Friday, February 17, 2012

Cessna 172S Skyhawk SP, N665SP: Fatal accident occurred February 15, 2012 in North Bend, Washington

Aviation Accident Final Report - National Transportation Safety Board: http://app.ntsb.gov/pdf 

Docket And Docket Items -   National Transportation Safety Board:   http://dms.ntsb.gov/pubdms

Aviation Accident Data Summary -  National Transportation Safety Board:   http://app.ntsb.gov/pdf

NTSB Identification: WPR12FA105
14 CFR Part 91: General Aviation
Accident occurred Wednesday, February 15, 2012 in North Bend, WA
Probable Cause Approval Date: 03/13/2013
Aircraft: CESSNA 172S, registration: N665SP
Injuries: 3 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.

During the local flight, which took place in dark night visual meteorological conditions, several witnesses reported observing the airplane’s lights at a low altitude and hearing the airplane’s engine running before the sound of impact. One witness, a certificated pilot, estimated that when he saw the airplane there was an overcast layer of clouds about 2,000 feet mean sea level (msl) with some lower level clouds and patchy areas of fog. Recorded radar data showed the flight departing the airport and ascending to an altitude of about 2,400 feet msl while traveling in a northeasterly direction. The data subsequently showed that the airplane descended on an east-southeasterly heading to an altitude of about 1,500 feet msl before radar contact was lost. The last recorded radar target was about 6 miles northwest of the accident site, which was located at an elevation of about 1,958 feet msl. The terrain along the pilot’s route of flight ranged between about 500 and 1,000 feet msl; the accident occurred as the airplane approached an area of rising (mountainous) terrain. A postaccident examination of the airframe and engine revealed no evidence of a mechanical malfunction or failure that would have precluded normal operation. Toxicology tests of the pilot revealed a blood alcohol concentration of 154 mg/dl. Federal Aviation Administration regulations prohibit operation of an airplane by persons with blood alcohol concentrations exceeding 40.0 mg/dL. It is likely that the pilot was impaired during the flight, which affected his ability to operate the airplane and maintain clearance from terrain.

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

The pilot's physical impairment due to alcohol, which adversely affected his ability to operate the airplane and to maintain clearance from mountainous terrain while operating in dark night conditions.

HISTORY OF FLIGHT
On February 15, 2012, about 0154 Pacific standard time, a Cessna 172S, N665SP, was substantially damaged following impact with terrain on the western face of Mount Si, near North Bend, Washington. The airplane was registered to Christiansen Aviation Inc., Wilmington, Delaware, and operated by the pilot, under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91. The commercial pilot and his two passengers sustained fatal injuries. Dark night visual meteorological conditions prevailed and no flight plan was filed for the personal flight. The local flight originated from the Renton Municipal Airport (RNT), Renton, Washington, at 0135.

A witness, who was a rated private pilot, reported that while driving in an easterly direction on Interstate 90 (I-90), he observed anti-collision and navigation lights from a low flying airplane that was flying in a southeasterly direction, about 1 mile north of I-90. The witness stated that as I-90 turned to a southwesterly direction, he lost sight of the airplane for a couple of minutes, however, reestablished visual contact with the airplane as he and the airplane approached North Bend. The witness said that at that time, the airplane altered its course and was traveling in a northeasterly direction at an estimated altitude of about 1,000 feet above ground level (agl). The witness added that visibility was at least 3 miles with a high overcast cloud ceiling and a few lower elevation clouds.

Several witnesses located near the accident site reported having heard an impact sound. One witness reported observing the lights of a low flying airplane over his location about 300 to 500 feet agl. The witness stated that he heard the engine rev up and couldn’t see the lights anymore. Shortly thereafter, they heard a pop along with the engine noise suddenly stop.

A review of Federal Aviation Administration (FAA) recorded radar data revealed that the accident airplane was on initial climb from RNT. The airplane ascended to an altitude of about 2,400 feet mean sea level (msl), initially traveling in a northeasterly direction. As the airplane approached the area of Snoqualmie Falls, it descended to an altitude of about 1,500 feet msl, and traveled along an east-southeasterly course. The last recorded radar target was at 0146, about 1.5 miles southwest of Snoqualmie Falls at an altitude of 1,500 feet msl. The last radar target was located about 6.11 miles northwest of the accident site.

According to one of the passenger’s family members, the pilot and the two passengers attended a local hockey game that started at 1930. Following the game, the pilot and passengers went to dinner.

