Service Bulletin 

Fokker 70/100 

Page 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17

Revision - - - - - - - - - - - - - - - - - 

Page 18 

Revision - 

Jul 14/11 SBF100-24-044 

Page 1 

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.

1. Planning Information

A. Effectivity 

(1) F28 Mark 0070/0100 aircraft serial numbers: 

11340 thru 11343, 11347, 11348, 11350 thru 11356, 11359 thru 11361, 

11367 thru 11371, 11374 thru 11378, 11382 thru 11385, 11387 thru 11390, 

11394 thru 11397, 11400 thru 11423, 11425 thru 11432, 11434 thru 11439, 

11441 thru 11453, 11456 thru 11585. 

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

B. Concurrent Requirements 

(1) Not applicable. 

C. Reason 

(1) Fokker Services received reports about burned contacts in production break 

plug/receptacle P 4259B/J 4259A. After investigation it is concluded that the high 

electrical load on the contacts M, L, X in combination with the loads on the adjacent 

connections causes this occurrence. For this reason it is decided to disconnect all 

galley power supply wiring, through this plug/receptacle which is protected by 25A or 

30A circuit breakers. The disconnected wires will be connected through splices. 

ELECTRICAL POWER

Galley Power Distribution - Removal of Galley Power Wiring from Production Break. 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 2 

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.

D. Description 

(1) This Service Bulletin tells you how to: 

- Rework the wiring on plug/receptacle P 4259B/J 4259A. 

E. Compliance 

(1) Recommended. 

Fokker Services recommends the accomplishment of this Service Bulletin within 2 

years after the issue date 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 under the authority of DOA nr. 

EASA.21J.059. 

G. Manpower 

(1) Approximately 3,5 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 1 1,0 1,0 

Modification 

Inspection 1 1,5 1,5 

Installation 

Testing 1 1,0 1,0 

Total 3,5 3,5 

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 SBF100-00-001 (Service Bulletin 

Introduction, section 2.C., "Manpower"). 

H. Weight and Balance 

(1) Weight change: None 

Index change: None. 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 3 

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. 

I. Electrical Load Data 

(1) Not changed. 

J. Software Accomplishment Summary 

(1) Not applicable. 

K. References 

(1) Fokker 70/100 Aircraft Maintenance Manual (AMM) 

Fokker 70/100 Wiring Manual (WM) 

Fokker internal reference(s): 

 - ECR 015764. 

L. Publications Affected 

(1) This SB affects the publications listed below: 

(a) Maintenance Documentation

- Fokker 70/100 Wiring Manual (WM) - chapter 24-54. 

NOTE: See attached Manual Change Notification MCNM F100-148. 

(b) Maintenance Programs

Not affected. 

(c) Special Instructions for Continued Airworthiness (ICA)

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

 YES NO 

- Electrical Wiring Interconnection System (EWIS) - X 

- Fuel Tank Safety (FTS) - X 

- Damage Tolerance of Fatigue Critical Structure - X 

NOTE: If “YES”, when not already incorporated, the changed ICA will be 

incorporated in the MRB document within one calendar year from the 

date of issue of this Service Bulletin. Until then, no actions are required. 

(d) Operational Documentation

Not affected. 

(2) Report to Fokker Services that this SB has been carried out on the applicable aircraft. 

Send to Fokker Services the “Reporting Quality Form” of this SB, see last SB page. 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 4 

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.

(3) For incorporation of this Service Bulletin in your documentation refer to 

SBF100-00-001 (Service Bulletin Introduction, section 4 "Incorporation of Service 

Bulletins in Documentation of Fokker Services"). 

(4) Accomplishment of this SB is only complete with incorporation of the manual 

change(s), per the ref. MCNM, Temporary Revision 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

MS27488-12-1 Sealing plug MS27488-12 Two-way 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 5 

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. 

2. Material Information

A. Material – Price and Availability 

(1) You can order the necessary parts as mod kits SB10024044-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

F0N1-5921-8 AR* Tape, silicone 

rubber 

Fk05-008** - Local source 

F0N1-7952-1 AR* Tape, lacing Fk05-090** - Local source 

NOTES: * Use as much as necessary 

** Refer to the CML for material numbers. 

(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

F0N2-7338E03 1* Clamp - - - 

F0N2-7338E04 1* Clamp - - - 

F0N9-1784VF12 1,0m* Wire - - - 

MS27488-12-1 12* Sealing plug 

(yellow) 

FC336/FC337 - - 

M81824-1-3 12* Splice FC400 - - 

NAS1100-3-8 1 Screw - NAS1100-3-7 Discard 

NOTES: * Maximum required Qty is given. 

C. Tooling – Price and Availability 

(1) Not applicable. 

D. Drawings Required 

(1) Not applicable. 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 6 

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.

