Friday, July 27, 2018

Propeller Contact with Person: Cessna 182P Skylane, N1311S; fatal accident occurred July 26, 2018 at Cleveland Regional Jetport (KRZR), Bradley County, Tennessee

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entities:

Federal Aviation Administration / Flight Standards District Office; Nashville, Tennessee
Federal Aviation Administration / Manufacturing and Inspection District Office; Phoenix, Arizona
Federal Aviation Administration / Aircraft Certification Office; Wichita, Kansas

Aviation Accident Factual Report - National Transportation Safety Board: https://app.ntsb.gov/pdf 

Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms

http://registry.faa.gov/N1311S

Location: Cleveland, TN
Accident Number: ERA18LA199
Date & Time: 07/26/2018, 1648 EDT
Registration: N1311S
Aircraft: Cessna 182
Aircraft Damage: None
Defining Event: AC/prop/rotor contact w person
Injuries: 1 Fatal
Flight Conducted Under: Part 91: General Aviation - Personal

HISTORY OF FLIGHT

On July 26, 2018, about 1648 eastern daylight time, the private pilot of a Cessna 182P, N1311S, was fatally injured when he was struck by the propeller during a preflight inspection of the airplane at the Cleveland Regional Jetport (RZR), Cleveland, Tennessee. The airplane, which was not damaged, was owned by NCFL Ltd., and privately operated under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91. Visual meteorological conditions prevailed for the intended personal flight to Blairsville Airport (DZJ), Blairsville, Georgia.

The pilot's wife reported that they had flown to RZR earlier that day, and her husband performed a normal shutdown of the engine utilizing the mixture control. They performed errands then returned to the airport. While outside the airplane behind the passenger door facing her seat, her husband was performing a preflight inspection of the airplane with the airplane's ignition key in his pocket. She heard the "propeller move" which she described as unusual and heard the engine like it was starting or trying to start. She looked up and noticed her husband fall to the ground. She went to him and thought the propeller stopped at that time, then went inside the fixed-base-operator to summon help.

According to FAA and airport personnel, airport security video did not capture the sequence of events.

AIRCRAFT INFORMATION

Airplane History

The four-place, high-wing airplane, serial number 18264876, was manufactured in 1976. It was powered by a 230-hp Continental O-470-S engine equipped with two independent engine-driven magnetos electrically controlled by an on-condition, key actuated, five position rotary ignition switch mounted on the lower left portion of the pilot's instrument panel.

The pilot purchased the airplane in April 2007, and it remained in his operational control the entire time. According to the pilot's wife, since then, there was no previous instance in which the ignition key could be removed from the switch in an intermediate position, or any position other than the off position. She also indicated that since owning the airplane, there was no previous issue of the key coming out, falling out, or being loose.

Cessna Service Bulletin SEB91-5 Revision 1, dated June 14, 1991, applicable to the accident make and model airplane by serial number and also by the installed ignition switch, specified an inspection and lubrication of the ignition switch; however, there was no requirement to determine if the key could be removed from any position other than off.

Review of the airplane service manual that describes inspection procedures at 50 Hours, 100 Hours, 200 Hours, and special inspection items, and review of 14 CFR Part 43 Appendix D which documents the scope and detail of items to be inspected in the annual or 100-hour inspections revealed no specific mention to check if the key could be removed from any position other than off.

A review of the Pilot's Operating Handbook that documents the preflight inspection items revealed a requirement to verify the ignition switch being in the off position before beginning the outside inspection. The inspection of the propeller specifies to check for nicks, security and oil leaks.

Airworthiness Directive (AD) 93-05-06, applicable to ACS Products Company and Gerdes Products Company ignition switches and the accident make and model airplane by serial number, specified an internal inspection for corrosion, lubrication of the ignition switch, and to determine if a diode or other surge suppresser was installed on the starter solenoid. The AD was required to be completed within 100 hours after the effective date of the AD (April 29, 1993), or at the next annual inspection, whichever occurred first. The AD did not specify a test to determine key to switch integrity, or to determine if the key could be removed from any position other than off. The maintenance records reflect that the AD was originally signed off as being completed on July 27, 1993, at airframe total time of 2,880.7 hours. The next compliance with the AD as part of an annual inspection was on January 10, 2018, at airframe total time 4,895 hours. Based on pilot records excluding the flight earlier that day, the airplane had been operated about 31 hours since the inspection was performed. There was no entry in the airframe maintenance records dating to manufacture indicating replacement of the ignition switch or key.

