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This text is OCR from a scan. OCR can misread letters and numbers. © Aviointeriors. Filed by the FAA in regulations.gov docket FAA-2011-1000; AD 2011-21-05 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
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AVIO
INTERIORS VENDOR SERVICE BULLETIN N° 12M/F68-06 CUSTOMER: ATR SEATS SUBJECT: BACKREST STRUCTURE WITH SLIM FITTING REPLACEMENT.
APPROVAL TABLE Prepared by Checked by Approved by REV DATE A. MANGANO D/ROSSILLI G. PERUGINI NEW 17/06/08 Manga aulu огло 1 F9/10/261 Caroa (houser REASON LEVIS PAG 10 (AEGIONN REASON REASON REASON
DISTRIBUTION LIST REV DATE SENT TO:
AVIO
INTERIORS Via Appia Km 66,400 - 04013 Tor Tre Ponti - ITALY
VENDOR SERVICE BULLETIN No. 12M/F68-06 Rev.: 1 MODEL: FUTURA FOR: 12M()()-00000)() EFFECTIVITY: REFER TO P/N LISTED IN PARA 1.A APPLICABILITY: ATR72 ATR42 ATA CMM: 25-20 SUBJECT: BACKREST STRUCTURE WITH SLIM FITTING REPLACEMENT.
COMPLIANCE: MANDATORY (For compliance time, see relevant airworthiness directive) SB 12M/F68-06 Rev. 1 Date: October 29, 2009 Page: 1
AVIO INTERIORS R
LIST OF ACTIVE PAGES PAGE REV. PAGE REV.
1 8 New 2 1 9 New New 10 1 4 New 11 New 5 New 12 New 6 New 13 New New SB 12M/F68-06 Rev. 1 Date: October 29, 2009 Page: 2
AVIO
INTERIORS
1. GENERAL INFORMATION A. APPLICABILITY:
This SB is applicable to all Seat P/N 12M the seat equipped with backrest P/N 31303300000 or 31303310000 (slim fitting or "0" marked backrest).
Note: The associated operator is given for information only.
CUSTOMER ORIGINAL SEAT P/N AIR TAHITI 12MA7-0)00()KX 12MA8-(00()KX 12MA9-()()0)(KX 12MC8-()()()()KX 12MP4-()00()KX CSA 12MA2-()000KX 12MA3-()00()KX 12MP2-()()()()KX BINTER 12MA4-0000)XR 12MA5-000()XR 12MA6-()0()()XR 12MC6-()00)()XR 12MP3-()((()XR FINNCOMM 12MC1-()()()()KX 12MC2-()()()()KX AIR MADAGASCAR 12ME1-()()()()XF 12ME2-()()()()XF 12ME3-()()()()XF 12MS3-()()()()XF AIR CALEDONIE 12MF1-0000KY 12MF2-()()()()KY 12MF3-()00)()KY 12MS4-()()()()KY KING FISHER 12MG1-()()()()XF 12MG2-()()()()XF 12MS5-()()()()XF SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 3
AVIO
INTERIORS B. PURPOSE:
Instruction to detect and replace of backrest structure with slim fitting on recline actuator side ("O" marked) with new Aluminium Backrest or reinforced Composite Backrest ("A" or "C" marked) and to re-identify Seat P/N accordingly.
C. REASON:
The aim of the SB is to prevent further failures of the seat backrest "O" marked which could result in injury to passengers or crew members during an emergency landing.
Whenever a slim backrest fitting or "O" marked backrest is detect, this SB allows to replace it with an Aluminium backrest, an "A" or a "C" marked composite backrest.
D. MANPOWER:
The operations described in this SB can be accomplished by one person in 30 minutes per backrest replacement and in 10 minutes per seat P/N change.
E. MATERIALS:
For applicable materials, see para. 2.0. herein after.
F. EQUIPMENT:
No special tools are required.
G. WEIGHT VARIATION:
Negligible.
H. COMPLIANCE TIME:
"Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). It is anticipated that the AD will confirm the (thresholds and/or intervals and/or date) given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale."
SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 4
AVIO
INTERIORS I. REFERENCE:
Not applicable.
J. REFERENCE PUBLICATIONS:
Component Maintenance Manual:
CMM 25-26-09 CSA, CMM 25-26-11 BINTER, CMM 25-26-15 AIR TAHITI, CMM 25-26-45 AIR MADAGASCAR, CMM 25-26-53 AIR CALEDONIE, CMM 25-26-43 FINNCOMM, CMM 25-26-52 KINGFISHER, K. APPROVAL:
"The modification described in this SB is classified as "minor" in regards of the ETSO requirements and is approved by Aviointeriors as the ETSO Authorization Holder in force of the privilege set in the paragraph 21A.611(a) of the European Commission Regulation (EC) no. 1702/2003 Part 21".
SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 5
AVIO
INTERIORS
2. MATERIAL INFORMATION TABLE 1: New Aluminium Backrest See Fig. 2 and Fig. 2A.
ITEM DESCRIPTION OLD P/N NEW P/N ACTION X SEAT Q.TY Backrest with recline 10 actuator on Rh side 313033000000 313952400000 Replace 2 Backrest with recline -10A 313033100000 313952500000 Replace 2 actuator on Lh side
- Item not shown TABLE 1A: Backrest Structure with reinforced Fitting See Fig. 2 and Fig. 2A.
Q.TY
ITEM DESCRIPTION OLD P/N NEW P/N ACTION X SEAT Backrest with recline 10 313033000000 3130330A0000 Replace 2 actuator on Rh side Backrest with recline -10A 313033100000 3130331A0000 Replace 2 actuator on Lh side Item not shown TABLE 1B: Backrest Structure with reinforced Composite and Fitting See Fig. 2 and Fig. 2A.
ITEM DESCRIPTION OLD P/N NEW P/N ACTION X SEAT Q.TY Backrest with recline 10 313033000000 3130330C0000 Replace 2 actuator on Rh side Backrest with recline -10A 313033100000 3130331C0000 Replace 2 actuator on Lh side Item not shown TABLE 2: Placard Information See Fig. 3 ITEM DESCRIPTION P/N ACTION X SEAT Q.TY INFO PLACARD K11181600000 Add 1 SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 6
AVIO
INTERIORS TABLE 3: SEAT P/N WITH COMPOSITE BACKREST
OLD SEAT P/N FOR NEW SEAT P/N NEW SEAT P/N
BACKREST P/N FOR BACKREST FOR BACKREST CUSTOMER 313033000000 P/N 313033A00000 P/N 313033C00000 313033100000 3130331A0000 3130331C0000 AIR TAHITI 12MA7-0000KX 12MH7-0000KX 12MJ7-0000KX 12MA8-0000KX 12MJ8-0)00(KX 12MA9-()00)(KX 12MH9-0000KX 12MJ9-0000KX 12MC8-()000KX 12ME8-0000KX 12MF8-0000KX 12MC9-()()()()KX 12ME9-()00()KX 12MF9-0)00(KX 12MP4-0000KX 12MR4-0000KX 12MR6-()00)()KX CSA 12MA2-0000KX 12MH2-()00)()KX 12MM2-0000KX 12MA3-()00(KX 12MH3-0000KX 12MM3-()0()(KX 12MP2-()000KX 12MR2-0000KX 12MT2-000()KX BINTER 12MA4-()00)()XR 12MJ4-000()XR 12MA5-0000XR 12MH5-()()0)()XR 12MJ5-()(0) ()XR 12MA6-()0()()XR 12MH6-()00)()XR 12MJ6-()()0()XR 12MC6-()000)XR 12ME6-()00(XR 12ME5-()()0)()XR 12MP3-()00(XR 12MR3-()0()()XR 12MR1-000()XR FINNCOMM 12MC1-0000KX 12ML1-0000KX 12ML3-0000KX 12MC2-()0()()KX 12ML2-0000KX 12ML4-0000KX 12MS1-0)00()KX 12MT1-0000KX 12MU1-0000KX AIR MADAGASCAR 12ME1-000()XF 12MK1-000()XF 12MK4-0)00()XF 12ME2-()()0)()XF 12MK2-0)00()XF 12MK5-()0()()XF 12ME3-()()()()XF 12MK3-()0)0)()XF 12MK6-()0()()XF 12MS3-()()()()XF 12MT3-()00()XF 12MU3-()()0)()XF AIR CALEDONIE 12MF1-0)000KY 12MF4-0000KY 12MG4-0000KY 12MF2-()0)0)()KY 12MF5-()00)()KY 12MG5-()00()KY 12MF3-()00()KY 12MF6-0000KY 12MG6-()0)()()KY 12MS4-()()00KY 12MT4-()00()KY 12MU4-0000KY KING FISHER 12MG1-()0()()XF 12MJ1-()(0()XF 12MN1-000(XF 12MG2-()()()()XF 12MJ2-()()()()XF 12MN2-(00()XF 12MS5-()()()()XF 12MT5-()000XF 12M05-()000XF SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 7
AVIO
INTERIORS TABLE 4: SEAT P/N WITH ALUMINIUM BACKREST OLD Rh & Lh New Aluminium Composite Back Backrest
CUSTOMER 313033000000 313952400000 313033100000 313952500000 AIR TAHITI 12MA7-0000KX 12M1G-()000KX 12MA8-()00()KX 12M1H-0000KX 12MA9-0000KX 12M1J-()00()KX 12MC8-()00()KX 12M1K-0000KX 12MC9-()000KX 12M1L-0000KX 12MP4-0)()()()KX 12M1X-0000KX CSA 12MA2-()0)0)()KX 12M4A-0000KX 12MA3-0000KX 12M4C-()000KX 12MP2-()0)0)()KX 12M1U-0000KX BINTER 12MA4-0000XR 12M4E-()()0)()XR 12MA5-()()()()XR 12M4F-000(XR 12MA6-()00)()XR 12M4G-()()()()XR 12MC6-0000)XR 12MM4-()00()XR 12MP3-()00()XR 12M1T-000()XR FINNCOMM 12MC1-0000KX 12M1M-0000KX 12MC2-()0()()KX 12M1N-0000KX 12MS1-000)()KX 12M1W-0000KX AIR MADAGASCAR 12ME1-0000XF 12M1P-()00)()XF 12ME2-()()0)()XF 12M1Q-()00()XF 12ME3-()00()XF 12M1R-000()XF 12MS3-()()()()XF 12M1V-(00()XF AIR CALEDONIE 12MF1-0000KY 12MF2-()()0)()KY 12M7F-0000KY 12MF3-()0)0)()KY 12M7G-()00()KY 12MS4-0000KY 12M4V-()()0)()KY KING FISHER 12MG1-()()0)()XF 12M4M-0)000XF 12MG2-()00()XF 12M4N-000()XF 12MS5-()()()()XF 12M4Y-(00()XF SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 8
