NTSB Final Report: Beech F33 | 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-05.06.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Thu, Mar 14, 2024

NTSB Final Report: Beech F33

Internal Failure Of The Autopilot Pitch Servo Actuator That Caused The Autopilot To Command A Nose Down Movement

Location: Bellefontaine, Ohio Occurrence Number: ENG22LA004
Date & Time: November 12, 2021, 09:02 Local Registration: N9035Q
Aircraft: Beech F33 Aircraft Damage: Minor
Defining Event: Sys/Comp malf/fail (non-power) Injuries: 1 None
Flight Conducted Under: Part 91: General aviation - Personal

Analysis: The pilot reported an uncommanded nose down pitch trim movement. The nose down pitch trim occurred immediately following the pilot’s engagement of the autopilot. The uncommanded nose down trim was repeated when the pilot engaged the autopilot later in the occurrence flight as well as during postflight troubleshooting. 

During the NTSB’s autopilot examination on the airplane, the uncommanded nose down pitch trim movement occurred repeatedly upon autopilot engagement. When the Garmin GSA 28 pitch servo actuator was removed and replaced with another GSA 28 servo, the uncommanded nose down pitch trim movement ceased.

The pitch servo actuator examination at Garmin resulted in test element failures (related to monitoring of the pitch servo torque) that, with the servo installed as part of the airplane’s autopilot, would have caused the autopilot pitch down movement, and, after several seconds, an automatic disconnect. Garmin’s analysis showed that an internal failure on the pitch servo actuator circuit card could cause uncommanded autopilot pitch trim movement before the autopilot would automatically disconnect.

As a result of the investigation, the FAA issued a notice of proposed rulemaking (NPRM) for various airplanes modified with the Garmin 500 GFC Autopilot System. The proposed Airworthiness Directive (AD) would require a mandatory software upgrade to the system. 

Probable Cause and Findings: The National Transportation Safety Board determines the probable cause(s) of this occurrence to
be -- The internal failure of the autopilot pitch servo actuator that caused the autopilot to command a nose down movement of the pitch trim.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (05.09.24): Hold Procedure

Hold Procedure A predetermined maneuver which keeps aircraft within a specified airspace while awaiting further clearance from air traffic control. Also used during ground operatio>[...]

ANN's Daily Aero-Term (05.06.24): Altitude Readout

Altitude Readout An aircraft’s altitude, transmitted via the Mode C transponder feature, that is visually displayed in 100-foot increments on a radar scope having readout cap>[...]

ANN's Daily Aero-Linx (05.06.24)

Aero Linx: European Hang Gliding and Paragliding Union (EHPU) The general aim of the EHPU is to promote and protect hang gliding and paragliding in Europe. In order to achieve this>[...]

Airborne-NextGen 05.07.24: AI-Piloted F-16, AgEagle, 1st 2 WorldView Sats

Also: Skydio Chief, Uncle Sam Sues, Dash 7 magniX, OR UAS Accelerator US Secretary of the Air Force Frank Kendall was given a turn around the patch in the 'X-62A Variable In-flight>[...]

Aero-News: Quote of the Day (05.07.24)

"The need for innovation at speed and scale is greater than ever. The X-62A VISTA is a crucial platform in our efforts to develop, test and integrate AI, as well as to establish AI>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC