# AD 97-07-04: Combustor Liner - Type: Airworthiness directive - Status: Historical - Products: Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H-36, RB211-524H-T-36, RB211-524H2-19 and RB211-524H2-T-19 - Effective: June 6, 1997 - Published: April 7, 1997, 62 FR 16475–16477 - Issued as: Final rule - Superseded by: [AD 2004-26-05](https://openairdocs.org/ad/2004-26-05) - Product type: Engine - Amendment: 39-9978 - Docket: 95-ANE-56 - Registered aircraft: 186 may be affected, by airframe or engine model (OpenAirDocs) - Official PDF: https://openairdocs.org/files/sha256/61/e5/61e586d8e5259e67ed40208b9e6c3d08283ddfc433037bbca34ab69167033119 (from https://www.govinfo.gov/content/pkg/FR-1997-04-07/pdf/97-8474.pdf) - Federal Register: https://www.federalregister.gov/documents/1997/04/07/97-8474/airworthiness-directives-rolls-royce-plc-rb211-524-series-turbofan-engines - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4DE16960D86D197F8625688000672F0E.0001 - DRS record last changed: August 7, 2025 - Page: https://openairdocs.org/ad/97-07-04 ## The airworthiness directive 97-07-04 ROLLS-ROYCE PLC: Amendment 39-9978. Docket 95-ANE-56. Applicability: Rolls-Royce plc (R-R) Models RB.211-524G and -524H turbofan engines that have not been modified in accordance with R-R Service Bulletin (SB) No. RB.211-72-9764, Revision 2, dated November 10, 1995, installed on but not limited to Boeing 747-400 and 767- 300 series aircraft. Note 1: This airworthiness directive (AD) applies to each engine identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For engines that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (d) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required as indicated, unless accomplished previously. To prevent engine combustor liner deterioration due to thermal fatigue, which can result in combustor liner and case burn-through and engine fire, accomplish the following: (a) Perform initial and repetitive borescope inspections of the engine combustor liner head section in accordance with the intervals listed in Section 1.C. Compliance (1), and the procedures described in Section 1.D. Action (1) of R-R SB No. RB.211-72-B482, Revision 3, dated September 27, 1996. Prior to further flight, remove combustors that do not meet the return to service criteria specified in Section 1.E. Acceptance Limits of the SB and replace with serviceable parts. (b) Perform initial and repetitive borescope inspections of the meterpanel in accordance with the intervals listed in Section 1.C. Compliance (2), andthe procedures described in Section 1.D. Action (2) of R-R SB No. RB.211-72-B482, Revision 3, dated September 27, 1996. Prior to further flight, remove combustors that do not meet the return to service criteria specified in Section 1.E. Acceptance Limits of the SB and replace with serviceable parts. (c) Installation of a front combustion liner with a strengthened head section in C263 material in accordance with R-R SB No. RB.211-72-9764, Revision 2, dated November 10, 1995, constitutes terminating action to the inspection requirements of this AD. (d) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Engine Certification Office. The request should be forwarded through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Engine Certification Office. Note 2: Information concerning the existence of approved alternativemethods of compliance with this airworthiness directive, if any, may be obtained from the Engine Certification Office. (e) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the requirements of this AD can be accomplished. (f) The actions required by this AD shall be done in accordance with the following R-R SBs: Document No Pages Revision Date RB.211-72-B482 1 3 September 27, 1996 2 2 March 11, 1996 3 3 September 27, 1996 4 2 March 11, 1996 5 3 September 27, 1996 6 2 March 11, 1996 7,8 3 September 27, 1996 9 2 March 11, 1996 Total Pages: 9. RB.211-72-9764 1 2 November 10, 1995 2 Original August 20, 1993 3 2 November 10, 1995 4-6 1 August 25, 1995 7-30 Original August 20, 1993 Supplement 1 Original August 20, 1993 Total Pages: 31. Thisincorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Rolls-Royce North America, Inc., 2001 South Tibbs Ave., Indianapolis, IN 46241; telephone (317) 230-3995, fax (317) 230-4743. Copies may be inspected at the FAA, New England Region, Office of the Assistant Chief Counsel, 12 New England Executive Park, Burlington, MA; or at the Office of the Federal Register, 800 North Capitol Street NW., suite 700, Washington, DC. (g) This amendment becomes effective on June 6, 1997. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS E30NE](https://openairdocs.org/tcds/E30NE): Rolls-Royce Deutschland Ltd & Co KG; names 8 of 8 models: RB211-524H-T-36, RB211-524H-36, RB211-524G2-19, RB211-524G2-T-19, RB211-524H2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19 ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 186 (0 by airframe model, 186 by engine model) - Makers: Boeing 185, Airbus 1 Models with the most aircraft: - [Rolls-Royce RB-211 series](https://openairdocs.org/engine/rolls-royce-rb-211-series): 182 aircraft (engine model) - [Rolls-Royce RB211-524H-36](https://openairdocs.org/engine/rolls-royce-rb211-524h-36): 2 aircraft (engine model) - [Rolls-Royce RB211-524HT36](https://openairdocs.org/engine/rolls-royce-rb211-524ht36): 2 aircraft (engine model) All 3 models: https://openairdocs.org/ad/97-07-04/models.md Every aircraft: https://openairdocs.org/ad/97-07-04/aircraft.md ## Related documents - [AD 2004-26-05](https://openairdocs.org/ad/2004-26-05) (historical): Head section and meterpanel assembly of the combustion liner · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 20 more. Effective Feb 9, 2005. Supersedes this AD - [Proposed rule 95-ANE-56](https://openairdocs.org/proposed/95-ANE-56): Notice of proposed rulemaking (NPRM), published Nov 13, 1996 Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.