Saturday, May 15, 2021

Cessna 210 Centurion, N7350E: Accident occurred May 15, 2021 in Lake Arrowhead, San Bernardino County, California

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

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

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Riverside, California


Location: Lake Arrowhead, CA 
Accident Number: WPR21LA194
Date & Time: May 16, 2021, 15:45 Local
Registration: N7350E
Aircraft: Cessna 210 Injuries: 2 Serious
Flight Conducted
Under: Part 91: General aviation - Personal

On May 16, 2021, about 1545 Pacific daylight time, a Cessna 210, N7350E, was substantially damaged when it was involved in an accident near Lake Arrowhead, California. The pilot and passenger were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that while climbing through an altitude of about 8,500 ft mean sea level (msl), enroute to Big Bear Airport (L35), Big Bear City, California, he noted a partial loss of engine power. He contacted Air Traffic Control (ATC) and was provided with alternate airports and current weather information. While over mountainous terrain, the engine experienced a total loss of power. 

Concerned he did not have sufficient altitude to clear rising terrain, he initiated a forced landing to a clearing on sloped terrain. The airplane subsequently collided with vegetation and came to rest upright on a steep slope.

Both wings and fuselage were substantially damaged. The wreckage was recovered for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N7350E
Model/Series: 210 
Aircraft Category: Airplane
Amateur Built: No
Operator: 
Operating Certificate(s) Held: None
Operator Designator Code:

Meteorological Information and Flight Plan

Conditions at Accident Site:
Condition of Light:
Observation Facility, Elevation: KSBD,1159 ft msl
Observation Time: 15:54 Local
Distance from Accident Site: 11 Nautical Miles
Temperature/Dew Point: 17°C /9°C
Lowest Cloud Condition: 
Wind Speed/Gusts, Direction: 7 knots / , 320°
Lowest Ceiling:
Visibility: 7 miles
Altimeter Setting: 29.98 inches Hg 
Type of Flight Plan Filed:
Departure Point:
Destination:

Wreckage and Impact Information

Crew Injuries: 1 Serious 
Aircraft Damage: Substantial
Passenger Injuries: 1 Serious
Aircraft Fire: None
Ground Injuries:
Aircraft Explosion: None
Total Injuries: 2 Serious
Latitude, Longitude: 34.263639,-117.15866 (est)
 
 



A pilot and passenger were alert and talking with firefighters after the small plane they were traveling in crashed into the side of a mountain in the Cedar Glen area of the San Bernardino Mountains on Saturday afternoon, authorities said.

San Bernardino County Sheriff’s Department deputies responded to the area of Torrey Road and Blackwood Drive, east of Lake Arrowhead and near Mackay Park, about 3 p.m. after a report came in of a plane, possibly a Cessna, that had gone down, sheriff’s spokeswoman Cindy Bachman said.

The pilot reported losing power at an altitude of about 8,500 feet, and was attempting to navigate to Snow Valley before going down, National Transportation Safety Board spokesman Chris O’Neil said. What caused the loss of power wasn’t immediately known.

The severity of the injuries to the two occupants was not immediately known.

The two occupants of the Cessna 210 Centurion were traveling from Chino to Big Bear City, said Elizabeth Cory of the Federal Aviation Administration. Air traffic control lost radio contact with the plan just before 3:15 p.m.

The FAA and National Transportation Safety Board will investigate the cause of the crash.

Loss of Lift: Let L-33 Solo, N355BA; accident occurred May 11, 2020 near Arlington Municipal Airport (KAWO), Snohomish County, Washington











Aviation Accident Final Report - National Transportation Safety Board

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Des Moines, Washington 

Investigation Docket - National Transportation Safety Board:


Location: Arlington, Washington
Accident Number: WPR20CA151
Date & Time: May 11, 2020, 12:53 Local 
Registration: N355BA
Aircraft: Let L 33 SOLO 
Aircraft Damage: Substantial
Defining Event: Loss of lift 
Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

The glider pilot reported that while on final approach to land, the ground speed decreased and the glider descended faster than expected. Unable to reach the runway, he diverted to a gravel area to land out. The glider landed hard, and during the landing roll he heard a loud bang that was later identified as a pothole.

The glider sustained substantial damage to the fuselage.

The pilot reported no mechanical malfunctions with the glider 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 loss of lift while on final approach which resulted in a hard off-airport landing.

Findings

Environmental issues Thermal lifting - Effect on operation
Aircraft Altitude - Not attained/maintained

Factual Information

History of Flight

Landing Loss of lift (Defining event)
Landing-flare/touchdown Hard landing
Landing-landing roll Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Commercial; Student 
Age: 58, Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Center
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: BasicMed Without waivers/limitations
Last FAA Medical Exam: May 19, 2017
Occupational Pilot: No 
Last Flight Review or Equivalent:
Flight Time: (Estimated) 4561 hours (Total, all aircraft), 4 hours (Total, this make and model), 15 hours (Last 90 days, all aircraft), 7 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Let
Registration: N355BA
Model/Series: L 33 SOLO No Series
Aircraft Category: Glider
Year of Manufacture: 1999 
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 990506
Landing Gear Type: Tandem
Seats: 1
Date/Type of Last Inspection: May 8, 2020 Annual 
Certified Max Gross Wt.:
Time Since Last Inspection: 
Engines:
Airframe Total Time: 814.35 Hrs as of last inspection
Engine Manufacturer:
ELT: 
Engine Model/Series:
Registered Owner:
Rated Power:
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: KPAE,606 ft msl 
Distance from Accident Site: 16 Nautical Miles
Observation Time: 12:53 Local 
Direction from Accident Site: 198°
Lowest Cloud Condition: Clear 
Visibility:  10 miles
Lowest Ceiling: None 
Visibility (RVR):
Wind Speed/Gusts: 5 knots / 
Turbulence Type Forecast/Actual: None / None
Wind Direction: 350° 
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.01 inches Hg
Temperature/Dew Point: 24°C / 8°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Arlington, WA (AWO)
Type of Flight Plan Filed: None
Destination: Arlington, WA (AWO) 
Type of Clearance: None
Departure Time: 12:21 Local 
Type of Airspace: Class G

Airport Information

Airport: Arlington Muni AWO
Runway Surface Type: Asphalt
Airport Elevation: 141 ft msl
Runway Surface Condition: Dry
Runway Used: 34
IFR Approach: None
Runway Length/Width: 5332 ft / 100 ft
VFR Approach/Landing: Straight-in

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None 
Latitude, Longitude: 48.160831,-122.158889 (est)

Loss of Lift: Schempp-Hirth Ventus 2cT, N514TW; accident occurred May 11, 2020 in Stuarts Draft, Augusta County, Virginia









Aviation Accident Final Report - National Transportation Safety Board 

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Richmond, Virginia 

Investigation Docket - National Transportation Safety Board:


Location: Stuarts Draft, VA
Accident Number: ERA20CA178
Date & Time: 05/11/2020, 1500 EDT
Registration: N514TW
Aircraft: Schempp Hirth VENTUS 2CT
Aircraft Damage: Substantial
Defining Event: Loss of lift
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal

Analysis

After departing on a local flight, the pilot of the motor glider crossed a ridge line into a valley at an altitude of about 8,000 ft mean sea level, and then glided to the south in search of lift, but was unsuccessful. He decided to land on a brown, flat, field that appeared to be recently tilled. The pilot set up for a landing, and then deployed the glider's sustainer engine. The engine did not start, so he continued his approach to land. During the landing, the right wing struck the ground, the glider ground looped, and was substantially damaged. The flight manual for the sustainer engine advised that, the sustainer engine should only be extended and started when there was suitable terrain for landing within gliding distance, and furthermore, below 984 ft above ground level, starting attempts were to be avoided "so as to have a safe height left for planning the approach pattern should the engine fail to run!" The pilot stated that there was no mechanical malfunction or failure with the glider, and that he would recommend trying to start the sustainer engine at a higher altitude.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
A loss of thermal lift during a motor glider flight, which resulted in an off-airport landing.

Contributing to the accident was the pilot's delayed attempted engine start.

