A. Scheduled Maintenance (continued)
2.
Definitions (continued):
(g) Operation Test - This test is used to ascertain that a system component is in operable condition
and can be performed with the equipment installed in the aircraft. In addition, each opera-
tional test must be performed by an FAA Certified Repair Station appropriately rated or by a
Certified Mechanic who is qualified on this aircraft. The recording of the above function
must be made in the permanent aircraft records by the authorized individual performing the
test.
(h) Functional Test - This test is used to ascertain that system or component is functioning proper-
ly and is in conformance with minimum acceptable design specifications. This test may
require the use of supplemental bench test equipment. In addition, each functional test must
be performed by an FAA Certified repair Station with appropriate ratings or by a Certified
Mechanic who is qualified on this aircraft. The recording of the above function must be made
in the permanent aircraft records by the authorized individual performing the test.
(i) Bench Check - Means removal of component from the aircraft to inspect for cleanliness,
impending failure, need for lubrication, repair or replacement of parts and calibration to at
least the manufacturers specifications using the manufacturers recommended test equipment
or standards or the equivalent.
Each bench test will be performed by a Piper Service Center, FAA Certified Repair Station
with appropriate rating or by a certified mechanic. This test will be performed at the sched-
uled interval regardless of any bench test performed on a particular component while being
repaired/overhauled before scheduled interval bench test. After the component is installed
into the aircraft, an operational test of the component and its related system should be per-
formed to ensure proper function. Serviceable parts that were issued to the component will be
filed in the aircraft permanent records. The person performing the check must make appropri-
ate entries in the aircraft’s permanent maintenance record.
(j) Maintenance - The word maintenance as defined by FAR Part 1, means “inspection, overhaul,
repair, preservation and the replacement of parts, but excludes preventive maintenance.”
(k) Routine Inspections - Consists of a visual examination or check of the aircraft and its compo-
nents and systems without disassembly.
(l) Special Inspections - Involve those components, systems or structure which by their applica-
tion or intended use require an inspection peculiar to, more extensive in scope or at a time
period other than that which is normally accomplished during the event inspection.
(m) Time in Service - As used in this procedure is the time from the moment the aircraft leaves the
ground until it touches the ground at the next point of landing.
(n) On Condition - Maintenance concept whereby some components of the engine remain in ser-
vice as long as they appear airworthy at each inspection. The replace-on-condition concept is
as opposed to replace after a “life-limited” time interval.the authorized individual performing
the test.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
5-20-00
Page 5-5
Reissued: July 1, 1993
1C10
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...