
[Federal Register Volume 81, Number 93 (Friday, May 13, 2016)]
[Proposed Rules]
[Pages 29807-29809]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-11171]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-6668; Directorate Identifier 2014-NM-149-AD]
RIN 2120-AA64


Airworthiness Directives; Saab AB, Saab Aeronautics (Type 
Certificate Previously Held by Saab AB, Saab Aerosystems) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Saab AB, Saab Aeronautics Model SAAB 2000 airplanes. This 
proposed AD was prompted by a report that on some airplanes, during the 
paint removal process for repainting the airplane, the basic corrosion 
protection (anodizing and primer) coating was sanded down to bare metal 
on the aluminum skin panels and the bare metal might not have been 
treated correctly for corrosion prevention. This proposed AD would 
require an inspection of structural components of the airplane for any 
damaged protective coating; inspections of those areas for pitting 
corrosion, if necessary; a thickness measurement to determine if there 
is reduced skin thickness, if necessary; and repair, if necessary. We 
are proposing this AD to detect and correct damaged protective 
coatings. This condition could result in pitting corrosion damage; and 
reduced metal thickness, which could result in reduced static and 
fatigue strength of the airplane's structural parts.

DATES: We must receive comments on this proposed AD by June 27, 2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this NPRM, contact Saab AB, 
Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; telephone +46 13 
18 5591; fax +46 13 18 4874; email saab2000.techsupport@saabgroup.com; 
Internet http://www.saabgroup.com. You may view this referenced service 
information at the FAA, Transport Airplane Directorate, 1601 Lind 
Avenue SW., Renton, WA. For information on the availability of this 
material at the FAA, call 425-227-1221.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
6668; or in person at the Docket Management Facility between 9 a.m. and 
5 p.m., Monday through Friday, except Federal holidays. The AD docket 
contains this proposed AD, the regulatory evaluation, any comments 
received, and other information. The street address for the Docket 
Operations office (telephone 800-647-5527) is in the ADDRESSES section. 
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace 
Engineer, International Branch, ANM-116, Transport Airplane 
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; 
telephone 425-227-1112; fax 425-227-1149.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2016-6668; 
Directorate Identifier 2014-NM-149-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD based on those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA 
Airworthiness Directive 2014-0160, dated July 9, 2014 (Correction: July 
9, 2014) (referred to after this as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for certain Saab AB, Saab Aeronautics Model SAAB 2000 
airplanes. The MCAI states:

    SAAB received evidence that on a number of SAAB 2000 aeroplanes, 
during paint removal before repainting, the basic corrosion 
protection anodizing and primer were removed. In these cases, the 
basic corrosion protection coating was sanded down to bare metal on 
the aluminium [aluminum] skin panel in spite of existing 
instruction(s) contained in the Structural Repair Manual (SRM) which 
prohibit(s) exposing the aluminium bare metal. Due to the fact that 
the skin panels are manufactured from aluminium without a protective 
covering (unclad), the anodizing and primer is the corner stone of 
the aeroplane corrosion protection system. If the anodizing and 
primer is removed and the aluminium surface is not correctly 
treated, pitting corrosion may occur. In addition, sanding to bare 
metal can inadvertently lead to metal removal and subsequently 
reduce the static and fatigue strength of the aeroplane structural 
parts.
    This condition, if not detected and corrected, could result in 
corrosion damage and/or reduced structural strength of the aeroplane 
structure.
    To address this potential unsafe condition, SAAB issued SB 2000-
51-002 to provide inspection instructions.
    For the reasons described above, this [EASA] AD requires a one-
time [detailed] inspection [for damage] * * * of required 
anticorrosion protective coating [e.g., bonding primer], [detailed] 
inspection for

[[Page 29808]]

pitting corrosion (if necessary) [, a dye penetrant inspection for 
pitting corrosion (if necessary)] and measure the skin thickness (if 
necessary) [to determine if there is reduced skin thickness] and, 
depending on findings, corrective action(s) [e.g., repair].
    This [EASA] AD is re-issued to correct typographical error of 
the effective date.

    You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
6668.

Relevant Service Information Under 1 CFR Part 51

    Saab has issued Service Bulletin 2000-51-002, Revision 01, dated 
May 23, 2014. This service information describes procedures for an 
inspection of structural components of the airplane for any damaged 
protective coating; inspections of those areas for pitting corrosion; a 
thickness measurement to determine if there is reduced skin thickness; 
and repair. This service information is reasonably available because 
the interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information referenced above. We are proposing this AD because we 
evaluated all pertinent information and determined an unsafe condition 
exists and is likely to exist or develop on other products of the same 
type design.

Costs of Compliance

    We estimate that this proposed AD affects 8 airplanes of U.S. 
registry.
    We also estimate that it would take about 20 work-hours per product 
to comply with the basic requirements of this proposed AD. The average 
labor rate is $85 per work-hour. Based on these figures, we estimate 
the cost of this proposed AD on U.S. operators to be $13,600, or $1,700 
per product.
    In addition, we estimate that any necessary follow-on actions would 
take about 45 work-hours, for a cost of $3,825 per product. We have no 
way of determining the number of aircraft that might need these 
actions. We have received no definitive data that would enable us to 
provide cost estimates for the parts cost of the follow-on actions 
specified in this proposed AD.

Authority for This Rulemaking

    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 Findings

    We determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    3. Will not affect intrastate aviation in Alaska; and
    4. 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.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

Saab AB, Saab Aeronautics (Type Certificate previously held by Saab 
AB, Saab Aerosystems): Docket No. FAA-2016-6668; Directorate 
Identifier 2014-NM-149-AD.

(a) Comments Due Date

    We must receive comments by June 27, 2016.

 (b) Affected ADs

    None.

 (c) Applicability

    This AD applies to Saab AB, Saab Aeronautics (Type Certificate 
previously held by Saab AB, Saab Aerosystems) Model SAAB 2000 
airplanes, certificated in any category, all manufacturer serial 
numbers, except as specified in paragraphs (c)(1) and (c)(2) of this 
AD.
    (1) Those airplanes identified in Table 1 of Saab Service 
Bulletin 2000-51-002, Revision 01, dated May 23, 2014, on which an 
applicable ``Related Statement'' identified in Table 1 was 
accomplished.
    (2) Those airplanes that either have retained the original paint 
or have been repainted by Saab AB, Saab Aeronautics.

 (d) Subject

    Air Transport Association (ATA) of America Code 51, Standard 
Practices/Structures.

 (e) Reason

    This AD was prompted by a report that on some airplanes, during 
the paint removal process for repainting the airplane, the basic 
corrosion protection (anodizing and primer) coating was sanded down 
to bare metal on the aluminum skin panels and the bare metal might 
not have been treated correctly for corrosion prevention. We are 
issuing this AD to detect and correct damaged protective coatings. 
This condition could result in pitting corrosion damage; and reduced 
metal thickness, which could result in reduced static and fatigue 
strength of the airplane's structural parts.

 (f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

 (g) Inspection, Related Investigative Actions, and Corrective Action

    (1) Within 2,000 flight hours or 12 months, whichever occurs 
first after the effective date of this AD, do a detailed inspection 
of the airplane structural parts to detect damaged protective 
coating (e.g., bonding primer), in accordance with the 
Accomplishment Instructions of Saab Service Bulletin 2000-51-002, 
Revision 01, dated May 23, 2014. If any damaged protective coating 
is found, before further flight, do a detailed inspection of the 
airplane structural parts to detect pitting corrosion and, if no 
pitting corrosion is found, do a dye penetrant inspection of the 
airplane structural parts to detect pitting

[[Page 29809]]

corrosion and a thickness measurement to determine if there is 
reduced skin thickness, as applicable, in accordance with the 
Accomplishment Instructions of Saab Service Bulletin 2000-51-002, 
Revision 01, dated May 23, 2014.
    (2) If, during any inspection required by paragraph (g)(1) of 
this AD, any damage (such as pitting corrosion or damaged primer) or 
reduced skin thickness is detected, as defined in Saab Service 
Bulletin 2000-51-002, Revision 01, dated May 23, 2014, before 
further flight, contact the Manager, International Branch, ANM-116, 
Transport Airplane Directorate, FAA; or the European Aviation Safety 
Agency (EASA); or Saab AB, Saab Aeronautics' EASA Design 
Organization Approval (DOA) for a repair method, and do the repair 
within the compliance time indicated in those instructions.

 (h) Credit for Previous Actions

    This paragraph provides credit for actions required by paragraph 
(g) of this AD, if those actions were performed before the effective 
date of this AD using Saab Service Bulletin 2000-51-002, dated April 
9, 2014, which is not incorporated by reference in this AD.

 (i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. In accordance with 14 CFR 
39.19, send your request to your principal inspector or local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Branch, send it to ATTN: Shahram 
Daneshmandi, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, 
WA 98057-3356; telephone 425-227-1112; fax 425-227-1149. Information 
may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any 
approved AMOC, notify your appropriate principal inspector, or 
lacking a principal inspector, the manager of the local flight 
standards district office/certificate holding district office. The 
AMOC approval letter must specifically reference this AD.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Branch, ANM-116, Transport Airplane Directorate, FAA; or the 
European Aviation Safety Agency (EASA); or Saab AB, Saab 
Aeronautics' EASA Design Organization Approval (DOA). If approved by 
the DOA, the approval must include the DOA-authorized signature.

 (j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2014-0160, dated July 9, 2014 
(Correction: July 9, 2014), for related information. This MCAI may 
be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-
2016-6668.
    (2) For service information identified in this AD, contact Saab 
AB, Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; telephone 
+46 13 18 5591; fax +46 13 18 4874; email 
saab2000.techsupport@saabgroup.com; Internet http://www.saabgroup.com. You may view this service information at the FAA, 
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. 
For information on the availability of this material at the FAA, 
call 425-227-1221.

    Issued in Renton, Washington, on May 4, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-11171 Filed 5-12-16; 8:45 am]
 BILLING CODE 4910-13-P