Findings

Environmental issues Thermal lifting - Effect on operation
Aircraft Altitude - Not attained/maintained
Personnel issues Use of equip/system - Pilot
Personnel issues Delayed action - Pilot

Factual Information

History of Flight

Maneuvering Loss of lift (Defining event)
Emergency descent Attempted remediation/recovery
Landing Off-field or emergency landing
Landing Dragged wing/rotor/float/other
Landing Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Airline Transport; Flight Instructor; Commercial
Age: 59, Male
Airplane Rating(s): Multi-engine Land; Multi-engine Sea; Single-engine Land; Single-engine Sea
Seat Occupied: Single
Other Aircraft Rating(s): Glider; Helicopter
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s):  Airplane Multi-engine; Airplane Single-engine; Glider; Instrument Airplane
Toxicology Performed: No
Medical Certification: Class 1 With Waivers/Limitations
Last FAA Medical Exam: 07/03/2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: 03/02/2020
Flight Time:  18000 hours (Total, all aircraft), 142 hours (Total, this make and model), 13732 hours (Pilot In Command, all aircraft), 81 hours (Last 90 days, all aircraft), 46 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Schempp Hirth
Registration: N514TW
Model/Series: VENTUS 2CT No Series
Aircraft Category: Glider
Year of Manufacture: 2007
Amateur Built: No
Airworthiness Certificate: Experimental
Serial Number: 191
Landing Gear Type: Tailwheel
Seats: 1
Date/Type of Last Inspection: 01/26/2020, Condition
Certified Max Gross Wt.: 1323 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 2150.6 Hours as of last inspection
Engine Manufacturer: SOLO
ELT: C91A installed, not activated
Engine Model/Series: 2350
Registered Owner: On file
Rated Power: 26 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: SHD, 1201 ft msl
Distance from Accident Site: 12 Nautical Miles
Observation Time: 1455 EDT
Direction from Accident Site: 18°
Lowest Cloud Condition:
Visibility:  10 Miles
Lowest Ceiling: Broken / 5500 ft agl
Visibility (RVR):
Wind Speed/Gusts: 16 knots / 21 knots
Turbulence Type Forecast/Actual: None / None
Wind Direction: 300°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30.03 inches Hg
Temperature/Dew Point: 12°C / 0°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Amelia Court House, VA (2VA3)
Type of Flight Plan Filed: None
Destination: Amelia Court House, VA (2VA3)
Type of Clearance: None
Departure Time: 1230 EDT
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: 37.992500, -78.981389 (est) 

Loss of Control on Ground: Piper PA-22-150, N4454A; accident occurred May 11, 2020 at Fayetteville Municipal Airport (KFYM), Tennessee








Aviation Accident Final Report - National Transportation Safety Board

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Nashville, Tennessee

Investigation Docket - National Transportation Safety Board:

 
Location: Fayetteville, Tennessee
Accident Number: ERA20CA185
Date & Time: May 11, 2020, 19:00 UTC 
Registration: N4454A
Aircraft: Piper PA22 
Aircraft Damage: Substantial
Defining Event: Loss of control on ground 
Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis

The pilot reported that he was performing touch and go landings. On his third landing, he knew there was a crosswind from his left side, so he touched down with the left main landing gear first. When the right main landing gear touched down, the airplane started to veer off to the left, so he corrected with right rudder and the airplane pulled hard to the right. The pilot then saw a ditch on the right side of the runway, so he applied "hard left rudder" to purposefully put the airplane into a ground loop so the airplane would not go off the runway and into the ditch. During the ground loop, the right main landing gear fractured and folded under the fuselage.

Examination of the airplane by a Federal Aviation Administration inspector revealed that the right main landing gear tube fractured, and that the fracture surfaces did not display corrosion. The right wing rear spar and the lower longeron were substantially damaged. Examination of the flight controls and brakes showed no evidence of any preaccident anomalies.

At the time of the accident a left crosswind component of between 9 and 17 knots prevailed.

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 in gusting crosswind conditions.

