NTSB Final Report: Britten-Norman BN-2A | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.17.25

AirborneNextGen-
11.11.25

Airborne-Unlimited-11.12.25

Airborne-FltTraining-11.13.25

AirborneUnlimited-11.14.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Tue, Oct 10, 2023

NTSB Final Report: Britten-Norman BN-2A

Pilot Allowed The Airspeed To Decrease During The Approach, Increased Pitch Attitude, And Exceeded Critical Angle Of Attack

Location: Beaver Island, Michigan Accident Number: CEN22FA031
Date & Time: November 13, 2021, 13:49 Local Registration: N866JA
Aircraft: Britten-Norman BN-2A Aircraft Damage: Substantial
Defining Event: Aerodynamic stall/spin Injuries: 4 Fatal, 1 Serious
Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled

Analysis: A pilot-rated witness observed the airplane during the final approach to the destination airport and stated that the airplane was flying slowly, with a high pitch attitude, and was “wallowing” as if nobody was flying. The airplane stalled and impacted the ground about 300 ft from the runway. GPS and automatic dependent surveillance-broadcast (ADS-B) data captured the accident flight, but the ADS-B data ended about 0.24 miles before the accident. GPS data showed that the airplane’s speed was at or near the published stall speed for the airplane’s given loading condition.

The airplane sustained substantial damage to the fuselage and both wings. Examination of the airplane verified flight and engine control continuity. No preimpact anomalies were found with respect to the airplane, engines, or systems.

The pilot allowed the airspeed to decrease during the approach, increased pitch attitude, and exceeded critical angle of attack, which resulted in an aerodynamic stall and spin into terrain. 

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 final approach, which resulted in an aerodynamic stall and loss of control at an altitude too low to recover.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (11.14.25): Marker Beacon

Marker Beacon An electronic navigation facility transmitting a 75 MHz vertical fan or boneshaped radiation pattern. Marker beacons are identified by their modulation frequency and >[...]

Aero-News: Quote of the Day (11.14.25)

“Aviation is an incredible tool for Samaritan’s Purse. After a disaster strikes, we want people to know why we are bringing life-saving supplies. We want them to know t>[...]

Classic Aero-TV: CiES All-Digital Fuel Senders

From 2024 (YouTube Edition): New Capabilities For Business Aviation CiES Corporation President Scott Philiben walked Aero-News Editor in Chief Jim Campbell through some of what set>[...]

Airborne 11.10.25: Affordable Expo Succeeds, Citation Ascend, Kenai Shuts Down

Also: Duffy Predicts ‘Mass Chaos’, Modern Skies Coalition, More Impacts, Archer Buys Hawthorne With only a few months of preparation—and minimal outside media sup>[...]

NTSB Final Report: Lancair 320

The Experienced Pilot Chose To Operate In Instrument Meteorological Conditions Without An Instrument Flight Rules Clearance Analysis: The airplane was operated on a personal cross->[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC