Showing posts sorted by relevance for query Ray Community Airport, MI (57D). Sort by date Show all posts
Showing posts sorted by relevance for query Ray Community Airport, MI (57D). Sort by date Show all posts

Friday, October 16, 2015

Comp Air 8 Turboprop, N244MS: Accident occurred October 15, 2015 at Ray Community Airport (57D), Michigan

http://registry.faa.gov/N244MS

NTSB Identification: CEN16LA017
14 CFR Part 91: General Aviation
Accident occurred Thursday, October 15, 2015 in Ray, MI
Aircraft: Comp Air CA8, registration: N244MS
Injuries: 1 Minor.

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 may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On October 15, 2015, about 1845 eastern daylight time, a Comp Air Inc. CA8 airplane, N422MS, was substantially damaged while landing at Ray Community Airport (57D), Ray, Michigan. The private pilot had minor injuries. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91 without a flight plan. The cross country flight was en route to 57D.

The pilot reported that while on the base to final turn the left wing dipped. The pilot increased power but experienced difficulties with controlling the airplane. The airplane struck the ground short of the runway and the left wing separated from the fuselage.

FAA Flight Standards District Office:  FAA East Michigan FSDO-23



A 46-year-old Clinton Township man walked away from a plane crash with only small lacerations on his face after the plane he was piloting crashed while approaching Ray Community Airport Oct. 15.

According to a report from the Macomb County Sheriff’s Office, deputies were dispatched at 6:10 p.m. to 59819 Indian Trail, the airport’s address, for a report of a plane crash. When deputies arrived, Ray Township Fire and MedStar Ambulance personnel were on the scene and treating the pilot.

The pilot reportedly told deputies that he was attempting to land the plane at the airport. The plane was a Comp Air 8 Turboprop.

The Sheriff’s Office reports stated that an independent witness said he saw the plane take a “hard left turn” into the ground while approaching the runway.

Weather reports at the time of the crash showed that winds were sustained at 27 knots, or 31 mph, with gusts as high as 29 knots, or 33 mph, with overcast skies.

There is no indication yet that weather played a factor in the crash.

A Federal Aviation Administration investigation into the crash is ongoing. Ray Community Airport is located northwest of the intersection of North Avenue and 27 Mile Road.

- Source:  http://www.candgnews.com



A Clinton Township pilot walked away with apparently minor injuries after his single-prop plane crashed while landing Thursday night at Ray Community Airport in Ray Township, the Macomb County Sheriff's Office said today.

Deputies were sent to the airport's administration office at 59819 Indian Trail for a report of a plane crash at about 6:10 p.m. Personnel from the township fire department and a local ambulance company were treating the 46-year-old pilot, who was the only one in the plane, the sheriff's office said.

The pilot appeared to have cuts on his face and was taken to a local hospital for treatment of non-life-threatening injuries, Lt. John Michalke said. He said the man was wearing a seat belt harness. Michalke did not know why the plane crashed.

The plane is a kit-built Comp Air 8 Turboprop said Tony Molinaro, a spokesman for the Federal Aviation Administration, which is investigating the crash. He also did not know why the plane crashed, but said the plane landed short of the runway. Molinaro said the investigation is expected to take several weeks.

He did not have the name of the pilot or know anything about the man's status as a pilot, such as how long he had been flying.

A witness told authorities that he watched as the plane made a hard left turn into the ground while on approach to runway No. 27, according to the sheriff's office.

Source: http://www.freep.com

Thursday, February 01, 2018

Piper PA-28-140, N5584U, owned and operated by the pilot: Accident occurred May 27, 2017 near Ray Community Airport (57D), Ray Township, Macomb County, Michigan


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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Belleville, Michigan

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/N5584U



Location: Ray, MI
Accident Number: CEN17LA341
Date & Time: 05/27/2017, 1135 EDT
Registration: N5584U
Aircraft: PIPER PA-28
Aircraft Damage: Substantial
Defining Event: Hard landing
Injuries: 1 Serious
Flight Conducted Under: Part 91: General Aviation - Personal 

On May 27, 2017, about 1135 eastern daylight time, a Piper PA-28-140, N5584U, impacted trees, terrain, and a tractor near Ray Township, Michigan. The private pilot on board sustained serious injuries and the airplane was substantially damaged. The airplane was owned and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. No flight plan was filed and day visual meteorological conditions prevailed at the time of the accident.

The pilot was landing at the Ray Community Airport following a 20 minute local flight. On his first attempt to land, he was high on the approach and elected to go around. On the second landing attempt, the pilot said he was long. He said he applied throttle and lost consciousness.

Witnesses reported that the pilot made several landing attempts, but each time the airplane was too fast or too high to land. On the last attempt, the airplane touched down fast about halfway down the 2,495' runway. The airplane skipped, floated, and impacted the runway nose gear first about 1/4 the distance from the end, breaking the nose gear. The airplane bounced and departed the east end of the runway. The airplane continued across a gravel road, through a field, and then struck several small trees and a farm tractor before coming to a stop.

The pilot's flight instructor said the pilot was not competent to operate the airplane. He had previously flown with the pilot and said that his traffic patterns, approaches and landings were very substandard for the certificate he held. The flight instructor discussed this with the pilot following their last flight together, and told the pilot he needed a lot of practice and should be flying with a competent pilot or instructor.

