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I am thinking of getting into a new homebuilt project but I wonder where to get
accurate numbers of how many of a particular design are flying or where I might see some examples of the kit I am thinking of building. Does the EAA keep a record of the kits flown into the big fly-ins Oshkosh or Sun-n-Fun? The FAA? Do they keep track of the kit manufacturer or just lump everything into amatuere built. Specifically, I wonder how many Zenith CH 701's (STOL) are flying and what has their accident history been? Anthony Memphis TN |
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(DL152279546231) wrote:
Specifically, I wonder how many Zenith CH 701's (STOL) are flying and what has their accident history been? Anthony Memphis TN Anthony, Chris Heintz and his Zenith aircraft designs have an excellent reputation in the homebuilt community. The Zenith Aircraft Company web site claims over 500 CH 701 flying throughout the world. The FAA registry database shows 151 registered in the USA but those would only be ones in which the builder chose to include "701" in the aircraft make description. Remember, the builder *is* the manufacturer and can put in anything for manufacturer and model on the FAA registration form. The NTSB accident database has 11 reports (plus one preliminary) for aircraft with "701" in the model field. Pull them up and you'll see that they are all clearly Zenith CH 701. Below, I've summarized those accidents and I've also added engine make/model and pilot hours information that is not included in the NTSB web site reports. The only accident that remotely suggests a problem with the Zenith CH 701 design is the 4-03-90 accident ("inadequate fuel drain design"). Reading between the lines, however, I doubt that there was truly a problem with the fuel drain. On the other hand, if there was indeed a problem with *Zenith's* fuel drain design I'm confident that Zenith would have addressed and fixed the problem long ago. After all, that accident occurred some 14 years ago. David O -- http://www.AirplaneZone.com ------ 7-10-03 - Suzuki 993cm (four stroke, water cooled, three cyl, auto engine) - The flight was to be a pre purchase test flight. The pilot was the prospective purchaser. The pilot said the engine faltered after takeoff. The owner said pilot faltered. 6/6/03 - Cont A-75 - Engine failure. The pilot/builder stated, "... engine quit because a jet came loose in the carburetor". 3/1/01 - Subaru - Engine failure. The pilot/bulder said he suspected "detonation" was the cause. 5/14/00 Rotax 582UL (two stroke, two cylinder, liquid cooled) - Fuel exhaustion due to pilot's improper fuel management. 8/21/99 Rotax 912 (four stroke, four cylinder, liquid cooled) - Pilot had 110 hours total time and claimed 4 hours in make/type. This was the third of his test flights in his newly completed airplane. The first and second test flights lasted approximately 30 minutes and ended without incident. From the NTSB narrative: "He was on a long, low, final approach, and the airplane bounced twice and headed towards a corn field. He applied full power to go-around but the airplane collided with the tops of trees adjacent to the field, then the ground. A witness reported seeing the airplane on a low approach and believed the airplane would land short of the runway." 8/11/97 AMW - (a 2 stroke outboard boat engine) Partial loss of power after takeoff at 50 ft AGL and total loss of power during the crosswind-downwind turn. 8/11/96 Cont C-85 - Total loss of power. Pilot had 1085 hours total time and 176 hours in make/type. Pilot said he switched tanks from left to right while on final. Post accident inspection revealed the left tank was empty and the right tank was full. 9/29/93 Rotax 582LC - Total loss of engine power for undetermined reasons. Pilot hat 542 total time and 96 hours in make/type. 6/12/93 Rotax 582 - Pilot had 338 hours total time, 60 hours glider time, and 2 hours in make/type. NTSB probable cause: PIC's failure to maintain aircraft control. The PIC's lack of total experience in aircraft type was a factor. 3/13/93 Rotax 582UL - Pilot had 800 hours total time, and 180 hours in make/type. Takeoff was from a backyard strip. NTSB probable cause: The pilot's inadequate compensation for wind conditions and failure to maintain directional control after lift-off. Factors related to the accident were; The unfavorable wind condition and proximity of the power line. 4/3/90 Rotax 532 - Pilot had 192 hours total time and 14 hours in make/type. NTSB probable cause: Manufacturers's inadequate design of the fuel drain. Contributing factor was PIC's disregarding the fuel supply which resulted in fuel exhaustion. |
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![]() "David O" wrote in message ... (DL152279546231) wrote: Specifically, I wonder how many Zenith CH 701's (STOL) are flying and what has their accident history been? Anthony Memphis TN Anthony, Chris Heintz and his Zenith aircraft designs have an excellent reputation in the homebuilt community. The Zenith Aircraft Company web site claims over 500 CH 701 flying throughout the world. The FAA registry database shows 151 registered in the USA but those would only be ones in which the builder chose to include "701" in the aircraft make description. Remember, the builder *is* the manufacturer and can put in anything for manufacturer and model on the FAA registration form. The NTSB accident database has 11 reports (plus one preliminary) for aircraft with "701" in the model field. Pull them up and you'll see that they are all clearly Zenith CH 701. Below, I've summarized those accidents and I've also added engine make/model and pilot hours information that is not included in the NTSB web site reports. The only accident that remotely suggests a problem with the Zenith CH 701 design is the 4-03-90 accident ("inadequate fuel drain design"). Reading between the lines, however, I doubt that there was truly a problem with the fuel drain. On the other hand, if there was indeed a problem with *Zenith's* fuel drain design I'm confident that Zenith would have addressed and fixed the problem long ago. After all, that accident occurred some 14 years ago. David O -- http://www.AirplaneZone.com ------ 7-10-03 - Suzuki 993cm (four stroke, water cooled, three cyl, auto engine) - The flight was to be a pre purchase test flight. The pilot was the prospective purchaser. The pilot said the engine faltered after takeoff. The owner said pilot faltered. Good reason not to let someone else fly your airplane. We have a trike at a local airport with this engine. It is flown regularly by the owner who installed it. 6/6/03 - Cont A-75 - Engine failure. The pilot/builder stated, "... engine quit because a jet came loose in the carburetor". Most likely this was the result of someone's carelessness. The Stromberg carburetor, which is usually fitted to the A-75 Continental, has a main jet which will come loose and starve the mixture when it has not been safety-wired. There are quite a few accidents in the literature attributable to the loose Stromberg jet, which someone has been tampering with, in an effort to set the float level --- and then neglected to safety the jet. |
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