TextOCR
This text is OCR from a scan. OCR can misread letters and numbers.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1b98f059a7401a3aed70a3b71e7815feb6cf078d1b96271f9020bfa7e4b4e6ae' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '1b98f059a7401a3aed70a3b71e7815feb6cf078d1b96271f9020bfa7e4b4e6ae' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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
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
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
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
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
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
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
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
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
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
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
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