# Embraer Service Bulletin 145-28-0030 Copy: Revision 01 ("SB145-28-0030R1"), 28 pages: PDF https://openairdocs.org/files/sha256/ad/29/ad290a41965b45651a9ddd4a4147c84bf84b3a4371c2de1d0fcf46e932fa240a; text https://openairdocs.org/service-documents/embraer/sb-145-28-0030/file/ad290a41965b.md. Rights: © Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2015-3143; AD 2017-12-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Embraer](https://openairdocs.org/service-documents/embraer.md) - Type: Service bulletin (Service Bulletin) - Number: 145-28-0030 - Latest revision known: 145-28-0030, Revision 01, dated October 22, 2010 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/embraer/sb-145-28-0030 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2017-12-09](https://openairdocs.org/ad/2017-12-09.md), effective Jul 20, 2017: Revision 01 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/embraer/sb-145-28-0030/proposed.md). ## Text (28 pages) Rights: © Embraer S.A. Filed by the FAA in regulations.gov docket FAA-2015-3143; AD 2017-12-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 TRANSMITTAL LETTER TRANSMITTAL LETTER SB No.: 145-28-0030 PAGE: 1 of 1 1. DESCRIPTION This sheet sends Revision 01 to Service Bulletin 145-28-0030. This is a complete reissue of the Bulletin. This revision incorporates the information presented in the Information Notice related to the previous issues of this Service Bulletin, as listed below: SB145-28-0030R00-IN02. 2. ADDITIONAL ACTION Aircraft that have complied with the previous issue of this bulletin do not need any additional action. 3. RECORD OF REVISION Original issue: 01/Sep/2010. Revision 01: 22/Oct/2010. 4. HIGHLIGHTS The topics, affected pages, and a brief description of the content-related changes introduced by this revision are presented below. Revision bars are put in the left margin of each page to show the location of the significant changes. Text displacement and text format changes are not indicated. TOPIC/ PAGE DESCRIPTION OF REVISION 1. PLANNING INFORMATION A. SB EFFECTIVITY / 03 thru 05 Rearranged aircraft serial numbers into Groups 1, 2 and 3 and added Group 4. C. REASON / 06 Added reason for revision 01. D. DESCRIPTION / 07 Added Group 4. 2. MATERIAL INFORMATION C. MATERIAL NECESSARY FOR EACH AIRCRAFT / 11 and 12 Added Group 4 and updated information. 3. ACCOMPLISHMENT INSTRUCTIONS / 14 thru 16 Added Group 4. FIGURE 02 / 19 Added new information. FIGURE 04 / 22 thru 24 Added new information. ### Page 2 (No text on this page.) ### Page 3 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 1 of 24 Copyright © by EMBRAER - All rights reserved - See page 1 for details. Copyright © 2010 by EMBRAER - Empresa Brasileira de Aeronáutica S.A. All rights reserved. The informat ion, technical data, designs and drawings disclosed in this document are proprie tary information of Embraer or third parties and sh all not be used or disclosed to any third party without permission of Embraer. FUEL – INSTALLATION OF THE FUEL PUMP HARNESS CLAMP 1. PLANNING INFORMATION A. SB EFFECTIVITY Aircraft affected: MODEL SN EMB-145( ) and EMB-135( ) 145002 thru 145362, 14536 4 thru 145411, 145413 thru 145461, 145463 thru 145483, 145485 thru 145494, 145496 thru 145504, 145506 thru 145515, 145517 thru 145527, 145529 thru 145539, 145541 thru 145548, 145550 thru 145554, 145556 thru 145585, 145587 thru 145590, 145592 thru 145624, 145626 thru 145636, 145638 thru 145641, 145643, 145645 thru 145677, 145679 thru 145685, 145687 thru 145698, 145700 thru 145705, 145707 thru 145710, 145712 thru 145716, 145718 thru 145729, 145731 thru 145769, 145771 thru 145774, 145776 thru 145779, 145781 thru 145788, 145790 thru 145795, 145797 thru 14500801, 14500803 thru 14500808, 14500810 thru 14500817, 14500819 thru 14500824, 14500826 thru 14500831, 14500833 thru 14500840, 14500842 thru 14500850, 14500852, 14500853, 14500855 