Airworthiness Directive

AD 2007-17-03 72 FR 46541 Active

Federal Aviation Administration · 14 CFR part 39

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.

FR document
E7-15978
Amendment
39-15161
Published
2007-08-21
Effective
2007-09-25
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2007-17-03

FR doc E7-15978 · 72 FR 46541

AD 2007-17-03Published 2007-08-21Effective 2007-09-25

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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:

More directives for Pacific Aerospace 750XL/FU24

  1. AD 2021-23-16 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2022-01-11
  2. AD 2021-23-19 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2022-01-11
  3. AD 2021-21-11 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-12-10
  4. AD 2021-21-10 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-12-10
  5. AD 2021-20-20 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-11-22

All Pacific Aerospace 750XL/FU24 directives

Applies to 1 model in our index