Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

Jun 23/10 SBF28-28-051 

Page 1 

1. Planning Information

A. Effectivity 

(1) F28 Mk 1000/2000/3000/4000(C) aircraft serial numbers: 

11003 thru 11241, 11991 and 11992. 

(2) Production version of this modification: Not applicable. 

B. Concurrent Requirements 

(1) Not applicable. 

C. Reason 

(1) The design review of the F28 Mk 1000/2000/3000/4000(C) 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. 

(2) Under certain failure conditions of the Level Control Pilot Valve solenoid or in the 

wiring to the solenoid, a short circuit may develop. Such a short circuit may result in 

an ignition source in the wing tank vapour space. 

(3) The fuse, packed in a jiffy junction will limit the current and thus prevent this ignition 

source in the wing tank vapour space. 

Page 1 2 3 4 5 6 7 

Revision - - - - - - - 

Attachments 3 Drawing sheets. For a detailed listing refer to page 5. 

FUEL

“This Service Bulletin is associated with the Fuel Tank Safety Program” 

Tank Fueling / De-fueling - The Introduction of a Fuse in the Level Control Pilot Valve Wiring 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

SBF28-28-051 Jun 23/10 

Page 2 

D. Description 

(1) This Service Bulletin tells you how to: 

- Install the jiffy junctions. 

- Perform system functional tests. 

E. Compliance 

(1) Recommended. 

Fokker Services recommends the accomplishment of this Service Bulletin within 2 

years after the date of issue of this Service Bulletin. 

NOTE: It is expected that EASA will issue an Airworthiness Directive (AD) with respect 

to this subject with the same compliance terms. Refer to the EASA website for 

the publication of a Proposed Airworthiness Directive for comments. 

F. Approval 

(1) The technical content of this document is approved by EASA or under the authority of 

DOA nr. EASA.21J.059. 

G. Manpower 

(1) Approximately 5 man-hours are necessary to do this Service Bulletin on one aircraft. 

This table of manpower will help you to schedule and do this Service Bulletin: 

Instructions Men Man-hours Elapsed time 

(hours) 

Removal - - - 

Modification 2 2 1 

Installation 2 2 1 

Testing 1 1 1 

Total 5 3 

NOTE: This estimate does not include the time necessary for the paint to dry 

 and/or the sealant to cure. 

(2) 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"). 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

Jun 23/10 SBF28-28-051 

Page 3 

H. Weight and Balance 

(1) Weight change: None 

Index change: None. 

I. Electrical Load Data 

(1) Not affected. 

J. Software Accomplishment Instructions 

(1) Not applicable. 

K. References 

(1) F28 Maintenance Manual (MM) 

F28 Wiring Diagram Manual (WDM) 

Fokker drawing(s): refer to page 5 

Fokker internal reference(s): 

 - ECR 15105. 

L. Publications Affected 

(1) This SB affects the publications listed below: 

(a) Maintenance Documentation

- F28 Wiring Manual (WDM) - chapter 28-21 

- F28 Maintenance Manual (MM) - chapter 28-21 

NOTE: See attached Manual Change Notification MCNM F28-034. 

(b) Maintenance Programs

Not affected. 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

SBF28-28-051 Jun 23/10 

Page 4 

(c) Special Instructions for Continued Airworthiness (ICA)

The effect of this Service Bulletin on the special ICA is as follows: 

 YES NO 

- Fuel Tank Safety (FTS) X - 

NOTE: The fuel CDCCL item as specified below shall be followed and 

incorporated in the approved aircraft maintenance program documents. 

CDCCL: It shall be assured that the over-current protection fuses (electronic 

in-line junction with integral fuse) in the wiring to the level control pilot 

valves, located close to the point where the wiring goes into the tank, 

are installed. 

Affected part number W48006-401. 

NOTE: The verification shall be performed in accordance with the 

Standard Practices applicable for the installation of this 

component as described in the Wiring Manual and/or in 

accordance with the instructions in the AMM, changed 

in accordance with the instructions in the attached 

MCNM F28-034. 

(d) Operational Documentation

Not affected. 

(2) For incorporation of this Service Bulletin in your documentation refer to SBF28-00-

001 (Service Bulletin Introduction, section 4 "Incorporation of Service Bulletins in 

Documentation of Fokker Services"). 

NOTE: Accomplishment of this SB is only complete with incorporation of the manual 

 changes, per the ref MCNM, Temporary Revision or general revision. 

M. Interchangeability or Intermixability of Parts 

(1) Not applicable. 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

Jun 23/10 SBF28-28-051 

Page 5 

2. Material Information

A. Material – Price and Availability 

(1) You can order the necessary parts as mod kit SB2828051-XU-A. 