PERSONNEL INFORMATION

The pilot, age 30, held a commercial pilot certificate with 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. A first-class airman medical certificate was issued to the pilot on August 8, 2007, with no limitations stated. Review of the pilot’s logbook revealed that as of the most current logbook entry, dated February 12, 2012, he had accumulated 991.5 hours of total flight time.

AIRCRAFT INFORMATION

The four-seat, high-wing, fixed-gear airplane, serial number (S/N) 172S8069, was manufactured in 1998. It was powered by a Lycoming IO-360-L2A engine, serial number L-27912-51A, rated at 180 horsepower. The airplane was also equipped with a McCauley 1A170E/JHA7660, serial number SH101, fixed pitch propeller. Review of the aircraft maintenance records revealed that the most recent annual inspection was completed on October 10, 2011, at an airframe total time of 5,477.3 hours and engine time since major overhaul of 560.7 hours.

METEOROLOGICAL INFORMATION

A review of recorded data from the Renton Municipal Airport automated weather observation station, located 21 miles east of the accident site, revealed at 0756, conditions were wind from 160 degrees at 5 knots, visibility 6 miles, mist, few clouds at 2,800 feet, overcast cloud layer at 4,000 feet, temperature 2 degrees Celsius, dew point 2 degrees Celsius, and an altimeter setting of 30.25 inches of mercury.

WRECKAGE AND IMPACT INFORMATION

Examination of the accident site revealed that the airplane impacted trees and terrain on an approximate heading of about 120 degrees magnetic at an elevation of about 1,958 feet msl. Multiple topped trees and damaged tree limbs were noted within the wreckage debris path. Both wings, horizontal, and vertical stabilizers were separated and located throughout the wreckage debris path. The fuselage came to rest inverted and the engine remained attached.

Partial flight control cable continuity was established due to the extent of impact damage to the aircraft. The rudder flight control cables remained attached to the control horn at the tail of the aircraft. The ailerons and flap control cables were observed with tension overload separations at the inboard section of each wing and remained attached to the flight controls. The flap actuator was observed with no threads exposed corresponding to a 0 degree flap setting. The elevator control cables were observed with tension overload separations consistent with the separation of the horizontal stabilizer surfaces. The elevator trim tab control cables and actuator remained attached to the tail. The elevator trim actuator was measured and found to be 1.3 inches, which equated to a neutral trim position.

The top spark plug for the number 2 cylinder was removed and exhibited normal wear signatures as per the Champion Aviation Check-a-Plug chart. The fuel distribution valve was opened and observed with no debris or damage to the diaphragm. The propeller was separated from the crankshaft and exhibited leading edge polishing and “S” bending.

The on-site examination of the airframe and engine, revealed no evidence of a mechanical malfunction or failure with the airframe or engine prior to impact. The wreckage was not recovered from the accident site.

MEDICAL AND PATHOLOGICAL INFORMATION

The King County Medical Examiner conducted an autopsy of the pilot on February 16, 2012. The medical examiner determined that the cause of death was “...blunt force trauma...”

The FAA's Civil Aeromedical Institute (CAMI) in Oklahoma City, Oklahoma, performed toxicology tests on the pilot. According to CAMI's report, carbon monoxide, cyanide, volatiles, and drugs were tested, and had positive results for 246 (mg/dL, mg/hg) Ethanol detected in the Urine, 195 (mg/dL, mg/hg) Ethanol detected in the Vitreous, 154 (mg/dL, mg/hg) Ethanol detected in the blood, 92.08 (ug/ml, ug/g) Acetaminophen detected in the urine, 6.852 (ug/ml, ug/g) Dipehnhydramine detected in the blood, and an unspecified amount of Dipehnhydramine in the urine and liver.

ADDITIONAL INFORMATION

Information obtained from CAMI revealed, “…ethanol is primarily a social drug with a powerful central nervous system depressant. After absorption, ethanol is uniformly distributed throughout all tissues and body fluids. The distribution pattern parallels the water content and blood supply of each organ. Postmortem production of ethanol also takes place due to putrefaction processes, but vitreous humor and urine do not suffer from such production to any significant extent in relation to blood. Vitreous humor would normally have about 12% more ethanol than blood if the system is in the post absorptive state, and urine would normally have about 25% more ethanol than blood. The average rate of elimination of ethanol from blood is 18 mg/dL (15-20 mg/dL) per hour.”

CAMI also states that Title 14 CFR 91.17 (a) “prohibits any person from acting or attempting to act as a crewmember of a civil aircraft while having 0.040 g/dL (40.0 mg/dL) or more alcohol in the blood.” Adverse clinical symptoms have been noted with blood ethanol levels as low as 20.0 mg/dL (0.020 g/dL).”






 NTSB Identification: WPR12FA105 
 14 CFR Part 91: General Aviation
Accident occurred Wednesday, February 15, 2012 in North Bend, WA
Aircraft: CESSNA 172S, registration: N665SP
Injuries: 3 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 February 15, 2012, about 0154 Pacific standard time, a Cessna 172S, N665SP, cruised into the western face of Mount Si, about 1.75 miles east of North Bend, Washington. The airplane fragmented upon impacting trees and upsloping mountainous terrain, which resulted in substantial structural damage. The airplane’s registered owner, Christiansen Aviation, Inc., Wilmington, Delaware, leased the airplane to a fixed base flight school operator in Renton, Washington, called AcuWings. The commercial pilot held a certified flight instructor certificate. The pilot and two passengers were fatally injured. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed during the dark nighttime, personal sightseeing flight. No flight plan was filed. The flight originated from Renton Municipal Airport (RNT), about 0135.

A review of Federal Aviation Administration (FAA) recorded radar was performed for an aircraft having performance characteristics of a Cessna 172, that flew on a route from RNT to the accident site vicinity, and that disappeared about the time of the accident near the crash site. Only one target was found that met these criteria. The FAA’s recorded radar shows an aircraft on initial climb out from RNT. The aircraft climbed to 2,400 feet mean sea level (msl), as indicated by its altitude encoding transponder. Initially, the aircraft proceeded in a northeasterly direction. However, as the aircraft approached Snoqualmie Falls, it descended to 1,500 feet and proceeded on an east-southeasterly course. The last radar hit occurred at 0146, at which time the aircraft was about 1 mile southwest of the Falls, and about 1 mile north of Interstate Highway 90 (I-90). During the last minute of recorded flight, the aircraft’s ground speed decreased from about 112 to 106 knots.

The National Transportation Safety Board investigator received information from a witness who stated that about 0150 he was driving in an easterly direction on I-90. The witness holds a private pilot certificate. He reported having observed the anticollision and navigation lights from a low flying airplane that was cruising in a southeasterly direction an estimated 1 mile north of I-90. The witness stated that when I-90 turned southeasterly, he lost sight of the airplane for a couple of minutes. However, he regained visual contact with the airplane as he and the airplane approached North Bend. At that time, the airplane had altered its course and was heading in a northeasterly direction. The witness estimated that the airplane’s altitude was about 1,000 feet above ground level. (North Bend’s elevation is 400 to 500 feet msl.) The witness stated that the visibility was at least 3 miles. There was an overcast ceiling several thousand feet above the ground, with a few lower elevation clouds. Based upon the flight path drawing provided by the witness, the Safety Board investigator notes that when the witness lost visual contact with the airplane, it was flying toward the Mount Si area and was within 3 miles of the crash site.

Beginning about 0154, several persons located in North Bend telephoned 911 and reported having heard an impact sound. At least one witness reported having observed the lights of a low flying airplane and the sound of its engine suddenly stop following its 0153 low altitude easterly direction flight over the city toward Mount Si.

The Safety Board investigator’s on scene examination of the accident site and airplane wreckage revealed evidence of multiple broken tree trunks and felled branches on the mountainside in Mount Si’s Natural Resource Conservation Area. Fragmented airframe components, including both crushed wings, were noted below dozens of felled branches on an approximate 120-degree magnetic track leading to the fuselage, which was upside down. No evidence of preimpact oil leaks, fuel filter blockage, flight control anomalies, or fire was noted at the estimated 1,950-foot msl crash site.

NORTH BEND, Wash. - Two investigators from the National Transportation Safety Board have arrived at a trailhead near the scene of a plane crash near North Bend, said KIRO 7 Eyewitness News reporter Jeff Dubois.

The two did not say anything as they geared up and walked into the woods, said Dubois, who reported earlier that the trailhead was closed to the public for the investigation.

A witness to the crash told Dubois that he called 911 after seeing the plane go down.  He said he heard nothing usual from the plane before it crashed, but he thought he was strange the pilot was flying so low.

 The crash early Wednesday morning of a Cessna 172 killed three people: Liz Redling, Seth Dawson and the pilot, Rob Hill.

Hill was a flight instructor for a company out of Renton Air Field.

According to The Seattle Times, no one at the flight school was aware Hill had taken the plane out late Tuesday night.

No flight plan was filed, and Hill hadn't been in contact with air traffic controllers.