Wednesday, July 10, 2019

Piper PA-24 Comanche, N5015P: Incident occurred July 09, 2019 at Ramona Airport (KRNM), San Diego County, California

Federal Aviation Administration / Flight Standards District Office; San Diego, California

Aircraft experienced landing gear problem on landing roll-out.

First Flight Corporation

https://registry.faa.gov/N5015P

Date: 09-JUL-19
Time: 18:25:00Z
Regis#: N5015P
Aircraft Make: PIPER
Aircraft Model: PA24
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: MINOR
Activity: INSTRUCTION
Flight Phase: LANDING (LDG)
Operation: 91
City: RAMONA
State: CALIFORNIA




RAMONA, California  — The pilot of a light airplane with landing gear trouble made a non-injury hard landing at Ramona Airport Tuesday.

The single-engine aircraft came down on its “belly” on the runway of the small airport on Montecito Road and safely slid to a halt shortly before 11:30 a.m., Cal Fire Capt. Thomas Shoots said.

No fire resulted, and the two occupants of the plane were unhurt, Shoots said.

Original article ➤ https://fox5sandiego.com

Beechcraft 65 (U-8F) Queen Air, N62069: Accidents occurred June 17, 2021, July 09, 2019 and February 22, 2019

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 Entities:
Federal Aviation Administration / Flight Standards District Office; Wichita, Kansas
Textron Aviation; Wichita, Kansas
Bemidji Aviation; Bemidji, Minnesota 

Bemidji Aviation Services Inc


Location: Goodland, KS 
Accident Number: CEN21LA274
Date & Time: June 16, 2021, 19:05 Local
Registration: N62069
Aircraft: Beech U-8F
Injuries: 1 Minor
Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled

On June 16, 2021, at 1905 mountain daylight time, a Beech U-8F airplane, N62069, was substantially damaged when it was involved in an accident at Goodland Municipal Airport (GLD), Goodland, Kansas. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 135 cargo flight.

The pilot stated that while starting the right engine he heard a loud bang and noticed flames coming out of the right wing. An airport surveillance video captured images of flames from the right wing for about 1 second. The pilot shut down the right engine with the mixture control and egressed the airplane.

Examination revealed damage to the outboard 12 ft of the right wing, with the forward spar deflected significantly aft and the right-wing leading edge curled aft. The outboard aft fuel bladder for the right wing was removed and observed to be in a degraded condition, with indications of fire damage. Wiring for the navigation light had a conductor exposed in two locations. The fuel bladder and right-wing wiring bundle were retained for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: Beech 
Registration: N62069
Model/Series: U-8F 
Aircraft Category: Airplane
Amateur Built: No
Operator:
Operating Certificate(s) Held: On-demand air taxi (135)
Operator Designator Code: BEMA

Meteorological Information and Flight Plan

Conditions at Accident Site: VMC
Condition of Light: Day
Observation Facility, Elevation: KGLD,3656 ft msl
Observation Time: 18:53 Local
Distance from Accident Site: 0 Nautical Miles
Temperature/Dew Point: 31°C /11°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: 6 knots / , 190°
Lowest Ceiling: None
Visibility: 10 miles
Altimeter Setting: 30.01 inches Hg 
Type of Flight Plan Filed: IFR
Departure Point: Goodland, KS
Destination: Denver, CO (DEN)

Wreckage and Impact Information

Crew Injuries: 1 Minor
Aircraft Damage: Substantial
Passenger Injuries: 
Aircraft Fire: None
Ground Injuries:
Aircraft Explosion: On-ground
Total Injuries: 1 Minor
Latitude, Longitude: 39.370627,-101.69898 (est)













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; Lincoln, Nebraska

Investigation Docket - National Transportation Safety Board:


Location: Sidney, Nebraska 
Accident Number: CEN19LA215
Date & Time: July 9, 2019, 08:13 Local 
Registration: N62069
Aircraft: Beech 65
Aircraft Damage: Substantial
Defining Event: Explosion (non-impact)
Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Positioning

Analysis

The pilot had topped off the outboard fuel tanks before departure. While taxiing for takeoff, the stall warning horn activated, and the pilot pulled the circuit breaker to disable the horn. During the takeoff roll, the pilot heard a loud bang, observed significant damage to the outboard left wing, and aborted the takeoff. While taxiing back to the ramp, the pilot noted smoke coming from the top of the left wing. The pilot taxied the airplane to the corner of the ramp, performed an abbreviated shutdown, grabbed a fire extinguisher, and evacuated. The pilot did not observe any additional smoke or fire and did not discharge the fire extinguisher.