3. Accomplishment Instructions

General: 

- Loosen the cable clamps where necessary. 

- Remove and discard the cable ties where necessary. 

- Remove and discard the lacing tape where necessary. 

- Route the new wires along the existing cable looms. 

- Use cable ties and lacing tape where necessary. 

- Remove and/or install sealing plugs in the connectors where necessary. 

- Use cable clamps where necessary. 

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

- Refer to the WM for: 

- The removal and installation of the wires, chapter 20-13-03, 

- Component Location, chapter 91-21-XX. 

- For finish codes references, refer to “Myfokkerfleet.com/Documentation/FC”. 

- Disconnect and reconnect the connectors where wires will be removed or inserted for the 

modification.

A. Remove all electrical power (Refer to the AMM, chapter 24-00-00-860-912A). 

B. Remove and keep the following ceiling panels to gain access to plug receptacle 

P 4259B / J 4259A : 

- 248AZ Ceiling panel 

and 

- 248CZ Ceiling panel for aircraft equipped with a smaller 248AZ ceiling panel 

and/or 

- 261GZ Ceiling panel for aircraft equipped with a smaller 248AZ ceiling panel. 

C. Route the new wires, which will be installed in one of the next steps, underneath the 

mounting bracket of plug/receptacle P 4259B / J 4259A according to figure 1. Discard 

screw pn NAS1100-3-7. 

Step D. is applicable for aircraft serial numbers: 11340, 11352 thru 11356, 11359 thru 11361, 

11367 thru 11370, 11376, 11377, 11385, 11395 thru 11397, 11402 thru 11408, 

11411 thru 11419, 11425 thru 11428, 11434 thru 11437, 11446 thru 11449, 

11456 thru 11460, 11464 thru 11469, 11478 thru 11483, 11490, 11491, 11498, 11499, 

11501, 11502, 11506, 11507, 11514, 11515 and 11520. 

D. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 2. Use: 

- 1 clamp pn F0N2-7338E03 

- 0,5m wire pn F0N9-1784VF12 

- 6 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 6 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 7 

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. 

Step E. is applicable for aircraft serial numbers: 11341 thru 11343, 11347, 11348, 11350, 

11351, 11371, 11374, 11375, 11378, 11382 thru 11384, 11387 thru 11390, 11394, 11400, 

11401, 11409, 11410, 11420 thru 11423, 11429 thru 11432, 11438, 11439, 

11441 thru 11443, 11451, 11461, 11462, 11470, 11472, 11473, 11476, 11496, 11500, 

11504, 11505, 11511, 11513, 11516, 11518, 11519, 11522 and 11523. 

E. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 3. Use: 

- 1 clamp pn F0N2-7338E03 

- 0,5m wire pn F0N9-1784VF12 

- 6 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 6 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

Step F. is applicable for aircraft serial numbers: 11444, 11445, 11450, 11452, 11453, 11463, 

11471, 11474, 11475, 11477, 11484 thru 11489, 11492 thru 11495, 11497, 11503, 11509, 

11512, 11517, 11521, 11527 thru 11529, 11532, 11537 thru 11541, 11543, 11545, 11547, 

11549, 11551, 11554 thru 11556, 11558 thru 11560, 11564, 11565, 11568, 11569, 11572 

and 11573. 

F. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 4. Use: 

- 1 clamp pn F0N2-7338E04 

- 1,0m wire (2 x 0,5m) pn F0N9-1784VF12 

- 12 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 12 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

Step G. is applicable for aircraft serial numbers: 11536, 11553, 11561, 11562, 11566, 11567, 

11570, 11574, 11576 thru 11579 and 11581 thru 11583. 

G. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 5. Use: 

- 1 clamp pn F0N2-7338E03 

- 0,5m wire pn F0N9-1784VF12 

- 6 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 6 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

Step H. is applicable for aircraft serial numbers: 11563, 11571and 11575. 

H. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 6. Use: 

- 1 clamp pn F0N2-7338E04 

- 1,0m wire (2 x 0,5m) pn F0N9-1784VF12 

- 12 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 12 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 8 

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.

Step I. is applicable for aircraft serial numbers: 11580 and 11585. 

I. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 7. Use: 

- 1 clamp pn F0N2-7338E03 

- 0,5m wire pn F0N9-1784VF12 

- 6 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 6 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

Step J. is applicable for aircraft serial numbers: 11557. 

J. Rework the wiring on plug/receptacle P 4259B / J 4259A according to figure 8. Use: 

- 1 clamp pn F0N2-7338E04 

- 1,0m wire (2 x 0,5m) pn F0N9-1784VF12 

- 12 sealing plugs (yellow) pn MS27488-12-1 FC336/FC337 

- 12 splices pn M81824-1-3 FC400 

- 1 screw pn NAS1100-3-8. 

