Typical partsĪre flow valve, relay, condenser, ram air sensor, heat exchanger, cooling The units and systems supplying cooled air to the cockpit or cabin.ĭoes not include the temperature control and indicating system. Typical parts are fuel pump, filter, plumbing, circuitry, Includes the heat source (heater), controlling aspects, and temperature The units and systems supplying heated air to the cockpit or cabin. Typical parts are pressure switch, transducer, etc. The units and systems which measure differential pressure and transmitĪ signal. The defective part should be identified by the part name and part numberįor reports of the cabin pressurization system, pressure indicators,įor reports of outflow/dump valves and associated parts such as Typical parts areĪmplifier, switch, electrical connector, etc.įor the reports pertaining to the controller units only and not for the Typical parts are bearing, bushing, motor, etc.įor reports of miscellaneous system components or parts other than theĬontroller, indicator, sensor, regulator, or outflow valves.
Which distributes air within the confine for comfort or equipment cooling. Typical parts are equipment rack cooling systems, ozone converters, scoops,ĭucting, inlets, check valves, wiring, etc.įor reports pertaining to the fan/blower including associated motor That are a part of the temperature control, pressurization, or the distributionįan. The system used to induct and distribute air. Indicating systems related to the compressors, wiring, etc. Specific defective part by name and part number. Related entries should include the component manufacturer's make, model, and the Reported problems with the compressor unit and not the associated system. The system and its controls supplying compressed air to the cabin. Ventilate areas of the fuselage within the pressure vessel. Heating, cooling, moisture controlling, filtering, and treating the air used to The general instructions are not applicable to any particularįor miscellaneous parts that cannot be associated with specific airĬonditioning, pressurization, or distribution codes.Įtc., with no reference to the specific using system on the incoming report.Īlso, for those units and components furnishing a means of pressurizing, The general instructions are not applicable to any particular system.įor reports indicating a problem relating to aviation lubricating oil.įor reports which indicate a problem with any type of hydraulic fluid.įor reports indicating a problem with any type of engine coolant used Text = the "closed and locked" decal is missing from the main passenger entrance door).įor reports indicating a problem relating to any type of aviation fuel. (Example: Item = placard location = entrance door part condition = missing. Such information should be extracted from the text and entered in the proper data fields. The location of the item is essential for a meaningful report. The report should include the system or component involved. For reports on all placards, decals, and markings installed by the manufacturer including those required by government regulations. 36 Levers and Bellcranks.37 Pressure Bulkhead Fairleads. 34 LH and RH Rudder Pedal Assemblies.35 LH and RH Pedal Adjustment Assemblies.35 LH and RH Forward Quadrant Assemblies. 32 Rudder Trim.33 INTERFACE TO OTHER SYSTEMS.33 Navigation System. 31 Standby Trim/Main Lockout Circuit Status.31 25 OPERATION.25 Power Supplies.25 System Power-Up. 24 Main Aileron Trim Switch 2CC.24 Standby Aileron Trim Switch 12CC.25 Aileron Trim Reset Switch/Light 17CC. 23 Aileron Trim Actuator 4CC (refer to Fig. FOR TRAINING PURPOSES ONLY TM-Flight Controls 19 Aileron Controls from Wing Root to Aileron. 18 Aileron Controls from Transition Units to Wing Roots. 18 Regulation of Cable Tension in Fuselage Control Run. 18 Flight Compartment to Upper Center Fuselage Control Run. 18 LH and RH Aileron Position Transmitters 5CX and 4CX. ATA CHAPTER 27 FLIGHT CONTROLS 27-00 GENERAL
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