Examination of the airplane revealed fire and thermal damage near the wing root area, including melted and burned wiring. Due to some loose installation screws, a fuel leak was found coming from the fuel sending unit, which had recently been replaced. In addition, a wiring harness was found pinched between a metal clamp and a wing rib. Metal-to-metal contact was noted between exposed wiring and
the wing rib. Based on the fuel leak in the left wing and the pinched wiring, it is likely fuel vapors ignited and caused an explosion of the outboard left wing.

A few months before the accident, the outboard left wing was replaced. The operator's director of maintenance stated that the electrical wiring in the wing was not inspected during the wing replacement.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The improper maintenance of the outboard left wing, which allowed electrical arcing and leaking of the fuel sending unit and subsequently resulted in ignition of fuel vapors and an explosion of the outboard left wing. 

Findings
Personnel issues Installation - Maintenance personnel
Personnel issues Post maintenance inspection - Maintenance personnel
Aircraft Electrical pwr sys wiring - Damaged/degraded
Aircraft Fuel quantity sensor - Incorrect service/maintenance

Factual Information

On July 9, 2019, about 0813 mountain daylight time, a Beech 65 airplane, N62069, experienced a left wing explosion during takeoff roll from the Sidney Municipal Airport (SNY), Sidney, Nebraska. The airline transport pilot was not injured, and the airplane sustained substantial damage to the left wing. The airplane was registered to and operated by Bemidji Aviation Services, Inc., as a Title 14 Code of Federal Regulations Part 91 positioning flight. Day instrument meteorological conditions prevailed at the time of
the accident, and an instrument flight rules flight plan was filed. The flight was originating from SNY, and destined for Denver, Colorado.

According to the operator, the pilot had topped off the outboard fuel tanks prior to departure, and the airplane contained about 230 gallons. While taxiing and advancing the engine throttles, the stall warning horn sounded so he pulled the circuit breaker as a corrective action which stopped the stall warning horn. The pilot thought the stall warning horn was in error and no further action was taken before the takeoff. During the takeoff roll, the pilot heard a loud bang and observed significant damage to the outboard left wing. Initially he thought maybe the airplane struck an animal, or the airplane impacted a pothole on the runway. While taxiing back to the ramp, the pilot noted a small amount of smoke coming from the top of the left wing. The pilot taxied the airplane to the corner of the ramp, performed an abbreviated shutdown of the airplane, grabbed a fire extinguisher, and evacuated. The pilot did not
observe any additional smoke or fire and did not discharge the fire extinguisher.

Postaccident examination of the airplane by a Federal Aviation Administration inspector and personnel from the operator revealed fire and thermal damage near the wing root area to include melted and burned wiring. After the accident as a precaution, the airplane was defueled by the operator, and in order to determine if a fuel leak was present, fuel was added to the outboard left wing during the examination. After fueling with 15 to 25 gallons of fuel, fuel began leaking from the top of the left wing fuel sending unit. Safety wire on the fuel sending unit screws was removed, and the fuel sending unit screws were found loose. The screws were tightened and fuel stop leaking from the sending unit. A hole was cut in the wing skin to examine the melted and burned wiring. A wiring harness was found pinched between a metal clamp and a wing rib. The clamp was removed and metal to metal contact was noted between exposed wiring and the wing rib. Due to the thermal damage, the wiring harness could not be separated to determine if the stall warning system could be functionally tested.

On February 22, 2019, the airplane was involved in an accident that required the replacement of the outboard left wing. According to the operator's director of maintenance, the electrical wiring in the wing was not inspected during the wing replacement. In addition, during recent maintenance at an unknown time, the inboard left fuel sending unit was replaced. The most recent continuous airworthiness inspection was completed on June 26, 2019.

History of Flight

Takeoff Explosion (non-impact) (Defining event)
Takeoff Aircraft structural failure

Pilot Information

Certificate: Airline transport; Commercial; Flight instructor
Age: 45, Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: 3-point
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): Airplane single-engine; Instrument airplane
Toxicology Performed: No
Medical Certification: Class 1 Without waivers/limitations
Last FAA Medical Exam:
Occupational Pilot: Yes
Last Flight Review or Equivalent: May 16, 2019
Flight Time: 7155 hours (Total, all aircraft), 2500 hours (Total, this make and model), 6301 hours (Pilot In Command, all aircraft), 150 hours (Last 90 days, all aircraft), 50 hours (Last 30 days, all aircraft), 3 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Beech
Registration: N62069
Model/Series: 65
Aircraft Category: Airplane
Year of Manufacture: 
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 62-3866
Landing Gear Type: Retractable - Tricycle 
Seats: 2
Date/Type of Last Inspection: June 26, 2019 Continuous airworthiness
Certified Max Gross Wt.: 8000 lbs
Time Since Last Inspection: Engines: 2 Reciprocating
Airframe Total Time: 8933 Hrs as of last inspection
Engine Manufacturer: Lycoming
ELT: C126 installed, not activated 
Engine Model/Series: IO-720-A1B
Registered Owner: 
Rated Power: 400 Horsepower
Operator: 
Operating Certificate(s) Held: None
Operator Does Business As:
Operator Designator Code: BEMA

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: 4313 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time: 07:53 Local
Direction from Accident Site: 0°
Lowest Cloud Condition: Clear
Visibility: 10 miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 7 knots / 
Turbulence Type Forecast/Actual: None /
Wind Direction: 300° 
Turbulence Severity Forecast/Actual:  /
Altimeter Setting: 30.04 inches Hg 
Temperature/Dew Point: 18°C / 12°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Sidney, NE (KSNY)
Type of Flight Plan Filed: IFR
Destination: Denver, CO (DEN) 
Type of Clearance: IFR
Departure Time: 08:13 Local
Type of Airspace: Class E

Airport Information

Airport: Sidney Municipal KSNY 
Runway Surface Type: Asphalt
Airport Elevation: 4313 ft msl 
Runway Surface Condition: Dry
Runway Used: 31
IFR Approach: None
Runway Length/Width: 6600 ft / 100 ft
VFR Approach/Landing: None

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: On-ground
Ground Injuries: N/A
Aircraft Explosion: On-ground
Total Injuries: 1 None
Latitude, Longitude: 41.101387,-102.985275(est)

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

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Wichita, Kansas

February 22, 2019

Location: Colby, KS
Accident Number: CEN19LA086
Date & Time: 02/22/2019, 0945 CST
Registration: N62069
Aircraft: Beech 65
Aircraft Damage: Substantial
Defining Event: Sys/Comp malf/fail (non-power)
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Positioning 

On February 22, 2019, about 0945 central standard time, a Beech 65 airplane, N62069, impacted terrain near Colby, Kansas, while maneuvering for a precautionary landing. The commercial pilot was not injured, and the airplane sustained substantial damage. The airplane was registered to and operated by Bemidji Aviation Services, Inc., as a Title 14 Code of Federal Regulations Part 91 positioning flight. Day instrument meteorological conditions prevailed at the time of the accident, and an instrument flight rules flight plan was filed. The flight was originating from Shalz Field Airport (CBK), Colby, Kansas, and destined for Denver, Colorado.

According to the pilot, shortly after takeoff, he noticed the crew hatch door, located next to the left front seat, had unexpectedly opened. The pilot attempted to close the door, without success. While focusing on trying to close the door, the pilot "wasn't able to fully control the airplane normally (mainly in heading and pitch)," so he initiated a precautionary landing back to CBK. While maneuvering at a low altitude to stay in visual flight rules conditions (overcast ceiling at 300 ft), the airplane's airspeed decreased, and the wing tips were dipping back and forth. The pilot retracted the landing gear and applied full engine power to try and gain airspeed. The pilot was unable to gain airspeed, the airplane was losing altitude, and he knew the airplane was going to impact terrain. Prior to the impact, the pilot kept the wings level, and the nose in a slightly pitch up attitude. The airplane then impacted the snow-covered terrain with the landing gear retracted.

Postaccident examination of the airplane by the operator revealed the left wing and left aileron were bent. No evidence was noted that the crew hatch door malfunctioned during the flight.

Pilot Information

Certificate: Flight Instructor; Commercial
Age: 27, Male
Airplane Rating(s): Multi-engine Land; Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: 3-point
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): Airplane Multi-engine; Airplane Single-engine; Instrument Airplane
Toxicology Performed: No
Medical Certification: Class 1 Without Waivers/Limitations
Last FAA Medical Exam: 01/28/2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: 02/18/2019
Flight Time:  (Estimated) 2550 hours (Total, all aircraft), 34 hours (Total, this make and model), 2444 hours (Pilot In Command, all aircraft) 

Aircraft and Owner/Operator Information

Aircraft Make: Beech
Registration: N62069
Model/Series: 65
Aircraft Category: Airplane
Year of Manufacture: 1962
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 62-3866
Landing Gear Type: Retractable - Tricycle
Seats: 2
Date/Type of Last Inspection: 01/29/2019, Continuous Airworthiness
Certified Max Gross Wt.: 8000 lbs
Time Since Last Inspection:
Engines: 2 Reciprocating
Airframe Total Time: 8877 Hours as of last inspection
Engine Manufacturer: Lycoming
ELT: C126 installed, not activated
Engine Model/Series: IA-720-A1B
Registered Owner: Bemidji Aviation Services Inc
Rated Power: 400 hp
Operator: Bemidji Aviation Services Inc
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Instrument Conditions
Condition of Light: Day
Observation Facility, Elevation: CBK, 3187 ft msl
Distance from Accident Site: 1 Nautical Miles
Observation Time: 0955 CST
Direction from Accident Site:
Lowest Cloud Condition: Clear
Visibility:  1.25 Miles
Lowest Ceiling: Overcast / 200 ft agl
Visibility (RVR):
Wind Speed/Gusts: 10 knots /
Turbulence Type Forecast/Actual: None / None
Wind Direction: 130°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.96 inches Hg
Temperature/Dew Point: -1°C / -1°C
Precipitation and Obscuration: Light - Drizzle
Departure Point: Colby, KS (CBK)
Type of Flight Plan Filed: IFR
Destination: Denver, CO (DEN)
Type of Clearance: IFR
Departure Time: 0945 CST
Type of Airspace: Class E

Airport Information

Airport: Shalz Field Airport (CBK)
Runway Surface Type: N/A
Airport Elevation: 3187 ft
Runway Surface Condition: Unknown
Runway Used: N/A
IFR Approach: None
Runway Length/Width:
VFR Approach/Landing: Precautionary Landing 

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: 39.427222, -101.052778 (est)

Stinson 108-3 Voyager, N6642M: Accident occurred July 09, 2019 near Crater Lake - Klamath Regional Airport (KLMT), Oregon

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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Portland, Oregon

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

https://registry.faa.gov/N6642M

Location: Klamath Falls, OR
Accident Number: WPR19LA207
Date & Time: 07/09/2019, 1320 PDT
Registration: N6642M
Aircraft: Stinson 108
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal

On July 9, 2019, about 1320 Pacific daylight time, a Stinson 108-3 airplane, N6642M collided with terrain near Klamath Falls, Oregon, following a partial loss of engine power. The private pilot and passenger were not injured. The airplane sustained substantial damage to the aileron and wing spar. The airplane was registered to an individual and operated by the pilot as a Title 14 Code of Federal Regulations personal flight. Visual meteorological conditions prevailed in the area about the time of the accident and no flight plan had been filed. The flight originated from an unknown location and time.

The pilot stated that he was repositioning the airplane to Alaska and had stopped for fuel in Klamath Falls. He stated that during the takeoff, the airplane did not make adequate power to establish a climb. He subsequently initiated a forced landing in a field near the airport. The airplane was relocated to a secure facility for further examination. 