thru 14500862, 14500864 thru 14500866, 14500868 thru 14500872, 14500874 thru 14500879, 14500881 thru 14500883, 14500885 thru 14500890, 14500892 thru 14500900, 14500902, 14500904 thru 14500909, 14500911, 14500912, 14500914, 14500915, 14500917, 14500918, 14500920 thru 14500924, 14500926 thru 14500932, 14500934 thru 14500936, 14500938, 14500940, 14500943, 14500945, 14500947, 14500949, 14500951, 14500953, 14500956, 14500958, 14500959, 14500962, 14500964, 14500968, 14500977, 14500984, 14500987, ### Page 4 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 2 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. MODEL SN 14500992, 14500996, 14501000, 14501005, 14501009, 14501013, 14501019, 14501022, 14501024, 14501027, 14501030, 14501033, 14501036, 14501040, 14501043, 14501047, 14501050, 14501053, 14501056, 14501063, 14501077, 14501084, and 14501124. In-production effectivity: EMB-145( ) and EMB-135( ) model aircraft SN 1450105 9, 14501065, 14501068, 14501070, 14501073, 14501125, 14501129, 14501130, a nd 14501135 and on, have an equivalent modification factory-incorporated. ### Page 5 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 3 Copyright © by EMBRAER - All rights reserved - See page 1 for details. The SB effectivity is divided into 4 GROUPS of aircraft, as follows: (1) GROUP 1 MODEL SN EMB-145( ) and EMB-135( ) 145002, 145003, 145044, 1 45046, 145048, 145055, 145057 thru 145059, 145061 thru 145064, 145067 thru 145069, 145071 thru 145075, 145078 thru 145081, 145085 thru 145087, 145091 thru 145093, 145097, 145098, 145100 thru 145106, 145108 thru 145111, 145115 thru 145117, 145121 thru 145125, 145128 thru 145133, 145135, 145138 thru 145141, 145143, 145144, 145146 thru 145151, 145154, 145156, 145158 thru 145164, 145166, 145168, 145170 thru 145175, 145179 thru 145184, 145190, 145191, 145193 thru 145195, 145199, 145200, 145202, 145204, 145205, 145208, 145209, 145211 thru 145214, 145217, 145218, 145221 thru 145226, 145228, 145231 145232, 145234, 145235, 145239 thru 145242, 145246 thru 145250, 145254 thru 145265, 145268 thru 145273, 145275 thru 145279, 145281 thru 145284, 145286 thru 145289, 145291 thru 145293, 145295, 145296, 145298, 145299, 145301 thru 145307, 145309 thru 145314, 145316 thru 145318, 145321, 145323, 145326 thru 145328, 145330 thru 145332, 145334, 145338, 145340, 145341, 145343 thru 145346, 145348 thru 145356, 145358 thru 145359, 145365 thru 145374, 145377 thru 145384, 145386 thru 145389, 145391 thru 145393, 145395 thru 145397, 145399 thru 145403, 145409 thru 145411, 145413 thru 145417, 145420 thru 145430, 145432 thru 145440, 145443, 145445 thru 145449, 145451 thru 145453, 145455 thru 145457, 145459 thru 145461, 145463 thru 145465, 145468 thru 145472, 145474 thru 145481, 145483, 145485 thru 145493, 145496 thru 145498, 145500 thru 145504, 145506 thru 145515, 145517 thru 145527, 145529 thru 145539, 145541 thru 145545, 145547, 145548, 145550 thru 145554, 145557 thru 145559, 145561 thru 145572, 145574 thru 145585, 145587 thru 145590, 145592 thru 145616, 145618 thru 145624, 145626 thru 145636, 145638 thru 145641, 145643, 145645 thru 145667, 145670 thru 145677, ### Page 6 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 4 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. MODEL SN 145679 thru 145685, 145687 thru 145698, 145700 thru 145705, 145707 thru 145710, 145712 thru 145716, 145718 thru 145729, 145731 thru 145769, 145771 thru 145774, 145776 thru 145779, 145781 thru 145788, 145790 thru 145795, 145797 thru 14500801, 14500803 thru 14500808, and 14500810 thru 14500817 (aircraft with wet wingstub). (2) GROUP 2 MODEL SN EMB-145( ) and EMB-135( ) 145004 thru 145043, 145045, 145047, 145049 thru 145054, 145056, 145060, 145065, 145066, 145070, 145076, 145077, 145082 thru 145084, 145088 thru 145090, 145094 thru 145096, 145099, 145107, 145112 thru 145114, 145118 thru 145120, 145126, 145127, 145134, 145136, 145137, 145142, 145145, 145152, 145153, 145155, 145157, 145165, 145167, 145169, 145176, 145177, 145178, 145185 thru 145189, 145192, 145196, 145197, 145198, 145201, 145203, 145206, 145207, 145210, 145215, 145216, 145219, 145220, 145227, 145229, 145230, 145233, 145236 thru 145238, 145243, 145244, 145245, 145251 thru 145253, 145266, 145267, 145274, 145280, 145285, 145290, 145294, 145297, 145300, 145308, 145315, 145319, 145320, 145322, 145324, 145325, 145329, 145333, 145335, 145336, 145337, 145339, 145342, 145347, 145357, 145360, 145361, 145362, 145364, 145375, 145376, 145385, 145390, 145394, 145398, 145404, 145405, 145406, 145407, 145408, 145418, 145419, 145431, 145441, 145442, 145444, 145450, 145454, 145458, 145466, 145467, 145473, 145482, 145494, 145499, 145546, 145556, 145560, 145573, 145617, 145668 and 145669, (aircraft with dry wingstub). ### Page 7 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 5 Copyright © by EMBRAER - All rights reserved - See page 1 for details. (3) GROUP 3 MODEL SN EMB-145( ) and EMB-135( ) 14500819 thru 14500824, 14500826 thru 14500831, 14500833 thru 14500840, 14500842 thru 14500850, 14500852, 14500853, 14500855 thru 14500862, 14500864 thru 14500866, 14500868 thru 14500872, 14500874 thru 14500879, 14500881 thru 14500883, 14500885 thru 14500889, 14500892 thru 14500900, 14500902, 14500904 thru 14500909, 14500911, 14500912, 14500914, 14500915, 14500917, 14500918, 14500920 thru 14500924, 14500926 thru 14500932, 14500934 thru 14500936, 14500938, 14500940, 14500943, 14500945, 14500947, 14500949, 14500951, 14500953, 14500956, 14500958, 14500959, 14500962, 14500964, 14500968, 14500977, 14500984, 14500987, 14500992, 14500996, 14501000, 14501005, 14501009, 14501013, 14501019, 14501022, 14501024, 14501027, 14501030, 14501033, 14501036, 14501040, 14501043, 14501047, 14501050, 14501053, 14501056, 14501063, 14501077, 14501084, and 14501124, (aircraft with wet wingstub). (4) GROUP 4 MODEL SN EMB-145( ) 14500890 (aircraft with dry wingstub). B. CONCURRENT REQUIREMENTS None. ### Page 8 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 6 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. C. REASON (1) HISTORY During a scheduled maintenance inspection, evidence s of chafing between the fuel pump electrical harness and fuel pump tubes were found. The harness is composed of three protective layers, however only the first one was found damaged. (2) OBJECTIVE To attach with clamps on each fuel electric fuel pu mp harness, located in the tank collector box, to the respective pump tube. (3) EXPECTED BENEFITS This modification is intended to protect the fuel p ump harness against chafing with other parts inside the tank due to fuel movement. (4) REVISION HISTORY (a) Revision 01 This revision is issued to rearrange the aircraft s erial numbers into Groups 1 2 and 3, and add Group 4. This revision incorporates the Information Notices: SB145-28-0030R00-IN02 D. DESCRIPTION NOTE : The modification presented in this bulletin does n ot affect Fatigue Critical Structure (FCS). This Bulletin is divided into 2 PARTS, as follows: PART I Inspection of fuel pump’s electrical harness Applicable to: ALL GROUPS For GROUP 1 and 2, the modification presented in th is PART consists in doing a detailed inspection on all fuel pumps electrical ha rness in the LH/RH fuel tanks, for chaffing and, if necessary, with the fuel pump replacement. ### Page 9 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 7 Copyright © by EMBRAER - All rights reserved - See page 1 for details. To do this, it is necessary to gain access to the w ork area at LH and RH half-wing fuel tanks, by removing access panels 155BZ, 156BZ, 192AL and 192BR. For GROUP 3, the modification presented in this PAR T consists in doing a detailed inspection on the fuel pump electrical harness in t he RH fuel tank, for chaffing and, if necessary, with the fuel pump replacement. To do this, it