Findings

Personnel issues Aircraft control - Pilot
Environmental issues Crosswind - Effect on operation
Aircraft Directional control - Not attained/maintained

Factual Information

History of Flight

Landing-landing roll Loss of control on ground (Defining event)
Landing-landing roll Landing gear collapse

Pilot Information

Certificate: Commercial 
Age: 28, Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied: Left
Other Aircraft Rating(s): None 
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 1 Without waivers/limitations
Last FAA Medical Exam: May 29, 2019
Occupational Pilot: No
Last Flight Review or Equivalent: June 5, 2019
Flight Time: 234 hours (Total, all aircraft), 42 hours (Total, this make and model), 166 hours (Pilot In Command, all aircraft), 36 hours (Last 90 days, all aircraft), 4 hours (Last 30 days, all aircraft), 0 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Piper 
Registration: N4454A
Model/Series: PA22 150 
Aircraft Category: Airplane
Year of Manufacture: 1956 
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 22-3787
Landing Gear Type: Tailwheel 
Seats: 4
Date/Type of Last Inspection: February 19, 2020 Annual 
Certified Max Gross Wt.: 2000 lbs
Time Since Last Inspection: 
Engines: 1 Reciprocating
Airframe Total Time: 2144.4 Hrs as of last inspection
Engine Manufacturer: Lycoming
ELT: Installed, not activated 
Engine Model/Series: O-320 SERIES
Registered Owner: 
Rated Power: 150 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: FYM
Distance from Accident Site:
Observation Time: 18:55 Local
Direction from Accident Site:
Lowest Cloud Condition: Clear 
Visibility: 10 miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 9 knots / 17 knots
Turbulence Type Forecast/Actual:  /
Wind Direction: 330° 
Turbulence Severity Forecast/Actual:  /
Altimeter Setting: 30.25 inches Hg
Temperature/Dew Point: 18°C / 2°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Fayetteville, TN (FYM)
Type of Flight Plan Filed: None
Destination: Fayetteville, TN (FYM) 
Type of Clearance: None
Departure Time: 18:00 UTC 
Type of Airspace: Class G

Airport Information

Airport: Fayetteville Muni FYM 
Runway Surface Type: Asphalt
Airport Elevation: 983 ft msl 
Runway Surface Condition: Dry
Runway Used: 02
IFR Approach: None
Runway Length/Width: 5900 ft / 100 ft
VFR Approach/Landing: Touch and go

Wreckage and Impact Information

Crew Injuries: 1 None
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 1 None
Latitude, Longitude: 35.060554,-86.563888(est)

Loss of Control in Flight: General Atomics MQ-9B, CBP213: accident occurred May 15, 2020 at San Angelo Regional Airport (KSJT), Tom Green County, Texas





Aviation Accident Final Report - National Transportation Safety Board

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Lubbock, Texas

Investigation Docket - National Transportation Safety Board:

U.S. Customs and Border Protection

Location: San Angelo, Texas
Accident Number: CEN20CA178
Date & Time: May 15, 2020, 10:26 Local 
Registration: CBP213
Aircraft: GENERAL ATOMICS MQ-9B
Aircraft Damage: Destroyed
Defining Event: Loss of control in flight 
Injuries: N/A
Flight Conducted Under: Public aircraft

Analysis

The pilot of the unmanned aircraft system (UAS) attempted a touch-and-go landing but then performed a go-around due to an unstable approach. The pilot re-entered the UAS into the traffic pattern for a second touch-and-go landing attempt, during which it initially touched down nose first and induced a porpoise. During the third porpoise, the UAS contacted the runway in a nose-down attitude resulting in a hard landing and post-crash fire. The UAS was destroyed by the post-crash fire. There was no mechanical malfunction / failure of the UAS at the time of the accident.

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 an adequate landing flare that resulted in a porpoise and impact with terrain.

Findings

Aircraft Pitch control - Not attained/maintained

Factual Information

History of Flight

Landing-flare/touchdown Loss of control in flight (Defining event)
Landing-flare/touchdown Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Commercial; Flight instructor 
Age: 36, Male
Airplane Rating(s): Single-engine land; Multi-engine land
Seat Occupied:
Other Aircraft Rating(s): None
Restraint Used:
Instrument Rating(s): Airplane 
Second Pilot Present:
Instructor Rating(s): Airplane single-engine 
Toxicology Performed: No
Medical Certification: Class 2 Without waivers/limitations
Last FAA Medical Exam: February 3, 2020
Occupational Pilot: Yes
Last Flight Review or Equivalent: January 16, 2020
Flight Time: 4629 hours (Total, all aircraft)

