NTSB Prelim: Piper PA22 | 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

Fri, Jul 24, 2020

NTSB Prelim: Piper PA22

Pilot Heard And Felt A "Pop" That Appeared To Emanate From Somewhere In The Airplane

Location: Soldotna, AK Accident Number: ANC20LA064
Date & Time: 07/04/2020, 1523 AKD Registration: N3604A
Aircraft: Piper PA22 Injuries: 1 None
Flight Conducted Under: Part 91: General Aviation - Personal

On July 4, 2020, about 1523 Alaska daylight time, a Piper PA-22 airplane, N3604A, was substantially damaged when it was involved in an accident near Soldotna, Alaska. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that once established in a cruise, level flight configuration, around 1,300 ft mean sea level (msl), he heard and felt a "pop" that appeared to emanate from somewhere in the airplane. He said that the airplane then began a shallow, uncommanded descent, and the elevator began to "flutter." The pilot noted that the elevator was not "stuck", but he was unable to maintain altitude. The pilot subsequently selected a paved, rural neighborhood road as an emergency landing site. During touchdown, the airplane landed hard, and the main landing gear collapsed, sustaining substantial damage to the left wing, both wing lift struts, and the fuselage.

A Federal Aviation Administration (FAA) aviation safety inspector examined the airplane after recovery and reported that flight control continuity was established. The inspector noted that the area above the windscreen, where the fabric was connected to the fuselage, had separated.

He also indicated that the fabric did not tear, rather the adhesive that held the fabric to the structure failed, and a portion of the fabric peeled aft.

FAA Airworthiness Directive (AD) 74-17-04, applies, in part, to Piper PA-22 series airplanes. In short, the AD provides instructions for installing a reinforcement metal strip to avoid a sudden failure of the fabric at the top of the windscreen where the fabric attaches to the channel.

An NTSB wreckage and maintenance logbook examination, to include historical AD compliance, is pending.

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