Tuesday, December 09, 2014

TL Ultralight SRO Stingsport, N177N: Accident occurred July 05, 2012 in Piru, California

NTSB Identification: WPR12FA295
14 CFR Part 91: General Aviation
Accident occurred Thursday, July 05, 2012 in Piru, CA
Probable Cause Approval Date: 12/11/2014
Aircraft: TL ULTRALIGHT SRO STINGSPORT, registration: N177N
Injuries: 2 Fatal.

NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

The flight instructor and commercial pilot were conducting a flight review during daytime visual flight rules conditions. Multiple witnesses near the accident site reported observing the accident airplane descending in a nose-low attitude while spinning. Witness reports, findings from the wreckage examination and recovered GPS data are consistent with the airplane entering a stall as part of the flight review and a subsequent spin. A postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The airplane was equipped with dual flight controls; however, it could not be determined which pilot was manipulating the controls at the time of the accident nor could it be determined why neither pilot was able to recover from the spin. The airplane was also equipped with a rescue ballistic parachute system. The arming handle was found fractured from the cabin roof due to a force on the handle that loaded the adhesive joint in peel mode. The arming pin was not engaged within the arming handle and exhibited a permanent bend. Fretting wear deposits were present on the retaining pin shank, suggesting that the pin was most likely engaged within the handle a significant portion of the time when the airplane was in motion. It could not be determined if the arming pin was removed before the flight or at some point during the flight. The parachute was not deployed. Medical record review revealed that the left seat pilot had significant preexisting heart disease. However, due to the limitations of the available medical evidence, the investigation could not determine if the pilot had an acute cardiac event during the flight that degraded his ability to operate the aircraft. Toxicology tests for the pilot were positive for Metoprolol, Ticlopidine, and Valsartan, which are commonly used to treat high blood pressure and angina, to control heart rate in some arrhythmias, and to reduce the risk of stroke. Toxicology testing for the flight instructor, who was seated in the right seat, revealed evidence of previous marijuana use; however no active compound was detected in the postmortem blood, thus it is unlikely that he was experiencing acute impairment from marijuana at the time of the accident.

The National Transportation Safety Board determines the probable cause(s) of this accident as follows:

The pilot’s failure to recover from a stall, which resulted in a spin. Contributing to the accident was the instructor’s inadequate remedial action.

HISTORY OF FLIGHT

On July 5, 2012, about 1324 Pacific daylight time, a TL Ultralight SRO Stingsport, N177N, was substantially damaged when it impacted terrain near Piru, California. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. The certified flight instructor and commercial pilot receiving instruction were fatally injured. Visual meteorological conditions prevailed and no flight plan was filed for the instructional flight. The local flight originated from Whiteman Airpark (WHP), Van Nuys, California, at 1300.

Multiple witnesses driving on Highway 126 within the vicinity of the accident site reported observing the accident airplane descending in a nose low attitude while spinning in a counter-clockwise direction before it descended below a tree line.

Friends of the pilot and flight instructor reported that the purpose of the flight was to conduct a flight review for the pilot.

PERSONNEL INFORMATION

It was not determined which one of the two pilots, a commercial pilot and owner of the airplane seated in the left seat or the certified flight instructor seated in the right seat, was manipulating the flight controls when the accident occurred.

The pilot, age 89, held a commercial pilot certificate with an airplane single-engine land, single-engine sea, and instrument airplane ratings. The most recent third class medical certificate was issued to the pilot November 3, 2005. The pilot reported on his most recent medical application that he accumulated a total of 3,600 hours of flight time. Review of the pilot's logbook revealed that as of the most recent entry dated May 22, 2012, he had accumulated 3,999.3 total hours of flight time.

The flight instructor, age 59, held an airline transport pilot certificate with an airplane single-engine land, airplane multi-engine land, and instrument airplane ratings. The pilot also held a flight instructor certificate with airplane single-engine land, airplane multi-engine land, and instrument airplane ratings. The most recent second class medical certificate issued to the pilot was on June 28, 2011, with no limitations stated. The flight instructor reported on his most recent medical certificate application that he had accumulated a total of 13,000 hours of flight time and 200 hours within the previous six months. The flight instructor's logbooks were not located.

AIRCRAFT INFORMATION

The light sport two-seat, low-wing, fixed-gear airplane, serial number (S/N) TLUSA 153, was manufactured in 2007. It was powered by a Rotax 912ULS engine, serial number 5647034, rated at 100 horsepower, driving a Wood comp ground adjustable three bladed wooden propeller. The airplane was equipped with a Galaxy Rescue Parachute System (GRS).

Review of the airframe, engine, and propeller logbooks revealed that the most recent annual inspection was completed on July 1, 2012, at a Hobbs time of 214.1 hours and tachometer time of 215.9 hours. The airplane had accumulated about 1 hour of flight time since the annual inspection at the time of the accident.

Review of the Pilot Operating Handbook (POH), Section 4, Normal Procedures, page 12, Pre Taxi checklist states under item 8, "GRS Safety Pin -- REMOVED and STOWED." Within the note section of page 13, the POH states in part "…Carefully remove the safety pin from the GRS activation handle. Stow it in a place where it can be easily reached after landing for securing it back into place. The canopy locking lever on the pilot's side is a recommended storing location. Then you will be reminded to secure the chute when you reach for the canopy latch to exit the cockpit."

METEOROLOGICAL INFORMATION

A review of recorded data from the Camarillo Airport (CMA) automated weather observation station, located about 20 miles southwest of the accident site, revealed at 1255 conditions were wind variable at 4 knots, visibility 10 statute miles, overcast cloud layer at 1,600 feet, temperature 18 degrees Celsius, dew point 15 degrees Celsius, and an altimeter setting of 29.98 inches of mercury. At 1355, CMA reported a broken cloud layer at 1,800 feet.

WRECKAGE AND IMPACT INFORMATION

Examination of the accident site revealed that the airplane came to rest upright within an open field adjacent to an orange tree orchard on an approximate heading of about 294 degrees magnetic. Wreckage debris remained within about 20 feet of the main wreckage. A large indention within the ground was located about 1 foot in front of the engine and contained two propeller blades.

The fuselage was mostly intact and exhibited impact damage to the forward and lower areas of the fuselage. The Galaxy Rescue Parachute System's handle was found displaced from its respective mount location on the cabin roof structure. The securing pin was found removed and located within the main wreckage. The handle appeared to have remained within its housing and not actuated. The left wing remained attached to the fuselage. The left aileron and flap remained attached via all their respective mounts. The left flap appeared to be in a partially extended position. The right wing remained attached to the fuselage. The right aileron and flap remained attached via all their respective mounts. The right flap appeared to be in a partially extended position.

The empennage was partially separated and displaced 45 degrees to the right, about one foot forward of the horizontal stabilizer. The vertical stabilizer and horizontal stabilizer remained attached to the empennage structure. The rudder was partially separated and remained attached via its lower mount. The elevator remained attached to its mounts, and the trim tab remained attached to the elevator.

Flight control continuity was established from the left and right cockpit controls to all primary flight control surfaces.

The engine remained attached to the engine mount structure. The 1/3 cylinder and 2/4 cylinder side carburetors remained attached. Both carburetors were disassembled and found unremarkable. The top spark plugs were removed and exhibited signatures consistent with normal operation. Rotational continuity was established throughout the engine and valve train when the propeller was rotated by hand. Thumb compression was obtained on all four cylinders.

The propeller assembly remained attached to the engine crankshaft propeller flange. One propeller blade remained attached to the propeller hub and the remaining two blades were separated just outboard of the hub. The separated blades exhibited slight chord wise scratching.

No evidence of any preexisting mechanical malfunction was observed during the examination of the engine and airframe.

The cabin roof structure surrounding the parachute handle mount area, parachute arming handle, and arming pin were sent to the National Transportation Safety Board (NTSB) Materials Laboratory for further examination.

MEDICAL AND PATHOLOGICAL INFORMATION

According to the FAA medical case review; the 89-year-old pilot had a history of high blood pressure and coronary artery disease treated with bypass surgery and medications. He had not renewed his medical certificate since it expired November 30, 2006.

The Ventura County Medical Examiner conducted an autopsy on the pilot on July 7, 2012. The medical examiner determined that the cause of death was "...blunt force injuries." The autopsy noted a palpable subcutaneous pacemaker. The pacemaker was not interrogated. The cardiovascular system examination was limited by the degree of injury; the heart was not intact. The coronary arteries were not examined. The brain was not examined.


The FAA's Civil Aeromedical Institute (CAMI) in Oklahoma City, Oklahoma, performed toxicology tests on the pilot. According to CAMI's report, no carbon monoxide was detected in the blood and no ethanol was detected in the vitreous. Metoprolol and Valsartan were detected in the blood and urine. Ticlopidine was detected in the urine but not the blood. Metoprolol is a beta blocker used to treat patients with cardiovascular disease. Valsartan is an angiotensin receptor blocker used to treat high blood pressure. Ticlopidine is used to prevent platelet aggregation (clotting) in patients at risk for strokes and also in people with coronary artery stents.

