Skip to content

Agusta Bollettino Tecnico 109-110

Service bulletin · Agusta

Revision AU.S. DOT/FAA - Agusta BT 109-110 Rev A · 6 pages · 3.1 MB

© Leonardo S.p.A. Filed by the FAA in regulations.gov docket FAA-2008-0834; AD 2008-24-06 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

Docket FAA-2008-0834 (document 0005) · AD 2008-24-06

Open PDF Read the text

Manufacturer: Leonardo
As issued by: Agusta
Type: Bollettino Tecnico
Number: 109-110
Latest revision known: 109-110, Revision A, dated December 12, 2005

A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.

On this page

ADs that cite it · 3

Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.

AD 2008-24-06Tail rotor blade · Agusta A109A and A109A IIEffective Dec 30, 2008 · Revision A AD 99-27-12Tail Rotor Blade · Agusta A109A and A109A IIEffective Jan 5, 2000 · No revision named AD 99-26-13Blade Crack Inspection · Agusta A109A and A109A IIEffective Jan 4, 2000 · No revision named

Also cited in 1 proposed AD.