Do you have a question about the HKS 700E and is the answer not in the manual?
Records changes made to the manual over time, including revision numbers, dates, affected pages, and descriptions of changes.
Details the specific model designation of the HKS700E engine, including manufacturer and piston displacement.
Provides a general overview of the engine's features, such as cooling type, cylinder arrangement, ignition, starter, and lubrication system.
Illustrates the engine from multiple angles to help users identify its components and layout.
Specifies the bore, stroke, displacement, compression ratio, rotation direction, and weight of the engine.
Lists the engine's key equipment, including ignition unit, timing, spark plugs, alternator, carburetor, air filter, fuel pump, and starter.
Outlines the engine's performance characteristics, detailing take-off power and maximum continuous power ratings.
Defines the maximum permissible and continuous revolutions per minute (RPM) and recommended idle RPM ranges for the engine.
Provides figures for fuel consumption at different operating RPMs, specified in liters per hour (L/H) and gallons per hour (GPH).
Details approved fuel types, fuel pressure requirements, and recommended oil types, viscosity, volume, and temperature ranges.
Describes the engine's cooling method, specifying free air-cooling and requirements for ducted installations.
States the maximum permissible cylinder head temperature and provides a caution regarding CHT probe usage.
Explains the engine's propeller reduction gear ratios and its shock absorption mechanism.
Specifies the maximum permissible propeller mass moment of inertia for different reduction gear ratios.
Lists maximum permissible exhaust gas temperatures based on the location of the EGT sending unit.
Outlines essential pre-flight checks and procedures to be performed before starting the engine.
Details the step-by-step procedure for starting the engine, including checks and cautions.
Instructs on proper engine warm-up procedures, including oil temperature checks and Mag checks.
Guides the pilot through the take-off and initial climb phases, emphasizing critical parameters and safety.
Provides the correct procedure for shutting down the engine, including necessary cool-down steps.
Explains procedures for engine shutdown and, if applicable, restarting the engine during flight.
Lists essential checks and inspections to be performed on the engine daily before operation.
Details scheduled maintenance inspections based on operating hours (25, 50, 100, 200 hours).
Specifies the tasks required for the initial 25-hour inspection and subsequent 50-hour inspections.
Outlines the maintenance tasks for the 100-hour inspection, including those from the 50-hour check and a compression check.
Details the procedures for the 200-hour inspection, including items from the 100-hour check and filter replacements.
Provides instructions for protecting the engine against corrosion during extended periods of inactivity.
Covers operational considerations and maintenance for engine use during winter conditions.
Specific guidance on checking and maintaining the engine's electrical system for winter operation.
Describes the recommended procedures for starting the engine in cold weather conditions.
Explains the causes of fuel system icing and provides remedies, including carburetor icing issues.
Step-by-step instructions for performing an engine oil change, including oil type recommendations.
Guidelines for cleaning or replacing the air filter, especially under dusty operating conditions.
Explains how to perform a compression test and the criteria for requiring engine inspection.
Covers essential carburetor adjustments, emphasizing their critical nature for engine performance.
Details the procedure for adjusting the engine's idle speed and vacuum synchronization.
Explains how to adjust the throttle cables to ensure synchronized throttle valve opening.
Provides a table with specific settings for carburetor jets and screws for different manifold configurations.
Instructions for spark plug maintenance, cleaning, replacement, and interpreting their condition.
Guidance on visually inspecting the exhaust system for damage, leaks, and securing flanges.
Instructions for checking the tightness of various bolts and nuts, with references to torque values.
Details how to check the electrical resistance of key engine components using a table of specifications.
Specifies that major inspections at Time Between Overhaul (TBO) must be performed by the manufacturer or approved centers.
States that major repairs and modifications should only be done by authorized service centers or the manufacturer.
Lists common causes and corresponding actions for when the engine fails to start or ignite.
Identifies reasons for rough idling in a warmed-up engine and suggests corrective measures.
Addresses causes of erratic engine running or occasional misfires and their solutions.
Explains potential causes of engine overheating or high oil temperatures and their remedies.
Lists issues that prevent the engine from achieving full power and provides troubleshooting steps.
Diagnoses problems related to low oil pressure, including insufficient oil, circulation issues, and gauge defects.
Covers scenarios where the engine fails to shut down promptly after the ignition is turned off.
Identifies causes for high oil consumption, such as worn internal parts or poor oil quality.
Addresses engine knocking issues, often related to fuel octane, spark plugs, or temperature.
Provides solutions for difficulties encountered when starting the engine in cold conditions.
Defines the duration of the limited warranty for HKS non-certified aircraft engines based on time or operation hours.
Outlines the responsibilities of authorized HKS distributors in repairing or replacing defective engine components.
Specifies the requirements for obtaining warranty service, including proof of purchase and registration.
Lists conditions and damages that are not covered under the engine's limited warranty.
Provides contact information and procedure for obtaining service or assistance for engine issues.
Details the requirements for warranty to be valid, including registration card completion and submission.
States the effective date for the warranty policy for non-certified aircraft engines delivered by HKS.
Highlights the risks associated with non-certified aircraft engines, emphasizing operational safety and responsibility.
Contains fields for engine details, buyer, seller, and confirmation of manual understanding for warranty eligibility.