{"id":19895,"date":"2019-11-08T17:50:44","date_gmt":"2019-11-08T21:50:44","guid":{"rendered":"http:\/\/hartzellprop.com\/?p=19895"},"modified":"2019-12-02T11:03:05","modified_gmt":"2019-12-02T15:03:05","slug":"weight-and-balance-terms-to-know","status":"publish","type":"post","link":"https:\/\/hartzellprop.com\/weight-and-balance-terms-to-know\/","title":{"rendered":"Balancing Act: 10 Weight and Balance Terms to Know"},"content":{"rendered":"\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Understanding the weight and balance limits of your aircraft is critical to flight safety. Exceeding an aircraft\u2019s maximum weight limitations may damage the structure of the aircraft and lead to stability and performance issues. When considering weight and balance, pilots need to know more than <span style=\"mso-bidi-font-style: italic;\">how much<i> <\/i><\/span>an aircraft can carry; they should also calculate the proper distribution of that weight to balance the load.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Too much weight distributed too far forward in an aircraft may create a nose-heavy effect, while too much weight too far aft will cause a tail-heavy condition. For safe and stable flight, the onboard load needs to be in balance throughout the aircraft, similarly to how a playground see-saw needs to have equal weight on both ends to stay level. Before every flight, pilots must determine both the weight and balance to ensure the aircraft is within its specified limits.\u00a0<\/span><\/p>\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">To understand weight and balance calculations, be sure you\u2019re familiar with these <\/span><\/b><a href=\"https:\/\/www.faa.gov\/regulations_policies\/handbooks_manuals\/aviation\/media\/faa-h-8083-1.pdf\"><b><span style=\"font-size: 11.0pt; font-family: Arial;\">terms<\/span><\/b><\/a><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">:<\/span><\/b><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Center of gravity (CG) <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">is the mass center of the aircraft. If the aircraft were to be suspended from above by a wire, this is the point where it would balance perfectly. The CG must be located within specific limits for safe flight. CG is usually expressed in inches from a reference datum.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Datum (reference datum)<\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"> is an imaginary vertical plane or line from which all measurements of arm are taken. The datum is established by the manufacturer and stated in the Airplane Flight Manual (AFM) or Pilot\u2019s Operating Handbook (POH). <\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Arm (moment arm) <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">is the horizontal distance in inches from the reference datum line to the CG of an item. The algebraic sign is plus (+) if measured aft of the datum and minus (\u2013) if measured forward of the datum.<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Moment <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">is a force that causes an object to rotate. It is the product of the weight of an item multiplied by its arm and is measured in pound-inches (in-lb).\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">CG limits<\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"> are the specified forward and aft points within which the CG must be located during flight. These limitations are determined by the aircraft manufacturer and are specified in the AFM\/POH. <\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">CG range<\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"> is the distance between the forward and aft CG limits indicated on pertinent aircraft specifications.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Basic empty weight <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">refers to the standard empty weight of the aircraft plus the weight of any optional and special equipment installed on the aircraft.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Fuel load <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">includes only usable fuel, not the fuel required to fill the lines or the fuel that\u2019s trapped in the tank sumps.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Useful load <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">is total usable fuel, cargo, pilot, passengers, and drainable oil. To find this number, subtract the basic empty weight from the maximum allowable takeoff weight.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in 0in .0001pt .5in;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Payload <\/span><\/b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">refers to how much weight the aircraft can carry in addition to basic empty weight and fuel. This includes all occupants, bags, and cargo.