Data Release Review Committee Charter, Exercises of Social Networks Theory and Analysis

Download Data Release Review Committee Charter and more Exercises Social Networks Theory and Analysis in PDF only on Docsity! £0, RESPONSIBILITIES. Responsibilities for and the implementation of this policy, as well as the establishment, participation, and operation of the DRRC, fie with the foilowing officials: a. The Associate Administrator for Air Traffic Services, ATS-1, is responsibie for: (1) Establishing and implementing the DRAC. (2) Providing approval of the original DRRC Charter and all subsequent changes to the document. (3) Ensuring a DRRC Chairperson is assigned. (4) Approving the final DRRC package. (5) Ensuring that a representative is appointed as a permanent member of the DRRC, as identified in the DRRC Charter. (8) Providing subject matter experts (ad hoc members) as required. b. The Air Traffic Division, AXX-500, shall designate a regional representative. The regional representative is responsible for: (1) Providing the requester with FAA Form 1200-5, NAS Data Release Request and associated application procedures. (2) Coordinating with appropriate regional affices to ensure NAS Data Release Request forms are completed and final approval packages contain all required information for the DRRC final decision. (3) Monitoring continued compliance with conditions identified in the DRRC final decision. (4) Ensuring notification to all outside interests for the requirement to reapply, as specified in this order. ¢. The Airway Facilities Division, AXX-400, shail designate a regional representative. who is responsible for: (1) Ensuring that if AF will maintain the outside interest's equipment, the requirements for maintenance are listed in the Memorandum of Agreement, Section II, Paragraph A. (See Appendix 2, Sample Memorandum of Agreement.) (2) Adhering to all applicable policies and procedures to escort the outside interest into AF workspace, if the vendor installs, maintains, or removes the equipment. (3) Providing a method of monitoring, or notifying the outside interest when her/his equipment fails. This method shail be described in the Memorandum of Agreement (MOA), Section ll, Paragraph A. d. The Office of the Chief Counsel, AGC-1, shail review all MOAs for NAS data releases for accuracy, validity, and legality. LI, PROCEDURES. The process for requesting release of NAS data or use of equipment interfaces is: a. Requests for release of NAS data or the use of equipment interfaces will be directed to the DRAC through the FAA regional office, AXX-510. If the requesting organization is a Program Office, Product Team, or integrated Product Team, the request will be given to the DRRC Executive Secretary. b. The requester will be provided a NAS Data Release Request Form (FAA Form 1200-5) which provides guidance for submitting a request. ¢. The DARC shail meet as required. The DRRC is the reviewing authority for release of NAS data to outside interests. The actions of the DRRC, as established by charter in Appendix 1, Data Release Review Committee Charter, shall result in one of the following decisions to the initial request: (1) Request Invalidation, along with the supporting rationale, will be sent by the DRRC to the requester with notification to the regional office, as appropriate. (2) A Request for Clarification, along with the supporting documentation, will be sent to the requester with notification to the regional office, as appropriate. This requires that the requester modify the submission in compliance with the direction provided by the DRRC and resubmit the NAS Data Release Request form for reconsideration. (3) A Request Validation will be forwarded to the Requirements Branch, AXX-510, with guidance to proceed with a submission of the final package. The package will be prepared between the requestor and the regional office with the appropriate information requested to develap the NAS Change Proposal (NCP, FAA Form 1800-2) and a MOA. The MOA shall be developed in accordance with the Appendix 2. 06 (2) Providing staffing and assigning an Executive Secretary for the DRAC. (3) Ensuring concerned Government organizations outside the FAA are invited as permanent members of the DRAC, as appropriate. (4) Providing recommendation to ATS-1 for FAA Form 1200-5, NAS Data Release Request, and final packages submitted to the DRRC. b. Executive Secretary. Staffing of this position shall be the responsibility of ATS-1. (1) Ensures that each FAA Form 1200-5, NAS Data Release Request, is processed and tracked from request initiation to final decision. (2) Ensures that required DRRC documentation, FAA Form 1200-5, NAS Data Release Request, and the final packages are provided to committee members in advance of the DRRC meetings. (3) Schedules and coordinates all DRRC meetings dates and arrangements. Absenteeism of DRRC permanent members will be recorded as a concurrence. (4) Maintains ail data pertinent to the functionality of the DRRC. (5) Develops and maintains a database that tracks the status of ail FAA Form 1200-5, NAS Data Release Request, and the DRRC final decisions. ¢. Permanent Members. Permanent members of the DRRC shail include a representative from: (1) Air Traffic Planning and Procedures (ATP). (2) Office of Information Systems Security (AIS). (3) Office of Civil Aviation Security Policy and Planning (ACP). (4) Operations Support (AOS). (5) NAS Operations (AOP). (8) Office of Civil Aviation Security Intelligence (ACI). (Z) Joint Radar Planning Group (JRPG). 69 (8) Office of the Chief Counsel (AGC) This member serves in an advisory capacity and is a non-voting member. (9) Office of Communications, Navigation, and Surveillance Systems (AND). d. The DRRC Permanent Members are responsible for: (1) Participating and/or ensuring proper representation to all scheduled meetings of the DRRC. (2) Providing their organization's position at the DRRC meetings that will contribute to the final decision. (3) Coordinating with subject matter experts within their organization to articulate their organization’s position during the DRRC meeting, as appropriate. (4) Ensuring regional compliance within the respective organization, as identified in this policy. . The following organizations may have representation as ad hoc, or subject matter expert members: (1) Department of Transportation, US Coast Guard (USCG). (2) Department of the Treasury, US Customs. (3) Department of Defense (DoD). (4) Department of Justice, Federal Bureau of Investigation (FBI). f, Ad Hoc Members. Subject matter experts will augment the standing membership on a case by case basis, after coordination with the DRRC Chairperson. Ad Hoc Members are non-voting members who serve in an advisory capacity only and are limited to Federal Government employees. 3. DRRC Administration. The DRAC Executive Secretary will be responsible for ensuring that FAA Form 1200-5, NAS Data Release Request, and the final packages are provided to committee members in advance of scheduled DRRC meetings. 6, Scheduled Meetings. The DARC secretary shall schedule DRRC meetings as follows: a. Quarterly. b. Whenever an additional meeting is required due to special circumstances. Z. DRRC Recommendations and Decisions. The DRRC will provide advice or recommendations to ATS-1 for the final decision on the submitted package. The DRRC may ask for additional information or modifications performed on each package to satisfy the committee before forwarding the request to ATS-1. 8, Delegation of DRRC Authority. The DRRC Chairperson may authorize FAA DRRC members to act as a chairperson via a memorandum to the DRRC Executive Secretary. DRRC permanent members can delegate specific authority (proxy) by a memorandum approved by the DRRC Chairperson. When a time critical or urgent processing of a data release request is necessary, the DRRC Chairperson shail cail an emergency meeting of the DRRC. Questions and concerns regarding ORRC decisions will be addressed to the DRRC Executive Secretary and will be presented to the DRRC Chairperson for resolution. APPENDIX 2. SAMPLE MEMORANDUM OF AGREEMENT. MEMORANDUM OF AGREEMENT Federal Aviation Administration (Insert name of AT Facility) and the (Insert name of outside interest) The (Insert name of outside interest) has requested that the Federal Aviation Administration (FAA) provide the outside interest access to certain flight track data to support the data requirements of the Environmentai Impact Statement (EIS) Airport Noise Compatibility Planning under 14 CFR Part 150/Noise Abatement, or . for (Insert city and the name of the airport: include the three-letter identification code for the airport). The FAA agrees to provide and 7 States money in an amount sufficient to compensaie for the loss sustained by the United States by reason of damage to or destruction of Government property. 12. The outside interest shall not release raw, unprocessed FAA data to the public, unless required by law; however, the outside interest may publicly release reports and analyses derived from the data, such as average flight trajectories and average flight events over a given point or track during designated time periods, as well as other derived data of a similar nature subject to the provisions of all other paragraphs of this agreement. At FAA's request, copies of all reports shalt be provided to FAA. 13. Additional procedures and restrictions, as required. 14. The outside interest shall direct requests and deliver discs/tapes to: (AT Facility name, address, and phone number). IV. INTERAGENCY COMMUNICATIONS. A. The outside interest shall direct communications to: (Provide the complete mailing address for the FAA facility). B. The FAA shall direct communications to: (Insert the complete mailing address for the outside interest). V. TERMINATION OF AGREEMENT. A. Either party may terminate this Agreement by giving the other party ninety (90) days written notification. The duration of this Agreement shail not exceed two years from the date signed by all parties. VI. ADDITIONAL PROCEDURES AND RES TRICTIONS. A. (Describe individually, by separate sub paragraph, each additional restriction and procedure that may apply). VIL. DATA COVERED BY THIS AGREEMENT. For purposes of the Agreement, the “Data” shall be defined as follows: (Describe the specific data here, and name the location; e.g., XYZ ASR-9). VU. SYSTEM REVIEW. The FAA and the outside interest agree to conduct a review, at the request of either party, to determine whether the system is operating in accordance with the specifications of this Agreement and to examine the need for modifications to this ot Agreement or to the operation of the system. The FAA and the outside interest will coordinate the location, time, and agenda of the review sessions. (Insert a time interval here, if applicable) The FAA and the outside interest concur with the provisions of this Agreement as indicated by the signatures of their duly authorized officials. FEDERAL AVIATION OUTSIDE INTEREST ADMINISTRATION (fill in name) By: menue . By: . : (Name and title) (Name and title) Date ave Dates __. By: a (Name and title} Date: ~4 an APPENDIX 3. FAA FORM 1200-5, NAS DATA RELEASE REQUEST NAS DATA RELEASE REQUEST OMB Approved 2120-0668 Paperwork Reduction Act Statement: This data is collected to assess the validity of your request for approval/disapproval. it will take approximately 27 hours or less to complete this form. The coffection is mandatory, and all information collected Shall be kept confidential. An agency may not collect, and a Person is not required to respond to an information collection, unless it displays a currently valid OMB Control Number. 1. Business/Organization Name 2. Business Phone Number 3. Address (Street, City, State, ZIP Code) 4. Paint of Contact (POC) Name 5. Phone 6. Full E-mail Address. Number 7. Are you currently receiving NAS data? Yes No (if no, skip to #10) | 8. Indicate your authority to access NAS Data, Memorandum of Agreement Government Contract Other (Explain) (Attach documentation) 9. Indicate if you have an approved NCP(s) of file: Yes No If yes, list the case file number(s) 10a. Type of data you are requesting: Delayed Recorded 10b. Describe the data requested: (Attach additional sheets) 11. Desenbe your proposed method for acquiring data: (Attach additional sheets) 12. Describe the nature of your organization‘business and the Purpose for this request. ;Aftach additional sheets) 73. Describe your sensitive data fitaring process. (attach additional sheets) 14. List any non-U.S. citizen personnel you wit! employ for this data request. Exolain his/her duties in relation to this data request Aitach adiaitional sheets) j U | Request Package Date // Date // Review Date // Issue FOR OFFICE USE ONLY: Date // FAA FORM 1200-5 (2/02) Local Reproduction Authorized NSN: 0052-00-923-3000 76 DD User Setup Sheet- Instructions General Instructions All Data Distribution users must complete the setup sheet prior to receiving DD data. To access the form simply click ‘on the tab at the bottom of the worksheet titled "User Setup Form". The setup form provides the necessary informat G1- Name of End User G2- End user Point of Contact G3- Have you submitted the following ? MOA FAA Form 1200-5 GA- Will you be sharing DD data with End Users who are not part of your company (Y/N)? F1 - Please Indicate in this section what types of information that you want DD to provide. F2 - Please indicate in this section whether there are areas of the airfield from which you do not want DD data. This must be the same Corporate name as is provided on your MOA and FAA Form 1200-5. tn the case of a Government End User your Agency name and code should be entered here, This information should be complete and maintained to prevent possible loss of information. This information will be used to follow up on any trouble calls that you initiate, A completed and approved MOA must be on file before you can begin receiving data. if you are a Government End User, skip down to Step F1 after answering this question. A completed and approved Form 1200-5 must be on file before you can begin receiving data You are required to indicate ail end users with whom you will be sharing your data, in accordance with he DD MOA. You are aiso responsible for providing updates to this information as needed. You shouid indicate all types of ASDE-X data that you want DD to provide. The fewer boxes that you check, the less data you will need to receive and store. Note: Do not forget to check one of the ADS-B data formats if you want to receive ADS-B data, This feature allows you to specify region(s) of the airfield that you do not wish to receive data from, An example would be the gate areas not associated with aircraft you are interested in. If you elect to use this feature you will most likely reduce the amount of data that you receive, 79 ASDE-X Data Distribution Government User Setup Sheet Gt- End Use Government Agency: Program/Dept/Code: End user address street street city, state zip code G2- End user Point of Contact Name Title Email Address Address (if different than above) street street city, state zip code Phone 1 Phone 2 ——— G3- Have you submitted the following (check all that apply)? MOA cg NCP I") NCP Number Gaé- Will you be sharing DD data with End Users who are not part of your company? (Y/N)? If you answered yes, then identify each user below and whether you have signed MOAs on file from them in accordance with the DD MOA Signed MOA on Company Name tile? POC Name POC Phone No. F1 - Please indicate in this section what types of information that you want DD to provide. Category 11 System Tracks Cr] Category10 SMR plots Category 10 ASR plots a) Category 10 MLAT \~ Category 10 ADS-B J Category 33 ADS-B 1 Ail of the above F2 - Please indicate in this section whether there are areas of the airfield from which you do not want DD data. Are there areas of the airfield from which you do not want to see aircraft or vehicle data? 80 - | hereby certify that the information provided above is correct and complete to the best of my knowledge. Name (please print) Name (Print): Signature: cee . Date: Title: ASDE-X Data Distribution User Setup Sheet G1- Name of End User: End user address street street city, state zip code G2- End user Point of Contact Name Title Email Address Address (if different than above} street street city, state zip code Phone 1 Phone 2 a ls the End User a US Government Entity? G3- Have you submitted the following (check ail that apply)? if the End User is a government agency then you may skip to step F1 MOA us after answering this question. FAA Form 1200-5 i NCP Gi NCP Number G4- Will you be sharing DD data with End Users who are not part of your company? if you answered yes. then identify each user below and whether you have signed MOAs on file from them in accordance with the DD MOA Signed MOA on Company Name file? POC Name POC Phone No. F1 - Please indicate in this section what types of information that you want DD to provide. Category 11 System Tracks oj Category10 SMA plots Category 10 ASR plots } Category 10 MLAT Category 10 ADS-B rt Category 33 ADS-B Wy All of the above st F2 - Indicate in this section whether there are areas of the airfield from which you do not want DD data. Are there areas of the airfield from which you do not want to see aircraft or vehicle data? f hereby certify that the information provided above is correct and complete to the best of my knowledge. Name (please print) Signature: Date: _ Title: ow co Technician Setup Sheet For Government Use Only This sheet is used ta provide a record of the initial setup as weil as any changes to the end users setup. If there are changes to an end-users setup then a new sheet should be filled out. Note: Be sure and provide the local AF office a copy of this for Is this a US Government end-user (pick one)? User Name User iD No. Primary Port Router Port/Jack Number IP Address Secondary Port Router Port/Jack Number IP Address TELCO Circuit ID The following F1 and F2 sections should be used to Provide a record of the setup. F1- Reports to be provided Category 11 System Tracks Oo Category 10 ASR plots Category10 SMR plots Category 10 MLAT All of the above Category 10 ADS-B OR La Category 33 ADS-B F2- Are there exclusion regions setup for the user? If the answer to the above question is yes then provide a brief description of the regions Name of technician Date of Action (setup, change, termination) Notes: 86 ADS-B - Automatic Dependent Surveillance-Broadcast subsystem ASDE - Airport Surface Detection Equipment ASR - Airport Surveillance Radar ASTERIX (All Purpose Structured Euro-control Radar {Information Exchange) - A Euro- control standard for the exchange of information that is used for the transmission of DD data. Data Distribution (DD) System - The ASDE-X subsystem, comprised of hardware, software, communications equipment and telecommunications lines, used to receive and transmit surface surveillance data to approved end users. MLAT (Multilateration) - A key component of the ASDE-X system, MLAT isa technique that uses an array of sensors strategically placed in and around the movement area of an airport to triangulate on transponder transmissions from aircraft and vehicles to track aircraft and vehicle movement. MOA - Memorandum of Agreement Movement Area- Those areas of an airport, such as runways, taxiways. and other areas, that are used for airport operations, such as taxiing, takeoff and landing of aircraft and vehicles, excluding ramps, gates and parking areas. Non-Movement Area - Non-operational areas of an airport, such as ramps, gates, and parking areas. SMR (Surface Movement Radar) — A Raytheon designed radar sometimes associated with ASDE-X. Generically it may refer to any radar used to monitor the movement area of an airport. Other radars that may be associated with the ASDE-X system in the future inctude the ASDE-3, SMRi, and SMRid radars. Third Party - A customer of an Outside Interest (Sensis Corporation), outside the United States Government, interested in receiving NAS data. 89 3 4 % 2 ee this document conta: orty of, Sensis © closed, in ete @ cartes heebtained won anther ic Overview 1. V4 1.2 1.3 1.4 3.4 3.2 3.3 44 4.2 43 44 45 6.1 6.2 63 Products amd Pricing ...........cccecccsecscsccsssessssttsesssssesssesceseeseeteseeseeses 2 Prime Mission Equipment... ccc. Ww ORD Prime Mission Equipment... fee “ 4.1.2 MDW Prime Mission Equipment... ccc cose . seed Recommended Spares Freee ee cece ene ie tec sneeneecccaetaetetacaerenieesnen 4 1.21 ORD Spares........ . vetecccenseeees tess eeeeesscccceveessetsveneases ech 4.2.2 MDW Spares ........ : sees : tetecceeceeee see a4 Time and Materiat Support... ccccceeccsccesssesecssesstescesrescesesseevensee 5 Payment Terms o..cecccccecsescsecsssseessercssrsevseessetescusesstesssvessseeeeeese wd Reference Documents Scape of Work and Responsibilities .....00...c.cccccccsseeecccccscssseceseeees 6 Data Distribution Cabinet ... 6 3.1.4 Sensis Responsibilities ....... 6 3.4.2 DOA’s Responsibilities 6 3.1.3 FAA's Responsibilities .... oe we 7? Display Processor and ATC Display Upgrade .. wd 3.24 Sensis Responsibilities ....... a? 3.22 DOA's Responsibilities . 8 3.23 FAA's Responsibilities 8 VeeLo NextGen 8 3.3.1 Sensis Responsibilities 00.00. eeaee 8 3.3.2 DOA’s Responsibilities ........... wees cease 9 3.3.3. FAA's Responsibilities ...... 9 Physicai Characteristics a] Data Distribution Cabinet... ccecccceeseseceeeeeee 9 Display Processor... ccceescece cseeseecccssesveseee see 10 Optional ATC Display ... -10 Optional ATC Keyboard ..... . al Optional ATC Trackball ............ 11 Schedule Support and Warranty... 213 Warranty occ beceeeaerees . 213 Post Warranty Product Support... oo. 213 Recommended Spares and Maintenance................. an we 13 6.3.4 Data Distribution 0... . : 13 6.3.2 Display Processor and Hi Brite Displays. vote tet 4.3.3 VeeLo NextGen. .. : : see . 13 SSensis Sensis Proprietary Duta 1. Products and Pricing Pricing is provided for Prime Mission Equipment, Spares, and Support. 1.1 Prime Mission Equioment +..4 ORD Prime Mi wipimant Figure 1 ORD Prime Mission Equipment Pricing 4) 1 Data Provides a firewall to the operational ASDE- $110,000 $14 10,000 26 weeks Distribution X system isolating the safety critical data ARO Cabinet from being used by other airport stakeholders. Includes Installation. 2) 3 Display The processor drives display allowing the $50,000 $150,000 26 weeks Processor ATC to view the equipment vehicles within ARO the movement area. Includes SW ticense. Comes with a Standard 19-inch LCD display, keyboard, and mouse. Includes SW license. 3) 3° Optional: Replaces 19-inch LCD Display, keyboard 20 500 $61,500 26 weeks ATC Display and mouse with ATC Hi Brite Display, ATC ARO Upgrade Keyboard and Trackball. 4) 176 VeeLo Magnetically Mounted Vehicle Locator. $1,748 $307,648 90 Days NextGen Allows the ASDE-X system to receive ARO; First (see notes identification as well as position information Availability 2,3) from vehicles, Sept 1, 2008 5) 1° Veelo PC Software that will allow the DOA to $544 $544 90 Days NextGen PC configure the VeeLos with Mode-S Codes, ARO; First Software 'D Codes, as well as coordinates that define Availability configuration transmit regions. Sept 1, 2008 kat 6) 1 Set-up and Sensis will send a person on-site for one $3,000 $3,000 <2 weeks Checkout day after the display is installed for a after system check-out and overview with the {Installation DOA. Total $632,692 | Note 1 - Prices quoted above are stated in 2008 calendar year dollars, representative of the base year, and are subject to an annual escalation rate of 3.5% per year over the five year period. Note 2 - Sensis’ jatest understanding from the FAA is that the FAA will issue only issue up to 200 Mode-S codes per airport and allow only 50 active in the movement area at a time. The FAA has also suggested some flexibility in thase restrictions Please note itis the buyer's responsibility to obtam from the FAA authorization to use this product in an airport environment, as. well as the Mode S address that needs to be loaded onto each unit, Contact info was previously provided. Note 3 - VeeLo NextGen price reflects a quantity discount, VeeLo NextGen Pricing for other quantities is as follows: Qty 1-50 $2,226/ea Qty 51-150 52,203/ea and Qly 151+ $1,748/ea vt 12 MON Prima Y sion Equipment Figure 2 MDW Prime Mission Equipment Pricing Data Provides a firewail to the operational $110,000 $110,000 26 weeks Distribution ASDE-X system isolating the safety ARO Cabinet critical data from being used by other airport stakeholders. Includes Installation 2) 1 Display The processor drives display allowing $50,000 $50,000 26 weeks Processor the ATC to view the equipment vehicles ARO within the movement area. Includes SW license. Comes with a Standard 19-inch LCD display, keyboard, and mouse. Includes SW license. 3) 50 VeeLo Magnetically Mounted Vehicle tocator. $2,226 $111,300 90 Days NextGen Allows the ASDE-X system to receive ARO; First (see notes 5,6) identification as well as position Availability information from vehicles. Sept 1, 2008 4) 1 VeeLo PC Software that will allow the DOA to $544 $544 90 Days NextGen PC configure the VeeLos with Mode-S ARO: First Software Codes, ID Codes, as well as Availability configuration coordinates that define transmit Sept 1, 2008 kit regions. 5) 1 Set-up and Sensis wilt send a person on-site for $3,000 $3,000 <2 weeks Checkout one day after the dispiay is installed for after a system check-out and overview with installation the DOA. | Total $274,844 Note 4 - Prices quoted above are stated in 2008 calendar yéar dollars, representative of the base year, and are subject to an annual escaiation rate of 3.5% per year over the five year period. Note 5 - Sensis’ latest understanding from the FAA is that the FAA will issue only issue up to 200 Mode-S codes per airport and allow only 50 active in the movement area at a time. The FAA has also suggested some flexibility in those restrictions. Please rote it is the buyer's responsibility to obtain from the FAA authorization ta use this product in an airport environment, as well as the Mode S address that needs to be loaded onto each unit. Contact info was previously provided. Note 6 - VaeLo NextGen price does not reflect a quantity discount. VeeLo NextGen pricing for other quantities is as follows: Oty 1-50 $2,.226/ea Qty 51-150 $2.203/ea and Qty 151+ $1,748/ea SAD pomary cae Sensis & Scnsis Propreetare: Dutta 3 1.2. Recommended Spares Pricing reflects 2008 base year prices. Pricing beyond 2008 base year will be subject to annual 3.5% escalation.. 12.4 ORD Soares Figure 3 outlines the recommended spares. Figure 3 ORD Spares Pricing Item [Qty [Name Description Unit Price | Price Delivery 1}} 1 |Dispiay Processor [Preloaded Spare CPU for the $ 5,000}3 5,000 |26 weeks CPU Display Processor, Does not include ARO SW license 2) 1 |ATC Display ATC Quality Display Workstation $ 18,000 | $ 18,000 126 weeks ARO 3) 4 [Trackball Trackball $ 2,000|$ 2,000 |26 weeks ARO 4) 1 [Keyboard Keyboard $ 2,000}$ 2,000 126 weeks ARO 5)f 9 |VeeLo NextGen Represents 5% of the 176 VeeLo $ 2.226 | $ 20,034 790 Days isée note 6) (ota! for ORD ARO. Total $47,034 Note 6 - VeeLo NextGen purchases can be cambined to receive a lower quantity discount price. 1.2.2 MDW Spares Figure 4 outlines the recommended Spares. Figure 4 MDW Spares Pricing item [Qty [Name Description Unit Price _] Price Delivery 1}} 1 |Display Processor [Preloaded Spare CPU for the Display |$ 5,000 1 $ §,000 |26 weeks CPU Processor, Does not include SW ARO license. 2), 3 }VeeLo NextGen Represents 5% of the 50 VeeLototal [$2,226 1$ 6,678 |90 Days (see note 7) for MDW ARO Total $11,678 Note 7 - VeeLo NextGen purchases can be combined to receive a lower quantity discount price ¢ Have required spares on-site ¢ Generate a Memorandum of Agreement with the EAA for the use of the ASDE-X Data. Please refer to the FAA Document; Airport Surveillance Detection Equipment ~ Model X (ASDE-X) Data Distribution (DD) System Ciuidance Document, May 29, 2007. 3.4.3 FAA'S Resoonsibi © Maintenance of the Data Distribution Cabinet once ownership is transferred to the FAA. * Approval of the Memorandum of Agreement between the DOA and the FAA. 3.2 Display Processor and ATC Display Upgrade The work scope and responsibilities are defined by the three major stakcholders: Sensis, the DOA, and the FAA. Semote Displays allow other airport users to view the Airport stakeholders can now benefit ame roabime waltic information that was once limited from Mis oa jeanne rrette i '9 the Air Traitic Control Tower intormation that air traffic controllers ala a ire are seeing as part of ASDE-X. Through OD, users can now receive a display that allows them to view delay- free traffic information unfolding on the movement areas of the airport Remote Displays provide the Human Machine Interface (HMI) function of the system, which provides users with a 7 > full-color, high-bright display and tae. ad clearly identifies ail targets with their associated Flight Identification (ID) in a single integrated picture. 