Monday, April 29, 2019

Landing Gear Not Configured: Beech 76 Duchess, N3733D; accident occurred April 26, 2019 at St. Charles County Smartt Airport (KSET), Missouri




Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; St. Louis, Missouri

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


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


https://registry.faa.gov/N3733D


Location: St Charles, MO
Accident Number: GAA19CA231
Date & Time: 04/26/2019, 1235 CDT
Registration: N3733D
Aircraft: Beech 76
Aircraft Damage: Substantial
Defining Event: Landing gear not configured
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Instructional

The flight instructor reported that during the instructional flight accomplishing takeoffs and landings, during the seventh landing, the landing checklist was called, but due to the "wind effects", the landing gear was not extended. During the approach, the airplane was configured with the left engine operating normally while the right engine was operating to simulate zero thrust. The airplane touched down on the runway centerline with the landing gear retracted. The airplane slid to the left, exited the runway, and impacted a landing light fixture. The lower fuselage longerons were substantially damaged.

The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Flight Instructor Information

Certificate: Flight Instructor; Commercial
Age: 71, Male
Airplane Rating(s): Multi-engine Land; Single-engine Land; Single-engine Sea
Seat Occupied: Right
Other Aircraft Rating(s): Helicopter
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: Yes
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 2 With Waivers/Limitations
Last FAA Medical Exam: 02/01/2017
Occupational Pilot:Yes
Last Flight Review or Equivalent:
Flight Time: (Estimated)

Student Pilot Information

Certificate: Commercial
Age:45, Male
Airplane Rating(s): Single-engine Land
Seat Occupied:Left
Other Aircraft Rating(s):None
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: Yes
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 1 With Waivers/Limitations
Last FAA Medical Exam: 10/01/2018
Occupational Pilot: Yes
Last Flight Review or Equivalent:
Flight Time: (Estimated)

Aircraft and Owner/Operator Information

Aircraft Make:Beech
Registration: N3733D
Model/Series: 76 No Series
Aircraft Category: Airplane
Year of Manufacture: 1980
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: ME-362
Landing Gear Type: Retractable - Tricycle
Seats: 4
Date/Type of Last Inspection: 100 Hour
Certified Max Gross Wt.: 3900 lbs
Time Since Last Inspection:
Engines: 2 Reciprocating
Airframe Total Time:
Engine Manufacturer: Lycoming
ELT:
Engine Model/Series: O&VO-360 SER
Registered Owner: Dury Aviation Services Inc
Rated Power:
Operator: Dury Aviation Services Inc
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KSET, 436 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time:1754 UTC
Direction from Accident Site: 115°
Lowest Cloud Condition: Clear
Visibility: 10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 17 knots / 10 knots
Turbulence Type Forecast/Actual: None / None
Wind Direction: 310°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.03 inches Hg
Temperature/Dew Point: 18°C / -1°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: St Charles, MO (SET)
Type of Flight Plan Filed: None
Destination: St Charles, MO (SET)
Type of Clearance: None
Departure Time: CDT
Type of Airspace: Class G

Airport Information

Airport: St Charles County Smartt (SET)
Runway Surface Type: Asphalt
Airport Elevation: 436 ft
Runway Surface Condition: Dry
Runway Used: 27
IFR Approach:None
Runway Length/Width: 2000 ft / 75 ft
VFR Approach/Landing: Traffic Pattern

Wreckage and Impact Information

Crew Injuries: 2 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 2 None
Latitude, Longitude: 38.929722, -90.430000 (est)













AIRCRAFT:   1980 BEECH 76 N3733D, s/n: ME-362

Last Annual Inspection on 01/03/19 at Tach 179.8, TTAF 11038.9
                               
ENGINES:    

(2) Lycoming LO-360-A1G6D 

PROPELLERS:  

(1) Hartzell HC M2YR 2CEUF/FB12118B & (1) Hartzell HC M2YR 2CLEUF/FJC7666A                                       

EQUIPMENT: #1 Nav/Com - Collins VHF 251

DME - Collins 451

Transponder - Collins TDR 950

Audio Panel - Collins AMR 350

#2 Nav/Com - Collins VHF 251

ADF - Collins 650

DESCRIPTION OF ACCIDENT: Gear up landing on 04/26/19

DESCRIPTION OF DAMAGES:   Damage includes but may not be limited to: 

Both Propellers,

Both engines experienced a prop strike

Belly skins and possibly ribs           

LOCATION OF AIRCRAFT: St Charles County Airport, St Charles, MO

Read more here:  http://www.avclaims.com

Beech E50, registered to Engen LLC and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91, N29Y: Accident occurred April 26, 2019 in Sheldon, Vernon County, Missouri

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

Additional Participating Entities: 

Federal Aviation Administration / Flight Standards District Office; Kansas City, Missouri
Textron Aviation; Wichita, Kansas 
Lycoming Engines; Williamsport, Pennsylvania 

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


https://registry.faa.gov/N29Y

Location: Sheldon, MO
Accident Number: CEN19LA127
Date & Time: 04/26/2019, 1455 CDT
Registration: N29Y
Aircraft: Beech 50
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal

On April 26, 2019, about 1455 central daylight time, a Beech E50 (Twin Bonanza) airplane, N29Y, sustained substantial damage during a forced landing to a dirt field following a dual partial loss of engine power near Sheldon, Missouri. The commercial pilot, the sole occupant, sustained no injury. The airplane was registered to Engen, LLC, and was operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a visual flight rules personal flight. Day visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The flight originated from the El Dorado Springs Memorial Airport (87K), El Dorado Springs, Missouri about 1445.

The purpose of the flight was to reposition the airplane from 87K to the pilot's home base at the Atkinson Municipal Airport (PTS), Pittsburg, Kansas. The pilot reported this was the airplane's first flight since maintenance work was performed, including the annual inspection, which was completed on the day of the accident by an independent certificated airframe and powerplant mechanic. After departing from 87K and climbing to about 3,000 ft above mean sea level (msl) and on heading of 246°, the pilot configured the airplane for cruise flight.

About 1452, the pilot heard the right engine emit "sputtering" noises and was backfiring. The pilot applied power to the left engine and then noticed a "large smoke trail" was emitting from the left engine about 1 minute after the right engine started emitting "sputtering" noises and was backfiring. The pilot did not have carburetor heat applied and he reported that he always operates with the mixture in the full rich setting. Once the degradation of both engines commenced, the airplane was at an altitude of about 1,700 ft msl (about 800 ft above ground level), and the pilot concluded that the two engines were no longer producing adequate power to remain airborne.

The pilot decided to execute a forced landing to a dirt field that was tilled. During the forced landing sequence, the pilot did not have adequate time to execute an emergency shutdown on both engines as he reported the dual engine degradation and loss of altitude sequence happened fast. The pilot configured the airplane for the forced landing and during the landing roll on the dry dirt, the nose landing gear wheel collapsed, which resulted in substantial damage to the fuselage as shown in figure 1. Once the nose landing gear wheel collapsed up into the fuselage, the nose of the fuselage and the two Hartzell full-feathering metal three-blade propellers impacted the dirt. The pilot, stationed in the front left seat, was able to egress from the airplane without further incident and contacted first responders with his cellular phone from the accident site.

Figure 1 - View of the front of the airplane. 
(Courtesy of the Federal Aviation Administration)

About 60 total gallons of 100 low lead fuel (about 30 gallons in each main fuel tank) were confirmed to be onboard at the time of the accident. The pilot purchased fuel from 87K, and the airport manager obtained a fuel sample from the onsite fuel storage facility and no contamination was noted in the sample. The airport manager further reported that other pilots who obtained fuel around the same time as the accident pilot did not report any issues with the fuel they purchased.

On April 27, 2019, an aviation safety inspector (ASI) from the Federal Aviation Administration (FAA) traveled to the accident site. During the onsite examination by the FAA ASI, no preimpact mechanical malfunctions or failures with the airframe and engine were noted. An examination of the airplane's maintenance records revealed no evidence of uncorrected mechanical discrepancies with the airframe and engine.

The FAA ASI interviewed the mechanic who reported the airplane was transported to 87K for the annual inspection in December 2018 and the annual inspection wasn't started until early March 2019. No major discrepancies were noted during the annual inspection. During the inspection of the fuel sumps, a small amount of water was discovered, but the mechanic reported this was "nothing more than usual" as seen during an annual inspection. No work was performed on the fuel system outside of the inspection. It was discovered that the right engine had a "bad" exhaust valve on one cylinder, and the cylinder was replaced by the mechanic. The mechanic further reported that both engines were ground ran several times at various power settings (including the highest power setting that could be safely accomplished without the airplane moving) during the annual inspection and no discrepancies were noted.

