Thursday, May 03, 2018

Loss of Lift: Mosquito XE, N725JC; accident occurred May 02, 2018 in Iron Station, Lincoln County, North Carolina






Aviation Accident Final Report - National Transportation Safety Board 

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


Investigation Docket - National Transportation Safety Board:


Location: Iron Station, NC
Accident Number: GAA18CA250
Date & Time: 05/02/2018, 1000 EDT
Registration: N725JC
Aircraft: MICHAEL R ALEXANDER MOSQUITO XE
Aircraft Damage: Destroyed
Defining Event: Loss of lift
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis 

The noncertificated pilot reported that, while practicing hovering the helicopter in his yard, the experimental amateur-built helicopter struck a tree with the tail rotor. He added that, the next thing he knew the helicopter developed "a huge vibration suddenly and [he] had no heading control". Subsequently, the helicopter impacted the ground.

The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The helicopter was destroyed by a post-crash fire.

The pilot reported in the NTSB Pilot/Operator Aircraft Accident/Incident Report form (6120.1) that he should have taken more dual instruction, and he should have chosen a more open area for hover practice. 

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The noncertificated pilot's decision to practice hovering the helicopter in a confined space, which resulted in the tail rotor striking a tree.

Findings

Aircraft Heading/course - Not attained/maintained
Personnel issues Aircraft control - Pilot
Environmental issues Tree(s) - Contributed to outcome
Aircraft Prop/rotor parameters - Not attained/maintained

Factual Information

History of Flight

Maneuvering-hover Loss of lift (Defining event)
Maneuvering-hover Controlled flight into terr/obj (CFIT)

Pilot Information

Certificate: None
Age: 56, Male
Airplane Rating(s): None
Seat Occupied: Single
Other Aircraft Rating(s): None
Restraint Used: None
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:
Flight Time: (Estimated)

Aircraft and Owner/Operator Information

Aircraft Make: MICHAEL R ALEXANDER
Registration: N725JC
Model/Series: MOSQUITO XE NO SERIES
Aircraft Category: Helicopter
Year of Manufacture: 2013
Amateur Built: Yes
Airworthiness Certificate: Experimental
Serial Number: MXE 1123110B
Landing Gear Type: Skid
Seats: 1
Date/Type of Last Inspection: 04/03/2018, Annual
Certified Max Gross Wt.: 612 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 350 Hours at time of accident
Engine Manufacturer: Intec
ELT: Not installed
Engine Model/Series: 800
Registered Owner: On file
Rated Power: 95 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: KIPJ, 875 ft msl
Distance from Accident Site: 3 Nautical Miles
Observation Time: 1355 UTC
Direction from Accident Site: 322°
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 8 knots /
Turbulence Type Forecast/Actual: / None
Wind Direction: 230°
Turbulence Severity Forecast/Actual: / N/A
Altimeter Setting: 30.32 inches Hg
Temperature/Dew Point: 20°C / 9°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Iron Station, NC
Type of Flight Plan Filed: None
Destination: Iron Station, NC
Type of Clearance: None
Departure Time: 1000 EDT
Type of Airspace: Class G

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Destroyed
Passenger Injuries: N/A
Aircraft Fire: On-Ground
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries:1 Minor
Latitude, Longitude: 35.440000, -81.120000 (est)



LINCOLN COUNTY, NC (FOX 46 WJZY) - An Iron Station man is lucky to be alive after his helicopter crashed and caught fire right on his front lawn.

Back in October, Timothy Kniess' wife won the lottery a hundred thousand dollars on a scratch off ticket.

Luck was definitely on their side again today when he was able to escape the crash with just a few scratches.

Neighbors weren’t surprised by the crash. They say they watched Kniess attempt to fly his Mosquito XE helicopter for weeks, just waiting for it all to go wrong.

"Is today the day? I came home and the neighborhood was blocked off and today was the day, it went down,” said neighbor John Aubery. 

North Carolina State Highway Patrol and other law enforcement agencies responded to the crash Wednesday morning, finding the helicopter on fire and Kniess watching his helicopter melt away.

"He was able to crawl away from the crash before it was engulfed in flames,” said NCSHP Trooper Jeffrey Swagger.

The Federal Aviation Administration says Kniess was attempting to hover when the helicopter's tail rotor got caught on a tree branch and the aircraft flew out of control.

"Man bought a helicopter, he woke up one day and said ‘today's the day, I identify as a pilot, bought a helicopter.’ Hell I can't tell a man what to do in his own property,” Aubery said. 

The FAA says investigators will be looking into the pilot's certification. State Highway Patrol tells FOX 46 Kniess wasn't experienced and we couldn't find any certifications under his name.

"Oh I knew it was going down. you don't see someone bouncing a helicopter around their yard like that, oh man this guy isn't going to make it,” said Aubery.

Many just can't believe Kniess' luck.

"The pilot was very fortunate that he didn't receive more injuries than he did,” Trooper Swagger said.

"God was watching out for him, that's all I can say,” said Aubery.

The National Transportation Safety Board will continue with the investigation and determine if any citations will be issued.


Story and video ➤  http://www.fox46charlotte.com


Timothy Kniess, left, was able to crawl away after his helicopter crashed on the front yard of his home.  


