AIRWORTHINESS DIRECTIVE

CAA-AD-T-097/2001R2

Nahrazuje CAA-AD-T-097/2001R1

Date of issue: February 21, 2002

HELICOPTER – MAIN ROTOR – STARFLEX STAR (ATA 05, 62) – INSPECTION

Applicability: AS 355 version E, F, F1, F2 and N helicopters equipped with STARFLEX stars P/N 350A31.1916.00.

Effective date: Upon receipt

Compliance : Required as indicated in DGAC AD 2001-558-064(A) R2.

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.: 2001-558-064(A) R2

EUROCOPTER

AS 355 Helicopters

Main rotor - STARFLEX star (ATA 05, 62)

1. EFFECTIVITY:

AS 355 version E, F, F1, F2 and N helicopters equipped with STARFLEX stars P/N 350A31.1916.00.

2. REASONS:

This Airworthiness Directive (AD)is issued following several occurrences of rapid bonding failure of the metal bush that is installed on the STARFLEX star arm ends. In some cases, these incidents caused the pilots to land quickly due to strong vibrations in the cabin.

Revision 1 introduces the Revision 1 of the Alert Telex which corrects a mistake in the number of this document at its issue and adds the Note in paragraph 3.1.

Revision 2 renders the embodiment of MOD 076221, which is subject of referenced EUROCOPTER AS 355 Alert Service Bulletin (ASB) No. 62.00.26, mandatory, in addition to the checks already required.

3. MANDATORY ACTIONS AND COMPLIANCE TIME:

3.1. Before the next flight after the effective date of this AD at original issue, then after each flight after which the rotors are stopped, check the adhesive bead of the metal bushes bonded at the end of the three arms of STARFLEX stars, in compliance with the instructions described in paragraph 2 of referenced AS 355 Alert Telex No. 05.00.37 R1.

Note: The check can be carried out by a pilot having received the appropriate training.

3.2. No later then May 31, 2002, install a stop stud at the bottom of each frequency adapter (MOD 076221), in compliance with the instructions described in paragraph 2 of referenced AS 355 ASB No. 62.00.26.

3.3. From the effective date of this AD Revision 2, before installation on aircraft, of a main rotor head held as spare (MOD 076221), install a stop stud at the bottom of each frequency adapter, in compliance with the instructions described in paragraph 2 of referenced AS 355 ASB No. 62.00.26.

REF.: EUROCOPTER AS 355 Alert Telex No. 05.00.37 R1

EUROCOPTER AS 355 Alert Service Bulletin No. 62.00.26.

This Revision 2 replaces AD 2001-558-064(A) R1 dated November 28, 2001.

EFFECTIVE DATES:

Original AD: On receipt of the telegraphic AD issued on NOVEMBER 12, 2001

Revision 1: On receipt from NOVEMBER 28, 2001

Revision 2: On receipt from FEBRUARY 06, 2002