The airplane was recovered from the accident site and was transported to a secure location for a future examination of the airframe and both engines.

The six-seat capacity airplane, serial number EH-16, was manufactured in 1957. The airplane was equipped with two 340 horsepower supercharged Lycoming Engines GSO-480 series engines.

Aircraft and Owner/Operator Information


Aircraft Make: Beech
Registration: N29Y
Model/Series: 50 E50
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: KPTS, 952 ft msl
Observation Time: 1955 UTC
Distance from Accident Site: 24 Nautical Miles
Temperature/Dew Point: 21°C / 4°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: Calm / ,
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.1 inches Hg
Type of Flight Plan Filed: None
Departure Point: El Dorado Springs, MO (87K)
Destination: Pittsburg, KS (PTS)

Wreckage and Impact Information


Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: Unknown
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude: 37.666111, -94.302222 (est) 

Bell 407, N403TD: Incident occurred April 28, 2019 in Newark, New Jersey

Federal Aviation Administration / Flight Standards District Office; Teterboro, New Jersey

Experienced a bird strike, landed without incident.

Helicopter Services LLC

https://registry.faa.gov/N403TD

Date: 28-APR-19
Time: 00:47:00Z
Regis#: N403TD
Aircraft Make: BELL
Aircraft Model: 407
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: SIGHT SEEING
Flight Phase: UNKNOWN (UNK)
City: NEWARK
State: NEW JERSEY

Loss of Engine Power (Partial): Zenith CH 601 HDS Zodiac, N61PG; accident occurred April 27, 2019 near Fuquay/Angier Field Airport (NC78), Angier, North Carolina














Aviation Accident Final Report - National Transportation Safety Board

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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Greensboro, North Carolina

Investigation Docket - National Transportation Safety Board:


Location: Angier, North Carolina
Accident Number: ERA19LA159
Date & Time: April 27, 2019, 15:00 Local
Registration: N61PG
Aircraft: Zenair Zodiac CH601 
Aircraft Damage: Substantial
Defining Event: Loss of engine power (partial)
Injuries: 1 Minor
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

About 10 nautical miles from the destination during a cross-country flight, the airplane's engine began to run rough, cut in and out, and surge. The pilot checked the header fuel tank level and noted that it was nearly full, and he activated the electrically driven fuel pump, but the engine issues continued. The airplane continued to lose altitude and the engine continued to run rough; about 1,000 ft above the ground and about two nautical miles from the destination airport, the pilot decided to reduce engine power to idle and complete a precautionary landing in a field. During the landing roll, the airplane impacted a dirt pile and nosed over, resulting in substantial damage to the fuselage, empennage, and wings.

Fuel was found in the bowls of both carburetors and in both wing tanks and the header tank. Examination of the engine found no preimpact mechanical malfunctions or failures that would have precluded normal operation, and when the engine was test run from an external fuel source using the engine-driven fuel pump, it started and produced power at multiple power settings.

Given the presence of fuel and the lack of anomalies found during the postaccident engine test run, it is possible that the fuel supply to the engine was partially interrupted, which resulted in the engine continuing to run rough to the extent that maintaining altitude was not possible; however, the reason for the interruption of the fuel supply could not be determined.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
A partial loss of engine power due to partial interruption of the fuel supply for undetermined reasons.

Findings

Aircraft (general) - Malfunction
Not determined (general) - Unknown/Not determined

Factual Information

On April 27, 2019, about 1500 eastern daylight time, an experimental amateur-built Zodiac CH 601 HDS, N61PG, was substantially damaged during a forced landing following a partial loss of engine power about one mile from Fuquay/Angier Field Airport (NC78), Angier, North Carolina. The sport pilot sustained minor injuries. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. Day visual meteorological conditions prevailed, and no flight plan was filed for the flight that originated from Gilliam-McConnell Airfield (BQ1), Carthage, North Carolina about 1415, and was destined for NC78.

The pilot reported that he departed BQ1 with about 15 gallons of fuel onboard and proceeded enroute without issue, until about 10 miles from his destination, where the engine "stumbled/stuttered briefly and then resumed running normally." About one or two minutes later, the engine again started to run rough, surge, and cut in and out. The pilot checked the fuel level of the header tank, which indicated it was nearly full, and he turned the electric fuel pump on, in case there was an issue with the engine driven fuel pump. He also observed the engine instruments which all appeared to be normal; however, the engine was "losing more and more power" and the airplane continued to lose altitude. For the remainder of the flight, the engine continued to run rough, and would continue to momentarily "cut out", but the engine did not stop completely.

