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Published 2013-02-01 · Federal Register document 2013-02074

Airworthiness Directives; EADS CASA (Type Certificate Previously Held by Construcciones Aeronáuticas, S.A.) Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for all EADS CASA (Type Certificate previously held by Construcciones Aeron[aacute]uticas, S.A.) Model CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes. This AD was prompted by reports of incorrect electrical polarity connections on engine fire extinguishing discharge cartridges. This AD requires a one-time inspection to identify the correct polarity for each pair of electrical connectors on each engine fire extinguisher cartridge, and repair if necessary. We are issuing this AD to detect and correct incorrect polarity connections, which could prevent the actuation of the discharge cartridge in case of automatic fire detection or manual initiation during a potential engine fire, and could result in damage to the airplane and injury to passengers.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2013-a7b684f4a1b4614e
Source row
results[36]
Raw source SHA-256
a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2013-02-12
Effective date printed in this edition
2013-03-08
Read 11 complete recorded clauses
Effective Date
(a) Effective Date

    This airworthiness directive (AD) becomes effective March 8, 
2013.

Exact source excerpt. Text positions 7792–7885, end exclusive, in the original decoded publication. SHA-256: 04ad66bbd7755ae8879d3b3e57ef3b79d3c4ffdf0594b179b6defa9ca4629404

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 7885–7914, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to all EADS CASA (Type Certificate previously 
held by Construcciones Aeron[aacute]uticas, S.A.) Model CN-235, CN-
235-100, CN-235-200, and CN-235-300 airplanes, certificated in any 
category, all serial numbers.

Exact source excerpt. Text positions 7914–8167, end exclusive, in the original decoded publication. SHA-256: 391dfd759e162d15edb4e57f3ae9be5f822546f3b7b5ac49852569a6b3a806ae

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire 
protection.

Exact source excerpt. Text positions 8167–8255, end exclusive, in the original decoded publication. SHA-256: d2a9cf8a8912242590075a047b779e20ffaf976cb7811f4525197162c9aaae16

Reason
(e) Reason

    This AD was prompted by reports of incorrect electrical polarity 
connections on engine fire extinguishing discharge cartridges. We 
are issuing this AD to detect and correct incorrect polarity 
connections, which could prevent the actuation of the discharge 
cartridge in case of automatic fire detection or manual initiation 
during a potential engine fire, and could result in damage to the 
airplane and injury to passengers.

Exact source excerpt. Text positions 8255–8702, end exclusive, in the original decoded publication. SHA-256: fb8e1b2d864e76ceb9cb4549bf3a55cb86302f98ebdf93f5960c3a3e09ba9ac4

Compliance
(f) Compliance

    You are responsible for having the actions required by this AD 
performed within the compliance times specified, unless the actions 
have already been done.

Exact source excerpt. Text positions 8702–8880, end exclusive, in the original decoded publication. SHA-256: af3956da952ca797ed39bc4b318e4356f7014ac5b4c12bda0147d37f1ffa6cb8

Inspection
(g) Inspection

    Within 30 days after the effective date of this AD, do a one-
time inspection to identify the correct polarity for each pair of 
electrical connectors on each engine fire extinguisher cartridge, in 
accordance with the Instructions of Airbus Military All Operator 
Letter 235-020, dated March 9, 2012.

Exact source excerpt. Text positions 8880–9203, end exclusive, in the original decoded publication. SHA-256: b772163075a5cffbe5849fb5a4a6881f949ef91ac3bcbb42e4d0833b9c5ef416

Corrective Action
(h) Corrective Action

    If, during the inspection required by paragraph (g) of this AD, 
erroneous wiring polarity is detected: Before further flight, repair 
in accordance with a method approved by the Manager, International 
Branch, ANM-116, Transport Airplane Directorate, FAA; or European 
Aviation Safety Agency (EASA) (or its delegated agent).

Exact source excerpt. Text positions 9203–9557, end exclusive, in the original decoded publication. SHA-256: 09c75c578264984580963b14b705194e1b2e2ebdd38a9e36d13306799ead0fb8

Other FAA AD Provisions
 (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: [email protected]. 
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) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.

Exact source excerpt. Text positions 9557–11014, end exclusive, in the original decoded publication. SHA-256: 3e1021a5403e4708808a1a4589c94c786ac2d0339800eb7ff324844003432685

Related Information
(j) Related Information

    Refer to MCAI EASA Airworthiness Directive 2012-0045, dated 
March 21, 2012, and Airbus Military All Operator Letter 235-020, 
dated March 9, 2012, for related information.

Exact source excerpt. Text positions 11014–11217, end exclusive, in the original decoded publication. SHA-256: 75b734d2a02553b96710ac27f2fd071f1b94a67bf0c6c0ef94a526566f1e260f

Material Incorporated by Reference
(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Airbus Military All Operator Letter 235-020, dated March 9, 
2012.
    (ii) Reserved.
    (3) For service information identified in this AD, contact EADS-
CASA, Military Transport Aircraft Division (MTAD), Integrated 
Customer Services (ICS), Technical Services, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 55 05; email [email protected]; 
Internet http://www.eads.net.
    (4) You may review copies of the 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.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 11217–12530, end exclusive, in the original decoded publication. SHA-256: dbf1d97e1e89658d34890ffdb75a3aed8ef55e1b404774fbd12a270e1e0b4736

No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.

Find all recorded historical references to AD 2013-02-12 · 1 printed reference observations in this pinned collection.

These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.

Why these observations are shown

They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.

Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 0f5b5a23897b2729b7e24974fd02bcf62e6d2c14f5e23798758f3a6b8171b568. Source manifest: 2ae4d7e62042b37922c1f60cd2472190ea8f56b0014a7e3614a3a869db5e4398.

Official source · 2013-02-01

Publication text

This is the complete recorded text of this dated publication.

Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.

Read the complete official publication text
[Federal Register Volume 78, Number 22 (Friday, February 1, 2013)]
[Rules and Regulations]
[Pages 7262-7264]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-02074]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-1102; Directorate Identifier 2012-NM-062-AD; 
Amendment 39-17333; AD 2013-02-12]
RIN 2120-AA64


Airworthiness Directives; EADS CASA (Type Certificate Previously 
Held by Construcciones Aeron[aacute]uticas, S.A.) Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

[[Page 7263]]


ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for all 
EADS CASA (Type Certificate previously held by Construcciones 
Aeron[aacute]uticas, S.A.) Model CN-235, CN-235-100, CN-235-200, and 
CN-235-300 airplanes. This AD was prompted by reports of incorrect 
electrical polarity connections on engine fire extinguishing discharge 
cartridges. This AD requires a one-time inspection to identify the 
correct polarity for each pair of electrical connectors on each engine 
fire extinguisher cartridge, and repair if necessary. We are issuing 
this AD to detect and correct incorrect polarity connections, which 
could prevent the actuation of the discharge cartridge in case of 
automatic fire detection or manual initiation during a potential engine 
fire, and could result in damage to the airplane and injury to 
passengers.

DATES: This AD becomes effective March 8, 2013.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of March 8, 
2013.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC.

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: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on October 18, 2012 (77 
FR 64053). That NPRM proposed to correct an unsafe condition for the 
specified products. The Mandatory Continuing Airworthiness Information 
(MCAI) states:

    Reports have been received of finding wrong electrical polarity 
connections of engine fire extinguishing discharge cartridges on 
CASA CN-235 aeroplanes. The results of the subsequent investigation 
showed that the incorrect discharge cartridge assembly was caused by 
production line errors.
    This condition, if not detected and corrected, could prevent the 
actuation of the discharge cartridge in case of automatic fire 
detection or manual initiation in case of engine fire, possibly 
resulting in damage to the aeroplane and injury to occupants.
    To address this potential unsafe condition, EADS CASA (Airbus 
Military) developed instructions to identify erroneous wiring 
polarity installation.
    For the reasons described above this [European Aviation Safety 
Agency] AD requires a one-time inspection to verify proper 
electrical polarity of wiring of each engine fire extinguisher 
discharge cartridge and, depending on findings, corrective action 
[accomplish the repair].

You may obtain further information by examining the MCAI in the AD 
docket.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (77 FR 64053, October 18, 
2012) or on the determination of the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD as proposed.

Costs of Compliance

    We estimate that this AD will affect 6 products of U.S. registry. 
We also estimate that it will take about 4 work-hours per product to 
comply with the basic requirements of this AD. The average labor rate 
is $85 per work-hour. Based on these figures, we estimate the cost of 
this AD to the U.S. operators to be $2,040, or $340 per product.
    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this 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 AD will not have federalism implications 
under Executive Order 13132. This AD will 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 that this AD:
    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.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this AD and placed it in the AD docket.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains the NPRM (77 FR 64053, October 18, 
2012), 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.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 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 AD:

2013-02-12 EADS CASA (Type Certificate previously held by 
Construcciones Aeron[aacute]uticas, S.A.): Amendment 39-

[[Page 7264]]

17333. Docket No. FAA-2012-1102; Directorate Identifier 2012-NM-062-
AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective March 8, 
2013.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all EADS CASA (Type Certificate previously 
held by Construcciones Aeron[aacute]uticas, S.A.) Model CN-235, CN-
235-100, CN-235-200, and CN-235-300 airplanes, certificated in any 
category, all serial numbers.

(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire 
protection.

(e) Reason

    This AD was prompted by reports of incorrect electrical polarity 
connections on engine fire extinguishing discharge cartridges. We 
are issuing this AD to detect and correct incorrect polarity 
connections, which could prevent the actuation of the discharge 
cartridge in case of automatic fire detection or manual initiation 
during a potential engine fire, and could result in damage to the 
airplane and injury to passengers.

(f) Compliance

    You are responsible for having the actions required by this AD 
performed within the compliance times specified, unless the actions 
have already been done.

(g) Inspection

    Within 30 days after the effective date of this AD, do a one-
time inspection to identify the correct polarity for each pair of 
electrical connectors on each engine fire extinguisher cartridge, in 
accordance with the Instructions of Airbus Military All Operator 
Letter 235-020, dated March 9, 2012.

(h) Corrective Action

    If, during the inspection required by paragraph (g) of this AD, 
erroneous wiring polarity is detected: Before further flight, repair 
in accordance with a method approved by the Manager, International 
Branch, ANM-116, Transport Airplane Directorate, FAA; or European 
Aviation Safety Agency (EASA) (or its delegated agent).

 (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: [email protected]. 
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) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.

(j) Related Information

    Refer to MCAI EASA Airworthiness Directive 2012-0045, dated 
March 21, 2012, and Airbus Military All Operator Letter 235-020, 
dated March 9, 2012, for related information.

(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (i) Airbus Military All Operator Letter 235-020, dated March 9, 
2012.
    (ii) Reserved.
    (3) For service information identified in this AD, contact EADS-
CASA, Military Transport Aircraft Division (MTAD), Integrated 
Customer Services (ICS), Technical Services, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 55 05; email [email protected]; 
Internet http://www.eads.net.
    (4) You may review copies of the 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.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Renton, Washington, on January 23, 2013.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2013-02074 Filed 1-31-13; 8:45 am]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:57:19.646507+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
a7af0f988baadb06c716943aa453e0437c1405083c9b5c566db2001d085ce438
Text SHA-256
0f5b5a23897b2729b7e24974fd02bcf62e6d2c14f5e23798758f3a6b8171b568

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Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.