A man who hit the lottery last year had a double dose of luck on Wednesday when he was able to crawl away after crashing a helicopter on the front yard of his home.

Investigators from the Federal Aviation Administration said Timothy Kniess, 56, was trying to hover when the helicopter's tail rotor got caught on a tree branch and the aircraft crashed at his home in Iron Station, located about 25 miles northwest of Charlotte.

"He was able to crawl away from the crash before it was engulfed in flames,” said North Carolina State Highway Patrol Trooper Jeffrey Swagger told FOX46.

Kniess suffered some minor scrapes but no serious injuries.

Swagger added that Kniess was "very fortunate" to not have received more serious injuries from the incident.

The 56-year-old was in the news last October when he won $100,000 on a scratch-off ticket after having his wife scratch the ticket, The Gaston Gazette reported at the time.

At the time, he said he planned to purchase a workshop with his winnings but neighbors said Wednesday he recently purchased the  Mosquito XE helicopter.

"Man bought a helicopter, he woke up one day and said ‘today's the day, I identify as a pilot, bought a helicopter.’ Hell I can't tell a man what to do in his own property,” neighbor John Aubery told FOX46.

The FAA said that investigators will be looking into the pilot's certification. The North Carolina State Highway Patrol told FOX 46 that Kniess wasn't experienced, and could not find any certifications under his name.

The National Transportation Safety Board will continue with the investigation, and determine if any citations will be issued. Neighbors said they couldn't believe Kniess' extended luck.

"God was watching out for him, that's all I can say,” Aubery said.

Story and video ➤ http://www.foxnews.com

Cargolux Airlines International, Boeing 747: Incident occurred May 02, 2018 at Dallas/Fort Worth International Airport (KDFW), Texas

Federal Aviation Administration / Flight Standards District Office; Dallas, Texas

Flight 774: While taxiing damaged taxiway lights.

Date: 02-MAY-18
Time: 22:50:00Z
Regis#: UNK
Aircraft Make: BOEING
Aircraft Model: B747
Event Type: INCIDENT
Highest Injury: UNKNOWN
Aircraft Missing: No
Damage: UNKNOWN
Activity: CARGO
Flight Phase: TAXI (TXI)
Operation: 121
Aircraft Operator: CARGOLUX
Flight Number: 774
City: DALLAS
State: TEXAS

Piper PA-44-180 Seminole, N30521: Incident occurred May 02, 2018 at Hampton Roads Executive Airport (KPVG), Norfolk, Virginia

Federal Aviation Administration / Flight Standards District Office; Richmond, Virginia

Aircraft struck a deer on landing, taxied to ramp without incident.

Tradewind Aviation International LLC

http://registry.faa.gov/N30521

Date: 03-MAY-18
Time: 06:35:00Z
Regis#: N30521
Aircraft Make: PIPER
Aircraft Model: 44 180
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: INSTRUCTION
Flight Phase: LANDING (LDG)
Operation: 91
City: NORFOLK
State: VIRGINIA

Piper PA-32RT-300T Turbo Lance II, N24BA: Incident occurred September 26, 2018 and Incident occurred May 02, 2018 at Malad City Airport (KMLD), Oneida County, Idaho

Federal Aviation Administration / Flight Standards District Office; Boise, Idaho

September 26, 2018: Went through a fence during aborted takeoff.

Biz Flyers LLC

https://registry.faa.gov/N24BA

Date: 26-SEP-18
Time: 22:50:00Z
Regis#: N24BA
Aircraft Make: PIPER
Aircraft Model: PA 32RT 300T
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: MINOR
Activity: UNKNOWN
Flight Phase: TAKEOFF (TOF)
Operation: 91
City: MALAD CITY
State: IDAHO

May 02, 2018:  Aircraft landed and nose gear collapsed.

Date: 02-MAY-18

Time: 16:15:00Z
Regis#: N24BA
Aircraft Make: PIPER
Aircraft Model: 32RT 300T
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: PERSONAL
Flight Phase: LANDING (LDG)
Operation: 91
City: MALAD CITY
State: IDAHO

Beech 95-55, N467T: Incident occurred May 02, 2018 at Concord Municipal Airport (KCON), Merrimack County, New Hampshire

Federal Aviation Administration / Flight Standards District Office; Portland, Maine

Aircraft experienced a prop strike on landing.

http://registry.faa.gov/N467T

Date: 02-MAY-18
Time: 18:35:00Z
Regis#: N467T
Aircraft Make: BEECH
Aircraft Model: 95 55
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: MINOR
Activity: UNKNOWN
Flight Phase: LANDING (LDG)
Operation: 91
City: CONCORD
State: NEW HAMPSHIRE

Sportsman GS-2, N3ZY: Incident occurred May 02, 2018 in Winnemucca, Humboldt County, Nevada

Federal Aviation Administration / Flight Standards District Office; Reno, Nevada

Aircraft landed on a highway.

http://registry.faa.gov/N3ZY

Date: 03-MAY-18
Time: 02:30:00Z
Regis#: N3ZY
Aircraft Make: EXPERIMENTAL
Aircraft Model: SPORTSMAN GS 2
Event Type: INCIDENT
Highest Injury: UNKNOWN
Aircraft Missing: No
Damage: NONE
Activity: UNKNOWN
Flight Phase: LANDING (LDG)
Operation: 91
City: WINNEMUCCA
State: NEVADA

Lancair ES, N33KT: Accident occurred May 02, 2018 in Albuquerque, New Mexico

Federal Aviation Administration / Flight Standards District Office; Albuquerque, New Mexico

Aircraft crash landed on a dirt road.

http://registry.faa.gov/N33KT

Date: 02-MAY-18
Time: 15:05:00Z
Regis#: N33KT
Aircraft Make: EXPERIMENTAL
Aircraft Model: LANCAIR ES
Event Type: ACCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: SUBSTANTIAL
Activity: UNKNOWN
Flight Phase: LANDING (LDG)
Operation: 91
City: ALBUQUERQUE
State: NEW MEXICO

Southwest Airlines, Boeing 737-700, N713SW: Incident occurred May 02, 2018 at Cleveland Hopkins International Airport (KCLE), Cuyahoga County, Ohio

Federal Aviation Administration / Flight Standards District Office; Cleveland, Ohio

Emergency landing due to possible cracked passenger window. Landed without further incident.

Southwest Airlines Company: http://registry.faa.gov/N713SW

Date: 02-MAY-18
Time: 14:41:00Z
Regis#: N713SW
Aircraft Make: BOEING
Aircraft Model: 737 7H4
Event Type: INCIDENT
Highest Injury: UNKNOWN
Aircraft Missing: No
Damage: MINOR
Activity: COMMERCIAL
Flight Phase: EMERGENCY DESCENT (EMG)
Operation: 121
Aircraft Operator: SOUTHWEST AIRLINES
Flight Number: 9001
City: CLEVELAND
State: OHIO




(Reuters) - A Newark, New Jersey-bound Southwest Airlines Co (LUV.N) flight made an emergency landing in Cleveland on Wednesday after a window pane cracked in flight, airline officials and the U.S. Federal Aviation Administration said.

No one was injured in the incident, which came two weeks after an engine on a Southwest 737 ripped apart in flight and shattered a window, killing a female passenger in the first U.S. airline passenger fatality since 2009.

The cause of Wednesday’s crack in one of the window’s multiple panes was not immediately known.

The flight, Southwest 957, was traveling to Newark Liberty International Airport from Chicago Midway International Airport with 76 passengers on board. The crew diverted the Boeing Company 737-700 to Cleveland-Hopkins International Airport at about 11 a.m. EDT to inspect a layer of a windowpane, said Southwest spokesman Brian Parrish.

“The aircraft has been taken out of service for maintenance review,” Parrish said.

FAA spokesman Tony Molinaro, who confirmed no one was hurt, said the organization was investigating the incident.

Wednesday’s incident is damaging more to Southwest’s public perception than evidence of any systemic issue, Teal Group Fleet analyst Richard Aboulafia said. The airline said in its first- quarter earnings report it is bracing for a decline in bookings following the April engine blowout.

“It’s unfortunate only from an optics and image standpoint,” Aboulafia said. “Windows are made by window manufacturers. Nothing to do with technology that’s unique to the 737 or to Southwest.”

The FAA on Tuesday ordered additional inspections of fan blades in hundreds of additional engines similar to the one that failed in the deadly Southwest accident on April 17.

Southwest has said it planned to complete ultrasonic inspections on all fan blades on the some 700 planes in its fleet with the CFM56-7B engines, the model involved in last month’s blowout, over the next two weeks, meeting the FAA’s August deadline by mid-May. The CFM engine is made by a joint venture of General Electric Company and France’s Safran.

Southwest said it has not found any cracks on fan blades inspected since the accident.

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

Cessna 510 Citation Mustang, N915CF; March 02, 2020 at John C. Tune Airport (KJWN), Nashville, Davidson County, Tennessee














https://registry.faa.gov/N915CF

AIRCRAFT: 2010 Cessna 510 N915CF, s/n: 5100328, Hobbs:  2039.9    

ENGINES:  Pratt & Whitney PW615F-A    S# PCE-LB0681, New: 2,039.9, Cycles: 1,503

Pratt & Whitney PW615F-A    S# PCE-LB0680, New: 2,039.9, Cycles: 1,503

EQUIPMENT:  Removed for safekeeping.

Garmin GDU 1550

Dual Garmin GDU 1050A

Dual Garmin GMA 1347D

Garmin GMC 710

DESCRIPTION OF ACCIDENT:  Tornado at John Tune Airport, Nashville, Tennessee

DESCRIPTION OF DAMAGE:   Damage includes but may not be limited to:  Lower Chin Fairing, Nose, Both Windscreens, Fuselage – Top, Fuselage – LH Side (Unable to Open Cabin Door), Wing, Both Ailerons and Both Flaps, Vertical Stab, Rudder, Horizontal Stab, Elevator.  Engines have not been borescoped and unsure of any possible FOD damage.  

