See Figure A2B for an illustration of the reference measurements: c. Alternative method for control dynamics evaluation. This document is for organisations that want to apply for a sponsorship licence. The most common grounds for delays or refusal are linked to applications in which the supporting documentation has not been submitted within the permitted timescale, it is incomplete or out-of-date, or copy documents have not been correctly certified. Up to 5° bank towards the operating engine(s) is permissible. (a) System displays/operation satisfactory. Significant overshoots, First overshoot and ±1 subsequent overshoots. The cross-plot or other alternative method must display the relevant validity regions for flaps up and flaps down at a minimum. (a) The sponsor's FFS identification number or code. Table A1C - Table of Simulator System Tasks. h. There is no requirement for any flight test data supplier to submit a flight test plan or program prior to gathering flight test data. b. Select one or several of the following test cases: (3) Rejected Takeoff (Dry/Wet/Icy Runway) and check the following: (c) Motion/visual effects during deceleration. The required dynamic control tests are described in Table A2A of this attachment. (d) The source of the basic aerodynamic model and the aerodynamic coefficient data used to modify the basic model. Related avionics such as stall warning and augmentation systems should also be considered. g. Form and manner of presentation of objective test results in the QTG: (1) The sponsor's FFS test results must be recorded in a manner acceptable to the NSPM, that allows easy comparison of the FFS test results to the validation data (e.g., use of a multi-channel recorder, line printer, cross plotting, overlays, transparencies). a. 406 0 obj <>/Filter/FlateDecode/ID[<2C7DD795F860C740983EBA598FA2AE48><4F68CF2A34B93743B5862999A6D35D11>]/Index[383 58]/Info 382 0 R/Length 114/Prev 243392/Root 384 0 R/Size 441/Type/XRef/W[1 3 1]>>stream This attachment applies to all simulators, regardless of qualification level, that are used to satisfy the training requirements of an FAA-approved low-altitude windshear flight training program, or any FAA-approved training program that addresses windshear encounters. (2) Sufficient size and incremental marking to allow similar measurement and comparison. Playback equipment and recordings of the QTG conditions should be provided during initial evaluations. ); The demonstration test may be conducted by initializing and maintaining a fixed amount of ice accretion throughout the maneuver in order to consistently evaluate the aerodynamic effects. This section applies to previously qualified Level C and Level D FSTDs being used to obtain credit for stall training maneuvers beyond the first indication of a stall (such as stall warning system activation, stick shaker, etc.) The evaluation requirements in this Directive are intended to validate FSTD fidelity at angles of attack sufficient to identify the stall, to demonstrate aircraft performance degradation in the stall, and to demonstrate recovery techniques from a fully stalled flight condition. b. However, inactive periods of 2 years or more will require requalification under the standards in effect and current at the time of requalification. Normal take-off/ground acceleration time and distance, Rejected take-off if performed for airplane certification, Data may be acquired by using a constant tiller position, measured with a protractor or full rudder pedal application for steady state turn, and synchronized video of heading indicator. 383 0 obj <> endobj %%EOF The reader is encouraged to review the Airplane Flight Simulator Evaluation Handbook, Volumes I and II, published by the Royal Aeronautical Society, London, UK, and AC 25-7, as amended, Flight Test Guide for Certification of Transport Category Airplanes, and AC 23-8, as amended, Flight Test Guide for Certification of Part 23 Airplanes, for references and examples regarding flight testing requirements and techniques. a. In order to be qualified at a particular qualification level, the FFS must: (1) Meet the general requirements listed in Attachment 1 of this appendix; (2) Meet the objective testing requirements listed in Attachment 2 of this appendix; and. Additionally, as part of your sponsor licence application, you will need to provide key documentary evidence in support within a limited timescale (see below). The specific force is required for the perception of the aircraft sustained specific force, while the angular rates and accelerations do not occur in the aircraft and should be minimized. http://www.faa.gov/about/initiatives/nsp/, Guidelines For Electronic Qualification Test Guide, Guidance for Design and Integration of Aircraft Avionics Equipment in Simulators. The following are the minimum distances at which runway features must be visible for simulators at Levels A, B, C, and D. Distances are measured from runway threshold to an airplane aligned with the runway on an extended 3° glide-slope in simulated meteorological conditions that recreate the minimum distances for visibility. c. The lateral-directional characteristics are also altered by ground effect. Other problems include inadequate information regarding initial conditions or test maneuvers. 2. Upset recovery or unusual attitude training maneuvers within the FSTD's validation envelope that are intended to exceed pitch attitudes greater than 25 degrees nose up; pitch attitudes greater than 10 degrees nose down, and bank angles greater than 45 degrees. 2. This document should clearly identify sources of data for all required tests, a description of the validity of these data for a specific engine type and thrust rating configuration, and the revision levels of all avionics affecting the performance or flying qualities of the aircraft. Hard copy documents must be the originals, although in some cases the Home Office will accept certified copies. The report should explain the predictive method used and illustrate past success of the method on similar projects. endobj (7) A glossary of terms and symbols used (including sign conventions and units). A sponsor using this method to comply with the QPS requirements should perform the tests as follows: (a) Underdamped response. j. 2. Operational navigation systems (including inertial navigation systems, global positioning systems, or other long-range systems) and the associated electronic display systems will be evaluated if installed. b. Food businesses must send evidence of registration or approval by food authority. 5 0 obj (iii) A model generated with an “off-board” or an “on-board” model development tool (by providing proper latitude/longitude reference; correct runway or landing area orientation, length, width, marking, and lighting information; and appropriate adjacent taxiway location) to generate a facsimile of a real world airport or landing area. Control systems that exhibit characteristics other than classical overdamped or underdamped responses should meet specified tolerances. (2) The Motion System tests in Section 3 of Table A2A are intended to qualify the FFS motion cueing system from a mechanical performance standpoint. b. (5) Manual Landing with Control Malfunction. No additional regulatory or informational material applies to § 60.1, Applicability, or to § 60.2, Applicability of sponsor rules to persons who are not sponsors and who are engaged in certain unauthorized activities. For example, data that exhibit rapid variations of the measured parameters may require interpolations or a “best fit” data selection. (1) The following guidelines apply to flight simulators representing airplanes with alternate engine applications or with more than one engine type or thrust rating. In either case, engineering validation or airplane manufacturer rationale should be submitted as justification for ground tests or for eliminating a configuration. (2) Turning Flight. Select one or several of the following test cases while monitoring flight control and hydraulic systems for normal operation and with malfunctions selected: (1) Flaps/Gear Normal Operation. 2. These effects may be due to engine dynamic characteristics, thrust levels or engine-related airplane configuration changes. FSTDs that are found to meet the requirements of this Directive will have their Statement of Qualification (SOQ) amended to reflect the additional training tasks that the FSTD has been qualified to conduct. However, flight crew training and certification often begins several months prior to the entry of the first airplane into service. The tests include a qualitative assessment of the FFS by an NSP pilot. (k) The visual system model and manufacturer, including display type. (3) An understanding of the accuracy of the data to be gathered using appropriate alternative data sources, procedures, and instrumentation that is traceable to a recognized standard as described in Attachment 2, Table A2E of this appendix. h�½H��OO�E��F�u����N�z�>�� �D����Pj9|��>o֤������ao�h5C��C>s1�db7xٲ�jx��bx0� b^]��x�B�����F��!�Yն� ~?��W�a��$G�. For circling approaches, all requirements of this section apply to the runway used for the initial approach and to the runway of intended landing. It is an appendix to the full policy guidance on sponsoring a worker or student. Additionally, the document should refer to other appropriate sources of validation data (e.g., sound and vibration data documents). Operations With Missing, Malfunctioning, or Inoperative Components (, 19. (b) Visual cues during flare to assess Depth perception. For passive sidesticks, whose displacement is the flight control input, the force applied by the pilot to the controls does not need to be displayed. d. When a person sponsors an FFS maintained by a person other than a U.S. certificate holder, the sponsor is accountable for that FFS originally meeting, and continuing to meet, the criteria under which it was originally qualified and the appropriate Part 60 criteria, including the airport models that may be used by instructors or evaluators for purposes of training, checking, or testing under this chapter. Fidelity Requirements: The requirements defined for the evaluation of full stall training maneuvers are intended to provide the following levels of fidelity: 4. In other cases, additional, category-specific documents are required, for example, for a Tier 2 Intra Company Transfer you will need to submit audited accounts or an annual report showing the link between the UK and foreign organisations. Data from a test airplane or engineering test bench with the correct engine controller (both hardware and software) are required. In most cases, you will need to provide at least four supporting documents from those cited in Appendix A. Therefore, when a test number (or series of numbers) is not required, the term “Reserved” is used in the table at that location. c. To be qualified to supply engineering simulator validation data, for aerodynamic, engine, flight control, or ground handling models, an airplane manufacturer or other acceptable data supplier must: (1) Be able to verify their ability able to: (a) Develop and implement high fidelity simulation models; and. Repeat of the alternate method during the initial evaluation satisfies this test requirement. Airspeeds may be cross checked with those in the TIR and AFM. Flight test data used to validate FFS performance and handling qualities must have been gathered in accordance with a flight test program containing the following: (a) The maneuvers and procedures required for aircraft certification and simulation programming and validation. c. At least one qualified ice accretion model must be objectively tested to demonstrate that the model has been implemented correctly and generates the correct cues as necessary for training. (2) Early CGI visual systems are excepted from the requirement of including runway numbers unless the runways are used for LOFT training sessions. It is always best to seek advice from a specialist with experience in helping employers with Tier 2 and Tier 5 licence applications.
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