The airplane sustained substantial damage to both wings, the engine and propeller, the engine cowling, and forward fuselage. The nose landing gear was broken aft and the left main landing gear was bent inboard. Flight control continuity was confirmed. An examination of the airplane's engine, and other systems revealed no pre-impact anomalies that contributed to the accident. 



Pilot Information

Certificate: Private
Age: 73, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 3 With Waivers/Limitations
Last FAA Medical Exam: 03/08/2016
Occupational Pilot: No
Last Flight Review or Equivalent: 09/10/2016
Flight Time:  210 hours (Total, all aircraft), 50 hours (Total, this make and model), 150 hours (Pilot In Command, all aircraft) 

Aircraft and Owner/Operator Information

Aircraft Manufacturer: PIPER
Registration: N5584U
Model/Series: PA-28 140
Aircraft Category: Airplane
Year of Manufacture: 1969
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 28-26314
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 07/01/2016, Annual
Certified Max Gross Wt.:
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time:  3715 Hours as of last inspection
Engine Manufacturer: LYCOMING
ELT:
Engine Model/Series:  0-320 SERIES
Registered Owner: On file
Rated Power: 0 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: KMTC
Observation Time: 1058 EDT
Distance from Accident Site: 8 Nautical Miles
Direction from Accident Site: 180°
Lowest Cloud Condition: Few / 300 ft agl
Temperature/Dew Point: 19°C / 15°C
Lowest Ceiling: None
Visibility:  10 Miles
Wind Speed/Gusts, Direction: 5 knots, 150°
Visibility (RVR):
Altimeter Setting: 29.9 inches Hg
Visibility (RVV):
Precipitation and Obscuration:
Departure Point: Ray, MI (57D)
Type of Flight Plan Filed: None
Destination: Ray, MI (57D)
Type of Clearance: None
Departure Time:  EDT
Type of Airspace: 

Airport Information

Airport: Ray Community Airport (57D)
Runway Surface Type: Asphalt
Airport Elevation: 630 ft
Runway Surface Condition: Dry
Runway Used: 9
IFR Approach: None
Runway Length/Width: 2495 ft / 60 ft
VFR Approach/Landing: Traffic Pattern 

Wreckage and Impact Information

Crew Injuries: 1 Serious
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Serious
Latitude, Longitude:  42.736667, -82.888889 (est)

Sunday, May 28, 2017

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

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Belleville, Michigan 

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/N5584U

Location: Ray, MI
Accident Number: CEN17LA341
Date & Time: 05/27/2017, 1135 EDT
Registration: N5584U
Aircraft: PIPER PA-28
Aircraft Damage: Substantial
Defining Event: Hard landing
Injuries: 1 Serious
Flight Conducted Under: Part 91: General Aviation - Personal 

On May 27, 2017, about 1135 eastern daylight time, a Piper PA-28-140, N5584U, impacted trees, terrain, and a tractor near Ray Township, Michigan. The private pilot on board sustained serious injuries and the airplane was substantially damaged. The airplane was owned and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. No flight plan was filed and day visual meteorological conditions prevailed at the time of the accident.

The pilot was landing at the Ray Community Airport following a 20 minute local flight. On his first attempt to land, he was high on the approach and elected to go around. On the second landing attempt, the pilot said he was long. He said he applied throttle and lost consciousness.

Witnesses reported that the pilot made several landing attempts, but each time the airplane was too fast or too high to land. On the last attempt, the airplane touched down fast about halfway down the 2,495' runway. The airplane skipped, floated, and impacted the runway nose gear first about 1/4 the distance from the end, breaking the nose gear. The airplane bounced and departed the east end of the runway. The airplane continued across a gravel road, through a field, and then struck several small trees and a farm tractor before coming to a stop.

The pilot's flight instructor said the pilot was not competent to operate the airplane. He had previously flown with the pilot and said that his traffic patterns, approaches and landings were very substandard for the certificate he held. The flight instructor discussed this with the pilot following their last flight together, and told the pilot he needed a lot of practice and should be flying with a competent pilot or instructor.

The airplane sustained substantial damage to both wings, the engine and propeller, the engine cowling, and forward fuselage. The nose landing gear was broken aft and the left main landing gear was bent inboard. Flight control continuity was confirmed. An examination of the airplane's engine, and other systems revealed no pre-impact anomalies that contributed to the accident. 

Pilot Information

Certificate: Private
Age: 73, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 3 With Waivers/Limitations
Last FAA Medical Exam: 03/08/2016
Occupational Pilot: No
Last Flight Review or Equivalent: 09/10/2016
Flight Time:  210 hours (Total, all aircraft), 50 hours (Total, this make and model), 150 hours (Pilot In Command, all aircraft) 

Aircraft and Owner/Operator Information

Aircraft Manufacturer: PIPER
Registration: N5584U
Model/Series: PA-28 140
Aircraft Category: Airplane
Year of Manufacture: 1969
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 28-26314
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 07/01/2016, Annual
Certified Max Gross Wt.:
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time:  3715 Hours as of last inspection
Engine Manufacturer: LYCOMING
ELT:
Engine Model/Series:  0-320 SERIES
Registered Owner: On file
Rated Power: 0 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: KMTC
Observation Time: 1058 EDT
Distance from Accident Site: 8 Nautical Miles
Direction from Accident Site: 180°
Lowest Cloud Condition: Few / 300 ft agl
Temperature/Dew Point: 19°C / 15°C
Lowest Ceiling: None
Visibility:  10 Miles
Wind Speed/Gusts, Direction: 5 knots, 150°
Visibility (RVR):
Altimeter Setting: 29.9 inches Hg
Visibility (RVV):
Precipitation and Obscuration:
Departure Point: Ray, MI (57D)
Type of Flight Plan Filed: None
Destination: Ray, MI (57D)
Type of Clearance: None
Departure Time:  EDT
Type of Airspace: 

Airport Information

Airport: Ray Community Airport (57D)
Runway Surface Type: Asphalt
Airport Elevation: 630 ft
Runway Surface Condition: Dry
Runway Used: 9
IFR Approach: None
Runway Length/Width: 2495 ft / 60 ft
VFR Approach/Landing: Traffic Pattern 

Wreckage and Impact Information

Crew Injuries: 1 Serious
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Serious
Latitude, Longitude:  42.736667, -82.888889 (est)



RAY TOWNSHIP, Mich. - A plane at Ray Community Airport had a hard landing that sent its pilot to the hospital Saturday, according to the Macomb County Sheriff’s Department.

The plane went off the runway during landing around 11:35 a.m. and hit trees and farm equipment.

The pilot, a man in his early 70s from Sterling Heights, was the only person in the single engine plane, authorities said.

His injuries are believed to be non-life threatening, authorities said.

The Federal Aviation Administration is investigating. 

Story and video:  http://www.clickondetroit.com

Macomb County Sheriff’s Office deputy / evidence technician Joseph Bosek sets up a Faro 3D Laser Scanner to take measurements and pictures of the crash scene with three of the plane's skid marks in the grass. 



Ray Township — The pilot of a Piper PA-28-140 crashed near Ray Community Airport.

John Roberts, captain of Macomb County Sheriff’s Office, said the pilot was alone in the aircraft and was transported by ambulance to a hospital, but he did not know which one. He also did not have an identity for the pilot.

“He is an experienced pilot in his early 70s out of Sterling Heights,” said Roberts. “His injuries are not believed to be life-threatening.” He added, “He’s fortunate.”

Roberts said no one else was injured on the road or adjoining property.

He said a 911 call came in at around 11:35 a.m. that a small plane had crashed on Indian Trial in Ray Township.

“We determined it was a hard landing with a single occupant pilot who was attempting to land,” said Roberts. “He ran off the end of the runway, across the road, through a field and struck some small trees and farm implements.”

He said the Ray Township fire department and an ambulance responded.

“He was removed from the plane and transported to a hospital by Medstar EMS,” said Roberts.

He described the area where the crash happened as rural, within 40 yards of a house when he was going through the field.

“I’m just happy he’s doing as well as he is, having gone through that,” said Roberts.

He added that his department is in contact with the FAA.

“We will be working with them and the investigation will continue,” he said.

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



According to Macomb County Sheriff’s Office Captain John Roberts, the plane made a hard landing, jumped over two ditches and came to rest approximately 75 yards east of Indian Trail. 


RAY TOWNSHIP, Mich. (WXYZ) - The Macomb County Sheriff's Office says a small plane crashed in Ray Township late Saturday morning.

According to the sheriff's office, a man in his 70s was attempting to land at Ray Community Airport near 27 Mile and Indian Trail when he suffered a hard landing. He was the only person on board.

The plane crossed Indian Trail and went into a field before crashing into some trees.

Deputies tell us the man was treated at the scene and taken to the hospital. His injuries are not life threatening.

The Federal Aviation Administration has been notified and will be conducting an investigation.

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









AIRCRAFT:   1969 Piper PA-28-140, N5584U, serial number 28-26314

ENGINE - M&M, S/N:  Lycoming IO-360-D3G, serial number L-26836-27A

PROPELLER – M&M, S/N: Sensenich M74DM K4179

APPROXIMATE TOTAL HOURS (estimated TT & TSMO from logbooks or other information):

ENGINE: As of last annual inspection 7/4/2016, Tach Time 3510.31,

PROPELLER: As of last annual inspection 7/4/2016, Tach Time 3510.31       

AIRFRAME:  As of last annual inspection 7/4/2016, Tach Time 3510.31                  

OTHER EQUIPMENT:     TKM  MX11 Comm., Narco AT150 Transponder, Collins VIR-351 Nav, Collins VIR-251 Comm. , Collins Audio Panel, David Clark 4 Place Intercom, CO Monitor, Unknown ELT

DESCRIPTION OF ACCIDENT:  Pilot attempted to abort the landing and attempted a go around, but the aircraft hit small trees off end of runway.

DESCRIPTION OF DAMAGES:

Nose Bowl, Upper and  Lower Cowling destroyed.
Other than Prop strike, Engine appears intact.
Engine mount is broken and Nose gear is missing.
Firewall and left side of Fuselage is buckled .
Left wing is destroyed. Left MLG appears OK.
Left Wing  rear attach is torn from Fuselage.
Right Wing is destroyed Right MLG torn from mount.
Instrument panel is dented as is Control Yokes, Instruments appear OK.
Interior in good shape, Blood on Co-Pilot carpet and seat.
Flaps and Ailerons appear OK.
Fuselage appears OK from Wing trailing edge back.
Tail Surfaces look OK.         

