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AirComm Corporation Airbus EC120 Cabin Air Conditioner Instructions for Continued Airworthiness User Manual
AirComm Corporation Airbus EC120 Cabin Air Conditioner Instructions for Continued Airworthiness User Manual
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AIR CONDITIONER SERVICE MANUAL EC120-200M-1 Revision 5 Page A-1 APPENDIX A WEIGHT AND BALANCE INFORMATION Weight breakdown – Airbus EC120B Air Conditioner System: Ref. Dwg. EC120-200 Item Wt. (lbs) X-Arm (in) X-M (in-lb.) Y-Arm (in) Y-M (in-lb) Total EC120B with Single Aft Evaporator 62.98 142.7 8990 -2.5 -162 Total EC120B with Single Forward & Aft Evaporator 75.48 128.4 9694 -2.1 -162
AIR CONDITIONER SERVICE MANUAL EC120-200M-1 Revision 5 Page B-1 APPENDIX B Modification Instructions for the Rotor Brake Pad Support Plate: NOTE During installation of the Air Conditioner kit, or any time the Rotor Brake Pads are replaced it will be necessary to modify the Rotor Brake Assembly. This section provides the information necessary to insure the proper clearance between the Compressor Drive Pulley and the Rotor Brake Assembly. NOTE Consult the EC120 B Maintenance Manual for Removal, Inspection, and Replacement / Installation instructions for the Rotor Brake Pads. Reference views for modification to Rotor Brake Assembly. 1. Using a “Rat Tail” file or Equivalent, remove .12 inch from the Rotor Brake Disk Caliper as shown in Section J-J or View H-H below.
AIR CONDITIONER SERVICE MANUAL EC120-200M-1 Revision 5 Page B-2 2. Using a “Rotary” file or Equivalent, Remove .06 inch X 1.12 inch from the top of the Rotor Brake Pad as shown in View G-G Below.