preamble attached >>> |
ADs updated daily at www.Tdata.com
|
2024-08-04 |
DE HAVILLAND AIRCRAFT OF CANADA LIMITED (TYPE CERTIFICATE
PREVIOUSLY HELD BY BOMBARDIER, INC.): Amendment 39-22737; Docket No. FAA-2023-2137; Project Identifier MCAI-2022-01389-T. |
(a) EFFECTIVE DATE
This airworthiness directive (AD) is effective June 20, 2024.
(b) AFFECTED ADS
None.
(c) APPLICABILITY
This AD applies to all De Havilland Aircraft of Canada Limited Model
DHC-8-401 and -402 airplanes, certificated in any category.
(d) SUBJECT
Air Transport Association (ATA) of America Code 05, Time Limits/Main-
tenance Checks.
(e) REASON
This AD was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The FAA is issuing this AD to
address new or more restrictive maintenance interval limitations.
Failure to adhere to the specified interval limitations may result in
reduced structural integrity of the airplane.
(f) COMPLIANCE
Comply with this AD within the compliance times specified, unless al-
ready done.
(g) MAINTENANCE OR INSPECTION PROGRAM REVISION
Within 60 days after the effective date of this AD, revise the exist-
ing maintenance or inspection program, as applicable, to incorporate
the information specified in figure 1 to paragraph (g) of this AD. The
initial compliance time for each task in the AMM Task column of figure
1 to paragraph (g) of this AD is at the time specified in the initial
compliance time column of figure 1 to paragraph (g) of this AD or
within 12 months after the effective date of this AD, whichever occurs
later.
______________________________________________________________________
FIGURE 1 TO PARAGRAPH (G) – MAINTENANCE OR INSPECTION PROGRAM REVISION
______________________________________________________________________
EFFECTIVITY INITIAL COMPLIANCE TIME INTERVAL AMM TASK
LIMITATION
______________________________________________________________________
All 10,000 total flight 10,000 FH 21-31-00-710-801
hours (FH)
All 20,000 total FH 20,000 FH 21-31-00-710-803
All 20,000 total FH 20,000 FH 21-31-00-710-804
All 35,000 total FH 35,000 FH 22-11-00-720-803
All 30,000 total FH 30,000 FH 26-20-00-900-801
All 30,000 total FH 30,000 FH 26-20-00-900-802
All 30,000 total FH 30,000 FH 26-20-00-900-805
All 30,000 total FH 30,000 FH 26-20-00-900-807
All 30,000 total FH 30,000 FH 26-20-00-900-803
All 30,000 total FH 30,000 FH 26-20-00-900-804
All 20,000 total FH 20,000 FH 26-20-00-710-801
All 20,000 total FH 20,000 FH 28-21-00-710-801
All 10,000 total FH 10,000 FH 29-12-00-720-803
All 4,950 total FH 4,950 FH 29-12-00-720-805
All 4,950 total FH 4,950 FH 29-12-00-720-802
All 4,950 total FH 4,950 FH 29-12-00-720-804
All 30,000 total FH 30,000 FH 30-11-00-710-802
All 5,280 total FH 5,280 FH 31-41-00-710-802
All 1,760 total FH 1,760 FH 32-11-00-210-802
All 30,000 total FH 30,000 FH 52-24-00-210-802
All 4,400 total FH 4,400 FH 61-20-00-710-802
All 150 total FH 150 FH 77-31-00-710-803
______________________________________________________________________
(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 or 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, International
Validation 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 International Validation Branch,
send it to the attention of the person identified in paragraph (j)(2)
of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
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, International
Validation Branch, FAA; or Transport Canada; or De Havilland Aircraft
of Canada Limited'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-2022-59, dated October 27, 2022, for
related information. This Transport Canada AD may be found in the AD
docket at regulations.gov under Docket No. FAA-2023-2137.
(2) For more information about this AD, contact Fatin Saumik, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone: 516-228-7300; email: 9-avs-nyaco-cos@faa.gov.
(k) MATERIAL INCORPORATED BY REFERENCE
None.
Issued on April 17, 2024. Victor Wicklund, Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.
FOR FURTHER INFORMATION CONTACT: Fatin Saumik, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-
228-7300; email: 9-avs-nyaco-cos@faa.gov.
PREAMBLE |
|
DEPARTMENT OF TRANSPORTATION |