The mechanic who performed the annual inspection and complied with AD 93-05-06 indicated that he also installed new internal ignition switch contacts and terminal board supplied in kit A3650-2. He also reportedly checked the ignition key to switch integrity in all switch positions other than off reporting no discrepancies. Additionally, as part of his procedures, while the engine was running, he slightly pulled aft on the key to see if it could be removed from any position and also in between positions. The key did not come out in any position other than off.

Postaccident Airplane and Ignition Switch Examination

Examination of the cockpit by representatives of the FAA revealed that the mixture control was in the idle-cutoff position, the throttle was full out, the battery and alternator rocker switches were each in the off position. From the pilot's perspective, the ignition switch appeared to be in the off position; however, on closer inspection the ignition switch was more toward the right magneto position. The ignition switch was photographed and then after installation of the ignition key, the switch was able to be turned counterclockwise to the OFF position. The inspector also noted that the ignition key was easily removable from the ignition switch in the right and left positions. Subsequent testing of the ignition system was performed by a mechanic with FAA oversight. The ignition switch was marked where found (between the off and right positions), and in that position, the right magneto was hot, or not grounded, and the key could be fully removed from the ignition switch that was tightly secured to the instrument panel. When in the off position, the switch did not align with the instrument panel placard marking. The airplane's ignition switch and key were then removed and sent to the FAA for operational testing at the manufacturer's facility with FAA oversight.

Examination of the Gerdes Products Company ignition switch (Model No. A-510, Cessna part number (P/N) C292501-0105) and key were performed at ACS Products Company. The switch was manufactured in April 1976, and there was no record of it being returned to either Gerdes or ACS since being manufactured as neither company repairs switches after delivery. The switch testing was performed using the current procedure for a A-510-2 Ignition Switch (With start), which required verification in part that the key could not be removed in any position other than off. The examination revealed that the key was removable in every position (left, right, both, start, and off). In the as-found position which was marked, testing verified the key could be removed and the right magneto was not grounded. The key tumbler was removed but company personnel reportedly were unable to determine why the key could be removed from the left, right, both, and start positions. With NTSB permission, a black rubber coating was removed from the end of the key that would be held by hand during rotation of the key. The key was marked with "Y11", "USA" and a single line parallel to the long axis. It also could not be determined if the key was the original supplied with the switch as there were no markings to indicate it was an original key (manufacturer logo and key number). The manufacturer representative indicated that the drawing specifies the key to be brass, but does not specify what type of brass. The key P/N is specified to be L1054B from ILCO (Kaba Ilco Corporation). The switch was reassembled and it and the key were sent to the NTSB Materials Laboratory.

According to the NTSB Materials Laboratory factual report, examination of the cut surfaces of the key notches revealed relatively smooth and reflective surface features consistent with a worn surface on the flank of the notch adjacent to the key retention ridge. A smooth and reflective surface consistent with wear was also observed on the tip end of the shank opposite the notched side. Examination of the key cylinder revealed a quadrilateral-shaped area with a smooth and reflective surface consistent with wear on the lower side of the key slot. The location and shape of the worn area was consistent with wear contact with the tip of the key as it was inserted and removed. Although not part of the report, the key material was determined to be brass alloy c377.

MEDICAL AND PATHOLOGICAL

An autopsy examination was not requested by NTSB or FAA, nor was an autopsy or external examination performed by the medical examiner's office. Forensic toxicology was performed on specimens of the pilot by the FAA Bioaeronautical Sciences Research Laboratory, Oklahoma City, Oklahoma. The toxicology report stated no ethanol or tested drugs were detected. Testing for cyanide was not performed and the specimens were insufficient for carbon monoxide analysis.

TESTS AND RESEARCH

Previous NTSB Investigations

A review of the NTSB's database for previous accidents and incidents in which a loss of ignition switch-to-key integrity led to unintended engine startup revealed three previous investigations. In all three, the key was not in the ignition switch which was believed to be in the off position, but the engine started which resulted in injury or uncommanded movement of the airplane. The three cases were NTSB Case Nos. NYC82FNA13, CHI87DER02, and BFO90DIG02.

FAA Service Difficult Reports (SDR's)

A search of FAA SDR's database from 1993 to October 2018 revealed four reports which cited that the ignition key could be removed from the ignition switch in various positions. 

Pilot Information

Certificate: Private
Age: 70, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: None
Other Aircraft Rating(s): None
Restraint Used: None
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: Yes
Medical Certification: BasicMed With Waivers/Limitations
Last FAA Medical Exam: 06/12/2017
Occupational Pilot: No
Last Flight Review or Equivalent: 07/10/2017
Flight Time:  1500 hours (Total, all aircraft), 811 hours (Total, this make and model), 1453 hours (Pilot In Command, all aircraft), 15 hours (Last 90 days, all aircraft), 12 hours (Last 30 days, all aircraft), 2 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N1311S
Model/Series: 182 P
Aircraft Category: Airplane
Year of Manufacture: 1976
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 18264876
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 01/10/2018, Annual
Certified Max Gross Wt.: 2950 lbs
Time Since Last Inspection: 31 Hours
Engines: 1 Reciprocating
Airframe Total Time: 4895 Hours
Engine Manufacturer: Continental
ELT:
Engine Model/Series: O-470-S
Registered Owner: On file
Rated Power: 230 hp
Operator: On file
Operating Certificate(s) Held: None 

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KRZR, 860 ft msl
Distance from Accident Site:
Observation Time: 1655 EDT
Direction from Accident Site:
Lowest Cloud Condition: Few / 6000 ft agl
Visibility: 10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: Calm /
Turbulence Type Forecast/Actual: Unknown / Unknown
Wind Direction:
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.98 inches Hg
Temperature/Dew Point: 31°C / 16°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Cleveland, TN (RZR)
Type of Flight Plan Filed: Unknown
Destination: Blairsville, GA (DZJ)
Type of Clearance: None
Departure Time: 1648 EDT
Type of Airspace: 

Airport Information

Airport: Cleveland Regional Jetport (RZR)
Runway Surface Type: N/A
Airport Elevation: 860 ft
Runway Surface Condition:
Runway Used: N/A
IFR Approach: None
Runway Length/Width:
VFR Approach/Landing: None

Wreckage and Impact Information

Crew Injuries: 1 Fatal
Aircraft Damage: None
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Fatal

Latitude, Longitude:  35.211944, -84.798056 (est)

Location: Cleveland, TN
Accident Number: ERA18LA199
Date & Time: 07/26/2018, 1650 EDT
Registration: N1311S
Aircraft: Cessna 182
Injuries: 1 Fatal
Flight Conducted Under: Part 91: General Aviation - Personal

On July 26, 2018, about 1650 eastern daylight time, the private pilot of a Cessna 182P, N1311S, was fatally injured when he was struck by the propeller during a preflight inspection of the airplane at the Cleveland Regional Jetport (RZR), Cleveland, Tennessee. The airplane, which was not damaged was owned by NCFL Ltd., and privately operated under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the intended personal flight to Blairsville Airport (DZJ), Blairsville, Georgia.

The pilot's wife reported to Federal Aviation Administration personnel that they had flown to RZR earlier that day, and her husband performed a normal shutdown of the engine utilizing the mixture control. They performed errands then returned to the airport. She reported to law enforcement that she was outside the airplane behind the passenger door facing her seat, and her husband was performing a preflight inspection of the airplane. She heard the "propeller move" which she described as unusual and heard the engine like it was starting or trying to start. She looked up and noticed her husband fall to the ground. She thought the propeller stopped at that time, and went inside the fixed-base-operator to summon help. She also indicated that the ignition key was in her husband's pocket at the time of the accident.

The airplane's ignition switch and key were retained for operational testing. 

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N1311S
Model/Series: 182 P
Aircraft Category: Airplane
Amateur Built: No
Operator: On file
Operating Certificate(s) Held: None 

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KRZR, 860 ft msl
Observation Time: 1655 EDT
Distance from Accident Site:
Temperature/Dew Point: 31°C / 16°C
Lowest Cloud Condition: Few / 6000 ft agl
Wind Speed/Gusts, Direction: Calm / ,
Lowest Ceiling:
Visibility:  10 Miles
Altimeter Setting: 29.98 inches Hg
Type of Flight Plan Filed: Unknown
Departure Point: Cleveland, TN (RZR)
Destination:  Blairsville, GA (DZJ)

Wreckage and Impact Information

Crew Injuries: 1 Fatal
Aircraft Damage: None
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Fatal
Latitude, Longitude:  35.211944, -84.798056 (est)


BRADLEY COUNTY, TN (WRCB) - UPDATE: Cleveland police say a Florida man who was struck by an airplane propeller at the Cleveland airport Thursday evening has passed away.

Authorities say 69-year-old Lenny Kramer was flown to Erlanger where he died from his injuries.

A Florida couple was using a Cessna 182 aircraft at the Cleveland Regional Jetport. The plane was grounded and running when Kramer was hit in the head by the plane's spinning propeller.

“His wife was with him at the airport,” Cleveland Police spokeswoman Evie West said. “He was flown out and his wife was taken by ground transport.”

Kramer's wife is okay.

“It was a private plane. I'm not sure if this was the victims’ plane or if it was rented,” said West.“We have to work with the FAA.

The response was fast because the Life Force helicopter is based at the airport.

Sergeant Evie West says everyone is working together to figure out how the propeller hit the man.

"We have to be very careful. Since this is an open investigation, we can't give details,” said West.

The airport is not closed, and the plane involved is secure.

“The ramp is open. I think they will be conducting normal operating procedures,” said West.

The plane will be examined during an investigation. The FAA and NTSB were notified by the Cleveland Police Department.

The FAA will be on the scene Friday morning to determine if it will take over the investigation.

PREVIOUS STORY: Cleveland police say a Florida man who was hit by plane propeller at the Cleveland airport Thursday evening has passed away.

It happened around 4:50 p.m. at Cleveland Regional Jetport on Dry Valley Road NE.

Police tell Channel 3, 69-year-old Lenny Kramer's head was hit by a propeller. He was found near his private plane with a severe head injury.

Kramer was flown from the scene to Erlanger.

Cleveland Police spokeswoman Evie West says Kramer passed away from his injuries.

Police say they are trying to figure out how this happened.

The Federal Aviation Administration (FAA) and National Transportation Safety Board (NTSB) are expected to begin an investigation on Friday morning.

Original article can be found here ➤ http://www.wsmv.com




CLEVELAND, Tenn. (WDEF) – A Florida man dies after getting hit by a propeller at the Cleveland Regional Jetport.

According to Cleveland Police, the man and his wife were at the airport, when somehow, the man was hit by the propeller.

69-year old Lenny Kramer suffered severe head injuries.

LifeForce took him to Erlanger Medical Center in Chattanooga, where he died from his injuries.

The Federal Aviation Administration, and the National Transportation Safety Board will investigate the accident on Friday.

Original article can be found here ➤ https://wdef.com




On Thursday, July 26, 2017, at 4:50 p.m. Cleveland Police Department Officers responded to the Cleveland Regional Jetport, 251 Dry Valley Road NE, on an incident involving an individual injured by an airplane propeller. Lenny Kramer, DOB 07/28/48, age 69, from Florida, was found near his private plane with a severe head injury. Kramer was transported by Life Force to Erlanger Hospital, where he later succumbed to his injuries. Cleveland investigators notified the FAA and NTSB as part of the ongoing investigation.

Sgt. Evie West
Cleveland Police Department

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