AD 2017-08-11

Airworthiness directive · Engine · Rolls-Royce RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17 and 4 more

Effective
May 30, 2017
Published
April 24, 2017 · 82 FR 18843–18845
Issued
April 13, 2017
Supersedes
AD2012-04-01
Models
RB211-Trent 875-17, RB211-Trent 877-17, RB211-Trent 884-17, RB211-Trent 884B-17, RB211-Trent 892-17, RB211-Trent 892B-17, RB211-Trent 895-17
Data sheet
TCDSE00050EN
Registered aircraft
182 matched by model
Product
Engine
ATA chapter
72 · Engine
Amendment
39-18860
Docket
FAA-2010-0755
Project
2010-NE-12-AD
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 2017-07984. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

We are superseding airworthiness directive (AD) 2012-04-01 for all Rolls-Royce plc (RR) RB211-Trent 800 model turbofan engines. AD 2012-04-01 required removal from service of certain critical engine rotating parts based on reduced life limits. This AD makes additional revisions to the life limits of certain critical engine rotating parts. This AD was prompted by RR further revising the life limits of certain critical engine rotating parts. We are issuing this AD to correct the unsafe condition on these products.

The airworthiness directive

2017-08-11 Rolls-Royce plc: Amendment 39-18860; Docket No. FAA-2010-0755; Directorate Identifier 2010-NE-12-AD.

(a) Effective Date

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This AD is effective May 30, 2017.

(b) Affected ADs

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This AD replaces AD 2012-04-01, Amendment 39-16956 (77 FR 10355, February 22, 2012).

(c) Applicability

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This AD applies to all Rolls-Royce plc (RR) RR RB211-Trent 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17, and 895-17 turbofan engines.

(d) Subject

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Joint Aircraft System Component (JASC) Code 7200, Engine (Turbine/Turboprop).

(e) Unsafe Condition

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This AD was prompted by RR revising the life limits of certain critical engine rotating parts. We are issuing this AD to prevent the failure of critical engine rotating parts, damage to the engine, and damage to the airplane.

(f) Compliance

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

(1) After the effective date of this AD, remove from service the parts listed in Table 1 to paragraph (f) of this AD before exceeding the new life limit indicated:

Table 1 to Paragraph ( f)—Reduced Part Lives
Part nomenclaturePart No.Life in standard duty cyclesLife in cycles using the HEAVY profile
Intermediate Pressure (IP) Compressor Rotor ShaftFK2410012,50011,500
IP Compressor Rotor ShaftFK244968,8608,180
High-Pressure Compressor (HPC) Stage 1 to 4 Rotor Discs ShaftFK240094,5604,460
HPC Stage 1 to 4 Rotor Discs ShaftFK261675,5805,280
HPC Stage 1 to 4 Rotor Discs ShaftFK325805,5805,280
HPC Stage 1 to 4 Rotor Discs ShaftFW115908,5506,850
HPC Stage 1 to 4 Rotor Discs ShaftFW616228,5506,850
HPC Stage 5 and 6 Discs and ConeFK252305,0005,000
HPC Stage 5 and 6 Discs and ConeFK278995,0005,000
IP Turbine Rotor DiscFK2111711,61010,400
IP Turbine Rotor DiscFK3308300

(2) Reserved.

(g) Installation Prohibition

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After the effective date of this AD, do not install any IP turbine discs, P/N FK33083, into any engine.

(h) Alternative Methods of Compliance (AMOCs)

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The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: ANE-AD-AMOC@faa.gov.

(i) Related Information

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(1) For more information about this AD, contact Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7754; fax: 781-238-7199; email: robert.green@faa.gov.

(2) Refer to MCAI European Aviation Safety Agency, AD 2016-0223, dated November 8, 2016, for more information. You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2010-0755.

(j) Material Incorporated by Reference

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None.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD is effective May 30, 2017.

AddressesPage 1

See the FOR FURTHER INFORMATION CONTACT section.

For further information contactPage 2

Robert Green, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7754; fax: 781-238-7199; email: robert.green@faa.gov.

DiscussionPage 2

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2012-04-01, Amendment 39-16956 (77 FR 10355, February 22, 2012), (“AD 2012-04-01”). AD 2012-04-01 applied to the specified products. The NPRM published in the Federal Register on January 18, 2017 (82 FR 5454). The NPRM proposed to continue to require removal from service of certain critical engine rotating parts based on reduced life limits.

CommentsPage 2

We gave the public the opportunity to participate in developing this AD. We considered the comments received. The Boeing Company and American Airlines support the NPRM as written.

ConclusionPage 2

We reviewed the available data, including the comments received, and determined that air safety and the public interest require adopting this AD as proposed.

Costs of CompliancePage 2

We estimate that this AD affects 16 engines installed on airplanes of U.S. registry.

We estimate the following costs to comply with this AD:

Estimated Costs
ActionLabor costParts costCost per productCost on U.S. operators
Replacement of critical engine rotating parts0 work-hours × $85 per hour = $0$45,000 (pro-rated cost of parts)$45,000$720,000
Authority for This RulemakingPage 2

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 findingsPage 2

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 DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979),

(3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction, 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.

Adoption of the AmendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:

Adoption of the amendmentPage 2

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by removing airworthiness directive (AD) 2012-04-01, Amendment 39-16956 (77 FR 10355, February 22, 2012) and adding the following AD:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 182

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing181 aircraft
  • Airbus1 aircraft
By year built
19822014
Registered aircraft by year built: 181 aircraft
19821
19831
19851
19873
19881
19894
19901
19914
19927
19931
199427
199515
19968
199713
199811
199924
200018
200126
20025
20034
20045
20141

1 with no year recorded

By model

Aircraft

See all 182 aircraft