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i only need theReview Questions to be answered--------------------------------------------------------------------------------------------------------------------- Module title: 	5 Runway Design Standards Matrix – AAC, ADG, RDC, Visibility Minimums --------------------------------------------------------------------------------------------------------------------- Overview -Runway Design Standards Matrix -Summary -Review Questions Assignment -Browse the online references listed below. -Read and study this lesson plan provided by your professor. -Answer the lesson plan review questions in writing. -Create a document containing only the review questions with answers, preferably in MS Word. -Save the document with the file name “YourLastName LessonNumber LessonTitle”, e.g., Cain 5 runway design standards matrix. -Upload the document into the ePortfolio Assignment Digital Dropbox. Outcomes: After completing this module, students will be able to: 1. Define runway design aircraft. 2. Define AAC, ADG, and RDC. 3. Given an aircraft type, determine AAC, ADG, and RDC. 4. Given several aircraft types, determine the runway design aircraft. 5. Describe the visibility minimums (runway) variable to be used in the Runway Design Standards Matrix. 6. Given an instrument approach procedure chart, determine the visibility minimum category variable to be selected in the Runway Design Standards Matrix. References AC 150/5300-13 -Chapter 1 Introduction --105 Planning  12 --105e Approaches  -Chapter 2 Design Process --201 General  31 --202 Design aircraft  33 --205 Planned visibility minimums for instrument procedures  35 -Chapter 3 Runway Design  43 --301 Introduction  43 --302k Runway design standards 45 --320 Runway design requirements matrix  92 -Appendix 7 Runway Design Standards Matrix  269 --------------------------------------------------------------------------------------------------------------------- 5 Runway Design Standards Matrix - AAC, ADG, RDC, Visibility Minimums  --------------------------------------------------------------------------------------------------------------------- Overview -Introduction -Design aircraft  -Aircraft Approach Category AAC -Airplane Design Group ADG -Runway Design Code RDC -Visibility minimums Introduction -AC 150/5300-13A, Table 3-5 is an interactive Runway Design Standards Matrix that provides a useful organizational structure for studying runway design.  --Runway design --Runway protection --Runway separation -The Runway Design Standards Matrix can be used to easily and interactively determine many runway design standards and dimensions. --The entire AC 150/5300-13A Airport Design document (Website) should be downloaded and saved to your local computer. After the download is complete, then open your PDF document handler such as Adobe Reader. Then open the AC from within the PDF program, not the file explorer. If your computer opens a PDF document in a browser such as Internet Explorer, then the matrix may not function interactively. --If you cannot get the matrix to respond interactively, then you will have to use the manual look-up tables (Appendix 7). --Ask your instructor or fellow students for help if you cannot get the matrix to function interactively. -The Runway Design Standards Matrix will guide sequentially the next few course lessons. -The entering arguments/variables for this runway design standards matrix are in the top lines and consist of: -Aircraft Approach Category AAC -Airplane Design Group ADG -Runway Design Code RDC -Visibility minimums  Runway Design Code (RDC) -In this lesson, these four runway design standards matrix input variables will be studied. Critical design aircraft - runway -Critical Design Aircraft - Runway --Identifies the aircraft utilizing a runway that requires the largest dimensions such as runway length, width, parallel runway separation, and many other dimensions associated with runway safety. --Every runway does not have to accommodate every aircraft, i.e., there can be a different runway design aircraft for different runways. -Design Aircraft. An aircraft with (most demanding, typically largest) characteristics that determine the application of airport design standards for a specific runway. This aircraft can be a specific aircraft model or a composite of several aircraft using, expected, or intended to use the airport or part of the airport. (Also called “critical aircraft” or “critical design aircraft.”) Aircraft characteristics and related airport design components 	These Aircraft Characteristics  	Determine These Airport Dimensions 	Approach Speed  	Runway width, runway-to-taxiway separation  	Landing and Takeoff Distance  	Runway length  	Cockpit to Main Gear Distance (CMG)  	Fillet design, parking layout  	Main Gear Width (MGW)  	Taxiway width, fillet design  	Wingspan / Tail Height  	Taxiway-to-taxiway separation, runway to taxiway separation  -Airports must be designed to accommodate one or more specific aircraft expected to utilize the airport, i.e., the design aircraft. --There can be a different design aircraft for runways and taxiways/taxilanes. -Critical Design Aircraft - Runway --Identifies the aircraft utilizing a runway that requires the largest dimensions such as runway length, width, parallel runway separation, and many other dimensions associated with runway safety. --Every runway does not have to accommodate every aircraft, i.e., there can be a different runway design aircraft for different runways. -The procedure to determine the runway design aircraft for a particular runway is as follows. --Starting with the largest few aircraft using the runway, determine for each aircraft the: ---Aircraft Approach Category AAC ---Airplane Design Group ADG ---Runway Design Code (RDC) --The aircraft with the highest RDC is the design aircraft for that runway. Aircraft Approach Category (AAC). -Aircraft approach category (AAC). A grouping of aircraft based on aircraft approach speed, a reference landing speed (VREF), if specified, or if VREF is not specified, 1.3 times stall speed (VSO) at the maximum certificated landing weight. VREF, VSO, and the maximum certificated landing weight are those values as established for the aircraft by the certification authority of the country of registry. -VREF = approach/reference speed in landing configuration (e.g., landing gear down, flaps down) at maximum landing weight. --Examples: Airbus 320 	VREF = 136 knots Boeing 747-400ER 	VREF = 157 knots --See AC 150/5300-13A, Appendix 1, Table A1-1, Aircraft characteristics database – sorted by aircraft manufacturer. -Aircraft approach speeds are categorized in the following table. Table 1-1. Aircraft Approach Category (AAC) 	AAC 	VREF/Approach Speed  	A 	Approach speed less than 91 knots  	B 	Approach speed 91 knots or more but less than 121 knots  	C 	Approach speed 121 knots or more but less than 141 knots  	D 	Approach speed 141 knots or more but less than 166 knots  	E 	Approach speed 166 knots or more  -Examples: Aircraft	AAC Airbus 320 	C Boeing 747-400ER 	D -AC 150/5300-13A, Appendix 1, Table A1-1, Aircraft characteristics database – sorted by aircraft manufacturer, contains AACs for common aircraft. Airplane Design Group ADG -Airplane Design Group (ADG). A classification of aircraft based on wingspan and tail height.  -Wingspan. The maximum horizontal distance from one wingtip to the other wingtip, including the horizontal component of any extensions such as winglets or raked wingtips. -Tail height is not so obvious as a design runway factor. --An aircraft holding for takeoff or on a parallel taxiway near the landing runway represents an obstacle to a landing aircraft, especially if the landing aircraft needs to go around or abort the approach. The tail height affects the safety of the overflying aircraft. Tail height will affect the runway protection zones and areas to be discussed later. -Knowing tail height and wingspan, ADG is determined from Table 1-2. When the aircraft wingspan and tail height fall in different groups, the higher group is used. Table 1-2. Airplane Design Group (ADG) 	ADG Group # 	Tail Height (ft [m]) 	Wingspan (ft [m]) 	I

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