Monday, June 03, 2019

Aerodynamic Stall / Spin: Silvaire Luscombe 8A, N2689K; accident occurred June 01, 2019 at Heber City Municipal Airport (KHCR), Wasatch County, Utah

Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Salt Lake City, Utah

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/N2689K


Location: Heber, UT
Accident Number: GAA19CA301
Date & Time: 06/01/2019, 1645 MDT
Registration: N2689K
Aircraft: Luscombe 8
Aircraft Damage: Substantial
Defining Event: Aerodynamic stall/spin
Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal 

Analysis 

The pilot of the tailwheel-equipped airplane reported that, during the landing roll in a gusting crosswind, the airplane veered left. He added right rudder, which slowed the veer. However, he saw that the airplane was going to depart the runway, so he added full power and right rudder to abort the landing. The airplane became airborne but "stopped the climb, and slid tail first onto the ground." The right main landing gear collapsed, and the propeller and the right wing struck the ground.

The airplane sustained substantial damage to the right wing.

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

The airport's automated weather observation station reported that, about 10 minutes before the accident, the wind was from 010° at 10 knots and that, about 10 minutes after the accident, the wind was from 340° at 14 knots. The pilot landed the airplane on runway 04.

It is likely that, during the aborted landing, the pilot aerodynamically stalled the airplane.

Probable Cause and Findings

The National Transportation Safety Board determines the probable cause(s) of this accident to be:
The pilot's exceedance of the airplane's critical angle of attack during an aborted landing, which resulted in an aerodynamic stall.

Findings

Aircraft
Angle of attack - Capability exceeded (Cause)

Personnel issues
Aircraft control - Pilot (Cause)

Environmental issues
Crosswind - Effect on operation

Factual Information

History of Flight

Landing
Other weather encounter
Loss of control on ground
Attempted remediation/recovery

Takeoff
Aerodynamic stall/spin (Defining event)
Collision with terr/obj (non-CFIT)

Landing gear collapse

Pilot Information

Certificate: Airline Transport; Flight Instructor; Commercial; Flight Engineer; Military
Age: 57, 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; Instrument Airplane
Toxicology Performed: No
Medical Certification: Class 1 With Waivers/Limitations
Last FAA Medical Exam: 12/18/2018
Occupational Pilot: Yes
Last Flight Review or Equivalent: 08/24/2018
Flight Time:  (Estimated) 12383 hours (Total, all aircraft), 179.81 hours (Total, this make and model), 9697 hours (Pilot In Command, all aircraft), 112.6 hours (Last 90 days, all aircraft), 58 hours (Last 30 days, all aircraft), 1 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Luscombe
Registration: N2689K
Model/Series: 8 A
Aircraft Category: Airplane
Year of Manufacture: 1947
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 5416
Landing Gear Type: Tailwheel
Seats:2 
Date/Type of Last Inspection: 10/04/2018, Annual
Certified Max Gross Wt.: 1400 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time: 3222.9 Hours as of last inspection
Engine Manufacturer: Lycoming
ELT: C91  installed, activated, aided in locating accident
Engine Model/Series: O-320-A2B
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: KHCR, 5637 ft msl
Distance from Accident Site: 0 Nautical Miles
Observation Time: 2235 UTC
Direction from Accident Site: 274°
Lowest Cloud Condition:
Visibility:  10 Miles
Lowest Ceiling:
Visibility (RVR):
Wind Speed/Gusts: 10 knots /
Turbulence Type Forecast/Actual: None / None
Wind Direction: 10°
Turbulence Severity Forecast/Actual: N/A / N/A
Altimeter Setting: 30 inches Hg
Temperature/Dew Point: 22°C / 5°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Heber, UT (HCR)
Type of Flight Plan Filed: None
Destination: Heber, UT (HCR)
Type of Clearance: None
Departure Time: 1630 MDT
Type of Airspace: Class G

Airport Information

Airport: HEBER CITY MUNI - RUSS MCDONAL (HCR)
Runway Surface Type: Asphalt
Airport Elevation: 5636 ft
Runway Surface Condition: Dry
Runway Used: 04
IFR Approach: None
Runway Length/Width: 6898 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: 40.481944, -111.428056 (est)

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