LOCATION OF AIRCRAFT:  Private Hangar located in Ray, Michigan          

REMARKS: Current Tach Time: 3520.42 hours. Please contact adjuster to inspect wreckage. Logbooks located in adjuster office.
  
Read more here:  http://www.avclaims.com/N5584U.htm

Saturday, February 04, 2012

Pipistrel Virus 912, N325MZ: Fatal accident occurred February 04, 2012 in Ray, Michigan

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
 
http://registry.faa.gov/N325MZ

NTSB Identification: CEN12LA149  

14 CFR Part 91: General Aviation
Accident occurred Saturday, February 04, 2012 in Ray, MI
Probable Cause Approval Date: 01/15/2013
Aircraft: Pipistrel Virus 912, registration: N325MZ
Injuries: 1 Fatal.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

A witness reported that the motorglider engine did not sound normal during the preflight run-up and takeoff. The engine subsequently lost power when the aircraft was about 200 feet above ground level. The motorglider took off to the west and entered a gradual left turn. It impacted a golf course less than a mile from the airport. The duration of the accident flight was about 2 minutes. A postaccident examination revealed an accumulation of debris on the inlet side of the fuel pump screen; however, the debris did not appear to obstruct the screen significantly. The appearance of the debris was similar to the fiberglass material used in the construction of the airframe. The fuel tanks had been repaired shortly before the accident due to damage related to the use of alcohol-containing fuel (ethanol). The engine fuel line did not contain any fuel and the carburetors contained only a minimal amount of fuel.

Although the finding of minimal fuel at the engine was consistent with fuel starvation, a definitive reason for a starvation event could not be determined. According to a carburetor icing probability chart, an airplane operating in the ambient conditions at the time of the accident could expect a serious risk of carburetor icing while at cruise and glide power. Engine operations at low power during ground operations are similar to that of operations at glide power, making the carburetor susceptible to icing prior to takeoff; however, a conclusive determination related to the presence of carburetor icing was not possible. A prescription medication commonly used for the management of anxiety disorders and for insomnia was detected at subtherapeutic levels. However, any impairment of the pilot at the time of the accident could not be determined.

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


A loss of engine power due to fuel starvation for reasons that could not be determined because the postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.


HISTORY OF FLIGHT

On February 4, 2012, at 1120 eastern standard time, a Pipistrel Virus 912 motorglider, N325MZ, was substantially damaged during a forced landing following a loss of engine power shortly after takeoff from Ray Community Airport (57D), Ray, Michigan. The pilot sustained fatal injuries. The aircraft was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from 57D at 1118.

A witness reported that the motorglider engine did not sound as if it was operating normally during the preflight run-up. He added that the engine sounded as if it was "missing" during takeoff, and it subsequently quit when the aircraft was about 200 feet above ground level (agl) after takeoff. He observed the motorglider climbing and descending during the glide prior to the forced landing. He lost sight of the aircraft when it descended below the trees.

Global positioning system (GPS) data related to the accident flight indicated that the motorglider departed runway 27 at 1118. Subsequent position data depicted the motorglider in a gradual left turn southwest of the airport. The final GPS data point was logged at 1120:19 (hhmm:ss) and located about 0.9 miles southwest of the initial data point at the arrival end of runway 27. GPS altitude data depicted the motorglider as high as 822 feet, about 200 feet agl, before it began to descend. The GPS altitude associated with the final data point was 674 feet. The elevation of the runway 27 threshold was 626 feet. The accident site was located on a golf course, about 325 feet south-southeast of the final GPS data point at an approximate elevation of 618 feet.

The motorglider impacted a golf course within 1 mile of the airport. The pilot was transported from the scene in critical condition and subsequently died from injuries received during the accident.

PERSONNEL INFORMATION


The accident pilot held a private pilot certificate with single-engine land airplane and glider ratings. The pilot's most recent application for an airman medical certificate, dated October 5, 2006, was denied. On that application, the pilot indicated a total flight time of 2,433 hours, with 61 hours acquired during the previous 6 months. The pilot's most recent flight review was completed on April 30, 2010.

The pilot's son reported that the pilot had discarded his logbook covering powered aircraft flight time when his medical certificate was denied. The pilot's flight time in gliders was estimated to be about 340 hours.

Regulations [14 CFR 16.23(b)(3)] do not require a person exercising the privileges of a pilot certificate with a glider category rating to hold a medical certificate when operating a glider.

AIRCRAFT INFORMATION


The accident aircraft was a 2007 Pipistrel Virus 912 motorglider, serial number 251VSW9121207. The motorglider was a two-place, high-wing monoplane, with a T-tail empennage and tri-cycle landing gear configuration. Significant portions of the airframe were constructed of composite (fiberglass) materials. The motorglider was powered by an 80-horsepower Rotax 912UL engine.

The accident motorglider was imported to the United States and sold to the accident pilot in December 2007. The motorglider was issued an experimental exhibition glider airworthiness certificate on June 4, 2008. The airworthiness certificate application noted a total of 2 hours on the airframe at that time.

Maintenance records revealed that the most recent inspection was completed on January 11, 2012, at a recording tachometer time of 298 hours. A maintenance entry dated June 25, 2011, indicated that the left and right fuel tanks were repaired due to damage caused by automotive fuel containing ethanol. The recording hour meter reportedly indicated 287 hours at that time. The repair was accomplished in accordance with Pipistrel Special Repair Instruction S.RI 02.r1 (March 5, 2011). The repair involved removing a portion of the upper wing skins in order to access and seal the fuel tanks. The motorglider had been operated about 11 hours since the fuel tank repair.

The Flight Manual stated that the use of fuel with alcohol content is not permitted. The repair instruction provided for the repair and internal protection of semi-integral wing fuel tanks that had been damaged by alcohol blended fuels (ethanol, methanol).

A representative of the manufacturer stated that additional in-line fuel filters are installed after the fuel tank repair in order to retain any residual debris. These filters are normally removed after 5 flight hours, and they were not installed at the time of the postaccident examination. Maintenance records available to the NTSB did not contain an entry denoting installation or removal of the additional filters.

METEOROLOGICAL CONDITIONS


Weather conditions at the Selfridge Air National Guard Base, located about 8 miles southeast of 57D, at 1055, were: Wind from 050 degrees at 3 knots; visibility 10 miles; scattered clouds at 12,000 feet agl; broken clouds at 15,000 feet agl; broken clouds at 18,000 feet agl; temperature 2 degrees Celsius; dew point -1 degrees Celsius, altimeter 30.28 inches of mercury.

At 1155, weather conditions at 57D were: Wind from 090 degrees at 4 knots; visibility 10 miles; few clouds at 3,500 feet agl; scattered clouds at 12,000 feet agl; broken clouds at 17,000 feet agl; temperature 3 degrees Celsius; dew point -2 degrees Celsius, altimeter 30.26 inches of mercury.

FAA guidance related to carburetor icing noted a possibility of serious icing at cruise power under the recorded temperature/dew point conditions.

WRECKAGE AND IMPACT INFORMATION

The motorglider impacted a golf course about 0.9 miles southwest of the airport. The main wreckage, which included the fuselage, engine and left wing, came to rest on a paved golf cart path. The right wing and empennage had separated from the fuselage and were located adjacent to the main wreckage. The forward portion of the fuselage was fragmented and the cockpit area was compromised. The engine was dislocated from the airframe, but remained partially attached to the firewall. The right cockpit door had separated. It came to rest adjacent to a ground impact scar located about 75 feet north of the main wreckage. One propeller blade had separated near the hub and was located about 125 feet north of the main wreckage. The second propeller blade remained attached.

The right flaperon was separated from the wing and located at the accident site. The left flaperon remained attached to the left wing. The rudder and elevators remained attached to the empennage. Flight control continuity was confirmed at the rudder and elevators. Discontinuities in the remainder of the flight control system appeared consistent with separations due to the impact sequence.

A postaccident teardown examination of the engine was conducted under the direct supervision of a Federal Aviation Administration inspector. The examination did not reveal any anomalies related to the cylinders, crankshaft, or valve train. The fuel pump had separated from the engine during the accident sequence and could not be actuated by hand. Teardown examination of the fuel pump revealed an accumulation of debris on the inlet side of the internal pump screen. However, the debris did not appear to significantly obstruct the screen. The debris was similar in appearance and texture to the fiberglass material used in the construction of the composite airframe. The gascolator also contained a minor amount of debris. The carburetors and fuel lines appeared to be free of any debris. The fuel line between the fuel pump and manifold did not contain any fuel when disconnected during the exam. The carburetor float bowls contained only a minimal amount of fuel. Approximately 5 gallons of fuel was recovered from the fuel tanks after the accident.

MEDICAL AND PATHOLOGICAL INFORMATION

An autopsy of the pilot was performed on February 6, 2012. The pilot's death was attributed to multiple injuries sustained in the accident.

The FAA Civil Aerospace Medical Institute toxicology report noted:
50.46 (UG/ML, UG/G) Acetaminophen detected in Urine
Lidocaine detected in Urine
Lidocaine detected in Blood
1.128 (ug/mL, ug/g) Lorazepam detected in Urine
0.058 (ug/mL, ug/g) Lorazepam detected in Blood
45.985 (ug/ml, ug/g) Morphine detected in Urine
0.215 (ug/ml, ug/g) Morphine detected in Blood
Propofol detected in Urine
Propofol detected in Blood
156 (mg/dl) Glucose detected in Urine
Glucose NOT detected in Vitreous
5.8 (%) Hemoglobin A1C detected in Blood

The pilot's son stated that the pilot had some difficulty with his eye sight and had been looking for a magnifying sheet to place over the aircraft multi-function display in order to make it easier to read. The pilot also reportedly had some issues with his hearing. In addition, a noise reduction headset was observed with the pilot at the accident site.

Acetaminophen is an over-the-counter analgesic medication, sold under the trade name Tylenol, commonly used to treat pain and fever. Morphine, Lidocaine, and Propofol are commonly used in hospital emergency treatment settings. Lorazepam is a prescription medication commonly used for the management of anxiety disorders and for insomnia. The medication was detected at sub-therapeutic levels.

