Ok, guess he's attributing the need for a go around to the gust of wind.
But the nose goes up, the bird turns left. The nose goes up again, the bird turns further left.
Maintain thine airspeed, lest the ground (or a moth balled fedex aircraft) come up and smite thee.
Great post, text book vmc.
I'm thinking he needs to re-examine aircraft design for multi engine. I doubt he had enough vertical stab for the asymmetric thrust.
His go around wasn't free.
You are brilliant, please continue posting articles related to the subject of the thread that at the same time add nothing to the conversation. Having an opinion about something and trying to express what you think about it isn't easy, I understand your frustration and appreciate your struggle. You must be hoot at a dinner party.http://www.asias.faa.gov/pls/apex/f?p=100:17:0::NO::AP_BRIEF_RPT_VAR:WPR16LA110
' The original design for a nose-mounted piston engine was modified by the builders; they fabricated and installed a faired nose cone, and installed the two turbine engines just aft of the cockpit, one on either side of the fuselage, near where the side surfaces transitioned to the bottom surface. One engine was attached to either end of a through-strut, so that each engine/thrust centerline was located about 2 feet outboard of the fuselage centerline. Engine Information The engine was designed and marketed for use on model aircraft. According to the engine manufacturer's Operation and Maintenance Manual (OMM), the TJ40-G1 was a single-shaft turbojet engine with a single-stage radial compressor, annular combustion chamber, single-stage axial turbine, and an exhaust nozzle. A starter-generator was housed in the compressor impeller assembly. A ceramic spark plug was integrated in the combustion chamber, and "evaporating pipes" were used for "generation of the mixture of fuel and air." The engine produced about 88 pounds of thrust. Idle fuel consumption was cited as 20 ml/min (0.32 gallons per hour- gph), and maximum fuel consumption rate was 19.2 gph. The OMM contained the following caution: "The TJ40-G1 turbojet engine is designed exclusively for model aircraft and is not suitable for any other purpose. Never use it for people, objects or vehicle; it can only be used for properly designed model aircraft. Any other use can result in injury or death." '
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Just throw him on the ignore list. It's like he left.You are brilliant, please continue posting articles related to the subject of the thread that at the same time add nothing to the conversation. Having an opinion about something and trying to express what you think about it isn't easy, I understand your frustration and appreciate your struggle. You must be hoot at a dinner party.
I feel like I'm jumping in a bar fight, but how is the article not related to the OP? I thought it was the accident synopsis.You are brilliant, please continue posting articles related to the subject of the thread that at the same time add nothing to the conversation. Having an opinion about something and trying to express what you think about it isn't easy, I understand your frustration and appreciate your struggle. You must be hoot at a dinner party.
I feel like I'm jumping in a bar fight, but how is the article not related to the OP? I thought it was the accident synopsis.
for which I've initiated NO punches.jumping into a bar fight