LOCATION OF AIRCRAFT:  Atlanta Air Recovery

WARRANTY:  There is no warranty, express or implied for the information provided herein or the condition, useability, workability, operability or marketability of the aircraft salvage.  All times are approximate and the logbooks and aircraft should be inspected by each bidder BEFORE BIDDING. Failure of the bidder to view the salvage or wreckage, or confirm any information provided is NOT grounds for a claim or withdrawal of bid after bid closing date.)  

HOURS estimated from logbooks or other information - not guaranteed or warranted

LOGBOOKS WILL BE AVAILABLE FOR REVIEW AT THE STORAGE FACILITY ON JULY 31, 2020

Numerous logbook entries prior to 2016 are not in English.

Insurer reserves the right to reject any and all bids. 

Salvage is as is/where is. 

The posting information is the best to our knowledge. 

An inspection of the salvage is highly recommended. 

LOGS ARE NOT GUARANTEED TO BE ACCURATE OR COMPLETE.

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

Fuel Related: Lancair 360, N92WL; accident occurred May 02, 2018 near West Woodward Airport (KWWR), Oklahoma










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; Oklahoma City, Oklahoma

Investigation Docket - National Transportation Safety Board:


Location: Woodward, OK
Accident Number: CEN18LA156
Date & Time: 05/02/2018, 1620 CDT
Registration: N92WL
Aircraft: LAMINAR Lancair 360
Aircraft Damage: Substantial
Defining Event: Fuel related
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis

The airline transport pilot was conducting a personal flight with a pilot-rated passenger in an experimental, amateur-built airplane. The pilot reported that, during flight at 10,000 ft, the airplane experienced moderate to severe turbulence for a few seconds. Shortly after, the engine stopped producing power without warning. The pilot immediately attempted to restart the engine to no avail. He flew at best glide speed toward the nearest airport, located about 12 nautical miles away, but landed short of the runway in a pasture, during which the airplane encountered sagebrush, which caused the landing gear to collapse as the airplane bounced and skidded to a stop; the fuselage sustained substantial damage.

The examination of the airplane at the accident site revealed that the emergency fuel shutoff valve, which was located on the right side of the center console under the instrument panel, was about 1/4 of the way between the on (horizontal) position and the off (vertical) position. The valve could not be seen by the pilot. Further, the pilot-rated passenger stated that he could not see the emergency fuel shutoff valve. He was not sure if his knee hit the valve handle and shut off the fuel flow from the header fuel tank to the engine during the turbulence event. The onboard flight and engine monitoring system indicated that the airplane was about 10,000 ft mean sea level when it experienced about a 2g vertical acceleration. The engine data indicated a rapid decrease of fuel flow after the 2g acceleration with a coinciding decrease in exhaust gas temperatures and fuel pressure.

About 30 gallons of fuel was drained from the airplane before it was transported to the recovery facility. An engine examination and test run were conducted, and the engine performed satisfactorily. A second test was conducted to determine the effectiveness of the emergency fuel shut off valve and where it needed to be positioned before it cut off all fuel to the engine. There was no indication of a power loss until the valve handle was in the full vertical position, which then caused the engine to stop within about 10 seconds.

The pilot-rated passenger reported that he had recently purchased the airplane and that he and the pilot were flying the airplane to his home base. He stated that although he and the pilot were experienced pilots, neither had any flight time in the airplane except for the orientation flight that the pilot had received.

Given the engine data, it is likely that the pilot-rated passenger's knee inadvertently hit the emergency fuel shutoff valve during the turbulence event and caused it to shut off the fuel flow from the header tank to the engine. Further, had the pilot been familiar with the airplane, he would have known where the fuel selector valve was, regardless of whether it was easy to see, and would have checked it when the engine lost power as a memory item check in the emergency procedures.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot-rated passenger's inadvertent contact with and closure of the emergency fuel shutoff valve, which resulted in the total loss of engine power due to fuel starvation. Contributing to the accident was the pilot's lack of experience in the accident airplane.

Findings

Aircraft Fuel - Fluid level
Personnel issues (general) - Passenger
Personnel issues Total experience w/ equipment - Pilot

Factual Information

On May 2, 2018, about 1620 central daylight time, an experimental, amateur-built Laminar Lancair 360 airplane, N92WL, experienced a total loss of engine power during cruise flight and impacted terrain during a forced landing to a field about 1/2 mile from the Woodward Municipal Airport (WWR), Woodward, Oklahoma. The pilot and pilot-rated passenger were not injured, and the airplane sustained substantial damage. The airplane was owned by an individual and operated by the pilot under the provisions of the Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time of the accident, which was operated on an instrument flight plan. The personal flight departed the Lee Summit Municipal Airport (LXT), Lee's Summit, Missouri, about 1416, and was en route to the Dalhart Municipal Airport, Dalhart, Texas.

The pilot reported he was in cruise flight at 8,000 ft but requested 10,000 ft to stay clear of clouds. As the airplane reached 10,000 ft, the airplane experienced moderate to severe turbulence for a few seconds. Shortly after the turbulence, the engine stopped producing power without any prior indications, such as sputtering. The pilot immediately started a descent and turned on the fuel boost pump, fuel transfer pumps, and changed throttle and mixture settings to try restart the engine but without success.

