AIRWORTHINESS DIRECTIVE
CAA-T-AD-2-041/98
Date of issue: May 14, 1998
Effective date: upon receipt
GSAC
TELEGRAPHIC AIRWORTHINESS DIRECTIVE
released by DIRECTION GENERALE DE L'AVIATION CIVILE
This text is not sent to foreign operators of aircraft non registered in France. It is up to the national authorities to forward it to them on receipt.
Translation of 'Consigne de Navigabilité'
ref.: T98-198(B)
In case of any difficulty, reference should
be made to the French original issue.
CFMI - Turbo-fan engines CFM56-3 all models.
Accessory gear box (AGB).
1. Applicability:
This AD applies to CFM56-3 / -3B / -3C engines identified and listed in table 1 of Service -Bulletin 72-877, and installed on Boeing 737 or other aeroplanes.
2. Reason:
An In-Flight Shut Down was experienced due to a failure of the starter gearshaft (line 5) in the accessory gear box (AGB).
3. Mandatory action:
Remove from service the starter gearshaft (line 5) in the AGB of concerned engines (see Service Bulletin 72-877).
4. Dates of compliance:
A) For planes which have the two engines concerned, perform on one engine the above mandatory action before 1st June 1998.
B) For planes which have only one engine concerned, perform the above mandatory action before 1st August 1998.
5. Reference: Service - Bulletin CFM56-3 / 3B / 3C S/B 72-877.
6. Effective date: On receipt.
Address inquiries concerning this AD to: Ing. Tůma, Civil Aviation
Authority, Airworthiness Division, Ruzyne Airport, 160 08 Prague 6, Czech Republic, tel.: 420 2 2011/1729, fax: 420 2 364112