As the airplane approached about 1,000 ft above ground level, about two miles from NC78, the pilot decided to pull the throttle to idle and approached a field to complete an off-airport landing. The airplane touched down in a rough farm field and during the landing roll, it impacted a pile of dirt and nosed over.

According to Federal Aviation Administration (FAA) airmen records, the pilot held a sport pilot certificate with an endorsement for airplane single-engine land. He did not hold a medical certificate as he was operating under sport pilot rules. He reported that his most recent flight review was in February 2019 and he had accumulated 337 total flight hours, 53 hours of which were in the accident airplane.

According to FAA-airworthiness and airplane maintenance records, the single-engine low-wing airplane was powered by a Rotax 912 ULS engine, that drove a three-blade fixed-pitch propeller. According to airplane logbook entries, an annual condition inspection was completed in December 2018. The airplane and engine had accumulated 723.9 hours of total flight time at the time of the accident.

According to the pilot, the airplane's fuel system contained two 8-gallon wing tanks that fed into one 8-gallon header tank that supplied fuel to the dual carburetors on the engine. A sight gauge mounted on the instrument panel was used to determine how much fuel was contained in the header tank; when the fuel level dropped below about 5 gallons, the pilot could select an electrical switch in the cockpit to transfer fuel from either wing tank via electric automotive fuel pumps installed in each wing tank. Filling the header tank was required about every 25-30 minutes. There were also two additional fuel pumps that supplied fuel to the engine from the header tank; one mechanically driven by the engine and one electrically driven.

The pilot reported that about 10 minutes prior to the engine starting to run rough, he had refilled the header tank from the left wing. He added that when the engine began to run rough, he turned on the electric fuel pump that supported the fuel delivery from the header tank to the engine. He reported that he utilized high octane-93 automotive fuel as per engine manufacturer recommendations and discovered no debris or water in the fuel prior to or after the accident.

At 1500, the weather conditions reported at Harnett Regional Jetport Airport (HRJ), Erwin, North Carolina, 10 miles south of the accident site were, visibility 10 miles, clear skies, wind 240° at 6 knots, temperature 24°C, dew point 2°C, and barometric pressure of 29.91 inches of mercury. According to an FAA Carburetor Icing Probability Chart accounting for the weather conditions about
the time of the accident, the engine was not at risk for carburetor icing at glide or cruise power. 

According to an FAA inspector who examined the airplane at a recovery facility 3 days after the accident, the fuselage, wings, and empennage sustained substantial damage. Both carburetors had fuel in their respective bowls, and fuel was present in both wing tanks and the header tank. The fuel was absent of debris or water contamination.

The engine was further examined about three months after the accident by a representative from the engine manufacturer, who was overseen by an FAA inspector. The airplane's engine-driven fuel pump and fuel lines leading to the carburetors did not contain any remnants of fuel. The engine's spark, compression, and continuity were evaluated by performing an engine test run.

The engine started and operated without issue at multiple power settings when fuel was supplied to the carburetors via the engine-driven fuel pump from an external fuel source. It was not possible to utilize the airplane's existing fuel supply system, due to the damage sustained in the accident. Photographs of the fuel filters provided by the pilot showed no debris or obstruction.

History of Flight

Enroute-cruise Loss of engine power (partial) (Defining event)
Enroute-cruise Off-field or emergency landing
Landing-flare/touchdown Nose over/nose down