According to the FAA medical case review; the 59-year-old flight instructor had a second class medical certificate with no restrictions or limitations.

The Ventura County Medical Examiner conducted an autopsy on the flight instructor on July 7, 2012. The medical examiner determined that the cause of death was "...blunt force injuries."

The FAA's Civil Aeromedical Institute (CAMI) in Oklahoma City, Oklahoma, performed toxicology tests on the flight instructor. According to CAMI's report, no carbon monoxide was detected in the blood and no ethanol was detected in the vitreous. Tetrahydrocannabinol was detected in the lung (0.0244 ug/ml) but not in the blood. Tetrahydrocannabinol is the psychoactive compound found in marijuana. Tetrahydrocannabinol carboxylic acid was detected in the blood (0.0071 ug/ml), in the urine (0.071 ug/ml) and in the lung (0.006 ug/ml). Tetrahydrocannabinol carboxylic acid is the inactive metabolite of tetrahydrocannabinol. Additionally, terazosin was detected in the blood and urine. Terazosin is an alpha blocker used to treat benign prostate disease.

TESTS AND RESEARCH

Two handheld global positioning system (GPS), Garmin GPSMAP 396 units were recovered from the airplane. The units were sent to the NTSB Office of Research and Engineering Recorders Laboratory for data extraction. The data revealed a flight track from the day of the accident showed the flight's departure from runway 12 at WHP, where the flight performed two take off and landings within the airport traffic pattern before proceeding on a northwesterly course.

The data depicted that as the accident airplane continued on a northwesterly course, a 360-degree right turn and 360-degree left turn were performed followed by a 90-degree turn to the right and left. About 3 miles south of the accident site, a 45-degree turn to a northerly heading was observed at an altitude of 4,774 feet mean sea level (msl) and ground speed of 91 knots. The following 10 recorded data points over a time period of 80 seconds depicted an increase in altitude to about 5,148 feet msl, and a decrease in ground speed to 55 knots followed by an increase of ground speed to 95 knots at an altitude of 5,056 feet msl, about 0.7 miles south of the accident site. The next two data points spanning 19 seconds showed a decrease in ground speed to 65 knots at an altitude of 5,020 feet msl, almost directly above the accident site. The remainder of the recorded data depicted a reduction in ground speed and a vertical descent to the accident site. For more information, see the GPS Factual Report within the public docket for this accident.

Examination of the roof structure, parachute release cable and handle assembly, and arming pin was conducted by a Senior Materials Laboratory technician. The cabin roof structure exhibited a disbonded area where the parachute arming-handle mounting-bracket was adhesively bonded to the roof structure. Higher magnification images of the faying surfaces of the adhesive bonding area on the mounting bracket and the roof structure revealed that the mounting bracket was loaded in peel with the disbonding crack propagating from the radiused bend in the bracket toward the square edge. The balance of the faying surfaces were too rough to establish interfacial contact sufficient to allow adhesive wetting between the adherends. Traces of roof structure paint were observed in areas between the faying surfaces.

Examination of the parachute arming handle through-holes with a 5X to 50X stereo- zoom microscope under white light revealed drilled and chamfered holes with a red anodized surface treatment. No heavy scratches, gouges or other indications of abusive use were present.

Examination of the arming pin revealed that permanent bending of the pin shank approximately 90 degrees to the plane of the slot cut through the pin shank. Fretting wear deposits were present on the surface of the arming pin shank consistent with shank contact with the surfaces of the through-holes in the parachute arming handle.

Scanning electron microscopy and standardless semi-quantitative energy-dispersive spectroscopy (ESD) were conducted on the arming-pin shank surfaces. The EDS analysis indicated that the fretting wear deposits are primarily composed of the oxidized constituents of the aluminum alloy used in the parachute arming handle. For further details on the laboratory examination of the arming handle, pin, and cabin roof, see the Materials Laboratory report within the public docket for this accident.

http://registry.faa.gov/N177N

http://tl-ultralight.cz

NTSB Identification: WPR12FA295
14 CFR Part 91: General Aviation
Accident occurred Thursday, July 05, 2012 in Piru, CA
Aircraft: TL ULTRALIGHT SRO STINGSPORT, registration: N177N
Injuries: 2 Fatal.


