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Regarding the night flight question. I had been informed by a CFI that I needed certain gyro instruments a while back. He even printed out the FAR. I KNEW I had seen it but couldn't find it in the manual. After everyone's reply, I figured that I had to really research to find what I saw. He printed out the VFR night and over the top for CARIIER ops. So..... tonight I went out and flew three hours until sun was down for 40 minutes. Smooth air, pretty sunset over Lake Michigan, but I didn't want to push my luck into real darkness just yet. I'll definitely need some more lumens than the old Grimes is giving me. Thanks for everyone's help. Just for info - here's the FAR I was given -- but now I know it does not apply!! §135.159 Equipment requirements: Carrying passengers under VFR at night or under VFR over-the-top conditions. No person may operate an aircraft carrying passengers under VFR at night or under VFR over-the-top, unless it is equipped with -- (a) A gyroscopic rate-of-turn indicator except on the following aircraft: (1) Airplanes with a third attitude instrument system usable through flight attitudes of 360 degrees of pitch-and-roll and installed in accordance with the instrument requirements prescribed in §121.305(j) of this chapter. (2) Helicopters with a third attitude instrument system usable through flight attitudes of ±80 degrees of pitch and ±120 degrees of roll and installed in accordance with §29.1303(g) of this chapter. (3) Helicopters with a maximum certificated takeoff weight of 6,000 pounds or less. (b) A slip skid indicator. (c) A gyroscopic bank-and-pitch indicator. (d) A gyroscopic direction indicator. (e) A generator or generators able to supply all probable combinations of continuous in-flight electrical loads for required equipment and for recharging the battery. (f) For night flights -- (1) An anticollision light system; (2) Instrument lights to make all instruments, switches, and gauges easily readable, the direct rays of which are shielded from the pilots' eyes; and (3) A flashlight having at least two size "D" cells or equivalent. (g) For the purpose of paragraph (e) of this section, a continuous in-flight electrical load includes one that draws current continuously during flight, such as radio equipment and electrically driven instruments and lights, but does not include occasional intermittent loads. (h) Notwithstanding provisions of paragraphs (b), (c), and (d), helicopters having a maximum certificated takeoff weight of 6,000 pounds or less may be operated until January 6, 1988, under visual flight rules at night without a slip skid indicator, a gyroscopic bank-and-pitch indicator, or a gyroscopic direction indicator. Rick Green N93686 415 C South Haven MI ==^================================================================ EASY UNSUBSCRIBE click here: http://topica.com/u/?aVxiLm.aVzvvT Or send an email To: [EMAIL PROTECTED] This email was sent to: [EMAIL PROTECTED] T O P I C A -- Register now to manage your mail! http://www.topica.com/partner/tag02/register ==^================================================================
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