K. Testing after the modification. 

(1) Operational test Galley(s). 

Step (a) is applicable for aircraft sn.: 11340 thru 11579 and 11581 thru 11584. 

(a) Do the operational test of Galley 2 (refer to the AMM, chapter 25-32-00. 

Step (b) is applicable for aircraft sn.: 11536, 11547, 11553, 11557, 11561, 11563, 

11570, 11574, 11580 and 11585. 

(b) Do the operational test of Galley 3 (refer to the AMM, chapter 25-33-00. 

(2) Do the following Operational tests: 

- Cabin Main Lighting System (refer to the AMM, chapter 33-21-00) 

- Lavatory Lighting (refer to the AMM, chapter 33-23-00) 

- Entrance Lighting (refer to the AMM, chapter 33-26-00). 

(3) Do the test of the reading lights as follows (refer to the AMM, chapter 33-22-00). 

Step (a) is applicable for Fokker 100 aircraft.. 

(a) On the MTP-A: 

- Operate the READ LTS TEST switch; make sure all reading lights come on. 

- Operate the READ LTS RESET switch; make sure all reading lights go off. 

Step (b) is applicable for Fokker 70 aircraft. 

(b) On the CFDU: 

- Select READ LTS TEST; make sure all reading lights come on. 

- Select READ LTS RESET; make sure all reading lights go off. 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 9 

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. 

L. Install the ceiling panel(s) which was (were) removed in step B. 

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

clean. 

 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 10 

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.

TOP VIEW 

Separation B2 added underneath mounting bracket. 

Figure 1 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 11 

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. 

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11340, 11352 thru 11356, 11359 thru 11361, 

11367 thru 11370, 11376, 11377, 11385, 11395 thru 11397, 11402 thru 11408, 

11411 thru 11419, 11425 thru 11428, 11434 thru 11437, 11446 thru 11449, 

11456 thru 11460, 11464 thru 11469, 11478 thru 11483, 11490, 11491, 11498, 11499, 

11501, 11502, 11506, 11507, 11514, 11515, 11520. 

Figure 2 

 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 12 

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.

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11341 thru 11343, 11347, 11348, 11350, 11351, 

11371, 11374, 11375, 11378, 11382 thru 11384, 11387 thru 11390, 11394, 11400, 11401, 

11409, 11410, 11420 thru 11423, 11429 thru 11432, 11438, 11439, 11441 thru 11443, 

11451, 11461, 11462, 11470, 11472, 11473, 11476, 11496, 11500, 11504, 11505, 11511, 

11513, 11516, 11518, 11519, 11522 and 11523. 

Figure 3 

 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 13 

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. 

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11444, 11445, 11450, 11452, 11453, 11463, 11471, 

11474, 11475, 11477, 11484 thru 11489, 11492 thru 11495, 11497, 11503, 11509, 11512, 

11517, 11521, 11527 thru 11529, 11532, 11537 thru 11541, 11543, 11545, 11547, 11549, 

11551, 11554 thru 11556, 11558 thru 11560, 11564, 11565, 11568, 11569, 11572 and 

11573. 

Figure 4 

 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 14 

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.

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11536, 11553, 11561, 11562, 11566, 11567, 11570, 

11574, 11576 thru 11579 and 11581 thru 11583. 

Figure 5 

 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 15 

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. 

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11563, 11571and 11575. 

Figure 6 

 
Service Bulletin 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 16 

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.

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial numbers: 11580 and 11585. 

Figure 7 

 
Service Bulletin 

Fokker 70/100 

Jul 14/11 SBF100-24-044 

Page 17 

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. 

Rework of wiring on plug/receptacle P 4259B / J 4259A. 

Applicable for aircraft serial number: 11557. 

Figure 8 
Service Bulletin Reporting Quality Form 

Fokker 70/100 

SBF100-24-044 Jul 14/11 

Page 18 

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.

Service Bulletin Reporting Quality Form 

Use this Service Bulletin Reporting Quality 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 231 

2150 AE Nieuw-Vennep 

The Netherlands
Manual Change Notification – Maintenance Documentation 

Fokker 70/100 

JUL 14/11 MCNM F100-148

Page 1 of 1 

MCNM-F100-148 

Subject : Electrical Power – Removal of Galley Power Wiring from Production Break. 

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 SBF100-24-044. 

Effectivity : Refer to SBF100-24-044. 

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 Wiring Manual (WM). 

Change Note : 

 WM

 Update Chapter 24-54 (Galley Power Distribution), in accordance with the Figures given in 

SBF100-24-044. 

NOTE: If you have a Documentation Revision Service (DRS) with Fokker Services, this 

information will be included into your manuals at the earliest opportunity.