Safety Publications Tool

G-009-07-89 : Engine Controls - Condition control break bias unit assembly Part No. 44650M01 - To introduce an inspection for link arms Part No. 44685 issue A with greater than 1000 flight hours at every 125 hours servicing period, for cracking at the lightening holes.

Number G-009-07-89
Issued by United Kingdom  United Kingdom
Issue date 1989-07-01
Effective date 1989-07-01
EASA approval number
ATA Chapter
Approval Holder
/ Type Designation
  • BAE SYSTEMS (OPERATIONS) LTD
    • ATP
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information SB ATP-76-3
Remarks Applicable to aircraft fitted with break bias pulley units JD007J1592-000 Sarma Part No. 44650M01. Compliance and requirement as detailed in Service Bulletin.