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Commercial Airplanes MD80 Service Bulletin ALERT Number: MD80-53A316 Original Issue: December 15, 2016 ATA System: 5313 SUBJECT: FUSELAGE - Fuselage, Tail Section - Inspect Cant Station 1463 Bulkhead, DC-9-87 (MD-87) Cant Station 1254 Bulkhead 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 © 2016 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Unpublished Work.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: December 15, 2016 MD80-53A316 1 of 26
3.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected13
B. Concurrent Requirements13
C. Reason13
D. Description13
E. Compliance14
F. Approval14
G. Manpower15
H. Weight and Balance Changes15
I. Electrical Load Data15
J. References15
1. Existing Data:15
2. Data Supplied with this Service Bulletin:15
3. Installation Drawings Used in the Preparation of this Service Bulletin:15
K. Publications Affected16
L. Interchangeability and Intermixability of Parts16
M. Software Accomplishment Summary16
2. MATERIAL INFORMATION17
A. Material - Price and Availability17
B. Industry Support Information17
C. Parts Necessary for Each Airplane17
1. Kits/Parts17
2. Parts and Materials Supplied by the Operator17
3. Parts Modified and Reidentified17
4. Parts Removed and Not Replaced17
D. Parts Necessary to Change Spares17
E. Special Tooling - Price and Availability17
F. Special Tooling Necessary to do this Service Bulletin17
3. ACCOMPLISHMENT INSTRUCTIONS19
A. GENERAL INFORMATION19
B. WORK INSTRUCTIONS21
FIGURE 1: DETAILED INSPECTION OF CANT STA 1463 BULKHEAD, DC-9-87 (MD-87) CANT STA 1254
BULKHEAD - LEFT SIDE22
FIGURE 2: DETAILED INSPECTION OF CANT STA 1463 BULKHEAD, DC-9-87 (MD-87) CANT STA 1254
BULKHEAD - RIGHT SIDE24
APPENDIX A: DETAILED INSPECTION OF CANT STA 1463 BULKHEAD, DC-9-87 (MD-87) CANT STA 1254
BULKHEAD26
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: December 15, 2016 MD80-53A316 3 of 26 BOEING SERVICE BULLETIN MD80-53A316
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: December 15, 2016 MD80-53A316 4 of 26 BOEING SERVICE BULLETIN MD80-53A316
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Commercial Airplanes MD80 Service Bulletin ALERT SummaryNumber: MD80-53A316Original Issue: December 15, 2016 ATA System: 5313 SUBJECT: FUSELAGE - Fuselage, Tail Section - Inspect Cant Station 1463 Bulkhead, DC-9-87 (MD-87) Cant Station 1254 Bulkhead
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 An MD-80 operator reported cracking of various structure in the MD-80 fuselage Cant STA 1463 Bulkhead, DC-9-87 (MD-87) Cant STA 1254 Bulkhead. The cracking was discovered during a heavy maintenance visit on an airplane with 63,480 total flight-hours, and 45,809 total flight cycles. The cracks were in the upper left area of the bulkhead, between Longerons L-2 and L-3, in the frame web, horizontal stiffeners, lower frame cap, rear spar cap, and spar cap web. Boeing analysis has determined that the operational and limit loads cannot duplicate this condition and the root cause is suspected to be the result of a High Load Event(s) based on service experience. Cracking of the bulkhead, if undetected, may result in the inability of the structure to sustain limit loads, and could adversely affect the structural integrity of the airplane.
Boeing Service Related Problem (SRP) MD80-SRP-53-0540 is related to this service bulletin.
Boeing Communication Systems (BCS) Message Number MOM-MOM-16-0684-01B 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 Paragraph 1.E., Compliance and Paragraph
1.F., Approval YesAD Related Paragraph 1.H., Weight and Balance ChangesNoWeight and Balance Change Paragraph 1.I., Electrical Load DataNoElectrical Load Changed Paragraph 1.K., Publications AffectedNoPublications Affected Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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ReferenceAffectedPlanning Data Paragraph 1.K., Publications AffectedNoAirplane Flight Operations Affected (Flight Crew Operations Manual and/or FAA Approved Airplane Flight Manual) Paragraph 2.C.1., Kits/PartsNoKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator NoOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION On the left and right sides, do a detailed inspection of the forward and aft surfaces of Cant STA 1463 Bulkhead, DC-9-87 (MD-87) Cant STA 1254 Bulkhead, for any crack in the upper caps, upper (cap) doublers, bulkhead webs and doublers, stiffeners, lower caps, and vertical stabilizer rear spar caps and webs, between longerons L-11L through L-11R.
If any crack is found in the stiffener, web, doubler, or cap, repair in accordance with DC-9/MD-80 SRM 51-70-04 or DC-9/MD-80 SRM 53-03.
If any crack is found that cannot be repaired in accordance with DC-9/MD-80 SRM 51-70-04, or DC-9/MD-80 SRM 53-03, contact The Boeing Company for repair instructions and do the repair.
If no crack is found, no further action is required.
EFFECTIVITY All DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes.
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.
Refer to Paragraph 1.E., Compliance.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection given in this service bulletin.
MANPOWER Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION None.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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BOEING SERVICE BULLETIN MD80-53A316
ALERT ALERT CANT STA 1463 DC-9-87 (MD-87) CANT STA 1254
ON THE LEFT AND RIGHT SIDES, DO A DETAILED INSPECTION OF THE FORWARD AND AFT SURFACES OF CANT STA 1463 BULKHEAD, DC-9-87 LONER CAPT AN VERTICAL STAI HER NEAR SPAR CAPE AND VESTS. BETWEEN LONGERONS L-11L THROUGH L-11R.
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes MD80 Service Bulletin ALERT Number: MD80-53A316 Original Issue: December 15, 2016 ATA System: 5313 SUBJECT: FUSELAGE - Fuselage, Tail Section - Inspect Cant Station 1463 Bulkhead, DC-9-87 (MD-87) Cant Station 1254 Bulkhead
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 applicable to all DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes. The line numbers are 909 through 2287 in 1 Group. The Variable Numbers and Group Information for the applicable airplanes is given below.
This service bulletin is for the airplanes shown below.
DESCRIPTIONCONFIGURATIONGROUP All DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 Airplanes.
-1 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 1909 1917 1924 1938 1941 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 1944 1946 1948 1950 1952 - 953 1955 1957 - 958 1960 1962 - 963 1965 - 967 1969 1970 - 971 1973 - 975 1977 - 979 1981 1983 1985 - 986 1988 - 989 1991 - 992 1994 - 999 11000 - 1013 11015 - 1016 11018 - 1020 11022 - 1023 11025 - 1026 11028 - 1029 11031 - 1032 11034 - 1035 11037 - 1038 11040 - 1041 11043 11045 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 11047 11049 11051 11053 11055 11057 11059 - 1080 11082 - 1083 11085 - 1099 11100 - 1199 11200 - 1299 11300 - 1399 11400 - 1499 11500 - 1599 11600 - 1699 11700 - 1799 11800 - 1899 11900 - 1999 12000 - 2007 12009 - 2016 12019 - 2034 12036 - 2069 12071 - 2093 12101 - 2114 12116 12118 - 2119 12121 12124 12127 - 2128 12130 12132 12134 - 2135 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 12137 12139 12145 12148 12151 - 2152 12155 12167 12174 12176 12178 12180 12183 12185 12187 12189 12192 12196 12199 12201 12204 12206 12208 12214 12218 12234 12239 12241 12244 12247 12249 12252 12254 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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