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Provides a list of all figures included in the preceding pages section of the manual.
General information about the manual's purpose and scope for the Viper SD-4 RTC.
Defines the scope of servicing and maintenance information provided for Viper SD-4 RTC aircraft.
Provides general information on acceptable methods and techniques for aircraft maintenance.
Lists relevant publications and documents for the Viper SD-4 RTC aircraft maintenance.
Lists contact information and addresses for TOMARK and other relevant service providers.
Explains the manual's organization, structure, and adherence to GAMA Specification No. 2.
Defines the meanings of DANGER, WARNING, CAUTION, NOTICE, and NOTE in the manual.
Provides a glossary of terms and abbreviations used throughout the Airplane Maintenance Manual.
Describes text elements and headline conventions used within the manual.
Outlines essential safety measures and precautions for maintenance personnel.
Provides a description of the Viper SD-4 RTC aircraft's key characteristics.
Sets out mandatory replacement and inspection intervals for aircraft airworthiness.
Specifies airframe and engine mount limitations and major inspection intervals.
Details components addressed in the major airframe inspection program.
Addresses approved software versions for the Viper SD-4 RTC.
Introduction to charts, tables, and checklists for time limits and maintenance.
Outlines the aircraft's scheduled inspection and maintenance program.
Details time between overhaul and replacement intervals for aircraft components.
Provides a detailed plan for scheduled inspections at various intervals.
Procedure for inspecting drain holes for obstructions.
Details the purpose and procedure for conducting a maintenance check flight.
Describes flight tests for checking climb, cruise, and full throttle level flight performance.
Explains the procedure for checking various aircraft systems.
Details checks for elevator, aileron, rudder, and flap control operations.
Procedures for checking magnetic compass and airspeed/altitude indicators.
Checks for COM, XPDR, GPS, and other avionics systems.
Procedures for checking EMS display, RPM indication, and other engine parameters.
Procedures for unscheduled maintenance after specific events.
Procedure for checking aircraft geometry after major events.
Provides the overall length, height, and wingspan of the aircraft.
Details wing area, chord, aspect ratio, profile, and angles.
Specifies the area, span, and chord of the ailerons.
Details the type, area, span, and depth of the flaps.
Provides dimensions and aerodynamic data for the horizontal stabilizer.
Specifies the area, span, and chord of the elevator.
Details the area and height of the vertical stabilizer.
Provides area and sweep angles for the rudder.
States the fuel tank capacity.
Details track width, wheel base, and wheel sizes.
Provides number of blades and diameter for the propeller.
Procedure for safely lifting the aircraft by its main wheel.
Procedure for safely lifting the aircraft by its nose wheel.
Instructions for placing a jack under the fuselage side.
Instructions for placing a jack under the fuselage front.
Details procedures for aircraft weighing and center of gravity calculation.
Instructions for achieving longitudinal and lateral leveling of the aircraft.
Critical safety precautions for refueling and defueling the aircraft.
Instructions for changing engine oil, referencing Rotax manual.
Procedure for replacing the aircraft's coolant system fluid.
Instructions for bleeding the aircraft's brake fluid system.
Procedure for replenishing brake fluid in the aircraft's braking system.
Guidelines for bolt torque and marking procedures.
A survey of rivet types and their usage in the aircraft structure.
Details on the types of hoses and tubes used and their connection methods.
Procedures for removal and installation of Bowden cables.
Describes the cockpit ventilation system and air nozzle locations.
Details the components of the aircraft's heating system.
Information on the aircraft's DC generator and battery.
Details on failure signaling and electrical current protection.
Procedures for removal and installation of the aircraft seats.
Description of the 3-point static harness restraint system.
Information on how cockpit paneling is attached.
Description of the baggage area location and features.
Table detailing nominal deflections for control surfaces.
Procedure for removing and installing the aircraft control stick.
Details on control rod types, removal, and installation.
Explains the use of bell cranks in transferring control inputs.
Description of the aileron control system and its components.
Procedure for removing and installing the aircraft ailerons.
Details the electric servo operation of the aileron trim tab.
Description of the rudder control system and pedal adjustments.
Explains the elevator control system via push-pull rods and bellcranks.
Procedure for removing and installing the aircraft elevator.
Describes the electric actuator and controller for the flap system.
Procedure for removing and installing the aircraft flaps.
Lists the components that comprise the aircraft's fuel system.
Details the location and features of the integrated fuel tanks.
Explains the routing of fuel from tanks to the engine.
Describes how fuel quantity, flow, and pressure are indicated.
Describes the layout of the instrument panel and control panels.
Procedures for removing and installing instrument panels.
Instructions for removal and installation of typical instruments.
Procedures for removal and installation of switches and circuit breakers.
Procedure for removal and installation of the main landing gear leg.
Details on nose gear strut fairing, wheel fairing, and wheel fork.
Procedure for replacing the shock cord rings in the nose gear strut.
Information on wheel fairings, brakes, and brake cylinder.
Procedures for removal and installation of main wheel fairings and wheels.
Procedures for adjusting brake linings and replacing brake discs.
Instructions for removal, installation, and disassembly of the nose wheel.
Procedure for removal and installation of position and strobe lights.
Procedure for removing and installing the aircraft landing light.
Overview of access points, covers, and fairings on the aircraft.
Procedure for removing and installing aircraft access hatches.
General procedures for determining and adjusting control surface weight and balance.
Guidelines for classifying and repairing damage to metal aircraft skins.
Method for removing small dents from the aircraft skin.
Procedure for stopping the propagation of small cracks in the skin.
Instructions for repairing aircraft skin damage using patches.
Procedures for repairing composite parts, including damage classification.
Repair methods for small damage on external composite parts.
Repair procedures for medium damage on composite parts.
Policy for major damage to composite parts: part exchange.
Safety rules and procedures for paint repair and surface treatment.
Describes the construction of the aircraft fuselage.
Details on the canopy's opening, closing, and locking mechanisms.
Information on the attachment of the fuselage tail fairing.
Information on the attachment of stabilizer tip fairings.
Description of the horizontal stabilizer construction and components.
Description of the elevator's all-metal design and features.
Description of the vertical stabilizer's all-metal construction.
Description of the rudder's all-metal design and composite horn.
Description of the wing's all-metal design and components.
Details on the center wing structure and wing root fairing attachment.
Procedures for removal and installation of wing tip fairings.
Descriptions of the flaps and ailerons construction.
Procedure for measuring and adjusting the propeller blade angle.
Information on attaching the propeller spinner.
Procedures for removing and installing top and bottom engine cowlings.
Description of the cylinder air cooling and air intake system.
Details on the engine inlet section and carburetor preheating.
Description of the throttle lever's function and location.
Description of the choke control knob for cold engine starting.
Description of the liquid-cooled cylinder heads and air-cooled cylinders.
Explains the function and location of the coolant thermostat.
How coolant temperature is indicated on the EMS screen.
Procedure for removing and installing the aircraft oil tank.
Description of oil radiator, filter, ventilation, sensor, and thermostat.
Information on the starter circuit control.
Details on the AEPS, its components, and installation.
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General