BOLLETTINO TECNICO 139-116

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AgustaWestland S.p.A
Via Giovanni Agusta, 520
21017 Cascina Costa di Samarate (VA) Italy
Tel.: +39 0331 229111 -Fax: +39 0331 229605/222595
A Finmeccanica Company
BOLLETTINO TECNICO
No
139-116
DATE
February 11, 2014
REV.
I
The technical content of this document is approved
under the authority of DOA nr. EASA.21J.005
MANDATORY
Compliance with
this bulletin is:
SUBJECT: RIGHT
AFT
FLOAT
RETRO-MODIFICATION
P/N
3G5306P47011,
INSTALLATION OF.
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REASON: to rework baggage RH floor panel, to prevent possible interference with AFT
Float Right Assy P/N 3G9560V00432 or P/N 3G9560V01532.
HELICOPTERS AFFECTED: all the following AB139/AW139 helicopters equipped with
AFT Float Right Assy P/N 3G9560V00432 or P/N 3G9560V01532:
-/ from S/N 31 005 to S/N 31157 (except S/N 31 007);
-/from S/N 31201 to S/N 31539, (except SIN's 31431, 31491, 31500, 31516, 31527,
31530,31531,31532, 31534);
-/ from S/N 41001 to S/N 41 023;
-/ from S/N 41201 to 41362; S/N 41365, S/N 41367 and S/N 41372.
COMPLIANCE: within three hundred (300) flight hours or six (6) months from receipt of
this Bollettino Tecnico, whichever comes first.
(_
An appropriate entry should be made in the aircraft log book upon accomplishment.
If ownership of aircraft has changed,
please,
forward to new owner.
Page 1 of 7
B.T. 139-116
DESCRIPTION: contact marks have been reported on some aircraft between the RHS
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rear float bottle valve connector and the baggage floor compartment panel.
It has been verified that by implementing the right connector orientation in
accordance with AMP instruction, this issue will not occur.
However, as a complementary preventive action to the above, this Bollettino Tecnico
provides the instructions to rework locally the panel increasing the tolerance of the
installation.
REQUIRED MANPOWER: it is estimated that in order to accomplish this Bollettino
Tecnico eight (8) maintenance man-hours (MMH) are necessary.
Man-hours are based on hands-on time and may vary with personnel and facilities
available.
WARRANTY:
•
Owners/Operators who comply with the instructions in this Bulletin, no later than
the applicable date in the "Compliance section" will be eligible to receive
replacements parts on a "free of charge basis", with the exception of consumable
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materials.
NOTE: Customers who fail to comply with the instructions in this bulletin before
the compliance date are not eligible for the aforementioned special policy
•
Please destroy locally the removed parts.
REQUIRED MATERIALS: the following materials are necessary to accomplish this
Bollettino Tecnico and can be requested to AgustaWestland:
Note
( 1)
PIN
3G5306P47011
Description
AFTER FLOAT RETROMOD (RH SIDE)
Composed of:
3G5306P4 7031
Floor Panel, Reworked
Composed of:
3G5306P47051
Doubler
Qty
Ref
Ref.
1
(_
Page 2 of 7
B.T. 139-116
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Moreover, the following consumable materials are necessary to accomplish this
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Bollettino Tecnico:
SPEC.IAW Code Number
DESCRIPTION
Q.TY
NOTE
199-05-002 TY I CL 2 Cod. No.900000581
Adhesive, Hysol
EA9309.3NA (C231)
AR
Local supply
Hexcel fabrics 20823 1200
Cod. No.
999999999000003617
Glass Fiber, thickness 0.15
mm, weight 195 g/m 2
AR
Local supply
NAS1721C4L2P or
NAS1721C4-2P
Rivet
4
Local supply
Notes
(1) Floor Panel P/N 3G5306P47031 is obtained reworking existing floor panel (P/N
3G5340A02432 or previous versions).
SPECIAL TOOLS: the following special tools are necessary to accomplish this
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Bollettino Tecnico:
PIN
Commercial
Commercial
DESCRIPTION
Q.TY I
AR
I
Local supply
I AR
I
Local supply
Permanent black ink
felt pen
IVibropen
NOTES
WEIGHT AND BALANCE CHANGES: N.A.
REFERENCES:
./ AW139 Aircraft Maintenance Data Information (AMDI)
./ AW139 Aircraft Maintenance Publication (AMP)
PUBLICATIONS AFFECTED: N.A.
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Page 3 of 7
B.T. 139-116
COMPLIANCE INSTRUCTIONS:
1.
Prepare the helicopter for a safe ground maintenance. Disconnect the battery and
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all the electrical power sources and/or the external power supply. Refer to AMP, see
OM no 39-A-00-20-00-00A-120A-A.
2.
Remove the AFT right float assembly. Referto AMP, see OM no 39-A-95-61-04-00A520A-K.
3.
With reference to figure 1, gain access to the right aft float area under the baggage
compartment.
4.
With reference to figure 2, countermark position for cut-out using doubler P/N
3G5306P4 7051 as a template.
5.
With reference to figures 2 and 3, perform cut-out on the floor panel according to
figure 3 section D-0.
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6
With reference to figures 3 section C-C and related schematic view, install doubler
P/N 3G5306P47051 on the floor panel using adhesive (C231) and one ply of fiber
glass. Fix the doubler with four rivets P/N NAS1721 C4L2P (or P/N NAS1721 C4-2P)
and let the adhesive cure.
7
Remark the floor panel as P/N 3G5306P47031 by means of permanent black ink felt
pen or by means of vibropen.
8
Install the AFT right float assembly. Refer to AMP, see OM no 39-A-95-61-04-00A720A-K.
9
Return the helicopter to flight configuration and record for compliance with this
Bollettino Tecnico on the helicopter logbook.
Page 4 of 7
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LOWER PANELASSY RH REF.
AFT FLOAT RIGHT SEMIRIGID COVERASSY REF.
REMOVE AND INSTALL WITH SAME SCREWS
VIEW LOOKING INBOARD RIGHT SIDE
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3G5306P47031 PANEL FLOOR REWORKED
FROM 3G5340A02432 AND PREViOUS
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3G5306P47031 PANEL FLOOR REWORKED
FROM 3G5340A02432 AND PREV\OUS
3G5306P47031 REF.
SECTION D-D
125.5
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3G5306P47031 REF.
3G5306P47051 DOUBLER
BOND W\TH EA9309.3NA
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SECTION C-C
3G5306P47051 REF.
ADH~IVE EA9309.3NA - \
3 5306P47031 REF.
ADHES\VE EA9309.3NA
SCHEMATIC SECTION C·C
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A Finmeccanica Company
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Prego spedire a questa indirizzo:
MODULO APPLICAZIONE BOLLETTINO TECNICO
Please send to the following address:
Data:
I Date:
TECHNICAL BULLETIN COMPLIANCE FORM
AGUSTAWESTLAND s.p.A.
CUSTOMER SUPPORT & SERVICES - ITALY
Numero:
Number:
PRODUCT SUPPORT ENGINEERING DPT.
Via del Gregge, 1 00
21015 Lonate Pozzolo (VA) - ITALY
Tel.: +39 0331 664905
Fax: +39 0331 664684
Revisione:
Revision:
Denominazione Cliente ed lndirizzo:
Telefono:
Customer Name and Address:
Telephone:
Fax:
Data Applicazione B.T.:
B. T. Compliance Date:
Modello Elicottero
Helicopter Model
S/N
Matricola
Ore Totali
Ore D.U.R.
Tail Number
Total Hours
T.S.O.
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Note:
Remarks:
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Informazion i:
Information:
AI fine di gestire le varianti alia configurazione base, in relazione all'emissione del Bollettino Tecnico, preghiamo di voler compilare il presente modulo in tutte le sue parti e spedirlo all'indirizzo sopra indicato. Si ringrazia per Ia 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.