Federal Aviation Administration (FAA), DOT.
Final special conditions; request for comments.
These special conditions are issued for Model MD-10-10/10F and MD10-30/30F airplanes, manufactured by the McDonnell Douglas Corporation, now a wholly owned subsidiary of The Boeing Company. These airplanes will have novel and unusual design features when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. These airplanes will utilize electrical and electronic systems that perform critical functions. The applicable type certification 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 provided by the existing airworthiness standards.
The effective date of these special conditions is February 15, 2000. Comments must be received on or before March 27, 2000.
Comments on these special conditions may be mailed in duplicate to: Federal Aviation Administration, Transport Airplane Directorate, Attention: Rules Docket (ANM-114), Docket No. NM168, 1601 Lind Avenue SW., Renton, Washington, 98055-4056; or delivered in duplicate to the Transport Airplane Directorate at the above address. Comments must be marked: Docket No. NM168. 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:
Gerry Lakin, FAA, Transport Airplane Directorate, Aircraft Certification Service, Standardization Branch, ANM-113, 1601 Lind Avenue SW., Renton, Washington, 98055-4056; telephone (425) 227-1187; facsimile (425) 227-1149.End Further Info End Preamble Start Supplemental Information
The FAA has determined that notice and opportunity for prior public comment are impracticable because these procedures would significantly delay issuance of the approval design and thus delivery of the affected aircraft. 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.
Interested persons are invited to submit such written data, views, or arguments, as they may desire. Communications should identify the regulatory docket and special conditions number and be submitted in duplicate to the address specified above. All communications received on or before the closing date for comments will be considered by the Administrator. These special conditions may be changed in light of the comments received. All comments received will be available in the Rules Docket for examination by interested persons, both before and after the closing date for comments. A report summarizing each substantive public contact with FAA personnel concerning this rulemaking will be filed in the docket. Persons wishing the FAA to acknowledge receipt of their comments submitted in response to this request must submit with those comments a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket No. NM168.” The postcard will be date stamped and returned to the commenter.
On February 14, 1997, McDonnell Douglas Corporation (MDC) submitted an application to amend the DC-10/MD-11 Type Certificate No. A22WE to include four new models, MD-10-10/-10F and MD-10-30/-30F. The MD-10 series aircraft are modified DC-10 aircraft with an Advanced Common Flightdeck (ACF), similar to that on the Model MD-11, that will allow operation with a two person flight crew. No changes to primary structures, engines, primary flight control systems, or aircraft performance are being made.
The ACF on the MD-10 series aircraft will utilize electrical and electronic systems that perform critical functions; examples of which include the electronic displays and flight control computers. These systems can be susceptible to disruption to both command/response signals as a result of electrical and magnetic interference. This disruption of signals could result in loss of all critical functions that would prevent the continued safe flight and landing of the airplane.
Type Certification Basis
Under the provisions of § 21.101, The Boeing Company must show that the Model MD-10 series airplanes continue to meet the applicable provisions of the regulations incorporated by reference in Type Certificate No. A22WE, or the applicable regulations in effect on the date of application for the change to the Model MD-10 series aircraft. The regulations incorporated by reference in the type certificate are commonly referred to as the “original type certification basis.” Based on the application date, February 14, 1997, the applicable regulations are 14 CFR part 25, effective February 1, 1965, including amendments 25-1 through 25-89, for all areas affected by the change.
If the Administrator finds that the applicable airworthiness regulations (i.e., part 25 as amended) do not contain adequate or appropriate safety standards for the Model MD-10 series aircraft because of novel or unusual design Start Printed Page 9997features, special conditions are prescribed under the provisions of § 21.16.
Special conditions, as appropriate, are issued in accordance with § 11.49, as required by §§ 11.28 and 11.29(b), and become part of the type certification basis in accordance with § 21.101(b)(2).
Special conditions are initially applicable to the model for which they are issued. Should McDonnell Douglas Corporation, now a wholly owned subsidiary of The Boeing Company, apply at a later date for a change to the type certificate to include another model incorporating the same type certificate to incorporate the same novel or unusual design feature, these special conditions would apply to the other model as well under the provisions of § 21.101(a)(1).
Novel or Unusual Design Features
The ACF on the MD-10 series aircraft will utilize electrical and electronic systems that perform critical functions; examples of which include the electronic displays and flight control computers. These systems may be vulnerable to HIRF external to the airplane.
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 electrical and electronic systems to command and control airplanes have made it necessary to provide adequate protection.
To ensure that a level of safety is achieved equivalent to that intended by the applicable regulations incorporated by reference, special conditions are needed for the Model MD-10 series aircraft, which require that new or significantly modified electrical and electronic systems, such as the electronic displays and flight control computers, that perform critical functions be designed and installed to preclude component damage and interruption of function due to both the direct and indirect effects of HIRF.
High-Intensity Radiated Fields (HIRF)
With the trend toward increased power levels from ground-based transmitters, plus the advent of space and satellite communications coupled with electronic command and control of the airplane, the immunity of critical digital avionics 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 conditions is shown with either paragraph 1 OR 2 below:
1. A minimum threat of 100 volts rms 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 following field strengths for the frequency ranges indicated.
|Field strength (volts per meter)||Frequency|
|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|
|1 GHz-2 GHz||2000||200|
|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 computer 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.
As discussed above, these special conditions are applicable to Model MD-10 series airplanes. Should McDonnell Douglas apply at a later date for a change to the type certificate to include another model incorporating 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).
This action affects only certain design features on Model MD-10 series airplanes. 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.
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. It is unlikely that prior public comment would result in a significant change from the substance contained herein. For this reason, and 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 25End List of Subjects Start Amendment Part
The authority citation for these special conditions is as follows:End Amendment Part
The Special ConditionsStart Amendment Part
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 Model MD-10 series airplanes.End Amendment Part
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 condition that would prevent the continued safe flight and landing of the airplane.Start Signature
Issued in Renton, Washington, on February 15, 2000.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service, ANM-100.
[FR Doc. 00-4484 Filed 2-24-00; 8:45 am]
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