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)
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.