Aircraft and Owner/Operator Information

Aircraft Make: Stinson
Registration: N6642M
Model/Series: 108 3
Aircraft Category: Airplane
Amateur Built: No 
Operator:On file 
Operating Certificate(s) Held: None 

Meteorological Information and Flight Plan

Conditions at Accident Site:
Condition of Light:
Observation Facility, Elevation:
Observation Time:
Distance from Accident Site:
Temperature/Dew Point:
Lowest Cloud Condition:
Wind Speed/Gusts, Direction:
Lowest Ceiling:
Visibility:  
Altimeter Setting:
Type of Flight Plan Filed:
Departure Point:
Destination: 

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries: 1 None
Aircraft Fire: Unknown
Ground Injuries:N/A 
Aircraft Explosion: Unknown
Total Injuries: 2 None
Latitude, Longitude:


A small aircraft had engine problems forcing it land in a field near the Klamath Falls Airport.

The privately owned aircraft a 1948 Stinson 108-3 was operated by Clayton DARR of Anchorage, Alaska. After taking off from the Klamath Falls Airport the aircraft experienced engine problems caused DARR put the aircraft in a field near the 10200 block of Homedale Road at approximately 1:14 PM.

Deputies responded to assist the pilot and the single passenger. No injuries were reported. The aircraft suffered minor damaged due to being landed in the field. No reports of property damage from the property owners were received.

The Sheriff’s Office is assisting the Federal Aviation Administration with the investigation and whether or not the incident is going to be classified as a crash.

Original Report: 3:09 PM, July 9, 2019

A single engine aircraft had just taken off from the Crater Lake - Klamath Regional airport when, for unknown reasons, crashed in a field south of the airport 3000’ off the end of the runway.

At 1:15 PM Klamath County 9-1-1 fielded the call dispatched first responders from Kingsley Field Fire Department and Klamath County Fire District 1, plus deputies from the Klamath County Sheriff’s Office to the scene.

Upon arrival first responders found the plane in the field right side up, pitched to the side with a broken landing gear and two uninjured passengers. 

“Two people were aboard the aircraft and were uninjured in the crash,” said John DuVal, Detective for the Klamath County Sheriff’s Office. “The aircraft is believed to be registered in Klamath Falls and that the passengers were just heading out on a day trip.”

According to John Barsalou, Manager of the Crater Lake - Klamath Regional Airport, the Federal Aviation Administration has been notified of the crash and that it was out of the airports jurisdiction as the crash occurred off airport property.  Barsalou did confirm that the aircraft crashed on takeoff.

The crash remains under investigation. 

Original article ➤ https://www.klamathfallsnews.org

Loss of Control on Ground: Luscombe 8E Silvaire, N2352K; accident occurred July 02, 2019 at Gatlinburg-Pigeon Forge Airport (KGKT), Sevierville, Sevier County, Tennessee

Substantially Damaged Right Wing. 
Federal Aviation Administration


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

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Nashville, Tennessee

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/N2352K

Location: Sevierville, TN
Accident Number: ERA19TA222
Date & Time: 07/02/2019, 0930 EDT
Registration: N2352K
Aircraft: Luscombe 8
Aircraft Damage: Substantial
Defining Event: Loss of control on ground
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal 




 View of Tailwheel.
 Federal Aviation Administration



On July 2, 2019, about 0930 eastern daylight time, a Luscombe 8E, N2352K, was substantially damaged during the landing and subsequent runway excursion at Gatlinburg-Pigeon Forge Airport (GKT), Sevierville, Tennessee. The private pilot and pilot-rated passenger were not injured. 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 local flight that departed about 0815.

The pilot reported that he had purchased the airplane the day prior to the accident and planned to complete a local time building flight. He departed the airport and performed maneuvers in the local area, returned to GKT, and completed 4 normal wheel landings on runway 28. On the fifth wheel landing, the pilot reported that both main landing gear touched down about 55-60 mph on the runway centerline, and about 30 mph, the tailwheel settled to the runway.

As soon as the tailwheel touched down, the pilot stated he felt a rumble "like a machine gun" and the airplane continued to track the centerline for about 5-6 seconds, but then veered to the right. He applied left rudder, and the airplane subsequently veered left off the runway and the right main landing gear collapsed. The right-wing spar sustained substantial damage when it impacted terrain. The pilot reported that when he exited the airplane, he observed that the tailwheel was at rest 90° to the right, perpendicular to the fuselage.

Examination of the tailwheel assembly by a Federal Aviation Administration (FAA) inspector revealed that it moved freely, and no binds or control linkage problems were discovered. He reported that the chain and spring assembly on the tailwheel were a "little loose."

According to FAA airman records, the pilot in command held a private pilot certificate, with a rating for airplane single-engine land. He completed the Basic Medical certification on September 12, 2018. He reported he had accumulated 439 total flight hours, of which 9 hours were in the accident make and model airplane. He reported he received a tailwheel endorsement in January 2009.

According to FAA airworthiness records, the tailwheel equipped airplane was powered by a Continental C85 engine. The most recent annual inspection was completed on July 1, 2019.

At 0940, the reported weather at GKT included 10 statute miles visibility, clear skies, calm wind, temperature 28°C, dew point 21°C, and barometric pressure of 30.06 inches of mercury. The pilot reported that the wind was calm.

Pilot Information

Certificate: Private
Age: 61, 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: Yes
Instructor Rating(s): None
Toxicology Performed:No 
Medical Certification: BasicMed None
Last FAA Medical Exam: 09/12/2018
Occupational Pilot:No 
Last Flight Review or Equivalent: 10/01/2018
Flight Time:  (Estimated) 439 hours (Total, all aircraft), 8.9 hours (Total, this make and model), 439 hours (Pilot In Command, all aircraft)

Pilot-Rated Passenger Information

Certificate: Flight Instructor; Commercial; Private
Age: 80, Male
Airplane Rating(s): Multi-engine Land; Single-engine Land
Seat Occupied: Right
Other Aircraft Rating(s):None 
Restraint Used:3-point 
Instrument Rating(s):Airplane 
Second Pilot Present:Yes 
Instructor Rating(s): Airplane Multi-engine; Airplane Single-engine; Instrument Airplane
Toxicology Performed: No
Medical Certification: None None
Last FAA Medical Exam:
Occupational Pilot:
Last Flight Review or Equivalent:
Flight Time:  8000 hours (Total, all aircraft), 0.5 hours (Total, this make and model)

Aircraft and Owner/Operator Information

Aircraft Make: Luscombe
Registration: N2352K
Model/Series: 8 E
Aircraft Category: Airplane
Year of Manufacture:
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 5079
Landing Gear Type: Tailwheel
Seats: 4
Date/Type of Last Inspection: 07/01/2019, Annual
Certified Max Gross Wt.: 1400 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 3813 Hours
Engine Manufacturer: Continental
ELT: Installed, not activated
Engine Model/Series: C-85-12F
Registered Owner: On file
Rated Power: 85 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: KGKT, 1013 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time: 0940 EDT
Direction from Accident Site: 0°
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: Calm /
Turbulence Type Forecast/Actual: None / None
Wind Direction:
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.06 inches Hg
Temperature/Dew Point: 28°C / 21°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Sevierville, TN (GKT)
Type of Flight Plan Filed: None
Destination: Sevierville, TN (GKT)
Type of Clearance: None
Departure Time: 0815 EDT
Type of Airspace: Class E

Airport Information

Airport: Gatlinburg-Pigeon Forge (GKT)
Runway Surface Type:Asphalt 
Airport Elevation: 1014 ft
Runway Surface Condition: Dry
Runway Used: 28
IFR Approach: None
Runway Length/Width: 5500 ft / 75 ft
VFR Approach/Landing: Full Stop; Traffic Pattern

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: 35.856944, -83.524444 (est)

==========

Location: Sevierville, TN
Accident Number: ERA19LA222
Date & Time: 07/02/2019, 0930 EDT
Registration: N2352K
Aircraft: Luscombe 8
Injuries: 2 None

Flight Conducted Under: Part 91: General Aviation - Personal

On July 2, 2019, about 0930 eastern daylight time, a Luscombe 8E, N2352K, was substantially damaged during a landing on runway 28 at Gatlinburg-Pigeon Forge Airport (GKT), Sevierville, Tennessee. The private pilot and passenger were not injured. 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 local flight.

