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FIGURE 8: BETWEEN P33 PANEL AND DISCONNECT BRACKET AD0880 - WIRE BUNDLE W4236 - WIRE
ROUTING (SHEET 11 OF 12) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 64 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
REQUIREMENTS BULLETIN 757-29A0071
ALERT ALERT GD5486S
FEEDTHRU
ROTATED TO D43412J POS 3 (POS 11 OPTIONAL) AD0880 (AD880)
DISCONNECT
BRACKET W4236 STA 900 RIGHT BODY FAIRING STA 860 2993348 FIGURE 8: BETWEEN P33 PANEL AND DISCONNECT BRACKET AD0880 - WIRE BUNDLE W4236 - WIRE
ROUTING (SHEET 12 OF 12) Original Issue: November 16, 2023 Revision 1 May 28, 2026 757-29A0071 RB Export Controlled ECCN: 9E991 See page 1 for details 65 of 286
REQUIREMENTS BULLETIN 757-29A0071
ALERT ALERT This Figure applies only to: Group 1-2, Configuration 1.
W4236 AD0880 (AD880) AP0033 (P33) PRESSURE SEAL 2 LOCATIONS 2 LOCATIONS 2 LOCATIONS 2519R-10 - 2 W1230 W2514 2519B-10 2 LOCATIONS 1 D43312P POS 11 QI I GD5486-ST D43412J POS 03 (POS 11 OPTIONAL) ADDED WIRE OR NEW ROUTING FIND NUMBER 2992156 REFERENCE: 757 WDM 29-22-11 The find numbers (No.) shown below agree with the find number symbol in the figure.
Find No. Name Identification Qty More Data CONTACT, SOCKET P-204541 (a) 2 CONNECTOR, RECEPT BACC63BV18F8S9 (a) BACKSHELL BACC10KD18 (b) 4 SLEEVE, OVERBRAID 280N3381-10301 (c) 5 TERMINAL, LUG BACT12AC12 (a) (e) (f) (g) WASHER BACW10BР3APU 1 (f) (t) NUT BACN10JC3CM (f) (t) 6 PLUG, END SEAL MS27488-12-2 (a) ID - WIRE 280N3381-10303 12 (i) 9 ID - BUNDLE 280N3381-10304 2 () 10 INSULATION SLEEVING, 829A9003-384 2 (k) (1)
HEAT SHRINKABLE, YEL- LOW, IN DIA 3/8", CLASS 1 FIGURE 9: BETWEEN P33 PANEL AND DISCONNECT BRACKET AD0880 - WIRE BUNDLE W4236 -
INSTALLATION (SHEET 1 OF 3) Original Issue: November 16, 2023 Revision 1 May 28, 2026 Export Controlled ECCN: 9E991 757-29A0071 RB See page 1 for details 66 of 286
More DataQtyIdentificationName Find No.
(l)(m)2829A9003-124INSULATION SLEEVING,
HEAT SHRINKABLE, YEL- LOW, IN DIA .5 INCH CLASS 1 11
(l)(n)1280N3381-10305SLEEVE, EXPANDABLE12
(d)(e)(f)1BACT12AC56TERMINAL, LUG13
(o)1280N3381-12502ID - GROUND14
(h)1280N3381-12501 (280N3381-12503 optional) ID - EQUIPMENT15
(p)-280N3381-103WWIRE - RAW MATERIAL16
(q)-280N3381-1001LACING TAPE - BLUE - PRESSURIZED (TEMP 135 DEG)
(r)(s)-BACS38K1STRAP
(r)(s)-BACS38K4STRAP
(r)(s)-BACS38K5STRAP
(a) Refer to SWPM 20-61-11 as an accepted procedure.
(b) Refer to SWPM 20-60-09 as an accepted procedure.
(c) Install between the pressure seal and the electrical connector. Refer to SWPM 20-25-11 as an accepted procedure.
(d) Refer to SWPM 20-30-11 as an accepted procedure.
(e) Refer to SWPM 20-20-00 as an accepted procedure.
(f) Refer to SWPM 20-20-10, Category 6 as an accepted procedure.
(g) Identify ground stud as GD5486S. Refer to SOPM 20-50-10, Part Mark M (Code M), as an accepted procedure.
(h) Install within 6 inches of equipment.
(i) Install within 4 inches of equipment and at 72 inches +/- 1 inch spaces between ID tapes.
(j) Install over sleeve, overbraid within 12 inches of the electrical connector and pressure seal.
(k) Install over ends of sleeve, expandable.
(l) Refer to SWPM 20-10-14 as an accepted procedure.
(m) Install over ends of sleeve, overbraid.
(n) Install under the sleeve, overbraid.
(o) Install within 4 inches of ground.
FIGURE 9: BETWEEN P33 PANEL AND DISCONNECT BRACKET AD0880 - WIRE BUNDLE W4236 -
INSTALLATION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 67 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
More DataQtyIdentificationName Find No.
(p) Refer to SWPM 20-10-11 as an accepted procedure.
(q) Refer to SWPM 20-10-11 and SWPM 20-10-19 as accepted procedures.
(r) Select the strap size to fit the wire bundle and install at 6 - 8 inch spacing intervals. Refer to SWPM 20- 10-11 as an accepted procedure.
(s) Only install in pressurized areas.
(t) If the part size does not fit, use WASHER BACW10BP( )APU and NUT BACN10JC( )CM as required.
WIRE LIST - CUT AND CODE AS REQUIRED
NOTESMATERIAL SPECIFICATIONLENGTH (INCHES) TYPE CODE GAGE COLOR WIRE NUMBER WIRE BUNDLE -BMS13-48T10C02G010821PB102519BW4236 -PB102519RW4236 FIGURE 9: BETWEEN P33 PANEL AND DISCONNECT BRACKET AD0880 - WIRE BUNDLE W4236 -
INSTALLATION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 68 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
REQUIREMENTS BULLETIN 757-29A0071
ALERT ALERT This Figure applies only to: Group 1-4, 7-8, Configuration 1.
STA 870 -S-19R -S-20R
STA BEFORE STA 879 (VIEW LOOKING INBOARD) 860 FWD -S-19R -S-20R
STA AFTER STA 879 (VIEW LOOKING INBOARD) 860 2993232 FIGURE 10: RIGHT BODY FAIRING - FEEDTHRU SEALS - INSTALLATION (SHEET 1 OF 2) Original Issue: November 16, 2023 Revision 1 May 28, 2026 757-29A0071 RB Export Controlled ECCN: 9E991 See page 1 for details 69 of 286
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 each airplane.
More DataQtyIdentificationNameTaskStep -1BACS12GU3K12SCREWRemove1 -1BACC50AK3WCOVER, SEALRemove -1BACC50AK3WNCOVER, SEALRemove
(a)1BACS11BD5 (BACS11BD6 optional) SEAL, RINGInstall (New)2
(a)2BACS45B3SEALInstall (New)
(a)1MS16624-2156RING, RETAINING, EXT Install (New)
(a)-BMS5-37, CLASS B-1/2 (BMS5-37, CLASS B-2 or BMS5-45, CLASS B-2 or BMS5-45, CLASS B-1/2 optional) SEALANTApply3
(a) Refer to SWPM 20-10-20 as an accepted procedure.
FIGURE 10: RIGHT BODY FAIRING - FEEDTHRU SEALS - INSTALLATION (SHEET 2 OF 2) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 70 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
REQUIREMENTS BULLETIN 757-29A0071
ALERT ALERT This Figure applies only to: Group 1-2, 4, 8, Configuration 1.
STA 870 W4236 W4236
ALTERNATIVE
CONFIGURATION 34€ W4236 S-18R - S-19R - S-20R -
STA STA RIGHT FORWARD CARGO COMPARTMENT MIXBAY 860 879 2993601 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 each airplane.
FIGURE 11: RIGHT FORWARD CARGO MIXBAY - WIRE BUNDLE W4236 CLAMP - INSTALLATION (SHEET 1 OF 2) Original Issue: November 16, 2023 Revision 1 May 28, 2026 757-29A0071 RB Export Controlled ECCN: 9E991 See page 1 for details 71 of 286
More DataQtyIdentificationNameTaskStep
(a)(b)(e)(f)1BACC10GE8CLAMP, LOOPInstall (New)1
(a)(b)(c)(e)(f)-35450-1BUSHING RUBBERInstall (New)2
(a)(b)(e)(f)1NAS1149D0332JWASHERInstall (New)3
(a)(b)(d)(e)(f)1BACS12GU3K8SCREWInstall (New)4
(a)(b)(e)(f)1BACN10YR3CDNUTInstall (New)5 -1BACS12GU3K( )SCREWRemove6
(a)(b)1287T0011-1CLAMP OLYMPICInstall (New)
(a)(b)(c)135450-1BUSHING RUBBERInstall (New)
(a)(b)(d)1BACS12GU3K12SCREWInstall (New)
(a)(b)1BACS38W3STRAPInstall (New)
(a) Alternate part numbers are acceptable that meet the requirements for SWPM 20-10-12.
(b) Refer to SWPM 20-10-12 as an accepted procedure.
(c) Use quantity of rubber bushings as necessary.
(d) It is acceptable to use one grip length up or down as necessary.
(e) If a ring post is found at this location, the ring post can be kept and used in place of the clamp.
(f) If no clamp or ring post is found at this location, do steps 1 through 5. If an existing clamp is found, do step 6.
FIGURE 11: RIGHT FORWARD CARGO MIXBAY - WIRE BUNDLE W4236 CLAMP - INSTALLATION (SHEET 2 OF 2) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 72 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
REQUIREMENTS BULLETIN 757-29A0071
ALERT ALERT This Figure applies only to: Group 1-2, 8, Configuration 1.
STA 870 W4236 45€ W4236 AD0880 (AD880)
DISCONNECT
BRACKET D43412J POS 3 STA (POS 11 OPTIONAL) 900
RIGHT BODY FAIRING STA 860
• W4236 ) 4 LOCATIONS 2993678 FIGURE 12: DISCONNECT BRACKET AD0880 - ELECTRICAL CONNECTOR D43412J AND WIRE BUNDLE
CLAMP - INSTALLATION (SHEET 1 OF 2) Original Issue: November 16, 2023 Revision 1 May 28, 2026 Export Controlled ECCN: 9E991 757-29A0071 RB See page 1 for details 73 of 286
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 each airplane.
More DataQtyIdentificationNameTaskStep
(a)4BACS12HN04-8SCREWInstall (New)1
(a)4NAS1149DN416JWASHERInstall (New)
(a)4BACN10YR04CDNUTInstall (New)2
(b)1BACC10GU102CLAMP, LOOPInstall (New)3
(b)1NAS1149D0332JWASHERInstall (New)4
(b)1BACS12GU3K8SCREWInstall (New)5
(b)1BACN10YR3CDNUTInstall (New)6
(a) Refer to SWPM 20-60-06 as an accepted procedure.
(b) Refer to SWPM 20-10-12 as an accepted procedure.
FIGURE 12: DISCONNECT BRACKET AD0880 - ELECTRICAL CONNECTOR D43412J AND WIRE BUNDLE
CLAMP - INSTALLATION (SHEET 2 OF 2) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 74 of 286 REQUIREMENTS BULLETIN 757-29A0071
ALERTALERT
This Figure applies only to: Group 1, 3, 7-8, Configuration 1.
REFERENCE: 757 WDM 29-22-11 DescriptionFlag Note Alternatively, deleted wire(s) can be capped and stowed. Refer to SWPM 20-10-11 as an accepted procedure.
A Seal connector cavities of deleted wire or capped and stowed with Plug, End Seals.
Refer to SWPM 20-60-08 as an accepted procedure.
B Wires can be AWG 20 or AWG 18.C FIGURE 13: BETWEEN DISCONNECT BRACKET AD1090 AND POWER TRANSFER UNIT CONTROL VALVE - WIRE BUNDLE W2514 - REMOVAL (SHEET 1 OF 1) Export Controlled ECCN: 9E991 See page 1 for details Original Issue: November 16, 2023 757-29A0071 RBRevision 1 May 28, 2026 75 of 286 REQUIREMENTS BULLETIN 757-29A0071