~) (~ '::)" AgustaWestland 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. c 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 ( 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 c 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 t Moreover, the following consumable materials are necessary to accomplish this ( 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 c 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. ( Page 3 of 7 B.T. 139-116 COMPLIANCE INSTRUCTIONS: 1. Prepare the helicopter for a safe ground maintenance. Disconnect the battery and t" (' ' 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. c 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 c n \ ~ I i__ ' ~ ~ fSTAl I i ! I ! ~ I II-------~ LOWER PANELASSY RH REF. AFT FLOAT RIGHT SEMIRIGID COVERASSY REF. REMOVE AND INSTALL WITH SAME SCREWS VIEW LOOKING INBOARD RIGHT SIDE II II II II II II II II II II II II II II II II II II II .m -1 . tXI ~ . 3G5306P47031 PANEL FLOOR REWORKED FROM 3G5340A02432 AND PREViOUS ~ CRti]-----"TT iD." c.., (I) N ~IEWB u.: w 0:: 3G5306P47031 PANEL FLOOR REWORKED FROM 3G5340A02432 AND PREV\OUS 3G5306P47031 REF. SECTION D-D 125.5 .., 3G5306P47031 REF. 3G5306P47051 DOUBLER BOND W\TH EA9309.3NA {ii c ""'CD w SECTION C-C 3G5306P47051 REF. ADH~IVE EA9309.3NA - \ 3 5306P47031 REF. ADHES\VE EA9309.3NA SCHEMATIC SECTION C·C '" AgustaWestland . ---· J -J"' A Finmeccanica Company ( 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. c Note: Remarks: c 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.
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