Federal Aviation Administration (FAA), DOT.
Final special conditions; request for comments.
These special conditions are issued for Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes modified by Gulfstream Aerospace Corporation. These modified airplanes 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 modification incorporates the installation of a Rockwell Collins FDS-2000 Electronic Display System that performs critical functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for the protection of this system from the effects of high-intensity radiated fields (HIRF). 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.
The effective date of these special conditions is October 11, 2002. Comments must be received on or before November 25, 2002.
Comments on these special conditions may be mailed in duplicate to: Federal Aviation Administration, Transport Airplane Directorate, Attention: Rules Docket (ANM-113), Docket No. NM236, 1601 Lind Avenue SW., Renton, Washington 98055-4056; or delivered in duplicate to the Transport Airplane Directorate at the above address. All comments must be marked: Docket No. NM236. Comments may be inspected in the Rules Docket weekdays, except Federal holidays, between 7:30 a.m. and 4 p.m.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Connie Beane, FAA, Standardization Branch, ANM-113, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98055-4056; telephone (425) 227-2796; facsimile (425) 227-1100.End Further Info End Preamble Start Supplemental Information
The FAA has determined that notice and opportunity for prior public comment hereon are impracticable because these procedures would significantly delay certification, and thus delivery, of the affected airplane. In addition, the substance of these special conditions has been subject to the public comment process in several prior instances with no substantive comments received. The FAA therefore finds that good cause exists for making these special conditions effective upon issuance; however, the FAA invites interested persons to participate in this rulemaking by submitting written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We ask that you send us two copies of written comments.
We will file in the docket all comments we receive, as well as a report summarizing each substantive public contact with FAA personnel concerning these special conditions. The docket is available for public inspection before and after the comment closing date. If you wish to review the docket in person, go to the address in the ADDRESSES section of this preamble between 7:30 a.m. and 4 p.m., Monday through Friday, except Federal holidays.
We will consider all comments we receive on or before the closing date for comments. We will consider comments filed late if it is possible to do so without incurring expense or delay. We may change these special conditions in light of the comments we receive.
If you want the FAA to acknowledge receipt of your comments on this proposal, include with your comments a pre-addressed, stamped postcard on which the docket number appears. We will stamp the date on the postcard and mail it back to you.
On July 31, 2002, Gulfstream Aerospace Corporation, Dallas, Texas, applied for a supplemental type certificate (STC) to modify Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes. These airplanes are low-wing, pressurized transport category airplanes with two fuselage-mounted jet engines. They are capable of seating a maximum of 19 passengers, depending upon the configuration. The modification incorporates the installation of a Rockwell Collins FDS-2000 five “tube” Electronic Display System consisting of the following major components:
- Five (5) AFD-2000A Adaptive Flight Displays: Pilot Electronic Attitude Indicator (EADI), Pilot Electronic Horizontal Situation Indicator (EHSI), Multi-Function Display (MFD), Copilot EADI, Copilot EHSI.
- Three (3) DCP-2000 Display Control Panels: Pilot, MFD, Copilot.
- Two (2) DCU-2000 Data Concentrator Units.
This system has a potential to be vulnerable to high-intensity radiated fields (HIRF) external to the airplane.
Type Certification Basis
Under the provisions of 14 CFR 21.101, Amendment 21-69, effective September 16, 1991, Gulfstream Aerospace Corporation must show that Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes, as modified to include installation of the Rockwell Collins FDS-2000 Electronic Display System, continue to meet the applicable provisions of the regulations incorporated by reference in Type Certificate No. A21EA or the applicable regulations in effect on the date of application for the change. Subsequent changes have been made to § 21.101 as Start Printed Page 65476part of Amendment 21-77, but those changes do not become effective until June 10, 2003. The regulations incorporated by reference in the type certificate are commonly referred to as the “original type certification basis.” The specific regulations included in the certification basis for Bombardier Model CL-600-1A11 and CL-600—A12 airplanes include 14 CFR part 25, dated February 1, 1965, including amendments 25-1 through 25-37, and sections 25.675(a), 25.685(a), 25.733(c), 25.775(e), 25.787(c), 25.815, 25.841(b), 25.951(a), 25.979(d) and (e), 25.1041, 25.1143(e), 25.1303(a), 25.1322, 25.1385(c), 25.1557(b), and 25.1583(a) of Amendment 25-38; sections 25.901(b) and (c), 25.903(c) and (e), 25.933(a), 25.943, 25.959, 25.1091(a) and (d), 25.1145(c), 25.1199(b) and (c), 25.1207, 25.1549, and 25.1585(a)(9) of Amendment 25-40; and section 25.1309 of Amendment 25-41; section 25.1353(c) of Amendment 25-42; section 25.571 and 25.629(d)(4)(v) of Amendment 25-45; and sections 25.351 and 25.603 of Amendment 25-46.
If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25, as amended) do not contain adequate or appropriate safety standards for the Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16.
Special conditions, as defined in 14 CFR 11.19, are issued in accordance with § 11.38 and become part of the airplane's type certification basis in accordance with § 21.101(b)(2), Amendment 21-69, effective September 16, 1991.
Special conditions are initially applicable to the model for which they are issued. Should Gulfstream Aerospace Corporation apply at a later date 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 the provisions of § 21.101(a)(1), Amendment 21-69, effective September 16, 1991.
