# Boeing Alert Service Bulletin MD80-30A132: No revision named - Rights: © The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2017-0805; AD 2018-07-04 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Boeing Alert Service Bulletin MD80-30A132](https://openairdocs.org/service-documents/boeing/md80-30a132.md) - Title as filed: SB-MD80-30A132 - Pages: 62 - PDF: https://openairdocs.org/files/sha256/7d/02/7d027fe299542686dc4f9f4b14d69fde87436a75b58688a40978eed7a3c04cef - Page: https://openairdocs.org/service-documents/boeing/md80-30a132/file/7d027fe29954 ## Text Some pages are 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 Commercial Airplanes MD80 Service Bulletin ALERT Number: MD80-30A132 Original Issue: April 28, 2017 ATA System: 3030 SUBJECT: ICE AND RAIN PROTECTION - Pitot and Static - Air Data Heat System Change Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 300-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws. 9E991ECCN: BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET Copyright © 2017 Boeing. Unpublished Work. All Rights Reserved. Treatment of this document and its content is governed by contract with Boeing. Rights to use this document are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The Boeing Company. Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KC-46, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8, Poseidon and Boeing liveries are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing. Original Issue: April 28, 2017 MD80-30A132 1 of 62 3.0 ### Page 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 2 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT BLANK PAGE ### Page 3 Table of Contents Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 2. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 27 K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 M. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28 2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 C. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 1. Kits/Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 2. Parts and Materials Supplied by the Operator . . . . . . . . . . . . . . . . . . . . . . . . 33 3. Parts Modified and Reidentified . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 4. Parts Removed and Not Replaced . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33 F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . 34 3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35 B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 FIGURE 1: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - RELAY BRACKET ASSEMBLY INSTALLATION [Group 2; Group 3, Configuration 2; Group 5] . . . . . . . . . . . . . . . 42 FIGURE 2: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - GROUND BRACKET INSTALLATION [Group 3, Configuration 2] . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 FIGURE 3: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - AFT RIGHT RADIO RACK - RELAYS AND SOCKETS INSTALLATION [Group 1-5] . . . . . . . . . . . . . . . . . . . . . . . . . 47 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING [Group 1-5] . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 FIGURE 5: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES [Group 1-5] . . . . . . . . . . . . . . . . . . 56 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 3 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 4 FIGURE 6: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT- AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES [Group 1-3] . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58 FIGURE 7: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT- AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES [Group 4-5] . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60 APPENDIX A: PART DEMAND INTENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 4 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 5 Commercial Airplanes MD80 Service Bulletin ALERT SummaryNumber: MD80-30A132Original Issue: April 28, 2017 ATA System: 3030 SUBJECT: ICE AND RAIN PROTECTION - Pitot and Static - Air Data Heat System Change THIS DOCUMENT IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH 1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER. CONCURRENT REQUIREMENTS None. BACKGROUND This service bulletin gives instructions to change the Air Data Heat (ADH) System. The accomplishment of this service bulletin will turn on the ADH system when the left and right fuel switches are set to the ON position. Air data sensors directly affect flight computers and flight deck instrumentation. The air data sensors have heaters to prevent blockage from ice formation in the sensor or from ice formation on the static plates. Incorrect airspeed indications can be the direct result of pitot tubes icing. Unheated Air Data sensors, mainly the pitot and static sensors, in icing conditions may result in irregular airspeed or altitude indications. If this service bulletin is not done, then failure of the Captain or First Officer to activate the ADH System can result in unsafe flight conditions. One operator reported that during takeoff, both the Captain's and First Officer's airspeed indications froze at 80 knots. The captain made the decision to continue the takeoff which resulted in an overboost of both engines. The flight was diverted to an alternate airport. A review of the weather at the departure airport indicated an Outside Air Temperature (OAT) of 25 degrees Fahrenheit and wind at approximately 20 knots in light snow. The airplane had been waiting in this weather condition for about two hours for de-icing before takeoff. A review of the flight data recorder from this event indicated the airspeed became irregular and could not be read during takeoff until the airplane reached 6000 feet Above Ground Level (AGL). The recorded data also indicated that the pitot tube was possibly blocked with ice. Boeing Service Related Problem (SRP) MD-80-SRP-30-0051 is related to this service bulletin. Boeing Fleet Team Digest (FTD) MD-80-FTD-30-15001 is related to this service bulletin. This table is provided to operators for planning purposes only. Refer to the applicable sections for more information. ReferenceAffectedPlanning Data Paragraph 1.A.2., Spares AffectedNoSpares Affected Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 5 of 62 ### Page 6 ReferenceAffectedPlanning Data Paragraph 1.E., Compliance and Paragraph 1.F., Approval YesAD Related Paragraph 1.H., Weight and Balance ChangesYesWeight and Balance Change Paragraph 1.I., Electrical Load DataYesElectrical Load Changed Paragraph 1.K., Publications AffectedYesPublications Affected Paragraph 1.K., Publications AffectedYesAirplane Flight Operations Affected (Flight Crew Operations Manual and/or FAA Approved Air- plane Flight Manual) Paragraph 2.C.1., Kits/PartsYesKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator YesOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION Group 1; Group 3, Configuration 1; Group 4: In the Electrical/Electronics (E/E) compartment and flight compartment do the following: – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 2, 5: In the E/E compartment and flight compartment do the following: – Install the new relay bracket assembly in the aft right radio rack STA 200. – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 3, Configuration 2: In the E/E compartment and flight compartment do the following: – Install the new relay bracket assembly in the aft right radio rack STA 200. – Install the new ground bracket in the aft right radio rack STA 200. – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 6: Contact Boeing to request the changes given in this service bulletin. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 6 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 7 Accomplishment of this service bulletin changes the flight deck and/or operations of the airplane. Refer to Paragraph 1.K., Publications Affected, for affected publications. EFFECTIVITY DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88 Airplane(s). Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplane(s). COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. Boeing recommends that the change given in this service bulletin be done within 28 months after the original issue date of this service bulletin. INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the changes given in this service bulletin. MANPOWER Refer to Paragraph 1.G., Manpower. MATERIAL INFORMATION Boeing Supplied Kits/Parts. Refer to Paragraph 2.A., Material - Price and Availability. Operators are encouraged to complete the survey provided in APPENDIX A of this service bulletin to help Boeing predict the quantity and timing of the Boeing Supplied Kits/Parts. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 7 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 8 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 8 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 9 Commercial Airplanes MD80 Service Bulletin ALERT Number: MD80-30A132 Original Issue: April 28, 2017 ATA System: 3030 SUBJECT: ICE AND RAIN PROTECTION - Pitot and Static - Air Data Heat System Change THIS DOCUMENT IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH 1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER. 1. PLANNING INFORMATION A. Effectivity 1. Airplanes This service bulletin is for the airplanes shown below. NOTE: The intent of this change was done on fuselage number 1443 prior to the Original Issue of this service bulletin in accordance with SP09300009 Drawing, Revision B. DESCRIPTIONCONFIGURATIONGROUP Airplanes with the relay bracket assembly installed in the aft right radio rack and SP09300009-7001 drawing configuration. -1 Airplanes without the relay bracket assembly installed in the aft right radio rack and SP09320009-7005 drawing configuration. -2 Airplanes with/without the relay bracket assembly installed in the aft right radio rack and different wiring configuration. -3 Airplanes with the relay bracket assembly installed in the aft right radio rack, SP09300009-7001 drawing configuration, and have accomplished MD80-28-058 service bulletin. 1 Airplanes without the relay bracket assembly installed in the aft right radio rack, SP09300009-7001 drawing configuration, and have not accomplished MD80-28-058 service bulletin. 2 Airplanes with the relay bracket installed in the aft right radio rack and SP09300009-7003 drawing configuration. -4 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 9 of 62 ### Page 10 DESCRIPTIONCONFIGURATIONGROUP Airplanes without the relay bracket installed in the aft right radio rack and SP09300009-7007 configuration. -5 Airplane operators that need to contact Boeing to request the changes given in this service bulletin. -6 Airplane Models: DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88 GroupFuselage Num- ber 2950 2953 2957 2962 2966 2969 2971 2978 2981 6986 2988 2992 2994 2999 21004 31005 61006 21011 61016 61018 - 1019 61031 61034 21045 61049 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 10 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 11 GroupFuselage Num- ber 61053 61055 61057 61059 - 1060 61068 - 1071 61075 31078 - 1079 31085 31088 - 1089 61090 - 1091 61095 - 1096 61098 61100 - 1102 61106 - 1107 61110 61112 61114 61117 61119 - 1121 61123 - 1125 61128 61133 - 1134 31137 - 1140 31142 61144 31151 - 1153 61154 - 1158 61160 61162 61164 - 1166 31171 61172 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 11 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 12 GroupFuselage Num- ber 61175 31178 - 1179 31181 31183 61187 31189 - 1190 61193 61196 - 1199 31203 31206 31210 31212 - 1213 31218 31220 31223 31226 31230 - 1231 31234 31238 - 1239 31243 - 1244 31247 31249 - 1252 31256 31258 31260 31263 31267 31269 31272 - 1273 31276 31279 - 1280 31283 - 1286 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 12 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 13 GroupFuselage Num- ber 31288 - 1290 31292 31295 31297 31300 - 1301 31303 31305 - 1307 31309 31311 - 1314 31316 - 1323 31325 31327 - 1328 31331 - 1332 31337 31340 31345 31347 - 1349 31352 - 1353 31355 - 1357 31362 - 1367 31370 - 1376 31378 - 1381 31384 - 1393 31395 31397 - 1399 31400 - 1402 61403 - 1404 31405 - 1406 31408 31413 - 1420 31423 - 1427 61429 - 1430 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 13 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 14 GroupFuselage Num- ber 31431 - 1436 61437 31439 - 1440 31443 - 1444 31446 - 1451 31453 - 1454 31459 - 1465 31467 - 1471 61472 31473 - 1475 31480 - 1487 31489 - 1493 31495 - 1499 31500 31503 31505 - 1507 31509 - 1511 31513 - 1516 31518 31520 - 1521 31523 - 1524 31526 - 1537 31540 61541 31543 31545 - 1548 31550 - 1551 31554 - 1555 31557 - 1571 31573 - 1588 31590 - 1593 31595 - 1597 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 14 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 15 GroupFuselage Num- ber 31599 31600 31602 - 1603 31605 - 1610 31612 - 1613 61614 31616 61617 31618 - 1619 31621 31623 31625 - 1629 61630 31632 31634 - 1635 31638 - 1645 31648 - 1655 31657 - 1666 31668 - 1669 31673 - 1680 31682 - 1692 31694 31697 - 1699 31700 - 1701 31703 31708 - 1713 61714 - 1716 31718 - 1720 61721 31722 - 1726 61727 31728 - 1729 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 15 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 16 GroupFuselage Num- ber 61730 31731 61733 31734 - 1738 61739 31740 61741 - 1742 31743 - 1744 61745 31746 - 1750 61751 31752 31754 - 1762 61763 31764 - 1770 61771 31773 - 1780 31782 31784 - 1787 31789 - 1797 31799 31800 - 1802 31804 - 1806 31808 - 1811 31813 - 1814 31816 - 1826 31828 - 1834 31836 - 1843 31845 61847 31848 - 1853 61854 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 16 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 17 GroupFuselage Num- ber 31857 - 1861 61862 31863 - 1864 61865 31866 61867 - 1868 31869 - 1870 61871 11872 31873 61874 31875 - 1876 61877 61879 31880 61881 31883 11886 31887 - 1889 31891 - 1896 61897 31898 11899 31900 - 1910 31912 - 1915 31917 - 1919 31921 11922 - 1924 11926 - 1928 61929 11931 - 1939 61940 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 17 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 18 GroupFuselage Num- ber 11941 - 1944 61945 11948 - 1952 11954 - 1966 11968 61969 11970 - 1973 61974 11978 - 1984 11986 - 1987 11989 - 1994 11996 - 1997 11999 12000 62001 12002 12004 - 2007 12009 - 2013 62014 - 2016 12019 - 2021 62022 - 2024 12026 - 2029 62031 12032 - 2034 12036 - 2040 12044 - 2045 12048 - 2060 12063 12065 - 2069 12071 12073 12075 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 18 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 19 