O-200-D & X Series Engine Installation and Operation Manual
3-9
3 January 2017
Engine Installation
d. Verify independent switched connections to aircraft ground potential is securely
attached to each magneto ‘Switch” connection.
7. Inspect the physical integrity of the fuel system.
8. Inspect the physical integrity of the induction system airbox, ducts, seals and
gaskets.
9. Inspect the physical integrity of the lubrication system.
a. Service the oil with the proper grade and quantity of aviation engine oil.
b. Lock the oil gauge rod in the fill tube after verifying the proper oil level on the
rod.
c. Inspect the exterior of the engine for oil leaks.
10. Inspect the physical integrity of the exhaust system.
11. Repair any observable damage before releasing the engine to service.
3-2.5. Initial Preflight and Ground Run-up
Perform an Engine Operational Check after completing the engine installation and before
performing the flight check according to the Airplane Flight Manual (AFM) or Pilot
Operating Handbook (POH). Perform a flight check before releasing the engine for
normal service to ensure the installed engine meets the aircraft manufacturer’s
performance and operational specifications.
WARNING
The fuel system must be adjusted after installation in the
aircraft according to the “Engine Operational Check”
instructions in Section 6-3.6 of the Maintenance and Overhaul
Manual (M-2) to ensure proper operation. Correct all
discrepancies prior to release for flight.
O-200 engines are neither designed, nor approved, for
continuous negative or zero “G” operation. Engine Mount
loads shall not exceed FAR 23 utility category load factors.
CAUTION: Adhere to the “Engine Specifications” in Section 2-4
during all modes of engine operation, including the Flight Check and
Break-In period.
NOTE: Perform a flight check according to instructions in Section 4-2.3
before releasing the engine for normal operations. New and rebuilt
engines, and engine with one or more new cylinders or pistons, require a
25-hour break-in. After installation, avoid prolonged ground operation at
high power.
1Procedure
1. Perform an “Engine Operational Check” instructions in Section 6-3.6 of the
Maintenance and Overhaul Manual (M-2).
Summary of Contents for O-200-D
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