- Effective
- July 28, 2010
- Published
- June 23, 2010 · 75 FR 35611–35613
- Issued
- June 10, 2010
- Models
- DC-10-10, DC-10-10F, MD-10-10F
- Data sheet
- TCDSA22WE
- Registered aircraft
- 2 matched by model
- Product
- Aircraft · Large airplane
- ATA chapter
- 57 · Wings
- Amendment
- 39-16337
- Docket
- FAA-2010-0043
- Project
- 2009-NM-128-AD
- Issued as
- Final rule
Unofficial copy from the Federal Register XML, document 2010-14982. 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 | 152 KB | 424d13fe…6d4d862 | 2010-14982.pdf on govinfo.gov |
| Federal Register XML | 18 KB | 7e4dc46d…7082d79 | 2010-14982.xml on federalregister.gov |
| FAA DRS HTML attachment | 55 KB | 49b56211…0595780 | FAA DRS (API key needed) |
| FAA DRS PDF | 48 KB | 533e5959…53b262a | FAA DRS (API key needed) |
On this page
Summary
We are adopting a new airworthiness directive (AD) for certain Model DC-10-10, DC-10-10F, and MD-10-10F airplanes. This AD requires a one-time high frequency eddy current inspection of fastener holes for cracks at the left and right side wing rear spar lower cap at station Xors=345, and other specified and corrective actions if necessary. This AD results from a report of three instances of Model DC-10-10F airplanes having fuel leaks in the wing rear spar lower cap at station Xors=345. We are issuing this AD to prevent cracks in the spar cap, which could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.
The airworthiness directive
2010-13-06 McDonnell Douglas Corporation: Amendment 39-16337. Docket No. FAA-2010-0043; Directorate Identifier 2009-NM-128-AD.
(a) Effective Date
PDF page 2(a) This airworthiness directive (AD) is effective July 28, 2010.
(b) Affected ADs
PDF page 2(b) None.
(c) Applicability
PDF page 2(c) This AD applies to McDonnell Douglas Corporation Model DC-10-10, DC-10-10F, and MD-10-10F airplanes, certificated in any category, as specified in Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009.
(d) Subject
PDF page 2(d) Air Transport Association (ATA) of America Code 57: Wings.
(e) Unsafe Condition
PDF page 2(e) This AD results from a report of three instances of Model DC-10-10F airplanes having fuel leaks in the wing rear spar lower cap at station Xors=345. The Federal Aviation Administration is issuing this AD to prevent cracking in the spar cap, which could lead to cracking of the lower wing skin, fuel leaks, and the inability of the structure to sustain limit load.
(f) Compliance
PDF page 2(f) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
(g) Inspection
PDF page 2(g) Within 3,000 flight cycles after the effective date of this AD, do a one-time high frequency eddy current inspection for cracking of fastener holes at the left and right side wing rear spar lower cap at station Xors=345, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009.
(1) If no cracking is found, before further flight, cold work open holes and install new second oversize fasteners and nut assemblies in the left and right side wing rear spar lower cap, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009.
(2) If any cracking is found during any inspection required by this AD, before further flight, repair the left and right side wing rear spar lower cap using a method approved in accordance with the procedures specified in paragraph (h) of this AD.
(h) Alternative Methods of Compliance (AMOCs)
PDF page 2(h)(1) The Manager, Los Angeles Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Nenita Odesa, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles ACO, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5234; fax (562) 627-5210.
(2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD.
(3) An AMOC that provides an acceptable level of safety may be used for any repair required by this AD, if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Los Angeles ACO, to make those findings. For a repair method to be approved, the repair must meet the certification basis of the airplane and 14 CFR 25.571, Amendment 45, and the approval must specifically refer to this AD.
(i) Material Incorporated by Reference
PDF page 2(i) You must use Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009, to do the actions required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
(3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221.
(4) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This AD is effective July 28, 2010.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of July 28, 2010.
AddressesPage 1
For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, 3855 Lakewood Boulevard, MC D800-0019, Long Beach, California 90846-0001; telephone 206-544-5000, extension 2; fax 206-766-5683; e-mail dse.boecom@boeing.com; Internet https://www.myboeingfleet.com.
For further information contactPage 1
Nenita Odesa, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5234; fax (562) 627-5210.
DiscussionPage 1
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to certain McDonnell Douglas Model DC-10-10, DC-10-10F, and MD-10-10F airplanes. That NPRM was published in the Federal Register on January 19, 2010 (75 FR 2831). That NPRM proposed to require a one-time high frequency eddy current inspection of fastener holes for cracks at the left and right side wing rear spar lower cap at station Xors=345, and other specified and corrective actions if necessary.
CommentsPage 1
We gave the public the opportunity to participate in developing this AD. We considered the comments received. FedEx supports the NPRM with the following comment.
Request for Clarification Regarding Estimated CostsPage 1
FedEx states that the numbers in the Estimated Costs table of the NPRM do not match the numbers in Boeing Alert Service Bulletin DC10-57A157, dated May 12, 2009. FedEx states that the cost per airplane is either $944 or $1,319 for parts, and requires 42.4 work-hours, totaling either $4,711 or $4,336 per airplane depending on group, according to the service bulletin. FedEx states that the NPRM gives a cost estimate of $160 per airplane.
We infer that the commenter wants clarification regarding the difference in the estimated costs. Since issuance of the NPRM, we have increased the labor rate used in the Costs of Compliance from $80 per work-hour to $85 per work-hour. The Costs of Compliance information, below, reflects this increase in the specified hourly labor rate. The cost of the required inspection is 2 hours at $85 per work-hour, totaling $170 per airplane. The service bulletin includes costs for on-condition actions, including $944 or $1,319 for the cost of parts and 42.4 work-hours. However, the economic analysis of an AD is limited to the cost of actions that are actually required. The economic analysis does not consider the costs of on-condition actions, such as repairing a crack detected during a required inspection (“repair, if necessary”). Such on-condition repairs would be required—regardless of AD direction—to correct an unsafe condition identified in an airplane and to ensure that the airplane is operated in an airworthy condition, as required by the Federal Aviation Regulations. We have not changed the AD in this regard.
ConclusionPage 1
We reviewed the relevant data, considered the comments received, and determined that air safety and the public interest require adopting the AD as proposed.
Costs of CompliancePage 1
We estimate that this AD affects 68 airplanes of U.S. registry. The following table provides the estimated costs for U.S. operators to comply with this AD.
| Action | Work hours | Average labor rate per hour | Cost per product | Number of U.S.- registered airplanes | Fleet cost |
|---|---|---|---|---|---|
| Inspection | 2 | $85 | $170 | 68 | $11,560 |
Authority for This RulemakingPage 2
Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. “Subtitle VII: Aviation Programs,” describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in “Subtitle VII, Part A, Subpart III, Section 44701: General requirements.” Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.
Regulatory findingsPage 2
This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a “significant regulatory action” under Executive Order 12866,
(2) Is not a “significant rule” under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), and
(3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.
You can find our regulatory evaluation and the estimated costs of compliance in the AD Docket.
Adoption of the amendmentPage 2
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
1. The authority citation for part 39 continues to read as follows:
2. The FAA amends § 39.13 by adding the following new AD:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 2
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1971 | 1 |
|---|---|
| 1972 | 1 |