3.2.4 sis Raspensioilities * Configure the Display Processors at Sensis (2 for MDW and 2 for ORD) © Ship the Units to the DOA specified locations weeTUs tS isis Proprietary Dats ¢ Come on-site for final configuration and traming once the displays are installed aitie OOA'S Sespensi * Power * Communications from the Data Distribution Cabinet to the Displays ¢ Installation of the Display Processors and the ATC Displays. Trackball, and keyboard. ¢ Inthe event of a failure, the DOA will remove and replace with a spare or from a repaired unit. 3.2.3 FAA's Responsibilities « None 3.3. Veelo NextGen The work scope and responsibilities are detined by the three major stakcholders: Sensis, the DOA, and the FAA. Sensis’ latest understanding from the FAA is that FAA will issue up to 200 Mode-S codes per airport and allow only 50 active in the movement area at atime. The FAA has also suggested some flexibitity in those restrictions. The Sensis VeeLo™ is a Mode S based vehicle locator that enables tracking and positive identification of surface vehicles at airports. Compliant with the RTCA DO- 260A MOPS for an ADS-B system operating on 1090 MHz frequency, these q | units tansmit ADS-B messages to allow for seamless integration with the MDS infrastructure. These units can be permanently or temporarily mounted and configured for use by airport personnel.  ¢ Obtain blocks of Mode-S Codes from the FAA ¢ Configuration of the Veelos for each airport ¢ Installation of the Units on the Vehicles 3 A’s Responsibilities we * Issue Mode-S Codes for MDW and ORD Physical Characteristics 4.4 Data Distribution Cabinet : : ania 08 a) ; Wea 1 24x29x72 329 Primary Circuit (estimated) 7.2A/120V Max 2.4A/120V (Steady State) Secondary Circuit 7.2A/120V Max 2.4A/120V (Steady State) Total 14.44 Max 4.84 (Steady State) Circuit C 20 A/120V (Convenience Outlet) 120 VAC; Ethernet hia a Figure 5 provides timeframes of key project milestones. Figure 5 Key Project Milestones Schedule 4} MOU Process Begins < 1 Week ARO 2) Request for Mode-S Codes <1 Week ARO 3) VeeLo Next Gen Ships 90 Days ARO: first availability is Sept 1, 2008 4) Mode-S Codes Received Before VeeLo Next Gen Configuration 5) Configure VeeLo Next Gens After VeeLo NextGen Arrives and Mode-S Codes Received 6) MOU Complete Before Installation 7) Site Survey and Project Kick-Off <4 Weeks ARO 8) Hardware Defivery * 26 Weeks ARO 9) Configuration and Training 27 Weeks ARO *. This date may be earlier depending on material lead times If the equipment is available before ASDE-X is available at MDW, Sensis will hold equipment at Sensis and ship/install at a mutually agreed upon time frame. Support and Warranty 3.1 Warranty Sensis warrants the products to be free from defects caused by faulty material or poor workmanship for a pertod of twelve (12) months from the date of delivery for hardware or for spares (if applicable), ninety (90) days for repairs and twelve (2) months from the date acceptance tor installed products. 8.2 Post Warranty Product Support Sensis recommends that Sensis and the DOA have a support contract in place where at the direction of the DOA, Sensis will perform work on behalf of the DOA at standard Sensis rates. (See Section 1.3.) 5.3. Recommended Spares and Maintenance S.24 Data Distribution The spares required by the FAA before the FAA takes ownership of the Data Distribution Cabinet are included in the delivery and installation of the Data Distribution Cabinet. 6.3.2 Display Processor and Hi Brite Displays Sensis recommends that the DOA purchase one additional M-Brite Display and one display processor CPU. Sce Section 1.2 for more information. In the unlikely event ofa failure the DOA would send the failed unit back to Sensis for evaluation and Sensis would prepare a quote for either repair or replacement. §.3.3 Lo NextGen Sensis recommends that the DOA purchase, as spares, approximately 5° of the total required VeeLo NextGens. See Section L.2 for more information. [n the unlikely event of a failure the DOA would send the failed unit back to Sensis for evaluation and Sensis would prepare a quote tor either repair or replacement. eliverables There are no deliverables beyond the equipment. qSensis is Proprichiry Lluaia ° 3  Terms ar A d Conditions of Sale 2 Terms and. conditions as mutually agreed by the parties. 14 AC 150/5220-xx CONTENTS CHAPTER 1. iNTRODUCTION. 100. BACKGROUND. 10k, EXPLANATION ¢ fo2. FUNCTIONAL DESCRIPTION, 13, OPERATIONAL ENVIRONMENT (Ost VTE CAPABILITY CATEGORE 105, VTE SUBSYSTEM FUNCTIONS i06, ADS-B DATA LINK STANDARDS 107, RLELATEDFREFERENCED READIN CHAPTER 2. VEHICLE TRACKING EQUIPMENT CERTIFICATION AND INSTALLATION APPROVAL PROCESS. 200. PROCESS OVERVIEV 20 A 202. 203 a 204. CONFIGURATIO 205 DEPLOYMENT PL 206. FLEE 207, VEHICLE TRAC KING FQt ([PMENT 208, ONSITE DOCUMENTATION 209. MAINTENANCE PROGRAM OMMISSIONING .. CHAPTER 3. PERFORMANCE AND TESTING SPECIFICATIONS FOR VEHICLE TRACKING EQUIPMENT. 300, GE NERAL Peete 301, OPERATING ENVIRONMENT ... 302. ADS-B DATA LINK. 303. GPS RECEIVER... . . 304. 1090 MHZ ADS-B TRANSMITTER AND RECE VAT ADS-B TRANSMITTER AND RECEIVER 306. OTHER RADIO DATA LINKS 307, OVERALL VTE SYSTEM PER 308, GENERAL DISPLAY FEATURES... CHAPTER 4. VEHICLE TRACKING EQUIPMENT MAINTENANCE AND OPERATING APPROVAL REQUIREMENTS ... 400, GENERAL se 407 DATABASE INFORMA] TON cl RR 402, PERIODIC RECERTIFICATION APPENDIX A. TITLE 14 CFR AND TITLE 47 CFR REFERENCES AND RELATED MATERIAL APPENDIX B. ADMINISTRATIVE INFORMATION... ' REQUESTS FOR INFORMATION. . 2 HOW CAN 1 OBTAIN THIS AND OTHER FA \ PL ‘BL Ic. ATION 3. SUBMISSION OF DATA : seine 4.0 CHANGES TO AN SPPROVED CONFIGURATION, Hi  AC 150/8220-xx CHAPTER 1. INTRODUCTION 100. BACKGROUND in an effort to reduce surface vehicle incursions on the airport movement area, various types of equipment can be used to minimize the frequency and severity of occurrences. lostalling such equipment on surface vehicles provides the vehicle operator with increased situational savarcness and enhameed safely and cfficieney. With position inlormation. vehicle operators and others will see where they ate on the Movement atea and, therefore, avoid incursions, 101. EXPLANATION OF TERMS The following definitions apply to this AC: a Airport movement area consists of airport runways and taxiways. b. Abnanac data tell the glubal positioning (GPS) receiver where each GPS satellite should be located throughout the day. Fach salellite fransmits almanac data showing orbital information tor all satellite in the system. «. Ephemeris data, constantly transmitted by each Satellite, contains the status of the salellile, along with current dale and time, This part of the GPS signal is essential to determine receiver position id. Non-movement area consists of the airerafi operational areas of the Surport other than the runways and laxiways. 102. FUNCTIONAL DESCRIPTION Several types of equipment are available to provide vehicle operators, pilots, and air tratfie contol (ATC) with the means to identify and tack surface vehicles more effectively. These include devices to broadeast a vehicle's location and to provide maps that show its position as well as that of other vehicles. ‘These devices can also display aircratl and the airport layout. User will determine the {ype of equipment to be used based on needs 103. OPERATIONAL ENVIRONMENT a. Geographic Transmission Limitations. Within an airport movement area, VTE should transmit vehicle Position, identitication, and other specific information, Upon leaving the aitport movement area, VTE should automatically inhibit its transmission. NOTE: This issue is stift under discussion and comments are welcome. One proposal is that transi: be allowed throughout the airport's aitside area, ion should b. Aeronautical Frequencies. VIE will operate on either one or both of the ADS-B data link systems (1090 MH<z Extended Squitter, 978 Miz Universal Access Transceiver) currently Approved for use nationwide [his <quipment is intended to operate with no more radiated puwwer than is required to function Properly. Therefore, iransmitter power is lo be adjustable. however. this adjustment should not be accessible to the vehicle operator, ‘Transmiter power adjustments are to be performed by maintenance Personnel responsible for the equipment Vquipment should also meet standard temperature, humidity, shock, and vibration requirements, e. Other Frequencies, VTE may operate on non-aeronautical frequencies in addition fo one or hoth aeronautical frequencies. Such operations may support non-ADS-B applications and users not specifivally addressed herein. These operations cannot have un adverse Impact on the National Airspace System (NAS) Ws. VTE CAPABILITY CATEGORIES The FAA and industry have defined the following four cilegories Of vehicle tracking equipment: a) situation display with own position: by broadcast of vehicle Position. ¢} situation display with own Position dad broadcast of vehicle position: und d) situation display of own position, broade: infernsiten. Chis information is stammiarized in the following lable: Cot vehicle position, and recepuon of iraitic  AG 150/5220-xx CHAPTER 2. CERTIFICATION AND INSTALLATION APPROVAL PROCESS 200, PROCE SS OVERVIEW To provide confidence that the VEE will perform properly, the FAA has defined a three-part certification and commissioning