Rule2026-08938
Special Conditions: Skyryse, Robinson Helicopter Company Model R66 Helicopter; Static Longitudinal Stability
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
May 6, 2026
Effective
June 5, 2026
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
These special conditions are issued for the Robinson Helicopter Company (Robinson) Model R66 helicopter. This helicopter, as modified by Skyryse, will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for normal category rotorcraft. This design features a four- axis full authority digital fly-by-wire (FBW) flight control system (FCS), which provides aircraft control through pilot input or coupled autopilot modes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Full Text
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<title>Federal Register, Volume 91 Issue 87 (Wednesday, May 6, 2026)</title>
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[Federal Register Volume 91, Number 87 (Wednesday, May 6, 2026)]
[Rules and Regulations]
[Pages 24339-24341]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2026-08938]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 27
[Docket No. FAA-2025-2303; Special Conditions No. 27-059-SC]
Special Conditions: Skyryse, Robinson Helicopter Company Model
R66 Helicopter; Static Longitudinal Stability
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
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SUMMARY: These special conditions are issued for the Robinson
Helicopter Company (Robinson) Model R66 helicopter. This helicopter, as
modified by Skyryse, will have a novel or unusual design feature when
compared to the state of technology envisioned in the airworthiness
standards for normal category rotorcraft. This design features a four-
axis full authority digital fly-by-wire (FBW) flight control system
(FCS), which provides aircraft control through pilot input or coupled
autopilot modes. The applicable airworthiness regulations do not
contain adequate or appropriate safety standards for this design
feature. These special conditions contain the additional safety
standards that the Administrator considers necessary to establish a
level of safety equivalent to that established by the existing
airworthiness standards.
DATES: Effective June 5, 2026.
FOR FURTHER INFORMATION CONTACT: Mitch Soth, Product Policy Management,
AIR-62B, Technical Policy Branch, Policy and Standards Division,
Aircraft Certification Service, Federal Aviation Administration, FAA
Southwest Regional Office, 10101 Hillwood Parkway, Fort Worth, TX
76177; telephone 817-222-5104; email <a href="/cdn-cgi/l/email-protection#f4999d80979cda879b809cb4929595da939b82"><span class="__cf_email__" data-cfemail="5835312c3b30762b372c30183e3939763f372e">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
On April 10, 2023, Skyryse applied for a supplemental type
certificate (STC) for the installation of novel control inputs and an
FBW system in the Model R66 helicopter. The Robinson Model R66
helicopter, currently approved under Type Certificate No. R00015LA, is
a single-engine, five-passenger helicopter with a maximum takeoff
weight of 2,700 pounds.
Title 14 CFR 27.171, 27.173, and 27.175 establish the minimum
requirements for static longitudinal stability for operation under
visual flight rules, and appendix B of part 27, sections IV and VII,
``Airworthiness Criteria for Helicopter Instrument Flight,'' provides
the airworthiness criteria for helicopter instrument flight. However,
these requirements are inadequate for the Robinson Model R-66
helicopter as modified by Skyryse because the longitudinal control laws
may permit neutral or negative static stability rather than requiring
positive static stability throughout the approved flight envelope.
Type Certification Basis
Under the provisions of Sec. 21.101, Skyryse must show that the
Robinson Model R66 helicopter, as changed, continues to meet the
applicable provisions of the regulations incorporated by reference in
Type Certificate No. R00015LA or with the regulations in effect on the
date of the application for the change.
If the Administrator finds that the applicable airworthiness
regulations (i.e., 14 CFR part 27) do not contain adequate or
appropriate safety standards for the Robinson Model R66 helicopter
because of a novel or unusual design feature, special conditions are
prescribed under the provisions of Sec. 21.16.
Special conditions are initially applicable to the model for which
they are issued. Should the applicant apply for an STC to modify any
other model included on the same type certificate to incorporate the
same novel or unusual design feature, these special conditions would
also apply to the other model under Sec. 21.101.
In addition to the applicable airworthiness regulations and special
conditions, the Robinson Model R66 helicopter must comply with the fuel
vent and exhaust emission requirements of 14 CFR part 34, and the noise
certification requirements of 14 CFR part 36.
The FAA issues special conditions, as defined in 14 CFR 11.19, in
accordance with Sec. 11.38, and they become part of the type
certification basis under Sec. 21.101.
Novel or Unusual Design Features
The Robinson Model R66 helicopter will incorporate the following
novel or unusual design feature:
A four-axis full authority digital FBW FCS that provides aircraft
control through pilot control inputs or coupled autopilot modes in
addition to degraded modes.
Discussion
The Skyryse Robinson Model R66 helicopter is configured with an FBW
FCS, which needs to be evaluated for
[[Page 24340]]
acceptable static stability characteristics.
For conventional rotorcraft having mechanical linkages from the
primary cockpit flight controls to the rotor, static longitudinal
stability means that a pull displacement or force on the cyclic will
result in a reduction of speed relative to the trim speed, and that a
push displacement or force will result in a higher speed relative to
the trim speed. Acceptable longitudinal stability is necessary for the
following reasons:
<bullet> Airspeed change cues are provided to the pilot through
increased and decreased forces on the controller.
<bullet> Short periods of unattended control of the rotorcraft do
not result in significant changes in attitude, airspeed, or load
factor.
<bullet> A predictable pitch response is provided to the pilot.
<bullet> An acceptable level of pilot workload, to attain and
maintain trim speed and attitude, is provided to the pilot.
<bullet> Longitudinal stability provides gust stability.
The pitch control movement of the cyclic for the FBW FCS is an
attitude command, which results in a rotor movement to attain the
commanded pitch attitude. The flight path commanded by the initial
cyclic input will remain stick-free until the pilot gives another
command. This control function is applied during ``normal'' control
laws within the approved flight envelope.
As detailed in Sec. 27.173(b) and considered in Advisory Circular
(AC) 27.173(A), ``Static Longitudinal Stability,'' which is contained
within AC 27-1B, ``Certification of Normal Category Rotorcraft,'' and
the positive control force stability requirements in appendix B to part
27, sections IV and VII, the slope of the control position (cyclic)
versus the airspeed curve must be positive (i.e., provide positive
static stability) throughout the full range of altitude for which
certification is requested with the throttle and collective pitch held
constant.
The design of the Skyryse FBW FCS is such that the static stability
requirements identified under part 27 and appendix B, section IV, may
not be met for all flight conditions.
The special conditions contain the additional safety standards that
the Administrator considers necessary to establish a level of safety
equivalent to that established by the existing airworthiness standards.
Discussion of Comments
The FAA issued notice of proposed special conditions No. FAA-2025-
2303 for the Robinson Model R66 helicopter, which was published in the
Federal Register on November 21, 2025 (90 FR 52569).
The FAA received a comment from the Citizens Rulemaking Alliance,
which raised several issues.
The commenter stated the FAA improperly relied on ``good cause'' to
bypass the notice and comment procedures and 30-day delayed effective
date under the Administrative Procedure Act. The commenter requested
that the FAA withdraw the immediate effectiveness of the special
conditions and republish them as proposed special conditions with a
reasonable comment period.
The FAA disagrees. As noted in 14 CFR 11.38, the Administrative
Procedure Act does not require notice and comment for special
conditions, which are rules of particular applicability. Nonetheless,
the FAA did provide notice and comment on these special conditions.
Citizens Rulemaking Alliance submitted this comment in response to a
notice of proposed special condition for which the FAA provided a 45-
day comment period. In addition, these final special conditions are
effective 30 days after publication in the Federal Register. Therefore,
no change is necessary.
The commenter stated that the FAA failed to provide the technical
rationale for its deviation from part 27 requirements and requested
that the FAA place in the docket a non-proprietary, substantive summary
of the technical basis and safety case. The commenter requested that
the FAA include a description of the modified flight control
architecture and control laws, a comparative assessment of the
applicable regulations, flight test plans and results, failure modes
and effects analysis excerpts, and proposed rotorcraft flight manual
changes.
The FAA disagrees. The preamble of the notice of proposed special
conditions explains the novel and unusual design feature and how the
current requirements in part 27 are not applicable to FBW rotorcraft
with indirect flight controls that have extensively augmented
stability. The preamble also explains the FAA's justification for the
safety standards in the special conditions. The additional information
requested by the commenter is proprietary. The Freedom of Information
Act (5 U.S.C. 552) and the Trade Secrets Act (18 U.S.C. 1905) prohibit
the FAA from disclosing such data.
The commenter stated that the special conditions are a ``novel
policy'' under Executive Order 12866 and requested that the FAA submit
them to the Office of Information and Regulatory Affairs for a
significance determination.
The FAA disagrees. Special conditions are not subject to review
under Executive Order 12866, which only applies to rules of general
applicability.
Lastly, the commenter stated that the FAA failed to comply with the
Regulatory Flexibility Act (5 U.S.C. 601-612) and requested that the
FAA include in the docket its assessment of the burden of the special
conditions on small entities.
The FAA disagrees. Special conditions are not subject to the
Regulatory Flexibility Act, which only applies to general notices of
proposed rulemaking.
Applicability
As discussed above, these special conditions are applicable to the
Robinson Model R66 helicopter. Should Skyryse apply at a later date for
an STC to modify any other model included on Type Certificate No.
R00015LA to incorporate the same novel or unusual design feature, these
special conditions would apply to that model as well.
Conclusion
This action affects only a certain novel or unusual design feature
on the Model R66 helicopter. It is not a rule of general applicability
and affects only the applicant who applied to the FAA for approval of
these features on the rotorcraft.
List of Subjects in 14 CFR Part 27
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
Authority Citation
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.
The Special Conditions
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special conditions are issued as part of
the type certification basis for the Robinson Helicopter Company Model
R66 helicopter, as modified by Skyryse.
In lieu of the requirements of Sec. Sec. 27.173(b) and 27.175 for
operation under visual flight rules and the airworthiness criteria for
helicopter instrument flight in appendix B to part 27, sections IV and
VII, the following special conditions apply:
The rotorcraft must be shown to have suitable longitudinal
stability in any condition normally encountered in
[[Page 24341]]
service, including the effects of atmospheric disturbance. The showing
of suitable static longitudinal stability must be based primarily on a
positive control movement (positive control sense of motion as
referenced in AC 27.173A), in addition to rotorcraft handling qualities
by assessing pilot workload, cues, and pilot compensation for specific
test procedures during the flight test evaluation.
Issued in Fort Worth, Texas, on April 29, 2026.
Jorge R. Castillo,
Manager, Technical Policy Branch, Policy and Standards Division,
Aircraft Certification Service.
[FR Doc. 2026-08938 Filed 5-5-26; 8:45 am]
BILLING CODE 4910-13-P
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</html>Indexed from Federal Register on May 6, 2026.
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