is necessary to gain access to the w ork area at RH half-wing fuel tank, by removing access panels 156BZ and 192BR. For GROUP 4, the modification presented in this PAR T consists in doing a detailed inspection on the fuel pump electrical harness in t he RH fuel tank, for chaffing and, if necessary, with the fuel pump replacement. To do this, it is necessary to gain access to the w ork area at RH half-wing fuel tank, by removing access panels 156BZ and 192BR. PART II Fuel pump electrical harness clamps install ation Applicable to: ALL GROUPS For GROUPS 1 and 2, the modification presented in t his PART consists in the installation of two clamps to fix the fuel pump’s e lectrical harness in the LH/RH fuel tanks. To do this, it is necessary to gain access to the w ork area at LH and RH half-wing fuel tanks, by removing access panels 155BZ, 156BZ, 192AL and 192BR. For GROUP 3, the modification presented in this PAR T consists in the installation of one clamp to fix the fuel pump electrical harness in the RH fuel tank. To do this, it is necessary to gain access to the w ork area at RH half-wing fuel tank, by removing access panels 156BZ and 192BR. For GROUP 4, the modification presented in this PAR T consists in the installation of one clamp to fix the fuel pump electrical harness in the RH fuel tank. To do this, it is necessary to gain access to the w ork area at RH half-wing fuel tank, by removing access panels 156BZ and 192BR. E. COMPLIANCE (1) APPLICABLE TO PART I Embraer recommends that this bulletin be accomplish ed at next 5000FH or 24 months or at next tank opening opportunity, whichever occurs first. ### Page 10 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 8 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. (2) APPLICABLE TO PART II PART II of this bulletin may be accomplished just a fter accomplishing PART I of this bulletin. F. APPROVAL The technical aspects of this Service Bulletin are approved by: ANAC – Agência Nacional de Aviação Civil. G. ESTIMATED MANPOWER This estimate is for direct labor only, performed b y experienced personnel, and does not include the time to plan, prepare, or inspect the work. It is assumed that all the tools, parts, and other means are readily available when necessary. This estimate does not include the sealant, paint, or adhesive curing time. (1) APPLICABLE TO PART I - Access opening: 3.0 man-hours. - Inspection: 1.0 man-hour. - Modification: None. - Access closure: 1.2 man-hours. - Test: 1.0 man-hour. NOTES: 1) The overall manpower required will be increased in 1.0 man-hour for each fuel pump replaced, in case of any discrepancy is detected. 2) These estimates do not include the time necessar y to defuel the tanks. 3) These estimates include the time necessary to ac complish LH and RH half-wing. ### Page 11 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 9 Copyright © by EMBRAER - All rights reserved - See page 1 for details. (2) APPLICABLE TO PART II - Access opening: 1.0 man-hour. - Inspection: None. - Modification: 2.0 man-hours. - Access closure: 1.2 man-hours. - Test: None. NOTE: 1) These estimates do not include the time nec essary to defuel the tanks. H. WEIGHT AND BALANCE None. I. REFERENCES AMM-145/( ) – Aircraft Maintenance Manual – Chapter 06-41-01 - Dimensions and Areas. AMM-145/( ) – Aircraft Maintenance Manual – Chapter 12-11-02 - Servicing. AMM-145/( ) – Aircraft Maintenance Manual – Chapter 28-00-00, 28-21-01, 28-11-01 and 28-45-00 - Fuel. J. OTHER PUBLICATIONS AFFECTED AMM-145/( ) – Aircraft Maintenance Manual – Chapter 28-21-01 - Fuel. IPC-145/( ) – Illustrated Parts Catalog - Chapter 2 8-21-00 - Fuel. ### Page 12 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 10 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. 2. MATERIAL INFORMATION A. MATERIAL – PRICE AND AVAILABILITY (1) MATERIAL AVAILABLE FROM EMBRAER None. (2) MATERIAL AVAILABLE FROM OTHER VENDORS None. B. INDUSTRY SUPPORT INFORMATION None. C. MATERIAL NECESSARY FOR EACH AIRCRAFT When applicable, the use of alternative or similar parts in place of the ones specified in the kit is allowable, provided that these altern ative or similar parts are approved by Embraer as indicated in the related Embraer Technic al Publications or through a formal Embraer communication channel. The expendable or consumable parts presented in the AMM Tasks referred to in this bulletin, which are necessary for its accomplishmen t, should be procured from the operator's inventories or ordered as spares. The complementary information, when necessary, is p resented as Notes in the respective Table. (1) TOP KITS AND KITS None. ### Page 13 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 11 Copyright © by EMBRAER - All rights reserved - See page 1 for details. (2) MATERIAL TO BE PROCURED (a) PARTS 1 Applicable to PART I The existing fuel pump should be replaced with a ne w one bearing same PN, in case of any discrepancy is detected during the accomplishment of PART I. This fuel pump should be procured from the operator inventories, or ordered as spares from Embraer. 2 Applicable to PART II The parts below should be procured from the operator’s inventories or from a local supplier. a) Parts applicable to GROUP 1 NEW PN DESCRIPTION OLD PN QTY DISP/ Notes H14-08 NUT - 4 2 MS21919WDF16 CLAMP - 4 2 MS21919WDF3 CLAMP - 4 2 NAS1149CN816R WASHER - 4 2 PE21107-2-8 SCREW - 4 2 b) Parts applicable to GROUP 2 NEW PN DESCRIPTION OLD PN QTY DISP/ Notes H41-08 NUT - 6 2 MS21919WDF16 CLAMP - 6 2 MS21919WDF3 CLAMP - 6 2 NAS1149DN816K WASHER - 6 2 PE21107-2-8 SCREW - 6 2 ### Page 14 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 12 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. c) Parts applicable to GROUP 3 NEW PN DESCRIPTION OLD PN QTY DISP/ Notes H14-08 NUT - 1 2 MS21919WDF16 CLAMP - 1 2 MS21919WDF3 CLAMP - 1 2 NAS1149CN816R WASHER - 1 2 PE21107-2-8 SCREW - 1 2 d) Parts applicable to GROUP 4 NEW PN DESCRIPTION OLD PN QTY DISP/ Notes H41-08 NUT - 1 2 MS21919WDF16 CLAMP - 1 2 MS21919WDF3 CLAMP - 1 2 NAS1149DN816K WASHER - 1 2 PE21107-2-8 SCREW - 1 2 (b) CONSUMABLES None. DISPOSITION : 2 = Incorporate part bearing NEW PN D. MATERIAL NECESSARY FOR EACH SPARE None. E. KIT EVOLUTION None. ### Page 15 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 13 Copyright © by EMBRAER - All rights reserved - See page 1 for details. F. KIT UPDATING None. G. REIDENTIFIED PARTS None. H. TOOLING – PRICE AND AVAILABILITY Whenever required, the tooling presented in the AMM Tasks referred to in this bulletin, should be procured from the operator’s inventories or ordered as spares. ### Page 16 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 14 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. 3. ACCOMPLISHMENT INSTRUCTIONS NOTES : 1) For the purpose of this Service Bulletin, a Det ailed Inspection (DI) is: “An intensive examination of a specific item, installat ion or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensi ty deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access pr ocedures may be required. 2) Obey all of the WARNINGS and CAUTIONS included i n the referenced manuals and procedures. 3) The Manuals and other documents are referred to by means of acronyms or using a simplified form. Refer to section “1. I. REFERENCES” for a more complete definition. 