- Effective
- July 14, 2003
- Published
- July 9, 2003 · 68 FR 40759–40761
- Issued
- July 4, 2003
- Models
- 737-200 Series, 737-200C Series, 737-300 Series, 737-400 Series, 737-500 Series
- Data sheet
- TCDSA16WE
- Registered aircraft
- 52 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-13225
- Docket
- 2003-NM-165-AD
- Issued as
- Final rule; request for comments
Unofficial copy from the Federal Register XML, document 03-17432. 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 | 141 KB | 514ae79f…1c3d78c | 03-17432.pdf on govinfo.gov |
| Official PDF | 136 KB | a3d7226e…f86b3a1 | 03-18421.pdf on govinfo.gov |
| Federal Register XML | 21 KB | d68713fc…9d6ebb6 | 03-17432.xml on federalregister.gov |
| Federal Register XML | 4 KB | bc77bf98…74f4865 | 03-18421.xml on federalregister.gov |
| FAA DRS HTML attachment | 66 KB | 149d6ac9…6932fdf | FAA DRS (API key needed) |
| FAA DRS PDF | 42 KB | 8419cf8b…0aa04ef | FAA DRS (API key needed) |
On this page
Summary
This document corrects a typographical error that appeared in airworthiness directive (AD) 2003-14-06 that was published in the Federal Register on July 9, 2003 (68 FR 40759). The typographical error resulted in an incorrect AD number in one location of the document. This AD is applicable to certain Boeing Model 737-200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for cracking of certain lap splices, and corrective action if necessary.
The airworthiness directive
2003-14-06 Boeing: Amendment 39-13225. Docket 2003-NM-165-AD.
On page 40761, in the first column, the Product Identification line of AD 2003-14-06 is corrected to read as follows:
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
Effective July 14, 2003.
For further information contactPage 1
Duong Tran, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6452; fax (425) 917-6590.
Supplementary informationPage 1
Airworthiness Directive (AD) 2003-14-06, amendment 39-13225, applicable to certain Boeing Model 737-200, -200C, -300, -400, and -500 series airplanes, was published in the Federal Register on July 9, 2003 (68 FR 40759). That AD requires repetitive inspections for cracking of certain lap splices, and corrective action if necessary.
As published, the AD number appears as “2003-14-60” in the Product Identification line in the regulatory text of the AD. The correct AD number is 2003-14-06. The number is referenced correctly throughout the remainder of the document.
Since no other part of the regulatory information has been changed, the final rule is not being republished in the Federal Register.
The effective date of this AD remains July 14, 2003.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 52
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1969 | 1 |
|---|---|
| 1975 | 1 |
| 1979 | 1 |
| 1981 | 1 |
| 1986 | 3 |
| 1987 | 4 |
| 1989 | 2 |
| 1990 | 1 |
| 1991 | 5 |
| 1992 | 4 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 3 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 1 |
16 with no year recorded