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2008-16-05: Intermediate pressure turbine (IPT) disk

FAA order 2008-16-05 is an airworthiness directive in force since September 4, 2008. The FAA's subject line: Intermediate pressure turbine (IPT) disk. It names the Rolls-Royce DART 529, Rolls-Royce DART 535-7R, Rolls-Royce DART 542 engines: about 6 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Engine
Makes
Rolls-Royce Deutschland Ltd & Co KG
Models
Dart 528-7E, Dart 528D-7E, Dart 529-7E, Dart 529-7H, Dart 529-8E, Dart 529-8H, Dart 529-8X, Dart 529-8Y, Dart 529-8Z, Dart 529D-7E, Dart 529D-7H, Dart 529D-8E, Dart 529D-8H, Dart 529D-8X, Dart 529D-8Y, Dart 529D-8Z, Dart 532-2L, Dart 532-7, Dart 532-7L, Dart 532-7N, Dart 532-7P, Dart 532-7R, Dart 535-2, Dart 535-7R, Dart 542-10, Dart 542-10J, Dart 542-10K, Dart 542-4, Dart 542-4K, Dart 552-2, Dart 552-7, Dart 552-7R
Engine series
Rolls-Royce DART 529 4 aircraft
Rolls-Royce DART 535-7R 1 aircraft
Rolls-Royce DART 542 1 aircraft

Dates and paperwork

In force since
September 4, 2008
Published
October 6, 2008 (signed July 24, 2008)
Docket
FAA-2006-24825
Replaces
2007-02-07
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding an existing airworthiness directive (AD) for RRD Dart 528, 529, 532, 535, 542, and 552 Series turboprop engines. That AD currently requires a dimensional inspection of the intermediate pressure turbine (IPT) disk or an ultrasonic inspection of the seal arm contact between the high pressure turbine (HPT) and the IPT disk seal arm and reworking or replacing the IPT disk if worn beyond acceptable limits. This AD continues to require those actions. This AD results from us including an incorrect engine model and omitting an engine model from the applicability of the existing AD. We are issuing this AD to prevent HPT disk failure, which can result in an uncontained engine failure and damage to the airplane. DATES: This AD becomes effective September 4, 2008. The Director of the Federal Register previously approved the incorporation by reference of certain publications listed in the regulations on February 26, 2007 (72 FR 2610, January 22, 2007).

The order itself the regulatory text, as published

Show the full text (4,503 characters)
2008-16-05 Rolls-Royce Deutschland Ltd & Co KG (formerly Rolls-Royce plc): Amendment 39-15623. Docket No. FAA-2006-24825; Directorate Identifier 2006-NE-17-AD. Effective Date (a) This airworthiness directive (AD) becomes effective September 4, 2008. (b) This AD supersedes AD 2007-02-07, Amendment 39-14894. Applicability (c) This AD applies to Rolls-Royce Deutschland Ltd & Co KG (RRD) Dart 528, 529, 532, 535, 542, and 552 series turboprop engines. These engines are installed on, but not limited to, Hawker Siddeley, Argosy AW.650, Fairchild Hiller F-27, F-27A, F-27B, F-27F, F-27G, F- 27J, FH-227, FH-227B, FH-227C, FH-227D, FH-227E, Fokker F.27 all marks; British Aircraft Corporation Viscount 744, 745D and 810; Gulfstream G-159, General Dynamics Convair 240D or 600, or 600-240D, and 340D or 440D, or 640-340D and 640-440D airplanes. Unsafe Condition (d) This AD results from us including an incorrect engine model and omitting an engine model from the applicability of the existing AD. We are issuing this AD to prevent HPT disk failure, which can result in an uncontained engine failure and damage to the airplane. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Intermediate Pressure Turbine (IPT) Disk and High Pressure Turbine (HPT)/IPT Disk Seal Arm Inspections (f) Within 60 days after the effective date of the AD, do either of the following: (1) Perform a dimensional inspection of the IPT disk and repair or replace the IPT disk, if necessary using paragraph 3 of the Accomplishment Instructions of RRD service bulletin (SB) Da72-538, dated June 10, 2005; or (2) Perform an ultrasonic inspection of the disk seal arm contact between the HPT and the IPT using paragraph 3 of the Accomplishment Instructions of RRD SB Da72-536, Revision 1, dated August 25, 2003. (i) For RRD Dart 528, 529, 532, 535, 542 series turboprop engines if wear is outside allowable limits, before June 30, 2008, perform a dimensional inspection and repair or replace the IPT disk, if necessary. Use paragraph 3 of the Accomplishment Instructions of RRD SB Da72-538, dated June 10, 2005. (ii) For RRD Dart 552 series turboprop engines if wear is outside allowable limits, before July 31, 2008, perform a dimensional inspection and repair or replace the IPT disk, if necessary. Use paragraph 3 of the Accomplishment Instructions of RRD SB Da72-538, dated June 10, 2005. (iii) If wear is within allowable limits, perform a dimensional inspection of the IPT disk at the next engine shop visit or at next overhaul, whichever occurs first and repair or replace the IPT disk, if necessary. Use paragraph 3 of the Accomplishment Instructions of RRD SB Da72-538, dated June 10, 2005. Alternative Methods of Compliance (g) The Manager, Engine Certification Office, has the authority to approve alternative methods of compliance for this AD if requested using the procedures found in 14 CFR 39.19. Related Information (h) LBA airworthiness directive D-2005-197, dated June 30, 2005, also addresses the subject of this AD. (i) Contact Jason Yang, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone (781) 238-7747, fax (781) 238-7199; e-mail: jason.yang@faa.gov, for more information about this AD. Material Incorporated by Reference (j) You must use the Rolls-Royce Deutschland Ltd & Co KG service information specified in Table 1 to perform the actions required by this AD. The Director of the Federal Register previously approved the incorporation by reference of the service information specified in Table 1 on February 26, 2007 (72 FR 2610, January 22, 2007). Contact Rolls-Royce Deutschland Ltd & Co KG, Eschenweg 11, D-15827 Dahlewitz, Germany; telephone 49 (0) 33-7086-1768; fax 49 (0) 33- 7086-3356 for a copy of this service information. You may review copies at the FAA, New England Region, 12 New England Executive Park, Burlington, MA; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http:// www.archives.gov/federal-register/cfr/ibr-locations.html. Table 1--Incorporation by Reference Service Bulletin No. Page Revision Date Da72-536 Total Pages: 23 All 1 August 25, 2003 Da72-538 Total Pages: 21 All Original June 10, 2005

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2008-16-05.json · aircraft systems.