CMC Electronics CMA-9000 Flight Management System Installation & Flight Line Manual (2007)

Description

CMC Electronics CMA-9000 Flight Management System Installation & Flight Line Manual

This is the complete original CMA-9000 Installation/Flight Line Manual published by CMC Electronics Inc. for the CMA-9000 Flight Management System, hardware variation 100-601951-VAR with software 169-614876-010. If you install, configure, or maintain a CMA-9000 FMS on the flight line, this CMA-9000 Flight Management System manual is the factory reference for the job.

File Details

• Manual type: Installation/Flight Line Manual
• Brand / Model: CMC Electronics CMA-9000 Flight Management System
• Hardware: 100-601951-VAR, Software: 169-614876-010
• Publication No. 9000-GEN-0840, Item No. 929-600026-000
• Reference 34-61-14, dated May 10, 2007 (Original, Revision 0)
• Language: English
• Page count: 395 pages
• File format: PDF, instant digital download

Chapters Covered

• Section I – Description and Operation: purpose, function, reliability/MTBF, external interface capabilities, primary navigation modes, annunciators and keys, related publications, equipment identification
• Equipment Specifications: applicable ARINC/FAA/RTCA/SAE/JAA/military documents
• Digital Equipment interfaces: ACMS, Air Data Computer (ARINC 429/575), AHRS, AFCS, DME receivers, EFIS interfaces (GAMA, IFDS/AHCAS, ARINC 702), Fuel Computer, GPS Sensor, Flight Recorder, VOR/ILS receiver, VOR receiver, X-FMS cross-talk, ELT, ATC transponders, VHF Comm, ADF, Audio Management Unit, APIRS, Digital Map System, Data Concentrator, Radio Altimeter, LN-100GT and SIGMA50H embedded GPS/INS, Weather Radar, Doppler Velocity Sensor, Personnel Locator System, TACAN, Data Loader units, Inertial Reference System
• Section II – Installation: equipment location, GPS receiver/antenna selection, active antenna installations, interwiring and outline drawing, harness voltage checkout, EGI installation, Doppler installation, annunciator installation
• Section III – Post-Installation Test: Built-In Test, front panel brightness, configuration selection, navigation database loading, power on, annunciator test, heading verification, true airspeed verification, GPS sensor unit, DME status, VOR/DME/TCN status, radio test, discrete output test, EFIS interface test, EMC test, IRS-to-FMS-to-IRS ground check
• Section IV – Flight Line Test/Troubleshooting: alert messages, troubleshooting philosophy, fault log with system alert, maintenance alert, maintenance advisory, and status advisory messages
• Section V – Maintenance Practices, Section VI – Servicing, Section VII – Removal/Installation procedures
• Section VIII – Cleaning/Painting, Section IX – Approved Repairs
• Section X – Configuration Selection: four configuration capabilities, configuration diskette and manual configuration procedures
• Section XI – Data Loader Unit (DLU): ARINC 615 DLU and RS-422 DLU database/configuration loading and saving
• Appendix A: Ground Functional Test Procedures; Appendix B: Flight Functional Test Procedures & Report; Appendix C: Procedures for Obtaining Civil Authorities Approval for follow-on FMS/GPS installations

Taken together, this CMA-9000 Flight Management System manual walks a technician from initial equipment location and wiring through post-installation testing, flight line fault diagnosis, and full configuration selection, with dedicated appendices for ground and flight functional test sign-off.

Physical, Power & Environmental Specifications

The manual documents the CMA-9000 unit as 147.57 mm (5.81 in) deep, 146.05 mm (5.75 in) wide, and 171.45 mm (6.75 in) high, weighing 3.86 kg (8.5 lb) maximum. Power dissipation is specified at +28 Vdc, 45.0W typical at ambient rising to 75.0W during cold-temperature startup, with integral lighting drawing up to 12.0W at 5.0 Vdc. Environmental qualification is documented to RTCA DO-160E, including temperature (Category A4B4), altitude, decompression, vibration, humidity, shock, EMI, lightning, and electrostatic discharge categories – all reproduced from the original CMC Electronics documentation.

Navigation Sensor & Interface Coverage

The CMA-9000 Installation/Flight Line Manual details external navigation sensor interfacing including GPS, EGI (Embedded GPS/INS), DME, VOR, ADF, ADC, DVS, AHRS, APIRS, TACAN, and IRS, along with exchange of information with XPDR, COM/V-UHF radios, EHSI, digital map, personnel locator, ACMS, AMU, EFIS, flight data recorder, weather radar, and ELT equipment. Civil and military navigation mode configuration options, navigation mode priority sequencing, and Receiver Autonomous Integrity Monitoring (RAIM) behavior for GPS are all covered in Section I.

Why Technicians Rely On This CMA-9000 Manual

With this CMA-9000 Flight Management System manual in hand, an avionics technician can correctly select and wire the FMS unit, GPS antenna, and related sensors; run the full post-installation Built-In Test and system verification sequence; interpret system alert, maintenance alert, maintenance advisory, and status advisory fault codes on the flight line; and step through the four-configuration selection procedure using either a configuration diskette or manual entry. Following CMC Electronics’ original installation and test procedures helps protect FMS accuracy, RAIM-based integrity monitoring, and certification compliance rather than relying on guesswork. This CMA-9000 Installation/Flight Line Manual is delivered as an instant PDF download – no shipping wait – and can be read, searched, and printed from a laptop, tablet, or phone in the hangar or on the flight line.