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Correction notice

AD 2001-23-07 66 FR 59357 Correction

Federal Aviation Administration · 14 CFR part 39

FR document
01-29492
Published
2001-11-28
Effective
2002-01-07
Models covered
1
Last live check
2026-10-01

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Correction

2001-23-07

FR doc 01-29492 · 66 FR 59357

AD 2001-23-07Published 2001-11-28Effective 2002-01-07

Requires repetitive inspections of the canted rib upper cap in the center wing carry-through area for cracks, and, if cracks are found, immediate repair of the cracks or modification of this area depending on the extent of any cracks found.

Full official abstract

This document makes a correction to Airworthiness Directive (AD) 2001-23-07, which was published in the Federal Register on November 15, 2001 (66 FR 57364), and concerns certain Reims Model F406 airplanes. The FAA incorrectly referenced the AD number as "AD 2001- 01-07" instead of "AD 2001-23-07." This AD requires repetitive inspections of the canted rib upper cap in the center wing carry-through area for cracks, and, if cracks are found, immediate repair of the cracks or modification of this area depending on the extent of any cracks found. This AD also requires modifying the canted rib upper cap at a certain time period as terminating action for the repetitive inspections. This action corrects the AD to reflect the correct AD number.

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All Cessna F406 Caravan II directives

This is a correction notice. The AD it corrects is not in our index yet, so we are showing the correction alone rather than implying we hold the directive itself.

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index