AD 97-19-01

This amendment adopts a new airworthiness directive (AD), applicable to certain Saab Model SAAB 2000 series airplanes, that requires a one-time inspection of the hydraulic tubes and electrical harness wires of the wing rear access door for chafing, leakage, or wear damage; repair of any discrepancy found; and modification of the wing rear access door. This amendment is prompted by reports of interference between the wing rear access door and the hydraulic tubes and electrical harnesses, and chafing damage to the hydraulic tubes. The actions specified by this AD are intended to prevent such interference or chafing damage, which could lead to failure of the number 2 hydraulic system or loss of certain electrical and landing systems, and resultant reduced controllability of the airplane.

Final rule

97-19-01 SAAB AIRCRAFT AB: Amendment 39-10121. Docket 96-NM-220-AD.
Applicability: Model SAAB 2000 series airplanes, serial numbers -004 through -030 inclusive, certificated in any category.

NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (d) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance: Required as indicated, unless accomplished previously.

To prevent damage to the hydraulic tubes and electrical harnesses, which could lead to failure of the number 2 hydraulic system or loss of certain electrical and landing systems, and resultant reduced controllability of the airplane, accomplish the following:

(a) Within 60 days after the effective date of this AD, perform a one-time visual inspection of the hydraulic tubes and electrical harness wires of the wing rear access door for chafing, leakage, or wear damage; in accordance with paragraph B. of the Accomplishment Instructions of Saab Service Bulletin 2000-53-010, Revision 01, dated October 10, 1995.

(1) If any chafing or leakage of the hydraulic tubes is detected, prior to further flight, repair in accordance with a method approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate.

(2) If any damage to the metal braid or wire insulation is detected, prior to further flight, repair in accordance with paragraph E. of the Accomplishment Instructions of Saab Service Bulletin 2000-53-010, Revision 01, dated October 10, 1995.

(b) Within 60 days after the effective date of this AD, modify the wing rear access door and apply silicon tape to the electrical harnesses, in accordance with paragraph C. of the Accomplishment Instructions of Saab Service Bulletin 2000-53-010, Revision 01, dated October 10, 1995.

(c) As of the effective date of this AD, no person shall install wing rear access doors, part numbers 7353500-713/ -714 or 7353500-715/ -716, on any airplane, unless the part has been modified in accordance with Saab Service Bulletin 2000-53-010, Revision 01, dated October 10, 1995.

(d) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, whomay add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.

(e) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished.

(f) The inspection, modification, and certain repairs shall be done in accordance with Saab Service Bulletin 2000-53-010, Revision 01, dated October 10, 1995. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from SAAB Aircraft AB, SAAB Aircraft Product Support, S-581.88, Linkoping, Sweden. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(g) This amendment becomes effective on October 16, 1997.

A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an airworthiness directive (AD) that is applicable to certain Saab Model SAAB 2000 series airplanes was published in the Federal Register on June 24, 1997 (62 FR 34024). That action proposed to require a one-time visual inspection of the hydraulic tubes and electrical harness wires of the wing rear access door for chafing, leakage, or wear damage; repair of any discrepancy found; and modification of the wing rear access door.

Interested persons have been afforded an opportunity to participate in the making of this amendment. Due consideration has been given to the single comment received.

The commenter supports the proposed rule.

Conclusion
After careful review of the available data, including the comment noted above, the FAA has determined that air safety and the public interest require the adoption of the rule as proposed.

Cost Impact
The FAA estimates that 3 Saab Model SAAB 2000 series airplanes of U.S. registry will be affected by this AD, that it will take approximately 4 work hours per airplane to accomplish the required actions, and that the average labor rate is $60 per work hour. Required parts will be provided by the manufacturer at no cost to operators. Based on these figures, the cost impact of the AD on U.S. operators is estimated to be $720, or $240 per airplane.

The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted.

Regulatory Impact
The regulations adopted herein will not have substantial direct effects 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. Therefore, in accordance with Executive Order 12612, it is determined that this final rule does not have sufficient federalism implications to warrant the preparation of a Federalism Assessment.

For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action and it is contained in the Rules Docket. A copy of it may be obtained from the Rules Docket at the location provided under the caption "ADDRESSES."

List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.

Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by theAdministrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

PART 39 - AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.

39.13 - [Amended]
2. Section 39.13 is amended by adding the following new airworthiness directive: