINEE) (After this form is signed, provide a copy to ILN MX Training) 4