(b)
The Instructions for Continued Airworthiness for each airplane must include the InstructionsforContinuedAirworthinessfor each engine andpropeller(hereinafter designated ’products’), for each appliance required by this chapter, and any re-quired information relating to the interface of those appliances and products with the airplane. If Instructions for Continued Airworthiness are not supplied by the manufacturer of an appliance orproductinstalledinthe airplane,theInstructions forContinuedAirworthinessfor the airplane mustinclude theinformation essential to the continued airworthiness of the airplane.
(c)
The applicant must submit to the FAA a program to show how changes to the Instructions for Continued Airworthiness made by the applicant or by the manu-facturers of products and appliances installed in the airplane will be distributed.]
Amdt. 23-26, E.. 10/14/80
FAR23.G2 :[Format.]
(a)
[The Instructions for Continued Airworthiness must be in the form ofa manual or manuals as appropriate for the quantity of data to be provided.
(b)
The format of the manual or manuals must provide for a practical arrangement.] Amdt. 23-26, E.. 10/14/80
FAR 23.G3 : Content.
The contents of the manual or manuals must be prepared in the English language. The Instructions for Continued Airworthiness must contain the following manuals or sections, as appropriate, and information :
(a)
Airplane maintenance manual or section.
(1)
Introductioninformationthatincludes an explanation ofthe airplane’sfeatures anddatatothe extent necessary for maintenance orpreventive maintenance.
(2)
A description of the airplane and its systems and installations including its engines, propellers, and appliances.
(3)
Basic control and operation information describing how the airplane compo-nents and systems are controlled and how they operate, including any special procedures and limitations that apply.
(4)
Servicing informationthat coversdetails regarding servicingpoints, capacities of tanks, reservoirs, types of .uids to be used, pressures applicable to the va-rious systems,location of accesspanelsforinspection and servicing,locations of lubrication points, lubricants to be used, equipment required for servicing, towinstructions andlimitations, mooring,jacking, andleveling information.
(b)
Maintenance Instructions.
(1) Scheduling informationfor eachpart of the airplane andits engines, auxiliary power units,propellers, accessories,instruments, andequipment thatprovides the recommended periods at which they should be cleaned, inspected, ad-justed, tested, and lubricated, and the degree of inspection, the applicable weartolerances,and work recommended attheseperiods.However,the appli-cantmay refertoan accessory,instrument,orequipment manufacturerasthe source of thisinformationif the applicant shows that theitemhas an exceptio-nally high degree of complexity requiring specialized maintenance techniques, test equipment, or expertise. The recommended overhaul periods and neces-sary cross reference to the Airworthiness Limitations section of the manual must also be included. In addition, the applicant must include an inspection program that includes the frequency and extent of the inspections necessary to provide for the continued airworthiness of the airplane.
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本文鏈接地址：FAA規(guī)章 美國聯(lián)邦航空規(guī)章 Federal Aviation Regulations 3(16)
