0912-EX-ST-2013

Filing overview

Special Temporary Authority application - Address

Attention:

Flight Test

City:

Greensboro

E-Mail Address:

david_wells@haci.honda.com

State:

NC

Street Address:

6430 Ballinger Road

Zip Code:

27410

Special Temporary Authority application - Applicant Name

Name of Applicant:

Honda Aircraft Company, LLC

Special Temporary Authority application - Best Contact

First Name:

David

Last Name:

Wells

Phone Number:

336-662-0246

Title:

Manager, Flight Test Instrumentation

Special Temporary Authority application - Certification

Applicant certification

Neither the applicant nor any other party to the application is subject to a denial of Federal benefits that includes FCC benefits pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C. Section 862, because of a conviction for possession or distribution of a controlled substance. The applicant hereby waives any claim to the use of any particular frequency or electromagnetic spectrum as against the regulatory power of the United States because of the prvious use of the same, whether by license or otherwise, and requests authorization in accordance with this application. (See Section 304 of the Communications Act of 1934, as amended.) The applicant acknowledges that all statements made in this application and attached exhibits are considered material representations, and that all the exhibits part hereof and are incorporated herein as if set out in full in this application; undersigned certifies that all statements in this application are true, complete and correct to the best of his/her knowledge and belief and are made in good faith. Applicant certifies that construction of the station would NOT be an action which is likely to have a significant environmental effect. See the Commission's Rules, 47 CFR1.1301-1.1319.

Date:

2013-09-25 00:00:00.0

Signature of Applicant (Authorized person filing form):

David D. Wells

Title of Applicant (if any):

Manager - Flight Test Instrumentation

Special Temporary Authority application - Explanation

Please explain in the area below why an STA is necessary:

This experimental license is required to conduct FAA mandated testing necessary to support certification for High Intensity Radiated Fields (HIRF) on the Honda Aircraft Company (HAC) Model HA-420 business jet aircraft. The test data will be used to validate low level HIRF models, and design improvements, and ensure compliance with HIRF requirements as specified by: 1. HAC document HA-100-00005, Certification Plan for The HondaJet Model HA-420 Electromagnetic and Environmental Effects. 2. FAA Advisory Circular AC-20-158 The Certification of Aircraft Electrical and Electronic Systems for Operation in the High-Intensity Radiated Fields (HIRF) Environment. 3. 14CFR23 § 23.1308 HIRF Protection. In lieu of frequency tolerance, the occupied bandwidth of the emission will not extend beyond the band limits requested in this application. Honda Aircraft Company will ensure that the 406 - 406.1 MHz band is nothced out of the frequency sweeps, and exclude this band.

Special Temporary Authority application - Information

Callsign:

WF9XXX

Class of Station:

MO

Nature of Service:

Experimental

Special Temporary Authority application - Initial values - Purpose of Operation

Please explain the purpose of operation:

Mandated testing necessary to support certification for High Intensity Radiated Fields (HIRF) on the Honda Aircraft Company (HAC) Model HA-420 business jet aircraft. This testing is a continuation of design improvements from previous test - refer to File # 0535-EX-ST-2012. The HIRF assessment to be performed is comprised of Low Level Swept Current (LLSC) and Low Level Swept Field (LLSF) tests. These are low power tests which are only used to map coupling and shielding functions, and not intended to generate equipment upset. The LLSC test will involve illuminating the aircraft with a low level external HIRF to measure the transfer function between the external field and the aircraft and equipment wire bundle currents. By calculating the ratio between the induced wire bundle current and the illuminating antenna field strength and normalizing the this ratio to 1 V/m HAC will obtain the transfer function in terms of induced current per unit of external field strength. The LLSF will be performed on the aircraft from 100 MHz to 18 GHz. The internal RF fields in the vicinity of the equipment will be measured instead of the wire bundle currents. The relation between the internal and external field provides the attenuation of the structure for each tested location. Dwell Time During the LLSC test method the dwell time per frequency point will be 1.0 millisecond per point based on 501 steps in a 500 millisecond maximum sweep. ? 0.5 - 25.5 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 25 - 45 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 40 - 205 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 200 - 400 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. During the LLSF test method the dwell time per frequency point will be 0.3 milliseconds per point based on 501 steps in a 140 millisecond maximum sweep. ? 100 MHz - 1 GHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. ? 1 - 8 GHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. ? 8 - 18 MHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. Modulation All testing is performed using a Continuous Wave (CW) signal (i.e. no modulation). Therefore, no actual data is being transmitted during the test. Power Transmitted powers are only high enough to allow accurate monitoring using a sensitive receiver system. All transmitted power levels will remain less than the specified band specific Effective Radiated Power (ERP) as specified in the application.