GroupFuselage Num- ber 12077 - 2084 12086 - 2089 12091 - 2093 12101 42102 12103 - 2114 12116 12118 - 2119 12121 12124 12127 12130 12132 12134 - 2135 12137 12139 12145 12152 12167 12174 12176 12178 12180 12183 12185 12187 22189 52192 52196 52199 52201 22204 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 19 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 20 GroupFuselage Num- ber 52206 52208 22214 22218 52234 52239 52241 52244 52247 52249 52252 52254 52264 - 2287 2. Spares Affected None. B. Concurrent Requirements None. C. Reason This service bulletin gives instructions to change the Air Data Heat (ADH) System. The accomplishment of this service bulletin will turn on the ADH system when the left and right fuel switches are set to the ON position. Air data sensors directly affect flight computers and flight deck instrumentation. The air data sensors have heaters to prevent blockage from ice formation in the sensor or from ice formation on the static plates. Incorrect airspeed indications can be the direct result of pitot tubes icing. Unheated Air Data sensors, mainly the pitot and static sensors, in icing conditions may result in irregular airspeed or altitude indications. If this service bulletin is not done, then failure of the Captain or First Officer to activate the ADH System can result in unsafe flight conditions. One operator reported that during takeoff, both the Captain's and First Officer's airspeed indications froze at 80 knots. The captain made the decision to continue the takeoff which resulted in an overboost of both engines. The flight was diverted to an alternate airport. A review of the weather at the departure airport indicated an Outside Air Temperature (OAT) of 25 degrees Fahrenheit and wind at approximately 20 knots in light snow. The airplane had been waiting in this weather condition for about two hours for de-icing before takeoff. A review of the flight data recorder from this event indicated the airspeed became irregular and could not be read during takeoff until the airplane reached 6000 feet Above Ground Level (AGL). The recorded data also indicated that the pitot tube was possibly blocked with ice. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 20 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 21 Boeing Service Related Problem (SRP) MD-80-SRP-30-0051 is related to this service bulletin. Boeing Fleet Team Digest (FTD) MD-80-FTD-30-15001 is related to this service bulletin. D. Description Group 1; Group 3, Configuration 1; Group 4: In the Electrical/Electronics (E/E) compartment and flight compartment do the following: – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 2, 5: In the E/E compartment and flight compartment do the following: – Install the new relay bracket assembly in the aft right radio rack STA 200. – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 3, Configuration 2: In the E/E compartment and flight compartment do the following: – Install the new relay bracket assembly in the aft right radio rack STA 200. – Install the new ground bracket in the aft right radio rack STA 200. – Install two new relays in the aft right radio rack STA 200. – Install new wires to the flight compartment aft pedestal, STA 110 relay panel, STA 200 aft right radio rack relays, and STA 207 aft right radio rack ground bracket. – Do the Pitot/Stall Heater Off Light functional test and the Enhanced Air Data System test. Group 6: Contact Boeing to request the changes given in this service bulletin. Accomplishment of this service bulletin changes the flight deck and/or operations of the airplane. Refer to Paragraph 1.K., Publications Affected, for affected publications. The work in this service bulletin is done in the maintenance zone(s) given below. Group 1, 3, 6: Affected Maintenance Zones ZoneModel 44, 45DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC- 9-87 (MD-87), MD-88 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 21 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 22 Group 2: Affected Maintenance Zones ZoneModel 44, 45DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) Group 4-5: Affected Maintenance Zones ZoneModel 44, 45DC-9-83 (MD-83) E. Compliance The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. Boeing recommends that the change given in this service bulletin be done within 28 months after the original issue date of this service bulletin. F. Approval This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this service bulletin comply with the applicable regulations and are FAA approved, as well as European Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other approved Boeing changes. If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this service bulletin. G. Manpower The table below shows an estimate of the task hours necessary to do this change for each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task hour data if necessary. The estimate does not include lost time. These are some examples of lost time: • Time to adjust to the workplace • Time to schedule the work • Time to inspect the work • Time to cure the materials • Time to make the parts • Time to find the tools Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 22 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 23 Group 1; Group 3, Configuration 1: Elapsed HoursTask HoursNumber of PersonsTask 1.252.502Open Access 0.500.501FIGURE 3 24.0048.002FIGURE 4 0.601.202FIGURE 5 0.501.002FIGURE 6 1.252.502Close Access 0.300.301Test 28.4056.00TOTAL FOR EACH AIRPLANE Group 2: Elapsed HoursTask HoursNumber of PersonsTask 1.252.502Open Access 1.001.001FIGURE 1 0.500.501FIGURE 3 24.0048.002FIGURE 4 0.601.202FIGURE 5 0.501.002FIGURE 6 1.252.502Close Access 0.300.301Test 29.4057.00TOTAL FOR EACH AIRPLANE Group 3, Configuration 2: Elapsed HoursTask HoursNumber of PersonsTask 1.252.502Open Access 1.001.001FIGURE 1 1.001.001FIGURE 2 0.500.501FIGURE 3 24.0048.002FIGURE 4 0.601.202FIGURE 5 0.501.002FIGURE 6 1.252.502Close Access 0.300.301Test Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 23 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 24 Group 3, Configuration 2: Elapsed HoursTask HoursNumber of PersonsTask 30.4058.00TOTAL FOR EACH AIRPLANE Group 4: Elapsed HoursTask HoursNumber of PersonsTask 1.252.502Open Access 0.500.501FIGURE 3 24.0048.002FIGURE 4 0.601.202FIGURE 5 0.501.002FIGURE 7 1.252.502Close Access 0.300.301Test 28.4056.00TOTAL FOR EACH AIRPLANE Group 5: Elapsed HoursTask HoursNumber of PersonsTask 1.252.502Open Access 1.001.001FIGURE 1 0.500.501FIGURE 3 24.0048.002FIGURE 4 0.601.202FIGURE 5 0.501.002FIGURE 7 1.252.502Close Access 0.330.331Test 29.4057.00TOTAL FOR EACH AIRPLANE Group 6: None. H. Weight and Balance Changes Change in Moment (Pound-Inches) Change in Weight (Pounds) Approximate Station (Inches)Airplane +891.1+5.4164.7Group 1 +1139.6+6.9164.7Group 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 24 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 25 Change in Moment (Pound-Inches) Change in Weight (Pounds) Approximate Station (Inches)Airplane +891.1+5.4164.7Group 3, Configuration 1 +1152.4+7.0164.7Group 3, Configuration 2 +891.1+5.4164.7Group 4 +1140.2+6.9164.7Group 5 Group 6: None. I. Electrical Load Data 1. Direct Current (DC) Load Changes Not changed. 