AIRWORTHINESS DIRECTIVE

CAA-AD-028/2002

Date of issue: February 27, 2002

SAILPLANE – C OF G RELEASE HOOK – INSPECTION/REPLACEMENT

Applicability: Kind of aeronautical product: Sailplane

Manufacturer: Grob, Tussenhausen-Mattsies, Germany

Type: TWIN ASTIR

Models / Serial numbers affected:

TWIN ASTIR

- S/N: 3000 - 3291

TWIN ASTIR TRAINER

- S/N: 3008 up to 3291 (with suffix ''T'')

G 103 TWIN II

- S/N: 3501 up to 3729

G 103A TWIN II ACRO

- S/N: 3544 up to 34078 (with suffix ''K'')

G 103C TWIN III ACRO

- S/N: 34101 and up

G 103C TWIN III

- S/N: 36001 up to 36014

Effective date: March 21, 2002

Compliance : Required as indicated in LBA AD 2002-067.

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

Airworthiness Directive No.: 2002-067

Luftfahrt-Bundesamt

Airworthiness Directive Section

Hermann-Blenk-Str. 26

38108 Braunschweig

Federal Republic of Germany

 

Effective Date: March 21, 2002

 

Grob

 

Affected:

Kind of aeronautical product: Sailplane

Manufacturer: Grob, Tussenhausen-Mattsies, Germany

Type: TWIN ASTIR

Models / Serial numbers affected:

TWIN ASTIR

- S/N: 3000 - 3291

TWIN ASTIR TRAINER

- S/N: 3008 up to 3291 (with suffix ''T'')

G 103 TWIN II

- S/N: 3501 up to 3729

G 103A TWIN II ACRO

- S/N: 3544 up to 34078 (with suffix ''K'')

G 103C TWIN III ACRO

- S/N: 34101 and up

G 103C TWIN III

- S/N: 36001 up to 36014

German Type Certificate No.: 315

 

Subject:

C of G Release hook - cracks at the forward attachment brackets

Reason:

After long time of operation, cracks at the forward C of G release hook attachment brackets might occur.

Action / Compliance:

1. Visually check the attachment brackets before April 30, 2002. If cracks have been found: replace the brackets

before the next flight.

2. If no cracks were found: exchange the attachment brackets not later than September 30, 2002.

The actions must be done in accordance with the instructions of the manufacturers Service Bulletin.

Technical publication of the manufacturer:

Grob Service Bulletin No. MSB315-62 dated January 21, 2002 which becomes herewith part of this AD can be obtained from Messrs.:

GROB Luft- und Raumfahrt

Lettenbachstrasse 9

D-86874 Tussenhausen-Mattsies / Germany

Phone: ++ 49 8268 / 998139

Fax: ++ 49 8268 / 998200

e-mail: productssupport@grob-aerospace.de

Holders of affected aircraft registered in Germany have to observe the following:

Action has to be accomplished by the owner of the aircraft or an approved service station and to be checked and

entered in the log book by a licensed inspector.

 

Enquiries regarding this Airworthiness Directive should be referred to Mr. Olaf Schneider, Airworthiness Directive Section at the above address, fax-no.

0049 531/2355-720. Please note, that in case of any difficulty, reference should be made to the German issue!

LTA´s / AD´s and Technical Notes are published on the internet at http://www.lba.de