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UAM.POL.VCA.110 General performance requirements

ANNEX IX (Part-IAM) · Regulation (EU) No 965/2012 · EAR revision 27 Mar 2026

IRImplementing rule

UAM.POL.VCA.110General performance requirements

(a)The mass of the VCA:

(1)at the start of the take-off; or

(2)in the event of in-flight replanning, at the point from which the revised operational flight plan applies; shall not be greater than the mass at which the requirements of this Subpart can be complied with for the flight to be conducted, considering expected reductions in mass as the flight proceeds and such fuel jettisoning as applicable.

(b)The approved performance data contained in the AFM shall be used to determine compliance with the requirements of this Subpart, supplemented as necessary with other data as prescribed in the relevant requirement. The IAM operator shall specify such other data in the operations manual (OM). When applying the factors prescribed in this Subpart, any operational factors already incorporated in the performance data contained in the AFM shall be considered to avoid double application of factors.

(c)When showing compliance with the requirements of this Subpart, the following parameters shall be taken into account:

(1)the mass of the VCA;

(2)the configuration of the VCA;

(3)the environmental conditions, in particular:

(i)density altitude;

(ii)wind:

(A)except as provided in point (C), for take-off, take-off flight path and landing, the correction for wind shall not be more than 50 % of any reported steady headwind component of 5 kt or greater;

(B)when take-off and landing with a tailwind component is permitted in the AFM, and in all cases for the take-off flight path, the correction for tailwind shall not be less than 150 % of any reported wind component;

(C)when precise wind-measuring equipment enables the accurate measurement of wind velocity over the point of take-off and landing, wind components in excess of 50 % may be taken into account by the IAM operator, provided that the IAM operator demonstrates to the competent authority that the proximity to the FATO and accuracy enhancements of the wind-measuring equipment provide an equivalent level of safety;

(4)the operating techniques; and

(5)the operation of any systems that have an adverse effect on the VCA performance.

IR · UAM.POL.VCA.110 — Regulation (EU) No 965/2012 · Regulation (EU) 2024/1111 · Air OPS Easy Access Rules · EAR revision 27 Mar 2026

AMCAcceptable means of compliance

AMC1 UAM.POL.VCA.110General performance requirements

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CORRECTION FOR WIND The PIC should apply the correction required in accordance with point UAM.POL.VCA.110(c) on the reported wind component and use the resulting value for correcting other performance parameters (e.g. TODRV, LDRV) as specified in the AFM.

AMC · AMC1 UAM.POL.VCA.110 — Regulation (EU) No 965/2012 · ED Decision 2025/010/R · Air OPS Easy Access Rules · EAR revision 27 Mar 2026

GMGuidance material

GM1 UAM.POL.VCA.110General performance requirements

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DENSITY ALTITUDE Point (c)(3)(i) of point UAM.POL.VCA.110 refers to the pre-flight performance calculation of density altitude, essentially but not only for take-off and landing, using reported pressure altitude and temperature. For in-flight replanning, if necessary, the pressure altitude and temperature at the destination as reported would be used, not the altitude read by the sensors. Therefore, neither the pressure altitude nor the GNSS altitude available in flight will ever be used for the purpose of point (c)(3)(i) of point UAM.POL.VCA.110.

GM · GM1 UAM.POL.VCA.110 — Regulation (EU) No 965/2012 · ED Decision 2025/010/R · Air OPS Easy Access Rules · EAR revision 27 Mar 2026

GMGuidance material

GM2 UAM.POL.VCA.110General performance requirements

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REPORTED HEADWIND COMPONENT The reported headwind component is the one reported at the time of flight planning. It may be used provided that there is no significant change of unfactored wind prior to take-off.

GM · GM2 UAM.POL.VCA.110 — Regulation (EU) No 965/2012 · ED Decision 2025/010/R · Air OPS Easy Access Rules · EAR revision 27 Mar 2026

All rules in SUBPART C — VTOL-CAPABLE AIRCRAFT (VCA) PERFORMANCE AND OPERATING LIMITATIONS

Consolidated from the EASA Easy Access Rules (revision 27 Mar 2026, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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