MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
Date
MAR 2017
Rev Date
Page
5
71-00-00 - GENERAL
The M20V aircraft has a Continental Motors Incorpor-
ated (CMI) TSIO- 550- G( ) series engine installed. This
is a six cylinder, 280 H.P., fuel injected, twin turbo-
normalized with dual intercoolers.
-WARNING-
Propeller Strike Incidents – OR Hydraulic
Lock – Refer to Continental Motors SB 96- 11
(or subsequent data) for required engine
maintenance action.
71-00-10 - ENGINE REMOVAL
It is recommended that engine mount be left on firewall
and engine assembly be removed at isolator attach
points. The engine will be removed with the turbines re-
maining attached to the engine.
To assist in installation, identify and tag each part as it is
removed. Plug or cap all lines, hoses, and fittings as
they are disconnected.
1. Make sure all cockpit switches are - OFF.
2. Turn fuel selector valve - OFF.
3. Remove engine cowling (see Section 71-10-00).
4. Disconnect battery ground cables.
5. Remove propeller (refer to section 61-00-10).
6. Drain engine oil sump.
7. Disconnect the following:
A. Cabin heat ducts (at engine).
B. Fuel vent lines, from engine mount and air-
frame.
C. Oil temperature bulb connections.
D. Oil pressure line connections.
E. Manifold pressure line from firewall.
F. Cylinder head temperature bulb connections.
8. Disconnect the following control linkage (ref.
Chapter 76 - Engine Controls):
A. Throttle control.
B. Propeller governor control.
C. Mixture control.
9. Disconnect ignition switch wires from magnetos.
-WARNING-
Ground magneto breaker points.
10. Disconnect fuel flow wires from fuel flow sensor.
11. Disconnect engine ground strap.
12. Disconnect alternator and starter wires.
CROSSOVER
PIPE STABILIZER
CROSSOVER
PIPE ASSY.
BRACKET
(BEHIND PIPE)
TAILPIPE
V- BAND CLAMP
CONNECTION
TAILPIPE
FORWARD
ENGINE RIGHT SIDE
FIGURE 71- 1
71-00-00
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