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PROVISIONAL ACCEPTABLE MEANS OF COMPLIANCE STANDARD IZ AT ION OF APPROVED AEROPLANE FLIGHT MANUALS AMENDMENT No. 1 - 10 DECEMBER 1968 1. AMEND the last sentence of paragraph 7.5 Conditions associated with graphs to read "speeds, including the power-off stalling speeds, should be stated in terms of IAS. The power-off ltrg" stalling speeds should be stated in terms of EAS." 2. ADD a new sub-paragraph 7.8.1 after the paragraph 7.8 Form of presentation of perform- ance to read - "7.8.1 Genera 1 inf orma t iontt. 3. AMEND the numbering of the existing sub-paragraph 7.8.1 A-i- meter error correction curves to read "7.8.1.1 Airspeed indicator and altimeter error correction curves" and AMEND the last sentence of this sub-paragraph to read "This is illustrated in Figure 2.1. ". 4. 4 a new sub-paragraph 7.8.1.2 after the subparagraph 7.8.1.1 - Airseed indicator and altimeter error correction curves to read "7.8.1.2 Power-off l"g" stalling speeds 7.8.1.2.1 A graph should be provided in which the power-off ll'g" stalling speeds are plotted as the ordinates with the aeroplane weight as the abscissa for the configura- tions cf wing flaps and other high-lift produding devices, if applicable and landing gear used in the operation. The power-off lttg" stalling speeds should be in terms of EAS. This is illustrated in Figure 2.2. 7.8.1.2.2 A graph analogical to that mentioned at 7.8.1.2.1 should be provided, illustrating the power-off stalling speeds in terms of IAS. This graph should be included, with the appropriate explanatory text, in Section 8 - Appendices.". 5. AMEND the existing sub-paragraph 7.8.4 Take-off field lengths to read "7.8.4 Take-of f field lengths 7.8.4.1 Characteristic speeds 7.8.4.1.1 A graph should be provided to enable the IAS value on the ground ofthe speed V1, appropriate to the V/VR ratio, the weight, and, if applicable, the altitude and temperature, to be obtained for dry runway conditions. This is illustrated in Figure 5.
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