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

ANNEX IX (Part-IAM) · Air Operations · Regulation (EU) No 965/2012 · UAM.POL.VCA.050 – UAM.POL.VCA.145

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  1. UAM.POL.VCA.050 Scope

    This Subpart establishes performance requirements and operating limitations for IAM operations with VTOL-capable aircraft (VCA).

  2. UAM.POL.VCA.100 Type of operation

    VCA shall be operated in accordance with the applicable performance requirements for the intended type of operation to be conducted.

    AMC1 UAM.POL.VCA.100 Type of operation

    GM1 UAM.POL.VCA.100 Type of operation

  3. UAM.POL.VCA.105 VTOL-capable aircraft (VCA) performance data

    VCA shall be operated in accordance with the certified performance data and limitations contained in the AFM.

    AMC1 UAM.POL.VCA.105 VTOL-capable aircraft (VCA) performance data

  4. UAM.POL.VCA.110 General performance requirements

    The mass of the VCA: 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…

    AMC1 UAM.POL.VCA.110 General performance requirements

    GM1 UAM.POL.VCA.110 General performance requirements

    GM2 UAM.POL.VCA.110 General performance requirements

  5. UAM.POL.VCA.115 Obstacle accountability

    For operations to/from final approach and take-off areas (FATO), the IAM operator shall, during pre-fight planning and for the purpose of…

    GM1 UAM.POL.VCA.115 Obstacle accountability

    GM2 UAM.POL.VCA.115 Obstacle accountability

  6. UAM.POL.VCA.120 Take-off

    The take-off mass of the VCA shall not exceed the maximum take-off mass specified in the AFM for the certified take-off procedure or procedures to be used.

    AMC1 UAM.POL.VCA.120 Take-off

    AMC2 UAM.POL.VCA.120 Take-off

    AMC3 UAM.POL.VCA.120 Take-off

    GM1 UAM.POL.VCA.120 Take-off

    GM2 UAM.POL.VCA.120 Take-off

  7. UAM.POL.VCA.125 Take-off flight path

    From the end of the take-off distance required for VCA (TODRV), following a CFP being recognised at or after the take-off decision point (TDP):

    GM1 UAM.POL.VCA.125 Take-off flight path

  8. UAM.POL.VCA.130 En route

    The mass of the VCA and the flight path at all points along the route following a critical failure for performance (CFP), and taking into account the…

  9. UAM.POL.VCA.135 Landing

    The landing mass of the VCA at the estimated time of landing shall not exceed the maximum mass specified in the AFM for the certified landing procedure…

    AMC1 UAM.POL.VCA.135 Landing

    GM1 UAM.POL.VCA.135 Landing

    GM2 UAM.POL.VCA.135 Landing

    GM3 UAM.POL.VCA.135 Landing

  10. UAM.POL.VCA.140 Mass and balance, and loading

    During any phase of the operation, the loading, mass, and centre of gravity (CG) of the VCA shall comply with the limitations specified in the AFM, or…

    AMC1 UAM.POL.VCA.140 Mass and balance, loading

    AMC2 UAM.POL.VCA.140 Mass and balance, loading

    AMC3 UAM.POL.VCA.140 Mass and balance, loading

    AMC4 UAM.POL.VCA.140 Mass and balance, loading

    AMC5 UAM.POL.VCA.140 Mass and balance, loading

    AMC6 UAM.POL.VCA.140 Mass and balance, loading

    GM1 UAM.POL.VCA.140 Mass and balance, loading

    GM2 UAM.POL.VCA.140 Mass and balance, loading

  11. UAM.POL.VCA.145 Mass and balance data, and mass and balance documentation

    The IAM operator shall establish mass and balance data and shall produce mass and balance documentation prior to each flight, specifying the load and its…

    AMC1 UAM.POL.VCA.145 Mass and balance data, documentation

    AMC2 UAM.POL.VCA.145 Mass and balance data, documentation

    AMC3 UAM.POL.VCA.145 Mass and balance data, documentation

    AMC4 UAM.POL.VCA.145 Mass and balance data, documentation

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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