- Effective
- January 7, 2002
- Published
- November 28, 2001 · 66 FR 59357–59358
- Issued
- November 6, 2001
- Model
- F406
- Data sheet
- TCDSA54EU
- Registered aircraft
- 4 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-12504
- Docket
- 99-CE-28-AD
- Issued as
- Final rule; correction
Unofficial copy from the Federal Register XML, document 01-29492. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 133 KB | fdff52e4…98b2818 | 01-29492.pdf on govinfo.gov |
| Federal Register XML | 5 KB | 8ee64eec…ff8b650 | 01-29492.xml on federalregister.gov |
| FAA DRS HTML | 64 KB | 607def4c…8a8ac4b | FAA DRS (API key needed) |
On this page
Summary
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.
The airworthiness directive
Correction of Publication
PDF page 2Accordingly, the publication of November 15, 2001 (66 FR 57364), of Amendment 39-12504; AD 2001-01-07, which was the subject of FR Doc. 01-28571, is corrected as follows:
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
Effective datePage 1
The effective date of this AD remains January 7, 2002.
For further information contactPage 1
Brian A. Hancock, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4143, facsimile: (816) 329-4090.
DiscussionPage 1
On November 6, 2001, FAA issued AD 2001-01-07, Amendment 39-12504 (66 FR 57364, November 15, 2001), which applies to certain Reims Model F406 airplanes. This AD currently 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.
Need for the CorrectionPage 2
We incorrectly referenced the AD number as “AD 2001-01-07” instead of “AD 2001-23-07.” If we did not correct the AD number, then the logbooks of the affected airplane would reference compliance with the wrong AD.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 4
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1985 | 1 |
|---|---|
| 1987 | 1 |
| 1991 | 1 |
1 with no year recorded