ADDITIONAL INFORMATION
The Rotax engine installation manual noted the presence of an electric fuel pump in the standard installation schematic. The accident motorglider was not equipped with an electric fuel pump. A representative of the manufacturer stated that Rotax does not require use of an electrical fuel pump in conjunction with the engine integrated mechanical fuel pump when the fuel is gravity fed from the wing tanks.


NTSB Identification: CEN12LA149 
14 CFR Part 91: General Aviation
Accident occurred Saturday, February 04, 2012 in Ray, MI
Aircraft: Pipistrel Virus 912, registration: N325MZ
Injuries: 1 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 may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On February 4, 2012, about 1120 eastern standard time, a Pipistrel Virus 912 motorglider, N325MZ, was substantially damaged when it impacted a golf course shortly after takeoff from Ray Community Airport (57D), Ray, Michigan. The pilot sustained fatal injuries. The aircraft was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from 57D about 1115.





Huron-Clinton Metroparks police officer Greg Smith and Macomb Sheriff K-9 Unit Sgt. Phil Neumeyer with his K-9 "Bullet" investigate a plane crash on the 11th hole of the Wolcott Mill Metropark Golf Course.

The Sheriff's Department said the plane crashed onto the Wolcott Mill golf course, which is on the grounds of the Huron-Clinton Metroparks.

The pilot was pulled from the wreckage. He suffered a head injury and broken bones. No other passengers were onboard the flight.

On Sunday, Metropark Police Chief George Phifer said that the pilot, a 78-year-old Washington Township man, died from his injuries. The man's name has not been released.

An autopsy will be performed in the next couple of days, Phifer said.

The Sheriff's Department received a 911 call about the plane crashing just short of the 11th hole green.

Phifer said a flight control tower lost contact with the plane shortly after it left the Ray Community Airport at about 11:20 a.m. Saturday.

Ray Community Airport is located on Indian Trail just north of 27 Mile Road and east of Ray Center Road.


The accident occurred a few minutes after 11 a.m. George Phifer, chief of the Metroparks Police Department, said the plane took off from Ray Community Airport, near Indian Trail and 27 Mile Road in Ray Township. Shortly after takeoff, airport personnel lost contact with the plane and notified authorities.

In response to a 911 call from an area resident, members of the Ray Township Fire Department responded to the Wolcott Mill Golf Course, also in Ray Township. The golf course is located near 27 Mile and Ray Center roads, about one mile from the airport. The plane had come to rest between two ponds.

Phifer said emergency medical personnel found the pilot alive, but “unresponsive.” He had suffered visible injuries. No passengers were aboard.

“We had to extricate him from the aircraft,” said Jim DiMaria, chief of the Ray Township Fire Department.

DiMaria said the pilot was an elderly man. He was transported to McLaren Medical Center – Macomb in Mount Clemens.

Authorities did not identify the pilot, but according to Federal Aviation Administration records, the aircraft is registered to Charles Zichichi of Washington Township.

A hospital spokeswoman reported later Saturday a patient admitted under that name was in serious condition.

Because of the pilot’s inability to communicate with emergency personnel, authorities are uncertain what type of trouble the plane might have encountered and what actions the pilot took, Phifer said.

According to the FAA’s online registry, the plane is a Virus 912 experimental craft manufactured by PIPISTREL. The plane was built in 2007. FAA spokesman Roland Herwig said the craft was destroyed.

Representatives from both the FAA and the National Transportation Safety Board were investigating the crash.

DiMaria, the Ray Township fire chief, said members of his department train specifically for airplane crashes because three airports are located within the township borders.

“We’ve responded to several (crashes) over the years,” he said.

Ray Township— A man was in serious condition Saturday morning after the single engine plane he was piloting crashed on a golf course.

Metroparks Police Chief George Phifer said the man, whose identity hasn't been released, took off from the Ray Community Airport shortly after 11 a.m. Saturday.

The airport lost contact with the pilot and notified the Macomb County Sheriff's Department. The Metroparks Police conducted a search for the pilot on their grounds and found the plane had crashed on the 11th hole of the Wolcott Mill Metropark Golf Course. The man suffered head injuries, was treated at the scene and then taken to a local hospital, Phifer said.

The golf course is near 27 Mile and Ray Center roads. The airport is a couple of driving miles from the golf course.

Thursday, February 09, 2012

Pipistrel Virus 912, N325MZ. Accident occurred February 4, 2012 in Ray, Michigan

NTSB Identification: CEN12LA149
 14 CFR Part 91: General Aviation
Accident occurred Saturday, February 04, 2012 in Ray, MI
Aircraft: Pipistrel Virus 912, registration: N325MZ
Injuries: 1 Fatal.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.


HISTORY OF FLIGHT


On February 4, 2012, at 1120 eastern standard time, a Pipistrel Virus 912 motorglider, N325MZ, was substantially damaged during a forced landing following a loss of engine power shortly after takeoff from Ray Community Airport (57D), Ray, Michigan. The pilot sustained fatal injuries. The aircraft was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from 57D at 1118.

A witness reported that the motorglider engine did not sound as if it was operating normally during the preflight run-up. He added that the engine sounded as if it was "missing" during takeoff, and it subsequently quit when the aircraft was about 200 feet above ground level (agl) after takeoff. He observed the motorglider climbing and descending during the glide prior to the forced landing. He lost sight of the aircraft when it descended below the trees.

Global positioning system (GPS) data related to the accident flight indicated that the motorglider departed runway 27 at 1118. Subsequent position data depicted the motorglider in a gradual left turn southwest of the airport. The final GPS data point was logged at 1120:19 (hhmm:ss) and located about 0.9 miles southwest of the initial data point at the arrival end of runway 27. GPS altitude data depicted the motorglider as high as 822 feet, about 200 feet agl, before it began to descend. The GPS altitude associated with the final data point was 674 feet. The elevation of the runway 27 threshold was 626 feet. The accident site was located on a golf course, about 325 feet south-southeast of the final GPS data point at an approximate elevation of 618 feet.

The motorglider impacted a golf course within 1 mile of the airport. The pilot was transported from the scene in critical condition and subsequently died from injuries received during the accident.

PERSONNEL INFORMATION

The accident pilot held a private pilot certificate with single-engine land airplane and glider ratings. The pilot's most recent application for an airman medical certificate, dated October 5, 2006, was denied. On that application, the pilot indicated a total flight time of 2,433 hours, with 61 hours acquired during the previous 6 months. The pilot's most recent flight review was completed on April 30, 2010.

The pilot's son reported that the pilot had discarded his logbook covering powered aircraft flight time when his medical certificate was denied. The pilot's flight time in gliders was estimated to be about 340 hours.

Regulations [14 CFR 16.23(b)(3)] do not require a person exercising the privileges of a pilot certificate with a glider category rating to hold a medical certificate when operating a glider.

AIRCRAFT INFORMATION

The accident aircraft was a 2007 Pipistrel Virus 912 motorglider, serial number 251VSW9121207. The motorglider was a two-place, high-wing monoplane, with a T-tail empennage and tri-cycle landing gear configuration. Significant portions of the airframe were constructed of composite (fiberglass) materials. The motorglider was powered by an 80-horsepower Rotax 912UL engine.

The accident motorglider was imported to the United States and sold to the accident pilot in December 2007. The motorglider was issued an experimental exhibition glider airworthiness certificate on June 4, 2008. The airworthiness certificate application noted a total of 2 hours on the airframe at that time.

Maintenance records revealed that the most recent inspection was completed on January 11, 2012, at a recording tachometer time of 298 hours. A maintenance entry dated June 25, 2011, indicated that the left and right fuel tanks were repaired due to damage caused by automotive fuel containing ethanol. The recording hour meter reportedly indicated 287 hours at that time. The repair was accomplished in accordance with Pipistrel Special Repair Instruction S.RI 02.r1 (March 5, 2011). The repair involved removing a portion of the upper wing skins in order to access and seal the fuel tanks. The motorglider had been operated about 11 hours since the fuel tank repair.

The Flight Manual stated that the use of fuel with alcohol content is not permitted. The repair instruction provided for the repair and internal protection of semi-integral wing fuel tanks that had been damaged by alcohol blended fuels (ethanol, methanol).

A representative of the manufacturer stated that additional in-line fuel filters are installed after the fuel tank repair in order to retain any residual debris. These filters are normally removed after 5 flight hours, and they were not installed at the time of the postaccident examination. Maintenance records available to the NTSB did not contain an entry denoting installation or removal of the additional filters.

METEOROLOGICAL CONDITIONS

Weather conditions at the Selfridge Air National Guard Base, located about 8 miles southeast of 57D, at 1055, were: Wind from 050 degrees at 3 knots; visibility 10 miles; scattered clouds at 12,000 feet agl; broken clouds at 15,000 feet agl; broken clouds at 18,000 feet agl; temperature 2 degrees Celsius; dew point -1 degrees Celsius, altimeter 30.28 inches of mercury.

At 1155, weather conditions at 57D were: Wind from 090 degrees at 4 knots; visibility 10 miles; few clouds at 3,500 feet agl; scattered clouds at 12,000 feet agl; broken clouds at 17,000 feet agl; temperature 3 degrees Celsius; dew point -2 degrees Celsius, altimeter 30.26 inches of mercury.

FAA guidance related to carburetor icing noted a possibility of serious icing at cruise power under the recorded temperature/dew point conditions.

WRECKAGE AND IMPACT INFORMATION

The motorglider impacted a golf course about 0.9 miles southwest of the airport. The main wreckage, which included the fuselage, engine and left wing, came to rest on a paved golf cart path. The right wing and empennage had separated from the fuselage and were located adjacent to the main wreckage. The forward portion of the fuselage was fragmented and the cockpit area was compromised. The engine was dislocated from the airframe, but remained partially attached to the firewall. The right cockpit door had separated. It came to rest adjacent to a ground impact scar located about 75 feet north of the main wreckage. One propeller blade had separated near the hub and was located about 125 feet north of the main wreckage. The second propeller blade remained attached.

The right flaperon was separated from the wing and located at the accident site. The left flaperon remained attached to the left wing. The rudder and elevators remained attached to the empennage. Flight control continuity was confirmed at the rudder and elevators. Discontinuities in the remainder of the flight control system appeared consistent with separations due to the impact sequence.

