(3)
Information describing the order and method of removing and replacing pro-ducts andparts with any necessaryprecautionstobetaken.
(4)
Othergeneralproceduralinstructionsincludingproceduresfor systemtesting duringgroundrunning, symmetry checks, weighing anddeterminingthe center of gravity, lifting and shoring, and storage limitations.
(c)
Diagrams of structural access plates and information needed to gain access for ins-pections when access plates are not provided.
(d)
Details for the application of special inspection techniques including radiographic and ultrasonic testing where such processes are speci.ed.
(e)
Informationneeded to applyprotectivetreatmentstothe structureafterinspection.
(f)
All data relative to structural fasteners such as identi.cation, discard recommenda-tions, and torque values.
(g)
A list of special tools needed.
(h)
[In addition, for commuter category airplanes, the following information must be furnished :
(1)
Electrical loads applicable to the various systems;
(2)
Methods of balancing control surfaces;
(3)
Identi.cation ofprimary and secondary structures; and
(4)
Special repair methods applicable to the airplane.] Amdt. 23-34, E.. 02/17/87
FAR 23.G4 : Airworthiness limitations section.
[The Instructions for Continued Airworthiness must contain a section titled Airwor-thiness Limitations that is segregated and clearly distinguishable from the rest of the document. This section must set forth each mandatory replacement time, structural inspectioninterval, and related structuralinspectionprocedure requiredfortype certi.-cation.If theInstructionsforContinuedAirworthiness consist of multipledocuments, the section requiredby thisparagraph mustbeincludedin theprincipal manual.This section must contain a legible statement in a prominent location that reads : ”The Airworthi-nessLimitations sectionisFAA approved and speci.es maintenance required underSecs.
43.16 and91.403 of theFederalAviationRegulations unless an alternativeprogramhas been FAA approved.”] Amdt. 23-37, E.. 08/18/90
′
Elodie Roux. Septembre 2003
Appendix G : Instructions for Continued Airworthiness
Chapitre 42
Appendix H : Installation of an Automatic Power Reserve (APR) System
Sommaire
FAR23.H1:[General.] . . . . . . . . . . . . . . . . . . . . . . 476 FAR23.H2:[De.nitions.] .................... 476 FAR23.H3:[Reliability andperformancerequirements.] . . . 476 FAR23.H4:[Powersetting.] .................. 477 FAR23.H5:[Powerplantcontrols–general.] . . . . . . . . . . 477 FAR23.H6:[Powerplantinstruments.] . . . . . . . . . . . . . 478
475
AppendixH:Installation of anAutomaticPowerReserve(APR) System
FAR23.H1 :[General.]
(a)
[This appendix speci.es requirementsforinstallation ofanAPR enginepower control system that automatically advances power or thrust on the operating engine(s) in the event any engine fails during takeo..
(b)
With the APR system and associated systems functioning normally, all applicable requirements(except asprovidedinthis appendix) mustbe met without requiring any action by the crew to increase power or thrust.]
Amdt. 23-43, E.. 05/10/93
FAR23.H2 :[De.nitions.]
(a)
[Automatic power reserve system, means the entire automatic system used only duringtakeo.,includingalldevicesboth mechanical and electricalthat sense engine failure, transmit signals, actuate fuel controls orpowerlevers on operating engines, includingpower sources,to achievethe scheduledpowerincrease andfurnishcockpit information on system operation.
(b)
Selectedtakeo.power,notwithstanding thede.nitionof ”Takeo.Power” inpart1 of the Federal Aviation Regulations, means the power obtained from each initial power setting approved for takeo..
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