Other flight crew Information

Certificate: Age:
Airplane Rating(s): 
Seat Occupied: None
Other Aircraft Rating(s): 
Restraint Used:
Instrument Rating(s): 
Second Pilot Present:
Instructor Rating(s): 
Toxicology Performed: No
Medical Certification: 
Last FAA Medical Exam:
Occupational Pilot: 
Last Flight Review or Equivalent:
Flight Time:

Aircraft and Owner/Operator Information

Aircraft Make: GENERAL ATOMICS
Registration: CBP213
Model/Series: MQ-9B 
Aircraft Category: Airplane
Year of Manufacture: 2011 
Amateur Built: No
Airworthiness Certificate: Certificate of authorization or waiver (COA)
Serial Number: Unknown
Landing Gear Type: Retractable - Tricycle
Seats: 0
Date/Type of Last Inspection: February 24, 2020 Continuous airworthiness
Certified Max Gross Wt.: 10500 lbs
Time Since Last Inspection:
Engines: Turbo prop
Airframe Total Time:
Engine Manufacturer: Honeywell
ELT:
Engine Model/Series: TPE331-10YGD
Registered Owner:
Rated Power:
Operator: 
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC) 
Condition of Light: Day
Observation Facility, Elevation: SJT,1919 ft msl 
Distance from Accident Site: 0 Nautical Miles
Observation Time: 10:20 Local
Direction from Accident Site:
Lowest Cloud Condition: Clear
Visibility 9 miles
Lowest Ceiling: Broken / 2500 ft AGL 
Visibility (RVR):
Wind Speed/Gusts: 10 knots / 
Turbulence Type Forecast/Actual:  /
Wind Direction: 190° 
Turbulence Severity Forecast/Actual: /
Altimeter Setting: 29.87 inches Hg
Temperature/Dew Point: 27°C / 20°C
Precipitation and Obscuration:
Departure Point: San Angelo, TX (SJT)
Type of Flight Plan Filed: None
Destination: San Angelo, TX (SJT) 
Type of Clearance: VFR
Departure Time: 
Type of Airspace: Class D

Airport Information

Airport: San Angelo Regional/Mathis Field SJT
Runway Surface Type: Asphalt
Airport Elevation: 1919 ft msl
Runway Surface Condition: Dry
Runway Used: 18
IFR Approach: None
Runway Length/Width: 8049 ft / 150 ft
VFR Approach/Landing: Touch and go

Wreckage and Impact Information

Crew Injuries:
Aircraft Damage: Destroyed
Passenger Injuries:
Aircraft Fire: On-ground
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: N/A 
Latitude, Longitude: 31.357778,-100.496391(est)

American Aviation AA-1A Trainer, N12YT: Accident occurred May 15, 2020 at Blythe Airport (KBLH), Riverside County, California

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. 

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

Additional Participating Entity
Federal Aviation Administration / Flight Standards District Office; Riverside, California


Location: Blythe, CA 
Accident Number: WPR20LA148
Date & Time: May 15, 2020, 13:57 Local 
Registration: N12YT
Aircraft: American Aviation AA1
Injuries: 1 Serious
Flight Conducted Under: Part 91: General aviation - Personal

On May 15, 2020, about 1357 Pacific daylight time, an American Aviation AA-1A airplane, N12YT, was substantially damaged when it was involved in an accident near Blythe, California. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

According to the pilot, shortly after takeoff and about 50 ft above ground level, the airplane would not climb. The pilot confirmed that the throttle was full forward and then pushed the airplane's nose forward to gain airspeed, but the airplane still would not climb, and the left wing struck terrain. The airplane subsequently impacted the ground, just past the departure runway's threshold, spun, and came to rest about 150 ft from the initial point of impact.

The airplane was recovered to a secure location for further examination.

