Additional Participating Entity:
Federal Aviation Administration / Flight Standards District Office; Wichita, Kansas
Aviation Accident Final Report - National Transportation Safety Board: https://app.ntsb.gov/pdf
Investigation Docket - National Transportation Safety Board: https://dms.ntsb.gov/pubdms
Aviation Accident Data Summary - National Transportation Safety Board: https://app.ntsb.gov/pdf
http://registry.faa.gov/N4189V
Accident Number: GAA17CA489
Date & Time: 08/11/2017, 1302 CDT
Registration: N4189V
Aircraft: CESSNA 170
Aircraft Damage: Substantial
Defining Event: Aerodynamic stall/spin
Injuries: 2 None
Flight Conducted Under: Part 91: General Aviation - Personal
Analysis
***This report was modified on January 3, 2018. Please see the docket for this accident to view the original report.***
The pilot reported that, during a go-around after a low approach, the left cabin door opened. He added that he reached back to close the door and that the airplane then aerodynamically stalled. The pilot was unable to recover, and the airplane impacted the ground and struck multiple fences.
The airplane sustained substantial damage to the fuselage.
The pilot reported that there were no preaccident mechanical failures or malfunctions 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 exceedance of the airplane's critical angle of attack during a go-around. Contributing to the accident was the pilot's decision to attempt to close a passenger door during a critical phase of flight.
Findings
Aircraft
Angle of attack - Capability exceeded (Cause)
Passenger/crew doors - Related operating info (Factor)
Personnel issues
Aircraft control - Pilot (Cause)
Decision making/judgment - Pilot (Factor)
Environmental issues
Fence/fence post - Contributed to outcome
Factual Information
History of Flight
Approach-VFR go-around
Aerodynamic stall/spin (Defining event)
Collision with terr/obj (non-CFIT)
Pilot Information
Certificate: Private
Age: 18, Male
Airplane Rating(s): Single-engine Land
Seat Occupied: Left
Other Aircraft Rating(s): None
Restraint Used: Unknown
Instrument Rating(s): None
Second Pilot Present: No
Instructor Rating(s): None
Toxicology Performed: No
Medical Certification: Class 1 With Waivers/Limitations
Last FAA Medical Exam: 01/17/2017
Occupational Pilot:
Last Flight Review or Equivalent:
Flight Time:
Aircraft and Owner/Operator Information
Aircraft Manufacturer: CESSNA
Registration: N4189V
Model/Series: 170 UNDESIGNATED
Aircraft Category: Airplane
Year of Manufacture:
Amateur Built: No
Airworthiness Certificate: Normal
Serial Number: 18522
Landing Gear Type: Tailwheel
Seats: 4
Date/Type of Last Inspection: Unknown
Certified Max Gross Wt.: 2200 lbs
Time Since Last Inspection:
Engines: 1 Reciprocating
Airframe Total Time:
Engine Manufacturer: CONT MOTOR
ELT:
Engine Model/Series: C145 SERIES
Registered Owner: BLONDEL, RONALD W.
Rated Power: 145 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: KFNB, 980 ft msl
Observation Time: 1753 UTC
Distance from Accident Site: 33 Nautical Miles
Direction from Accident Site: 68°
Lowest Cloud Condition: Scattered / 3700 ft agl
Temperature/Dew Point: 25°C / 16°C
Lowest Ceiling:
Visibility: 10 Miles
Wind Speed/Gusts, Direction: 7 knots, 20°
Visibility (RVR):
Altimeter Setting: 30.13 inches Hg
Visibility (RVV):
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: SENECA, KS (62K)
Type of Flight Plan Filed: Unknown
Destination:
Type of Clearance: Unknown
Departure Time: 1301 CDT
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: 39.870833, -96.259167 (est)
Preventing Similar Accidents
Prevent Aerodynamic Stalls at Low Altitude
While maneuvering an airplane at low altitude in visual meteorological conditions, many pilots fail to avoid conditions that lead to an aerodynamic stall, recognize the warning signs of a stall onset, and apply appropriate recovery techniques. Many stall accidents result when a pilot is momentarily distracted from the primary task of flying, such as while maneuvering in the airport traffic pattern, during an emergency, or when fixating on ground objects.
An aerodynamic stall can happen at any airspeed, at any altitude, and with any engine power setting. Pilots need to be honest with themselves about their knowledge of stalls and preparedness to recognize and handle a stall situation. Training can help pilots fully understand the stall phenomenon, including angle-of-attack (AOA) concepts and how weight, center of gravity, turbulence, maneuvering loads, and other factors can affect an airplane's stall characteristics. The stall characteristics may be different in each type of airplane, so learn them before you fly.
The stall airspeeds marked on the airspeed indicator (for example, the bottom of the green arc and the bottom of the white arc) typically represent steady flight speeds at 1G at the airplane's maximum gross weight in the specified configuration. Maneuvering loads and other factors can increase the airspeed at which the airplane will stall. For example, increasing bank angle can increase stall speed exponentially.
Reducing AOA by lowering the airplane's nose at the first indication of a stall is the most important immediate response for stall avoidance and stall recovery. This may seem counterintuitive at low altitudes, but is a necessary first step.
See https://www.ntsb.gov/safety/safety-alerts/documents/SA_019.pdf for additional resources.
The NTSB presents this information to prevent recurrence of similar accidents. Note that this should not be considered guidance from the regulator, nor does this supersede existing FAA Regulations (FARs).
==========
AXTELL, Kan. (KWCH) - No one was hurt after a plane crash on Friday afternoon near Axtell.
According to the Kansas Highway Patrol, 18-year-old Nicholas Buessing was piloting the plane one mile west of Axtell when the door opened unexpectedly. Buessing tried to grab the door but ended up flying the plane into the ground.
The crash happened one mile west of Axtell on Jayhawk Road.
One other passenger was inside of the plane at the time.
Original article ➤ http://www.kwch.com
MARSHALL COUNTY – Two people avoided serious injury after an airplane accident just before 2p.m. Friday in Marshall County.
A 1948 Cessna 170 fixed wing aircraft piloted by Nicholas Buessing, 18, Axtel, was 600 feet above the ground with a ground speed of 90 mph in the 2900 Block of Jayhawk Road, one mile West of Axtell, according to the Kansas Highway Patrol.
The pilot’s side door opened unexpectedly. When the pilot reached to grab the door, he lost control of the aircraft and it struck the ground.
Buessing and a passenger Christian Buessing, 21, Axtel, were not injured.
The Federal Aviation Administration is investigating the incident, according to the KHP.
Original article ➤ https://www.hayspost.com
No comments:
Post a Comment