2007-17-03
FR doc E7-15978 · 72 FR 46541AD 2007-17-03Published 2007-08-21Effective 2007-09-25
Prompted by mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.
1 correction to this AD FAA · 2007-09-18
Correction published 2007-09-18
- Issued by
- Federal Aviation Administration
- Published
- 2007-09-18
- Document
- Federal Register E7-18136 · Final rule; correction
- Corrects
- the version published August 21, 2007 at 72 FR 46541
This document makes a correction to Airworthiness Directive (AD) 2007-17-03, which was published in the Federal Register on August 21, 2007 (72 FR 46541), and applies to certain Pacific Aerospace Corporation Ltd Model 750XL airplanes. AD 2007-17-03 requires inspecting the inboard end of the rear spar for security of the blind rivets, inspecting the radii of the rear spar upper and lower flanges for cracking, inspecting the aft flange of the inboard rib for cracking, replacing the rear spar if cracks are found in any of the inspections, and replacing rear spar blind rivets with bolts or rivets. The paragraph following the section heading Materials Incorporated by Reference does not have a paragraph designator. This document corrects that paragraph by inserting the paragraph designator "(i)" preceding the paragraph text.
A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.
Source: Federal Register document E7-18136, retrieved 2026-08-17
Full official abstract
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: