Tuesday, May 26, 2020

Landing Area Overshoot: Cirrus SR20, N902ES; accident occurred May 31, 2019 near Bulverde Airpark (1T8), Texas












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

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/N902ES

Location: San Antonio, TX
Accident Number: GAA19CA299
Date & Time: 05/31/2019, 1432 CDT
Registration: N902ES
Aircraft: Cirrus SR20
Aircraft Damage: Substantial
Defining Event: Landing area overshoot
Injuries: 1 Minor
Flight Conducted Under: Part 91: General Aviation - Personal 

The pilot reported that, during the approach, the airspeed was about 80 knots, but he was slightly high. The pilot stated that the airplane floated down the runway further than normal before it touched down, and when he determined that he would not have enough runway to stop, he aborted the landing. The airplane did not climb as he expected, and subsequently impacted trees. The pilot added that he believed that the reason for the lack of climb was due to his failure to retract the flaps to 50%.

A witness reported that the airplane landed further down the runway than normal, departed the runway, and began the takeoff from the grass alongside the runway.

The airplane sustained substantial damage to the left wing.

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

Pilot Information

Certificate: Private
Age: 51, 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: Class 3 With Waivers/Limitations
Last FAA Medical Exam: 04/19/2019
Occupational Pilot: No
Last Flight Review or Equivalent: 09/27/2018
Flight Time:  (Estimated) 116.7 hours (Total, all aircraft), 12.7 hours (Total, this make and model), 59.1 hours (Pilot In Command, all aircraft), 12.2 hours (Last 90 days, all aircraft), 3.3 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Cirrus
Registration: N902ES
Model/Series: SR20 No Series
Aircraft Category: Airplane
Year of Manufacture: 2002
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 1253
Landing Gear Type: Tricycle
Seats: 4
Date/Type of Last Inspection: 03/21/2019, Annual
Certified Max Gross Wt.: 3000 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 992.4 Hours as of last inspection
Engine Manufacturer:Continental 
ELT: Installed, not activated
Engine Model/Series: IO-360-ES16B
Registered Owner: On file
Rated Power: 200 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: , 789 ft msl
Distance from Accident Site: 13 Nautical Miles
Observation Time: 1430 CDT
Direction from Accident Site: 262°
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 8 knots /
Turbulence Type Forecast/Actual: None / None
Wind Direction: 6°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting:
Temperature/Dew Point: 32°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: San Antonio, TX (1T8)
Type of Flight Plan Filed: None
Destination: San Antonio, TX (1T8)
Type of Clearance:None 
Departure Time: 1400 CDT
Type of Airspace: Class G

Airport Information

Airport: Bulverde Airpark (1T8)
Runway Surface Type: Asphalt
Airport Elevation: 1080 ft
Runway Surface Condition: Dry
Runway Used: 16
IFR Approach: None
Runway Length/Width: 2890 ft / 40 ft
VFR Approach/Landing: Go Around

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: 29.743889, -98.453056 (est)

Piper PA-44-180 Seminole, N417EP: Incident occurred May 23, 2020 at New Smyrna Beach Municipal Airport (KEVB), Volusia County, Florida

Federal Aviation Administration / Flight Standards District Office; Orlando, Florida

Aircraft lost directional control and struck a runway light.

Epic Aviation Inc

https://registry.faa.gov/N417EP

Date: 23-MAY-20
Time: 14:35:00Z
Regis#: N417EP
Aircraft Make: PIPER
Aircraft Model: PA44
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: INSTRUCTION
Flight Phase: TAKEOFF (TOF)
Operation: 91
Aircraft Operator: EPIC FLIGHT ACADEMY
Flight Number: EPIA684
City: NEW SMYRNA BEACH
State: FLORIDA

Cirrus SR22, N525SR: Accident occurred March 02, 2020 at John C. Tune Airport (KJWN), Nashville, Davidson County, Tennessee





















AIRCRAFT: 2006 CIRRUS SR22 N525SR, S/N: 2326, Hobbs 1209.0

ENGINE: Continental IO-550N, s/n: 690142


PROPELLER:  Hartzell


EQUIPMENT:


Garmin 327


Garmin 430


Garmin 340


Avidyne DFC 90


Avidyne IFD 440


DESCRIPTION OF ACCIDENT: Tornado damage

DESCRIPTION OF DAMAGES: Entire Airframe. Propeller strike. CAPS disassembled.


LOCATION OF AIRCRAFT: AMF Aviation LLC, Springfield, Tennessee


REMARKS: AIRFRAME, ENGINE AND PROPELLER LOGBOOKS WERE LOST IN STORM


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.


