Teledyne TSIO-360-RB, Maintenance Manual

Page: 117 / 206

13-7
Unless otherwise specified by the servo or airframe manufacturer, apply LPS 2,
PERMATEX “Maintain” Lubricant or equivalent to the two pivot points shown in Figure 13-
5. If lever or link rods are replaced initial lubrication must be accomplished using SHELL
#5 or LUBRICATE #630AA or equivalent. The other pivot points and control connections
shown in Figure 13-5 must be maintained in accordance with the servo or airframe
manufacturer’s instructions.
WARNING
Anytime fuel control to throttle linkage, attaching hardware, levers or lever
bushings haven replaced or reassembled, the fuel system must be checked,
adjusted and tested in accordance with Precision Airmotive Corporation RSA-5
Operation and Service Manual. See Related Publication Section 1-4 ordering
information.
Worn or corroded linkage or attaching hardware must be replaced in accordance with
Chapters 9 and 10 of the L/TSIO-360 overhaul manual, Form X30596A. Fuel servo levers
or lever bushings must be replaced in accordance with Precision Airmotive Corporation
RSA-5 Operation and Service Manual. See Related Publications Section 1-4 for ordering
information.
Consult the airframe manufacturer and /or their most current published instructions
concerning aircraft engine control cable attach point inspection, cleaning, repair,
installation and lubrication.
After the preceding procedures have been accomplished verify that each control has full
limit of travel, the required safeties are in place, that no binding of levers or linkages is
occurring and that control movement is unrestricted by contact with other parts or
components that are located in close proximity.
Compare recorded findings of operational inspection with the following data:
ENGINE
{
RPM
Propeller
{
Unmetered or
Pump Pressure
(PSID)
Fuel Flow
Lbs./Hr.
Fuel Flow
Gal./Hr.
(APPROX.)
L/TSIO-360-RB 700 RPM IDLE
2600 RPM F/T 35-45 140-150 24.0 - 25.0
NOTE . . . The fuel system must be adjusted using a calibrated Porta-Test Unit

connected in
accordance with the manufacturer’s instructions.
{
See Aircraft Specifications for other values where applicable.
NOTE… Fuel pressures must be checked using external, calibrated instrumentation connected to
the fuel system as shown in Chapter 23, “Fuel System Adjustment.”
Do not use airframe
cockpit gages when checking fuel pressures.
If the fuel system is not functioning properly, proceed to fuel system troubleshooting to determine
the cause and procedure for correction.
(continued on next page)