4) This Service Bulletin effectivity is divided int o 04 aircraft GROUPS according to the relevant configuration. REFERENCE APPLICATION TABLE Aircraft GROUP APPLICABLE FIGURES 1 1 and 3 2 and 4 2 and 4 3 1 and 3 The steps below outline the general accomplishment instructions. The detailed sequence is included in the respective figure, when necessary. A. Make sure that the aircraft is safe for mainte nance. WARNING : BEFORE YOU DO THE TASK, OBEY THE SAFETY PRECAUTIONS GIVEN IN AMM 28-00-00/201 TO PREVENT INJURY TO PERS ONS AND DAMAGE TO MATERIAL. B. De-fuel the tank. Refer to the applicable AMM 12-11-02 (TASK 12-11-01-600-802- A) – Servicing. (1) For GROUPS 1 and 2, de-fuel the LH and RH tanks . (2) For GROUP 3 and 4, de-fuel only the RH tank. ### Page 17 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 15 Copyright © by EMBRAER - All rights reserved - See page 1 for details. C. Make sure that the GPU pushbutton, on the overhe ad panel, is set at OFF. D. Place a DO-NOT-SET-TO-ON tag on the GPU pushbutt on. E. Make sure that the BATT 1 and BATT 2 switches, o n the overhead panel, are set at OFF. F. Place DO-NOT-SET-TO-AUTO tags on the BATT 1 and BATT 2 switches. G. Set the BACKUP pushbutton, on the overhead panel , to OFF. H. Place a DO-NOT-SET-TO-AUTO tag on the BACKUP pus hbutton. I. Open access, as follows: (1) For GROUP 1, open panels 155BZ, 156BZ, 192AL an d 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-000-801-A) – Fuel-Tank Access Panels – Removal. Refer to the applicable AMM 06-41 -01 – Dimensions and Areas. (2) For GROUP 2, open panels 155BZ, 156BZ, 192AL an d 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-000-802-A) – Fuel-Tank Access Panels – Removal. Refer to the applicable AMM 06-41 -01 – Dimensions and Areas. (3) For GROUP 3, open panels 156BZ and 192BR accord ing to the applicable AMM 28-11-01 (TASK 28-11-01-000-801-A) – Fuel-Tank Access Panel – Removal. Refer to the applicable AMM 06-41-01 – Dimensions and Areas (4) For GROUP 4, open panels 156BZ and 192BR accord ing to the applicable AMM 28-11-01 (TASK 28-11-01-000-802-A) – Fuel-Tank Access Panels – Removal. Refer to the applicable AMM 06-41-01 – Dimensions and Areas J. Applicable to PART I (1) Applicable to GROUP 1, GROUP 3 (a) Inspect the fuel pump electrical harnesses look ing for chafing signs. Refer to Figure 1 and AMM 28-21-01 (TASK 28-21-01-200-803-A) – Electric Fuel Pump - Inspection/Check . (b) If any discrepancy is found, replace the affect ed electrical pump with new one bearing same PN. Refer to AMM 28-21-01 (TASK 28 -21-01-000-801- A for removal, and TASK 28-21-01-400-801-A for inst allation) – Electric Fuel Pump. See Figure 1. ### Page 18 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 16 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. Applicable to GROUP 2 and GROUP 4 (c) Inspect the fuel pump electrical harnesses look ing for chafing signs. Refer to Figure 2 and AMM 28-21-01 (TASK 28-21-01-200-804-A) – Electric Fuel Pump - Inspection/Check. (d) If any discrepancy is found, remove the affecte d electrical pump with new one bearing same PN. Refer to AMM 28-21-01 (TASK 28 -21-01-000-802- A for removal and TASK 28-21-01-400-802-A for insta llation) – Electric Fuel Pump. See Figure 2. K. Applicable to PART II (1) Applicable to ALL GROUPS a) Install the clamps of fuel pump electrical harne ss according to Figure 3 or Figure 4, as applicable. L. For GROUP 1, close access panel 155BZ, 156BZ, 19 2AL and 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-400-801- A) – Fuel-Tank Access Panels – Installation. Refer to the applicable AMM 06-41-01 – Dimensions and Areas M. For GROUP 2, close access panel 155BZ, 156BZ, 19 2AL and 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-400-802- A) – Fuel-Tank Access Panels – Installation. Refer to the applicable AMM 06-41-01 – Dimensions and Areas. N. For GROUP 3, close access panels 156BZ and 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-400-801-A) – Fuel-Tank Access Panels – Installation. Refer to the applicable AMM 06-41-01 – Dimensions and Areas. O. For GROUP 4, close access panel 156BZ and 192BR according to the applicable AMM 28-11-01 (TASK 28-11-01-400-802-A) – Fuel-Tank Access Panels – Installation. Refer to the applicable AMM 06-41-01 – Dimensions and Areas P. Remove the DO-NOT-SET-TO-AUTO tag from the BACKU P pushbutton. Q. Set the BACKUP pushbutton, on the overhead panel , to AUTO. R. Remove the DO-NOT-SET-TO-AUTO tags from the BATT 1 and BATT 2 switches. S. Remove the DO-NOT-SET-TO-ON tag from the GPU pus hbutton. T. Re-refuel the tank. Refer to the applicable AMM 12-11-02 (TASK 12-11-01-600- 801-A) – Servicing. ### Page 19 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 17 Copyright © by EMBRAER - All rights reserved - See page 1 for details. U. Examine the access panels which were removed for fuel leakage. Correct as necessary. V. Carry out the Fuel Low – Pressure Warning System - operational test as given in the applicable AMM 28-45-00 (TASK 28-45-00-700-801- A) – Fuel Low-Pressure Warning System – Operational Check. W. Restore the aircraft to the normal condition. X. Enter the accomplishment of PART I and PART II t his bulletin in the applicable documents. NOTES : 1) Please inform us by e-mail fleet.reliability@em braer.com.br of the aircraft manufacturer serial number and the SB incorporation date, specifying the SB Part(s) incorporated or whether the whole SB has been incorporated. This will enable Embraer to consider your aircraft configuration when providing future modifications. 2) To formally inform that the SB has been incorpor ated fleetwide or that the SB will not be incorporated, so that Embraer can up date the affected technical publications, use the “Service Bulletin F ull-Fleet Incorporation Report” form, which is available on the Flyembraer portal (http://www.flyembraer.com ). 3) Use the attached “Service Bulletin Evaluation” f orm to send us your comments regarding this SB. Your feedback will be m uch appreciated as an aid for us to improve the quality of the SBs. ### Page 20 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 18 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. DET. B DET. A B B A ZONES 155 156 157 FUEL PUMP HARNESS (INSPECT) 1 REPLACE THE FUEL PUMP WITH PART BEARING SAME PN, IF NECESSARY. 1 FUEL PUMP HARNESS (INSPECT) 1 2 3 2 APPLICABLE TO GROUP 1. APPLICABLE TO GROUP 3. 2 3 EM145SB280617B.DGN STGR 1 STGR 2 STGR 3 STGR 4 STGR 5 STGR 6 STGR 7 STGR 8 STGR 9 STGR 10 STGR 11 SPAR II X=15315 STUB SPAR I X=13601 STUB FUEL PUMP 2C (REF.)FUEL PUMP 2A(REF.) FUEL PUMP 2B (REF.) P0214 (REF.) P1978 (REF.) APPLICABLE TO GROUP 1 AND GROUP 3 FIGURE 1: INSPECTION OF FUEL PUMP’S ELECTRICAL HARNESS (SHEET 01 OF 01) ### Page 21 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 19 Copyright © by EMBRAER - All rights reserved - See page 1 for details. FUEL PUMP 1A (LH) FUEL PUMP 2A (RH) (REF.) FUEL PUMP 1B (LH) FUEL PUMP 2B (RH) (REF.) EXISTING FUEL PUMP (REPLACE, IF NECESSARY) DET. B C 1 FUEL PUMP HARNESS (INSPECT) DET. A B A A ZONE 531 ZONE 631 LEFT SIDE SHOWN RIGHT SIDE OPPOSITE 1 REPLACE THE FUEL PUMP WITH PART BEARING SAME PN, IF NECESSARY. APPLICABLE TO GROUP 2. APPLICABLE TO GROUP 4. 2 3 3 2 2 2 FUEL PUMP 1C (LH) (REF.) FUEL PUMP 2C (RH) (REF.) 2 EM145SB280618C.DGN APPLICABLE TO GROUP 2 AND GROUP 4 FIGURE 2: INSPECTION OF FUEL PUMP’S ELECTRICAL HARNESS (SHEET 01 OF 01) ### Page 22 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 20 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. DET. A A ZONES 155 156 157 C B FUEL PUMP 2A (REF.) FUEL PUMP 2C (REF.) FUEL PUMP 2B (REF.) P1978 (REF.) P0214 (REF.) P1976 (REF.) P1974 (REF.) DET. B D D F F EM145SB280619B.DGN STGR 1 STGR 2 STGR 3 STGR 4 STGR 5 STGR 6 STGR 7 STGR 8 STGR 9 STGR 10 STGR 11 SPAR II X=15315 STUB SPAR I X=13601 STUB APPLICABLE TO GROUP 1 AND GROUP 3 FIGURE 3: INSTALLATION OF FUEL PUMP ELECTRICAL HARNESS CLAMPS (SHEET 01 OF 02) ### Page 23 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 21 Copyright © by EMBRAER - All rights reserved - See page 1 for details. FUEL PUMP 1A (REF.) FUEL PUMP 1B (REF.) FUEL PUMP 1C (REF.) P1975 (REF.) P1977 (REF.) D D DD TYPICAL DET. EDET. D E CLAMP PN MS21919WDF3 CLAMP PN MS21919WDF16 SCREW PN PE21107−2−8 WASHER PN NAS1149CN816R NUT PN H14−08 (INSTALL) P1979 (REF.) P0213 (REF.) 1 1 KEEP THE MINIMUM SEPARATION OF 10MM BETWEEN FUEL TUBES AND WIRES. DET. C APPLICABLE TO GROUP 1. APPLICABLE TO GROUP 3. 