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

Powerplant System/Component Malfunction/Failure: Lancair LC41-550FG, N2514F; accident occurred May 30, 2019 near Cleburne Regional Airport (KCPT), Johnson County, Texas



Oil Pressure Switch with heat damage.
Continental Aerospace Technologies

Threaded end of oil pressure switch.
Continental Aerospace Technologies
 


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

Additional Participating Entities:

Federal Aviation Administration / Flight Standards District Office; Irving, Texas
Continental Aerospace Technologies; Mobile, Alabama
Textron Aviation, Inc; Wichita, Kansas
Van Bortel Aircraft Inc; Arlington, Texas
 
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/N2514F

Location: Cleburne, TX
Accident Number:CEN19LA159 
Date & Time: 05/30/2019, 1100 CDT
Registration: N2514F
Aircraft: Lancair LC41
Aircraft Damage: Substantial
Defining Event: Powerplant sys/comp malf/fail
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Business 

On May 30, 2019, about 1100 central daylight time, a Lancair LC41 airplane, N2514F, conducted a forced landing near the Cleburne Regional Airport (CPT), Cleburne, Texas. The pilot was not injured, and the airplane sustained substantial damage. The airplane was registered to and operated by Van Bortel Aircraft, Inc under the provisions of Title 14 Code of Federal Regulations Part 91 as a maintenance test flight. Visual meteorological conditions prevailed for the local flight at the time of the accident.

The flight was conducted to break-in the engine's No. 5 cylinder, which had just been replaced. During the flight, the pilot noticed the oil pressure warning light illuminate, followed by a low oil temperature indication. The pilot attempted to divert to CPT; however, the engine experienced a loss of power and he conducted a forced landing. During the landing, the airplane collided with trees and came to rest upright and partly submerged in a small pond about one mile from CPT.

Inspection of the airplane revealed substantial damage to the wings, and water submersion damage to the airplane. The airplane's Hobbs meter read 1,090.1 hours.

The airplane was recovered to a secure facility for further examination. The examination was conducted by the NTSB Investigator-in-Charge, a representative from Van Bortel Aircraft, and technical representatives from the engine and airframe manufacturers. The examination noted the engine case had a hole above the No. 4 cylinder, and when the propeller was rotated by hand, the engine had limited rotation and internal binding was noted. A light, oil film was noted on the bottom of the airplane. The exam also found an oil pressure switch separated in two pieces. The threaded section remained to its mating joint; the other section rested on an exhaust tube and attached by its wire connector as seen in Figure 1.

Figure 1: Oil Pressure Switch 

A visual inspection of the switch noted that the switch had separated at a manufacturing joint between the body and threaded section.

The switch was removed and sent to Textron Aviation, Inc, Materials Laboratory for a detailed examination of the switch. Textron's examination noted the switch failed at the swaged joint between the threaded section and the base cap section of the switch. The examination was not able to determine how the joint failed, since there were no physical indications as to how the swaged joint failed.

Pilot Information

Certificate: Airline Transport; Commercial; Flight Engineer
Age: 58
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
Toxicology Performed: No
Medical Certification: Class 1 Without Waivers/Limitations
Last FAA Medical Exam: 02/25/2019
Occupational Pilot:
Last Flight Review or Equivalent: 05/05/2019
Flight Time:  20019 hours (Total, all aircraft), 165 hours (Total, this make and model), 233 hours (Last 90 days, all aircraft), 73 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Lancair
Registration: N2514F
Model/Series: LC41 550FG
Aircraft Category: Airplane
Year of Manufacture:
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 41093
Landing Gear Type: Tricycle
Seats:
Date/Type of Last Inspection:  Annual
Certified Max Gross Wt.:
Time Since Last Inspection:
Engines: Reciprocating
Airframe Total Time: 1090.1 Hours at time of accident
Engine Manufacturer: Continental
ELT: C91A installed, activated, did not aid in locating accident
Engine Model/Series: TSIO-550-C(5)
Registered Owner: Van Bortel Aircraft, Inc
Rated Power: 310 hp
Operator: Van Bortel Aircraft, Inc
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: KCPT
Distance from Accident Site:
Observation Time: 0955 CDT
Direction from Accident Site:
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling:
Visibility (RVR):
Wind Speed/Gusts: 7 knots /
Turbulence Type Forecast/Actual:
Wind Direction: 350°
Turbulence Severity Forecast/Actual:
Altimeter Setting: 30.01 inches Hg
Temperature/Dew Point: 26°C / 17°C
Precipitation and Obscuration: No Precipitation
Departure Point: Arlington, TX (GKY)
Type of Flight Plan Filed: None
Destination: Arlington, TX (GKY)
Type of Clearance: None
Departure Time:
Type of Airspace:

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: 32.390278, -97.433611 (est)

Cessna 182A Skylane, N5179D: Accident occurred May 22, 2020 at Ionia County Airport (Y70), Michigan

Federal Aviation Administration / Flight Standards District Office; Grand Rapids, Michigan

School of Missionary Aviation Technology

https://registry.faa.gov/N5179D

NTSB Identification: CEN20CA193
14 CFR Part 91: General Aviation
Accident occurred Friday, May 22, 2020 in Ionia, MI
Aircraft: Cessna 182, registration: N5179D

NTSB investigators will use data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator, and will not travel in support of this investigation to prepare this aircraft accident report.

Aircraft ground looped after landing.

Date: 22-MAY-20
Time: 23:18:00Z
Regis#: N5179D
Aircraft Make: CESSNA
Aircraft Model: 182
Event Type: INCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: UNKNOWN
Activity: PERSONAL
Flight Phase: LANDING (LDG)
Operation: 91
City: IONIA
State: MICHIGAN

Landing Gear Not Configured: de Havilland Canada DHC-2 Beaver Mk I, N501J; accident occurred May 28, 2019 in Hollister, San Benito County, California








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

Aviation Accident Final 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/N501J


Location: Hollister, CA
Accident Number: GAA19CA108
Date & Time: 05/28/2019, 1530 PDT
Registration: N501J
Aircraft: De Havilland DHC 2
Aircraft Damage: Substantial
Defining Event: Landing gear not configured
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis 

The pilot in the amphibious float-equipped airplane reported that he intended to perform a water landing. On the downwind leg of the approach, he performed his prelanding checks from memory, and he confirmed that the three green landing gear safe lights were illuminated. However, he added that he "should have looked for blue lights." The pilot landed on the water with the landing gear wheels extended, and the airplane pitched forward and nosed over. The airplane sustained substantial damage to the right wing, the empennage, and the windscreen. The pilot asserted that he "should have used a checklist once airborne. Both the after takeoff and before landing checks would have saved me from this event." The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's failure to retract the amphibious float's landing gear wheels before landing on the water. Contributing to the accident was the pilot's failure to use the after takeoff and before landing checklists.

Findings

Aircraft 

Personnel issues
Use of equip/system - Pilot (Cause)
Use of checklist - Pilot (Factor)

Environmental issues
Water - Effect on operation (Cause)

Factual Information

History of Flight

Landing-flare/touchdown
Landing gear not configured (Defining event)

Nose over/nose down

Pilot Information

Certificate: Airline Transport; Flight Instructor; Commercial
Age: 63, Male
Airplane Rating(s): Multi-engine Land; Single-engine Land; Single-engine Sea
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 2 With Waivers/Limitations
Last FAA Medical Exam: 10/25/2018
Occupational Pilot: Yes
Last Flight Review or Equivalent: 05/07/2019
Flight Time: (Estimated) 15560 hours (Total, all aircraft), 111 hours (Total, this make and model), 11326 hours (Pilot In Command, all aircraft), 37 hours (Last 90 days, all aircraft), 9 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: De Havilland
Registration: N501J
Model/Series: DHC 2 I
Aircraft Category: Airplane
Year of Manufacture: 2004
Amateur Built: No
Airworthiness Certificate:
Serial Number: 1451
Landing Gear Type: Amphibian
Seats: 8
Date/Type of Last Inspection: 06/19/2018, Annual
Certified Max Gross Wt.: 5370 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 4690 Hours as of last inspection
Engine Manufacturer: PRATT & WHITNEY
ELT: C91A installed, not activated
Engine Model/Series: R-985 AN-14B
Registered Owner: Diesel Acquisitions Llc
Rated Power: 450 hp
Operator: Diesel Acquisitions Llc
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual Conditions
Condition of Light: Day
Observation Facility, Elevation: CVH, 705 ft msl
Distance from Accident Site: 17 Nautical Miles
Observation Time: 2235 UTC
Direction from Accident Site: 313°
Lowest Cloud Condition: Clear
Visibility:  10 Miles
Lowest Ceiling: None
Visibility (RVR):
Wind Speed/Gusts: 15 knots /
Turbulence Type Forecast/Actual:
Wind Direction: 260°
Turbulence Severity Forecast/Actual:
Altimeter Setting: 29.97 inches Hg
Temperature/Dew Point: 21°C / 13°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Hollister, CA (CVH)
Type of Flight Plan Filed: None
Destination: Hollister, CA (CVH)
Type of Clearance: None
Departure Time: 1500 PDT
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: 37.038056, -121.118056 (est)

Rockwell International S-2R, N5573X: Accident occurred May 23, 2020 in Artois, Glenn County, California

Federal Aviation Administration / Flight Standards District Office; Sacramento, California

Whitaker Inc

https://registry.faa.gov/N5573X


NTSB Identification: WPR20CA153
14 CFR Part 91: General Aviation
Accident occurred Saturday, May 23, 2020 in Artois, CA
Aircraft: Ayres S 2R, registration: N5573X

NTSB investigators will use data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator, and will not travel in support of this investigation to prepare this aircraft accident report.

Aircraft struck power lines and cartwheeled while attempting to land on a dirt strip.

Date: 23-MAY-20
Time: 02:00:00Z
Regis#: N5573X
Aircraft Make: ROCKWELL
Aircraft Model: S2R
Event Type: ACCIDENT
Highest Injury: NONE
Aircraft Missing: No
Damage: SUBSTANTIAL
Activity: AERIAL APPLICATION
Flight Phase: EN ROUTE (ENR)
Operation: 137
City: ARTOIS
State: CALIFORNIA

Landing Gear Not Configured: Beech A36 Bonanza, N998LS; accident occurred May 28, 2019 at Hilton Head Airport (KHXD), Beaufort County, South Carolina




Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Columbia, South Carolina

Aviation Accident Final 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/N998LS


Location: Hilton Head, SC

Accident Number: GAA19CA294
Date & Time: 05/28/2019, 1400 EDT
Registration: N998LS
Aircraft: RAYTHEON AIRCRAFT COMPANY A36
Aircraft Damage: Substantial
Defining Event: Landing gear not configured
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal

Analysis 

The pilot reported that, during an instrument flight rules approach, he failed to extend the landing gear, and the airplane landed on the runway with the landing gear retracted. The pilot added that the accident could have been prevented by "paying much closer attention to the checklists." The airplane sustained substantial damage to the lower fuselage. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's failure to extend the landing gear before landing. Contributing to the accident was the pilot's failure to complete the before landing checklist.

Findings

Aircraft
Gear extension and retract sys - Not used/operated (Cause)

Personnel issues
Use of equip/system - Pilot (Cause)
Use of checklist - Pilot (Factor)

Factual Information

History of Flight

Landing-flare/touchdown
Landing gear not configured (Defining event)

Pilot Information


Certificate: Private
Age: 53, Male
Airplane Rating(s): Single-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 3 Without Waivers/Limitations
Last FAA Medical Exam: 02/26/2019
Occupational Pilot: No
Last Flight Review or Equivalent: 03/31/2019
Flight Time:  (Estimated) 600 hours (Total, all aircraft), 350 hours (Total, this make and model), 500 hours (Pilot In Command, all aircraft), 15 hours (Last 90 days, all aircraft), 4 hours (Last 30 days, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: RAYTHEON AIRCRAFT COMPANY
Registration: N998LS
Model/Series: A36
Aircraft Category: Airplane
Year of Manufacture: 1998
Amateur Built: No
Airworthiness Certificate: Utility
Serial Number: E-3204
Landing Gear Type: Retractable - Tricycle
Seats: 4
Date/Type of Last Inspection: 03/05/2019, 100 Hour
Certified Max Gross Wt.: 3651 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 2083.4 Hours as of last inspection
Engine Manufacturer: Continental
ELT: C126 installed, not activated
Engine Model/Series: IO-550
Registered Owner: F & S Aviation Llc
Rated Power: 300 hp
Operator: F & S 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: KHXD, 24 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time: 1750 UTC
Direction from Accident Site: 196°
Lowest Cloud Condition: Few / 7000 ft agl
Visibility: 10 Miles
Lowest Ceiling: Broken / 25000 ft agl
Visibility (RVR):
Wind Speed/Gusts: 4 knots /
Turbulence Type Forecast/Actual:
Wind Direction: 100°
Turbulence Severity Forecast/Actual: 
Altimeter Setting: 29.94 inches Hg
Temperature/Dew Point: 35°C / 19°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Asheville, NC (AVL)
Type of Flight Plan Filed: IFR
Destination: Hilton Head, SC (HXD)
Type of Clearance: Cruise; IFR; Traffic Advisory
Departure Time: 1230 EDT
Type of Airspace: Class D

Airport Information

Airport: Hilton Head (HXD)
Runway Surface Type: Asphalt
Airport Elevation: 19 ft
Runway Surface Condition: Dry
Runway Used: 03
IFR Approach: Visual
Runway Length/Width: 5000 ft / 100 ft
VFR Approach/Landing: None

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: 32.224444, -80.697500 (est)