2. Alternating Current (AC) Load Changes Group 1-5: VAC/Phase PF 115 C UNITS %OPR 1 100 E/NE E UNIT LOAD (W) 5 NOTES (B1-415) SUPPLIER Leach Inter- national EQUIPMENT NAME PART NUMBER Left Fuel Switch Re- lay 5D0024-1 ITEM 4503 R2- 1505 CHAP 300 BUS 1L AVERAGE WATTS% TIME OPR 15/30 M2/5 M5 S15/30 M2/5 MCONDITION 011030LOADING 011030START 0550100TAXI 555100100TAKEOFF & CLIMB 555100100CRUISE COLD 555100100CRUISE HOT 555100100DESCENT & LAND 00000EMERGENCY 00000GROUND SERVICE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 25 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 26 Group 1-5: VAC/Phase PF 115 C UNITS %OPR 1 100 E/NE E UNIT LOAD (W) 5 NOTES (B1-416) SUPPLIER Leach Inter- national EQUIPMENT NAME PART NUMBER Right Fuel Switch Relay 5D0024-1 ITEM 4504 R2- 1506 CHAP 300 BUS 2R AVERAGE WATTS% TIME OPR 15/30 M2/5 M5 S15/30 M2/5 MCONDITION 011030LOADING 011030START 0550100TAXI 555100100TAKEOFF & CLIMB 555100100CRUISE COLD 555100100CRUISE HOT 555100100DESCENT & LAND 00000EMERGENCY 00000GROUND SERVICE Group 6: Not changed. J. References 1. Existing Data: a. Standard Overhaul Practices Manual (SOPM) 20-50-01 b. Standard Wiring Practices Manual (SWPM) 20-00-03, 20-00-09, 20-00-13, 20-00-16, 20-10-01, 20-10-04, 20-20-01, 20-20-03, 20-50-01 c. MD-80 Aircraft Maintenance Manual (AMM) 06-24-00, 06-31-00, 23-20-02, 23-21-00, 23-24-01, 23-50-02, 24-00-00, 25-13-00, 25-13-01, 30-30-00, 33-11-02, 33-16-00, 34-21-13, 34-25-03, 34-41-03, 34-53-04, 34-54-02, 34-59-03, 34-63-01, 53-20-01 d. MD-80 Fleet Team Digest (FTD) 30-15001 e. MD-80 Wiring Diagram Manual (WDM) 30-31-01, 30-31-02, 74-11-00 f. Boeing Service Related Problem (SRP) MD-80-SRP-30-0051 g. Boeing Service Bulletin MD80-28-58 h. Approved Equivalents Parts List (AEPL) Drawing 7595071 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 26 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 27 2. Data Supplied with this Service Bulletin: None. 3. Installation Drawings Used in the Preparation of this Service Bulletin: Group 1-5: ChangeTitleDocument Number CENHANCED ACTUATION OF THE AIR DATA HEAT (ADH) SYSTEM SPECIAL PRODUCT DRAWING SP09300009 The table above lists the applicable drawing used to prepare this service bulletin. The drawing is not necessary to make the specified changes, and is not supplied with this service bulletin. The drawing may not be applicable to all airplane configurations or operators. Group 6: None. K. Publications Affected 1. Publications: Group 1-5: Chapter-SectionPublication Volume 2, Chkl.130, Chkl.160Flight Crew Operations Manual 25-53Illustrated Parts Catalog 30-31, 74-11Wiring Diagram Manual 23-30, 30-30, 31-31, 74-00, 76-12Aircraft Maintenance Manual 30-30, 76-13Schematic Manual Group 6: None. 2. Damage Tolerance Based Structural Inspections: Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the Maintenance Program. This service bulletin does not affect FCS, therefore DTIs are not necessary. L. Interchangeability and Intermixability of Parts Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 27 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 28 M. Software Accomplishment Summary Not affected. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 28 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 29 2. MATERIAL INFORMATION A. Material - Price and Availability Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary for Each Airplane. Operators are encouraged to share schedule requirements with Boeing for incorporation of the service bulletin. The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment. Prices are in United States Dollars. Terms: Net 30 days. Reference this service bulletin and submit your purchase order by one of these methods: 1. Order on-line via ATA Spec 2000 or The Boeing PART Page 2. Fax to (206) 662-7145 Group 1-3: REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Unit Price as of the original issue date of this Ser- vice Bulletin (US Dollars) ROLT as of the original issue date of this Ser- vice Bulletin (Cal- endar Days) NameKit Number $4,459.00120SERVICE KIT - ENHANCED ACTUATION OF THE AIR DATA HEAT (ADH) SYSTEM SA09300132-3 Group 4-5: REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Unit Price as of the original issue date of this Ser- vice Bulletin (US Dollars) ROLT as of the original issue date of this Ser- vice Bulletin (Cal- endar Days) NameKit Number $4,479.00120SERVICE KIT - ENHANCED ACTUATION OF THE AIR DATA HEAT (ADH) SYSTEM SA09300132-5 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 29 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 30 Group 2; Group 3, Configuration 2; Group 5: REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Unit Price as of the original issue date of this Ser- vice Bulletin (US Dollars) ROLT as of the original issue date of this Ser- vice Bulletin (Cal- endar Days) NameKit Number $6,555.00120SERVICE KIT - RELAY BRACKET ASSEM- BLY INSTALLATION SA09300132-7 Group 3, Configuration 2: REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Unit Price as of the original issue date of this Ser- vice Bulletin (US Dollars) ROLT as of the original issue date of this Ser- vice Bulletin (Cal- endar Days) NameKit Number $1,705.00120SERVICE KIT - GROUND BRACKET IN- STALLATION SA09300132-9 Group 6: None. Operators are encouraged to complete the survey provided in APPENDIX A of this service bulletin to help Boeing predict the quantity and timing of the Boeing Supplied Kits/Parts. B. Industry Support Information Boeing warranty remedies are not available for the changes given in this service bulletin. C. Parts Necessary for Each Airplane 1. Kits/Parts To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability. NOTE: One top kit and the items shown in Paragraph 2.C.2., Parts and Materials Supplied by the Operator, are necessary for each airplane. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 30 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 31 Group 1-3: Kit SA09300132 MORE DATANameQTYNew Part Number -101-3 SERVICE KIT - ENHANCED ACTUATION OF THE AIR DATA HEAT (ADH) SYSTEM .-SA09300132-3 WIRE KIT-1SA09300132-101 (a)SOCKET.25D0020-10 (a)RELAY.25D0024-1 (a)TERMINAL LUG 76612.5D0086-26 (a)TERMINAL LUG 7616.5D0086-5 (a)TERMINAL LUG 7622.5D0086-6 WIRE CODE 801415 FT.D2426-1C-16NM WIRE CODE 801275 FT.D2426-1C-20NM SKT T/C 112320.DC39-16S (a)SOCKET T/C 7064.LRC16M-32DJ5 (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. Group 4-5: Kit SA09300132 MORE DATANameQTYNew Part Number -102-5 SERVICE KIT - ENHANCED ACTUATION OF THE AIR DATA HEAT (ADH) SYSTEM .-SA09300132-5 WIRE KIT-1SA09300132-102 (a)SOCKET.25D0020-10 (a)RELAY.25D0024-1 (a)TERMINAL LUG 76612.5D0086-26 (a)TERMINAL LUG 7616.5D0086-5 (a)TERMINAL LUG 7622.5D0086-6 WIRE CODE 801415 FT.D2426-1C-16NM WIRE CODE 801275 FT.D2426-1C-20NM SKT T/C 112320.DC39-16S Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 31 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 32 Group 4-5: Kit SA09300132 MORE DATANameQTYNew Part Number -102-5 (a)SOCKET T/C 7064.LRC16M-32DJ5 (a)END CAP T/C 9154.CYW16 (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. Group 2; Group 3, Configuration 2; Group 5: Kit SA09300132 MORE DATANameQTYNew Part Number -7 SERVICE KIT - RELAY BRACKET ASSEMBLY INSTALLATION -SA09300132-7 BRACKET ASSEMBLY15939723-503 (a)SCREW2NAS1096-3-8 (a)SPACER2NAS43DD3-5FC (a)SCREW2NAS514P1032-7 (a)SCREW2S124682-3D10-6 (a)WASHER4NAS1252-10L (a)NUT4MS21042L3 (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. Group 3, Configuration 2: Kit SA09300132 MORE DATANameQTYNew Part Number -9 SERVICE KIT - GROUND BRACKET INSTALLATION -SA09300132-9 BRACKET1ABN7294-627 (a)NUT2MS21042L3 (a)LOCK WASHER2MS35338-43 (a)SCREW2NAS1096-3-7 (a)SCREW2NAS1096-3-11 (a)WASHER2NAS1252-10L Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 32 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 33 Group 3, Configuration 2: Kit SA09300132 MORE DATANameQTYNew Part Number -9 (a)WASHER2NAS1149F0332P (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. Group 6: None. 2. Parts and Materials Supplied by the Operator The following parts or materials are necessary to do the change in this service bulletin. Parts and materials in the manuals given in Paragraph 1.J., References, can also be necessary. Examine operator part and material supply to make sure all necessary parts and materials are available. Group 1-5: NotesNameQTYPart Number / Specification (a)STRING TIE-18XTZ, 23XTZ (DMS 2089) or Equivalent (a) For new wire installation. Use the quantity needed to do the changes given in this service bulletin. Group 6: None. 3. Parts Modified and Reidentified None. 4. Parts Removed and Not Replaced None. D. Parts Necessary to Change Spares None. E. Special Tooling - Price and Availability None. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 33 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 34 F. Special Tooling Necessary to do this Service Bulletin No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance and overhaul tools in the manuals given in Paragraph 1.J., References, can be necessary. Examine operator tool supply to make sure all necessary tools are available. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 34 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 35 3. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL INFORMATION WARNING: IF ELECTRICAL POWER IS APPLIED TO THE AIRPLANE, MAKE SURE YOU OBEY ALL PRECAUTIONS WHILE YOU DO WORK. IF YOU DO NOT OBEY THE PRECAUTIONS, DEATH OR INJURY TO PERSONS, AND DAMAGE TO THE AIRPLANE CAN OCCUR. CAUTION: ELECTRICALLY GROUND THE AIRPLANE. THIS WILL HELP TO PREVENT DAMAGE TO THE AIRPLANE OR EQUIPMENT. CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL, METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR OTHER ELECTRICAL DAMAGE. NOTE: 1. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for definition of the acronyms. 2. Equivalent parts are listed in the AEPL, Drawing 7595071. 3. If the length of any fastener specified in this service bulletin does not meet installation standards given in Structural Repair Manual (SRM) Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used. In addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51. Refer to SOPM 20-50-01 for alternate full threaded fasteners (screws) needed for installation in this service bulletin. If the length of any fastener specified in this service bulletin does not meet installation standards, fasteners of the same specification or an approved AEPL part with grip length longer or shorter may be used. Make sure that if a longer screw is used, it does not interfere with or chafe any wiring or adjacent installation. 4. Use the approved fastener and process material substitutions, in accordance with MD-80 SRM 51. 5. Unless shown differently, these dimensions and tolerances are used: – Linear dimensions are in inches – Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus or minus 0.03 inch. – Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch – Angular tolerance is plus or minus 2 degrees – Hole dimensions for standard solid rivets are in MD-80 SRM 51. – Torque Values: — Values for structural fasteners are given in MD-80. Structural Repair Manual, Chapter 51. — Values for airframe maintenance tasks are included in Chapter 20 of MD-80 Aircraft Maintenance Manual (AMM). Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 35 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 36 — Values for electrical maintenance tasks are included in Chapter 20 of Standard Wiring Practices Manual (SWPM). — Values for engine maintenance tasks are included in Chapter 70 of MD-80 Aircraft Maintenance Manual (AMM). — Non-standard torque values for maintenance tasks are included in the applicable installation step. 6. Refer to SWPM 20-10-01 as accepted wire installation procedures. Refer to these SWPM chapters for applicable operations, as accepted procedures: – Identification of electrical wires, refer to SWPM 20-00-03 as an accepted procedure. – Electrical wire end terminal codes, refer to SWPM 20-00-16 as an accepted procedure. – Alternative wire type list, refer to SWPM 20-00-13 as an accepted procedure. – Wiring Installation, refer to SWPM 20-10-01 as an accepted procedure. – Coil and stow excess wire length, refer to SWPM 20-10-04 as an accepted procedure. – Electrical identification and shop practice, refer to SWPM 20-00-09 as an accepted procedure. – Installation of STA strap to existing wire bundle, refer to SWPM 20-10-01 as an accepted procedure. – Terminals - maintenance practices, refer to SWPM 20-20-01 as an accepted procedure. – Rivnut grounds and hardware installation, Refer to SWPM 20-20-03 as an accepted procedure. – Electrical bonding, refer to SWPM 20-50-01 as an accepted procedure. 7. Where parallel wire assemblies make contact due to space limitations, install a spacer to maintain category separation. Refer to SWPM 20-10-01 as an accepted procedure. 8. Obey all of the warnings and cautions given in the specified manual sections. 9. These work instructions refer to procedures included in other Boeing documents. When the words "refer to" are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words "in accordance with" are included in the instruction, the procedure in the Boeing document must be used. 10. If it is necessary to remove more parts for access, you can remove those parts. If you can get access without removing identified parts, it is not necessary to remove all of the identified parts. Jacking and shoring limitations must be observed. 11. Where the work instructions include installation of a kept part, a new or serviceable part with the same part number can be installed as an alternative to the kept part. 12. This service bulletin includes functional test procedures for the systems changed by this service bulletin. More functional tests can possibly be necessary in accordance with standard maintenance practices because of interruption to other airplane systems. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 36 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 37 13. If shading is used, shaded areas in Figures are reference only. Shaded areas in Figures may look different than your airplane. 14. Use of colors in Figures is based on guidance from the ATA e-Business Program (ATA) iSpec 2200. 15. Some steps in the Work Instructions are labeled as Required for Compliance (RC). If this service bulletin is mandated by an Airworthiness Directive (AD), then the steps labeled as RC, including sub-steps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or sub-step is labeled "RC Exempt," then the RC requirement is removed from that step or sub step. An Alternative Method of Compliance (AMOC) is required for any deviations to RC steps, including sub-steps and identified figures. Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC. This is provided that the RC steps, including sub-steps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. B. WORK INSTRUCTIONS Group 1-5: 1. RC Exempt - Remove electrical power from the airplane. Refer to MD-80 AMM 24-00-00 as an accepted procedure. 2. RC Exempt - Open the Electrical/Electronics (E/E) compartment access door 4501A. Refer to MD-80 AMM 06-24-00 as an accepted procedure. 3. Group 2; Group 3, Configuration 2; Group 5: RC - In the E/E compartment install the new relay bracket assembly in the aft right radio rack, in accordance with FIGURE 1. 4. Group 3, Configuration 2: RC - In the E/E compartment install the new ground bracket in the aft right radio rack, in accordance with FIGURE 2. 5. RC - Install new relays in the aft right radio rack in accordance with FIGURE 3. 6. RC Exempt - In the flight compartment remove and keep the captain's seat to get access to the work area. Refer to MD-80 AMM 25-13-01 as an accepted procedure. 7. RC Exempt - In the flight compartment remove and keep the captain's writing table to get access to the work area. Refer to MD-80 AMM 25-13-00 as an accepted procedure. 8. RC Exempt - In the flight compartment remove and keep the access panels 4403A, 4405A and 4431A to get access to the work area. Refer to MD-80 AMM 06-31-00 to locate the panels. 9. RC Exempt - In the flight compartment remove and keep the floor panels at STA 120, between the aft pedestal and the captain's side console, to get access to the work area. Refer to MD-80 AMM 53-20-01 as an accepted procedure. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 37 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 38 10. RC Exempt - In the flight compartment remove and keep the pedestal side access panels and remove and keep the control panels in the aft pedestal to get access to the work area. Refer to the applicable MD-80 AMM chapters that follow as an accepted procedure: MD-80 AMM ReferenceControl Panel Name (a) MD-80 AMM 34-25-03Head Up Display (HUD) Control Panel MD-80 AMM 34-41-03Weather Radar Control Panel MD-80 AMM 33-11-02Center Instrument And Pedestal Lights Control Panel MD-80 AMM 23-21-00Selective Calling (SELCAL) Control Panel MD-80 AMM 34-53-04Automatic Direction Finder (ADF) Control Panel MD-80 AMM 23-20-02Very High Frequency (VHF) Control Panel MD-80 AMM 34-59-03Multifunction Control Display Unit (MCDU) Control Panel MD-80 AMM 34-63-01Performance Management System (PMS) Control Display Unit (CDU) Control Panel MD-80 AMM 34-54-02Air Traffic Control (ATC) Transponder Control Panel MD-80 AMM 23-50-02Audio Control Panel MD-80 AMM 33-16-00Checklist Panel MD-80 AMM 34-21-13AHRS Compass Controller MD-80 AMM 23-24-01Automatic Communication Addressing and Reporting System (ACARS) Control Panel (a) This table may not include all the control panels that could be installed in the aft pedestal. Refer to the applicable MD-80 AMM chapter to get the instructions to put back the control panels that were removed for access. 11. Group 1-3: RC - Install new wires between the flight compartment aft pedestal and the E/E compartment STA110 relay panel and the aft right radio rack in accordance with FIGURE 4, FIGURE 5 and FIGURE 6. 12. Group 4-5: RC - Install new wires between the flight compartment aft pedestal and the E/E compartment STA110 relay panel and the aft right radio rack in accordance with FIGURE 4, FIGURE 5 and FIGURE 7. 13. RC Exempt - Supply electrical power to the airplane. Refer to MD-80 AMM 24-00-00 as an accepted procedure. 14. RC - Do the tests that follow: Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 38 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 39 CAUTION: IN ORDER TO AVOID ANY POTENTIAL HAZARD OR DAMAGE TO EQUIPMENT IT IS RECOMMENDED THAT POWER AND GROUND CONNECTIONS, IF AFFECTED AS PART OF THIS MODIFICATION, BE VERIFIED BY APPROPRIATE SHOP TOOLS AND PROCEDURES, PRIOR TO APPLICATION OF POWER. CAUTION: IN ORDER TO ASSURE THE INTEGRITY OF THE AIRCRAFT AFTER THE WORK IS COMPLETED IT IS EXPECTED THAT ALL APPLICABLE RETURN TO SERVICE TESTS WILL BE PERFORMED ON ALL THE SYSTEMS DIRECTLY OR INDIRECTLY AFFECTED BY THIS MODIFICATION. CAUTION: POTENTIAL ELECTRICAL POWER HAZARD EXISTS WHEN PERFORMING THIS TEST. USE APPLICABLE SHOP PROCEDURES AS REQUIRED. CAUTION: PRIMARY COMPONENTS INSTALLED DURING THIS MODIFICATION CONTAIN ELECTROSTATIC DISCHARGE (ESD) SENSITIVE MICROELECTRONIC SEMICONDUCTOR COMPONENTS. USE PROPER PERSONAL GROUNDING, ENCLOSURE, AND SHIELDING PROCEDURES WHEN WORKING AROUND THIS EQUIPMENT AND ASSOCIATED WIRING. a. Do the test of the Pitot/Stall Heater Off Light. Refer to MD-80 AMM 30-30-00, "Test PITOT/STALL HEATER OFF Light" as an accepted procedure. If the Pitot/Stall Heater Off Light test fails, do corrective actions, repeat the test, and do corrective actions until the Pitot/Stall Heater Off Light passes the test. NOTE: Leave the airplane in the same configuration after the Pitot/Stall Heater Off Light test has been completed. b. Do the Enhanced Air Data System Test that follows: (1) Make sure that the ICE PROTECTION METER SEL & HEAT switch is in the OFF position. (2) Make sure that the PITOT/STALL HEATER OFF light located on the OAP (Overhead Annunciator Panel) or the EOAP (Electronic Overhead Annunciator Panel) is on. (3) Set the R FUEL SHUTOFF LEVER to the ON position. (4) Make sure that the PITOT/STALL HEATER OFF light is on. (5) Set the R FUEL SHUTOFF LEVER to the OFF position. (6) Make sure that the PITOT/STALL HEATER OFF light is on. (7) Set the L FUEL SHUTOFF LEVER to the ON position. (8) Make sure that the PITOT/STALL HEATER OFF light is on. (9) Set the L FUEL SHUTOFF LEVER to the OFF position. (10) Make sure that the PITOT/STALL HEATER OFF light is on. (11) Set the L FUEL SHUTOFF LEVER and R FUEL SHUTOFF LEVER to the ON position. (12) Make sure that the PITOT/STALL HEATER OFF light is off. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 39 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 40 (13) If the Enhanced Air Data System test fails, do corrective actions, repeat the test, and do corrective actions until the Enhanced Air Data System passes the test. 15. RC Exempt - In the flight compartment put back the pedestal side access panels and put back the control panels in the aft pedestal that were removed for access. Refer to the applicable MD-80 AMM chapters that follow as an accepted procedure: MD-80 AMM ReferenceControl Panel Name (a) MD-80 AMM 34-25-03Head Up Display (HUD) Control Panel MD-80 AMM 34-41-03Weather Radar Control Panel MD-80 AMM 33-11-02Center Instrument And Pedestal Lights Control Panel MD-80 AMM 23-21-00Selective Calling (SELCAL) Control Panel MD-80 AMM 34-53-04Automatic Direction Finder (ADF) Control Panel MD-80 AMM 23-20-02Very High Frequency (VHF) Control Panel MD-80 AMM 34-59-03Multifunction Control Display Unit (MCDU) Control Panel MD-80 AMM 34-63-01Performance Management System (PMS) Control Display Unit (CDU) Control Panel MD-80 AMM 34-54-02Air Traffic Control (ATC) Transponder Control Panel MD-80 AMM 23-50-02Audio Control Panel MD-80 AMM 33-16-00Checklist Panel MD-80 AMM 34-21-13AHRS Compass Controller MD-80 AMM 23-24-01Automatic Communication Addressing and Reporting System (ACARS) Control Panel (a) This table may not include all the control panels that could be installed in the aft pedestal. Refer to the applicable MD-80 AMM chapter to get the instructions to put back the control panels that were removed for access. 