kpayne on VMOFRWIN702 with $$_JOB VerDate Sep<11>2014 QPS requirements Information Jkt 247047 Test Tolerance(s) Entry No. 1.c.3. ........... PO 00000 One Engine inoperative, rejected take off. Frm 00352 Sfmt 8002 342 Fmt 8010 1.d. ............. B C D Ground, Takeoff .................... Time history from the take off point to touch down. Test conditions near limiting performance. X X Torque - Section3%, Pitch Attitude - Section1.5Section, Bank Attitude - Section1.5Section, Longitudinal Control Position - Section5%, Lateral Control Position - Section5%, Directional Control Position - Section5%, Collective Control Position - Section5%. In Ground Effect (IGE); and Out of Ground Effect (OGE). Record results for light and heavy gross weights. May be a series of snapshot tests. X X Vertical Velocity - Section100 fpm (0.50 m/sec) or Section10%, Directional Control Position - Section5%, Collective Control Position - Section5%. From OGE Hover .................. Record results for light and heavy gross weights. May be a series of snapshot tests. X X Notes PC31 Level Flight 14 CFR Ch. I (1-1-19 Edition) Q:\14\14V2.TXT Airspeed - Section3 kt, Altitude - Section20 ft (6.1m), Torque - Section3%, Rotor Speed - Section1.5%, Pitch Attitude - Section1.5Section, Roll angle - Section1.5Section, Heading - Section2Section, Longitudinal Control Position - Section10%, Lateral Control Position - Section10%, Directional Control Position - Section10%, Collective Control Position - Section10%, Distance - Section7.5% or Section30m (100ft). Vertical Climb Performance .......................... 1.f. .............. Test details Hover Performance .......................... 1.e. ............. Flight condition Title Simulator level Pt. 60, App. C 16:30 Jun 25, 2019 TABLE C2A - FULL FLIGHT SIMULATOR (FFS) OBJECTIVE TESTS - Continued