The pilot-rated passenger declared a MAYDAY and determined the course to the nearest airport, which was WWR located about 12 nautical miles to the southeast. The pilot flew the airplane at best glide airspeed by putting the propeller lever to the coarsest pitch, which produced a glide ratio with a 1,000 to 1,100 fpm rate of descent. About 5,700 ft above mean sea level (msl), the pilot decided that it did not look favorable to make it to the airport, so he pushed the propeller back in and attempted to restart the engine. However, the rate of descent increased to 1,800 to 2,000 fpm. The engine did not restart so the pilot decided to conduct a forced landing to a road, but once he saw that power lines and trees near the road, he decided to land in a pasture. He lowered the landing gear (the flaps were found in the retracted position).

As the airplane landed in the pasture, the airplane encountered sagebrush which caused the landing gear to collapse as the airplane bounced and skidded to a stop. Later, the pilot examined the airplane and the only anomaly he reported was that "the main fuel cutoff valve (hidden in the co-pilot's foot well) was just partially moved." He stated that he was not sure if the valve was moved during the turbulence event or while bouncing across the pasture.

The pilot-rated passenger stated that he could not see the main fuel cutoff valve located on the right side of the center console and under the instrument panel. He was not sure if his knee hit the valve handle and shut off the fuel flow from the header fuel tank to the engine during the turbulence event. He stated that the fuel valve handle was found about ¼ of the way from the on position (horizontal) to the off position (vertical). He stated that the handle moved without much resistance.

The airplane's builder reported that he used 2 similar stainless steel, Teflon coated ball valves with 3/8-inch lines in constructing the airplane. Both valves had orange handles. One of the valve handles was located on the left side of the center console on the pilot's side and under the instrument panel. The pilot's side valve was an emergency gear dump valve. The valve dumped hydraulic pressure to allow the landing gear to lower if the hydraulic pumps were inoperative. The other orange valve handle was the emergency fuel shutoff valve located on the right side of the center console on the passenger's side, which could not be seen by the pilot. The valve shut the fuel off from the airplane's header tank to the engine. The handle for the emergency fuel shutoff valve was in the horizontal position for normal operations. To turn the fuel off, the handle was placed in the vertical position.

The airplane was equipped with a Garmin EFIS which provided flight and engine monitoring data. The SD card was downloaded, and it provided engine performance data that included exhaust gas temperatures (EGT) for all cylinders, tachometer (rpm), fuel flow, oil pressure, and manifold pressure. The flight data indicated that the airplane was at about 10,000 ft msl when it experienced about a 2g vertical acceleration. The data for the engine indicated a rapid decrease of fuel flow within 20 seconds of the 2g acceleration with a coinciding decrease in EGTs and fuel pressure.

The airplane wreckage was partially disassembled and transported to an aircraft recovery facility. About 30 gallons of fuel was drained from the airplane before transporting it to the recovery facility. The header tank was found "nearly" full, and the rest of the fuel came from the wing tanks. The National Transportation Safety Board conducted an examination/engine run at the recovery facility. The engine was a 180-horsepower four-cylinder Lycoming IO-360-C1E6 engine. The engine was started and run at various power settings. The magneto drop was "high" but similar between both left and right magnetos. The engine performed satisfactorily during the test, and a reason for the lost power on the accident flight was not found.

A second test was conducted to determine the effectiveness of the emergency fuel shut off valve and where it needed to be positioned before it cut off all fuel to the engine. The engine was started and run at 2,090 rpm at 18.3 inches of manifold pressure. The emergency fuel shut off valve was slowly moved from the on position (horizontal) to the vertical position. There was no indication of a loss of power until the valve handle was in the full vertical position, which then caused the engine to stop within about 10 seconds.

The pilot-rated passenger reported that he had recently purchased the airplane and that he and the pilot were flying the airplane to his home base. He stated that although he and the pilot were experienced pilots, neither had any flight time in the airplane except for the orientation flight that the pilot had received. 

History of Flight

Enroute-cruise Turbulence encounter
Enroute-cruise Fuel related (Defining event)
Enroute-cruise Fuel starvation
Enroute-cruise Loss of engine power (total)
Emergency descent Off-field or emergency landing
Landing-landing roll Collision with terr/obj (non-CFIT)
Landing-landing roll Landing gear collapse

Pilot Information

Certificate: Airline Transport; Commercial
Age: 41, Male
Airplane Rating(s): Multi-engine Land; Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: Yes
Instructor Rating(s): Airplane Single-engine
Toxicology Performed: No
Medical Certification: Class 2 Without Waivers/Limitations
Last FAA Medical Exam: 03/26/2018
Occupational Pilot:Yes 
Last Flight Review or Equivalent:
Flight Time: 5000 hours (Total, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: LAMINAR
Registration: N92WL
Model/Series: Lancair 360
Aircraft Category:Airplane 
Year of Manufacture: 2016
Amateur Built: Yes
Airworthiness Certificate: Experimental
Serial Number: 719-320-563
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection:  Condition
Certified Max Gross Wt.:
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 90 Hours at time of accident
Engine Manufacturer: Lycoming
ELT: Installed, activated, did not aid in locating accident
Engine Model/Series: IO-360-C1E6
Registered Owner: LOWEN WILLIAM H
Rated Power: 180 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: WWR, 2189 ft msl
Distance from Accident Site: 1 Nautical Miles
Observation Time: 1555 CDT
Direction from Accident Site: 90°
Lowest Cloud Condition: Scattered / 4700 ft agl
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 23 knots / 32 knots
Turbulence Type Forecast/Actual:
Wind Direction: 160°
Turbulence Severity Forecast/Actual:
Altimeter Setting: 29.78 inches Hg
Temperature/Dew Point: 27°C / 15°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Lee Summit, MO (LXT)
Type of Flight Plan Filed: IFR
Destination: Dalhart, TX (DHT)
Type of Clearance: IFR
Departure Time: 1416 CDT
Type of Airspace:

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: 36.443611, -99.515000 (est)

Location: Woodward, OK
Accident Number: CEN18LA156
Date & Time: 05/02/2018, 1620 CDT
Registration: N92WL
Aircraft: LAMINAR Lancair 360
Injuries: 2 None
Flight Conducted Under:  Part 91: General Aviation - Personal 

On May 2, 2018, about 1620 central daylight time, an experimental, amateur-built Laminar Lancair 360 airplane, N92WL, experienced a total loss of engine power during cruise flight and impacted terrain during a forced landing to a field about 1/2 mile from the Woodward Municipal Airport (WWR), Woodward, Oklahoma. The pilot and one passenger were not injured, and the airplane sustained substantial damage. The airplane was owned by an individual and operated by the pilot under the provisions of the Title 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed at the time of the accident, which was operated on an instrument flight plan. The flight departed the Lee Summit Municipal Airport (LXT), Lee's Summit, Missouri, about 1416, and was en route to the Dalhart Municipal Airport, Dalhart, Texas.

At 1555, the surface weather observation at WRR was wind 160° at 23 knots, gusting to 32 knots; visibility 10 miles; scattered clouds 4,700 ft, scattered clouds 5,500 ft, scattered clouds 6,500 ft; temperature 27° C; dew point 15° C; and altimeter 29.78 inches of mercury. Lightning observed distant to northeast, south, and west. 

Aircraft and Owner/Operator Information

Aircraft Manufacturer: LAMINAR
Registration: N92WL
Model/Series: Lancair 360
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: WWR, 2189 ft msl
Observation Time: 1555 CDT
Distance from Accident Site: 1 Nautical Miles
Temperature/Dew Point: 27°C / 15°C
Lowest Cloud Condition: Scattered / 4700 ft agl
Wind Speed/Gusts, Direction: 23 knots/ 32 knots, 160°
Lowest Ceiling: None
Visibility: 10 Miles
Altimeter Setting: 29.78 inches Hg
Type of Flight Plan Filed: IFR
Departure Point: Lee Summit, MO (LXT)
Destination: Dalhart, TX (DHT)

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: 36.443611, -99.515000 (est)




Two men flying an experimental aircraft from Missouri to Arizona forced landed their plane in the field just north of the Woodward Airport on Wednesday afternoon.

The men, Pilot Mark Johnson of Cypress, Texas and passenger Matthew Lafe of Prescott, Arizona were piloting the experimental Lancair 360 back to Arizona after purchasing the aircraft in Missouri, according to Oklahoma Highway Patrol Trooper Steve Nightengale.

At 10,000 feet, the pilot told Nightengale that the aircraft suffered a complete engine failure and they had too much headwind from nearby storms so they tried to make it back to Woodward's airport, where they hoped to make a controlled landing.

However, the aircraft lost altitude and they were forced to put the aircraft dopwn in the field just north of the Woodward Regional Airport.

Called to the scene were law enforcement, firefighters and ambulance service. The two men on the plane appeared to be in good condition upon setting the plane down in the grass.

The investigation is being headed by Trooper Roy Anderson of the Oklahoma Highway Patrol's aircraft incident investigation unit.

Original article can be found here ➤ http://www.woodwardnews.net

Flight Control System Malfunction / Failure: Robinson R22 Mariner, N923SM, accident occurred May 02, 2018 in Panama City, Florida







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; Vestavia Hills, Alabama

Investigation Docket - National Transportation Safety Board:


Location: Panama City, FL
Accident Number: ERA18LA140
Date & Time: 05/02/2018, 1000 CDT
Registration: N923SM
Aircraft: ROBINSON R22
Aircraft Damage: Substantial
Defining Event: Flight control sys malf/fail
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Positioning 

Analysis 

The float-equipped helicopter was in cruise flight at an airspeed of 80 knots and an altitude of 800 ft mean sea level when it slowly started losing airspeed. The commercial pilot responded by pushing the cyclic control forward, but the airspeed continued to decrease, and the helicopter began to lose altitude. The pilot continued to push the cyclic forward until it contacted the control stop; he then realized that he had no cyclic control authority. The helicopter descended with no forward airspeed until it impacted the water. The helicopter floated briefly until waves struck its side and it rolled inverted. Postaccident examination of the helicopter revealed that the main rotor blades were deformed, the fuselage was substantially damaged, and the tail boom was partially separated. Further, the ropes used to tie down the helicopter’s main rotor blades were  found wrapped around the rotor head swashplate and pitch control rods.