2 3 2 3 EM145SB280620B.DGN 2 DET. F STGR 1 STGR 2 STGR 3 STGR 4 STGR 5 STGR 6 STGR 7 STGR 8 STGR 9 STGR 10 STGR 11 SPAR II X=15315 STUB SPAR I X=13601 STUB APPLICABLE TO GROUP 1 AND GROUP 3 FIGURE 3: INSTALLATION OF FUEL PUMP ELECTRICAL HARNESS CLAMPS (SHEET 02 OF 02) ### Page 24 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 22 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. FUEL PUMP 1A (LH) FUEL PUMP 2A (RH) (REF.) FUEL PUMP 1B (LH) FUEL PUMP 2B (RH) (REF.) DET. B D C DET. A B A A ZONE 531 ZONE 631 LEFT SIDE SHOWN RIGHT SIDE OPPOSITE APPLICABLE TO GROUP 2. APPLICABLE TO GROUP 4. 1 2 1 2 1 1 FUEL PUMP 1C (LH) (REF.) FUEL PUMP 2C (RH) (REF.) 1 EM145SB280621D.DGN APPLICABLE TO GROUP 2 AND GROUP 4 FIGURE 4: INSTALLATION OF FUEL PUMP ELECTRICAL HARNESS CLAMPS (SHEET 01 OF 03) ### Page 25 SERVICE BULLETIN DATE: 01/Sep/2010 SB No.: 145-28-0030 REVISION No.: 01 – 22/Oct/2010 PAGE: 23 Copyright © by EMBRAER - All rights reserved - See page 1 for details. E F DET. C CLAMP PN MS21919WDF3 CLAMP PN MS21919WDF16 SCREW PN PE21107−2−8 WASHER PN NAS1149DN816K NUT PN H41−08 (INSTALL) DET. D KEEP THE MINIMUM SEPARATION OF 10MM BETWEEN FUEL TUBES AND WIRES. 1 APPLICABLE TO GROUP 2. APPLICABLE TO GROUP 4. 1 2 3 3 FUEL PUMP 1C (LH) (REF.) FUEL PUMP 2C (RH) (REF.) 1 2 FUEL PUMP 1C (LH) (REF.) FUEL PUMP 2C (RH) (REF.) 1 21 EM145SB280622C.DGN APPLICABLE TO GROUP 2 AND GROUP 4 FIGURE 4: INSTALLATION OF FUEL PUMP ELECTRICAL HARNESS CLAMPS (SHEET 02 OF 03) ### Page 26 SERVICE BULLETIN SB No.: 145-28-0030 DATE: 01/Sep/2010 PAGE: 24 REVISION No.: 01 – 22/Oct/2010 Copyright © by EMBRAER - All rights reserved - See page 1 for details. DET. F DET. E FUEL PUMP 1B (LH) FUEL PUMP 2B (RH) (REF.) CLAMP PN MS21919WDF3 CLAMP PN MS21919WDF16 SCREW PN PE21107−2−8 WASHER PN NAS1149DN816K NUT PN H41−08 (INSTALL) FUEL PUMP 1A (LH) FUEL PUMP 2A (RH) (REF.) CLAMP PN MS21919WDF3 CLAMP PN MS21919WDF16 SCREW PN PE21107−2−8 WASHER PN NAS1149DN816K NUT PN H41−08 (INSTALL) 1 KEEP THE MINIMUM SEPARATION OF 10MM BETWEEN FUEL TUBES AND WIRES. 3 3 1 APPLICABLE TO GROUP 2. 3 1 EM145SB280623B.DGN APPLICABLE TO GROUP 2 AND GROUP 4 FIGURE 4: INSTALLATION OF FUEL PUMP ELECTRICAL HARNESS CLAMPS (SHEET 03 OF 03) ### Page 27 ... SERVICE BULLETIN EVALUATION THE PURPOSE OF THIS FORM IS TO COLLECT DATA THAT WI LL BE USED TO IMPROVE THE QUALITY OF OUR SERVICE BULLETINS AND UPDATE THE TECHNICAL PUBLICATION. PLEASE FILL IN FORM AND RETURN IT TO: EMBRAER – EMPRESA BRASILEIRA DE AERONÁUTICA S.A. TECHNICAL PUBLICATIONS AV. BRIG. FARIA LIMA, 2170 SÃO JOSÉ DOS CAMPOS - SP - 12227-901 BRASIL Fax: ++ 55 12 3927-7546 e-mail: service.bulletin@embraer.com.br SB Title: SB: (Number / Rev.) Operator: Aircraft serial number affected: (per SB effectivity list) PRE-ACCOMPLISHMENT EVALUATION: (check applicable squares below) [ ] WILL BE ACCOMPLISHED ON FIRST A/C [ ] WILL BE ACCOMPLISHED AS REQUIRED [ ] WILL BE ACCOMPLISHED ON FLEET [ ] DECISION DEFERRED (Explain below) [ ] UNECONOMICAL [ ] SERVICE EXPERIENCE DOES NOT JUSTIFY [ ] OPERATIONAL ENVIRONMENT DOES NOT JUSTIFY [ ] WILL NOT BE ACCOMPLISHED: [ ] OTHER (Explain below) POST-ACCOMPLISHMENT EVALUATION: (Check applicable squares below) ESTIMATED MANPOWER: [ ] OK [ ] NOT OK (Explain below) MATERIAL & KITS: [ ] OK [ ] NOT OK (Explain below) ACCOMPLISHMENT INSTRUCTIONS: [ ] OK [ ] NOT OK (Explain below) FIGURES: [ ] OK [ ] NOT OK (Explain below) SB GENERAL EVALUATION: [ ] OK [ ] NOT OK (Explain below) COMMENTS: (Bulletin quality/ Difficulties found at the time of incorporation/ Suggested improvements/ Other) Organization: Fax: Phone: E-mail: Address: Prepared by: (Name/ Title) Date: ENS-003393 ### Page 28 (No text on this page.) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.