Amdt. 33-3, E.. 4/3/67
FAR 33.99 : General conduct of block tests.
(a)
Each applicant may, in making a block test, use separate engines of identical design and construction in the vibration, calibration, endurance, and operation tests, ex-cept that, if a separate engine is used for the endurance test it must be subjected to a calibration check before starting the endurance test.
(b)
Each applicant may service and make minor repairs to the engine during the block tests in accordance with the service and maintenance instructions submitted in compliance with [Sec. 33.4]. If the frequency of the service is excessive, or the number of stops due to engine malfunction is excessive, or a major repair, or re-placement of a part is found necessary during the block tests or as the result of .ndings from the teardown inspection, the engine or its parts must be subjected to any additional tests the Administrator .nds necessary.
(c)
Eachapplicant mustfurnish all testingfacilities,including equipment and competent personnel, to conduct the block tests.
Amdt. 33-9, E.. 10/14/80
Chapitre 94
Appendix A : Instructions for Continued Airworthiness
Sommaire
FAR33.A1:[General.] . . . . . . . . . . . . . . . . . . . . . . 1174 FAR33.A2:[Format.] ...................... 1174 FAR33.A3:[Content.] ..................... 1174 FAR 33.A4 : Airworthiness Limitations section. . . . . . . . . 1175
1173
Appendix A : Instructions for Continued Airworthiness
FAR33.A1 :[General.]
(a)
[This appendix speci.es requirements for the preparation of Instructions for Conti-nued Airworthiness as required by Sec. 33.4.
(b)
The Instructions for Continued Airworthiness for each engine must include the Ins-tructionsforContinuedAirworthinessfor all engineparts.IfInstructionsforConti-nued Airworthiness are not supplied by the enginepart manufacturerfor an engine part, the Instructions for Continued airworthiness for the engine must include the information essential to the continued airworthiness of the engine.
(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 engine parts will be distributed.]
Amdt. 33-9, E.. 10/14/80
FAR33.A2 :[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. 33-9, E.. 10/14/80
FAR33.A3 :[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) Engine Maintenance Manual or Section.
(1)
Introduction information that includes an explanation of the engine’s features anddatatothe extent necessary for maintenance orpreventive maintenance.
(2)
A detailed description of the engine and its components, systems, and instal-lations.
(3)
Installation instructions, including proper procedures for uncrating, deinhibi-ting, acceptance checking, lifting, and attaching accessories, with any neces-sary checks.
(4)
Basic control and operating information describing how the engine compo-nents, systems, and installations operate, and information describing the me-thods of starting, running, testing, and stopping the engine and its parts in-cluding any special procedures and limitations that apply.
(5)
Servicing informationthat coversdetails regarding servicingpoints, capacities of tanks, reservoirs, types of .uids to be used, pressures applicable to the various systems, locations of lubrication points, lubricants to be used, and equipment required for servicing.
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本文链接地址：FAA规章 美国联邦航空规章 Federal Aviation Regulations 5(152)
