AD 98-08-26

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AD Number:
98-08-26
Document Type:
AD Final Rules
Docket Number:
97-CE-46-AD
Subject Heading:
Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes.
Subject:
Fuel Tank Underwing Access Panels
Status:
Current
Citation:
Federal Register: April 20, 1998 (Volume 63, Number 75)
Citation Publish Date:
04/20/1998
Effective Date:
05/29/1998
Make:
Pilatus Aircraft Limited
Model:
PC-12 | PC-12/45
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39 [63 FR 19390 No. 75 04/20/98]
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 98-08-26
CITATION:   [Federal Register: April 20, 1998 (Volume 63, Number 75)]

PAGE NUMBER:   [Page 19390]

DOCKET NUMBER:   97-CE-46-AD

AMENDMENT:   39-10475

AD NUMBER:   98-08-26

SUBJECT HEADING:   Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes.

ACTION:   Final rule.

SUMMARY:   This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD requires installing aluminum bonding bushings over certain screws in certain fuel tank underwing access panels. Several reports from the field revealing fuel tank access panels insufficiently electrically bonded to the airframe prompted this action. The actions specified by this AD are intended to prevent electrical arcing in the fuel tanks and detonation of the fuel-air mixture, which can be created by poor electrical bonding of fuel tank underwing access panels, and could result in a fire on the airplane.

DATES:   Effective May 29, 1998. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of May 29, 1998.

ADDRESSES:   Service information that applies to this AD may be obtained from Pilatus Aircraft Ltd., CH-6370 Stans, Switzerland; telephone: +41-41-6196-233; facsimile: +41-41-6103-351. This information may also be examined at the Federal Aviation Administration (FAA), Central Region, Office of the Regional.

Counsel, Attention: Rules Docket No. 97-CE-46-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106; or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC.


FOR FURTHER INFORMATION CONTACT:   Mr. Roman Gabrys, Project Officer, FAA, Small Airplane Directorate, Aircraft Certification Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-6934; facsimile: (816) 426-2169.


SUPPLEMENTARY INFORMATION:  
Events Leading to the Issuance of This AD
A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain Pilatus Models PC-12 and PC-12/45 airplanes was published in the Federal Register as a notice of proposed rulemaking (NPRM) on December 19, 1997 (62 FR 66561). The NPRM proposed to require installing aluminum bonding bushings over certain screws in certain fuel tank underwing access panels. Accomplishment of the proposed action as specified in the NPRM would be in accordance with Pilatus Service Bulletin No. 57-001, dated February 28, 1997.

The NPRM was the result of several reports from the field revealing fuel tank access panels insufficiently electrically bonded to the airframe.
Interested persons have been afforded an opportunity to participate in the making of this amendment. No comments were received on the proposed rule or the FAA's determination of the cost to the public.

The FAA's Determination
After careful review of all available information related to the subject presented above, the FAA has determined that air safety and the public interest require the adoption of the rule as proposed except for minor editorial corrections. The FAA has determined that these minor corrections will not change the meaning of the AD and will not add any additional burden upon the public than was already proposed.

Cost Impact
The FAA estimates that 40 airplanes in the U.S. registry will be affected by this AD, that it will take approximately 6 workhours per airplane to accomplish this action, and that the average labor rate is approximately $60 an hour. Parts will be provided at no cost by the manufacturer. Based on these figures, the total cost impact of this AD on U.S. operators is estimated to be $14,400 or $360 per airplane.

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 copy of the final evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting 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 the Administrator, 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 a new airworthiness directive (AD) to read as follows:

REGULATORY TEXT:  
98-08-26 PILATUS AIRCRAFT LTD.: Amendment 39-10475; Docket No. 97-CE-46-AD.

Applicability: Model PC-12 and PC-12/45 airplanes, serial numbers MSN 001 through MSN 168, certificated in any category.

NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been 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 (c) 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 within the next 100 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished.

To prevent electrical arcing in the fuel tanks and detonation of the fuel-air mixture, which can be created by poor electrical bonding of fuel tank underwing access panels, and could result in a fire on the airplane, accomplish the following:

(a) Install aluminum bonding bushings onto the screws for certain fuel tank underwing access panels in accordance with Part A and Part B of the Accomplishment Instructions in Pilatus Service Bulletin No. 57-001, dated February 28, 1997.

(b) 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.

(c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Small Airplane Directorate, Aircraft Certification Service, 1201 Walnut, suite 900, Kansas City, Missouri 64106. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Small Airplane Directorate.

NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Small Airplane Directorate.

(d) Questions or technical information related to Pilatus Service Bulletin No. 57-001, dated February 28, 1997, should be directed to Pilatus Aircraft Ltd., CH-6370 Stans, Switzerland. This service information may be examined at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri.

(e) The installations required by this AD shall be done in accordance with Pilatus Service Bulletin No. 57-001, dated February 28, 1997. 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 Pilatus Aircraft Ltd., CH-6370 Stans, Switzerland. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC.

(f) This amendment becomes effective on May 29, 1998.


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