This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

On July 5, 2012, about 1324 Pacific daylight time, a TL Ultralight SRO Stingsport, N177N, was substantially damaged when it impacted terrain near Piru, California. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91. The certified flight instructor and commercial pilot receiving instruction were fatally injured. Visual meteorological conditions prevailed and no flight plan was filed for the instructional flight. The local flight originated from Whiteman Airpark, Van Nuys,  California, at 1300.

Multiple witnesses driving on Highway 126 within the vicinity of the accident site reported observing the accident airplane descending in a nose low attitude while spinning in a counter-clockwise direction before it descended below a tree line.

Examination of the accident site by the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) revealed that the airplane came to rest upright in an open field. Wreckage debris remained within about 20 feet of the main wreckage and all major structural components of the airplane were present. The wreckage was recovered to a secure location for further examination.



Harry Bell


Michael Boolen


[KHTS] – More than two years after a fatal Piru-area plane crash killed the 2011 SCV Man of the Year and his co-pilot, a federal aviation report shed little light on the circumstances of the incident.

The factual findings, which were released recently on the National Transportation Safety Board website, are expected to be followed within a couple of weeks by a Probable Cause Report, an NTSB official said Tuesday.

The Probable Cause Report is expected to include NTSB investigators’ determination for the cause of the crash.

Harry Bell, 89, and co-pilot, Michael Dwain Boolen, 59, of Pacoima, both died of “blunt force injuries,” according to a report released Thursday in federal officials’ Factual Report.

“Multiple witnesses driving on Highway 126 within the vicinity of the accident site reported observing the accident airplane descending in a nose low attitude while spinning in a counter-clockwise direction before it descended below a tree line,” according to the report.

A federal aviation report detailed the sequence of events and the status of the two men in the cockpit; however, the report fails to identify whether Bell or Boolen was in charge of the aircraft, noting only that both were capable of controlling the craft before its final descent.

The fact-finding reports notes there’s an additional investigation that’s ongoing into the recovered materials, including microscopy and other lab tests.

The report doesn’t identify any mechanical concerns with the aircraft based on a National Transportation Safety Bureau investigation.

The two were flying a TL Ultralight SRO Stingsport, a small two-person propeller-driven aircraft in 2012, when it crashed in Piru about 24 minutes after takeoff from Van Nuys.

The crash site is across the street from the Rancho Camulos historic site, about 100 feet from Highway 126.

Friends stated Boolen was working on a flight review for Bell when the two crashed.

Bell held a commercial pilot certificate with approximately 4,000 hours of airtime logged, and the 89-year-old pilot had a history of high blood pressure and coronary artery disease treated with bypass surgery and medications, according to the FAA medical case review.

He had not renewed his medical certificate since it expired Nov. 30, 2006.

Boolen, a flight instructor, reported on his most recent medical certificate application that he had accumulated a total of 13,000 hours of flight time and 200 hours within the previous six months.

The airplane had accumulated about one hour of flight time since its annual inspection before its final flight.

The plane had a Galaxy Rescue Parachute System, but the system was reportedly undeployed, according to the report.

“The Galaxy Rescue Parachute System’s handle was found displaced from its respective mount location on the cabin roof structure,” the report stated. “The securing pin was found removed and located within the main wreckage. The handle appeared to have remained within its housing and not actuated.”

Sgt. Eric Buschow of the Ventura County Sheriff’s Department said that members of the sheriff’s bomb squad were sent to the scene to deactivate a small rocket device used to deploy a parachute in the event the aircraft experienced an emergency.

“On these lightweights, a parachute can deploy and slow down the landing if they have an emergency,” Buschow said. “For some reason, they didn’t activate it. We had to deactivate it to remove the danger to our officers and the coroner.”


From a previous story on SCVHistory.com | Leon Worden:

Harry Allen Bell was born July 2, 1923, five years after the end of World War I — “the war to end all wars.” In the United States, the 1920s were a decade of extremes: a new prosperity had swept into some parts of the country prompting novelist F. Scott Fitzgerald to write about America’s growing fascination with flappers, jazz, fancy cars, and airplane barnstorming.

On the darker side, the Harding presidency was rocked by scandal when shady land dealings were exposed in California’s Teapot Dome Scheme; discrimination had risen to a high pitch in Oklahoma prompting the governor to declare war on the terrorist activities carried out by the Ku Klux Klan; and the politically astute were becoming alarmed about the growing unrest in Germany and the rise of a fanatical National Socialist Party leader named Adolf Hitler.

These events were a world away from the small Michigan farm that was tended by Harry’s parents, Harry O. and Thelma Bell. Harry and his sister Ruth, who was born a few years later, not only helped out on their parents’ land, but their grandparents’ as well. In a vivid contrast to the bright, flashing lights of America’s big cities, one of Harry’s chores was to keep the oil lamps lit on his grandparents’ farm because they had no electricity.

Harry became an engineer on B-24 bombers, completing 50 missions in Europe before being released stateside. On those missions Harry. learned literally to “act on the fly.” One minute he could be top turret gunner, the next he was rushing to patch up enemy fighter and flak damage, and the next, tending to wounded crew members. Staying alive was a big part of every mission.Harry graduated from high school on June 16, 1938. Besides the typical teenage preoccupation with girls and all things mechanical, Harry developed a love of airplanes that would dramatically shape his future. He enrolled in flying school and just naturally assumed that his country would use his skills when he joined the Army Air Corps right after Pearl Harbor was bombed. His bubble was burst when halfway through pilot training, the Army began pulling men out randomly to engage in active combat.

Perhaps nothing can illustrate more clearly the actions of “Our Country’s Greatest Generation” than Harry’s own reminiscing in a World War II publication:

Our bomb group headquarters was in an old winery in Cerignola, Italy where we could watch girls stomp grapes as we were briefed for our missions. We flew our first two missions individually with a seasoned crew. Then we got an old dog of a plane, an olive-drab aircraft. Now the fun began. Up early and down to the Bomb Group headquarters for our briefing as we watched the Italian girls stomp the grapes. I thought about security and wondered if the girls could pass on anything to the enemy.

From briefing to breakfast, then to a bin where we kept our sheepskins, our parachutes and our flak suits. And then on to our B-24. Pre-flight, takeoff, form up, and climb to 40 below zero, usually about 23,000 feet. We would level off at the assigned altitude following our lead plane. Now it becomes real fun! Oxygen mask on, icicles on your chin, open gun-port windows, nice 140 mph breeze, throat mike, and COLD!

Harry returned from the war with seven battle stars and seven air medals. Of the 1,200 airmen in his 757 Air Squadron, only six hundred made it home.

Back on U.S. soil, it was time to put his war experiences behind him. A young woman who caught his eye at a Michigan dance helped him do that when she consented to be his wife several months later. Harry and Barbara Bell were married on Nov. 17, 1945. The young couple set up housekeeping while Harry completed his studies at Central Michigan College, graduating as a civil engineer.

According to Harry, his first “real” job was in a six-man engineering department for the Los Angeles Transit Lines. That led to a 15-year job working as an associate civil engineer with the office of the Los Angeles County Engineer. Harry opened the County Engineering Office in Lancaster and sat on the County Planning Commission as an advisor on grading and drainage.

Barbara and Harry moved to Lancaster where daughter Janet was born in 1955 and son Ken in 1958. Between business and family obligations, Harry kept his love of flying alive purchasing his own private plane to make annual trips back to his Michigan homestead. Through his association with the Los Angeles Shriners, Harry would also use his plane to fly Third World children suffering from severe injuries and birth defects to Children’s Hospital.

In the early 60s, another civil engineer applying for a grading permit walked into Harry’s office. The two began talking business, but soon found a personal connection that led to a life-long friendship. Ed Bolden, SCV’s 1970 Man of the Year, not only became a friend, but a partner as well, in real estate and engineering businesses.

Harry and Barbara moved their family to Saugus in 1965 and Harry immediately became involved in a myriad of organizations that helped shape our valley into the thriving community it is today. A few of his contributions to the development of the SCV include being one of five local realtors who founded the SCV Real Estate Board, serving on the formation committee of Henry Mayo Newhall Memorial Hospital, and lobbying to make Castaic Lake a public rather than a private entity.

Harry served as president of the Real Estate Board twice and was named a Realtor of the Year two times. In addition to being a Shriner, he is also a Mason 32nd Degree, a founding member of the local Elks Lodge, and an active member of the SCV Rotary Club for 48 years. Rotary International’s annual conventions gave him and Barbara a chance to visit other countries and meet foreign speaking Rotarians who were also dedicated to the Rotary motto “Service Above Self.” One of Harry’s proudest moments as a Rotarian was welcoming his daughter.

Story and Comments:   http://scvnews.com


Michael Boolen and family | Facebook photo





















The plane crashed near buildings and a residence off Highway 126 east of Piru.

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