The pilot reported that he had purchased the airplane the day prior to the accident and planned to complete a local time building flight. He departed the airport and performed maneuvers in the local area, returned to GKT, and completed 4 normal wheel landings. On the fifth landing, the pilot reported that during the wheel landing, both main landing gear touched down about 55-60 mph on the runway centerline, and about 30 mph, the tailwheel settled to the runway. As soon as the tailwheel touched down, the pilot stated he felt a rumble "like a machine gun" and the airplane veered to the right. He applied left rudder, and the airplane subsequently veered left off the runway, the right main landing gear collapsed, and the right wing spar sustained substantial damage when it impacted terrain.

When the pilot exited the airplane he observed that the tailwheel was at rest 90° to the right, perpendicular to the fuselage.

According to Federal Aviation Administration (FAA) airman records, the pilot held a private pilot certificate, with a rating for airplane single-engine land. He completed the Basic Medical certification on September 12, 2018.

According to FAA airworthiness records, the tailwheel equipped airplane was powered by a Continental C85 engine. The most recent annual inspection was completed on July 1, 2019.

At 0940, the reported weather at GKT included 10 statute miles visibility, clear skies, calm wind, temperature 28°C, dew point 21°C, and barometric pressure of 30.06 inches of mercury. The pilot reported that the wind was calm.

The wreckage was retained for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: Luscombe
Registration: N2352K
Model/Series: 8 E
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: KGKT, 1013 ft msl
Observation Time: 0940 EDT
Distance from Accident Site: 0 Nautical Miles
Temperature/Dew Point: 28°C / 21°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction: Calm / ,
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 30.06 inches Hg
Type of Flight Plan Filed: None
Departure Point: Sevierville, TN (GKT)
Destination: Sevierville, TN (GKT)

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: 35.856944, -83.524444 (est)

Robinson R22 Beta, N334DC: Accident occurred July 08, 2019 in Water Valley, Tom Green County, Texas







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; Lubbock, Texas

Investigation Docket - National Transportation Safety Board:


Location: Water Valley, Texas 
Accident Number: CEN19LA245
Date & Time: July 8, 2019, 17:30 Local 
Registration: N334DC
Aircraft: Robinson R22 
Aircraft Damage: Substantial
Defining Event: Miscellaneous/other 
Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Aerial observation

Analysis

The pilot and passenger of the helicopter were conducting a wildlife survey when the engine and main rotor began to lose rpm. The pilot lowered the collective, rolled the engine throttle control to full power, and attempted to regain the engine and main rotor rpm without success. The pilot conducted a forced landing to an opening in the canopy of vegetation below the helicopter, during which the helicopter rolled over onto its left side, resulting in the separation of the tail boom and substantial damage to the fuselage and main rotor.

An examination of the helicopter and engine revealed no mechanical anomalies that would have precluded normal operation; and the reason for the loss of performance could not be determined with the available information.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The loss of helicopter performance for undetermined reasons. 

Findings

Aircraft Altitude - Attain/maintain not possible
Not determined (general) - Unknown/Not determined

Factual Information

On July 8, 2019, about 1730 central daylight time, a Robinson R22 II Beta helicopter, N334DC, was substantially damaged when it was involved in an accident near Water Valley, Texas. The commercial pilot and passenger were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 aerial observation flight.

The pilot and passenger were conducting a wildlife survey. About 1.5 hours into the flight, at an altitude between 50 and 100 ft above the top of the canyon and an airspeed of about 35 mph, the "engine began to bog" and the both the engine and main rotor lost rpm. The pilot stated that he lowered the collective, rolled the engine throttle control to full rpm, and attempted to regain the engine and main rotor rpm. The rpm continued to decay so the pilot elected to conduct a forced landing to an opening in the vegetation below the helicopter.

During the descent into the vegetation the main rotor blades struck the trees. The helicopter rolled over on its left side during the ground impact. The tail boom separated from the fuselage and the main rotor blades and fuselage were substantially damaged.

An examination of the helicopter and engine revealed no mechanical anomalies that would have precluded normal operations prior to the accident. The tail rotor blade fracture signatures were consistent with separation of the blades under power.

History of Flight

Enroute Miscellaneous/other (Defining event)
Enroute Attempted remediation/recovery
Enroute Emergency descent initiated
Landing Roll over

Pilot Information

Certificate: Commercial 
Age: 27,Male
Airplane Rating(s): None
Seat Occupied: Right
Other Aircraft Rating(s): Helicopter
Restraint Used: 3-point
Instrument Rating(s): None 
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 2 Without waivers/limitations
Last FAA Medical Exam: February 21, 2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: June 10, 2017
Flight Time: (Estimated) 2153 hours (Total, all aircraft), 1700 hours (Total, this make and model), 2000 hours (Pilot In Command, all aircraft), 161 hours (Last 90 days, all aircraft), 30 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Robinson
Registration: N334DC
Model/Series: R22 Beta
Aircraft Category: Helicopter
Year of Manufacture: 2003
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 3511
Landing Gear Type: N/A; Skid 
Seats: 2
Date/Type of Last Inspection: May 2, 2019 100 hour
Certified Max Gross Wt.: 1370 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 5810.3 Hrs as of last inspection
Engine Manufacturer: Lycoming
ELT: Not installed
Engine Model/Series: O-360 J2A
Registered Owner:
Rated Power: 124 Horsepower
Operator: 
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: KSJT,1916 ft msl 
Distance from Accident Site: 31 Nautical Miles
Observation Time: 22:51 Local 
Direction from Accident Site: 161°
Lowest Cloud Condition: Clear 
Visibility: 10 miles
Lowest Ceiling: None 
Visibility (RVR):
Wind Speed/Gusts: 9 knots / 
Turbulence Type Forecast/Actual: None / None
Wind Direction: 140°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.88 inches Hg 
Temperature/Dew Point: 32°C / 23°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Water Valley, TX 
Type of Flight Plan Filed: None
Destination: Water Valley, TX 
Type of Clearance: None
Departure Time: 16:00 Local 
Type of Airspace: Class G

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: 31.834999,-100.686668(est)

=============

Location: Water Valley, TX
Accident Number: CEN19LA245
Date & Time: 07/08/2019, 1730 CDT
Registration: N334DC
Aircraft: Robinson R22
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Aerial Observation 

On July 8, 2019, about 1730 central daylight time, a Robinson R22 helicopter, N334DC, was substantially damaged during a forced landing near Watter Valley, Texas. The commercial pilot and passenger were not injured. The helicopter sustained substantial damage. The aerial observation flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no Federal Aviation Administration (FAA) flight plan had been filed for the flight.

The pilot stated that during the flight over a canyon, it felt as if "the bottom fell out from under him". He reported that the main rotor RPMs dropped and he was unable to recover. The helicopter rolled over on its left side during the impact with the ground. The pilot stated that the tail boom separated from the fuselage and the main rotor blades were damaged. The pilot later reported a loss of engine power. The helicopter has been retained for further examination. 

Aircraft and Owner/Operator Information

Aircraft Make: Robinson
Registration: N334DC
Model/Series: R22 BETA
Aircraft Category: Helicopter
Amateur Built: No
Operator: Trans-Pecos Aviation Llc
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KSJT, 1916 ft msl
Observation Time: 2251 UTC
Distance from Accident Site: 31 Nautical Miles
Temperature/Dew Point: 32°C / 23°C
Lowest Cloud Condition: Clear
Wind Speed/Gusts, Direction:  knots / , 140°
Lowest Ceiling: None
Visibility:  10 Miles
Altimeter Setting: 29.89 inches Hg
Type of Flight Plan Filed: None
Departure Point: Water Valley, TX
Destination: Water Valley, TX

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: 31.835000, -100.686667 (est) 

Cessna 560XLS Citation Excel, N614QS: Incident occurred July 09, 2019 at William P. Hobby Airport (KHOU), Houston, Texas



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

Aircraft reached the departure end of runway and veered off into the grass.

NetJets Sales Inc
CPCO Holding Company LLC
Toby LLC

https://registry.faa.gov/N614QS

Date: 09-JUL-19
Time: 17:00:00Z
Regis#: N614QS
Aircraft Make: CESSNA
Aircraft Model: 560
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: NONE
Activity: CORPORATE
Flight Phase: TAKEOFF (TOF)
Operation: 91
City: HOUSTON
State: TEXAS