[Federal Register Volume 60, Number 209 (Monday, October 30, 1995)] [Proposed Rules] [Pages 55220-55222] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 95-26770] ======================================================================= ----------------------------------------------------------------------- [[Page 55221]] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. NM-118; Notice No. SC-95-6-NM] Special Condition: Israel Aircraft Industries (IAI), Model Galaxy, High-Intensity Radiated Fields AGENCY: Federal Aviation Administration, DOT. ACTION: Notice of proposed special conditions. ----------------------------------------------------------------------- SUMMARY: This notice proposes special conditions for the Israel Aircraft Industries (IAI) Model Galaxy airplane. This new airplane will utilize new avionics/electronic systems, such as electronic displays and electronic engine controls, that perform critical functions. The applicable regulations do not contain adequate or appropriate safety standards for the protection of these systems from the effects of high- intensity radiated fields (HIRF). These proposed 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: Comments must be received on or before December 14, 1995. ADDRESSES: Comments on this proposal may be mailed in duplicate to: Federal Aviation Administration, Office of the Assistant Chief Counsel, Attn: Rules Docket (ANM-7), Docket No. NM-118, 1601 Lind Avenue SW., Renton, Washington, 98055-4056; or delivered in duplicate to the Office of the Assistant Chief Counsel at the above address. Comments must be marked: Docket No. NM-118. Comments may be inspected in the Rules Docket weekdays, except Federal holidays, between 7:30 a.m. and 4:00 p.m. FOR FURTHER INFORMATION CONTACT: Timothy Dulin, FAA, Standardization Branch, ANM-113, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington, 98055-4056; telephone (206) 227-2141; facsimile (206) 227-1149. SUPPLEMENTARY INFORMATION: Comments Invited Interested persons are invited to participate in the making of these proposed special conditions by submitting such written data, views, or arguments as they may desire. Communications should identify the regulatory docket or notice 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 before further rulemaking action is taken on these proposals. The proposals contained in this notice may be changed in light of comments received. All comments submitted will be available in the Rule 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 notice must submit with those comments a self-addressed, stamped postcard on which the following statement is made: ``Comments to Docket No. NM-118.'' The postcard will be date stamped and returned to the commenter. Background On July 29, 1992, Israel Aircraft Industries (IAI), Ben Gurion International Airport, Tel Aviv 70100, Israel, applied for a new type certificate in the transport airplane category for the Model Galaxy airplane. On April 19, 1995, IAI applied for an extension of the original application and selected June 21, 1994, as the new reference date of application. The Model Galaxy is a derivative of the IAI Model 1125 Westwind Astra and is designed to be a long-range, high-speed airplane with a swept low wing and two aft-fuselage-mounted Pratt & Whitney Canada (PWC) 306A engines. The Model Galaxy will have a maximum takeoff weight of 33,450 pounds, a conventional empennage, a crew of two, and will be operated as an executive/corporate or commuter airplane with a maximum seating capacity of 19 passengers. Type Certification Basis Under the provisions of Sec. 21.17, IAI must show, except as provided in Sec. 25.2, that the Model Galaxy meets the applicable provisions of part 25, effective February 1, 1965, as amended by Amendments 25-1 through 25-82. In addition, the proposed certification basis for the Model Galaxy includes part 34, effective September 10, 1990, including all amendments in effect at the time of certification; and part 36, effective December 1, 1969, including all amendments in effect at the time of certification. No exemptions are anticipated. The special conditions that may be developed as a result of this notice will form an additional part of the type certification basis. In addition, the certification basis may include other special conditions that are not relevant to these proposed special conditions. 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 Galaxy because of a novel or unusual design feature, special conditions are prescribed under the provisions of Sec. 21.16 to establish a level of safety equivalent to that established in the regulations. Special conditions, as appropriate, are issued in accordance with Sec. 11.49 of the FAR after public notice, as required by Secs. 11.28 and 11.29, and become part of the type certification basis in accordance with Sec. 21.17(a)(2). In addition to the applicable airworthiness regulations and special conditions, the Model Galaxy must comply with the fuel vent and exhaust emission requirements of part 34 and the noise certification requirements of part 36, and the FAA must issue a finding of regulatory adequacy pursuant to Sec. 611 of Public Law 92-574, the ``Noise Control Act of 1972.'' Special conditions are initially applicable to the model for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same novel or unusual design feature, the special conditions would also apply to the other model under the provisions of Sec. 21.101(a)(1). Novel or Unusual Design Features The Model Galaxy airplane incorporates new avionic/electronic systems, such as electronic displays and electronic engine controls, that perform critical functions. These systems may be vulnerable to high-intensity radiated fields external to the airplane. Discussion 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, special conditions are proposed for the IAI Galaxy that would require that electrical and electronic systems which 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. [[Page 55222]] 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 condition is shown with either paragraphs 1 OR 2 below: 1. A minimum threat of 100 volts per meter peak 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 indicted. ------------------------------------------------------------------------ Peak (V/ Average Frequency M) (V/M) ------------------------------------------------------------------------ 10 KHz-100 KHz.................................... 50 50 100 KHz-500 KHz................................... 60 60 500 KHz-2 MHz..................................... 70 70 2 MHz-30 MHz...................................... 200 200 30 MHz-100 MHz.................................... 30 30 100 MHz-200 MHz................................... 150 33 200 MHz-400 MHz................................... 70 70 400 MHz-700 MHz................................... 4,020 935 700 MHz-1 GHz..................................... 1,700 170 1 GHz-2 GHz....................................... 5,000 990 2 GHz-4 GHz....................................... 6,680 840 4 GHz-6 GHz....................................... 6,850 310 6 GHz-8 GHz....................................... 3,600 670 8 GHz-12 GHz...................................... 3,500 1,270 12 GHz-18 GHz..................................... 3,500 360 18 GHz-40 GHz..................................... 2,100 750 ------------------------------------------------------------------------ As discussed above, the proposed special conditions would be applicable initially to the IAI Model Galaxy. Should IAI apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, the special conditions would apply to that model as well, under the provisions of Sec. 21.101(a)(1). Conclusion This action affects certain design features only on the IAI Galaxy airplane. It is not a rule of general applicability and affects only the manufacturer 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 record keeping requirements. The authority citation for this special condition is as follows: Authority: 49 U.S.C. app. 1344, 1354(a), 1355, 1421, 1423, 1424, 1425, 1428, 1429, 1430, and 49 U.S.C. 106(g). The Proposed Special Condition Accordingly, the Federal Aviation Administration (FAA) proposes the following special condition as part of the type certification basis for the IAI Model Galaxy airplanes. 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. For the purpose of this special condition, 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. Issued in Renton, Washington, on October 13, 1995. Darrell M. Pederson, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service, ANM-100. [FR Doc. 95-26770 Filed 10-27-95; 8:45 am] BILLING CODE 4910-13-M