AD 95-15-13

This amendment adopts a new airworthiness directive (AD) that applies to Jetstream Aircraft Limited (JAL) Jetstream Models 3101 and 3201 airplanes. This action requires inspecting the main passenger/crew door locking mechanism to ensure that a taper pin is installed, installing a taper pin if not already installed, and modifying the passenger door warning system. The actions specified by this AD are intended to prevent the inability to open the passenger/crew door or failure of the passenger door warning system, which could result in passenger injury if emergency evacuation is needed.

Final rule

95-15-13 JETSTREAM AIRCRAFT LIMITED: Amendment 39-9319; Docket No. 92-CE-23-AD.
Applicability: Jetstream Models 3101 and 3201 airplanes (all serial numbers), 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 use the authority provided in paragraph (d) of this AD to request approval from the FAA. This approval may address either no action, if the current configuration eliminates the unsafe condition, or different actions necessary to address the unsafe condition described in this AD. Such a request should include an assessment of the effect of the changed configuration on the unsafe condition addressed by this AD. In no case does thepresence of any modification, alteration, or repair remove any airplane from the applicability of this AD.

Compliance: Required within the next 500 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent the inability to open the passenger/crew door or failure of the passenger door warning system, which could result in passenger injury if emergency evacuation is needed, accomplish the following:

(a) For all affected airplanes that have a main passenger/crew door installed with one of the following serial numbers, accomplish paragraphs (a)(1) and (a)(2) of this AD, as applicable:

WIPL-SD-0001 through WIPL-SD-0005,

WIPL-SD-0008 through WIPL-SD-0031,

WIPL-SD-0034 through WIPL-SD-0046,

WIPL-SD-0049, WIPL-SD-0051 through WIPL-SD-0065,

WIPL-SD-0067, WIPL-SD-0070, WIPL-SD-0071,

SDJ10883, SDJ10884A, SDJ10884B, and SDJ10886 through SDJ10891

(1) To ensure that a part number SP28E4 taper pin is installed, visually inspect the passenger/crew door locking mechanism in the area between the locking dog and indicator button assembly in accordance with Part 2 of the ACCOMPLISHMENT INSTRUCTIONS section of Jetstream Service Bulletin (SB) 52-A-JA 911140, which incorporates the following pages:

Pages
Revision Level
Date
4, 5, 7, and 9
Original Issue
February 3, 1992
2
Revision 1
June 26, 1992
1, 3, 6, and 8
Revision 2
October 6, 1992

(2) If a taper pin (part number SP28E4) is not installed, prior to further flight, accomplish Part 3 of the ACCOMPLISHMENT INSTRUCTIONS section of Jetstream SB 52-A-JA 911140.

(b) For all affected airplanes regardless of the serial number passenger door installed, modify the passenger door warning system in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Jetstream SB 52-JM 7793, which incorporates the following pages:

Pages
Revision Level
Date
4 through 11
Original Issue
November 19, 1992
1, 2, and 3
Revision 1
August10, 1993

NOTE 2: Compliance with a previous revision level of the service bulletins referenced in this AD fulfills the applicable requirements of this AD and is considered "unless already accomplished" for that portion of the AD.

(c) 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.

(d) An alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Brussels Aircraft Certification Office (ACO), FAA, Europe, Africa, and Middle East Office, c/o American Embassy, B-1000 Brussels, Belgium. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Brussels ACO.

NOTE 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Brussels ACO.

(e) The inspection and possible installation required by this AD shall be done in accordance with Jetstream Service Bulletin 52-A-JA 911140, which incorporates the following pages:

Pages
Revision Level
Date
4, 5, 7, and 9
Original Issue
February 3, 1992
2
Revision 1
June 26, 1992
1, 3, 6, and 8
Revision 2
October 6, 1992

The modification required by this AD shall be done in accordance with Jetstream Service Bulletin 52-JM 7793, which incorporates the following pages:

Pages
Revision Level
Date
4 through 11
Original Issue
November 19, 1992
1, 2, and 3
Revision 1
August 10, 1993

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 Jetstream Aircraft Limited, Manager Product Support, Prestwick Airport, Ayrshire, KA9 2RW Scotland; or Jetstream Aircraft Inc., Librarian, P.O. Box 16029, Dulles International Airport, Washington, DC, 20041-6029. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief 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 September 7, 1995.

A proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain JAL Models 3101 and 3201 airplanes was published in the Federal Register on February 22, 1995 (60 FR 9794). The action proposed to require inspecting the main passenger/crew door locking mechanism to ensure that a taper pin is installed, installing a taper pin if not already installed, and modifying the passenger door warning system. Accomplishment of the proposed inspection and possible installation would be in accordance with Jetstream Service Bulletin (SB) 52-A-JA 911140, which incorporates the following pages:

Pages
Revision Level
Date
4, 5, 7, and 9
Original Issue
February 3, 1992
2
Revision 1
June 26, 1992
1, 3, 6, and 8
Revision 2
October 6, 1992

Accomplishment of the proposed door warning system modification would be in accordance with Jetstream SB 52-JM 7793, which incorporates the following pages:Pages
Revision Level
Date
4 through 11
Original Issue
November 19, 1992
1, 2, and 3
Revision 1
August 10, 1993

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.

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.

The FAA estimates that 200 airplanes in the U.S. registry will be affected by this AD, that it will take approximately 10 workhours (2 workhours for the taper pin installation and 8 workhours for the passenger door warning system modification) per airplane to accomplish the required action, and that the average labor rate is approximately $60 an hour. Parts to accomplish the modifications will be provided by JAL at no cost to the owner/operator. Based on these figures, the total cost impact of this AD on U.S. operators is estimated to be $120,000. This figure is based on the assumption that no affected owner/operator has accomplished either of the modifications; that all airplanes will need a taper pin installed on the passenger/crew door locking mechanism; and that no airplane owner/operator has accomplished the passenger door warning system modification. The FAA anticipates that a majority of the affected airplanes already have taper pins installed and passenger door warning system modifications incorporated, thereby reducing the cost impact upon the public.

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 thedistribution 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. App. 1354(a), 1421 and 1423; 49 U.S.C. 106(g); and 14 CFR 11.89.

Section 39.13 - [AMENDED]
2. Section 39.13 is amended by adding a new AD to read as follows: