kpayne on VMOFRWIN702 with $$_JOB VerDate Sep<11>2014 QPS requirements Information Jkt 247047 Test FTD level Tolerances Entry No. Flight conditions Test details Title PO 00000 Performance and Trimmed Flight Control Positions. Notes 5 6 7 Frm 00454 Vertical Velocity - Section100 fpm (61 m/sec) or Section10% Pitch Attitude - Section1.5Section Sideslip Angle - Section2Section Longitudinal Control Position - Section5% Lateral Control Position - Section5% Directional Control Position - Section5% Collective Control Position - Section5%. All engines operating One engine inoperative. Augmentation System(s) On and Off. Record results for two gross weight and CG combinations. The data presented must be for normal climb power conditions. May be a series of snapshot tests. X X X Sfmt 8002 1.h.1. ..................... Descent Performance and Trimmed Flight Control Positions. Torque - Section3% Pitch Attitude - Section1.5Section Sideslip Angle - Section2Section Longitudinal Control Position - Section5% Lateral Control Position - Section5% Directional Control Position - Section5% Collective Control Position - Section5%. At or near 1,000 fpm (5 m/sec) rate of descent (RoD) at normal approach speed. Augmentation System(s) On and Off. Record results for two gross weight and CG combinations. May be a series of snapshot tests. X X X 1.h.2. ..................... Autorotation Performance and Trimmed Flight Control Positions. Pitch Attitude - Section1.5Section Sideslip Angle - Section2Section Longitudinal Control Position - Section5% Lateral Control Position - Section5% Directional Control Position - Section5% Collective Control Position - Section5%. Steady descents. Augmentation System(s) On and Off. Record results for two gross weight conditions. Data must be recorded for normal operating RPM. (Rotor speed tolerance applies only if collective control position is full down.) Data must be recorded for speeds from 50 kts, Section5 kts through at least maximum glide distance airspeed. May be a series of snapshot tests. X X X 1.i. .......................... Autorotation. Q:\14\14V2.TXT PC31 14 CFR Ch. I (1-1-19 Edition) Descent. 444 Fmt 8010 1.h. ........................ Pt. 60, App. D 16:30 Jun 25, 2019 TABLE D2A - FLIGHT TRAINING DEVICE (FTD) OBJECTIVE TESTS - Continued