AIRWORTHINESS DIRECTIVE

 

CAA-AD-054/2001

 

Date of issue: June 18, 2001

 

AIRCRAFT - RAM AIR TURBINE - OVERHAUL

 

Applicability: AIRBUS INDUSTRIE A300, A310 and A300-600 aircraft, all certified models and all serial numbers, which are fitted with a DOWTY or HAMILTON SUNDSTRAND ram air turbine.

 

Effective date: August 09, 2001

 

Compliance: Required as indicated in DGAC AD 2001-212(B).

 

Remarks: The compliance of this AD must be recorded in Aircraft Logbook, where applicable the requirements of this AD must be integrated into Aircraft Technical Documentation. Address inquiries concerning this AD to: Civil Aviation Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel: 420 2 33320922, fax: 420 2 20562270.

 

Ing. Pavel MATOUŠEK

Director of Airworthiness Division

CAA CZ

 

DGAC AD No.: 2001-212(B)

AIRBUS INDUSTRIE

 

A300, A310 and A300-600 aircraft

 

Auxiliary hydraulic power - Overhaul and modification to the ram air turbine (ATA 29)

 

APPLICABILITY:

 

AIRBUS INDUSTRIE A300, A310 and A300-600 aircraft, all certified models and all serial numbers, which are fitted with a DOWTY or HAMILTON SUNDSTRAND ram air turbine.

 

REASONS:

 

The extension of the "Ram Air Turbine" (RAT) operating life has been justified to 60,000 flight hours. However, and in order to take into account technical considerations linked to the life limitation of the grease and corrosion issues, a periodic overhaul of the RAT is rendered mandatory.

 

In addition, modifications recommended until now are also rendered mandatory on the occasion of this overhaul.

 

ACTIONS:

 

1) Prior to accumulation of 20 years since the first installation on aircraft, or within two years following the effective date of this AD, whichever occurs later, perform an overhaul of the RAT, in accordance with the instructions of AIRBUS INDUSTRIE Service Bulletins (SBs) A300-29-0118, A310-29-2087 or A300-29-6049.

 

This overhaul will be completed simultaneously and depending on the configuration of each RAT, by the application of modifications in accordance with the instructions of SBs A300-29-0118, A310-29-2087 or A300-29-6049.

 

2) Perform an overhaul of the RAT every 20 years, in accordance with the instructions of SBs A300-29-0118, A310-29-2087 or A300-29-6049.

 

REF:       AIRBUS INDUSTRIE Service Bulletin A300-29-0118

AIRBUS INDUSTRIE Service Bulletin A310-29-2087

AIRBUS INDUSTRIE Service Bulletin A300-29-6049

(Any later approved revision of these SBs is acceptable).

 

EFFECTIVE DATE: JUNE 09, 2001