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Commercial Airplanes DC10 Requirements Bulletin ALERT Number: DC10-53A184 RB Original Issue: February 06, 2020 ATA System: 5314 SUBJECT: FUSELAGE - Center Fuselage Main Frame - Overwing Floor Beams - Inspection 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:
Copyright © 2020 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Unpublished Work.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: February 06, 2020 DC10-53A184 RB 1 of 62
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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Table of Contents
1 . E F F E C T I V I T Y5
A. Airplanes5
B . S p a r e s A f f e c t e d8
2. CONCURRENT REQUIREMENTS8
3 . C O M P L I A N C E8
4. APPROVAL ................................................ 1 2
5. ACCOMPLISHMENT INSTRUCTIONS .................................. 1 3 A. General Information ......................................... 1 3 B. Work Instructions ........................................... 1 4 FIGURE 1: LEFT SIDE - GENERAL VISUAL INSPECTION OF THE OVERWING FLOOR BEAMS . . 21 FIGURE 2: RIGHT SIDE - GENERAL VISUAL INSPECTION OF THE OVERWING FLOOR BEAMS . 23 FIGURE 3: LEFT SIDE - EDDY CURRENT HIGH FREQUENCY (ETHF) INSPECT ION OF THE OVERWING FLOOR BEAMS ........................................ 2 5 FIGURE 4: RIGHT SIDE - EDDY CURRENT HIGH FREQUENCY (ETHF) INSPECTION OF THE OVERWING FLOOR BEAMS ........................................ 3 5 FIGURE 5: LEFT SIDE - EDDY CURRENT HIGH FREQUENCY (ETHF) INSPECT ION OF THE OVERWING FLOOR BEAM SUPPORTS [Group 1] ............................ 4 5 FIGURE 6: RIGHT SIDE - EDDY CURRENT HIGH FREQUENCY (ETHF) INSPECTION OF THE OVERWING FLOOR BEAM SUPPORTS [Group 1] ............................ 5 1 FIGURE 7: LEFT SIDE - DETAILED INSPECTION OF OVERWING FLOOR BEAM SUPPORTS [Group 2] .................................................. 5 7 FIGURE 8: RIGHT SIDE - DETAILED INSPECTION OF OVERWING FLOOR BEA M SUPPORTS [Group 2 ] ................................................ 6 0 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes DC10 Requirements Bulletin ALERT Number: DC10-53A184 RB Original Issue: February 06, 2020 ATA System: 5314 SUBJECT: FUSELAGE - Center Fuselage Main Frame - Overwing Floor Beams - Inspection
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. THIS IS AN ENHANCED REQUIRED FOR COMPLIANCE DOCUMENT. THE BOEING
PROCESSES USED TO CREATE THE SERVICE BULLETIN (SB) AND THE REQUIREMENTS BULLETIN (RB) ENSURE THAT THE INFORMATION BETWEEN "RC START" AND "RC END" IN THE SB ARE IDENTICAL TO THE INFORMATION IN THE SAME SECTIONS (COMPLIANCE, WORK INSTRUCTIONS…) OF THE RB WHICH THE SB REFERS TO AS THE RELATED DOCUMENT.
1. Effectivity A. Airplanes This bulletin is applicable to DC-10-10, DC-10-15, DC-10-30, DC-10-40, DC-10-10F, DC-10-30F, DC-10-40F, DC-10-30F (KC-10A), DC-10-30F (KDC-10), MD-10-10F, MD-10-30F Airplane(s), line number(s) 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45-49, 50-59, 60-69, 70-79, 80-89, 90-99, 100-109, 110-119, 120-129, 130-139, 140-149, 150-159, 160-169, 170-179, 180-189, 190-199, 200-209, 210-219, 220-229, 230-239, 240-249, 250-259, 260-269, 270-279, 280-289, 290-299, 300-309, 310-319, 320-329, 330-339, 340-349, 350-359, 360-369, 370-379, 380-389, 390-399, 400-409, 410-419, 420-429, 430-439, 440-446 in 2 Group(s). Where the effectivity is presented with hyphens between line numbers, the airplane applicability means "through" and "inclusive", e.g. line numbers 1-9 means line numbers 1 through 9 inclusive.
DESCRIPTIONCONFIGURATIONGROUP Floor beam support stanchion not rod end type: Series 10 and 15-1 Floor beam support stanchion rod end type: Series 30 and 40-2 Airplane Models:
DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC-10A), DC-10-30F (KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 06, 2020 DC10-53A184 RB 5 of 62
GroupFuselage Number 11 12 13 14 15 16 17 18 19 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 228 129 130 131 132 133 GroupFuselage Number 134 135 236 137 138 139 140 141 142 143 144 145 246 147 148 149 150 151 152 253 154 155 156 257 158 159 260 161 162 263 164 165 266 GroupFuselage Number 167 168 269 170 271 172 273 174 275 176 277 178 279 180 281 282 183 284 285 186 287 288 189 290 291 192 293 294 195 296 297 198 299 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 2100 1101 2102 - 103 1104 2105 - 106 1107 2108 - 109 2110 - 111 1112 2113 - 117 1118 - 119 2120 - 129 2130 - 137 1138 - 139 1140 2141 1142 2143 1144 - 145 2146 - 147 1148 2149 2150 - 152 1153 - 155 2156 - 159 2160 - 161 1162 - 163 2164 - 168 1169 2170 - 172 1173 2174 - 176 1177 GroupFuselage Number 2178 - 179 2180 - 189 2190 1191 2192 - 193 1194 2195 - 197 1198 2199 2200 - 202 1203 2204 1205 2206 1207 - 209 1210 2211 - 219 2220 - 221 1222 2223 - 229 2230 - 239 2240 - 246 1247 2248 1249 1250 - 252 2253 - 259 2260 - 268 1269 1270 - 273 2274 - 279 2280 - 282 1283 GroupFuselage Number 2284 1285 2286 - 289 2290 - 293 1294 2295 1296 - 298 2299 2300 - 306 1307 2308 1309 2310 - 317 1318 - 319 2320 1321 - 323 2324 - 329 2330 - 339 2340 - 343 1344 2345 1346 - 347 2348 - 349 2350 1351 2352 1353 2354 - 356 1357 - 358 2359 2360 - 361 1362 2363 - 364 Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 1365 2366 - 369 2370 - 371 1372 2373 GroupFuselage Number 1374 2375 - 378 1379 2380 - 389 2390 - 399 GroupFuselage Number 2400 - 409 2410 - 419 2420 - 429 2430 - 439 2440 - 446 B. Spares Affected None.
2. CONCURRENT REQUIREMENTS None.
3. COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to Requirements Bulletin DC10-53A184 RB. The Airworthiness Directive will make the compliance tasks and times given in Requirements Bulletin DC10-53A184 RB mandatory.
Accomplish the required action(s), based on the applicable condition(s) in Table(s) 1 and 2, in accordance with the Accomplishment Instructions.
When more than one OPTION is given for a CONDITION, do only one of the OPTION numbers. When more than one ACTION is given for a CONDITION or an OPTION, do all of the ACTION numbers for that CONDITION or OPTION.
Group 1:
Table 1: ETHF Inspection of the Overwing Floor Beams and Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition -Within 1,990 flight cycles or within 27 months, after the original issue date of Requirements Bulletin DC10- 53A184 RB, whichever occurs first.
Before 20,000 total flight cycles.
Do a General Visual Inspection of the overwing floor beams for any repair.
ALL AIR- PLANES Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 06, 2020 DC10-53A184 RB 8 of 62 REQUIREMENTS BULLETIN DC10-53A184
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Group 1:
Table 1: ETHF Inspection of the Overwing Floor Beams and Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition -Before further flight.CONDITION 1 (ACTION 1):
Contact The Boeing Company for alternative inspection(s) to Requirements Bulletin DC10- 53A184 RB, incorporate the inspection(s) into the maintenance programs and do the inspection(s) at the times specified by Boeing.
CONDITION 1:
ANY REPAIR FOUND -Before further flight.CONDITION 1 (ACTION 2):
Do ETHF Inspections of the overwing floor beams and supports at any unrepaired areas, for any crack.
-Before further flight.CONDITION 1.1 (ACTION 1):
Contact The Boeing Company for repair instructions and do the repair.
CONDITION 1.1:
ANY CRACK FOUND 6040 Flight Cycles or 121 months.
-CONDITION 1.1 (ACTION 2):
Repeat ETHF Inspections of the overwing floor beams and supports at any unrepaired areas, for any crack. (a) 6040 Flight Cycles or 121 months.
-Repeat ETHF Inspections of the overwing floor beams and supports at any unrepaired areas, for any crack. (a) CONDITION 1.2:
NO CRACK FOUND -Before further flight.Do ETHF Inspections of the overwing floor beams and supports for any crack.
CONDITION 2:
NO REPAIR FOUND -Before further flight.CONDITION 2.1 (ACTION 1):
Contact The Boeing Company for repair instructions and do the repair.
CONDITION 2.1:
ANY CRACK FOUND 6040 Flight Cycles or 121 months.
-CONDITION 2.1 (ACTION 2):
Repeat ETHF Inspections of the overwing floor beams and supports for any crack. (a) Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 06, 2020 DC10-53A184 RB 9 of 62 REQUIREMENTS BULLETIN DC10-53A184
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Group 1:
Table 1: ETHF Inspection of the Overwing Floor Beams and Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition 6040 Flight Cycles or 121 months.
-Repeat ETHF Inspections of the overwing floor beams and supports for any crack. (a) CONDITION 2.2:
NO CRACK FOUND
(a) It is not required to do the inspections in Requirements Bulletin DC10-53A184 RB in areas where a repair covers the affected inspection zone provided that:
1. The repair is the corrective action to the crack condition identified while performing Requirements Bulletin DC10-53A184 RB and installed after the original issue date of Requirements Bulletin DC10-53A184 RB, AND
2. The installed repair was approved by the Boeing Organization Designation Authorization (ODA) via a FAA Form 8100-9.
Group 2:
Table 2: ETHF Inspection of the Overwing Floor Beams and Detailed Inspection of the Overwing Floor Beam Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition -Within 1,990 flight cycles or within 27 months, after the original issue date of Requirements Bulletin DC10- 53A184 RB, whichever occurs first.
Before 20,000 total flight cycles.
Do a General Visual Inspection of the overwing floor beams for any repair.
ALL AIR- PLANES Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 06, 2020 DC10-53A184 RB 10 of 62 REQUIREMENTS BULLETIN DC10-53A184
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Group 2:
Table 2: ETHF Inspection of the Overwing Floor Beams and Detailed Inspection of the Overwing Floor Beam Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition -Before further flight.CONDITION 3 (ACTION 1):
Contact The Boeing Company for alternative inspection(s) to Requirements Bulletin DC10- 53A184 RB, incorporate the inspection(s) into the maintenance programs and do the inspection(s) at the times specified by Boeing.
CONDITION 3:
ANY REPAIR FOUND -Before further flight.CONDITION 3 (ACTION 2):
Do Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams at any unrepaired areas, for any crack.
-Before further flight.CONDITION 3.1 (ACTION 1):
Contact The Boeing Company for repair instructions and do the repair.
CONDITION 3.1:
ANY CRACK FOUND 3610 Flight Cycles or 73 months.
-CONDITION 3.1 (ACTION 2):
Repeat Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams at any unrepaired areas, for any crack. (a) 3610 Flight Cycles or 73 months.
-Repeat Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams at any unrepaired areas, for any crack. (a) CONDITION 3.2:
NO CRACK FOUND -Before further flight.Do Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams for any crack.
CONDITION 4:
NO REPAIR FOUND Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
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Group 2:
Table 2: ETHF Inspection of the Overwing Floor Beams and Detailed Inspection of the Overwing Floor Beam Supports, Left and Right Sides Repeat Interval (Not to Exceed, Whichever Occurs First) Compliance Time (Whichever Occurs Later) ActionCondition -Before further flight.CONDITION 4.1 (ACTION 1):
Contact The Boeing Company for repair instructions and do the repair.
CONDITION 4.1:
ANY CRACK FOUND 3610 Flight Cycles or 73 months.
-CONDITION 4.1 (ACTION 2):
Repeat Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams for any crack. (a) 3610 Flight Cycles or 73 months.
-Repeat Detailed Inspections of the overwing floor beam supports and ETHF Inspections of the overwing floor beams for any crack. (a) CONDITION 4.2:
NO CRACK FOUND
(a) It is not required to do the inspections in Requirements Bulletin DC10-53A184 RB in areas where a repair covers the affected inspection zone provided that:
1. The repair is the corrective action to the crack condition identified while performing Requirements Bulletin DC10-53A184 RB and installed after the original issue date of Requirements Bulletin DC10-53A184 RB, AND
2. The installed repair was approved by the Boeing Organization Designation Authorization (ODA) via a FAA Form 8100-9.
4. APPROVAL This Requirements Bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this document 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 document and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other Boeing changes.
If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this Requirements Bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this Requirements Bulletin.
Export Controlled ECCN: 9E991 Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 06, 2020 DC10-53A184 RB 12 of 62 REQUIREMENTS BULLETIN DC10-53A184