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## EASA EMERGENCY AIRW ORTHINESS DIRECTIVE

AD No : 2007- 0060R1 - E

Date: 20 April 2007

No person may operate an aircraft to which an Airworthines s Directive applies, except in accordance with the requirements of that Airworthiness Directive unless otherwi se agreed with the Authority of the State of Registry.


### Type Approval Holder’s Name :

BRP-Rotax GmbH & Co. KG Type/Model designation(s) :

Rotax 912 A series Rotax 912 F series Rotax 912 S series

TCDS Number: EASA.E.121

Foreign AD: N/A

Supersedure: N/A



### ATA 73 Engine Fuel and Control - Fuel Pump - Replacement

Manufacturer(s): BRP-Rotax GmbH & Co. KG; Bom bardier-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH;

Applicability: All versions of the engine type Rotax 912 A, 912 F and 912 S all serial numbers if Fuel pump part no. 892230, 892232, 892540 (standard version) or part no. 892235, 89 2236, 892545 (version including flexible fuel line), are installed.

These engines are known to be installed on, but not limited to, the following aircraft types:

Skyfox CA-25, CA-25N; Diamond (formerly HOAC) HK-36R Super Dimona, DV 20 Katana; Aeromot AMT-200 Super Ximango; Diamond DA20-A1 Katana; Evektor-Aerotechnik EV-97 Eurostar; Issoire APM-20 Lionceau; EIS (Fournier) RF-9; Scheibe SF 36R, SF 25C; Technoflug TFK-2 Carat; WD D4 BK Fascinatio n; III Sky Arrow 650 TC, 650 TCN and 650 TCNS; ABS RF-9 motor glider (Fournier design);

Reason: Due to high fuel pressure, caused by exceeding pressure in front of the mechanical fuel pump (e.g. due to an electrical fuel pump), in limited cases a deviation in the fuel supply could occur. This can result in exceeding of the fuel pressure and might cause engine malfunction and/or massive fuel leakage.2/2 Non-compliance with these instructions could result in engine damages, personal injuries or death. This Airworthiness Directive has been revised to incorporate reference to BRP Rotax SB-912-053, which has been issued to replace BRP Rotax ASB-912-053. If the operator has shown compliance with BRP Rotax ASB-912-053, as mandated by EASA Airworthiness Di rective 2007-0060 -E, no further action is required.

Effective Date: 24 April 2007

Compliance: At the next maintenance event, or within the next 25 hours of engine operation, but not later than 01 July 2007, whichever occurs first after the effective date of this directive: -replace the affected fuel pumps with part no. 892230, 892232, 892540 by part no. 892542 or replace fuel pumps with part no. 892235, 892236, 892545 by part no. 892546 After the effective date of this AD no person may install a replacement engine on any aircraft unless fuel pump part no. 892542 or part no. 892546 are installed.

Ref. Publications: BRP Rotax Service Bulletin SB-912-053, dated 13 April 2007, or later approved revision

Remarks : 1. If requested and appropriately su bstantiated the responsible EASA manager for the related product has the authority to accept Alternative Methods of Compliance (AMOC) for this AD. 2. The safety assessment has requ ested not to implement the full consultation process and an immedi ate publication and notification. 3. Enquiries regarding this Airworthin ess Directive should be referred to the AD Focal Point - Certification Directorate, EASA. E-mail: ADs@easa.europa.eu

. 4. For any question concerning the te chnical content of the requirements in this AD, please contac t BRP-Rotax GmbH & Co.KG Ph.: +43 7246 601 0; Fax: +43 7246 601 760