(3)
Thefollowingperformanceinformation(determinedbyextrapolation and com-puted for the range of weights between the maximum landing weight and the maximum takeo. weight) :

(i)
Climb in the landing con.guration.

(ii)
Climb in the approach con.guration.

(iii) Landing distance.

(4)
Procedures established under Sec. 25.101(f) and (g) that are related to the limitations and information required by Sec. 25.1533 and by this paragraph

(b) in the form of guidance material, including any relevant limitations or information.

(5)
Anexplanationof signi.cantorunusual .ightorgroundhandling characteris-tics of the airplane.

(6)
Corrections to indicated values of airspeed, altitude, and outside air tempera-ture.

(7)
An explanation of operational landing runway length factors included in the presentation of the landing distance, if appropriate.

Amdt. 25-108, E.. 12/26/2002
Chapitre 51 Appendix A
FAR 25.A1 : Appendix A.

Tail wheel type

707
Appendix A

One wheel landing

Nose or tail wheel type
Lateral drift landing
2VM+1.0W
1.40V
M
W/2

W/2

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Appendix A

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Appendix A
Chapitre 52 Appendix B
713
Appendix B
FAR 25.B1 : Appendix B.

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Appendix B
Chapitre 53
Appendix C
FAR 25.C1 : Appendix C.
(a)
Continuous maximumicing.The maximum continuousintensity of atmosphericicing conditions (continuous maximum icing) is de.ned by the variables of the cloud liquid water content, the mean e.ective diameter of the cloud droplets, the am-bient air temperature, and the inter-relationship of these three variables as shown in (Figure 53.1, p. 718) of this appendix. The limiting icing envelope in terms of altitude and temperature is given in (Figure 53.2, p. 719) of this appendix. The inter-relationship of cloud liquid water content with drop diameter and altitude is determinedfrom(Figure53.1,p.718)and (Figure53.2,p.719).The cloudliquid water contentfor continuous maximumicing conditions of ahorizontal extent, other than

17.4 nautical miles, is determined by the value of liquid water content of (Figure 53.1, p. 718), multiplied by the appropriate factor from (Figure 53.3, p. 720) of this appendix.

(b)
Intermittent maximum icing. The intermittent maximum intensity of atmospheric icing conditions (intermittent maximum icing) is de.ned by the variables of the cloud liquid water content, the mean e.ective diameter of the cloud droplets, the ambient air temperature, and theinterrelationship ofthese three variables as shown in (Figure 53.4, p. 720) of this appendix. The limiting icing envelope in terms of altitude and temperature is given in (Figure 53.5, p. 721) of this appendix. The inter-relationship of cloud liquid water content with drop diameter and altitude is determined from (Figure 53.4, p. 720) and (Figure 53.5, p. 721). The cloud liquid water content for intermittent maximum icing conditions of a horizontal extent, other than 2.6 nautical miles, is determined by the value of cloud liquid water content of (Figure 53.4, p. 720) multiplied by the appropriate factor in (Figure 53.6,

p. 722) of this appendix.
717
Appendix C

Fig. 53.2– Continuous Maximum(Stratiform Clouds). Atmospheric IcingConditions. Ambient Temperature vs. Pressure Altitude
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Appendix C

Fig. 53.4– Intermittent Maximum(CumuliformClouds).AtmosphericIcingConditions.Liquid Water Content vs. Mean E.ective Drop Diameter

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