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  Safety Publications Tool

List of Mandatory Continuing Airworthiness Information

Displaying records 17061 to 17080 out of a total of 18179 publications.

Number Issued by Issue date Sorted in descending order Subject Approval Holder / Type Designation Effective date Attachment
G-0155-PRE80
UK
 1980-01-01 Inspection of main wing spar for corrosion.
  • ORPHANED (No TC Holder)
    • SLINGSBY
1980-01-01
G-0675-PRE80
UK
 1980-01-01 Electrical Generation System – Warning of loss of generated electrical power.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0674-PRE80
UK
 1980-01-01 Landing Gear – Retention of internal support ring for main undercarriage shock absorber within undercarriage leg extension tube.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0673-PRE80
UK
 1980-01-01 Flight Controls – Inspection of rudder drive lever and final drive rod end in base of fin.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0672-PRE80
UK
 1980-01-01 Flight Controls – Replacement of 20 SWG (0.036" thick) rudder bar pillar/slides tube assemblies at first pilot’s position.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0671-PRE80
UK
 1980-01-01 Stabilizers – Inspection of tailplane attachment bracket and surrounding structure at rear of pod.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0670-PRE80
UK
 1980-01-01 Landing Gear – Attachment of undercarriage shock absorber mounting flange to main undercarriage leg tube.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0669-PRE80
UK
 1980-01-01 Flight Controls – Corrosion of rudder mass balance arm support brackets.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0668-PRE80
UK
 1980-01-01 Equipment/Furnishings – Introduction of single buckle safety harness with inertia reel tensioning.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0667-PRE80
UK
 1980-01-01 Flight Controls – Examination of rudder bar pillar and slider tube assembly.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0666-PRE80
UK
 1980-01-01 Engine/Propeller Controls – Reinforcement of Teleflex conduit swivel bracket attachment on propeller and engine controls.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0664-PRE80
UK
 1980-01-01 Engine Indicating – Engine Tachometer Calibration.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0663-PRE80
UK
 1980-01-01 Flight Controls – Cracking of rudder stop structure.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0662-PRE80
UK
 1980-01-01 Flight Controls – Inspection and protection against electrolytic corrosive action – control rods.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0661-PRE80
UK
 1980-01-01 Flight Controls – Corrosion inside aileron mass balance tube.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0660-PRE80
UK
 1980-01-01 Propellers – Propeller Blade Shank failure – rear engine.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0659-PRE80
UK
 1980-01-01 Nacelles/Pylons – Corrosion of engine mounting brackets.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0658-PRE80
UK
 1980-01-01 Landing Gear – Torque tightening of bolts and defects in undercarriage lower bracket.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0657-PRE80
UK
 1980-01-01 Fire Protection – Rear engine fire detection system.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01
G-0656-PRE80
UK
 1980-01-01 Fuselage – Omission of drain holes from under-surface of rear fuselage.
  • BRITTEN-NORMAN AEROSPACE LTD
    • BN2A Mark III (Trislander)
1980-01-01