# Fokker Service Bulletin SBF28-28-059: Revision 1 - Rights: © Fokker. Filed by the FAA in regulations.gov docket FAA-2015-1982; AD 2015-26-05 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Fokker Service Bulletin SBF28-28-059](https://openairdocs.org/service-documents/fokker/sbf28-28-059.md) - Title as filed: FAA-2015-1982_Appendix SB_SBF28-28-059_APP01 - FOKKER - Pages: 27 - PDF: https://openairdocs.org/files/sha256/1b/98/1b98f059a7401a3aed70a3b71e7815feb6cf078d1b96271f9020bfa7e4b4e6ae - Page: https://openairdocs.org/service-documents/fokker/sbf28-28-059/file/1b98f059a740 ## 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) Fokker Service Bulletin Fokker Services B.V. F28 Appendix SB SBF28-28-059/APP01 Revision - FUEL - GENERAL Installation of additional Bonding Provisions Outside the Fuel Tank Prepared Function / Note Date scheidema-ps04192 Jun 19/14 Colleague Check blay barba-mb00609 FS-TECH Jun 24/14 Manager Final Approval groot-jg01801 FS-TECI Jul 15/14 Office of Airworthiness Approval visser-hv01800 FS-TW Jul 15/14 Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker production or disclosure i prior written permission of Fokker S EASA approved procedure for electronic sign-off ### Page 2 (OCR) tokker Service Bulletin Fokker Services B.V. 1. General Information A. General (1) This Service Bulletin Appendix supersedes steps B. and J. of the accomplishment instructions of Service Bulletin SBF28-28-026. FUEL "This Service Bulletin is associated with the Fuel Tank Safety Program" Fuel System - Introduction of Improved Bonding Provisions Outside the Fuel Tanks. B. Table of Contents • Section 1: General Information Section 2: Planning Information • Section 3: Material Information Section 4: Accomplishment Instructions • Service Bulletin Quality Reporting Form and attachments: • List of drawings • Required drawings C. Service Bulletin Revision History Revision Date (Mmm dd/yy) Reason for Revision Refer to footer First Release Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Ceproduction or discosure do ted paris of this document any part thered of the ten any no matie dontained een for purposes other t lect to the provisions of an agreemer Reproduction or disclosure to third parties of this document or any part thereof, or the us d agreement, is not permitted except with the prior written permission of Fokker services BiV Page 1 of 26 ### Page 3 (OCR) okker Service Bulletin Fokker Services B.V. 2. Planning Information A. Effectivity (1) F28 Mark 1000 through 4000 aircraft serial number(s): 11003 thru 11241, 11991 and 11992. (2) Production version of this change: Not applicable. B. Concurrent Requirements (1) Not applicable. C. Reason (1) The design review of the F28 Mk 1000 thru 4000 fuel system, in accordance with the guidelines related to FAA SFAR 88 and JAA INT/POL/25/12, revealed that an unsafe condition may develop in the wing tanks because no controlled bonding provisions are present on a number of critical locations, outside the Fuel Tank or connected to the Fuel Tank Wall. (2) This Service Bulletin gives instructions for the introduction of additional electrical bonding provisions that do not require opening of the fuel tanks access panels. D. Description (1) This Service Bulletin Appendix is divided in four (4) Parts as follows: Part 1: Installation of Improved Bonding Provisions for: Fuel Quantity Tank Unit (FQTU) no.7 mounting flange. (Applicable to Aircraft Serial Numbers 11003 thru 11241, 11991 and 11992 in POST SBF28-57-098 configuration) NOTE: For aircraft PRE SBF28-57-098, the FQTU no. 7 mounting flange bonding is included in SBF28-28-058. - FQTU no. 7 attachment screws. (Applicable to Aircraft Serial Numbers 11003 thru 11241, 11991 and 11992 in POST SBF28-57-098 configuration) NOTE: For aircraft PRE SBF28-57-098, the FQTU no. 7 attachment screws bonding is included in SBF28-28-058. This Part tells you how to: • Remove FQTU no.7. • Rework and prepare the bonding surfaces at two (bolt) locations. • Apply of a finish on the mounting flange. • Install FQTU no.7. Status: Revision: Released date: (Mmm ddly) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Sen Is). This document has been s ses B.V. to its custome 1s of an agreeme Reproduction or disclosure to third parties of this doc t thereof, or the use of any information co for purposes other than expli d by the aforesaid agreement, is not permitted exce Page 2 of 26 ### Page 4 (OCR) Yokker Service Bulletin Fokker Services B.V. Part 2: Installation of Improved Bonding Provisions for Refueling Line. (Applicable to Aircraft Serial Numbers Mark 1000: 11003 thru 11061, 11991 and 11992 in PRE SBF28-28-026 configuration, and Mark 2000: 11053 in PRE SBF28-28-026 configuration) This Part tells you how to: • Install bonding clamp at four locations • Rework and prepare the bonding surfaces at four (screw) locations. Part 3: Installation of Improved Bonding Provisions for Suction Relief Valve line. (Applicable to Aircraft Serial Numbers 11016 thru 11061, 11991 and 11992, in POST SBF28-28-020 configuration, and Aircraft Serial Numbers 11062 thru 11241 if equipped with Center Wing Tanks) This Part tells you how to: • Install bonding clamp at one location. • Rework and prepare the bonding surfaces at two (screw) locations. Part 4: Installation of Improved Bonding Provisions for Boost Pump attachment screws. (Applicable to Aircraft Serial Numbers 11003 thru 11241, 11991 and 11992) This Part tells you how to: • Rework and prepare the bonding surfaces at two (bolt) locations. NOTE Incorporation of this Service Bulletin is only complete when all Parts are incorporated. (2) This Service Bulletin Appendix supersedes steps B. and J. of the accomplishment instructions of Service Bulletin SBF28-28-026. E. Compliance (1) Recommended Fokker Services recommends the accomplishment of Part 1 thru Part 4 of the Service Bulletin Appendix at the same time within 2 years (24 months) after the date of issue (January 9th, 2014) of the Proforma of this Service Bulletin. NOTE: EASA Airworthiness Directive 2014-0109 has been issued with respect to this subject. Refer to the EASA website for details on this AD. F. Approval (1) The technical content of this document is approved under the authority of DOA ref. EASA.21J.059. Status: Revision: Released date: (Mmm ddly) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands) This document has been supplied by Fokk • Services B.V. to its customers or ubject to the provisions of an agreeme Reproduction or disclosure to third parties of this document or any part thereof, or the use of any info erein for purposes other than ex id agreement, is not permitted exce with the prior written permission of Fokker Services B.V. Page 3 of 26 ### Page 5 (OCR) fokker Service Bulletin Fokker Services B.V. G. Manpower (1) Approximately 5 man-hours are necessary to do Part 1 of this Service Bulletin Appendix on one aircraft. This table of manpower will help you to schedule and do this Service Bulletin Appendix: Instructions Men Man-hours Elapsed time (hours) Removal 2 0.6 0.3 Modification 2 3.8 1.9 Inspection Installation 2 0.6 0.3 Testing Total 5.0 2.5 NOTE: This estimate does not include the time necessary: for the paint to dry and/or the sealant to cure. (2) Approximately 5 man-hours are necessary to do Part 2 of this Service Bulletin Appendix on one aircraft. This table of manpower will help you to schedule and do this Service Bulletin Appendix: Instructions Men Man-hours Elapsed time (hours) Removal 1 1.0 1.0 Modification 1 3.0 3.0 Inspection Installation 1 1.0 1.0 Testing Total 5.0 5.0 NOTE: This estimate does not include the time necessary: for the paint to dry and/or the sealant to cure. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confiden basis subject to the provisions of an agreement Reproduction or disclosure to third parties of this document or any part thereof, or the use of any info tained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted excep with the prior written permission of Fokker Services B.V. Page 4 of 26 ### Page 6 (OCR) Yokker Service Bulletin Fokker Services B.V. (3) Approximately 3 man-hours are necessary to do Part 3 of this Service Bulletin Appendix on one aircraft. This table of manpower will help you to schedule and do this Service Bulletin Appendix: Instructions Men Man-hours Elapsed time (hours) Removal 1 0.6 0.6 Modification 1.8 1.8 Inspection Installation 0.6 0.6 Testing Total 3.0 3.0 NOTE: This estimate does not include the time necessary: for the paint to dry and/or the sealant to cure. (4) Approximately 3 man-hours are necessary to do Part 4 of this Service Bulletin Appendix on one aircraft. This table of manpower will help you to schedule and do this Service Bulletin Appendix: Instructions Men Man-hours Elapsed time (hours) Removal 0.6 0.6 Modification 1.8 1.8 Inspection Installation 1 0.6 0.6 Testing Total 3.0 3.0 NOTE: This estimate does not include the time necessary: for the paint to dry and/or the sealant to cure. (5) The estimated hours are for direct labor done by experienced personnel. They are calculated based on the conditions given in SBF28-00-001 (Service Bulletin Introduction, section 2.C., "Manpower"). H. Weight and Balance (1) For Part 1 of this Service Bulletin: Weight change: None. Index change: None. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokke tent of any part thered of the use of any in main don ander ten for ply to the the scol al basis subject to the provisions of an agreement ained therein for purposes other than exp lowed by the aforesaid agreement, is not permitted excep with the prior written permission of F Page 5 of 26 ### Page 7 (OCR) tokker Service Bulletin Fokker Services B.V. (2) For Part 2 of this Service Bulletin: Weight change: + 0.55 kg (1.21 lb). Index change: - 0.001. (3) For Part 3 of this Service Bulletin: Weight change: + 0.32 kg (0.71 lb). Index change: - 0.007. (4) For Part 4 of this Service Bulletin: Weight change: None. Index change: None. 1. Electrical Load Data (1) Direct Current (DC) Loads: (a) Not changed. (2) Alternating Current (AC) Loads: (a) Not changed. J. Software Accomplishment Summary (1) Not applicable. K. References (1) F28 Maintenance Manual (MM) F28 Illustrated Parts Catalog (IPC) Fokker Standards & Process Manual (SPM) F28 Structural Repair Manual (SRM) EASA Airworthiness Directive 2014-0109 F28 Service Bulletin (SB): - SBF28-28-026 - SBF28-28-050 SBF28-28-058 - SBF28-57-098 Fokker drawing(s): refer to attachment "List of drawings" Fokker internal reference: - ECR 015105. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Se hed by ne ran for pur to star than explay loved ey bastard a he pot i not pen tod except. Reproduction or disclosure to third parties of this doc with me pror written permission or roker services o Page 6 of 26 ### Page 8 (OCR) fokker Service Bulletin Fokker Services B.V. L. Publications Affected (1) This Service Bulletin Appendix affects the publications listed below: (a) Maintenance Documentation - Fokker F28 Maintenance Manual (MM) - chapter 28-00 - chapter 28-14 - chapter 28-22 - chapter 28-41 - Fokker F28 Illustrated Parts Catalog (IPC) - chapter 28-10 - chapter 28-20 - chapter 28-40 NOTE: Manual Change Notification MCNM F28-044 will be published before September 15, 2014. We do not plan to issue a revision of this Service Bulletin Appendix when the MCNM is published. For preliminary MCNM information, if required, please contact Fokker (b) Maintenance Programs - Fokker F28 Customized Maintenance Program (CMP) NOTE: The affected maintenance program change is described in the paragraph Special Instructions for Continued Airworthiness (ICA). Special Instructions for Continued Airworthiness (ICA) The effect of this Service Bulletin Appendix on the special ICA is as follows: NO - Electrical Wiring Interconnection System (EWIS) - Fuel Tank Safety (FTS) NOTE: Existing Fuel ALI items 280000-02 and 280000-08 and CDCCL items 4 and 5 (refer to SBF28-28-050 revision 2 or subsequent revision) are effective and not affected After accomplishment of this Service Bulletin Appendix change the instructions in MM tasks 28-00, 28-14, 28-22 and 28-41, in accordance with the instructions in MCNM-F28-044. (c) Operational Documentation Not affected. (2) Report to Fokker Services that this Service Bulletin Appendix has been carried out on the applicable aircraft. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Ne -okker Services B.V. to its c ect to the provisions of an agreement Reproduction or disclosure to third parties of this document or any part thereof, or the use of any into so were ior purposes other than a with the pror writen permission or rokker services bes Page 7 of 26 ### Page 9 (OCR) okker Service Bulletin Fokker Services B.V. (3) You have the possibility to send your SB feedback to Fokker Services perService Bulletin Reporting Quality Form". This form is located on the last Service Bulletin Appendix page. (4) For incorporation of this Service Bulletin Appendix in your documentation refer to SBF28-00-001 (Service Bulletin Introduction, section 4 "Incorporation of Service Bulletins in Documentation of Fokker Services"). (5) Accomplishment of this Service Bulletin Appendix is only complete with incorporation of the manual change(s), per the ref MCNM/MCNO, Temporary Revision (if applicable) or General Revision. M. Interchangeability or Intermixability of Parts (1) The interchangeability of the parts is as follows: New Part Number Keyword Old Part Number Interchangeability FON2-3306-05010 Washer (cupal) FON2-3306-5A One-way MS21919WDE28 Clamp FON2-7313-28 One-way MS21919WDE18 Clamp FON2-7313-18 One-way Status: Revision: Released date: (Mmm ddly) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 ### Page 10 (OCR) Fokker Service Bulletin Fokker Services B.V. 3. Material Information A. Material - Price and Availability (1) You can order the necessary parts against list price. B. Material Required (1) These parts, which are necessary to complete this Service Bulletin on 1 aircraft, are not part of the mod kit. New Part Number Qty +3 * Keyword Info Old Part Number Instructions/ Disposition AN3-4A " AN735-D16 2 - 2 Clamp Screw Local source Local source AN735-D18 1 2 Clamp Local source AN735-D28 1 4 2 Clamp Local source AS3578-137 2 2 2 O-Ring Local source FON2-3306-05010 2 Washer Cupal Local source FON2-3306-5A 1 4 4 Washer Cupal Local source FON2-7313-18 " 2 Clamp Local source FON2-7313-28 1 6 4 Clamp Local source FON9-1901C80C 1 4 2 Lead Local source FON9-1901C100C 1 2 Lead Local source FON9-1901C200C 2 Lead Local source MS21042-L3 2 Nut Local source MS27039-1-07 1) 4 4 Screw Local source MS27039-1-09 1 4 Screw Local source NAS1100-3-8 2 Screw Local source NAS1291-3" 4 Nut Local source NAS1133-3 2 Screw Local source NAS1581C3T6 4 4 Screw Local source NAS1149D0332K 6 Washer Local source NAS1291-3 1 2 Nut Local source NAS1252-10L " 10 12 Washer Local source NAS1581C3T10 4 4 4 Screw Local source NAS1581C3T14 4 Screw Local source ALODINE 1200 AR* AR* AR* Coating Local source PR 1422A AR* AR* AR* Sealant Local source PR 1782B AR* AR* AR* Sealant Local source WHITE SPIRIT AR* AR* AR* AR* Solvent Local source NOTES: * Use as much as necessary 1) Applicable for PRE SBF28-28-026 configuration only. Applicable to standard F28 Mk. 1000 and Mk.2000 aircraft. *2 Applicable to F28 Mk. 1000 aircraft equipped with centre wing *3 Applicable to F28 Mk. 3000 and Mk.4000 aircraft. +4 Applicable to F28 Mk. 1000 thru 4000 aircraft equipped with centre wing bag tank. Status: Revision: Released date: (Mmm dd/yy) Released | Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers bject to the provisions of an agreement Reproduction or disclosure to third parties of this document or any part thereof, or the use of any informa resaid agreement, is not permitted except with the prior written permission of Fokker Services B.V. Page 9 of 26 ### Page 11 (OCR) Fokker Service Bulletin Fokker Services B.V. C. Tooling - Price and Availability (1) Not applicable. D. Tooling Required (1) Not applicable. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement. production or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted excel rith the prior written permission of Fokker Services B.\ Page 10 of 26 ### Page 12 (OCR) lazer Service Bulletin Fokker Services B.V. 4. Accomplishment Instructions General: - In general, use MM chapter 20, standard practices-airframe, as guide line for the aircraft modification. - Loosen tubing clamps where necessary. - Refer to the SPM for: - The mounting of electrical bonds on metal parts, chapter TH NC4.610. - If not indicated on drawing, seal all electrical bonds acc to TH4.610 - For Standards and Process Manual (SPM) references refer to "MyFokkerFleet.com > Documentation and select SPM". - For the application of sealing compound refer to MM chapter 20-20. For alternative sealants see Notice to Operators NTO-262, refer to ®MyFokkerFleet.com > Documentation > Service Publications and select NTO". - For the installation of bolts and screws refer to SRM chapter 51-32-01 and/or TH6.3400. - If not indicated on drawing, in the accomplishment instructions or referenced MM procedures, use standard application and inspection of torque values acc to MM chapter 20-30-05 and/or TH6.3202. - For the application of Primer & Paint refer to the MM chapter 51-30 and/or TH6.73xx. - For the application of Alodine refer to SRM chapter 51-10-04 and/or TH6.73xx. WARNING: BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. OBEY THE INSTRUCTIONS AND MANUFACTURER'S HEALTH AND SAFETY INSTRUCTIONS. WARNING: OBEY THE SAFETY PRECAUTIONS. JET FUEL IS EXPLOSIVE AND POISONOUS. A. Remove all electrical power (refer to MM, chapter 24-00-00). B. Set BATT switch to OFF and disconnect the batteries (refer to MM, chapter 24-31-03). C. Put up warning signs to tell persons: "DO NOT CONNECT THE ELECTRICAL POWER" "DO NOT CONNECT THE BATTERIES" Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreement production or disclosure to third parties of this document or any part thereof, or the use of any info contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except th the prior written permission of Fokker Services B. Page 11 of 26 ### Page 13 (OCR) fokker Service Bulletin Fokker Services B.V. Part 1: Installation of Improved Bonding Provisions for the Fuel Quantity Tank Unit (FQTU) no. 7 mounting flange and attachment screws. (Applicable to Aircraft Serial Numbers 11003 thru 11241, 11991 and 11992 in POST SBF28-57-098 configuration) Perform steps (A) thru (E) for LH and RH Fuel Quantity Tank Unit. NOTE: Care must be taken to observe the safety precautions detailed in MM chapter 28-11-00 (SERVICING). Before removal of unit drain fuel if necessary. Drain until level is below unit hole. A. Removal of Fuel Quantity Tank Unit (FQTU) no. 7. (1) Remove and keep the attachment screws from FQTU no.7 mounting flange, at the position as indicated on drawing. (2) Carefully pull the FQTU from the tank (do not disconnect electrical wiring from FQTU) and temporary hold FQTU in position. Refer to MM chapter 28-41-01. CAUTION: CARE SHOULD BE TAKEN NOT TO SCRATCH, BEND OR SCORE THE OUTER TUBE ASSEMBLY AS SUCH DAMAGE MAY NECESSITATE FQTU REPLACEMENT. (3) Remove and discard the O-ring seal from the wing top skin mounting joint. B. Application of surface treatment for Fuel Quantity Tank Unit (FQTU) no. 7 mounting flange. (1) Rework surface treatment of the flange mounted area on the upper skin with Alodine 1200 in accordance with SRM chapter 51-10-4 for Alodine treatment. Use: - AR Conversion coating pn Alodine 1200 C. Installation of Improved Bonding Provisions for Fuel Quantity Tank Unit (FQTU) no. 7 attachment screws. Refer to drawing W69315 sheet 2 for rework of LH Fuel Quantity Tank Unit. Refer to drawing W69385 sheet 2 for rework of RH Fuel Quantity Tank Unit. (1) Prepare the bond surface of the FQTU attachment screws, at the position as indicated on drawing; in accordance with NC4.610/937 (refer to TH4 of SPM for instructions and materials). NOTE: This bonding code applies to two screws holes; use the locations at the position as indicated on drawing. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been sup ct to the provisions of an agreement Reproduction or disclosure to third parties of this document or any part thereof, or the use of any inforn r purposes other tha resaid agreement, is not permitted except with the prior written permission of Fokker Services B.V Page 12 of 26 ### Page 14 (OCR) fokker Service Bulletin Fokker Services B.V. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (2) Remove dust and grease from the prepared area. Use: - AR Solvent (white spirit) pn WHITE SPIRIT D. Prepare Fuel Quantity Tank Unit (FQTU) no. 7. (1) If the aircraft is in the PRE SBF28-28-054 configuration, then examine the FQTU that must be installed, as follows: (a) Ensure that the FQTU is "clean and free of any deposits and that the mounting holes are unobstructed". (b) Make sure that the FQTU is not corroded, bent or broken. (2) If the aircraft is in the POST SBF28-28-054 configuration, then do these steps: (a) Make sure that the self-locking nuts including the washers below these nuts and the stud-ends are fully covered with a layer of the sealant. (b) Make sure that the layer of sealant is not damaged. (c) If the layer of sealant is damaged, then do these steps: 1 Make sure that the installation of the FQTU to the mounting-flange is tight. 2 If necessary, re-tighten the three self-locking nuts. Replace the layer of sealant (PR 1422B) on the self-locking nuts including the washers below these nuts and the stud-ends, ref. MM chapter 20-20- E. Install Fuel Quantity Tank Unit (FQTU) no. 7. (1) Fit a new O-ring seal, lubricated with Vaseline VV-P-236 or with fuel, in the groove of the FQTU mounting point. Use: O-Ring pn AS3578-137 (2) Carefully insert the FQTU probe into the fuel tank. (3) Align the six mounting holes and secure the probe with six retained screws that have been removed in step A. (1); refer to MM chapter 28-41-01. New screws are to be installed on the positions as indicated on drawing. Use: Screw pn NAS1581C3T6 (4) Seal off the reduced countersink screw head level/flush to the skin surface to obtain an aerodynamic smooth finish. Use: - AR Sealant pn PR 1782B Status: Revision: Released date: (Mmm ddly) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has been supplied by F • Services B.V. to its custo Reproduction or disclosure to third parties of this document or any part thereof, or the use of any in for purposes other thar with the prior written permission of Fokker Services B.V. Page 13 of 26 ### Page 15 (OCR) okker Service Bulletin Fokker Services B.V. NOTE If more Parts of this Service Bulletin Appendix are accomplished at the same time than steps F. thru G. may be accomplished with similar tasks of other Parts. F. Remove all tools, materials and equipment from the work area. Make sure that the area is clean. G. Restore electrical power. (1) Restore all electrical power (refer to MM, chapter 24-00-00). (2) Remove the warning signs to tell persons: "DO NOT CONNECT THE ELECTRICAL POWER" "DO NOT CONNECT THE BATTERIES". Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Reproducian orde cosue do fire pates el the document any pantal To of no use thany on t d bv Fokker Services B.V. to its customen ject to the provisions of an agreeme aforesaid agreement, is not permitted excep with the prior written permission of Fokker Services B Page 14 of 26 ### Page 16 (OCR) okker Service Bulletin Fokker Services B.V. Part 2: Installation of Improved Bonding Provisions for the Refueling Line. (Applicable to Aircraft Serial Numbers Mark 1000: 11003 thru 11061, 11991 and 11992 in PRE SBF28-28-026 configuration, and Mark 2000: 11053 in PRE SBF28-28-026 configuration) A. Get access to work area, remove and keep access panels 27A, 27B,28A and 28B (refer to MM, chapter 06-30). B. Installation of Improved Bonding Provisions for the Refueling Line. Refer to figure 1 or 2 for rework of the Refueling Line. Figure 1 is applicable for standard Mark 1000 and Mark 2000 aircraft. Figure 2 is applicable for Mark 1000 aircraft equipped with Centre Wing Tank. (1) Remove and discard clamp pn AN742-D28 and attached parts at the positions as indicated as "View A" in figure 1 or 2. (2) Rework and prepare the bond surface for the clamp on the pressure fuelling line (or centre wing tank fuel supply line if equipped with Centre Wing Tank) on rear spar of centre wing, at the positions as indicated as "View A" in figure 1 or 2, in accordance with NC4.610/905 (refer to TH4 of SPM for instructions and materials). Clamp pn FON2-7313-28 - 1 Screw pn MS27039-1-09 - 1 Washer (cupal) pn FON2-3306-5A Washer pn NAS1252-10L - 1 Lead pn FON9-1901C80C NOTE: All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. NOTE: The NC4.610/905 bonding design build-up is as follows: screw, washer, clamp, bonding lead, cupal washer and anchor nut. CAUTION: BE SURE THAT THE CUPAL WASHERS ARE INSTALLED WITH THE COPPER SIDE OF THE CUPAL WASHERS AGAINST THE BONDING LEAD TERMINAL. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rig! I B.V. to its c ect to the provisions of an agreement art thereof. or the use of any in resaid agreement, is not permitted except Page 15 of 26 ### Page 17 (OCR) Fokker Service Bulletin Fokker Services B.V. (3) Rework and prepare the bond surface for the bonding clamp on the pressure fuelling line (or centre wing tank fuel supply line if equipped with Centre Wing Tank) on rear spar of centre wing, at the positions as indicated as "View A" in figure 1 or 2, in accordance with NC4.610/910 (refer to TH4 of SPM for instructions and materials). Use: - 1 Clamp pn AN735-D28 pn NAS1291-3 pn MS27039-1-07 - 2 Washer pn NAS1252-10L NOTE: All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (4) Remove and discard clamp pn AN742-D28 and attached parts at the position as indicated as "View B" in figure 1 or 2. (5) Rework and prepare the bond surface for the clamp on the pressure fuelling line (or centre wing tank fuel supply line if equipped with Centre Wing Tank) on rear spar of centre wing, at the position as indicated as "View B" in figure 1 or 2, in accordance with NC4.610/920 (refer to TH4 of SPM for instructions and materials). pn FON2-7313-28 pn MS27039-1-09 pn NAS1252-10L All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. Steps (6) thru (8) are only applicable for standard Mark 1000 and Mark 2000 aircraft. (6) Remove and discard clamp pn AN742-D28 and attached parts at the position as indicated as "View C" in figure 1. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 s B.V. to its c ons of an agre ed by the aforesaid agreement, is not permitted excep Page 16 of 26 ### Page 18 (OCR) fokker Service Bulletin Fokker Services B.V. (7) Rework and prepare the bond surface for the clamp on the pressure fuelling line on rear spar of centre wing, at the position as indicated as "View C" in figure 1, in accordance with NC4.610/905 (refer to TH4 of SPM for instructions and materials). Use: Clamp pn FON2-7313-28 - 1 Screw pn MS27039-1-09 - 1 Washer (cupal) pn FON2-3306-5A Washer pn NAS1252-10L - 1 Lead pn FON9-1901C80C NOTE All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. NOTE: The NC4.610/905 bonding design build-up is as follows: screw, washer, clamp, bonding lead, cupal washer and anchor nut. CAUTION: BE SURE THAT THE CUPAL WASHERS ARE INSTALLED WITH THE COPPER SIDE OF THE CUPAL WASHERS AGAINST THE BONDING LEAD TERMINAL. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (8) Rework and prepare the bond surface for the bonding clamp on the pressure fuelling line on rear spar of centre wing, at the position as indicated as "View C" in figure 1, in accordance with NC4.610/910 (refer to TH4 of SPM for instructions and materials). Use: Clamp pn AN735-D28 - 1 Nut pn NAS1291-3 - 1 Screw pn MS27039-1-07 - 2 Washer pn NAS1252-10L NOTE: All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. Steps (9) thru (11) are only applicable for Mark 1000 aircraft equipped with Centre Wing Tank. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands) This document has been supplied ices B.V. to its cu subject to the provisions of an agreement Reproduction or disclosure to third parties of this document or any part thereof, or the use of any inform r purposes oth foresaid agreement, is not permitted excep with the prior written permission of Fokker Services B.V. Page 17 of 26 ### Page 19 (OCR) okker Service Bulletin Fokker Services B.V. (9) Remove and discard clamp pn AN742-D16 and attached parts at the position as indicated as "View C" in figure 2. (10) Rework and prepare the bond surface for the clamp on the centre wing tank fuel supply line on rear spar of centre wing, at the position as indicated as "View C" in figure 2, in accordance with NC4.610/905 (refer to TH4 of SPM for instructions and materials). Use: Clamp pn FON2-7313-18 - 1 Screw pn AN3-4A - 1 Washer (cupal) pn FON2-3306-5A Washer pn NAS1252-10L Lead pn FON9-1901C100C NOTE: All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. NOTE: The NC4.610/905 bonding design build-up is as follows: screw, washer, clamp, bonding lead, cupal washer and anchor nut. CAUTION: BE SURE THAT THE CUPAL WASHERS ARE INSTALLED WITH THE COPPER SIDE OF THE CUPAL WASHERS AGAINST THE BONDING LEAD TERMINAL. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (11) Rework and prepare the bond surface for the bonding clamp on the centre wing tank fuel supply line on rear spar of centre wing, at the position as indicated as "View C" in figure 2, in accordance with NC4.610/910 (refer to TH4 of SPM for instructions and materials). Use: - 1 Clamp pn AN735-D18 - 1 Screw 1 Nut pn NAS1291-3 pn MS27039-1-07 2 Washer pn NAS1252-10L NOTE: All electrical contact areas should be cleaned before, and painted after installation of the applicable parts, in accordance with F28 Maintenance Manual, chapter 20-40-2. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Foki This document has been supplied by ervices B.V. to its cus ect to the provisions of an agreeme reproducen or discosure o my pares or ma det for purposes omen ma aid agreement, is not permitted excep Page 18 of 26 ### Page 20 (OCR) fokker Service Bulletin Fokker Services B.V. (12) Remove dust and grease from the prepared area. Use: - AR Solvent (white spirit) pn WHITE SPIRIT NOTE If more Parts of this Service Bulletin Appendix are accomplished at the same time than steps C. thru E. may be accomplished with similar tasks of other Parts. C. Remove all tools, materials and equipment from the work area. Make sure that the area is clean. D. Install access panels. (1) Install access panels 27A, 27B, 28A and 28B (refer to MM, chapter 06-30). E. Restore electrical power. (1) Restore all electrical power (refer to MM, chapter 24-00-00). (2) Remove the warning signs to tell persons: DO NOT CONNECT THE ELECTRICAL POWER" "DO NOT CONNECT THE BATTERIES". Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 pyright All rights reserved by Fokker Services B.V. (The Netherlands). This document has b production or disclosure to third parties of this document or any part thereof, or the use of with the prior written permission of Fokker Services B.V. applied by Fokker Services B.V. to its customers on a confidential basis subject to the provisions of an agreemen therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted excep Page 19 of 26 ### Page 21 (OCR) okker Service Bulletin Fokker Services B.V. Part 3: Installation of Improved Bonding Provisions for the Suction Relief Valve line. (Applicable to Aircraft Serial Numbers 11016 thru 11061, 11991 and 11992, in POST SBF28-28-020 configuration, and Aircraft Serial Numbers 11062 thru 11241 if equipped with Center Wing Tanks) A. Get access to work area, remove and keep access panels 91K and 92K (refer to MM, chapter 06-30). NOTE: If access to the Suction Relief Valve line is found insufficient, remove and keep access panels 91J and 92J (refer to MM, chapter 53-50-02). B. Installation of Improved Bonding Provisions for the Suction Relief Valve line. Refer to drawing W69711 sheet 1 for rework of LH and RH Suction Relief Valve line. Perform steps (1) thru (4) for LH and RH Suction Relief Valve line. (1) Rework and prepare the bond surface for the clamp on the Suction Relief Valve line, at the position as indicated in drawing W69711 sheet 1, in accordance with NC4.610/905 (refer to TH4 of SPM for instructions and materials). Use: pn NAS1100-3-8 - 1 Washer (cupal) pn FON2-3306-05010 - 1 Washer pn NAS1149D0332K - 1 Lead pn FON9-1901C200C All electrical bonds must be sealed in accordance with SPM NC4.610; 5.3, Finishing Requirements 5.6, Finishing with Sealing Compound. CAUTION BE SURE THAT THE CUPAL WASHERS ARE INSTALLED WITH THE COPPER SIDE OF THE CUPAL WASHERS AGAINST THE BONDING LEAD TERMINAL. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (2) Rework and prepare the bond surface for the bonding clamp on the Suction Relief Valve line, at the position as indicated in drawing W69711 sheet 1, in accordance with NC4.610/910 (refer to TH4 of SPM for instructions and materials). Use: - 1 Clamp pn AN735-D16 - 1 Nut pn MS21042L3 - 1 Screw pn NAS1133-3 - 2 Washer pn NAS1149D0332K NOTE: All electrical bonds must be sealed in accordance with SPM NC4.610; 5.3, Finishing Requirements Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fol ices B.V, to its c the feat here, not pan ade r purposes other than explicitly allowed by with the prior witten permis Page 20 of 26 ### Page 22 (OCR) tokker Service Bulletin Fokker Services B.V. 5.6, Finishing with Sealing Compound. CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (3) Apply a fillet sealant on the installed screws, washers, nut and clamp, installed in steps (1) and (2), in accordance with SRM chapter 51-20-0. Use: - AR Sealant pn PR 1422A (4) Remove dust and grease from the prepared area. Use: - AR Solvent (white spirit) pn WHITE SPIRIT NOTE: If more Parts of this Service Bulletin Appendix are accomplished at the same time than steps C. thru E. may be accomplished with similar tasks of other Parts. C. Remove all tools, materials and equipment from the work area. Make sure that the area is clean. D. Install access panels. (1) Install access panels 91K and 92K (refer to MM, chapter 06-30). (2) Install access panels 91J and 92J, if removed (refer to MM, chapter 06-30). E. Restore electrical power. (1) Restore all electrical power (refer to MM, chapter 24-00-00). (2) Remove the warning signs to tell persons: "DO NOT CONNECT THE ELECTRICAL POWER" "DO NOT CONNECT THE BATTERIES". Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B V. (The Netherlands) This document has been supp vices d.V. to as customers on a condi subject to the provisions of an agreemer Wep the phor wor on perre son of Forker of vices sument or any part thered, or the use of any infor r purposes other than explicitly allowed by the aforesaid agreement, is not permitted excep Page 21 of 26 ### Page 23 (OCR) fokker Service Bulletin Fokker Services B.V. Part 4: Installation of Improved Bonding Provisions for Boost Pump attachment screws. (Applicable to Aircraft Serial Numbers 11003 thru 11241, 11991 and 11992). A. Installation of Improved Bonding Provisions for Boost Pump attachment screws. Refer to drawing W69205 sheet 1 for rework of LH Boost Pump. Refer to drawing W69245 sheet 1 for rework of RH Boost Pump. Perform steps (1) thru (6) for LH and RH Boost Pumps. (1) Remove and discard the 2 screws from the front and rear Boost Pump attachment, at the positions as indicated on drawing. NOTE: The bonding locations are also engraved in the Boost Pump flange by the manufacturer. The paint scheme may/can cover these engravings. When not visible, use the locations indicated on the drawings. (2) Rework and prepare the bond surface of the screw holes for the front and rear Boost Pump, at the positions as indicated on drawing, in accordance with NC4.610/937 (refer to TH4 of SPM for instructions and materials). NOTE This bonding code applies to two screws holes; use the positions as indicated on drawing CAUTION: INSTALL THE CONNECTION IMMEDIATELY AFTER THE CONTACT SURFACE IS CLEANED, TO PREVENT CORROSION OF THE CONTACT SURFACES. DO NOT TOUCH THE CLEANED SURFACE WITH A BARE HAND, THE SEALING COMPOUND WILL NOT BOND TO A GREASY SURFACE. (3) Remove dust and grease from the prepared area. Use: - AR Solvent (white spirit) pn WHITE SPIRIT (4) Install new screws (reduced- head) for front Boost Pump (refer to MM, chapter, 28-22-02). Use: - 2 Screw pn NAS1581C3T10 (5) Install new screws (reduced- head) for rear Boost Pump (refer to MM, chapter, 28-22-02). Use: - 2 Screw pn NAS1581C3T14 (6) Seal off the reduced countersink screw head level/flush to the skin surface to obtain an aerodynamic smooth finish. Use: - AR Sealant pn PR 1782 Class A NOTE If more Parts of this Service Bulletin Appendix are accomplished at the same time than steps B. and C. may be accomplished with similar tasks of other Parts. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights rese ervices B.V. to its cus said agreement, is not permitted excep Page 22 of 26 ### Page 24 (OCR) okker Service Bulletin Fokker Services B.V. B. Remove all tools, materials and equipment from the work area. Make sure that the area is clean. C. Restore electrical power. (1) Restore all electrical power (refer to MM, chapter 24-00-00). (2) Remove the warning signs to tell persons: "DO NOT CONNECT THE ELECTRICAL POWER" "DO NOT CONNECT THE BATTERIES". Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: • F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Ser ands) This document has been supp ed by Fokker Services B.V. to its customers on a co ibiect to the provisions of an agreeme Reproduction or disclosure to third parties with the prior written permission of Fokker S Page 23 of 26 ### Page 25 (OCR) Service Bulletin Fokker Services B.V. 2 OFF) NC4.610/910 ANO ATTACHMENT CLAMP P/N FOH2.7313 ASHER P/M FON2.330 ASHER P/N FON2. NC4.610/905 * VIEW A TASHER P/N WAS SCREW P/N NC4.610/920 VIEW B NC4.610/905 * 1-07 NC4.610/910 VIEW C Figure 1 Modified Bonding for Pressure Fuelling Line * The NC4.610/905 bonding design is build-up as follows: screw, washer, clamp, bonding lead, cupal washer and anchor nut. Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 ervices B.V. to its to me provisions or an agreemen a use of any information contained therein for purposes other than exp oresaid agreement, is not permitted excep Page 24 of 26 ### Page 26 (OCR) Service Bulletin Fokker Services B.V. REMOVE: CLAMI INSTALL: CLAMP NC4.610/905 * INSTA NC4.610/910 VIEW B VIEW C BASHER P/N HAS SCREW P/N WS27039 NC4.610/920 INSTALL: SCREE P/N US SCREW P/N M$2703 181 (2 OFF) NC4.610/905 * NC4.610/910 VIEW A * The NC4.610/905 bonding design is build-up as follows: screw, washer, clamp, bonding lead, cupal washer and anchor nut. Figure 2 Modified Bonding for Centre Wing Tank Fuel Supply Line Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Copyright All rights reserved by Fokker Services B.V. (The Netherlands): This document has been supplied by Fokker Services B.V. to its customers on a c Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than foresaid agreement, is not permitted except win me pror wisten permission of rokker services b. V Page 25 of 26 ### Page 27 (OCR) okker Service Bulletin Quality Reporting Form Fokker Services B.V. SB Title: Installation of additional Bonding Provisions Outside the Fuel Tank Use this Service Bulletin Quality Reporting Form to tell us your perception of the quality of the Service Bulletin. The reported data that you provide to us will be used to analyze areas of difficulties and to take corrective actions to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. * Rate the scale of 1 to 4, with 1 the lowest score and 4 the highest score. Chapters * 1 2 3 4 a) Quality rating of this SB (overall) b) Quality rating of the Planning Information c) Quality rating of the Material Information d) Quality rating of the Accomplishment Instructions e) Quality rating of the Test Instructions (if applicable) f) Quality rating of the Illustrations or Drawings (if applicable) g) Timely delivery of the SB If you have had difficulties with one of the chapters of this Service Bulletin and/or one of your rating(s) is lower than 3, please give a short description of the issue. Comments: Operator: Date: Name / Title: Please return this form to: Fokker Services B.V. Technical Services, Quality Department P.O. Box 1357 2130 EL Hoofddorp The Netherlands Fax: +31 (0) 88 6280111 or E-mail: technicalservices@fokker.com Status: Revision: Released date: (Mmm dd/yy) Released Jul 15/14 Security class: F28 Appendix SB no.: UNCLASSIFIED SBF28-28-059/APP01 Geprodu fon or of resured bud parer s of tha decu mee rehy panthe Tol. of ce uat h an eato mailed d lands). This document has been supplied by Fokker Services B.V. to its customers on basis subject to the provisions of an agreement manouWero oTtuposes ooertan expiy dlcwec pv me aotesao acreeent is nos permet ecep YU tE DIO WEn DeTSSn OI OET SWICOS HEW Page 26 of 26 --- 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.