Before the flight, the pilot conducted a preflight inspection of the helicopter, which would have included removing the rotor blade tie-down ropes and associated socks that cover the rotor blade tips and storing them under the cockpit seat. However, because the ropes were found wrapped around the swashplate and pitch control rods, it is likely that the tie-down ropes were not properly removed and secured and, at some point during the flight, became entangled with the swashplate and pitch control rods, which prevented the pilot from being able to effectively control the pitch of the helicopter.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's failure to properly remove and secure the tie-down ropes during the preflight inspection, which resulted in the ropes becoming entangled in the rotor head swashplate and pitch control rods during flight and the subsequent loss of pitch control. 

Findings

Personnel issues Incomplete action - Pilot 
Aircraft Pitch control - Attain/maintain not possible 
Personnel issues Preflight inspection - Pilot 
Environmental issues  Water - Contributed to outcome

Factual Information

On May 2, 2018, about 1000 central daylight time, a Robinson R-22 Mariner helicopter, N923SM, operated by N923SM LLC., was substantially damaged during a forced landing near Panama City Beach, Florida. The commercial pilot received minor injuries. The flight was operated in accordance with Title 14 Code of Federal Regulations Part 91 as a positioning flight. Visual meteorological conditions (VMC) prevailed and no flight plan was filed for the flight that departed Perry-Foley Airport (40J) Perry, Florida at 0830, that was destined for Destin Executive Airport (DTS), Destin, Florida.

The pilot reported that about 90 minutes after departing 40J, while in cruise flight at 80 kts and 800 ft mean sea level (msl), the helicopter slowly started losing airspeed; he pushed the cyclic forward, but the airspeed kept decreasing and the helicopter was beginning to lose altitude. He continued to push the cyclic forward until it hit the stop and then realized he had no cyclic authority. The pilot stated there was no forward airspeed and the helicopter continued to descend until it impacted the water with nearly zero forward airspeed and little flare. The helicopter floated briefly until waves struck the side of it and it turned inverted.

Prior to the flight, the pilot was conducting a preflight inspection, which included removal and storage of the blade tie down ropes and associated "socks" that cover the rotor blade tips. During this procedure, the pilot removed the tie down ropes and thought he placed them under the left cockpit seat storage container. In addition, the flight was conducted with the doors off; they were not installed on the helicopter.

A coworker and fellow pilot was flying in formation with the accident helicopter about 700 ft msl. He was at the 5 o'clock position of the accident helicopter at the same altitude when he noticed that the helicopter slowed from about 80 knots to 30 knots in about 15 seconds. He reported that "I felt something wrong and flew to his 10 o'clock position to see what was happening to him." The pilot further reported that the helicopter was descending in a reverse gliding attitude and struck the water with the tail boom first, before rolling upside down.

Witnesses on the ground from the United States Coast Guard and salvage company stated that the tie down ropes used for the rotor blades were found wrapped around the rotor head assembly, swash plate and pitch control rods. The ropes remained in place when the Coast Guard and recovery team arrived prior to the recovery operation taking place.

According to the pilot and Federal Aviation Administration (FAA) records, the pilot held a commercial pilot certificate with a rating for rotorcraft-helicopter as well as a flight instructor certificate with a rating for rotorcraft-helicopter. The pilot reported 467.7 total hours of flight experience and 467.7 of those hours where in the accident helicopter make and model. In the previous 90 and 30 days, the pilot reported about 50 hours and 20 hours respectively.

According to the FAA airworthiness and the helicopter's maintenance records, the two-seat, semi-rigid single-main-rotor, single-engine helicopter, serial number 1923M, was manufactured in 1991 and was issued a standard airworthiness certificate. The helicopter was equipped with floats and powered by a 160-horsepower Lycoming O-320-B2C series engine, which had 4,988.6 hours total time. As of the most recent annual inspection completed on December 28, 2017, the airframe had 6,988.7 hours total time. The current airframe and engine logbooks were on the helicopter at the time of the accident and were lost.

Examination of the helicopter by an FAA inspector revealed that the main rotor blades were deformed, the fuselage was substantially damaged, and the tail boom was partially separated. In addition, a tiedown rope and blade sock used to secure the helicopter rotor blades on the ground was found tightly wrapped around the swash plate and pitch change links of the main rotor.

At 0953, the weather recorded at Northwest Florida Beaches International Airport Panama City (ECP), Florida, about 12 miles north of the accident site included no clouds or restriction to visibility, wind from 140° true at 9 knots, and visibility 10 statute miles. The temperature was 20°C, and the dew point was 18°C. The altimeter setting was 30.27 inches of mercury. 

