[Federal Register Volume 63, Number 102 (Thursday, May 28, 1998)]
[Proposed Rules]
[Pages 29159-29161]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-14081]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97-CE-112-AD]
RIN 2120-AA64


Airworthiness Directives; Pilatus Britten-Norman Ltd. BN-2, BN-
2A, BN-2B, and BN-2T Series Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Supplemental notice of proposed rulemaking (NPRM); Reopening of 
the comment period.

-----------------------------------------------------------------------

SUMMARY: This document proposes to revise an earlier proposed 
airworthiness directive (AD) that would have required replacing the 
washers on the attachment bolts of the lower fitting of the main 
landing gear (MLG) on certain Pilatus Britten-Norman Ltd. (Pilatus 
Britten-Norman) BN-2, BN-2A, BN-2B, and BN-2T series airplanes. The 
proposed AD was the result of mandatory continuing airworthiness 
information (MCAI) issued by the airworthiness authority for the United 
Kingdom. The actions specified by the proposed AD are intended to 
prevent the bolts that attach the lower fitting of the MLG to the 
nacelle from becoming threadbound, which could result in structural 
failure of the MLG with consequent loss of control of the airplane 
during takeoff, taxi, or landing operations. Since issuing the NPRM, 
the Federal Aviation Administration (FAA) has realized that the Model 
BN-2T-4R airplanes were inadvertently omitted from the proposed AD. In 
addition, Pilatus Britten-Norman has revised the service information to 
include replacing the attachment bolts and nuts of the lower fitting of 
the MLG instead of re-using the existing bolts and nuts. This service 
information also adjusts the torque values of the nuts. The FAA has 
determined that the procedures included in the revised service 
information should be incorporated into the proposed AD, and that the 
comment period for the proposal should be reopened and the public 
should have additional time to comment.

DATES: Comments must be received on or before July 3, 1998.

ADDRESSES: Submit comments in triplicate to the FAA, Central Region, 
Office of the Regional Counsel, Attention: Rules Docket No. 97-CE-112-
AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. 
Comments may be inspected at this location between 8 a.m. and 4 p.m., 
Monday through Friday, holidays excepted.
    Service information that applies to the proposed AD may be obtained 
from Pilatus Britten-Norman Limited, Bembridge, Isle of Wight, United 
Kingdom PO35 5PR; telephone: 44-1983 872511; facsimile: 44-1983 873246. 
This information also may be examined at the Rules Docket at the 
address above.

FOR FURTHER INFORMATION CONTACT: Mr. Roger Chudy, Aerospace Engineer, 
Small Airplane Directorate, Aircraft Certification Service, 1201 
Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-
6932; facsimile: (816) 426-2169

SUPPLEMENTARY INFORMATION:

Comments Invited

    Interested persons are invited to participate in the making of the 
proposed rule by submitting such written data, views, or arguments as 
they may desire. Communications should identify the Rules Docket number 
and be submitted in triplicate to the address specified above. All 
communications received on or before the closing date for comments, 
specified above, will be considered before taking action on the 
proposed rule. The proposals contained in this supplemental notice may 
be changed in light of the comments received.
    Comments are specifically invited on the overall regulatory, 
economic, environmental, and energy aspects of the proposed rule. All 
comments submitted will be available, both before and after the closing 
date for comments, in the Rules Docket for examination by interested 
persons. A report that summarizes each FAA-public contact concerned 
with the substance of this proposal will be filed in the Rules Docket.
    Commenters wishing the FAA to acknowledge receipt of their comments 
submitted in response to this supplemental notice must submit a self-
addressed, stamped postcard on which the following statement is made: 
``Comments to Docket No. 97-CE-112-AD.'' The postcard will be date 
stamped and returned to the commenter.

Availability of Supplemental NPRM's

    Any person may obtain a copy of this supplemental NPRM by 
submitting a request to the FAA, Central Region, Office of the Regional 
Counsel, Attention: Rules Docket No. 97-CE-112-AD, Room 1558, 601 E. 
12th Street, Kansas City, Missouri 64106.

Discussion

    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 
Britten-Norman BN-2, BN-2A, BN-2B, and BN-2T series airplanes was 
published in the Federal Register as a notice of proposed rulemaking 
(NPRM) on March 19, 1998 (63 FR 13379). The NPRM proposed to require 
replacing the washers on the attachment bolts of the lower fitting of 
the MLG. Accomplishment of the proposed action as specified in the NPRM 
would be in accordance with Pilatus Britten-Norman Service Bulletin BN-
2/SB.231, Initial Issue, dated October 17, 1996.

[[Page 29160]]

    The NPRM was the result of mandatory continuing airworthiness 
information (MCAI) issued by the airworthiness authority for the United 
Kingdom.
    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.

Events Since Issuance of the NPRM

    Since issuance of the NPRM, Pilatus Britten-Norman has informed the 
FAA that Service Bulletin BN-2/SB.231 has been revised to the Issue 2 
status (dated October 1, 1997). This revision changes the procedures to 
specify replacing the attachment bolts and nuts of the lower fitting of 
the MLG instead of re-using the existing bolts and nuts. This service 
information also adjusts the torque loading values of the bolts.
    In addition, the FAA has realized that the Model BN-2T-4R airplanes 
were inadvertently omitted from the proposed AD. The Model BN-2T-4R 
airplanes are of similar type design to those currently listed in the 
NPRM.

The FAA's Determination

    After examining all information related to the subject described in 
this document, the FAA has determined that:

--The revised service information should be incorporated into the 
proposed AD;
--The unsafe condition could exist or develop on the Model BN-2T-4R 
airplanes and should be part of the applicability of the NPRM; and
--AD action should be taken to incorporate these changes to prevent the 
bolts that attach the lower fitting of the MLG to the nacelle from 
becoming threadbound, which could result in structural failure of the 
MLG with consequent loss of control of the airplane during takeoff, 
taxi, or landing operations.

The Supplemental NPRM

    Since replacing the attachment bolts and nuts of the lower fitting 
of the MLG, adjusting the torque values of these bolts, and adding the 
Model BN-2T-4R airplanes to the Applicability of the NPRM proposes 
actions that go beyond the scope of what was already proposed, the FAA 
is reopening the comment period to allow the public additional time to 
comment on this proposed action.

Cost Impact

    The FAA estimates that 80 airplanes in the U.S. registry would be 
affected by the proposed AD, that it would take approximately 3 
workhours per airplane to accomplish the proposed action, and that the 
average labor rate is approximately $60 an hour. Parts cost 
approximately $10 per airplane. Based on these figures, the total cost 
impact of the proposed AD on U.S. operators is estimated to be $15,200.

Regulatory Impact

    The regulations proposed herein would 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 
proposal would 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) if promulgated, 
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 draft regulatory evaluation 
prepared for this action has been placed 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, Safety.

The Proposed Amendment

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration proposes to amend 
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.

Sec. 39.13  [Amended]

    2. Section 39.13 is amended by adding a new airworthiness directive 
(AD) to read as follows:

Pilatus Britten-Norman Ltd: Docket No. 97-CE-112-AD. Applicability: 
Models BN-2, BN-2A, BN-2A-3, BN-2A-6, BN-2A-8, BN-2A-2, BN-2A-9, BN-
2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, 
BN-2B-27, BN-2T, and BN-2T-4R 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 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 50 landings after the 
effective date of this AD, unless already accomplished.

    Note 2: The compliance time of this AD is presented in landings 
instead of hours time-in-service (TIS). If the number of landings is 
unknown, hours TIS may be used by multiplying the number of hours 
TIS by 1.5.

    To prevent the bolts that attach the lower fitting of the main 
landing gear (MLG) to the nacelle from becoming threadbound, which 
could result in structural failure of the MLG with consequent loss 
of control of the airplane during takeoff, taxi, or landing 
operations, accomplish the following:
    (a) Replace the attachment bolts, nuts, and washers of the lower 
fitting of the MLG, in accordance with Pilatus Britten-Norman 
Service Bulletin No. BN-2/SB.231, Issue 2, dated October 1, 1997.
    (b) Special flight permits may be issued in accordance with 
Secs. 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, 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 3: 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 
Britten-Norman Service Bulletin BN-2/SB.231, Issue 2, dated October

[[Page 29161]]

1, 1997, should be directed to Pilatus Britten-Norman Limited, 
Bembridge, Isle of Wight, United Kingdom PO35 5PR; telephone: 44-
1983 872511; facsimile: 44-1983 873246. 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 64106.

    Note 4: The subject of this AD is addressed in British AD No. 
008-10-96, dated January 31, 1997.

    Issued in Kansas City, Missouri, on May 21, 1998.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 98-14081 Filed 5-27-98; 8:45 am]
BILLING CODE 4910-13-P