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Type Rating Training Cessna 172R

ATA01 Introduction ATA05 Time limit ATA06 Dimension ATA07 Lifting ATA08 Leveling&Weighing ATA09 Towing&Taxiing ATA10 Parking&Mooring ATA11 Placard&Marking ATA12 Servicing ATA20 Standard Practices  ATA23  Comm ATA24 Electrical Power ATA25 Equip&Furnishin ATA27 Flight Control ATA28 Fuel  System   ATA31 Instrument ATA32 L/G ATA33 Light ATA34 Navigation ATA37 Vacuum  ATA51 SP-Structure ATA52 Cabin Door ATA53 Fuselage ATA54 Nacelles  ATA55 Stabelizer ATA56 Window ATA57 Wing ATA60 SP- Propeller ATA61  Propeller  ATA70 SP-Engine ATA71 Power Plant ATA73 Engine Fuel  ATA74 Ignition System ATA76 Engine Control ATA77 Engine Indicating System ATA78 Exhaust System ATA79 Engine Oil System ATA80 Starting System                                    

Engine Fuel System

720000 Fuel line (Stainless steel tube assembly)  and support clamp inspection and installation.  Refer to Lycoming Service Bulletin Number 342E or later version.  V 05-12-23 120 722001 Engine - Inspect for evidence of oil and fuel  leaks. Wash engine and check for security  of accessories.  A 05-12-01 120 722002 Crankcase, Oil Sump, and Accessory Section  - Inspect for cracks and evidence of oil leakage. Check bolts and nuts for looseness  and retorque as necessary. Check crankcase breather lines for obstructions,  security, and general condition. B 05-12-02 120 722003 Hoses, Metal Lines, and Fittings - Inspect  for signs of oil and fuel leaks. Check for abrasions, chafing, security, proper routing  and support and for evidence of deterioration 723001 Engine Cylinders, Rocker Box Covers, and  Pushrod Housings - Check for fin damage,  cracks, oil leakage, security of attachment,  and general condition.  B 05-12-02 120 723002 Engine Metal Lines, Hoses, Clamps, and  Fit

Air Supply

212001 Ventilation System - Inspect clamps,  hoses, and valves for condition and security. 212002 Remote Avionics Cooling Fan -  Op Check 214001 Cold and Hot Air Hoses - Check condition,  routing, and security.  05-12-02 Z120

Practical training

Practical training is a structured training event which consolidates the knowledge gained during the theoretical phase of type training and as such, may be performed after or integrated within the theory training. However, it must not be performed before theoretical training. Practical training should: Address the different parts of the aircraft which are representative of the structure, the systems/components installed and the cabin. Include the use of technical manuals, maintenance procedures and the operational interfaces with the aircraft (e.g. FMC, electronic flight bag, etc). Include common maintenance and ground handling activities. Cover both type specific and generic safety elements of the aircraft’s maintenance. Develop the student’s competence in performing safe maintenance, prior to the practical assessment. Purpose of Practical training is not to include all the maintenance tasks associated with a particular type, but a representative sample of them that will a

Fire extinguisher

A portable, hand operated fire extinguisher is mounted on the floor between the pilot and copilot seats for use in the event of a fire. The extinguishing agent is Halon 1211 and may be used on solid combustible, electrical or liquid fires. Servicing of the extinguisher can be handled by most fire equipment dealers. The fire extinguisher is mounted within a quick release, clamp type bracket assembly. 262001 Portable Hand Fire Extinguisher - Inspect  for proper operating pressure, condition,              security of installation, and servicing date.  B 05-12-01 230 262002 Cockpit Mounted Halon Type Fire Extinguisher  - Weigh bottle. Bottle must be                         reserviced  by qualified individual if more than  2 ounces is lost. 262003 Cockpit Mounted Halon Type Fire Extinguishers  - Perform hydrostatic test. The                      hydrostatic  test shall be at twelve-year intervals  based on initial servicing or date of               last  hydrostatic test.

Auto flight

A single axis autopilot with heading hold is on airplanes with IFR. Heading hold is used with directional gyro input and can have VOR, GPS or Localizer input as required. Dual-axis autopilot is available. The dual-axis system gives both vertical speed and altitude hold selection. The autopilot on this aircraft uses a pitch servo, a pitch trim servo and a roll servo. GFC-700 is a dual-axis autopilot with heading, altitude, and vertical speed hold 221003 Autopilot Servo Actuators. Inspect for evidence  of corrosion and or buildup of dirt or other particulate matter which may interfere  with servo operation.  O 05-12-16 Z610

Level

Level 1 A brief overview of the airframe, systems and powerplants as outlined in the Systems Description Section of the Aircraft Maintenance Manual / Instructions for Continued Airworthiness. Course objectives: Upon completion of the course, the student will be able to: a) provide a simple description of the whole subject, using common words and examples, using typical terms and identify safety precautions related to the airframe, its systems and powerplant; b) identify aircraft manuals, maintenance practices important to the airframe, its systems and powerplant; c) define the general layout of the aircraft's major systems; d) define the general layout and characteristics of the powerplant; e) identify special tooling and test equipment used with the aircraft Level 2 Basic system overview of controls, indicators, principal components including their location and purpose, servicing and minor troubleshooting. General knowledge of the theoretical and practical aspect

Standard Practices - Propeller