Pt. 60, App. A 14 CFR Ch. I (1-1-19 Edition) (3) Differences between the two sets of results, other than variations attributable to repeatability issues that cannot be explained, should be investigated. (4) The flight simulator should retain the ability to over-plot both automatic and manual validation test results with reference data. END INFORMATION lllllllllllllllllllllll BEGIN QPS REQUIREMENTS ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION: LEVEL A AND LEVEL B SIMULATORS ONLY 17. a. Sponsors are not required to use the alternative data sources, procedures, and instrumentation. However, a sponsor may choose to use one or more of the alternative sources, procedures, and instrumentation described in Table A2E. END QPS REQUIREMENTS lllllllllllllllllllllll kpayne on VMOFRWIN702 with $$_JOB BEGIN INFORMATION b. It has become standard practice for experienced simulator manufacturers to use modeling techniques to establish data bases for new simulator configurations while awaiting the availability of actual flight test data. The data generated from the aerodynamic modeling techniques is then compared to the flight test data when it becomes available. The results of such comparisons have become increasingly consistent, indicating that these techniques, applied with the appropriate experience, are dependable and accurate for the development of aerodynamic models for use in Level A and Level B simulators. c. Based on this history of successful comparisons, the NSPM has concluded that those who are experienced in the development of aerodynamic models may use modeling techniques to alter the method for acquiring flight test data for Level A or Level B simulators. d. The information in Table A2E (Alternative Data Sources, Procedures, and Instrumentation) is presented to describe an acceptable alternative to data sources for simulator modeling and validation and an acceptable alternative to the procedures and instrumentation traditionally used to gather such modeling and validation data. (1) Alternative data sources that may be used for part or all of a data requirement are the Airplane Maintenance Manual, the Airplane Flight Manual (AFM), Airplane Design Data, the Type Inspection Report (TIR), Certification Data or acceptable supplemental flight test data. (2) The sponsor should coordinate with the NSPM prior to using alternative data sources in a flight test or data gathering effort. e. The NSPM position regarding the use of these alternative data sources, procedures, and instrumentation is based on the following presumptions: (1) Data gathered through the alternative means does not require angle of attack (AOA) measurements or control surface position measurements for any flight test. However, AOA can be sufficiently derived if the flight test program ensures the collection of acceptable level, unaccelerated, trimmed flight data. All of the simulator time history tests that begin in level, unaccelerated, and trimmed flight, including the three basic trim tests and - fly-by - trims, can be a successful validation of angle of attack by comparison with flight test pitch angle. (Note: Due to the criticality of angle of attack in the development of the ground effects model, particularly critical for normal landings and landings involving cross-control input applicable to Level B simulators, stable - fly-by - trim data will be the acceptable norm for normal and cross-control input landing objective data for these applications.) (2) The use of a rigorously defined and fully mature simulation controls system model that includes accurate gearing and cable stretch characteristics (where applicable), determined from actual aircraft measurements. Such a model does not require control surface position measurements in the flight test objective data in these limited applications. f. The sponsor is urged to contact the NSPM for clarification of any issue regarding airplanes with reversible control systems. Table A2E is not applicable to Computer Controlled Aircraft FFSs. g. Utilization of these alternate data sources, procedures, and instrumentation (Table A2E) does not relieve the sponsor from compliance with the balance of the information contained in this document relative to Level A or Level B FFSs. h. The term - inertial measurement system - is used in the following table to include the use of a functional global positioning system (GPS). i. Synchronized video for the use of alternative data sources, procedures, and instrumentation should have: (1) Sufficient resolution to allow magnification of the display to make appropriate measurement and comparisons; and (2) Sufficient size and incremental marking to allow similar measurement and comparison. The detail provided by the video should provide sufficient clarity and accuracy to measure the necessary parameter(s) to at least 1-2 of the tolerance authorized for the specific test being conducted and allow 122 VerDate Sep<11>2014 16:30 Jun 25, 2019 Jkt 247047 PO 00000 Frm 00132 Fmt 8010 Sfmt 8002 Q:\14\14V2.TXT PC31