Flight Simulation Training Device Initial and Continuing Qualification and Use, 11995-11996 [C7-4884]
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[Federal Register Volume 73, Number 44 (Wednesday, March 5, 2008)] [Corrections] [Pages 11995-11996] From the Federal Register Online via the Government Printing Office [www.gpo.gov] [FR Doc No: C7-4884] Federal Register / Vol. 73, No. 44 / Wednesday, March 5, 2008 / CORRECTIONS [[Page 11995]] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 60 [Docket No. FAA-2002-12461; Notice No. 07-14] RIN 2120-AJ12 Flight Simulation Training Device Initial and Continuing Qualification and Use Correction In proposed rule document 07-4884 beginning on page 59600 in the issue of Monday, October 22, 2007, make the following correction: 1. On page 59670, in Table A3A, entry 2.b. is corrected as follows: Table A3A.--Functions and Subjective Tests ---------------------------------------------------------------------------------------------------------------- <<>> ----------------------------------------------------------------------------------------------------------------- Simulator level Number Operation tasks ------------------- A B C D ---------------------------------------------------------------------------------------------------------------- Tasks in this table are subject to evaluation if appropriate for the airplane simulated as indicated in the SOQ Configuration List or the level of simulator qualification involved. Items not installed or not functional on the simulator and, therefore, not appearing on the SOQ Configuration List, are not required to be listed as exceptions on the SOQ. ---------------------------------------------------------------------------------------------------------------- * * * * * * * 2.b..................................... Pushback/Powerback............................ ... X X X * * * * * * * ---------------------------------------------------------------------------------------------------------------- 2. On page 59684, the heading to Table A3F is corrected as follows: Table A3F.--Functions and Subjective Tests ------------------------------------------------------------------------ << >> ------------------------------------------------------------------------- Simulator level Number Special effects ------------------- A B C D ------------------------------------------------------------------------ * * * * * * * ------------------------------------------------------------------------ 3. Beginning on page 59718, in Table B2A, entries 2.a.3.a. and 2.c.9.a. are corrected as follows: [[Page 11996]] Table B2A.--Flight Training Device (FTD) Objective Tests ---------------------------------------------------------------------------------------------------------------- << >> ----------------------------------------------------------------------------------------------------------------- Test FTD < > ------------------------------- Flight level ----------------- Tolerances conditions Test details ---------- Number Title 5 6 Notes ---------------------------------------------------------------------------------------------------------------- * * * * * * * 2.a.3.a..... Rudder Pedal 5 lb Ground.......... Record results X Position vs. (2.2 daN) for an Force and breakout, 10% or control sweep Position 5 to the stops. Calibration. lb (2.2 daN) force, 2[deg] rudder angle. * * * * * * * 2.c.9.a..... Phugoid Dynamics 10% Cruise.......... The test must X period, 10% of whichever is time to \1/2\ less of the or double following: amplitude or Three full .02 cycles (six of damping overshoots ratio. after the input is completed), or the number of cycles sufficient to determine time to \1/2\ or double amplitude. * * * * * * * ---------------------------------------------------------------------------------------------------------------- 4. Beginning on page 59842, in Table D1A, entry 2.c. is corrected as follows: Table D1A.--Minimum FTD Requirements ------------------------------------------------------------------------ << >> ------------------------------------------------------ FTD level < > Number General FTD -------------------- notes requirements 4 5 6 7 ------------------------------------------------------------------------ * * * * * * * 2.c.......... Relative responses X X X The intent is to of the flight verify that the deck instruments FTD provides must be measured instrument cues by latency tests that are, within or transport the stated time delay tests, and delays, like the may not exceed helicopter 150 milliseconds. responses. For The instruments helicopter must respond to response, abrupt input at acceleration in the pilot's the appropriate, position within corresponding the allotted rotational axis time, but not is preferred. before the time that the helicopter or set of helicopters would respond under the same conditions.. Latency: ... ... ... ... The FTD instrument and, if applicable, the motion system and the visual system response must not be prior to that time when the helicopter responds and may respond up to 150 milliseconds after that time under the same conditions. Transport Delay: As an alternative to the Latency requirement, a transport delay objective test may be used to demonstrate that the FTD system does not exceed the specified limit. The sponsor must measure all the delay encountered by a step signal migrating from the pilot's control through all the simulation software modules in the correct order, using a handshaking protocol, finally through the normal output interfaces to the instrument display and, if applicable, the motion system, and the visual system. An objective test is required. * * * * * * * ------------------------------------------------------------------------ [FR Doc. C7-4884 Filed 3-4-08; 8:45 am] BILLING CODE 1505-01-D
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