process. a. Manufacturer Responsibility. The inanufacturer should provide the FAA with the test data and other documentation to demonstrate that the VTE meets the minimum standards of this AC. The FAA reserves the Tight to witness testing and examine raw data, Upon review of test data and s: tisfactory completion of ail requirements set forth in this document, the FAA may grant approval to the specific equipment documented in the request, b. Airport Authority Responsibility. When VTE is to be installed, the Aitport Authority should closely coordinate plans with ihe FAA regional Airway Facilities Office, ¢. Airport Tenant Responsibi the FAA regional Airway Facilities When an airport tenant plans to install VTE, they should coordinate with tee, d. FAA Responsibility. (1) Commissioning. After VTE is installed on site, FAA Airway Facilities will conduct a commissioning inspection (o verity that the equipment is installed and operating properly and that the airport has the resources to maintain the system in proper operating condition (par. 206, tleet commissioning, and par 207, vehicle commissioning. of this AC). This process must be successfully completed for VTE to be commissioned by the E44 and authorized for use. (2) Periodic System Recertification. The FAA and other techmeal representatives mav make periodic 8 fo the airpuct Lo verify that the system continues to operate correctly. Guidance for these visits may be found in Chapter 4 of this AC, 20L. MANUFACTURER SUBMITTALS FOR CERTIFIC ATION a. Three Submittals, The FAA grants VTE cerlitication after review and approval of three submittals trom the manufacturer, (U) Requests for certification should be sent to the FAA Solutions Development Division al the address, listed in Appendix B. paragraph 3. (2) The first submittal consist of test procedures and dala sheets that demonstrate that the proposed VTE meels the minimum hardware und sottware standards of this AC. ‘This submittal should include a matrix, showing cach specific minimum standard from this AC, cross-referenced to. the specific lecation (paragraph, page, ete.) within the manufacturer's submittal where the mininwim standard has been ad (3) The second submittal should consist of training and maintenance documents intended to support the vehicle tacking system owner. (4) The third submittal should consist of a configuration control plan that identifies the components and aplions approved for use with the system. 202. TEST PROGRAM a Chapter 3 of this AC’ contains the minimum performance and testing stindards for VEEL The manufacturer should demonstrate compliance wiih these minimum standards through pertormance testing: {where a test 13 specified) or by analysis and inspection, “The manufacturer provides all necessary equipment ind hears ull testing costs b. Prior to performing tests. the manuracturer should propase a test plan to the PAA containing detailed procedures for conducting the tests. as well as the game and localien of the sility where the tesis are to he conducted. Prior FAA review of the fest plan should minimize the fikelihood of improper test procedures that might result in reyection uf the data AG 150/5220-xx ¢. It is the responsibility of the manufacturer to provide credible test data to the FAA that is based on (ict, and representative of the equipment being certified. Subynissions should include all data collected during a test, Dats should not be omitted be Falls outside of the recommended acceptable liamts of the ACL Afi completion of the tests, the manufacturer should teduce the data to an easily understood format to demonstrate conformity with this AC. 203. SYST 1 DOCUMENTATION a. Submission of Draft Documents, The manufacturer should submit three copies of the draft documentation described in this paragraph lo the FAA for review and approval. The System Description Manual, Maintenance Manual, Installation and Checkout Manual, Operating Instructions Manual, Training Program, and the Periodic yetem Recertification Plan should be Provided as separate manuals. These documents are intended to assist the VTE owner in installing, operating. and maintaining the system. The items may be cross-referenced to avoid duplication, but the elements of each document should be clear. (For example, the maintenance procedures that are performed durmg the periodic system recertification should be explicitly referenced.) b. System Description Manual ‘The system description manual identifies and catalogs the hardware components to the tevel of the smallest tield-replaceable module and describes computer sofiware. The principles of system operation are described using schematics, block diagrams, and How diagrams. For Peripheral devices, the performance parameters are included along with the name and address of the original manutacturer. NOTE: Spevilically who uses this document and for what purposes? © Manufacturer's Maintenance Manual. The manufacturer's Maintenance Manual should contain Maintenance information and procedures for use by maintenance personnel to ensure reliable and accurate performance over the life of the equipments. As a minimum, the program should define all maintenance action et Gre lequired and a reconimiended flequeney (eg, quarterly, annually, biennially) for each operation. ‘The following topics shoutd be addressed in the Maintenance Manual: (0) Maintenance Procedures. ‘The manual should contain a step-by-step procedure for cach scheduled (1.c., periodic) and unscheduled (‘.e., repair) mainienance operation. It should discuss calibration methods, voubleshooting procedures, suggested spare parts, and identify wil test equipment required. This document should aiso include the detailed procedures (eg., the keystrokes) the maintenance technician follows when using (he operator terminal to perform maintenance ona piece of VTE. Note: At the time this AC is being developed, there are no FAA certified Stations for the repair of VTE. Maintenance manuals and procedures, should distinguish between what tasks can be done by local maintenance personnel and what tasks must be done by others such as the manufueturec’s own personnel, [E VTE components are to be shipped tor repair, the manutacturer should address how and when this should be done. The manufacturer should also dev elop a list of spare components that are expected to be needed to maintain continuity of service while repairs are underway. Maintenance manuals and procedures should address who is responsible for the various components of a vehicle tacking system. In some cases, we suspect that maintenance responsibilities may be split among the airport authority, an airline corporation, and the E AA, @) System Performance Parameters, The manual should contain a complete fisting of the test points, Sensor outputs, waveforms, and other paranreters that indicate system performance that ma be measured in the field. If these quantities are tield adjustable, then an initial value (for use during inidal ceruticstion) and an operating tolerance (for use during periodic recertification) should be given. The key system parameters should also be identified ~ those values that best indicate svstem performance and need to be checked most Frequently. The frequency of scheduled maintenance acuions (2... weukiy, monthly, innuatly, etc.) should alse be given. d. lustaltation and Checkout Manual. This decument should thoroughly deseribe the installation aod eckeut procedures to be followed by the technician at the installation site, Installation instructions should inckide details on the proper mounting of the equipment and include details on any areas that could adversely affect system performance fe g. installing component in close proximity lo the engine or another source of possible extreme heat) e. Operating [astrections Manual (Le. a Lser Handbook). This document should provide detailed iMetructions for an equipment operator to use the syatem, AC 150/5220-xx and identity are being broadeast aecuratel data do so uecurately Verily that equipment displaymg received broadcast position nd without any duplicate targets, (2) Data Broadcast (while the vehicle is in motion), VT): should be tested in motion while installed on the vehicle that the equipment will normally be used with, VTE that is not permanently mounted on a vehicle fe.g., equipment available for transient contractors working on the airport movement area) should be tested using a vehicle similar to the vehicle ihat could realistically be operated with the equipment, ta) Move the vehicle and ensure the sysiem is transmitting position, heading, velocity, and identity information per the requirements of euch installed ADS-[3 dats link system {b) Drive the vehicle around and offen the ‘port movement area and verify that VEE operates Properly (c.g.. does position broadcast properly, does map show position properly, does tansinission stop and start as necessary} using the specitications contained in Chapter 3 of this AC and the Maautucturer’s Maintenance Manual, as discussed in paragraph 203.¢.(2). (3) Database Current. Verify that procedures are in place to receive current database information from in approved source per that source's update cycle and to install the mose current indormation on ail applicable vehicles, 208. ONSITE DOCUMENTATION, he equipment operator should maintain the following documentation. It should contain all pertinent onsite documentation and is to be maintained and kept at the ait port The FAA will review the documentation at the commissioning inspection, ertification. The onsite documentation should include a copy of the FAA letter to the manufacturer granting certification for ihe VTE Conification letters are to be availuble for the ty pes of VTE in use at the suport. Altemately, a list of equipment thal has been certificated by the FAA may be used to satisfy this requirement. 