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Definitions for Warnings (risk of injury/death), Cautions (risk of damage), and Notes (additional info).
Precautions to prevent injury and damage during maintenance procedures on XA41/XA42 aircraft.
Details engine manufacturer, type, rated power, and propeller type.
Details components that must be replaced within specified periods or according to manufacturer data.
Lists items requiring replacement during regular maintenance periods, including fuselage connection bolt.
Specifies the service life for the composite structure as 6000 flight hours.
All scheduled maintenance checks have specified time limits that must be adhered to.
Lists overhaul time limits for various aircraft components like engine, magnetos, propeller, etc.
Lists replacement times for items like battery, bolts, brake assemblies, ELT batteries, etc.
Outlines mandatory scheduled maintenance checks to be performed after the first 25 hours and at 50, 100, and 1000-hour intervals.
Procedures defined in the 50 Hour inspection must be performed after the first 25 hours of operation.
Detailed inspection checklist for canopy, rear seat, rudder pedals, rudder cables, torque tube, control stick, and fuel selector switch.
Includes all 50-hour inspection steps plus additional checks for electrical system, fuel selector switch, and structure.
Requires disassembly of the aircraft and a full inspection of all components.
Procedures for checks following hard landing, engine/propeller strike, engine fire, lightning strike, bird strike, and hail damage.
Procedures for lifting the aircraft, including removing cowling and attaching straps to engine mount.
Necessary to shore aircraft during installation/removal of main or tail landing gear.
Procedure for supporting the front of the aircraft, requiring a support area of 100 x 500 mm.
Procedure for supporting the tail of the aircraft, requiring a tail support of 500x300x300 mm.
Step-by-step procedure to level the aircraft using wheel chocks, tailwheel jack, and water level.
Refer to the form in Appendix 2 for weighing and calculating the center of gravity.
Procedure to measure the aircraft empty mass by weighing at main and tailwheel scales.
Explains how to calculate the center of gravity (XS) using moment arms and mass values.
Instructions for towing the aircraft, emphasizing ignition switch OFF and avoiding spinner damage.
Guidance for taxiing, including slow speeds, brake checks, turning, stopping, and propeller clearance.
Procedures for parking the aircraft, including wheel chocks and control stick safety.
Steps for parking the aircraft, aligning into wind, using wheel chocks, and closing canopy.
Procedure for aircraft not operated for 30 days or more, including corrosion prevention and battery disconnection.
Procedure for tiedown if aircraft must be stored outdoors for a long time, using specific tie-down points.
Recommends a 50-hour inspection and engine service procedure if parked for over 30 days.
Procedures for adding fuel, engine oil, and brake fluid; tire inflation info is also included.
Instructions for refueling, emphasizing engine OFF, electrical systems de-energized, and no spilled fuel.
Procedure for defueling the aircraft, ensuring electrical grounding and using appropriate containers.
Procedure to examine oil quantity and add oil if necessary, referring to chapter 12-10-08 for quantity/specs.
Procedure for replacing engine oil, including removing cowling, draining oil, and examining oil pressure screen.
Method for bleeding and filling aircraft brakes from bottom up, including master cylinder details.
Procedures for cleaning external and internal surfaces, and engine cleaning.
Procedure for cleaning the engine and compartment to prevent fire and ensure proper operation.
Instructions on removing snow and ice, advising against sharp objects or de-icing fluids.
Provides standard maximum torque values for DIN/LN bolts and standard installation torque values for AN/MS bolts.
Lists special torque values for specific aircraft items like engine mount, spar bolts, and brake caliper bolts.
Procedure using coin tapping inspection to examine airframe composite structure for delamination.
Procedures for disassembling the aircraft for transportation or storage, and for assembly.
Step-by-step instructions for assembling the aircraft, including major components and systems.
Steps for disassembling the aircraft, including removing wings and stabilizers for transportation or storage.
Details the BC410-H or BC462-H gear-driven DC generator, its rated outputs, and installation.
Describes the 12-Volt DC system, power supply from alternator/battery, and switch/breaker locations.
Information related to emergency equipment, specifically the Emergency Locator Transmitter (ELT).
Describes the KANNAD 406 AF-Compact ELT and its remote control RC200.
Procedure for removing and installing control sticks, including checks for play.
Details the torque tube assembly, removal, and installation, including checks for free movement and play.
Procedure for removing, installing, measuring, and adjusting control rods.
Describes aileron construction, attachment, balancing mass, spades, and travel stops.
Describes rudder operation, attachment, balancing mass, and control system.
Describes fuel selector valve attachment and control rod connection to the rear cockpit switch.
Procedure for calibrating fuel quantity sensors for main and wing tanks using MVP-50 system.
Details Beringer HE2 and Grove brake systems, including inspection and removal/disassembly.
Describes brake actuation via rudder pedals, master brake cylinders, and fluid reservoir.
Procedures for weighing and calculating control surface moments.
Steps to weigh control surfaces and calculate moments, including mass and arm data.
Standard practices for repairing composite structures, emphasizing approved materials and designs.
Procedure for damage inspection after incidents, including visual checks and tap tests.
Guidelines for composite repairs, including resin/hardener mixture ratios and application.
Procedure for removing and installing the wing, including disconnecting lines, wires, and rods.
Describes the Textron Lycoming AEIO-580-B1A engine, its features, and attachment.
Describes throttle operation via lever and Bowden cable, adjustment, and removal procedures.
General