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2009-07-01 R1: High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs

FAA order 2009-07-01 R1 is an airworthiness directive in force since August 6, 2012. The FAA's subject line: High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs. It names the Rolls-Royce Deutschland BR700-715A130, Rolls-Royce Deutschland BR700-715B130, Rolls-Royce Deutschland BR700-715C130 engines: about 8 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: BR700-715A1-30, BR700-715B1-30, BR700-715C1-30
Engine series: Rolls-Royce Deutschland BR700-715A130 6 aircraft
Rolls-Royce Deutschland BR700-715B130 1 aircraft
Rolls-Royce Deutschland BR700-715C130 1 aircraft

Dates and paperwork

In force since: August 6, 2012
Published: July 2, 2012 (signed June 7, 2012)
Docket: FAA-2008-0224
Replaces: 2009-07-01
Status: Current
The FAA's document: Read the order on the FAA's site

The FAA's summary their words, unchanged

We are rescinding an airworthiness directive (AD) for RRD BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines. The existing AD resulted from the need to reduce the published life limits of high-pressure (HP) turbine stage 1 discs, part numbers (P/Ns) BRH20130 and BRH20131, and HP turbine stage 2 discs, P/Ns BRH19423 and BRH19427. We are rescinding the existing AD because RRD has revised the approved published life limits of these parts to the same or higher limits as originally certified.

The order itself the regulatory text, as published

Show the full text (1,324 characters)

Adoption of the Amendment 

	Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: 

PART 39--AIRWORTHINESS DIRECTIVES 

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

	Authority:  49 U.S.C. 106(g), 40113, 44701. 

Sec.  39.13  [Amended] 

0 2. The FAA amends Sec.  39.13 by rescinding airworthiness directive (AD) 2009-07-01, Amendment 39-15860 (74 FR 12086, March 23, 2009): 

2009-07-01 R1 Rolls-Royce Deutschland Ltd & Co KG (formerly BMW Rolls-Royce GmbH, formerly BMW Rolls-Royce Aero Engines): Amendment 39-17085; Docket No. FAA-2008-0224; Directorate Identifier 2007-NE- 44-AD. 

(a) Effective Date 

	This AD is effective August 6, 2012. 

(b) Affected ADs 

	This AD rescinds AD 2009-07-01 (74 FR 12086, March 23, 2009). 

(c) Applicability 

	This AD applies to Rolls-Royce Deutschland Ltd & Co KG BR700- 715A1-30, BR700-715B1-30, and BR700-715C1-30 turbofan engines.[[Page 39157]] 

(d) Related Information 

	For more information about this AD, contact Mark Riley, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781-238-7758; fax: 781-238-7199; email: mark.riley@faa.gov. 

(e) Material Incorporated by Reference 

	None.

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 8, 2026. Connections as data: /graph/directive/2009-07-01 R1.json · aircraft systems.