History of Flight

Prior to flight Preflight or dispatch event
Enroute-cruise Flight control sys malf/fail (Defining event)
Enroute-cruise Loss of control in flight
Emergency descent Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Commercial
Age: 22, Male
Airplane Rating(s): None
Seat Occupied: Right
Other Aircraft Rating(s): Helicopter
Restraint Used: 3-point
Instrument Rating(s): Helicopter
Second Pilot Present: No
Instructor Rating(s): Helicopter
Toxicology Performed: No
Medical Certification: Class 2 Without Waivers/Limitations
Last FAA Medical Exam: 05/08/2018
Occupational Pilot: Yes
Last Flight Review or Equivalent: 04/08/2018
Flight Time:  (Estimated) 467.7 hours (Total, all aircraft), 467.7 hours (Total, this make and model), 369.2 hours (Pilot In Command, all aircraft), 50 hours (Last 90 days, all aircraft), 20 hours (Last 30 days, all aircraft) 


Aircraft and Owner/Operator Information

Aircraft Make: ROBINSON
Registration: N923SM
Model/Series: R22 MARINER
Aircraft Category: Helicopter
Year of Manufacture: 1991
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 1923M
Landing Gear Type: Float; Skid;
Seats: 2
Date/Type of Last Inspection: 12/28/2017, Annual
Certified Max Gross Wt.: 1369 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 6988.7 Hours as of last inspection
Engine Manufacturer: LYCOMING
ELT: Not installed
Engine Model/Series: O-320-B2C
Registered Owner: N923SM LLC
Rated Power: 160 hp
Operator: N923SM LLC
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: ECP, 68 ft msl
Distance from Accident Site: 12 Nautical Miles
Observation Time: 0953 CDT
Direction from Accident Site: 320°
Lowest Cloud Condition: Clear
Visibility:  
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 9 knots /
Turbulence Type Forecast/Actual: /
Wind Direction: 140°
Turbulence Severity Forecast/Actual: /
Altimeter Setting: 30.27 inches Hg
Temperature/Dew Point: 20°C / 18°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: PERRY, FL (40J)
Type of Flight Plan Filed: None
Destination: DESTIN, FL (DTS)
Type of Clearance: None
Departure Time: 0830 EST
Type of Airspace: Class G

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: 30.173889, -85.807500 (est)


PANAMA CITY BEACH — The pilot of a Robinson R22 helicopter that crashed in the Gulf of Mexico near Carillon Beach Resort made it to shore safe and uninjured Wednesday morning, though the same could not be said for his aircraft.

Witnesses reported seeing the R22, a light, single-bladed helicopter about 28 feet long, flying with another, larger helicopter moments before the crash. Shauna Rutt, who was laying on the beach with her mother, remembered seeing the larger helicopter flying up and down the beach the day before. Helicopters are a common sight in the area, ferrying tourists out for spectacular views of the Gulf.

When the R22 began to lose altitude, she didn’t think anything of it. The aircraft had buoys on its skids allowing it to float and for a moment she thought the pilot was attempting a water landing.

“At first I thought, ’This is really cool, a landing right in front of us,” she said.

Then, she noticed the propellers were barely spinning. The helicopter took a nose dive into the Gulf and for several heart-stopping moments was submerged.




Less than a minute later, the helicopter popped back up to the surface with the pilot - the lone occupant - clinging to the buoy. Rutt said he climbed onto the helicopter, floating belly-up between the first and second sandbars, and waited for a rescue.

The crash triggered a massive emergency response, with the Bay County Sheriff’s Office, Fish and Wildlife, US Coast Guard, Panama City Beach Police Department, Panama City Beach and Surf and even several lifeguards answering the call. Numerous first responders jumped on paddleboards and made their way out to the pilot, who made it back on shore with “just a little salt water ingestion,” according to BCSO Lt. Chad King.

Chriss and Monika Morrisson, who live nearby, ran down to the beach expecting the worst. They stood together on the white sand, nervously watching the Coast Guard vessel keeping an eye on the overturned helicopter.

“I am just so happy he walked away from it,” Chriss Morrison remarked.

After the excitement died down, the wreck attracted quite a crowd, with about two dozen bystanders out on the water line watching the upturned helicopter bob in the surf, a buoy emblazoned with “Boatpix.com” sticking up in the air.

With the help of its two buoys and a decent wind, the wreck floated about a half mile west down the beach before drifting in far enough to get stuck on the first sandbar while emergency crews waited for the Federal Aviation Administration to respond and begin its investigation. At one point, the helicopter’s door was pushed open, the pilot’s belongings drifting away into the Gulf.




According to the FAA, the downed R22 Mariner was a commercial helicopter built in 1991 and was most recently registered in 2014. Also according to the FAA, an aircraft’s owner is responsible for removing an aircraft from a crash site. The FAA will be investigating the crash, and the National Transportation Safety Board will issue a probable cause.

When the R22 emerged from the Gulf later in the afternoon and was flipped right-side up, it was clear the crash could have been much worse. All of the glass had shattered in the impact, the snapped propeller hung at an awkward angle like a broken arm, and the tail lay several feet away, completely severed.

The name of the pilot has not yet been released. Efforts to reach Boatpix.com were unsuccessful, but a website for the company says they operate out of West Palm Beach, shooting photos of boats, primarily at events, which they then sell back to the owners. Helicopters operated by the company, many of them the same R22 model or the slightly larger R44 model, have been involved in several accidents, including one near Oaks Island Pier in Brunswick County, North Carolina in 2012 and over Lake Travis in Austin, Texas in May 2008. 

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