AD (Australia) Air Tractor | 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-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Wed, May 07, 2003

AD (Australia) Air Tractor

Wing Centreline Splice Joint 6/2003
Applicability: Models AT-300, AT-301, AT-302, and AT-400A aircraft, all serial numbers, that
have aluminium spar caps; Models AT-400 aircraft, serial numbers 400-0244 through 400-0415, that have aluminium spar caps; Models AT-300 and AT-301 aircraft, all serial numbers, that have aluminium spar caps and are, or have been converted to turbine power.
Accomplish either the Requirement 1 spar lower cap replacement or the Requirement...
2 spar lower cap repetitive inspections.
Repetitively inspect the wing lower spar caps instead of replacement...
Replace the wing spar lower caps before further flight after whichever occurs first:
(i) The date of the scheduled replacement;
(ii) Cracks are found during any inspection allowed by Requirement 2 of this Directive; or,
(iii) Upon accumulating 600 hours time in service after the initial inspection
accomplished in accordance with Requirement 2.b. of this Directive.
This Amendment becomes effective on 7 May 2003.
Background: The FAA received a report of an in- flight separation of a wing from a Model AT-400A aircraft. Investigation revealed that fatigue caused the lower aluminium spar cap to fail across the 3/8- inch hole, 6.5 inches outboard of the fuselage centreline in the centre splice connection. The actions specified in this Directive are intended to detect and correct cracks in the centreline splice joint. Undetected cracks could eventually result in in- flight separation of the wing. Amendment 1 is issued in response to a new FAA AD which further reduces the mandatory wing spar lower cap replacement times; in response to inspection results from FAA AD 2002-13-02.
The original issue of this Airworthiness Directive became effective on 24 July 2002.

FMI: www.casa.gov.au/avreg/aircraft/ad/ADfiles/Under/at/at-022.pdf

Advertisement

More News

NTSB Final Report: Rutan Long-EZ

He Attempted To Restart The Engine Three Times. On The Third Restart Attempt, He Noticed That Flames Were Coming Out From The Right Wing Near The Fuel Cap Analysis: The pilot repor>[...]

ANN FAQ: Turn On Post Notifications

Make Sure You NEVER Miss A New Story From Aero-News Network Do you ever feel like you never see posts from a certain person or page on Facebook or Instagram? Here’s how you c>[...]

Classic Aero-TV: ICAS Perspectives - Advice for New Air Show Performers

From 2009 (YouTube Edition): Leading Air Show Performers Give Their Best Advice for Newcomers On December 6th through December 9th, the Paris Las Vegas Hotel hosted over 1,500 air >[...]

ANN's Daily Aero-Linx (06.28.25)

Aero Linx: NASA ASRS ASRS captures confidential reports, analyzes the resulting aviation safety data, and disseminates vital information to the aviation community. The ASRS is an i>[...]

Aero-News: Quote of the Day (06.28.25)

“For our inaugural Pylon Racing Seminar in Roswell, we were thrilled to certify 60 pilots across our six closed-course pylon race classes. Not only did this year’s PRS >[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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