kpayne on VMOFRWIN702 with $$_JOB VerDate Sep<11>2014 QPS requirements Information Jkt 247047 Test Tolerance(s) Entry No. 3.b. ............. PO 00000 Frm 00362 C D Sfmt 8002 Based on Simulator Capability. N/A ......................................... Required as part of the MQTG. The test must demonstrate motion system leg balance as specified by the applicant for flight simulator qualification. X X X Based on Simulator Capability. N/A ......................................... Required as part of the MQTG. The test must demonstrate a smooth turnaround (shift to opposite direction of movement) of the motion system as specified by the applicant for flight simulator qualification. X X X With the same input signal, the test results must be repeatable to within Section0.05g actual platform linear acceleration in each axis. Accomplished in both the - ground - mode and in the - flight - mode of the motion system operation. Required as part of the MQTG. The test is accomplished by injecting a motion signal to generate movement of the platform. The input must be such that the rotational accelerations, rotational rates, and linear accelerations are inserted before the transfer from helicopter center of gravity to the pilot reference point with a minimum amplitude of 5Section/sec/ sec, 10Section/sec and 0.3g, respectively. X X X 352 Fmt 8010 Notes Motion system repeatability PC31 Motion cueing performance signature See Paragraph 6.c. in this attachment for additional information. Note: if there is no difference in the model for - ground - and - flight - operation of the motion system, this should be described in an SOC and will not require tests in both modes. 14 CFR Ch. I (1-1-19 Edition) Q:\14\14V2.TXT 3.e. ............. B Turn Around Turn Around .......................... 3.d. ............. Test details Leg Balance Leg Balance .......................... 3.c. .............. Flight condition Title Simulator level Pt. 60, App. C 16:30 Jun 25, 2019 TABLE C2A - FULL FLIGHT SIMULATOR (FFS) OBJECTIVE TESTS - Continued