(4)
Servicing information that covers details regarding servicing points, capaci-ties of tanks, reservoirs, types of .uids to be used, pressures applicable to the various systems,location of accesspanelsforinspection and servicing,lo-cations of lubrication points, the lubricants to be used, equipment required for servicing,towinstructions andlimitations, mooring,jacking, andleveling information.
(b)
Maintenance Instructions.
(1)
Schedulinginformationfor eachpartofthe rotorcraft andits engines, auxiliary power units, rotors, accessories,instruments, andequipment thatprovides the recommended periods at which they should be cleaned, inspected, adjusted, tested, and lubricated, and the degree of inspection, the applicable wear tole-rances, and work recommended attheseperiods.However,the applicant may refer to an accessory, instrument, or equipment manufacturer as the source of thisinformationif the applicant shows that theitemhas an exceptionallyhigh degree of complexity requiring specialized techniques, test equipment, or ex-pertise.The recommended overhaulperiods and necessary cross referencesto the AirworthinessLimitations section of the manual must also be included. In addition,the applicant mustinclude aninspectionprogramthatincludesthe frequency and extent of the inspections necessary toprovidefor the continued airworthiness of the rotorcraft.
(2)
Troubleshooting information describing probable malfunctions, how to reco-gnize those malfunctions, and the remedial action for those malfunctions.
(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.] Amdt. 29-20, E.. 10/14/80
FAR 29.A4 : 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 ins-pectioninterval, andrelated structuralinspectionprocedure approved underSec.29.571. IftheInstructionsforContinuedAirworthiness consist of multipledocuments, the section required by this paragraph must be included in the principal manual. This section must contain a legible statement in a prominent location that reads : ”The Airworthiness Li-mitations section is FAA approved and speci.es maintenance required under Secs. 43.16 and[91.403] of theFederalAviationRegulationsunless an alternativeprogramhasbeen FAA approved.” Amdt. 29-27, E.. 8/18/90
′
Elodie Roux. Septembre 2003
Appendix A : Instructions for Continued Airworthiness
Chapitre 79
Appendix B : Airworthiness Criteria for Helicopter Instrument Flight
Sommaire
FAR29.B1:[I.General.] .................... 1082 FAR29.B2:[II.De.nitions.] . . . . . . . . . . . . . . . . . . 1082 FAR29.B3:[III.Trim.] ..................... 1082 FAR29.B4:[IV.Staticlongitudinal stability.] . . . . . . . . 1082 FAR29.B5:[V.Staticlateral-directional stability.] . . . . . . 1083 FAR29.B6:[VI.Dynamicstability.] . . . . . . . . . . . . . . 1083 FAR29.B7:[VII.Stability augmentationsystem(SAS).] . . 1084 FAR 29.B8 : VIII. Equipment, systems, and installation. . . . 1084 FAR29.B9:[IX.RotorcraftFlightManual.] . . . . . . . . . 1085 FAR29.C1:[Icing certi.cation.] . . . . . . . . . . . . . . . . 1085 FAR29.D1 :[CriteriaForDemonstration ofEmergencyEva-
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