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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Unpublished Work.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
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.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
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BLANK PAGE
Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected20
B. Concurrent Requirements20
C. Reason20
D. Description21
E. Compliance22
F. Approval22
G. Manpower22
H. Weight and Balance Changes24
I. Electrical Load Data25
J. References26
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 Affected27
L. Interchangeability and Intermixability of Parts27
M. Software Accomplishment Summary28
2. MATERIAL INFORMATION29
A. Material - Price and Availability29
B. Industry Support Information30
C. Parts Necessary for Each Airplane30
1. Kits/Parts30
2. Parts and Materials Supplied by the Operator33
3. Parts Modified and Reidentified33
4. Parts Removed and Not Replaced33
D. Parts Necessary to Change Spares33
E. Special Tooling - Price and Availability33
F. Special Tooling Necessary to do this Service Bulletin34
3. ACCOMPLISHMENT INSTRUCTIONS35
A. GENERAL INFORMATION35
B. WORK INSTRUCTIONS37
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
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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 INTENT62
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
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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
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 Airplane 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
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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
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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
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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
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 Number 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
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GroupFuselage Number 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
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GroupFuselage Number 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