Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes; Correction
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Issuing agencies
Abstract
The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to all MHI RJ Aviation ULC Model CL-600-2C10 (Regional Jet Series 700, 701 & 702) airplanes, Model CL-600-2C11 (Regional Jet Series 550) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and Model C-600-2E25 (Regional Jet Series 1000) airplanes. As published, a portion of the initial compliance time for doing the new ram-air valve task specified in the regulatory text for certain airplanes is incorrect. This document corrects that error. In all other respects, the original document remains the same.
Full Text
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<title>Federal Register, Volume 88 Issue 70 (Wednesday, April 12, 2023)</title>
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[Federal Register Volume 88, Number 70 (Wednesday, April 12, 2023)]
[Rules and Regulations]
[Pages 21900-21902]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2023-07588]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0679; Project Identifier MCAI-2021-01213-T;
Amendment 39-22392; AD 2023-06-06]
RIN 2120-AA64
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that was
published in the Federal Register. That AD applies to all MHI RJ
Aviation ULC Model CL-600-2C10 (Regional Jet Series 700, 701 & 702)
airplanes, Model CL-600-2C11 (Regional Jet Series 550) airplanes, Model
CL-600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24
(Regional Jet Series 900) airplanes, and Model C-600-2E25 (Regional Jet
Series 1000) airplanes. As published, a portion of the initial
compliance time for doing the new ram-air valve task specified in the
regulatory text for certain airplanes is incorrect. This document
corrects that error. In all other respects, the original document
remains the same.
DATES: This correction is effective April 28, 2023. The effective date
of AD 2023-06-06 remains April 28, 2023.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-0679; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule; correction, the mandatory continuing
airworthiness information (MCAI), any comments received, and other
information. The address for Docket Operations is U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Chirayu A. Gupta, Aerospace Engineer,
Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#7e47531f080d5310071f1d11531d110d3e181f1f50191108"><span class="__cf_email__" data-cfemail="eed7c38f989dc380978f8d81c38d819dae888f8fc0898198">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
AD 2023-06-06, Amendment 39-22392 (88 FR 17682, March 24, 2023) (AD
2023-06-06), requires revising the existing maintenance or inspection
program, as applicable, to incorporate two aircraft maintenance manual
(AMM) tasks. That AD applies to all MHI RJ Aviation ULC Model CL-600-
2C10 (Regional Jet Series 700, 701 & 702) airplanes, Model CL-600-2C11
(Regional Jet Series 550) airplanes, Model CL-600-2D15 (Regional Jet
Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900)
airplanes, and Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
Need for the Correction
As published, a portion of the initial compliance time specified in
paragraph (g)(1)(ii) of AD 2023-06-06 is incorrect. The initial
compliance time specified in paragraph (g)(1)(ii) of AD 2023-06-06 is
within 90 days after the effective date of this AD or before
accumulating 3,000 total flight hours, ``whichever occurs later.'' That
compliance time should be within 90 days after the effective date of
this AD or before accumulating 3,000 total flight hours, ``whichever
occurs first.'' This is the compliance time provided in Transport
Canada AD CF-2021-38R1, dated May 25, 2022, which the FAA intended to
match.
Correction of Publication
This document corrects an error and correctly adds the AD as an
amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, the FAA is publishing the
entire rule in the Federal Register.
The effective date of this AD remains April 28, 2023.
Since this action only corrects a certain compliance time, it has
no adverse economic impact and imposes no additional unforeseen burden
on any person. Therefore, the FAA has determined that notice and public
procedures are unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, pursuant to the authority delegated to me by the
Administrator,
[[Page 21901]]
the FAA amends part 39 of the Federal Aviation Regulations (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 [Corrected]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2023-06-06 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22392; Docket No. FAA-2022-0679;
Project Identifier MCAI-2021-01213-T.
(a) Effective Date
This airworthiness directive (AD) is effective April 28, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all MHI RJ Aviation ULC airplanes,
certificated in any category, identified in paragraphs (c)(1)
through (5) of this AD.
(1) Model CL-600-2C10 (Regional Jet Series 700, 701 & 702)
airplanes.
(2) Model CL-600-2C11 (Regional Jet Series 550) airplanes.
(3) Model CL-600-2D15 (Regional Jet Series 705) airplanes.
(4) Model CL-600-2D24 (Regional Jet Series 900) airplanes.
(5) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
(d) Subject
Air Transport Association (ATA) of America Code: 21, Air
conditioning.
(e) Reason
This AD was prompted by a determination that the existing
maintenance or inspection program, as applicable, must be revised to
incorporate two aircraft maintenance manual (AMM) tasks. The FAA is
issuing this AD to address in-service reports of emergency ram air
valve part number (P/N) GG670-95019-1 stuck in closed or partially
open positions, which, if not corrected could result in a complete
loss of outside air supply, leading to an increase in flight deck
and cabin temperatures and a possible increased level of
contaminated air (carbon monoxide, carbon dioxide, or ozone).
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision
(1) Within 90 days after the effective date of this AD, revise
the existing maintenance or inspection program, as applicable, to
incorporate the information specified in figure 1 to the
introductory text of paragraph (g)(1) of this AD. The initial
compliance time for doing the task is at the applicable time
specified in paragraph (g)(1)(i) or (ii) of this AD.
Figure 1 to the Introductory Text of Paragraph (g)(1)--AMM Task for the
Ram-Air Valve
BILLING CODE 4910-13-P
[GRAPHIC] [TIFF OMITTED] TR12AP23.024
(i) For airplanes that have accumulated less than 1,800 flight
hours since the last operational check of the ram air shutoff valve
was performed as specified in AMM Task 21-52-04-710-801-A01, and for
airplanes that have accumulated less than 1,800 flight hours from
the date of issuance of the original airworthiness certificate or
original export certificate of airworthiness: Within 90 days after
the effective date of this AD, or before accumulating 1,800 total
flight hours, whichever occurs later.
(ii) For airplanes that have accumulated 1,800 flight hours or
more since the last operational check of the ram air shutoff valve
was performed as specified in AMM Task 21-52-04-710-801-A01, and for
airplanes that have accumulated 1,800 flight hours or more since the
date of issuance of the original airworthiness certificate or
original export certificate of airworthiness and for which no
operational check of the valve has been performed: Within 90 days
after the effective date of this AD or before accumulating 3,000
total flight hours, whichever occurs first.
(2) Within 90 days after the effective date of this AD, revise
the existing maintenance or inspection program, as applicable, to
incorporate the information specified in figure 2 to the
introductory text of paragraph (g)(2) of this AD. The initial
compliance time for doing the task is at the applicable time
specified in paragraph (g)(2)(i) or (ii) of this AD.
[[Page 21902]]
Figure 2 to the Introductory Text of Paragraph (g)(2)--AMM Task for the
Pack Discharge and Ram-Air Supply Ducts
[GRAPHIC] [TIFF OMITTED] TR12AP23.025
BILLING CODE 4910-13-C
(i) For airplanes that have accumulated less than 17,600 flight
hours since the last detailed inspection of the pack discharge and
ram air supply ducts was performed as specified in AMM Task 21-51-
00-220-801-A01, and for airplanes that have accumulated less than
17,600 flight hours since the date of issuance of the original
airworthiness certificate or original export certificate of
airworthiness: Within 90 days after the effective date of this AD,
or before accumulating 17,600 total flight hours, whichever occurs
later.
(ii) For airplanes that have accumulated 17,600 flight hours or
more since the last detailed inspection of the pack discharge and
ram air supply ducts as specified in AMM Task 21-51-00-220-801-A01,
and for airplanes that have accumulated 17,600 flight hours or more
since the date of issuance of the original airworthiness certificate
or original export certificate of airworthiness, and for which no
detailed inspection of the pack discharge and ram air supply ducts
has been performed: Within 90 days after the effective date of this
AD.
(h) No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be used unless the
actions and intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (i)(1) of this AD.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO Branch, 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 responsible Flight Standards Office, as appropriate. If
sending information directly to the manager of the certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the responsible Flight
Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or Transport Canada; or MHI RJ Aviation ULC's Transport
Canada Design Approval Organization (DAO). If approved by the DAO,
the approval must include the DAO-authorized signature.
(j) Additional Information
(1) Refer to Transport Canada AD CF-2021-38R1, dated May 25,
2022, for related information. This Transport Canada AD may be found
in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-0679.
(2) For more information about this AD, contact Chirayu A.
Gupta, Aerospace Engineer, Airframe and Propulsion Section, FAA, New
York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email <a href="/cdn-cgi/l/email-protection#1a23377b6c693774637b7975377975695a7c7b7b347d756c"><span class="__cf_email__" data-cfemail="063f2b6770752b687f6765692b6569754660676728616970">[email protected]</span></a>.
(k) Material Incorporated by Reference
None.
Issued on April 6, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-07588 Filed 4-11-23; 8:45 am]
BILLING CODE 4910-13-P
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