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時(shí)間:2011-04-25 08:29來源:藍(lán)天飛行翻譯 作者:航空
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Piper inspection programs comply with the Federal Aviation Regulations Parts 43, 91 and 135. The owner/operator is primarily responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness Directives and conformity with the requirements in FAR 91.409, 91.411 and 91.413.
The first overhaul or replacement of components should be performed at the given periods. The condition of various components can then be used as criteria for determining subsequent periods applicable to the individual airplane, depending on usage, providing the owner/operator has an established Part 91 Progressive Inspection Program (see 91.409(d)) or Part 135 Approved Aircraft Inspection Program (see 135.419).
The time periods given for inspections of various components are based on average usage and environmental conditions.
— Note —
The listed inspection, overhaul and replacement schedules do not guarantee that a particular item or component will reach the listed time without malfunction. Unique operating conditions encountered by individual airplanes cannot be controlled by the manufacturer.
B. DEFINITIONS
1.  Inspections - Must be performed only by Certified Mechanics who are qualified on this aircraft, utilizing acceptable methods, techniques and practices to determine physical condition and detect defects.
a.  Routine Inspection - Consists of a visual examination or check of the aircraft and its 
components and systems without disassembly. 
b.  Detailed Inspection - Consists of a thorough examination of the aircraft, appliance, component, 
or system; with disassembly as necessary to determine condition. 

Page 5-9 Revised: February 28, 2002
1B15
THE NEW PIPER AIRCRAFT, INC.
PA-44-180
AIRPLANE MAINTENANCE MANUAL

c.  Special Inspection - Involves those components, systems or structure which by their application 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 an event or annual inspection.
2.  
Checks - Can be performed by pilots and/or mechanics who are qualified on this aircraft and consists of examinations in the form of comparisons with stated standards for the purpose of verifying condition, accuracy and tolerances.

3.  
Approved Inspection - Means a continuing airworthiness inspection of an airplane and its various component and systems at scheduled interval in accordance with procedures approved by the FAA under FAR Part 91.409(d) or Part 135.419.

4.  
Inspection Time Limitations - For owners/operators conducting flight instruction for hire, carrying any person for hire, or with an established Part 91 Progressive Inspection Program (see 91.409(d)) or Part 135 Approved Aircraft Inspection Program (see 135.419), late compliance with the inspection interval of 100 hours may be extended by not more than ten (10) hours while enroute to a maintenance facility. The time used to reach the next inspection facility must be deducted from the next inspection time.

5.  
Tests - Operation of aircraft components, appliances or systems to evaluate functional performance.


a.  
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 operational 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.

b.  
Functional Test - This test is used to ascertain that system or component is functioning properly 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.


6.  
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 scheduled 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 performed 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 appropriate entries in the aircraft’s permanent maintenance record.
 
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