A postaccident teardown examination of the engine was conducted under the direct supervision of a Federal Aviation Administration inspector. The examination did not reveal any anomalies related to the cylinders, crankshaft, or valve train. The fuel pump had separated from the engine during the accident sequence and could not be actuated by hand. Teardown examination of the fuel pump revealed an accumulation of debris on the inlet side of the internal pump screen. However, the debris did not appear to significantly obstruct the screen. The debris was similar in appearance and texture to the fiberglass material used in the construction of the composite airframe. The gascolator also contained a minor amount of debris. The carburetors and fuel lines appeared to be free of any debris. The fuel line between the fuel pump and manifold did not contain any fuel when disconnected during the exam. The carburetor float bowls contained only a minimal amount of fuel. Approximately 5 gallons of fuel was recovered from the fuel tanks after the accident.

MEDICAL AND PATHOLOGICAL INFORMATION

An autopsy of the pilot was performed on February 6, 2012. The pilot's death was attributed to multiple injuries sustained in the accident.

The FAA Civil Aerospace Medical Institute toxicology report noted:
50.46 (UG/ML, UG/G) Acetaminophen detected in Urine
Lidocaine detected in Urine
Lidocaine detected in Blood
1.128 (ug/mL, ug/g) Lorazepam detected in Urine
0.058 (ug/mL, ug/g) Lorazepam detected in Blood
45.985 (ug/ml, ug/g) Morphine detected in Urine
0.215 (ug/ml, ug/g) Morphine detected in Blood
Propofol detected in Urine
Propofol detected in Blood
156 (mg/dl) Glucose detected in Urine
Glucose NOT detected in Vitreous
5.8 (%) Hemoglobin A1C detected in Blood

The pilot's son stated that the pilot had some difficulty with his eye sight and had been looking for a magnifying sheet to place over the aircraft multi-function display in order to make it easier to read. The pilot also reportedly had some issues with his hearing. In addition, a noise reduction headset was observed with the pilot at the accident site.

Acetaminophen is an over-the-counter analgesic medication, sold under the trade name Tylenol, commonly used to treat pain and fever. Morphine, Lidocaine, and Propofol are commonly used in hospital emergency treatment settings. Lorazepam is a prescription medication commonly used for the management of anxiety disorders and for insomnia. The medication was detected at sub-therapeutic levels.

ADDITIONAL INFORMATION

The Rotax engine installation manual noted the presence of an electric fuel pump in the standard installation schematic. The accident motorglider was not equipped with an electric fuel pump. A representative of the manufacturer stated that Rotax does not require use of an electrical fuel pump in conjunction with the engine integrated mechanical fuel pump when the fuel is gravity fed from the wing tanks.

NTSB Identification: CEN12LA149
 14 CFR Part 91: General Aviation
Accident occurred Saturday, February 04, 2012 in Ray, MI
Aircraft: Pipistrel Virus 912, registration: N325MZ
Injuries: 1 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 may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.


On February 4, 2012, about 1120 eastern standard time, a Pipistrel Virus 912 motorglider, N325MZ, was substantially damaged when it impacted a golf course shortly after takeoff from Ray Community Airport (57D), Ray, Michigan. The pilot sustained fatal injuries. The aircraft was registered to and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from 57D about 1115. 



 Charles Vito Zichichi passed away on February 4, 2012 with his family by his side. He died from injuries sustained while doing what he loved most, flying his power glider. Chuck was born in Detroit, Michigan on November 5, 1933 the son of Vito and Josephine (Agosta) Zichichi. He attended Aero Mechanics School as well as Pershing High School in Detroit and worked at Big Bear Market before serving as a Private First Class in the Army during the Korean Conflict.
Read more:  http://www.legacy.com

Saturday, September 12, 2020

Cessna 414, N698D: Accident occurred August 30, 2020 at Ray Community Airport (57D), Macomb County, Michigan

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. 

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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Belleville, Michigan

Yuli Services Inc

https://registry.faa.gov/N698D

Location: Ray, MI
Accident Number: CEN20LA372
Date & Time: 08/30/2020, 1700 UTC
Registration: N698D
Aircraft: Cessna 414
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal

On August 30, 2020, about 1700 eastern daylight time, a Cessna 414 airplane, N697D, was substantially damaged when it was involved in an accident at the Ray Community Airport (57D), near Ray, Michigan. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A witness, who was a pilot with multiengine experience, reported seeing the airplane taxi onto runway 28 for departure. The airplane stopped on the runway and then the engines went to full power. The airplane accelerated and started to veer to the left and then over corrected to the right and at that point it was going to exit the runway. The the nose of the airplane came up and the airplane attempted to fly in ground effect with both wings wallowing near stall. One wing eventually dropped and the airplane pancaked sideways near the end of runway 28 in the grass field.

The airplane sustained substantial damage including crushing damage to its forward fuselage. The nose of the airplane was bent upward and rearward.

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N698D
Model/Series: 414 Undesignated
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: MTC, 580 ft msl
Observation Time: 2055 UTC
Distance from Accident Site: 8 Nautical Miles
Temperature/Dew Point: 22°C / 15°C
Lowest Cloud Condition: Few / 4500 ft agl
Wind Speed/Gusts, Direction: 5 knots / , 140°
Lowest Ceiling: Broken / 5500 ft agl
Visibility: 10 Miles
Altimeter Setting: 29.89 inches Hg
Type of Flight Plan Filed:
Departure Point:
Destination:

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 Minor
Latitude, Longitude: