Document ID: FAA-2020-0519-0004
Agency: faa
Document Type: Rule
Title: Special Conditions: Aerospace Design and Compliance, LLC, Bombardier, Inc. Model CL-600-2B19 Airplane; Installation of a Therapeutic Oxygen System for Medical Use
Posted Date: 2020-08-12T04:00Z

[Federal Register Volume 85, Number 156 (Wednesday, August 12, 2020)]
[Rules and Regulations]
[Pages 48645-48646]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-16280]

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 Rules and Regulations
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  Federal Register / Vol. 85, No. 156 / Wednesday, August 12, 2020 / 
Rules and Regulations  

[[Page 48645]]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 25

[Docket No. FAA-2020-0519; Special Conditions No. 25-773-SC]

Special Conditions: Aerospace Design and Compliance, LLC, 
Bombardier, Inc. Model CL-600-2B19 Airplane; Installation of a 
Therapeutic Oxygen System for Medical Use

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions.

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SUMMARY: These special conditions are issued for the Bombardier Inc. 
(Bombardier) Model CL-600-2B19 airplane. This airplane, as modified by 
Aerospace Design and Compliance, LLC (Aerospace Design and Compliance), 
will have a novel or unusual design feature when compared to the state 
of technology envisioned in the airworthiness standards for transport 
category airplanes. The design feature is an installation of a 
therapeutic oxygen system for medical use. 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 August 12, 2020.

FOR FURTHER INFORMATION CONTACT: Robert Hettman, Propulsion & 
Mechanical Systems, AIR-672, Transport Standards Branch, Policy and 
Innovation Division, Aircraft Certification Service, Federal Aviation 
Administration, 2200 South 216th Street, Des Moines, Washington 98198; 
telephone and fax 206-231-3171; email Robert.Hettman@faa.gov.

SUPPLEMENTARY INFORMATION: 

Background

    On November 20, 2019, Aerospace Design and Compliance applied for a 
supplemental type certificate for the installation of a therapeutic 
oxygen system for medical use in the executive interiors of the 
Bombardier Model CL-600-2B19 airplane. The Model CL-600-2B19 airplane, 
which is currently approved under Type Certificate No. A21EA, is a 
twin-engine transport airplane with a maximum takeoff weight of 47,450 
lbs. The Model CL-600-2B19 airplane will have 55 seats approved for 
taxi, takeoff, and landing.

Type Certification Basis

    Under the provisions of title 14, Code of Federal Regulations (14 
CFR) 21.101, Aerospace Design and Compliance must show that the 
Bombardier Model CL-600-2B19 airplane, as changed, continues to meet 
the applicable provisions of the regulations listed in Type Certificate 
No. A21EA, or the applicable regulations in effect on the date of 
application for the change, except for earlier amendments as agreed 
upon by the FAA.
    If the Administrator finds that the applicable airworthiness 
regulations (e.g., 14 CFR part 25) do not contain adequate or 
appropriate safety standards for the Bombardier Model CL-600-2B19 
airplane 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 a supplemental type 
certificate 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 Bombardier Model CL-600-2B19 airplane 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 Bombardier Model CL-600-2B19 airplane will incorporate the 
following novel or unusual design features:
    A therapeutic oxygen system for medical use.
    As a part of the executive interior installation, the gaseous 
passenger-oxygen system will be outfitted with a therapeutic oxygen 
system. The therapeutic oxygen system shares the same supply of oxygen 
with the existing passenger oxygen system and consists of multiple 
constant-flow oxygen outlets located throughout the cabin. The 
flightcrew can turn the therapeutic oxygen system on and off from the 
flightdeck to allow use at any point during the flight, and to preserve 
a sufficient remaining oxygen reserve, in the event therapeutic oxygen 
is used for medical purposes, to accommodate the passengers in the 
event of an emergency oxygen situation.

Discussion

    No specific regulations address the design and installation of 
required passenger oxygen systems that share a supply source with an 
optional oxygen system used specifically for therapeutic applications. 
Therapeutic oxygen systems have been previously certified, and were 
generally considered an extension of the passenger oxygen system for 
the purpose of defining the applicable regulations. As a result, 
existing requirements, such as Sec. Sec.  25.1309, 25.1441(b) and (c), 
25.1451, and 25.1453, in the Bombardier Model CL-600-2B19 airplanes' 
certification basis applicable to this STC project, provide some design 
standards appropriate for oxygen system installations. In addition, 
Sec.  25.1445 includes standards for oxygen distribution systems when 
oxygen is supplied to flightcrew and passengers. If a common source of 
supply is used, Sec.  25.1445(a)(2) requires a means to separately 
reserve the minimum supply required by the flightcrew.
    Section 25.1445 is intended to protect the flightcrew by ensuring 
that an adequate supply of oxygen is available to complete a descent 
and landing following a loss of cabin pressure. When the regulation was 
written, the only passenger oxygen system designs were supplemental 
oxygen systems intended to protect passengers from hypoxia in the event 
of a decompression. Existing

[[Page 48646]]

passenger oxygen systems did not include design features that would 
allow the flightcrew to control oxygen to passengers during flight. 
There are no similar requirements in Sec.  25.1445 when oxygen is 
supplied from the same source to passengers for use during a 
decompression, and for discretionary or first-aid use any time during 
the flight. In the design, the passenger and therapeutic oxygen systems 
use the same source of oxygen. These special conditions contain 
additional design requirements for the equipment involved in this dual 
therapeutic oxygen plus gaseous oxygen installation.
    Furthermore, the potential hazard that can exist when the oxygen 
content of an enclosed area becomes too high because of system leaks, 
malfunction, or damage from external sources, make it necessary to 
ensure that adequate safety standards are applied to the design and 
installation of the oxygen system in Bombardier Model CL-600-2B19 
airplanes. These potential hazards also necessitate development and 
application of appropriate additional design and installation 
standards.
    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.

Discussion of Comments

    The FAA issued Notice of Proposed Special Conditions No. 25-20-06-
SC for the Bombardier Model CL-600-2B19 airplane, which was published 
in the Federal Register on June 16, 2020 (85 FR 36351). No substantive 
comments were received, and the special conditions are adopted as 
proposed.

Applicability

    As discussed above, these special conditions are applicable to the 
Bombardier Model CL-600-2B19 airplane. Should Aerospace Design and 
Compliance apply at a later date for a supplemental type certificate to 
modify any other model included on Type Certificate No. A21EA to 
incorporate the same novel or unusual design feature, these special 
conditions would apply to that model as well.
    Under standard practice, the effective date of final special 
conditions would be 30 days after the date of publication in the 
Federal Register. However, as the certification date for the Bombardier 
Model CL-600-2B19 airplane is imminent, the FAA finds that good cause 
exists to make these special conditions effective upon publication.

Conclusion

    This action affects only a certain novel or unusual design feature 
on one model of airplane. 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 airplane.

List of Subjects in 14 CFR Part 25

    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 Bombardier Model CL-600-2B19 
airplanes, as modified by Aerospace Design and Compliance, LLC.
    The distribution system for the passenger therapeutic oxygen 
systems must be designed and installed to meet requirements as follows:
    1. When oxygen is supplied to passengers for both supplemental and 
therapeutic purposes, the distribution system must be designed for 
either--
    a. A source of supplemental oxygen for protection following a loss 
of cabin pressure, and a separate source for therapeutic purposes: Or
    b. A common source of supply with means to separately reserve the 
minimum supply required by the passengers for supplemental use 
following a loss of cabin pressure.

    Issued in Des Moines, Washington, on July 22, 2020.
James E. Wilborn,
Acting Manager, Transport Standards Branch, Policy and Innovation 
Division, Aircraft Certification Service.
[FR Doc. 2020-16280 Filed 8-11-20; 8:45 am]
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