Aircraft and Owner/Operator Information

Aircraft Make: American Aviation 
Registration: N12YT
Model/Series: AA1 A 
Aircraft Category: Airplane
Amateur Built: No
Operator: On file
Operating Certificate(s) Held: None
Operator Designator Code:

Meteorological Information and Flight Plan

Conditions at Accident Site: 
Condition of Light:
Observation Facility, Elevation: KBLH,392 ft msl 
Observation Time: 20:52 Local
Distance from Accident Site: 0 Nautical Miles
Temperature/Dew Point: 33°C /2°C
Lowest Cloud Condition: Clear 
Wind Speed/Gusts, Direction: 9 knots / 16 knots, 140°
Lowest Ceiling: None 
Visibility: 10 miles
Altimeter Setting: 29.78 inches Hg 
Type of Flight Plan Filed:
Departure Point: Blythe, CA (BLH)
Destination:

Wreckage and Impact Information

Crew Injuries: 1 Serious
Aircraft Damage: Substantial
Passenger Injuries: 
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 1 Serious
Latitude, Longitude: 33.616943,-114.706108 (est)

Loss of Control on Ground: Cessna 120, N120MZ; accident occurred May 15, 2020 in Chatham, Sangamon County, Illinois











Aviation Accident Final Report - National Transportation Safety Board 

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Springfield, Illinois

Investigation Docket - National Transportation Safety Board:


Location: Chatham, IL
Accident Number: CEN20CA182
Date & Time: 05/15/2020, 1520 CDT
Registration: N120MZ
Aircraft: Cessna 120
Aircraft Damage: Substantial
Defining Event: Loss of control on ground
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis

The pilot was conducting a visual flight rules (VFR) cross-country flight at 5,500 ft mean sea level (MSL) above a cloud layer, and the airplane was not equipped with an attitude indicator or flight instruments to operate in instrument meteorological conditions. According to the pilot, the weather was forecast VFR at her destination. While en route, a cloud layer above her started lowering, so she descended to 5,000 ft MSL. The pilot could see blue sky between the layers when the two layers started to come together and then she inadvertently entered instrument meteorological conditions (IMC).

The pilot transitioned to an "inside instrument scan", turned on carburetor heat, and added full power to attempt to climb to find VFR conditions. After climbing 300 to 500 ft and about 5 minutes after entering the clouds, the pilot noticed a right turn had developed as confirmed on the heading indicator and her electronic flight device. The right turn became tighter, and the pilot recognized she was disoriented, and the airplane was descending. She elected to perform corrective action for a nose low unusual attitude and attempted to descend to visual flight conditions. The airplane broke out of the clouds about 1,500 ft above the ground (AGL) in a 25° to 30° right bank and 10° to 15° nose low attitude.

The pilot recovered to level flight and added full power. The airplane would not accelerate above 60 to 65 knots in level flight and the pilot felt the rudder was ineffective. The pilot elected to conduct a precautionary landing to nearby field that was muddy due to recent rains. During the landing, the airplane flipped over when the wheels dug into the ground. The vertical stabilizer, rudder, and both wings sustained substantial damage. Examination of the airplane revealed flight control continuity to all flight control surfaces. The pilot reported that the airplane was operating normally prior to entering IMC conditions.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's decision to continue flight in instrument meteorological conditions in an airplane not equipped for instrument flight, which forced her to perform a precautionary landing to a muddy field resulting in the airplane nosing over.

Findings

Personnel issues Decision making/judgment - Pilot
Environmental issues Wet/muddy terrain - Contributed to outcome
Environmental issues Clouds - Ability to respond/compensate
Aircraft Directional control - Not attained/maintained
Aircraft Pitch control - Not attained/maintained

Factual Information

History of Flight

Enroute-cruise Loss of visual reference
Enroute-cruise Loss of control in flight
Landing Off-field or emergency landing
Landing Loss of control on ground (Defining event)