6. Liceuse Information. The unsite documentation should include the fleet’s FCC-issued license for operation on the installed frequencies and a current record of the identity of cach vehicle lo which the license upplies. If the user has chosen to maintain individual station licenses for each vehicle (as opposed to a fleet heense) the user should still maintain a current record of the identity of each licensed vehicle. ¢. Manufacturer’s Documentation. The onsite documentation should include copies of the VTE System Description Manual, Manufieturer’s Maintenance Manual, and Operating fustructions Manual. When changes are made to these documents, the manulacturer should forward revisions to the VTE oy ner, d. Operatioual Procedures. ‘he equipment owner should develop the operational procedures that set forth mandatory site procedures tor both routine and aonscheduled situations in the onsite docurneniation. “These Procedures may incorporate appropriate sections of the manufacturer's manuals, The tollowing items should be addressed: (1) Physical security of equipment, @) Maintenance and operations by authorized persons. including who should be notified if an eyuipment specification is discovered out of tolerance or other maintenance is necessary {3) Keeping of equipment maintenance fogs and other techmeal Teports, {4} Procedures io determine whether a database is current and how to update the database when necessary, {5) Procedures for conducting periodic scheduled maintenance, {6) Procedures for amending or revisiag the operational procedures, (7) Procedures to be followed to freeze the vehicle tracking data in an archive file tor a specitied penod betore and atier the time of a vehicle accident or incursion, and the procedures to be followed to teve these dati. These procedures should describe the responsibility for accomplishing these actions hey should be aitomatically accomplished in the event of an devident, incident, or upon the request ola ber of the FAA, 2 This issue is still under discussion, AC 150/5220-xx (8) List of vehicle tracking equipment on the airport. This list includes the following information: (2) Modet and serial number of all VTE (b) Routine inspection of equipment lo be performed. (cr Record of license expiration dates for alt equipnient requiring a ticense, (9) A Memorandum of Agreement (MOA) signed by the owner and the FAA Airway Facilities Office, This Memorandum should state that the owner agrees lo maintain, repair, and modify the VCE in accordance with the minimum requirements, standards or criteria governing VTE, The owner understands that noncompliance with the specific site's EAA/Sponsor MOA tuay result in the VTE"s removal from service or decommissioning, OTE This issue is up for discussion. 209. MAINTENANCE PROGRAM Phe user should establish a maintenance Program with properly trained personnel who meet all FCC and FAA Fequirements, adequate test equipment, and resources to (uf the manutucturer’s recommended scheduled inaintenance and calibration procedures defined in the Maiglenance Manual. The maintenance program is the owner's tesponsibility, but can only be performed by a Person meeting FAA and FCC requirements, The FAA will issue 4 verification authority letter to a person who meets FAA and FCC Mmamtcnance requirements. a. Maintenance Personnel. The owner should show that the maintenance program adopted has qualified petsonnel available (0 maintain the VLE. The personnel should have completed the manufacturer's training Program or an FAA-approved exam. They should be able to demonstrate Proficiency in accomplishing the required maintenance procedures and using the specialized test equipment. The FAA will issue an unrestricted BAA verification authority letter to the candidate maintenance person if he/she is able to meet the concepts and performance requirements of the VIF and has a FCC 3 assuciited transmuter, H rediowlephone ticense for maintenance of the b. Test Equipment. Prior to the time of commissioning, the owner should have available at the facility all ‘est equipment required by the approved maintenance plan tor maintenance and calibration of VTE. The owner should have available test equipment that is capable of avcumately measuring the appropriate technical standards and tolerances necded for facility verification” Test eqlupment requiring calibration should be calibrated in accordance with the schedule submitted to (and approved by) the FAA during certification. In case an acceptable lest equipment calibration sebedule was not included and equipment requires calibration, test equipment will be calibrated as per the test equipment manufacluter's recommendations or the FA A,Sponsor MOA/OMM. Test equipment should be traceable to national stindards, and proot of required calibration (e m. a current calibration sticker) should accompany each piece of test equipment when it is being used. Aner commissioning, the test equipment should be available when required for scheduled 5) calibration or for repairs afier system finlure tem maintenance and & Periodic System Recertification Plan, The owner should plan for complying with the manutucturer's "seammended procedure for periodic system recertilication (pi ‘graphs 2031, and Chapter 4). ‘This phan should include a list of the procedures to be tollowed during the recertification and the source of the qualified person to conduet the inspection, AC 150/5220-xx CHAPTER 3. PERFORMANCE AND TESTING SPECIFICATIONS 300. GENERAL, a, System Components. For descriptive Purposes the system is sepatated into four main components. The components are as follows: (1) GPS Receiver (2) Map Display (3) Pransmitter (4) Receiver implied that the components will be brought together by one or more computers and that the entire system uceds to be tested. bo ication of Components. One or more of these components can be combined to farm a system. The following requirements will define the minimum standards the components will be required to meet. For certification the system will only have to meet the requirements of the components in that system. For example: Certification of a Category 2 system would require consideration of only the GPS receiver. the GPS antenna, the L090 MHz and/or UAT transmitter. and the transmitter’s antenna. NOTE: The goat is to indicate that the system will be made of a combination of these tour components. [tis ¢. Manufacturer's Responsibility. Some of the requirements may not have a specific test listed. It is still required that functionality be demonstrated betore the device is vertified. [Lis up to the manufacturer to develop tests and provide testing documentation that satisfies the certitication official, d. Transmitter Performance. This is fi fy defined ht the Sppropriite RTCA documents, 1BO-260A for 1000 Miz ADS-B and DO-282 for U AT ADS-B. The manufacturer will be required to obtain an ECC license for manulacture and use of these transmitters, At the time of the writing of this document the oulput power is being limited to 20 Watts for a 1090 MHz transmitter. As further testing and simulation are performed this power limitation may be modified within this AC. The FAA radio spectrum group has stated that the allowed (ransmission power must be less then what is currently specified in the RTCA DO-260A and DO. 2424, Minimum Aviation Sysiem Performance Standards For Automatic Dependent Surveillance Broadeast (AD! B), MASPS document. & Displays Goals. There are two major goals that a display is expected to weet, (1) The display must represent information clearly and un-ambiguously. The display should be easy to understand. (2) The display must have certain standardized features. Lt is important that the displays made by alt manufacturers display certain information, such ¢ lacget display, using the same symbology and colors Since it is likely that some of the ychicle drivers will be pilots, it is Important that information displayed in the vehicle look the same as 4 pilot would see in a cockpit, This standardization of the displays is to prevent 4 potential safety problem. [Fa pilot traitied to use his aireratt display is dris ing a vehicle that uses symbols similar to whal the pilot sees in his cockpit display but they are different in color or meaning. an accident could result NOTE: A problem can occur at airports with roads that ge uoder runways. A pilot in an airplane vould see a vehicle heading straight for a nmway and net know if the vehicle will be going through a tunnel ot actoss the tunway surface. This may require changes to airborne systems clisplay of ground maps, The problem is complex and needs to be addressed in greater detail in this AC. We solicit Advice from the aviation community on how thts should be done, 301, OPERATING ENV IRONMENT NOTE: Aiter much research, it was found that SAK 1455 Joint Society of Automotive engineers (SAE) Technical Maoagement Council (TMC) Recommended Environrentat Pra Nees for Elecironic Fquipment Design (Heavy Duty Trucks) is a aood standard base tor all env ronmental tes The tests a system will require will he differcer ‘pending on where itis will be placed invon the vehicle, ‘The manufacturer decides which environmental tests are te he conducted based on where they mtend their sysiem tw be placed on. in the vehicle, For example, different tests AC 150/5220-xx a, Performance Standard. 