Experimental Licensing System
0535-EX-ST-2012
Experimental Licensing System filing 0535-EX-ST-2012 submitted by Honda Aircraft Company, LLC.
Filing overview
| Status | Grant Expired Due to New License |
|---|---|
| Call sign | WF9XXX |
| Date filed | 2012-06-29 |
| Status date | 2012-08-30 |
| FCC source | View the FCC filing record |
Special Temporary Authority application - Address
- Attention:
- Flight Test
- City:
- Greensboro
- E-Mail Address:
- robert_brock@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:
- Robert
- Last Name:
- Brock
- Phone Number:
- 336-662-0246
- Title:
- Manager, Flight Test Coordination
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:
- 2012-06-29 00:00:00.0
- Signature of Applicant (Authorized person filing form):
- Thorton Wooding
- Title of Applicant (if any):
- Manager, Procurement
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 frequency HIRF models 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 ยง 23.1308 ?HIRF Protection.
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:
- 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 - Initial values - Requested Period of Operation
- Operation End Date:
- 06/08/2012
- Operation Start Date:
- 03/08/2012
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. 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:
- 06/08/2013
- Operation Start Date:
- 03/08/2013
Frequencies
| Action | Lower MHz | Upper MHz | Class | Output W | ERP W | Emission | Signal |
|---|---|---|---|---|---|---|---|
| North Carolina | 0.10 | ||||||
| New | MO | 0.400000 | N0N | ||||
| State | Radius of Operation | ||||||
| New | 0.50000000 | 25.50000000 | MO | 100.000000 | N0N | ||
| New | 0.50000000 | 25.50000000 | MO | 0.100000 | N0N | ||
| New | 25.00000000 | 130.00000000 | MO | 100.000000 | N0N | ||
| New | 25.00000000 | 130.00000000 | MO | 0.100000 | N0N | ||
| New | 125.00000000 | 1200.00000000 | MO | 0.100000 | N0N |
Sites
| Site | Location | Coordinates | Operating area | County | Radius |
|---|---|---|---|---|---|
| North Carolina | North 36 6 8 West 79 55 28 | Honda Aircraft Company apron | 0.10 | ||
| Greensboro, North Carolina | North 36 6 8 West 79 55 28 | Greensboro, NC: Honda Aircraft C | 0.10 |
Grant actions
| Date | Category | Description |
|---|---|---|
| 2012-08-30 | Grant | Grant Generated [Aug 30 2012] |
Sources and provenance
| Source | Source record | Retrieved | Match |
|---|---|---|---|
| ELS | 0535-EX-ST-2012 | 2026-07-30 08:57:07 | Source Primary |
Selected field provenance
| Field | Displayed value | Source | Observed |
|---|---|---|---|
| Status | Grant Expired Due to New License | ELS 0535-EX-ST-2012 | 2026-07-30 08:57:07 |
| Applicant Name | Honda Aircraft Company, LLC | ELS 0535-EX-ST-2012 | 2026-07-30 08:57:07 |
| Call Sign | WF9XXX | ELS 0535-EX-ST-2012 | 2026-07-30 08:57:07 |
| Receipt Date | 2012-06-29 | ELS 0535-EX-ST-2012 | 2026-07-30 08:57:07 |
| Status Date | 2012-08-30 | ELS 0535-EX-ST-2012 | 2026-07-30 08:57:07 |
Documents
| Document | Type | Date | Status |
|---|---|---|---|
| Grant E-mail Notification generated [Aug 31 2012] | Correspondence | 2012-08-31 | Available |
| Exhibit Update for Shielding by Bldg | Images | 2012-08-06 | Available |
| Incoming generated [Aug 6 2012] | Correspondence | 2012-08-06 | Available |
| E-Mail generated [Jul 3 2012] | Correspondence | 2012-07-03 | Available |
| Antenna Drawing | Text Documents | 2012-06-29 | Available |
| Test Narrative | Text Documents | 2012-06-29 | Available |
| View Grant | Pending archive |