(2) You can contact your Fokker Services Account Manager for the price and lead-time of 

this mod kit. 

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 Keyword Info Old Part Number Instructions/ 

Disposition

22 DR * Tape, Lacing Fk05-090(A)** - Local Source

M81824-1-1 2 Splice*** FC400 - - 

- 2 Wire mate*** - CM041 Discard 

NOTE: * Use as much as necessary. 

** Refer to the CML for material numbers. 

*** If applicable. 

(2) These mod kit parts are necessary to do this Service Bulletin on 1 aircraft. 

New Part Number Qty Keyword Info Old Part Number Instructions/ 

Disposition

W48006-401 2 Fuse, Jiffy Junction 1 Amp - - 

F0N1-3613-24-4 1m* Sleeve - - - 

W58048-402 1** Cableloom - - - 

NOTE: * Use as much as necessary, put remaining material into storage. 

** This part of the mod kit is not always applicable. 

C. Tooling – Price and Availability 

(1) Not applicable. 

D. Drawings Required 

(1) These drawings are necessary to do this Service Bulletin: 

Drawing Sheet Issue Size Description Aircraft Effectivity

W57231 010 K A4 RF WD Fuel Control System Refer to A/C config. 

W57231 011 K A4 RF WD Fuel Control System Refer to A/C config. 

W58048 002 - A3 Cableloom connectionlist All 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

SBF28-28-051 Jun 23/10 

Page 6 

3. Accomplishment Instructions

General 

- For CML material number references, refer to “Myfokkerfleet.com/documentation/CML”. 

- For the finish codes, refer to “Myfokkerfleet.com/documentation/FC”. 

- Cut the new wires to the correct length where necessary. 

- Loosen the cable clamps where necessary. 

- Remove and discard the cable ties where necessary. 

- Refer to the WM, chapter 20, for the removal and installation of the wires. 

A. The Job Set-Up. 

(1) Remove all electrical power (Refer to the AMM, chapter 24-00). 

(2) Put up warning signs to tell persons: 

"DO NOT CONNECT THE ELECTRICAL POWER" 

"DO NOT CONNECT THE BATTERIES". 

B. Get access to work area, open panels 83B & 84B. 

C. Rework of wiring. 

Refer to drawing W57273 sheet 010 or 011*. 

NOTE: * Use sheet 11 if the wiring contains wire mates (to be verified on A/C). 

(1) Rework the LH outside Fuel tank aircraft wiring. 

(a) Remove the splice or the wire mate (with grommet and contacts). 

(2) Install and identify the jiffy junction. Use: 

- 1 wire (QC33E22)* ref cableloom W58048-402 

- 1 fuse, jiffy junction (QC98-831) pn W48006-401 

- 1 splice* pn M81824-1-1 (FC400) 

- AR tape, lacing pn Fk05-090(A) 

- AR sleeve, identification** pn F0N1-3613-24-4. 

NOTE: * If applicable. 

 ** Write “QC98-831” on the identification sleeve. 

Do not shrink the sleeve. 

. 
Service Bulletin 

Fokker F28 

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. 

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 explicitly allowed by the aforesaid agreement, is not permitted 

except with the prior written permission of Fokker Services B.V. 

Jun 23/10 SBF28-28-051 

Page 7 

(3) Rework the RH outside Fuel tank aircraft wiring. 

(a) Remove the splice or the wire mate (with grommet and contacts). 

(4) Install and identify the jiffy junctions. Use: 

- 1 wire (2QC33E22)* ref cableloom W58048-402 

- 1 fuse, jiffy junction (2QC98-841) pn W48006-401 

- 1 splice* pn M81824-1-1 (FC400) 

- AR tape, lacing pn Fk05-090(A) 

- AR sleeve, identification** pn F0N1-3613-24-4. 

NOTE: * If applicable. 

 ** Write “2QC98-841” on the identification sleeve. 

Do not shrink the sleeve. 

D. Restore electrical power. 

(1) Restore all electrical power (Refer to the AMM chapter 24) 

(2) Remove the warning signs to tell persons: 

"DO NOT CONNECT THE ELECTRICAL POWER" 

"DO NOT CONNECT THE BATTERIES". 

E. Do the following operational test to verify correct operation: 

(1) Do the after installation test of the Level Control Pilot Valve, refer to 

Maintenance Manual, chapter 28-21-03. 

F. Close access panels 83B & 84B. 

G. Remove all tools, materials, and equipment from the work area. Make sure the area is 

clean. 


