(3)
The landing distance, appropriate airspeed, and type of landing surface, toge-ther with all pertinent information that might a.ect this distance, including the e.ects of weight, altitude, and temperature;
(4)
The maximum safe wind for operation near the ground;
(5)
The airspeed calibrations;
(6)
The height-speed envelope except for rotorcraft incorporating this as an ope-rating limitation;
(7)
Glide distance as a function of altitude when autorating at the speeds and conditionsforminimum rateofdescent andbestglideangle,asdeterminedin Sec. 29.71;
(8)
Out-of-ground e.ect hover performance determined under Sec. 29.49 and the maximum safewinddemonstrated underthe ambientconditionsfordatapre-sented; and
(9)
Anyadditionalperformancedata necessaryforthe application of any operating
rule in this chapter. Amdt. 29-44, E.. 11/17/99
′
Elodie Roux. Septembre 2003
Subpart G : Operating Limitations and Information
FAR 29.1589 : Loading information.
There must be loading instructions for each possible loading condition between the maximum and minimum weights determined under Sec. 29.25 that can result in a center ofgravitybeyond any extremeprescribedin Sec. 29.27, assuming anyprobable occupant weights.
Chapitre 78
Appendix A : Instructions for Continued Airworthiness
Sommaire
FAR29.A1:[General.] . . . . . . . . . . . . . . . . . . . . . . 1078 FAR29.A2:[Format.] ...................... 1078 FAR29.A3:[Content.] ..................... 1078 FAR 29.A4 : Airworthiness Limitations section. . . . . . . . . 1079
1077
Appendix A : Instructions for Continued Airworthiness
FAR29.A1 :[General.]
(a)
[This appendix speci.es requirements for the preparation of Instructions for Conti-nued Airworthiness as required by Sec. 29.1529.
(b)
The Instructions for Continued Airworthiness for each rotorcraft must include the Instructions for Continued Airworthiness for each engine and rotor (hereinafter designated ”products” ),foreachappliancerequiredby thischapter,and any re-quired information relating to the interface of those appliances and products with the rotorcraft. If Instructions for Continued Airworthiness are not supplied by the manufacturer of an appliance or product installed in the rotorcraft, the Instruc-tions for Continued Airworthiness for the rotorcraft must include the information essential to the continued airworthiness of the rotorcraft.
(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-facturersofproducts and appliancesinstalledinthe rotorcraft willbedistributed.]
Amdt. 29-20, E.. 10/14/80
FAR29.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. 29-20, E.. 10/14/80
FAR29.A3 :[Content.]
[The contents of the manualor 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)
Rotorcraft maintenance manual or section.
(1)
Introduction information that includes an explanation of the rotorcraft’s fea-tures anddatatothe extent necessaryfor maintenance orpreventive mainte-nance.
(2)
A description of the rotorcraft and its systems and installations including its engines, rotors, and appliances.
(3)
Basic control and operation information describing how the rotorcraft compo-nents and systems are controlled and how they operate, including any special procedures and limitations that apply.