Pilot Information

Certificate: Airline Transport; Flight Instructor; Commercial
Age: 24, Female
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: No
Instructor Rating(s): Airplane Multi-engine; Airplane Single-engine
Toxicology Performed: No
Medical Certification: Class 1 Without Waivers/Limitations
Last FAA Medical Exam: 08/21/2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: 11/07/2019
Flight Time:  2868 hours (Total, all aircraft), 92 hours (Total, this make and model), 1178 hours (Pilot In Command, all aircraft), 117 hours (Last 90 days, all aircraft), 29 hours (Last 30 days, all aircraft), 0 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N120MZ
Model/Series: 120 No Series
Aircraft Category: Airplane
Year of Manufacture: 1946
Amateur Built:No 
Airworthiness Certificate: Normal
Serial Number: 9226
Landing Gear Type: Tailwheel
Seats:
Date/Type of Last Inspection: 12/17/2019, Annual
Certified Max Gross Wt.: 1451 lbs
Time Since Last Inspection: 28 Hours
Engines: 1 Reciprocating
Airframe Total Time: 2675 Hours as of last inspection
Engine Manufacturer: Continental
ELT: C91 installed, activated, aided in locating accident
Engine Model/Series: C85 SERIES
Registered Owner: Mazzu Anthony J
Rated Power: 85 hp
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Instrument Conditions
Condition of Light: Day
Observation Facility, Elevation:
Distance from Accident Site:
Observation Time:
Direction from Accident Site:
Lowest Cloud Condition: 
Visibility:  10 Miles
Lowest Ceiling: Overcast / 1500 ft agl
Visibility (RVR):
Wind Speed/Gusts: Light and Variable /
Turbulence Type Forecast/Actual:
Wind Direction: Variable
Turbulence Severity Forecast/Actual:
Altimeter Setting: 29.96 inches Hg
Temperature/Dew Point: 19°C / 17°C
Precipitation and Obscuration:
Departure Point: St Louis, MO (1H0)
Type of Flight Plan Filed: None
Destination: Chicago, IL (06C)
Type of Clearance: VFR; VFR on top
Departure Time:
Type of Airspace: Class E; 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: 39.704167, -89.717222 (est)

Loss of Control on Ground: Piper PA-18-150 Super Cub, N323DH; accident occurred May 15, 2020 at Skwentna Airport (PASW), Alaska






Aviation Accident Final Report - National Transportation Safety Board 

Additional Participating Entity: 
Federal Aviation Administration / Flight Standards District Office; Anchorage, Alaska

Investigation Docket - National Transportation Safety Board:


Location: Skwentna, AK
Accident Number: ANC20CA048
Date & Time: 05/15/2020, 1625 AKD
Registration:N323DH 
Aircraft: Piper PA18
Aircraft Damage: Substantial
Defining Event: Loss of control on ground
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis

The pilot was landing the tailwheel and tundra tire-equipped airplane on a gravel surfaced runway. After touchdown, the airplane veered right and the pilot applied left rudder and left brake, but the airplane continued and ground looped. The airplane sustained substantial damage to the left elevator and left wing.

The pilot reported no preaccident mechanical failures or malfunctions that would have precluded normal operations.

In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been prevented if she had been more proficient in the accident airplane.

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 the landing roll, which resulted in a ground loop.

Findings

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

Factual Information

History of Flight

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

Pilot Information

Certificate: Airline Transport; Private
Age: 31, Female
Airplane Rating(s): Multi-engine Sea; Single-engine Land
Seat Occupied: Front
Other Aircraft Rating(s): None
Restraint Used:
Instrument Rating(s): Airplane
Second Pilot Present: No
Instructor Rating(s):None 
Toxicology Performed: No
Medical Certification: Class 1 Without Waivers/Limitations
Last FAA Medical Exam: 07/15/2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: 11/30/2019
Flight Time:  1848.5 hours (Total, all aircraft), 12.6 hours (Total, this make and model), 248.6 hours (Pilot In Command, all aircraft), 46.2 hours (Last 90 days, all aircraft), 12.6 hours (Last 30 days, all aircraft), 3.3 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Piper
Registration: N323DH
Model/Series: PA18 150
Aircraft Category: Airplane 
Year of Manufacture:1963 
Amateur Built: No 
Airworthiness Certificate: Normal
Serial Number: 18-7939
Landing Gear Type: Tailwheel
Seats:
Date/Type of Last Inspection: 04/27/2020, Annual
Certified Max Gross Wt.: 1750 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 4441 Hours as of last inspection
Engine Manufacturer: Lycoming
ELT: C126 installed, not activated
Engine Model/Series: O-320 SERIES
Registered Owner: Kleinsmith Stacee F
Rated Power: 150 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:
Distance from Accident Site:
Observation Time: 0053 UTC
Direction from Accident Site:
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 7 knots /
Turbulence Type Forecast/Actual:
Wind Direction: 280°
Turbulence Severity Forecast/Actual: 
Altimeter Setting: 29.91 inches Hg
Temperature/Dew Point: 18°C / 1°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Birchwood, AK (BCV)
Type of Flight Plan Filed: None
Destination: Skwentna, AK (SKW)
Type of Clearance: None
Departure Time: 1515 AKD
Type of Airspace: Class G

Airport Information

Airport: Skwentna (SKW)
Runway Surface Type: Gravel
Airport Elevation: 148 ft
Runway Surface Condition: Dry 
Runway Used: 10
IFR Approach: None
Runway Length/Width: 3400 ft / 75 ft
VFR Approach/Landing: Full Stop; Traffic Pattern

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: 61.966111, -151.195278

Fuel Starvation: Cessna 172M Skyhawk, N92036; accident occurred May 15, 2020 in Colchester, McDonough County, Illinois








Aviation Accident Final Report - National Transportation Safety Board 

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Springfield, Illinois

Investigation Docket - National Transportation Safety Board:


Location: Colchester, IL
Accident Number: CEN20CA181
Date & Time: 05/15/2020, 1630 CDT
Registration:N92036 
Aircraft: Cessna 172
Aircraft Damage: Substantial 
Defining Event: Fuel starvation
Injuries: 1 Serious
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis

The private pilot reported that he checked the fuel tanks prior to takeoff. It was dark in the hangar where he used a wire to check the fuel level in the tanks. He was not wearing his glasses and he thought he had "an inch or so" of fuel. The pilot thought that was enough fuel and departed on a cross country flight where he flew the airplane towards a local lake. During the flight, the engine "sputtered" and lost power. The pilot turned towards the destination airport but lost airspeed, so he lowered the airplane's nose and did a forced landing impacting trees below. A postaccident examination revealed that the airplane sustained substantial empennage, fuselage, and wing damage. The fuel tanks were empty and there was no fuel odor anywhere at the scene. The emergency locator transmitter (ELT) battery was recently replaced. However, at the time of the crash, the ELT switch was in the OFF position. The pilot reported that there was no mechanical malfunction/failure of the airplane during the flight. 

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's inadequate preflight of the fuel quantity which resulted in a loss of engine power due to fuel starvation during cruise flight.

Findings

Personnel issues Preflight inspection - Pilot
Aircraft Fuel - Fluid level
Environmental issues Tree(s) - Contributed to outcome

Factual Information

History of Flight

Prior to flight Aircraft inspection event
Enroute Fuel starvation (Defining event)
Emergency descent Off-field or emergency landing
Landing Collision with terr/obj (non-CFIT)

Pilot Information

Certificate: Private
Age: 73, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s):None 
Restraint Used:
Instrument Rating(s): None
Second Pilot Present: No 
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: BasicMed
Last FAA Medical Exam: 08/19/2018
Occupational Pilot: No
Last Flight Review or Equivalent: 08/01/2018
Flight Time: (Estimated) 942 hours (Total, all aircraft), 942 hours (Total, this make and model), 5 hours (Last 90 days, all aircraft), 5 hours (Last 30 days, all aircraft) 

Aircraft and Owner/Operator Information

Aircraft Make: Cessna
Registration: N92036
Model/Series:172 M 
Aircraft Category: Airplane
Year of Manufacture:1973 
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 17261541
Landing Gear Type: Tricycle
Seats:4 
Date/Type of Last Inspection: 07/03/2019, Annual
Certified Max Gross Wt.: 2300 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 3948 Hours as of last inspection
Engine Manufacturer: Lycoming 
ELT: C91 installed, not activated
Engine Model/Series: O-320-E2D
Registered Owner: On file 
Rated Power: 150 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: KMQB, 707 ft msl
Distance from Accident Site: 8 Nautical Miles
Observation Time: 1635 CDT
Direction from Accident Site: 57°
Lowest Cloud Condition: Scattered / 3400 ft agl
Visibility:  10 Miles
Lowest Ceiling:
Visibility (RVR):
Wind Speed/Gusts: 3 knots /
Turbulence Type Forecast/Actual: Unknown / Unknown
Wind Direction: 360°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 29.97 inches Hg
Temperature/Dew Point: 23°C / 14°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Colusa, IL (IL84)
Type of Flight Plan Filed: None
Destination: Macomb, IL (MQB)
Type of Clearance: None
Departure Time: 1545 CDT
Type of Airspace: Class G

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: 40.451111, -90.790833 (est)