AD 82-12-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Rolls-Royce plc | RB211-22B-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-22B/MOD 72-8700 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B-B-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B2-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B2-B-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B3-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B4-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524B4-D-02 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524C2-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524C2-B-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4-39 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4-B-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4-B-39 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4X-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524D4X-B-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524G2-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524G2-T-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524G3-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524G3-T-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524H-36 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524H-T-36 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524H2-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
| engine | Rolls-Royce plc | RB211-524H2-T-19 | ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. |
Unsafe Condition
Possible loss of the fan assembly
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install the Rolls-Royce axial fan retention modification as specified in Service Bulletin 72-6574 or 72-6576, depending on engine model.
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Compliance Time
Center engines on Lockheed L1011 by September 30, 1982; wing-mounted engines on Lockheed L1011 and Boeing B747 by December 31, 1982.
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Affected Aircraft
Rolls-Royce RB211-22B and -524 series engines including models RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02, RB211-524B-B-02, RB211-524B2-19, RB211-524B2-39, RB211-524C2-19, RB211-524B3-02, RB211-524B4-02, and RB211-524D4-19.
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Federal Register Abstract
Fan Assembly
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_82-12-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-12-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. Subject: Fan Assembly Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/07/1982 Make: Rolls-Royce plc Model: RB211-22B-02 | RB211-22B/MOD 72-8700 | RB211-524B-02 | RB211-524B-B-02 | RB211-524B2-19 | RB211-524B...Show more Product Type: Engine Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-12-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4398 AD NUMBER: 82-12-05 SUBJECT HEADING: ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. ACTION: SUMMARY: DATES: Effective June 7, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-12-05 ROLLS-ROYCE, LTD.: Amendment 39-4398. Applies to Rolls-Royce, Ltd., RB211-22B and -524 series turbofan model engines. Compliance required as indicated unless already accomplished. To preclude possible loss of the fan assembly, install the Rolls-Royce axial fan retention modification as specified in Rolls-Royce Service Bulletin 72-6574, Revision 2, dated March 19, 1982, or later revision approved by the FAA, applicable to RB211-22B, -524B-02, -524B2-19, -524B2-39, and -524C2-19 engines and as specified in Rolls-Royce Service Bulletin 72-6576, Revision 2, dated March 19, 1982, or later revision approved by the FAA, applicable to RB211-524B3-02, -524B4-02, and -524D4-19 engines in accordance with the following schedule: 1. Center (fuselage mounted) engines on Lockheed L1011 aircraft by September 30, 1982. 2. Wing mounted engines on Lockheed L1011 and Boeing B747 by December 31, 1982. All persons affected by this directive who have not already received the referenced service bulletins from the manufacturer may obtain copies upon request to Technical Publications Department, Rolls-Royce, Ltd., P.O. Box 31, Derby, England DE2 8BJ. This document may also be examined at Federal Aviation Administration, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD is maintained by the FAA at the New England Regional Office. Upon request of the operator, an FAA Maintenance Inspector, subject to prior approval of the Chief, Aircraft Certification Division, FAA, New England Region, may adjust the compliance date(s) specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the adjustment for that operator. This amendment becomes effective June 7, 1982. FOOTER:
Document Text
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AD Final Rules - DRS_82-12-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 82-12-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. Subject: Fan Assembly Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/07/1982 Make: Rolls-Royce plc Model: RB211-22B-02 | RB211-22B/MOD 72-8700 | RB211-524B-02 | RB211-524B-B-02 | RB211-524B2-19 | RB211-524B...Show more Product Type: Engine Product Subtype: Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 82-12-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4398 AD NUMBER: 82-12-05 SUBJECT HEADING: ROLLS-ROYCE, LTD. Model RB211-22B and -524 series turbofan model engines. ACTION: SUMMARY: DATES: Effective June 7, 1982. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 82-12-05 ROLLS-ROYCE, LTD.: Amendment 39-4398. Applies to Rolls-Royce, Ltd., RB211-22B and -524 series turbofan model engines. Compliance required as indicated unless already accomplished. To preclude possible loss of the fan assembly, install the Rolls-Royce axial fan retention modification as specified in Rolls-Royce Service Bulletin 72-6574, Revision 2, dated March 19, 1982, or later revision approved by the FAA, applicable to RB211-22B, -524B-02, -524B2-19, -524B2-39, and -524C2-19 engines and as specified in Rolls-Royce Service Bulletin 72-6576, Revision 2, dated March 19, 1982, or later revision approved by the FAA, applicable to RB211-524B3-02, -524B4-02, and -524D4-19 engines in accordance with the following schedule: 1. Center (fuselage mounted) engines on Lockheed L1011 aircraft by September 30, 1982. 2. Wing mounted engines on Lockheed L1011 and Boeing B747 by December 31, 1982. All persons affected by this directive who have not already received the referenced service bulletins from the manufacturer may obtain copies upon request to Technical Publications Department, Rolls-Royce, Ltd., P.O. Box 31, Derby, England DE2 8BJ. This document may also be examined at Federal Aviation Administration, New England Region, 12 New England Executive Park, Burlington, Massachusetts 01803. A historical file on this AD is maintained by the FAA at the New England Regional Office. Upon request of the operator, an FAA Maintenance Inspector, subject to prior approval of the Chief, Aircraft Certification Division, FAA, New England Region, may adjust the compliance date(s) specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the adjustment for that operator. This amendment becomes effective June 7, 1982. FOOTER:
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Retrieved: Apr 8, 2026
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