Pilot Information

Certificate: Sport Pilot 
Age: 67,Male
Airplane Rating(s): Single-engine land
Seat Occupied: Left
Other Aircraft Rating(s): None 
Restraint Used: 3-point
Instrument Rating(s): None 
Second Pilot Present: No
Instructor Rating(s): None 
Toxicology Performed: No
Medical Certification: Sport pilot None 
Last FAA Medical Exam:
Occupational Pilot: No
Last Flight Review or Equivalent: February 28, 2019
Flight Time: 337 hours (Total, all aircraft), 53 hours (Total, this make and model), 312 hours (Pilot In Command, all aircraft), 11 hours (Last 90 days, all aircraft), 5 hours (Last 30 days, all aircraft), 0 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Zenair
Registration: N61PG
Model/Series: Zodiac CH601 HDS 
Aircraft Category: Airplane
Year of Manufacture: 1999 
Amateur Built: Yes
Airworthiness Certificate: Experimental light sport (Special)
Serial Number: 63888
Landing Gear Type: Tricycle
Seats: 2
Date/Type of Last Inspection: December 11, 2018 Annual
Certified Max Gross Wt.: 1200 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 723.9 Hrs at time of accident 
Engine Manufacturer: Rotax
ELT: Installed
Engine Model/Series: 912 ULS
Registered Owner: 
Rated Power: 100 Horsepower
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: KHRJ,201 ft msl 
Distance from Accident Site: 10 Nautical Miles
Observation Time: 15:00 Local
Direction from Accident Site: 180°
Lowest Cloud Condition: Clear 
Visibility: 10 miles
Lowest Ceiling: Non
e Visibility (RVR):
Wind Speed/Gusts: 6 knots / 
Turbulence Type Forecast/Actual: None / None
Wind Direction: 240° 
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.9 inches Hg 
Temperature/Dew Point: 24°C / 2°C
Precipitation and Obscuration: No
Obscuration; No Precipitation
Departure Point: Carthage, NC (BQ1) 
Type of Flight Plan Filed: None
Destination: Fuquay/Angier, NC (NC78)
Type of Clearance: None
Departure Time: 14:15 Local
Type of Airspace: Class G

Airport Information

Airport: Fuquay/Angier Field NC78
Runway Surface Type: Grass/turf
Airport Elevation: 1070 ft msl
Runway Surface Condition: Rough
Runway Used: 
IFR Approach: None
Runway Length/Width:
VFR Approach/Landing: Forced landing

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 1 Minor
Latitude, Longitude: 35.392501,-78.706665(est)


Location: Angier, NC
Accident Number: ERA19LA159
Date & Time: 04/27/2019, 1500 EDT
Registration: N61PG
Aircraft: Zenair Zodiac CH601
Injuries: 1 Serious
Flight Conducted Under: Part 91: General Aviation - Personal 

On April 27, 2019, about 1500 eastern daylight time, an experimental, amateur-built Zodiac CH 601 HDS, N61PG, was substantially damaged during a forced landing following a partial loss of engine power about 1 mile from Fuquay/Angier Field Airport (NC78), Angier, North Carolina. The sport pilot sustained serious injuries. The airplane was registered to and operated by the pilot under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. Day visual meteorological conditions prevailed, and no flight plan was filed for the flight that originated from Gilliam-McConnell Airfield (BQ1), Carthage, North Carolina about 1415.

The pilot reported that he departed BQ1 with about 15 gallons of fuel. While about 10 miles from his destination of NC78, the engine "stumbled/stuttered briefly and then resumed running normally," but then 1 or 2 minutes later, the same conditions occurred, but were more severe and more sustained. For the remainder of the flight, the engine continued to run rough, and would momentarily "cut out" intermittently, but the engine did not stop completely. When the airplane was about 1,000 ft above ground level and losing altitude, the pilot pulled the throttle to idle and approached a field to complete an off-airport landing. During the subsequent landing roll, the airplane impacted a pile of dirt and nosed over.

According to a Federal Aviation Administration (FAA) inspector who examined the airplane at the recovery facility, the fuselage, wings, and empennage sustained substantial damage. The inspector confirmed that the engine had compression and continuity when the propeller was rotated by hand. Both carburetors had fuel in their respective bowls, and fuel was present in both wing tanks and the header tank.

According to FAA airmen records, the pilot held a sport pilot certificate with a rating for airplane single-engine land. He reported a total of 337 flight hours, 53 hours of which were in the accident airplane.

At 1500, the weather conditions reported at Harnett Regional Jetport Airport (HRJ), Erwin, North Carolina, 10 miles south of the accident site were, visibility 10 miles, clear skies, wind 240° at 6 knots, temperature 24°C, dew point 2°C, and barometric pressure of 29.91 inches of mercury.

The wreckage was retained for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: Zenair
Registration: N61PG
Model/Series: Zodiac CH601 HDS
Aircraft Category: Airplane
Amateur Built: Yes
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: KHRJ, 201 ft msl
Observation Time: 1500 EDT
Distance from Accident Site: 10 Nautical Miles
Temperature/Dew Point: 24°C / 2°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 6 knots / , 240°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 29.91 inches Hg
Type of Flight Plan Filed: None
Departure Point: Carthage, NC (BQ1)
Destination: Fuquay/Angier, NC (NC78)

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: 35.392500, -78.706667 (est)

FUQUAY-VARINA, North Carolina  — A pilot experienced a close call Saturday when his plane went down in a field in Fuquay-Varina.