Special Temporary Authority application - Manufacturer

Equipment 1 Experimental

Yes

Equipment 1 Manufacturer

ERA Technology

Equipment 1 Model Number

HF Dipole

Equipment 1 No. Of Units

1

Equipment 2 Experimental

Yes

Equipment 2 Manufacturer

Teseq

Equipment 2 Model Number

CBL 6111

Equipment 2 No. Of Units

1

Equipment 3 Experimental

Yes

Equipment 3 Manufacturer

AH Systems

Equipment 3 Model Number

SAS-571

Equipment 3 No. Of Units

1

Equipment 4 Experimental

Yes

Equipment 4 Manufacturer

Rohde and Schwartz

Equipment 4 Model Number

SMR20

Equipment 4 No. Of Units

1

Equipment 5 Experimental

Yes

Equipment 5 Manufacturer

Rohde and Schwartz

Equipment 5 Model Number

FSP30

Equipment 5 No. Of Units

1

Equipment 6 Experimental

Yes

Equipment 6 Manufacturer

ENI

Equipment 6 Model Number

5100L

Equipment 6 No. Of Units

1

Equipment 7 Experimental

Yes

Equipment 7 Manufacturer

LUCIX

Equipment 7 Model Number

S001200L3205

Equipment 7 No. Of Units

1

Special Temporary Authority application - Purpose of Operation

Please explain the purpose of operation:

Mandated testing necessary to support certification for High Intensity Radiated Fields (HIRF) on the Honda Aircraft Company (HAC) Model HA-420 business jet aircraft. Mandated testing necessary to support certification for High Intensity Radiated Fields (HIRF) on the Honda Aircraft Company (HAC) Model HA-420 business jet aircraft. This testing is a continuation of design improvements from previous test - refer to File # 0535-EX-ST-2012. The HIRF assessment to be performed is comprised of Low Level Swept Current (LLSC) and Low Level Swept Field (LLSF) tests. These are low power tests which are only used to map coupling and shielding functions, and not intended to generate equipment upset. The LLSC test will involve illuminating the aircraft with a low level external HIRF to measure the transfer function between the external field and the aircraft and equipment wire bundle currents. By calculating the ratio between the induced wire bundle current and the illuminating antenna field strength and normalizing the this ratio to 1 V/m HAC will obtain the transfer function in terms of induced current per unit of external field strength. The LLSF will be performed on the aircraft from 100 MHz to 18 GHz. The internal RF fields in the vicinity of the equipment will be measured instead of the wire bundle currents. The relation between the internal and external field provides the attenuation of the structure for each tested location. Dwell Time During the LLSC test method the dwell time per frequency point will be 1.0 millisecond per point based on 501 steps in a 500 millisecond maximum sweep. ? 0.5 - 25.5 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 25 - 45 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 40 - 205 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. ? 200 - 400 MHz: sweep time 500 ms, 501 frequency steps, dwell time at each discrete frequency = 1 ms. During the LLSF test method the dwell time per frequency point will be 0.3 milliseconds per point based on 501 steps in a 140 millisecond maximum sweep. ? 100 MHz - 1 GHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. ? 1 - 8 GHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. ? 8 - 18 MHz: sweep time 140 ms, 501 frequency steps, dwell time at each discrete frequency = 0.3 ms. Modulation All testing is performed using a Continuous Wave (CW) signal (i.e. no modulation). Therefore, no actual data is being transmitted during the test. Power Transmitted powers are only high enough to allow accurate monitoring using a sensitive receiver system. All transmitted power levels will remain less than the specified band specific Effective Radiated Power (ERP) as specified in the application.

Special Temporary Authority application - Requested Period of Operation

Operation End Date:

04/28/2014

Operation Start Date:

10/28/2013

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