Urgent CASA AD: Airbus | 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-04.29.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Tue, Jan 10, 2006

Urgent CASA AD: Airbus

Applicability: Model A318, A319, A320, and A321 aircraft, with Manufacturer Serial Number 0791, 1464, 1660, 1969, 1979, 2026, 2028, 2030, 2032, 2033, 2035, 2037, 2039, 2041, 2043, 2045, 2047, 2050 through 2053, 2055, 2057, 2059, 2060, 2062, 2064, 2066, 2067, 2069, 2071, 2072, 2074, 2078 through 2269, 2271 through 2506, 2508 through 2565, 2567 through 2580, 2582 through 2591, 2593 through 2597, 2600, 2601, 2605, 2607, 2610, or 2615.

Requirement:

  1. The following operational procedure is rendered mandatory for all flights: In the case of severe turbulence, strictly adhere to reduced speeds as defined in Aircraft Flight Manual Section 4.03.00 Page 03. Insertion of this Directive in the Aircraft Operations Manual and application of this procedure by flight crew complies with the above requirement of this Directive.
  2. For aircraft equipped with CFM engines: Inspect ribs 7, 8, and 9 of the left and right engine pylon spar box and apply all necessary corrective actions in accordance with Airbus All Operators Telex (AOT) A320-54A1015. Report the results of the inspection to Airbus in accordance with AOT A320-54A1015.
  3. For aircraft equipped with IAE engines: Inspect ribs 7, 8, and 9 of the left and right engine pylon spar box and apply all necessary corrective actions in accordance with AOT A320-54A1015. Report the results of the inspection to Airbus in accordance with AOT A320-54A1015.

Note: DGAC AD F-2006-011 refers.

Compliance:

  1. Effective from 14 January 2006.
  2. Within 6 months after 14 January 2006.
  3. Within 9 months after 14 January 2006.

This Airworthiness Directive becomes effective on 14 January 2006.

Background: The manufacturer recently discovered that certain engine pylon spar box ribs constructed of stainless steel material may not have been heat-treated in production, prior to installation in the pylon. The omission of the heat treatment operation results in a significant reduction of the material allowable yield stress. As a consequence, non heat-treated ribs may not meet all the certification requirements, especially for vertical gust.

FMI: www.casa.gov.au

Advertisement

More News

ANN's Daily Aero-Linx (05.02.24)

Aero Linx: Model Aeronautical Association of Australia MAAA clubs are about fun flying, camaraderie and community. For over 75 years, the MAAA has been Australia’s largest fl>[...]

ANN's Daily Aero-Term (05.02.24): Touchdown Zone Lighting

Touchdown Zone Lighting Two rows of transverse light bars located symmetrically about the runway centerline normally at 100 foot intervals. The basic system extends 3,000 feet alon>[...]

Aero-News: Quote of the Day (05.02.24)

“Discovery and innovation are central to our mission at Virgin Galactic. We’re excited to build on our successful record of facilitating scientific experiments in subor>[...]

ANN FAQ: Contributing To Aero-TV

How To Get A Story On Aero-TV News/Feature Programming How do I submit a story idea or lead to Aero-TV? If you would like to submit a story idea or lead, please contact Jim Campbel>[...]

NTSB Final Report: Cirrus Design Corp SR20

Student Pilot Reported That During Rotation, “All Of A Sudden The Back Of The Plane Kicked To The Right..." Analysis: The student pilot reported that during rotation, “>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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