Novel or Unusual Design Features
As noted earlier, Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes modified by Gulfstream Aerospace Corporation will incorporate the Rockwell Collins FDS-2000 Electronic Display System that will perform critical functions. This system may be vulnerable to high-intensity radiated fields external to the airplane. The current airworthiness standards of part 25 do not contain safety standards adequate or appropriate to protect this equipment from the adverse effects of HIRF. Accordingly, this system is considered to be a novel or unusual design feature.
There is no specific regulation that addresses protection requirements for electrical and electronic systems from HIRF. Increased power levels from ground-based radio transmitters and the growing use of sensitive avionics/electronics and electrical systems to command and control airplanes have made it necessary to provide such protection.
To ensure that a level of safety is achieved that is equivalent to that intended by the regulations which are incorporated by reference, special conditions are needed for Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes modified by Gulfstream Aerospace Corporation. These special conditions will require that the Rockwell Collins FDS-2000 Electronic Display System, which perform critical functions, be designed and installed to preclude component damage and interruption of function due to the direct and indirect effects of HIRF.
High-Intensity Radiated Fields (HIRF)
With the trend toward increased power levels from ground-based transmitters and the advent of space and satellite communications, coupled with electronic command and control of the airplane, the immunity of critical digital avionics/electronics and electrical systems to HIRF must be established.
It is not possible to precisely define the HIRF to which the airplane will be exposed in service. There is also uncertainty concerning the effectiveness of airframe shielding for HIRF. Furthermore, coupling of electromagnetic energy to cockpit-installed equipment through the cockpit window apertures is undefined. Based on surveys and analysis of existing HIRF emitters, an adequate level of protection exists when compliance with the HIRF protection special condition is shown with either paragraph 1 or 2 below:
1. A minimum threat of 100 volts rms (root mean square) per meter electric field strength from 10 KHz to 18 GHz.
a. The threat must be applied to the system elements and their associated wiring harnesses without the benefit of airframe shielding.
b. Demonstration of this level of protection is established through system tests and analysis.
2. A threat external to the airframe of the field strengths indicated in the table below for the frequency ranges indicated. Both peak and average field strength components from the table are to be demonstrated.
|Frequency||Field strength (volts per meter)|
|10 kHz-100 kHz||50||50|
|100 kHz-500 kHz||50||50|
|500 kHz-2 MHz||50||50|
|2 MHz-30 MHz||100||100|
|30 MHz-70 MHz||50||50|
|70 MHz-100 MHz||50||50|
|100 MHz-200 MHz||100||100|
|200 MHz-400 MHz||100||100|
|400 MHz-700 Mhz||700||50|
|700 MHz-1 GHz||700||100|
|2 GHz-4 GHz||3000||200|
|4 GHz-6 GHz||3000||200|
|6 GHz-8 GHz||1000||200|
|8 GHz-12 GHz||3000||300|
|12 GHz-18 GHz||2000||200|
|18 GHz-40 GHz||600||200|
|The field strengths are expressed in terms of peak of the root-mean-square (rms) over the complete modulation period.|
The threat levels identified above are the result of an FAA review of existing studies on the subject of HIRF, in light of the ongoing work of the Electromagnetic Effects Harmonization Working Group of the Aviation Rulemaking Advisory Committee.
Applicability: As discussed above, these special conditions are applicable to Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes modified by Gulfstream Aerospace Corporation to incorporate the Rockwell Collins FDS-2000 Electronic Display System. Should Gulfstream Aerospace Corporation apply at a later date for a supplemental type certificate to modify any other model included on Type Certificate A21EA to incorporate the same novel or unusual design feature, these special conditions would apply to that model as well under the provisions of § 21.101(a)(1), Amendment 21-69, effective September 16, 1991.
This action affects only certain design features on Bombardier Model CL-600-1A11 and CL-600-A12 airplanes modified by Gulfstream Aerospace Corporation to incorporate a Rockwell Collins FDS-2000 Electronic Display System. It is not a rule of general applicability and affects only the applicant which applied to the FAA for approval of these features on the airplanes. Start Printed Page 65477
The substance of the special conditions for these airplanes has been subjected to the notice and comment procedure in several prior instances and has been derived without substantive change from those previously issued. Because a delay would significantly affect the certification of the airplane, which is imminent, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon issuance. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above.Start List of Subjects
List of Subjects in 14 CFR Part 25
- Aviation safety
- Reporting and recordkeeping requirements
The authority citation for these special conditions is as follows:
The Special Conditions
Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the supplemental type certification basis for Bombardier Model CL-600-1A11 and CL-600-2A12 airplanes as modified by Gulfstream Aerospace Corporation.
1. Protection from Unwanted Effects of High-Intensity Radiated Fields (HIRF). Each electrical and electronic system that performs critical functions must be designed and installed to ensure that the operation and operational capability of these systems to perform critical functions are not adversely affected when the airplane is exposed to high-intensity radiated fields external to the airplane.
2. For the purpose of these special conditions, the following definition applies: Critical Functions: Functions whose failure would contribute to or cause a failure that would prevent the continued safe flight and landing of the airplane.Start Signature
Issued in Renton, Washington, on October 11, 2002.
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 02-27171 Filed 10-24-02; 8:45 am]
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