\u00a0<\/span><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><b><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">There are several ways to calculate aircraft weight and balance, including using graphs, tables, and simple math. Here\u2019s how to use the computational method to run the numbers:<\/span><\/b><\/p>\n<p class=\"MsoNormal\"><span lang=\"EN\" style=\"mso-fareast-font-family: 'Times New Roman';\">\u00a0<\/span><\/p>\n<p style=\"text-indent: -.25in; mso-list: l0 level1 lfo1; tab-stops: list .5in; vertical-align: baseline; margin: 0in 0in .0001pt .5in;\"><!-- [if !supportLists]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"><span style=\"mso-list: Ignore;\">1.<span style=\"font: 7.0pt 'Times New Roman';\">\u00a0\u00a0\u00a0\u00a0 <\/span><\/span><\/span><!--[endif]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Refer to the AFM\/POH of your aircraft to find the basic empty weight of the aircraft. Then, list the weights of occupants, baggage, cargo, and fuel.\u00a0<\/span><\/p>\n<p style=\"text-indent: -.25in; mso-list: l0 level1 lfo1; tab-stops: list .5in; vertical-align: baseline; margin: 0in 0in .0001pt .5in;\"><!-- [if !supportLists]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"><span style=\"mso-list: Ignore;\">2.<span style=\"font: 7.0pt 'Times New Roman';\">\u00a0\u00a0\u00a0\u00a0 <\/span><\/span><\/span><!--[endif]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Find the moment for each weight listed by multiplying each weight by the arm (the horizontal distance from the reference datum).\u00a0<\/span><\/p>\n<p style=\"text-indent: -.25in; mso-list: l0 level1 lfo1; tab-stops: list .5in; vertical-align: baseline; margin: 0in 0in .0001pt .5in;\"><!-- [if !supportLists]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"><span style=\"mso-list: Ignore;\">3.<span style=\"font: 7.0pt 'Times New Roman';\">\u00a0\u00a0\u00a0\u00a0 <\/span><\/span><\/span><!--[endif]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Add all the weights together to find the gross weight. Then, add all the moments to find the total moment.\u00a0<\/span><\/p>\n<p style=\"text-indent: -.25in; mso-list: l0 level1 lfo1; tab-stops: list .5in; vertical-align: baseline; margin: 0in 0in .0001pt .5in;\"><!-- [if !supportLists]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"><span style=\"mso-list: Ignore;\">4.<span style=\"font: 7.0pt 'Times New Roman';\">\u00a0\u00a0\u00a0\u00a0 <\/span><\/span><\/span><!--[endif]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">Find the center of gravity by dividing the total moment by the gross weight.<\/span><\/p>\n<p style=\"text-indent: -.25in; mso-list: l0 level1 lfo1; tab-stops: list .5in; vertical-align: baseline; margin: 0in 0in .0001pt .5in;\"><!-- [if !supportLists]--><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\"><span style=\"mso-list: Ignore;\">5.<span style=\"font: 7.0pt 'Times New Roman';\">\u00a0\u00a0\u00a0\u00a0 <\/span><\/span><\/span><!--[endif]--><span 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Normal\";\n\tmso-tstyle-rowband-size:0;\n\tmso-tstyle-colband-size:0;\n\tmso-style-noshow:yes;\n\tmso-style-priority:99;\n\tmso-style-parent:\"\";\n\tmso-padding-alt:0in 5.4pt 0in 5.4pt;\n\tmso-para-margin:0in;\n\tmso-para-margin-bottom:.0001pt;\n\tline-height:115%;\n\tmso-pagination:widow-orphan;\n\tfont-size:11.0pt;\n\tfont-family:Arial;\n\tmso-ansi-language:EN;}\n<\/style>\n<![endif]--> <!--StartFragment--> <!--EndFragment--><\/p>\n<p style=\"margin: 0in; margin-bottom: .0001pt;\"><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">For more information on the basic principles of weight and balance calculation, refer to the <\/span><a href=\"https:\/\/www.faa.gov\/regulations_policies\/handbooks_manuals\/aviation\/media\/faa-h-8083-1.pdf\"><span style=\"font-size: 11.0pt; font-family: Arial; color: #1155cc;\">FAA\u2019s weight and balance handbook<\/span><\/a><span style=\"font-size: 11.0pt; font-family: Arial; color: black;\">.\u00a0\u00a0<\/span><\/p>\n","protected":false},"excerpt":{"rendered":"<p>Understanding the weight and balance limits of your aircraft is critical to flight safety. Exceeding an aircraft\u2019s maximum weight limitations may damage the structure of the aircraft and lead to stability and performance issues. When considering weight and balance, pilots need to know more than how much an aircraft can carry; they should also calculate [&hellip;]<\/p>\n","protected":false},"author":726,"featured_media":19303,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":""},"categories":[8],"tags":[105,436,12,438,437,191,136],"class_list":["post-19895","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-blog","tag-aircraft","tag-aircraft-balance","tag-aviation-safety","tag-aviation-tip","tag-balance","tag-flying-tips","tag-propeller"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v28.0 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Balancing Act: 10 Weight and Balance Terms to Know - Hartzell Propeller<\/title>\n<meta name=\"description\" content=\"In aviation, balance matters. 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