Continental Motors O-200-D, Инструкция по установке и эксплуатации

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3-6 O-200-D & X Series Engine Installation and Operation Manual
3 January 2017
Engine Installation
4. Install the exhaust system according to the aircraft manufacturer's instructions.
WARNING
Oil pressure is applied to the face of the accessory drive pads. If
gasket or accessory covers are not properly installed and
torqued to Appendix B specifications, oil leakage will occur.
5. Connect the remote mounted oil cooler (if equipped) hoses to the engine oil cooler
adapter according to the aircraft manufacturer's instructions.
6. Service the engine to the specified oil sump capacity according to the “Engine Oil
Servicing” instructions in Section 6-4.8 of M-0, Standard Practice Maintenance
Manual.
WARNING
Do not install the ignition harness “B” nuts on the spark plugs
until the propeller installation and the ignition system
operational checkout is complete. Failure to comply may result
in bodily injury when the propeller is rotated during
installation.
7. Verify the Ignition Switch is OFF according to the aircraft manufacturer's
instructions.
8. Install the propeller according to the aircraft and propeller manufacturer's
instructions.
9. Perform the “Engine Pre-oiling” procedure according to the instructions in Section
5-2.9 of M-0, Standard Practice Maintenance Manual.
10. If the magnetos were loosened or rotated during engine installation, adjust magneto
to engine timing according to the “Ignition Timing” instructions in Section 6-4.9.1
of M-0, Standard Practice Maintenance Manual.
11. Install any remaining aircraft accessories according to the aircraft manufacturer’s
instructions.
12. Purge the aircraft fuel lines, connect the fuel lines to the carburetor, and leak check
the installed fuel lines according to the instructions in Section 3-2.3.2.
WARNING
Do not operate the engine until all hardware, spark plugs,
gaskets, and seals are in place and torqued and the oil sump is
properly filled to the specified capacity with oil.
13. Inspect the engine for any debris, discrepancies, or damage. Correct any
discrepancies.
14. Perform an “Installation Inspection” according to instructions in Section 3-2.4.
15. Perform the “Engine Operational Check” according to instructions in Section 6-3.6
of M-2, Maintenance and Overhaul Manual.