FOKKER SERVICES B.V.

ENGINEERING DEPARTMENT

CABLELOOM CONNECTIONLIST

PART NUMBER PART NAME EQUIVALENT DWG NR : W58048

El. Cable

DASH NR : -402

ISSUE : -

SHEET : 2

DATE : 10-04-29

FROM CABLE LENGTH TO WD DRAWING

EQUIPNR CNT FC NUMBER SEP TYP GG mm EQUIPNR CNT FC NUMBER REFERENCE

QC33E22 1 NK 22 500 W57231 W58048-402-

2QC33E22 2 NK 22 500 W57231 W58048-402-

F0N9-1780NK22 01316-95003

QTY

A.R.
Manual Change Notification – Maintenance Documentation 

Fokker 28 

JUN 23/10 MCNM F28-034 

Page 1 of 3 

MCNM-F28-034 

Subject : Fuel – Introduction of Fuses in the Wiring of the Level Control Pilot Valve. 

Reason : This MCN is issued to provide you with the changes on the content(s) of the 

affected manual(s), due to the introduction of SBF28-28-051. 

Effectivity : Refer to SBF28-28-051. 

 

Compliance : Once you have determined the applicability of this MCN for one or more of your 

aircraft, incorporate this information into the applicable manual(s). 

Publications 

affected : The Maintenance Manual (MM) 

 The Wiring Diagram Manual (WDM). 

Change Note : MM

NOTE: Make sure that your manual contains the contents of MCNM F28-023, 

before you incorporate this MCNM. 

If your manual contains Temporary Revision No. 28-49, then do as follows: 

- In 3. Removal/Installation, add the following step between the steps 

B.(13) and B.(14), and re-identify the existing steps B.(14) thru B(23) 

accordingly: 

NOTE: Start of Fuel System CDCCL affected section. 

(14) Do a check of the fuse jiffy-junction assembly 

NOTE: The installation of the fusible jiffy-junction assembly is identified 

with a yellow sleeve at each end. 

(a) Find the installation of the fuse jiffy-junction assembly QC98-831 or 2Q98-

841 between the electrical-wires (Refer to the Wiring Diagram Manual 28-

21-02 for more data). 

(b) Make sure that the installation of the fuse jiffy-junction assembly is in 

good condition and not damaged. 

(c) Make sure that the partnumber W48006-401 is clearly shown on the fuse 

jiffy-junction assembly. 

NOTE: End of Fuel System CDCCL affected section. 
Manual Change Notification – Maintenance Documentation 

Fokker 28 

JUN 23/10 MCNM F28-034 

Page 2 of 3 

If your manual contains Temporary Revision No. 28-30, or your manual contains 

28-21-03 pageblock 401 only, then do as follows: 

- In 1. General, add the following paragraph: 

- In 3. Removal/Installation, add the following step between the steps 

B.(11) and B.(12), and re-identify the existing steps B.(12) thru B(20) 

accordingly: 

NOTE: Start of Fuel System CDCCL affected section. 

(12) Do a check of the fuse jiffy-junction assembly 

NOTE: The installation of the fuse jiffy-junction assembly is identified with a 

yellow sleeve at each end. 

(a) Find the installation of the fuse jiffy-junction assembly QC98-831 or 2Q98-

841 between the electrical-wires (Refer to the Wiring Diagram Manual 28-

21-02 for more data). 

(b) Make sure that the installation of the fuse jiffy-junction assembly is in 

good condition and not damaged. 

(c) Make sure that the partnumber W48006-401 is clearly shown on the fuse 

jiffy-junction assembly. 

NOTE: End of Fuel System CDCCL affected section. 

If your manual contains Temporary Revision No. 28-57 after 28-21-03 pageblock 

401, then remove and discard this document from your manual. 

In 28-21-00 pageblock 001 (all codes), add the following paragraph to 2.B. 

Electrical System: 

There are fuse jiffy-junction assemblies installed in the electrical-wiring of the 

level-control pilot-valves, between the wing rear-spar and the main tank, in 

zone 830 and 840. The fuses prevent that a short-circuit in the electricalinstallation of a level-control pilot valve can result in an ignition-source in the 

fuel tank. 
Manual Change Notification – Maintenance Documentation 

Fokker 28 

JUN 23/10 MCNM F28-034 

Page 3 of 3 

 WDM

 Update Chapter 28-21-02, in accordance with the drawings as given in SBF28-

28-051, paragraph 2.D.). 

NOTE: If you have a Continued Airworthiness Documentation Service with Fokker Services, this 

MCN will be included into your manuals, at the earliest opportunity.