.. _glossary: Glossary ========= .. glossary:: :sorted: candel spring classification label. A *candel* is a support fitting for a :term:`rail`. leg spring classification label. A *leg* is a support fitting for :term:`OWB`. section Section of the Aircraft, as defined by the OEM. This differs from the term :term:`zone`, which is a section defined by the organization of the :term:`LOPA` itself. zone Section of the Aircraft, as defined by the :term:`LOPA` itself. It is a section of homegenous analysis (standard or non-standard). The zone is not to be confused with :term:`section`, the latter being an Aircraft sction as defined by the OEM. OWB owb Overwing Beams. Those longitudinal beams are located over the wingbox. trace in the context of Checkers Analysis, a *trace* is a set of chronological tabular log of what has been done by the checker. MS Margin of Safety Calculation provinding a positive number for a non-failing item, and a negative one for a failing item. Usually defined as :math:`MS = allowable / applied - 1`. CID *Checker ID*. A checker identification number, *eg.* "02" is the non-standard Crossbeam Shear checker. lcid LCID *Load Case ID* A Load case ID identification number. dressing dressed dress in the context of :term:`MS` calculation, the *MS* dressing consists in make a float number easily readable *eg.* a raw MS = -0.001 is shown as ">-0.01". OEM Original Equipment Manufacturer In the User Manual, OEM is mostly used to refer to aircraft manufacturer Boeing or Airbus. However it could also be used to designate cabin equipment manufacturer like seats. PAX Passengers Throughout the User Manual, PAX is used to designate cabin passengers. AC Abbreviation of Aircraft fsconf Floor Structure Configuration fsconf is a key word used by the FloorTools software referring to a floor structure configuration. Loading Reference Reference A "critical" standard PAX seating installating entered in the FTools software and used as reference to pass the non standard seating installation SSR Structural Substantiation Report IFL Interface Load In the User Manual, IFL refers to any cabin monument floor interface load (seat, shroud, shell, partition, small cabinet, etc...) vbeam Virtual Beam Beam of unique property ID regrouping several Finite Elements. See :ref:`vbeam_explained` for further references. Crossbeam Designate the transversal floor beam. This more generic term "floor beam" is also used to designate a crossbeam Rail Designate the longitudinal seat track. Rail or seat track can be independantly used. Checked model FE model of the floor structure loaded with user defined loading corresponding to a non standard seating installation Reference model FE model of the floor structure loaded with standard PAX seating installation interface load. POC Passenger Occupancy Combination TTOL Taxi, Take Off and Landing MISW Maximum Installed Seat Weight. The maximum installed seat weight is the maximum allowable weight for the seat with all components and includes all equipment the seat installer may add to the seat, such as emergency equipment or literature pocket contents. This weight is equal to the minimum total tested seat weight of all static/dynamic tests used for substantiation of the subject seat P/Ns. However, this weight must be verified against seat track interface loads and other aircraft/structural limitations. LOPA Layout of passenger Accomodations. In the `FTools` context, `lopa` refers to Aircraft layout to be bound on an Aircraft :term:`fsconf`. The lopa is provided by user as an XLSX input data file. Checker One analysis module that performs an independant calculation on a dedicated structural item. Wheelbase In a LOPA context, a seat's wheelbase is the distance between seat's front and aft legs.