- Effective
- May 2, 2008
- Published
- March 28, 2008 · 73 FR 16515–16517
- Issued
- March 20, 2008
- Models
- 727-100 Series, 727-200 Series, 727-200F Series, DC-9-14, DC-9-32, DC-9-32 (VC-9C) and 4 more
- Registered aircraft
- 32 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-15450
- Docket
- FAA-2007-0389
- Project
- 2007-NM-222-AD
- Issued as
- Final rule
Unofficial copy from the Federal Register XML, document E8-6298. 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 | e18ec728…4ef1b7e | E8-6298.pdf on govinfo.gov |
| Federal Register XML | 20 KB | 8edc1812…f325ace | E8-6298.xml on federalregister.gov |
| FAA DRS HTML attachment | 59 KB | cf0610b5…6953387 | FAA DRS (API key needed) |
| FAA DRS PDF | 28 KB | 33dd399b…cdce590 | FAA DRS (API key needed) |
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Summary
We are adopting a new airworthiness directive (AD) for various transport category airplanes. This AD requires deactivation of Southeast Aero-Tek, Inc., auxiliary fuel tanks. This AD results from fuel system reviews conducted by the manufacturer, which identified potential unsafe conditions for which the manufacturer has not provided corrective actions. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
The airworthiness directive
2008-07-09 Southeast Aero-Tek, Inc.: Amendment 39-15450. Docket No. FAA-2007-0389; Directorate Identifier 2007-NM-222-AD.
(a) Effective Date
PDF page 2(a) This airworthiness directive (AD) is effective May 2, 2008.
(b) Affected ADs
PDF page 2(b) None.
(c) Applicability
PDF page 2(c) This AD applies to airplanes, certificated in any category, equipped with auxiliary fuel tanks installed in accordance with specified supplemental type certificates (STCs), as identified in Table 1 of this AD. This AD does not apply to any airplane where an auxiliary fuel tank was installed in accordance with an STC identified in Table 1 of this AD and subsequently removed by an FAA-approved method.
| Airplanes | Auxiliary tank STC(s) |
|---|---|
| Boeing Model 727-100 series airplanes | ST01587AT |
| Boeing Model 727-200 and -200F series airplanes | SA2033NM, SA1474SO |
| McDonnell Douglas Model DC-9-14 airplanes | SA1334NM |
| McDonnell Douglas Model DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, and DC-9-32F (C-9A, C-9B) airplanes | SA1710SO, SA1358NM |
(d) Unsafe Condition
PDF page 2(d) This AD results from fuel system reviews conducted by the manufacturer, which identified potential unsafe conditions for which the manufacturer has not provided corrective actions. We are issuing this AD to prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplane.
(e) Compliance
PDF page 2(e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
(f) Report
PDF page 2(f) Within 45 days after the effective date of this AD, submit a report to the Manager, Atlanta Aircraft Certification Office (ACO), FAA. The report must include the information listed in paragraphs (f)(1) and (f)(2) of this AD. Under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements contained in this AD, and assigned OMB Control Number 2120-0056.
(1) The airplane registration and auxiliary tank STC number installed.
(2) The usage frequency in terms of total number of flights per year and total number of flights per year for which the auxiliary tank is used.
(g) Prevent Usage of Auxiliary Fuel Tanks
PDF page 2(g) On or before December 16, 2008, deactivate the auxiliary fuel tanks, in accordance with a deactivation procedure approved by the Manager, Atlanta ACO. Any auxiliary tank component that remains on the airplane must be secured and must have no effect on the continued operational safety and airworthiness of the airplane. Deactivation may not result in the need for additional instructions for continued airworthiness.
Note 1:
Appendix A of this AD provides criteria that should be included in the deactivation procedure. The proposed deactivation procedures should be submitted to the Manager, Atlanta ACO, as soon as possible to ensure timely review and approval.
Note 2:
For technical information, contact Randy Smith, President, Southeast Aero-Tek, Inc., 675 Oleander Drive, Merritt Island, Florida 32952; telephone (321) 453-7876; fax (321) 453-7872.
(h) Alternative Methods of Compliance (AMOCs)
PDF page 2(h)(1) The Manager, Atlanta ACO, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(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 appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.
(i) Material Incorporated by Reference
PDF page 2(i) None.
Appendix A—Deactivation Criteria
PDF page 2The auxiliary fuel tank deactivation procedure required by paragraph (g) of this AD should address the following actions.
(1) Permanently drain auxiliary fuel tanks, and clear them of fuel vapors to eliminate the possibility of out-gassing of fuel vapors from the emptied auxiliary tank.