1) RTCA Standards. Must follow RTCA DO-260A, except as stated in this document. Ay of publication of this document the following restrictions have been placed on a 1050 MHz transmitter und inay change in the future: (a) Operations are timited to the atrport movement area. Transmissions must cs feaves the airport movement area, Note: This topic is still under dis that (ransniission should be allowed throughout the aiport’s airside area, {b}) Transmissions must be in accordance with 1090 MHz ADS-B MOPS (RTCA DO-260.4) aNe once the vehicle sion. One proposal suggests (c) The etfective radiated power of transmissions is limited (o 20 watts. NOTE: The current 1090 MOPS and FCCEAA rules disagree on output power and FCCVEAA rales musi supercede the MOPS. (d) Installation uf 1090 NMOtz fransmilters are cantined (o these vehicles that have a need to be on the funway movement area (4 snowplows, emergency response vehicles, maintenance vehicles), Installation of 1090 Mblz uansmitters on vehicles in the Tarp areas such as baggage carts and catering irucks iy not authorized. {e) Frequency Transmit Authorizations are obtained for the airports that testing is desired, (f) Action is initiated through the FAA Office of Specirum Policy and Management (ASR) to obtain Spectruin certification for the 1090 Mz, transmitters, (2) Environment. The transmitter and receiver must be tested to show it will maintain DO-2604. specifications in the environment it will be installed. This eny iconment will be defined by the manuf 1 sing stanckied methods as outlined fat iis document or the equivalent, ee Contiguration management sections need to be wrilten to address ihe issues of system component pkicement in vehicles to ensure the system is not placed in an area of a vehicle that has environmental exiremes outside what the system component is designed to handle. (3) Unique Vehicte Identification. The International Civil Aviation Organization (ICAO) Mode Select (Mode S) address will be used as the VTE electronic identifi ation. See FAA Order WA $200. xx for instructions on how to obtain such an identification, wh Transmitting Boundaries The transmitter must Slop transmitling when outside the Urport novement This area will be predefined by maps available from the FAA, (lysteresis must be included so that the system will not constantly switch on and off when near a boundary. [is known that a GPS may uritt and a vehicle parked on the boundary line may have its Pusition move cnough fo cause the transmitter to randomly switch on and o NOTE: {he issue of how to handle hysteresis will need farther discussion. The extent of the problem needs to be exammed, There can be unique problems und solutions depending upon the airport in which this system is instilled, Some of the potential problems are: (1) vehicle parked next to a fence, (2) a vehicle driving along the edge on a Perimeter road and (3) a vehicle approaching the movement area are urthogonat to the line. b. Performance Testing, (2) RTCA Standards. Must follow RICA-DO 260A lest procedures except as stated in this ACL Transmitter ouput power must not exceed the standard set by this AC (2) Environmental conditions. ‘The system must be tested for the environmental extrem : as required for intended place of instatlatien (3) Unique Vehicle Identification. System must comply with FAA Order WA S200.4x. 4 Criteria - Mode S$ Codes for Attport Surface Vehicle. Obstractions, Skydis ers und parachutists, signment 44) Transmitting Boundaries, {t must be demonstrated that the tcansmitter will sutomatically cease fmiasmilting when the position is outside the detined ANPOIT movement urea. [t rust also be sbown that a swsten oa the border of the altpocl mos ement area will not cause The transmitter to randomly tara on and atfas the GES position sitters around, AC 150/5220-xx 305. UAE ADS-B TRANSMITTER AND RECEIVER The LAT transmitter and receiver are defined completely in DO-282 with exception to environmental testing and vutpal power. The receiver will need to be tested or used on Category 4 systems, 4. Performance Standard. (0 RTCA Standards, Must follow RTCA DO-282 except as stated in this AC. (a) Operations are limited to the rubway movement area of the airport. Transmissions must cease ance the vehicle leaves the airport movement area. Note: ‘this issue is still under discussion. @) Environment. ‘fhe transmitler and receiver must be tested to show it will maintain DO 282 specifications in the environment it will be installed, This environment will be defined by the manuf: using standard methods :is outlined in this document or the equivalent. CLULeE, NOTE: Configuration Management sections need to be written to address the issues of system component placement in vehicles ty ensure the system is net placed in an urea of a vehicle that has environmental extremes outside what he system component is designed to handle (3) Unique Vehicte Identification, The [CAO Mode S address will be used as the VTE electronic identification. See FAA Order WA $200.xx for fnstructions on how to ebtain such an identification, (4) Transmitting Boundaries, The transmitter must stop fmansmitting when outside the airport movement area, This area will be predefined by maps available from the FAA. Hysteresis must be ineluded so that the system will not constantly switch on and off when near a boundary. (We known that a GPS may drift and a vehicle parked on the boundai y line may have its position move enough to cause the transmitter to randomly switch on and off.) NOTE: The issue of how to handle hystetsis will need further discussion, The extent of the problem needs to be examined. There can he unique problems and solutinns depending upon the airport in which this system fy installed. Some of the potential problems are: (1) a vehicle parked next to a fence. (2) a vehicle driving along the edye of a perimeter road and (3) a vehicle approaching the movement area are orlhogonal to the line, b. Performance Testing. () RTCA Standards. Must follow RTCA 00-282 test procedures except as stated in this document. @) Environmental conditions, The system must be tested for the environmental extremes as required for intended place of installation. () Unique Vehicle Identification. System must comply with FAA Order WA 3200.xx for assignment of Mode $ codes lor each vehicie. (4) Transmitting Boundaries. [t must be demonstrated that the transmitter will aulomatically cease transmitting when the position is outside the defined Alport movement area. UW must also be shown that a system on the border of the airport movement area will not cause the transmitter to tandomly tum on and otf as the GPS position jitters around. 306. OTHER RADIO DATA LINKS Ifthe manulaetrer develops # system based on a data fink other then the lwo listed in this AC then it will be up to the manufacturer to yain approvals for use. This approval will require full documentation of the systems operation and a full test suite to prove it works as it was designed, The system imust be documented and demonstrated to show it will not have a negative Impact to the NAS system, 307, OVERALL VTE SYSTEM PERFORMANCE a. Performance Standard. (0 Start Up Time. The sysiein should be fully functional in 1S seconds from a power off condition. Phe system is allowed to take an average of 45 seconds to be fully Fuoctional when the GPS js deing a cold stark, {2} Internal Recording. Systems that display targets should implement recording ystent for diagnostics and testing, The recorded data should have an accurate time stamp o aid data analysis. Recommended data to record would include: AC 150/5220-xx (a) Unprocessed target intormation, (b) Processed target information from the tracking algorithm. (c) System state data such as position, velocity, display settings, ete. (d) The recording system could be included within the system or be a separate device connected to the o¥stem, (3) Filtering and Shielding. The system should be shielded commumeations (reler (6 AC 20-138 tor additional details), (4) Transient Power. ‘The system should be able to recognize power problems, {t should be able to vonunue cunning without restart when high current devices may cause the voltage to briefly drop below or Jump above normal operating levels. The system should not be allowed te enter a non-functioning state because of a transient power problem. If the system is unabje to maintain Proper operation then the system should automatically reset itselt to return to Proper operation with no operator intervention. wtinsl_ very high lrequency (VHE) b. Performance Testing. (1) Start Up Time. Tum syslem on and measure amount of time until the system is fully operational, Q) Internal Recording. Che system should be given a large. known quantity of targets for a long duration of time. The recorder should accurately represent what is input into the system, NOVE: The following is from DO-220C and is slightly rewritten to fit the vehicle application, This is a copy of the test from the GPS section and was copied to here more as a placehoider until we give more thought on the Proper approach to this type of test, Comments gladly accepted on this subject. (3) Filtering and Shielding. The system should be installed in a vehicle to complete this test. The GPS should be in a WAAS corrected full navigation mode. { sing both a handheld radio and a nommaily installed vehicle mounted radio tune each nidio to each of ihe fisted frequencies and wansmit tor a period of 20 seconds. The individually received satellite signals should not degrade below a point where they cannot be used to find a position. The handheld and vehicle mounted radios are specified because both are commonly found at airports. The following VHF frequencies will be used: (ay F2L150 MHz (b) 121.175 MHz {c) 121.200 Milz (d) 131.250 MHz MEIiz (8 131.300 MHz (4) Transient Power. The system should be given voltage bigher and lower than the specitied limits The system should be able to handle these. For ihe case oF a power extreme show that the system is automatically reset with no tlerruption ty the operator. The system should not enter a slate w here it stops operating normally and does not reset or indicate a problem to the operittor, 308. GENERAL DISPLAY FEATURES The minimum standards defined in this Palagraph are intended to keep cerlain features of the display uniforn between manutucturers, For safely reasons these minimum Standards are also the same ag will be used on aiterait Inounted displays. We intend to keep the hasie display ed informnation similar between all systeniy used in the NAS system. Manulzeuyers sbould aveid using contleting sy inbology that ight inerease the possibility of an accident The symbols used to display traffic are the same as what will be used on an aiteraft und devianon trom these syanbols § not recommended. An example of a moving map is shown in Figure 1, 4. Performance Standard. (1) Failure Indication. The systvur should have separate indivators clearly showing the vehicle operator that the device is tiled, Chis display wust be in the operator's field of view while opening the vehicle ‘The failure indicator should alse indicate which module has filed Such as transimitter, GPS, receiver, ete ifthe system bas a imap display, 2 clear indication of the failure should be shown on the chsplay. A failure la AC 150/5220-xx G4) Cyan. The color cyan is detined by green und blue intensity being OXF (full intensity mlensity will be between 0x00 and O80 (35) Red. The color red is detined by having no green or blue intensity Performance esting. (0) Display should be checked for clutter. (2) Displa y should be checked for coloring to prevent objects from blending with each other, (3) All features should be tested for tanction, (4) Table t and Table 2 should be filled oul. These tables correspond io requirements nutnhered 4. and red -35, i9 AC 150/5220-xx fable 1. Human Factors Checklist: L ability | dT Evaluation Criteria Pass Pass/exception Fail Display Information oT |. Display range indication is clear and displayed at all limes. 2. Auto-range on/off is clearly indicated, 3. Map orientation js clearly indicated, Current position is clearly indicated in pan mode. 5. Textual information is easily readable. 6. Failure indicators are clear and obvious, 7 Own position is drawn on lop of all other displayed data, 8. Display range can go to at feast five nautical miles. Moving Map L. Display of cach map feature is unique, | 2, Labeling is casily readable 3 Display is not cluttered at any ranue. 4. For Category 4 only: display is not cluttered with 20 ' targets distributed evenly within one nautical mile ; 3. Displayed data is less than one second old, 6. The default display is in track up. 7. User caa easily change displayed range. , 8. Pan tunction (if implemented) can be cancelled in two button presses or less. 9. All the symbols have an appropriate color in all lighting | conditions, : i | Controls [1 Controls provide adequate feedback, | 12. Controts do not obscure display | [ 3. Control tabeling is easily readable | | WwW AC 150/5220-xx Fable 2. Human Factors Checklist: Brightness Evaluation Criteria ! Dark Conditions | | I |. Brightness adjustments acceptable, 2. Colors clearly distinguishable. | | | { | t | | 3. Fext is readuble front 30 inches, | 1. Target symbols are distinguishable, Lt a Se ee | tnuiceet Conditions I | | 1. Brightness adjustments acceptable. 12. Colors clearly distinguishable. | 3. Text is readable from 30 inches. | [4 Target symbols are distinguishable, [—————__ — | Bright Light | 1. Brightness adjustments acceptable, Colors clearly distinguishable Teat is readable irom 30 inches, | + Reflection causes no interterence. Target symbols are distinguishable, AC 150/5220-xx c. Mandatory Configuration Changes. If a detect is found in data transmitted from a vehicle tea king system VTS, then the Mmanuiacturer should be notified and the system manufacturer should issue a mandatory service bulletin, to owners of similar systems, requiring removal af the sys ems found (o contain the error from, Servive pending repair, {f the manufacturer has a validated repair procedure, the procedure coud be included in the same service bulletin, Otherwise, the repair procedure would be in a subsequent ser ice bulletin. dd. Revoking Approval. Product approval may be revoked {or uperation at an individual airport may be suspended) iff ()) Vatid performance of the operating system cannot be certified, Q) Changes are made to eilher the software or hardware without FAA approval. (3) 1 (4) The certify ing official detects other problems with the systera that would Significantly system performance, Nsmitted data does not conform to upplicable standards e. Unacceptable Failure Rate. The FAA will temove equipment that Proves uoreliable from the listing of certificated equipment. The determination of unreliability should be based on Judgment and experience with similar equipment, C1) Where equipment is determined to have an unsutist fory failure rate or is deficient in workmanship or materials, the FAA will notify the manufacturer in writing as to the basis for this determination, The manufacturer should then nouty the FAA in writing as te its plan of action for resolving the issue. [f the manufacturer dues not resolve the problem within a reasonable time (the timeframe would, of necessity, be based on safety considerations and the nature of the problem), the eytupment would be removed from the list of certificated equipment @) The FAA reserves the right to require the “uipment to under go any or all qualifcanon‘ealibration tests when the equipment has been determined unteliable or deficient in design, materials, or workmanship. (3) The manufacturers must noti Y owners of similar VTE of any problems uncovered during their ‘testing through the configuration control procedure disvussed in paragraphs 204 and 40%. (4) Failure to meet the criteria of this program may result in decommissioning the VIE syslem and withdrawal of the broadcast frequency authonzation, AC 150/5220-xx Appendix A. TITLE 14 CFR and TITLE 47 CFR REFERENCES AND RELATED MATERIAL 2000 CFR Title 47, Chapter 1, Part 87, Section 18, Telecommunication A tion Services. See. 87.18 Station license required, (a) Except as noted in paragraph (b) of this Section, stations in the aviation service must be licensed by the FOC either tadividually or by fleet (b) An aircratt station is licensed by rule and does not necd an indivi Aircraft station is not required by statute, treaty, or agreement to which the United States is Signatory to carry a radio, and the aircraft station does fot make international flights or communications Even though an indis idual license is bot required, an aireratt station licensed by rule must he operated in accordance with all applicable operating requirements, procedures, and technical specifications found in this par. dual license issued by the FCC if the NOTE: This AC addresses equipment to be installed in ‘urport surface vehicles, not “urcratt stations” (i.e, ‘ureraf). ‘Thus, paragraph (bb) does nut apply.  AC 160/5220-xx APPENDIX C. ACRONYMS AND ABBREVIATIONS AC advisory circular ADS-B Automatic Dependent Surveillance Broadcast AE FAA Airway Facilities AIP Airport Lmpros ement Program AND Office of Communications, Navigation, and Surveillance Systems ANI NAS Inplementation ARL FAA Office ot Runway Safety ARQ FAA Research & Requirements Development Directarate ASD FAA Office of System Architecture and Investment Analysis ASDE Atrport Surface Detection Equipment ASDE-X Auport Surface Detection Fyuipment Next Gieneration ASR FAA Office of Spectrum Policy and Management ATC air tratfie control ATCRBS Air Tratfic Control Radar Beavon System ATOV ‘mort trattic control tower ATP FAA Air Tratfie Planning and Procedures ATS PAA Air Trattic Service CDTI cockpit display of trafti information CRS certified repair station DO RTCA document “AA Federal Aviation Administration ECC Federal Communication Commission GPS Global Positioning System HAZMAT. hazardous material ICAO International Civil Aviation Organization tEC International Electrotechnical Commission IFR instrument flight riles [pss a TEC ingress protection rating for equipment and enclosures [PT Integrated product team MASBS MINIMUM i iation system performance standards MUz megahertz MOA meiorandum of agreement Mode S Mode Select MOPS inutium uperatiogal pectormance standards OEP Openitional Evokiion Plan PSR plimary surveillance radar 4 NAS R&D RGB RRGGBR RTCA SAE SF21 SMA SMR SSR TIS-B TMC UAT VER VUE vPD VTE VTS WAAS National Airspace System research and development red, ureen, bhie 4 formal for defining color Radio Technical Contnission for Aeronautics Society of Automotive Engineers Safe Hight 21 surface movement area surface movement radar secondary surveillance radar Frat Information Services - Broadcast Technology and Maintenance Council untversal access transceiver visual Hight rules very high trequeney vehicle‘pedestrian deviations vehicle tracking eqaipment vehicle tracking sy dem Wide Area Augmentation System Xerox WorkCentre Pro Network Scanning Confirmation Report a ROX 0 out of 1 filed successfully. 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