The pilot, 67-year-old Rolf M. Grandstaff, was taken to Harnett Central Hospital for treatment of minor injuries after crawling to a nearby house, where a family provided help.

The plane went down in the Penley family’s backyard, but they didn’t hear a crash, only a knock at the door.

“This gentleman came to the door and said, ‘My plane had crashed’ and he said, ‘I need help,” Tammy Penley said. “He was very bruised, very cut up. He had several lacerations.”

Authorities in Harnett County said Grandstaff was flying a single-engine private plane when he started having engine issues. He turned the engine off, then coasted into a field behind the Penleys’ home, where the plane flipped over.

“You could see where he had crawled out of the window and where he broke the window and the stuff laying around it,” Penley said.

Penley immediately offered help, first calling 911.

“I called the ambulance and they told us what to do. I got a washcloth and held it on top of his head. He had a pretty serious wound on his head,” she said.

Grandstaff is expected to be OK, and Penley credits a little help from above.

“I’m just thankful he’s alive because, when you see those pictures, it was God that protected him and kept him safe,” she said.

Story and video ➤ https://www.wral.com

Loss of Control on Ground: Bakeng Deuce, N19RG; accident occurred April 27, 2019 at Smith-Reynolds Airport (KINT), Winston-Salem, Forsyth County, North Carolina





Aviation Accident Final Report - National Transportation Safety Board

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Greensboro, North Carolina

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


Location: Winston Salem, North Carolina 
Accident Number: GAA19CA235
Date & Time: April 27, 2019, 16:30 Local 
Registration: N19RG
Aircraft: Bakeng BAKENG DEUCE
Aircraft Damage: Substantial
Defining Event: Loss of control on ground 
Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

The pilot of the tailwheel-equipped airplane reported that, after a three-point landing, during the landing roll, the airplane veered right and ground looped, and the right wing impacted the ground.

The airplane sustained substantial damage to the right wing. 

The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's failure to maintain directional control during landing, which resulted in a ground loop.

Findings

Aircraft Directional control - Not attained/maintained
Personnel issues Aircraft control - Pilot

Factual Information

History of Flight

Landing-landing roll Loss of control on ground (Defining event)
Landing Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Airline transport; Commercial 
Age: 53,Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Rear
Other Aircraft Rating(s): None
Restraint Used: 4-point
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 2 With waivers/limitations 
Last FAA Medical Exam: October 16, 2018
Occupational Pilot: No
Last Flight Review or Equivalent: April 16, 2019
Flight Time: (Estimated) 20000 hours (Total, all aircraft), 8 hours (Total, this make and model), 18000 hours (Pilot In Command, all aircraft), 720 hours (Last 90 days, all aircraft), 240 hours (Last 30 days, all aircraft), 3 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Bakeng 
Registration: N19RG
Model/Series: BAKENG DEUCE No Series 
Aircraft Category: Airplane
Year of Manufacture: 2014 
Amateur Built: Yes
Airworthiness Certificate: Experimental (Special) 
Serial Number: 1017
Landing Gear Type: Tailwheel 
Seats: 2
Date/Type of Last Inspection: June 18, 2018 Condition
Certified Max Gross Wt.: 1650 lbs
Time Since Last Inspection: 
Engines: 1 Reciprocating
Airframe Total Time: 76 Hrs at time of accident
Engine Manufacturer: Lycoming
ELT: C91 installed, not activated
Engine Model/Series: O-320-D2J
Registered Owner:
Rated Power: 160 Horsepower
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC) 
Condition of Light: Night
Observation Facility, Elevation: KINT, 970 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time: 00:54 Local 
Direction from Accident Site: 353°
Lowest Cloud Condition: Clear
Visibility: 10 miles
Lowest Ceiling: None 
Visibility (RVR):
Wind Speed/Gusts: 4 knots / 
Turbulence Type Forecast/Actual: None / None
Wind Direction: 180° 
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.88 inches Hg 
Temperature/Dew Point: 19°C / 4°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Shelby, NC (EHO)
Type of Flight Plan Filed: None
Destination: Winston Salem, NC (INT) 
Type of Clearance: None
Departure Time: 15:00 Local 
Type of Airspace: Class G

Airport Information

Airport: Smith Reynolds INT
Runway Surface Type: Asphalt
Airport Elevation: 969 ft msl
Runway Surface Condition: Dry
Runway Used: 22
IFR Approach: None
Runway Length/Width: 3938 ft / 150 ft
VFR Approach/Landing: Full stop; Straight-in

Wreckage and Impact Information

Crew Injuries: 1 None 
Aircraft Damage: Substantial
Passenger Injuries: 1 None 
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 2 None 
Latitude, Longitude: 36.133609,-80.221946(est)




A plane crash at Smith Reynolds Airport in Winston-Salem caused no injuries Saturday afternoon, according to the Winston-Salem Police Department.

The small private plane, which was coming from Georgia, crashed upon landing around 4:45 p.m.

The pilot and passenger were not injured in the crash, police said.

"The crash happened on Smith Reynolds' property," said Julie Koppang, communications supervisor for the police department. "There were no injuries. It seemed to be very minor."

Forsyth County and Winston-Salem fire department personnel responded to the crash.

The Federal Aviation Administration will investigate the cause of the crash.

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

Bell 206B-3 Jet Ranger III, registered to and operated by Wilbur Ellis Company under the provisions of Title 14 Code of Federal Regulations Part 137 as an agricultural aerial application flight, N206JH: Accident occurred April 26, 2019 in Oakridge, Lane County, Oregon

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

Additional Participating Entities:
Federal Aviation Administration / Flight Standards District Office; Hillsboro, Oregon
Rolls Royce; Indianapolis, Indiana 

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

https://registry.faa.gov/N206JH

Location: Oakridge, OR
Accident Number: WPR19LA122
Date & Time: 04/26/2019, 0700 PDT
Registration: N206JH
Aircraft: Bell 206
Injuries: 1 None
Flight Conducted Under: Part 137: Agricultural 

On April 26, 2019, about 0700 Pacific daylight time, a Bell 206B, N206JH, struck trees during a forced landing in Oakridge, Oregon. The commercial pilot was not injured, and the helicopter sustained substantial damage. The helicopter was registered to and operated by Wilbur Ellis Company under the provisions of Title 14 Code of Federal Regulations Part 137 as an agricultural aerial application flight. Visual meteorological conditions prevailed, and no flight plan had been filed. The local flight departed from a remote landing spot in Oakridge at 0642.

The pilot had just sprayed a load of herbicide on trees, and was maneuvering the helicopter for a final pass to complete the dispersal, when he heard a faint buzzing sound that lasted about 1 to 2 seconds. There were no accompanying annunciator light warnings, and he did not hear any alert horns, but noticed that the engine power turbine (N2) gauge was oscillating about the 11 to 12 o'clock position (50-65% range). The rotor tachometer speed remained within the operating range, and he decided to perform an autorotation. With no landing spots close by, the helicopter landed on sloping tree-covered terrain and rolled over. 

Aircraft and Owner/Operator Information

Aircraft Make: Bell
Registration: N206JH
Model/Series: 206 B
Aircraft Category: Helicopter
Amateur Built: No
Operator: Wilbur Ellis Co
Operating Certificate(s) Held: Agricultural Aircraft (137) 

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KRBG, 509 ft msl
Observation Time: 1453 UTC
Distance from Accident Site: 43 Nautical Miles
Temperature/Dew Point: 9°C / 3°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: Calm / ,
Lowest Ceiling: None
Visibility: 10 Miles
Altimeter Setting: 30.2 inches Hg
Type of Flight Plan Filed: None
Departure Point: Oakridge, OR
Destination: Oakridge, OR 

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude: 43.553889, -122.475833

OAKRIDGE, Oregon -- A helicopter crash has been confirmed in rural Lane County Friday morning.

Lane County Sheriff's Office says the pilot is OK and with the helicopter.

The pilot has refused medical care, the sheriff's office said.

The Bell 206 crashed around 7:15 a.m. Friday while doing agricultural spraying, according to Peter Knudsen with the National Transportation Safety Board.

NTSB confirmed that the pilot was not injured but that the helicopter suffered substantial damage.

As of 9:30 a.m., emergency personnel hadn’t yet made their way to the wreck because it is in such a remote area, about an hour from Oakridge, according to the sheriff's office.

There are no base camps or staging areas at this time, officials said, as they are attempting to reach the site through downed trees and rural terrain.

There is no cell service in the area of the crash. The pilot managed to reach air traffic controllers by radio.

Original article can be found here ➤ https://nbc16.com