Safety Publications Tool

G-0137-PRE80 : DOWTY ROTOL Landing Gear – Introduction of new Sub-assembly of Hub and Bush to the Axle Assembly of Nose Undercarriage

Number G-0137-PRE80
Issued by United Kingdom  United Kingdom
Issue date 1967-08-01
Effective date 1971-05-01
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • APPLIANCES
    • ATA 32 LANDING GEAR
      • Landing Gears
  • BAE SYSTEMS (OPERATIONS) LTD
    • HS748
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Dowty Rotol SB 32-43E (original dated August 1967) re-issued May 1971. Applicable to parts installed on HS 748 Series aircraft. Compliance required not later than 31 December 1971.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu