# Agusta Bollettino Tecnico 119-21: No revision named

- Rights: © Leonardo S.p.A. Filed by the FAA in regulations.gov docket FAA-2009-0226; AD 2009-12-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Agusta Bollettino Tecnico 119-21](https://openairdocs.org/service-documents/leonardo/sb-119-21.md)
- Title as filed: U.S. DOT/FAA - Agusta ABT 119-21
- Pages: 8
- PDF: https://openairdocs.org/files/sha256/4c/2d/4c2d1555eeaf5aa763d98d01d3825f551b2a823acfa9a621efcf44b557ea9eac
- Page: https://openairdocs.org/service-documents/leonardo/sb-119-21/file/4c2d1555eeaf

## Text

This text is OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1 (OCR)

ALERT  Via Giovanni Agusta, 520
AGUSTA  21017 Cascina Costa di Samarate (VA) Italy
Tel.: +39 0331-229111 - Fax: +39 0331-229605/222595
AN AGUSTAWESTLAND COMPANY
TRANSLATION OF  BOLLETTINO TECNICO  N 119-21
The technical content of this document is approved  DATE June 06, 2007
under the authority of DOA nr EASA.21J.005.
REV.
this Bollettino is:  Compliance with  MANDATORY
SUBJECT: LEVER P/N 232-028-00 OF THE HOOK P/N 528-010-01 (ONBOARD
SUPPLIER)  THE  CARGO  HOOK INSTALLATION
P/N 109-0810-31-139 AND DUAL CARGO HOOK INSTALLATION
P/N 109-0811-75-115, INSPECTION OF.
REASON: Perform a visual inspection of the subject lever to verify possible
presence of cracks.
HELICOPTERS AFFECTED:
All the Agusta A119 helicopters equipped with the cargo hook
109-0810-31-139 (alone), or with
P/N 109-0810-31-139 and the dual cargo hook P/N 109-0811-75-115,
which install the hook P/N 528-010-01.
COMPLIANCE:
Before the next cargo hook operation after the receipt of this Bollettino
and however within and not later than August 31, 2007.
Successively before each single operation of the cargo hook.
WARNING
In presence of cracks the operation with the
cargo hook is prohibited.
DESCRIPTION:
Two cases of cracks on the lever assy P/N 232-028-00 have been
reported by the Onboard Systems International company. The lever is
considered a critical component of the hook P/N 528-010-01 for the
effects on the load (possible loss of the load).
Since the subject lever is installed on the Agusta A119 helicopters
equipped with the cargo hook P/N 109-0810-31-139 (alone), or with the
cargo hook P/N 109-0810-31-139 and the dual cargo hook
An appropriate entry should be made in the aircraft log book upon accomplishment.
ownership of aircraft has changed, please, forward to new owner.
ALERT  Page 1 of 5

### Page 2 (OCR)

B.T. 119-21
P/N 109-0811-75-115, this Bollettino provides the instructions to perform
a visual inspection of the lever, in order to determine if cracks are
present.
However, Agusta has in progress the evaluation and the certification of a
hook provided with a lever not affected by these problems.
REQUIRED MANPOWER:
Negligible.
WARRANTY:
N.A.
REQUIRED MATERIALS:
The following consumable material is required for compliance with this
Bollettino:
SPECIFICATION  DENOMINATION  Q.TY
TT-N-95 type 2  Aliphatic naphtha  A.R
(code 531055030)
SPECIAL TOOLS:
N.A.
WEIGHT AND BALANCE CHANGES:
N.A.
REFERENCES:
N.A.
PUBLICATIONS AFFECTED:
N.A.
COMPLIANCE INSTRUCTIONS:
(See figures 1 and 2)
1.  Prepare the helicopter on ground for a safe maintenance,
disconnect any power supply.
2.  In accordance with figures 1 and 2 perform a visual inspection for
presence of cracks on the lever P/N 232-028-00 of the hook
P/N 528-010-01 as follows:
2.1.  Clean the area with aliphatic naphtha or equivalent.
2.2.  Open the hook acting on the relevant release lever and illuminate
with a light source.
Page 2 of 5

### Page 3 (OCR)

B.T. 119-21
2.3.  Thoroughly inspect all the edge areas of the lever.
NOTE
In case of doubt use a magnifying glass.
2.4.  Close the hook.
Return the helicopter in ready to flight condition.
4.  Record compliance of this Bollettino in the helicopter log book.
Page 3 of 5

### Page 4 (OCR)

B.T. 119-21
Hook
528-010-01  Lever
232-028-00
Possible position
of cracks
Lever
232-028-00
FIGURE 1
Page 4 of 5

### Page 5 (OCR)

B.T. 119-21
Hook
528-010-01
Lever
232-028-00
Edge areas to be
inspected
FIGURE 2
Page 5 of 5

### Page 6

(No text on this page.)

### Page 7 (OCR)

AGUSTA
AN AGUSTAWESTLAND COMPANY
Prego spedire a questo indirizzo:  Data:
Please send to the following address:  MODULO APPLICAZIONE BOLLETTINO TECNICO  Date:
TECHNICAL BULLETIN COMPLIANCE FORM
AGUSTA S.p.A.
VICE DIREZIONE GENERALE  Numero:
Number:
CUSTOMER SUPPORT
Via per Tornavento, 15
21019 Somma Lombardo (VA) - ITALY  Revisione:
Tel.: +39 0331 711100  Revision:
Fax: +39 0331 711397
Denominazione Cliente ed Indirizzo:  Telefono:
Customer Name and Address:  Telephone:
Fax:
Data Applicazione B.T.:
B.T. Compliance Date:
Modello Elicottero  Helicopter Model  S/N  Tail Number  • Matricola  Ore Totali  Total Hours  Ore D.U.R.  T.S.O.
Note:
Remarks:
Informazioni:
Mod. AG AST 034 E 07  Information:
Al fine di gestire le varianti alla configurazione base, in relazione all'emissione del Bollettino Tecnico, preghiamo di voler compilare il presen-
te modulo in tutte le sue parti e spedirlo all'indirizzo sopra indicato. Si ringrazia per la gentile collaborazione data.
We request your cooperation in filling this form, in order to keep out statistical data relevant to aircraft configuration up-to-date. The form should be filled in all
its parts and sent to the above address. We thank you beforehand for the information given.

### Page 8

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