(2) Disconnect all electrical connections from the fuel quantity indication system (FQIS), fuel pumps if applicable, float switches, and all other electrical connections required for auxiliary tank operation, and stow them at the auxiliary tank interface.
(3) Disconnect all pneumatic connections if applicable, cap them at the pneumatic source, and secure them.
(4) Disconnect all fuel feed and fuel vent plumbing interfaces with airplane original equipment manufacturer (OEM) tanks, cap them at the airplane tank side, and secure them in accordance with a method approved by the FAA; one approved method is specified in Advisory Circular 25-8 Fuel Tank Flammability Minimization. In order to eliminate the possibility of structural deformation during cabin decompression, leave open and secure the disconnected auxiliary fuel tank vent lines.
(5) Pull and collar all circuit breakers used to operate the auxiliary tank.
(6) Revise the weight and balance document, if required, and obtain FAA approval.
(7) Amend the applicable sections of the applicable airplane flight manual (AFM) to indicate that the auxiliary fuel tank is deactivated. Remove auxiliary fuel tank operating procedures to ensure that only the OEM fuel system operational procedures are contained in the AFM. Amend the Limitations Section of the AFM to indicate that the AFM Supplement for the STC is not in effect. Place a placard in the flight deck indicating that the auxiliary tank is deactivated. The AFM revisions specified in this paragraph may be accomplished by inserting a copy of this AD into the AFM.
(8) Amend the applicable sections of the applicable airplane maintenance manual to remove auxiliary tank maintenance procedures.
(9) After the auxiliary fuel tank is deactivated, accomplish procedures such as leak checks and pressure checks deemed necessary before returning the airplane to service. These procedures must include verification that the airplane FQIS and fuel distribution systems have not been adversely affected.
(10) Include with the operator's proposed procedures any relevant information or additional steps that are deemed necessary by the operator to comply with the deactivation and return the airplane to service.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This AD is effective May 2, 2008.
For further information contactPage 1
Robert Bosak, Aerospace Engineer, Propulsion and Services Branch, ACE-118A, FAA, Atlanta Aircraft Certification Office, One Crown Center, 1895 Phoenix Boulevard, Suite 450, Atlanta, Georgia 30349; telephone (770) 703-6094; fax (770) 703-6097.
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 various transport category airplanes equipped with auxiliary fuel tanks installed in accordance with certain supplemental type certificates (STCs). That NPRM was published in the Federal Register on January 2, 2008 (73 FR 84). That NPRM proposed to require deactivation of Southeast Aero-Tek, Inc., auxiliary fuel tanks.
CommentsPage 1
We gave the public the opportunity to participate in developing this AD. We considered the comment received from the one commenter.
Request to clarify proposed applicabilityPage 1
FedEx Express requests that we clarify the applicability statement in the NPRM to state that the AD does not apply to airplanes where auxiliary tanks were removed by an FAA-approved method. FedEx states that the unsafe condition does not exist on these airplanes.
We agree that the unsafe condition does not exist on the airplanes FedEx describes. We have included a statement in paragraph (c) of the final rule that excludes these airplanes.
Explanation of Change to Product Identification LinePage 1
We have changed the product identification line of the AD from “Various Transport Category Airplanes” to “Southeast Aero-Tek, Inc.” In ADs written against products with an STC, that statement is intended to identify the name of the STC holder.
ConclusionPage 1
We reviewed the relevant data, considered the comment received, and determined that air safety and the public interest require adopting the AD with the changes described previously. We also determined that these changes will not increase the economic burden on any operator or increase the scope of the AD.
Costs of CompliancePage 1
The following table provides the estimated costs for the 37 U.S.-registered airplanes to comply with this AD. Based on these figures, the estimated costs for U.S. operators could be as high as $239,760 to prepare and report the deactivation procedures, and $133,200 to deactivate tanks.
| Action | Work hours | Average labor rate per hour | Parts | Individual cost |
|---|---|---|---|---|
| Report | 1 | $80 | None | $80, per STC. |
| Preparation of tank deactivation procedure | 80 | 80 | None | $6,400, per STC. |
| Physical tank deactivation | 30 | 80 | $1,200 | $3,600, per airplane. |
Authority for This RulemakingPage 1
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 · 2
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 32
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1967 | 1 |
|---|---|
| 1969 | 2 |
| 1970 | 1 |
| 1971 | 1 |
| 1973 | 1 |
| 1975 | 2 |
| 1976 | 3 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 1 |
| 1981 | 5 |
| 1982 | 1 |
10 with no year recorded