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iv
WARNING
BACKGROUND.
Replacement parts, materials and accessories may be sold as being of aircraft
quality when actually the quality and origin of these units are unknown. Users of such units are
usually unaware of potential hazards involved with replacement parts not eligible for use on
certificated aircraft. Units may be deceptively advertised as "unused," "like new" or
"remanufactured." This implies the quality of such units is equal to an original, repaired or
overhauled unit.
Federal Aviation Regulations (FAR) 43.13 and FAR 145.57 specify performance rules for
replacement of parts and materials used in maintenance and alteration of United States (US)
certificated aircraft. As outlined in FAR 91.403, FAR 121.363, FAR 123.45, and FAR 135.143 (a),
the
owner/operator
is responsible for continued airworthiness of the aircraft which includes parts
replacement.
IDENTIFICATION OF THE APPROVED PARTS.
Approved serviceable replacement parts are
identified by:
a. A Federal Aviation Administration (FAA) Form 8130-3 Airworthiness Approval Tag. An
Airworthiness Approval Tag identifies a part or group of parts approved by authorized FAA
representatives.
b. An FAA Technical Standard Order (TSO) number and identification mark that indicates the
part or appliance has been manufactured under the requirements of FAR 21 Subpart O.
c. An FAA Parts Manufacturer Approval (PMA) symbol, together with the manufacturer's name,
part number and make and model of the type certified product on which the part might be
installed, stamped on the part. An FAA / PMA is issued under FAR 21.305. The make and
model information may be on a tag attached to the part.
d. Shipping ticket, invoice or other document which verifies the part was manufactured by a
facility holding an FAA Approved Production Inspection System issued under FAR 21 Subpart
F or by a manufacturer holding an FAA Production Certificate issued under FAR 21 Subpart G.
e. Certificate of airworthiness for export issued by a foreign government under the provisions of
FAR 21 Subpart N.
KNOW YOUR SUPPLIER.
Many reproduced parts and components are available for purchase
and installation on US certified aircraft. Often, an original part is used as a sample to produce
duplicates. The reproduced parts appear to be as good as the original part; however, many
unknown factors are not readily apparent to the purchaser such as degree of heat treating, plating,
inspections, tests and calibrations. Often the faulty part is not discovered until a malfunction or an
accident occurs.
SUMMARY.
In accordance with FAR certification of materials, parts and appliances for
return to service for use on aircraft is the responsibility of the person\agency who signs the
approval.
The
owner/operator
is responsible for the continued airworthiness of the aircraft. To
assure continued safety in aircraft operation, great care must be used when inspecting, testing
and determining the acceptability of all parts and materials. Exercise extreme discretion to identify
and establish the origin of materials, parts, and accessories.
Содержание TSIO-360-RB
Страница 11: ...1 5 FIGURE 1 1 Engine Description L TSIO 360 RB ...
Страница 12: ...1 6 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Страница 13: ...1 7 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Страница 14: ...1 8 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Страница 15: ...1 9 FIGURE 1 2 ENGINE DESCRIPTION L TSIO 360 RB Cont d ...
Страница 25: ...3 1 CHAPTER 3 SEALANTS AND LUBRICANTS Sealants Lubricants 3 2 ...
Страница 32: ...4 2 INTENTIONALLY LEFT BLANK ...
Страница 54: ...6 2 INTENTIONALLY LEFT BLANK ...
Страница 58: ...6 6 FIGURE 6 1 INSTALLATION DRAWING ...
Страница 59: ...6 7 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Страница 60: ...6 8 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Страница 61: ...6 9 FIGURE 6 1 INSTALLATION DRAWING cont d ...
Страница 64: ...6 12 INTENTIONALLY LEFT BLANK ...
Страница 70: ...7 6 INTENTIONALLY LEFT BLANK ...
Страница 82: ...10 2 INTENTIONALLY LEFT BLANK ...
Страница 85: ...11 3 FIGURE 11 1 INDUCTION AND EXHAUST SYSTEM ...
Страница 94: ...11 12 INTENTIONALLY LEFT BLANK ...
Страница 110: ...12 16 INTENTIONALLY LEFT BLANK ...
Страница 124: ...14 4 INTENTIONALLY LEFT BLANK ...
Страница 128: ...15 4 INTENTIONALLY LEFT BLANK ...
Страница 132: ...16 4 INTENTIONALLY LEFT BLANK ...
Страница 139: ...17 7 FIGURE 17 4 STARTER ADAPTER FITS LIMITS ...
Страница 140: ...17 8 INTENTIONALLY LEFT BLANK ...
Страница 143: ...18 3 FIGURE 18 1 ACCESSORY CASE DESCRIPTION ...
Страница 147: ...19 3 FIGURE 19 1 LUBRICATION SYSTEM SCHEMATIC ...
Страница 149: ...19 5 ACCESSORY CASE INTERNAL VIEW TSIO 360 FIGURE 19 2 OIL PUMP DESCRIPTION TSIO 360 ...
Страница 150: ...19 6 ACCESSORY CASE INTERNAL VIEW LTSIO 360 FIGURE 19 3 OIL PUMP DESCRIPTION LTSIO 360 ...
Страница 158: ...19 14 INTENTIONALLY LEFT BLANK ...
Страница 176: ...20 18 FIGURE 20 12 CYLINDER ASSEMBLY SERVICE LIMITS For Maintenance Cylinder Dimensions see next page ...
Страница 181: ...21 3 FIGURE 21 1 CRANKCASE DESCRIPTION ...
Страница 186: ...21 8 INTENTIONALLY LEFT BLANK ...
Страница 194: ...22 8 INTENTIONALLY LEFT BLANK ...
Страница 203: ...23 9 FIGURE 23 6 CONSTANT SPEED SEA LEVEL PERFORMANCE CURVE ...
Страница 204: ...23 10 FIGURE 23 7 FUEL FLOW VS METERED FUEL PRESSURE ...
Страница 205: ...23 11 FIGURE 23 8 FUEL FLOW VS BRAKE HORSEPOWER ...