16. RC Exempt - In the flight compartment put back the floor panels that were removed for access. Refer to MD-80 AMM 53-20-01 as an accepted procedure. 17. RC Exempt - In the flight compartment put back the access panels 4403A, 4405A and 4431A that were removed for access. Refer to MD-80 AMM 06-31-00. 18. RC Exempt - In the flight compartment put back the captain's writing table that was removed for access. Refer to MD-80 AMM 25-13-00 as an accepted procedure. 19. RC Exempt - In the flight compartment put back the captain's seat that was removed for access. Refer to MD-80 AMM 25-13-01 as an accepted procedure. 20. RC Exempt - Close the E/E compartment access door 4501A. Refer to MD-80 AMM 06-24-00 as an accepted procedure. 21. Put the airplane back to serviceable condition. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 40 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 41 Group 6: 1. Contact Boeing for change instructions and do the change instructions provided by Boeing. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 41 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 42 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 2; Group 3, Configuration 2; Group 5. ....00 ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT X = -44.00 STA PLENUM 200 • RAIL (2 LOCATIONS) A-A (4.88) RELAY BRACKET ASSEMBLY AFT RIGHT RADIO RACK 2534533 FIGURE 1: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - RELAY BRACKET ASSEMBLY INSTALLATION (SHEET 1 OF 2) Original Issue: April 28, 2017 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING MD80-30A132 Work - See page 1 for details. 42 of 62 ### Page 43 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for this figure. More DataQtyIdentificationNameTaskStep 15939723-503BRACKET ASSEMBLYLocate1 15939723-503BRACKET ASSEMBLYInstall (New)2 2NAS1096-3-8SCREWInstall (New) 2NAS43DD3-5FCSPACERInstall (New) (a)2S124682-3D10-6WASHERInstall (New) (b)2NAS1252-10LWASHERInstall (New) 2MS21042L3NUTInstall (New) 2NAS514P1032-7SCREWInstall (New)3 2NAS1252-10LWASHERInstall (New) 2MS21042L3NUTInstall (New) (a) Install S124682-3D10-6 washer between NAS1096-3-8 screwhead and NAS43DD3-5FC spacer. (b) Install NAS1252-10L washer between MS21042L3 nut and rail. FIGURE 1: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - RELAY BRACKET ASSEMBLY INSTALLATION (SHEET 2 OF 2) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 43 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 44 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 3, Configuration 2. ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT -44.00 88 STA 200 •0a0000aa0a0 0.0.0....0.000000 RELAY BRACKET ASSEMBLY AFT RIGHT RADIO RACK 2569625 FIGURE 2: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - GROUND BRACKET INSTALLATION (SHEET 1 OF 3) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished MD80-30A132 Work - See page 1 for details. 44 of 62 ### Page 45 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT STA 200 (7.88) (2 LOCATIONS) B-B A-A BRACKET GROUND TERMINAL LUG (2 LOCATIONS) C-C 2569628 FIGURE 2: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - GROUND BRACKET INSTALLATION (SHEET 2 OF 3) Original Issue: April 28, 2017 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING MD80-30A132 Work - See page 1 for details. 45 of 62 ### Page 46 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for this figure. More DataQtyIdentificationNameTaskStep (a) (b)1ABN7294-627BRACKETInstall (New)1 2NAS1096-3-7SCREWInstall (New) 2NAS1252-10LWASHERInstall (New) 2MS21042L3NUTInstall (New) (f)2NAS1096-3-11SCREWInstall (New)2 (f)2MS35338-43LOCK WASHERInstall (New) (f)2NAS1149F0332PWASHERInstall (New) (c) (e)---Identify3 (d) (e)---Identify4 (a) Do a Faying Surface Preparation Procedure between the bracket surface and the mating structure. Refer to SWPM 20-50-01 as an accepted procedure. (b) Measure the electrical bond resistance between the surfaces common to the bracket and the mating structure. Make sure the bond resistance is not greater than 0.0025 ohms. Refer to SWPM 20-50-01 as an accepted procedure. (c) Ink stamp the ground number "4234" on the bracket. Refer to SWPM 20-00-09 as an accepted procedure. Use ink color black, text height 0.18 inches minimum. The marking must be visible after the bracket is installed. (d) Ink stamp the ground number "4235" on the bracket. Refer to SWPM 20-00-09 as an accepted procedure. Use ink color black, text height 0.18 inches minimum. The marking must be visible after the bracket is installed. (e) As an option to ink stamp marking install adhesive backed markers. Refer to SWPM 20-00-09 as an ac- cepted procedure. (f) Loose install. The ground terminal lug is installed in another figure and electrical bonding will be completed at that time. FIGURE 2: MAIN EQUIPMENT CENTER - AFT RIGHT RADIO RACK - GROUND BRACKET INSTALLATION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 46 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 47 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 1-5. R5-1505 R2-1505 R5-1506 R2-1506 STA 200 ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AFT RIGHT RADIO RACK 6 LOCATIONS (TYPICAL) 6 LOCATIONS ( 6 LOCATIONS 2 2) 2 LOCATIONS 1 2 LOCATIONS AFT RIGHT RADIO RACK 6 LOCATIONS (TYPICAL) 6 LOCATIONS 1 2529376 FIGURE 3: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - AFT RIGHT RADIO RACK - RELAYS AND SOCKETS INSTALLATION (SHEET 1 OF 2) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING MD80-30A132 PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 47 of 62 ### Page 48 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for this figure. More DataQtyIdentificationNameTaskStep (a) (b) (f)25D0020-10SOCKETInstall (New)1 (a)6-WASHERInstall (New) (a)6-NUTInstall (New) (a) (b) (f)25D0024-1RELAYInstall (New)2 (a)12-WASHERInstall (New) (a)6-NUTInstall (New) (c) (e)2--Identify3 (d) (e)2--Identify4 (a) Relay and relay socket mounting hardware are furnished with the relays. (b) Install the relay and relay socket in the next available location on the aft right radio rack. (c) Ink stamp the relay number "R2-1505" and relay socket number "R5-1505" on the structure, adjacent to the equipment. Refer to SWPM 20-00-09 as an accepted procedure. Use ink color black, text height 0.18 inches minimum. The marking must be visible after the relay and socket are installed. (d) Ink stamp the relay number "R2-1506" and relay socket number "R5-1506" on the structure, adjacent to the equipment. Refer to SWPM 20-00-09 as an accepted procedure. Use ink color black, text height 0.18 inches minimum. The marking must be visible after the relay and socket are installed. (e) As an option to ink stamp marking install adhesive backed markers. Refer to SWPM 20-00-09 as an ac- cepted procedure. (f) Or approved equivalent. Refer to AEPL, Drawing 7595071. FIGURE 3: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - AFT RIGHT RADIO RACK - RELAYS AND SOCKETS INSTALLATION (SHEET 2 OF 2) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 48 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 49 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 1-5. ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT A 51-3 P1-429- S1-4 P1-430 • AAB FLIGHT COMPARTMENT AFT PEDESTAL STA 2529425 120.05 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 1 OF 7) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING MD80-30A132 PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 49 of 62 ### Page 50 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 2 OF 7) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 50 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 51 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT STA 148.550 STA 141.248 STA 125.800 AAB STA 120.050 STA 110.000 STA 2529970 101.550 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 3 OF 7) Original Issue: April 28, 2017 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING MD80-30A132 Work - See page 1 for details. 51 of 62 ### Page 52 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT STA 160 AAC AAB • AAJ 2530039 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 4 OF 7) Original Issue: April 28, 2017 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING MD80-30A132 Work - See page 1 for details. 52 of 62 ### Page 53 FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 5 OF 7) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 53 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 54 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT STA 133.425 STA 160 GND 4234 GND 4235 AC STA 200 AAC STA 160 R5-1505 RAF R2-1505 R5-1506 R2-1506 STA 200 AFT RIGHT RADIO RACK 2529711 (TYPICAL) FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 6 OF 7) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished MD80-30A132 Work - See page 1 for details. 54 of 62 ### Page 55 The wires are contained in Wire Kits SA09300132-101 or SA09300132-102 and the String Tie is operator supplied. FIGURE 4: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT - AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRE ROUTING (SHEET 7 OF 7) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 55 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 56 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 1-5. 3 LOCATIONS (1123 (AAJ, AAC, RAF) D3 (1123) 3 LOCATIONS F951D16- (AAJ, AAC, RAF) 415 IN. D1 F1664C16- (AAJ, AAC, RAF) СЗ 415 IN F952C16- C2 (AAJ, AAC, RAF 415 IN. C1 • F1663C16• (AAJ, AAC, RAF) ВЗ 415 IN. F950D16 - B2 AAJ, AAC, RAF 415 IN. - F1662C16- 415 IN. R5-1506 R2-1506 R5-1506 RIGHT FUEL SW RELAY 3 LOCATIONS (1123) (AAJ, AAC, RAF) D3 (1123) 3 LOCATIONS F951C16• -D2 (AAJ, AAC, RAF 415 IN. D1 F1664B16 (AAJ, AAC, RAF) СЗ 415 IN. F952B16• C2 AAJ, AAC, RAF 415 IN. F1663B16 (AAU, AAC, RAF) -ВЗ 415 IN. F950C16• - B2 (AAJ, AAC, RAF) 415 IN. F1662B16 AFT RIGHT R5-1505 R2-1505 R5-1505 415 IN. RADIO RACK LEFT FUEL SW RELAY STA 200 2 LOCATIONS (766 (766) 2 LOCATIONS - F950B16- A1 | A2 - F1662A16- R2-97 CAPT PITOT HEATER 4 LOCATIONS (766 (766) 4 LOCATIONS - F952A16- - F1663A16- B1 B2 - F951B16 - F1664A16-→ F/O AND AUX PITOT HEATER A1 R2-98 A2 STA 110 RELAY PANEL ADDED WIRE OR NEW ROUTING + DELETED WIRE OR FORMER ROUTING EXISTING WIRE TERMINAL CODE FIGURE 5: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES (SHEET 1 OF 2) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING MD80-30A132 PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 56 of 62/ ### Page 57 REFERENCE: MD-80 WDM 30-31-01 The Terminal Code numbers shown below agree with the number shown in the Terminal Code symbol in this figure. NOTESQTYIDENTIFICATIONNAMETERMINAL CODE (a)125D0086-26TERMINAL LUG 766766 12DC39-16SSKT T/C 11231123 (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. FIGURE 5: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT - STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES (SHEET 2 OF 2) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 57 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 58 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 1-3. 3 LOCATIONS (1123 AAJ, AAC, RAF АЗ (1123 2F988D20 A2 (AAJ, AAC, RAF) 415 IN. • 2F965B20 OFF (706) 2 LOCATIONS (AAB, AAC, RAF) 415 IN. 2F991A20 450 IN. (RAF) F971B20N= X2 ON 150 IN. R FUEL SHUTOFF P1-430 S1-4 R5-1506 R2-1506 R5-1506 RIGHT FUEL SW RELAY AFT RIGHT RADIO RACK STA 200 OFF 706) 2 LOCATIONS 761) 3 LOCATIONS ON - 2086020 0432 • 2F988A20 A2 S1-3 P1-429 265 IN. L FUEL SHUTOFF • 2F965A20 A AFT PEDESTAL x20 R2-100 RIGHT STALL WARN VANE AND STATIC PORT HEATERS STA 110 RELAY PANEL 3 LOCATIONS (1123 AAJ, AAC, RAF 1123) • 1 F988D20 (AAJ, AAC, RAF) 415 IN. • 1F965B20 415 IN. (AAB, AAC, RAF) 1F991A20 400 IN. (RAF) F970B20N 150 IN. R5-1505 R2-1505 R5-1505 LEFT FUEL SW RELAY AFT RIGHT RADIO RACK STA 200 (761) 3 LOCATIONS • (AAB, AAJ) 1F988C20 1F988A20 B2 B3 > 215 IN 1F965A20 - X2 R2-99 LEFT STALL WARN VANE AND STATIC PORT HEATERS STA 110 RELAY PANEL ADDED WIRE OR NEW ROUTING EXISTING WIRE TA DELETED WIRE OR FORMER ROUTING TERMINAL CODE FIGURE 6: ELECTRICALELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT-AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES (SHEET 1 OF 2) Original Issue: April 28, 2017 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished MD80-30A132 Work - See page 1 for details. 58 of 62 ### Page 59 REFERENCE: MD-80 WDM 30-31-02, MD-80 WDM 74-11-00 The Terminal Code numbers shown below agree with the number shown in the Terminal Code symbol in this figure. NOTESQTYIDENTIFICATIONNAMETERMINAL CODE (a)4LRC16M-32DJ5SOCKET T/C 706706 (a)65D0086-5TERMINAL LUG 761761 (a) (b)25D0086-6TERMINAL LUG 762762 8DC39-16SSKT T/C 11231123 (a) Or approved equivalent. Refer to AEPL, Drawing 7595071. (b) Measure the electrical bond resistance between the terminal lug and the ground stud. Make sure the bond resistance is not greater than 0.0025 ohms. Refer to SWPM 20-50-01 as an accepted procedure. FIGURE 6: ELECTRICAL/ELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT- AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES (SHEET 2 OF 2) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: April 28, 2017 MD80-30A132 59 of 62 BOEING SERVICE BULLETIN MD80-30A132 ALERTALERT ### Page 60 (OCR) BOEING SERVICE BULLETIN MD80-30A132 ALERT ALERT This Figure applies only to: Group 4-5. 3 LOCATIONS (1123 AAJ, AAC, RAF АЗ 1123 2F988D20 A2 (AAJ, AAC, RAF) 415 IN. • 2F965B20 OFF 706) 2 LOCATIONS (AAB, AAC, RAF) 415 IN. 2F991A20 (914) 450 IN. F971B20N= (RAF) Х2 + 2J3A168 150 IN. ON R5-1506 R2-1506 R5-1506 S1-4 R FUEL P1-430 914 RIGHT FUEL SW RELAY SHUTOFF 2J1A16 AFT RIGHT RADIO RACK STA 200 761) 3 LOCATIONS OFF G 06 2 LOCATIONS (AAB, AA. F988C2( • 2F988A20 A2 0432 (914 265 IN. AAT→ ON 1J3A16 • 2F965A20 A 914 x20 S1-3 L FUEL P1-429 R2-100 SHUTOFF RIGHT STALL WARN VANE AFT PEDESTAL AND STATIC PORT HEATERS STA 110 RELAY PANEL 3 LOCATIONS (1123 AAJ, AAC, RAF 1123) • 1 F988D20 (AAJ, AAC, RAF) 415 IN. • 1F965B20 415 IN. (AAB, AAC, RAF) 1F991A20 400 IN. (RAF) F970B20N 150 IN. R5-1505 R2-1505 R5-1505 LEFT FUEL SW RELAY AFT RIGHT RADIO RACK STA 200 (761) 3 LOCATIONS • (AAB, AAJ) 1F988C20 1F988A20 B2 ~B3> 215 IN. 1F965A20- X2 R2-99 LEFT STALL WARN VANE AND STATIC PORT HEATERS STA 110 RELAY PANEL ADDED WIRE OR NEW ROUTING EXISTING WIRE TA DELETED WIRE OR FORMER ROUTING TERMINAL CODE FIGURE 7: ELECTRICALELECTRONICS (E/E) COMPARTMENT AND FLIGHT COMPARTMENT-AFT PEDESTAL, STA 110 RELAY PANEL AND AFT RIGHT RADIO RACK - WIRING CHANGES (SHEET 1 OF 2) Original Issue: April 28, 2017 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING MD80-30A132 Work - See page 1 for details. 60 of 62 The text continues at https://openairdocs.org/service-documents/boeing/md80-30a132/file/7d027fe29954.md?from=61 --- 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.