AVIO INTERIORS R
3. DETECTION OF "0" MARKED COMPOSITE BACKREST Refer to Table 1, Table 1A, and Table 1B to identify the part.
a) Remove cushions covers in order to detect all "o" marked backrest and/or the slim fitting backrest.
FRONT VIEW FIGURE 1
b) If a "O" marked backrest are installed on a seat replace this backrest by a new one following the instruction shown on Para 4. Refer to Table 1 to identify the P/N of new aluminium backrest to be ordered, or Table 1A and Table 1B in case the customers have "A" or "C" composite spare backrest to recycle.
c) After backrest replacement change seat P/N following instruction on Para 5 and refer to Table 3 and Table 4 to identify the old and the new Seat P/N with aluminium or composite backrest.
Note: Fill Engineering Survey Form, attached to Para 6 of present S.B., and return to: AVIOINTERIORS Attn. Eng. Customer Support Dep., Fax +39-0773-631546.
SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 9
AVIO
INTERIORS
4. BACKREST REPLACEMENT INSTRUCTION Refer to Table 1, Table 1A, and Table1B to identify the part.
a) Remove the existing backrest (10) from the seat by loosening bolts (A)*(B)*, and recline lock by loosening bolt (C). as shown on Fig.2. Recover 10 all the attaching parts.
Note: If the customers have "A" or "C" composite spare backrest to recycle, refer to Table 1A and Table 1B in order to identify the parts. In the other case refer to Table 1 to identify new aluminium backrest P/N to be ordered.
b) Remove quadrant (D)(E) from backrest structure by loosening bolt (L) with nut recover washers (H)(F) (P).
Remove pivot (G), by means of circlips (N). Recover all the attaching parts.
See Fig 2A.
FIGURE 2
c) Install recovered quadrant (D)(E) on 10 new aluminium or composite backrest
(10), using recovered attaching parts as follows: insert pivot (G), by means M of circlips (N). Insert bolt (L) with H E washers (H)(E)(P), and fix with nut (M), P as shown on Fig 2A.
d) Install the new backrest (10) by tighten recline lock with recovered attaching parts and bolt (C)*, and lock it on the structure by bolts (A)*(B)* as shown on N Fig.2.
G
e) Follow the instruction shown on Para 5 to seat P/N change.
*TORQUE VALUE: 12 ‡ 1Nm N L FIGURE 2A SB 12M/F68-06 Rev. 1 Date: December 11, 2009 Page: 10
AVIO
INTERIORS
5. SEAT P/N CHANGE Refer to Table 3 and Table 4 to identify the Seat P/N.
a) Install the seat modification placard (X) beside the ID placard as shown in Fig.3.
b) Print the old and new seat P/N as shown on Table 3 (for Seat with Composite Backrest) and Table 4 (for Seat with Aluminium Backrest), SB number, revision and date on seat modification placard (X) by using permanent ink.
c) Apply transparent adhesive Mylar over the new placard (X) to avoid detachment.
d) Strikethrough with a line, in order to consent legible the TSO seats P/N shown on the existing Component ID placard by using permanent ink.
00000 00000 2000 8000 ID.Placard *NEROS FUTURA seat model SIDE 2.0 THIS SEAT P/N CHANGES 12M00-000000- AFT
FROM P/N TO P/N BY THE INTRODUCTION OF DATE OF MANUFACT. COMPLES WITH.
DOCUMENT No. SB 12M/F68-01 AVIOINTERIORS * DO FONG -750 - Case Ne. 1 FIGURE 3 SB 12M/F68-06 Rev. New Date: June 17, 2008 Page: 11