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### ATA CHAPTER: 92 ELECTRICAL AND ELECTRONIC INSTALLATIONS – INSPECTION AND REPAIR/REPLACEMENT OF ELECTRICAL CONNECTORS AND BRAID IN ZONES 191/192
Mod No. –

A. EFFECTIVITY (1) Aircraft: Aircraft Mfg. Serial No’s SAAB 2000 – 004 thru – 063. (2) Spares: Not affected.

B. REASON Environmentally friendly de– /anti–icing agents (acetates or formates) are a known cause of corrosion to components of the Electrical Wiring–Interface System (EWIS). Investigation has identified affected connectors and braids in the areas of the center wing fuselage. Examples of acceptable and unacceptable corrosion levels are given in Service Newsletter SN2000–1001 Electrical and Electronic Installations – Guidelines for Service Bulletin Saab 2000–92–005/006.

C. DESCRIPTION This Service Bulletin gives instructions for: – Inspection of the harness braid, connectors and backshells – Inspection of the LRU connectors and backshells – Repair of the harness braid – Treatment of harness braid, connectors and backshell with Corrosion Preventive Compound (CPC) – Replacement of damaged connectors and backshells – Inspection of the access panel seals – Replacement of the access panel seals – Applicable tests after connector replacement.

D. COMPLIANCE Mandatory. To be performed within 2 years. This Service Bulletin is under EASA consideration for an Airworthiness Directive (AD).

E. APPROVAL The technical content of this Service Bulletin is approved under the authority of DOA nr. EASA.21J.066.

F. MANPOWER Estimated time to complete this Service Bulletin is: 2 persons required.
Total manhours: 320 Elapsed time (hours): 320

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Page 2 of 41 Labour cost at operators expense.

G. MATERIAL – COST AND AVAILABILITY Price and availability of the parts required to do this modification will be furnished on request.

H. TOOLING (1) Heat gun. (2) Soldering iron. (3) EMI–band tool, EAK214 or DBS–1100, or equivalent. Crimp tool Positioner Insert tool Removal tool Used for M22520/1–01 /1–04RD M81969/14–10 M81969/14–10 5CN–P1 (POST SB27–024), 5GG–P1, 6GG–PL1, 6LA–P1, 7LA–P1, 11MH–P1, 12MH–P1, 14FD–P1, 44HD–P1, 131VP–J1, 131VP–J2, 131VP–J4, 131VP–J6, 132VP–J1, 132VP–J2, 132VP–J4, 132VP–J6, 135VP–J1, 135VP–J2, 135VP–J3, 136VP–J1, 136VP–J2, 136VP–J3, 131VP–P1, 131VP–P2, 131VP–P4, 131VP–P6, 132VP–P1. 132VP–P2, 132VP–P4, 132VP–P6, 135VP–P1, 135VP–P2, 135VP–P3, 136VP–P1, 136VP–P2, 136VP–P3. M22520/2–01 /2–09 M81969/14–10 M81969/14–10 131VP–P3, 131VP–P5, 132VP–P3, 132VP–P5, 137VP–P1, 138VP–P1.

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Page 3 of 41 Crimp tool Used for Removal tool Insert tool Positioner M22520/2–01 /2–07 M81969/14–01 M81969/14–01 2CM–J1, 2CP–J1, 2CM–J2, 2CP–J2, 5CN–P1 (PRE SB 27–024) 26GA–P1, 14MJ–P1 (extended water system option), 131VP–J3, 131VP–J5, 132VP–J3, 132VP–J5, 137VP–J1, 138VP–J1. M22520/1–01 /1–02BL M81969/14–03 M81969/14–03 21HP–P1, 22HP–P1. M22520/1–01 /1–02RD M81969/14–11 M81969/14–11 1DE–P1, 2DE–P1.

I. WEIGHT AND BALANCE
None.

J. ELECTRICAL LOAD DATA Not affected.

K. REFERENCES Aircraft Maintenance Manual (AMM) TASK 20–70–00–200–801 TASK 24–00–00–860–801 TASK 24–00–00–860–802 TASK 24–00–00–860–805 TASK 24–00–00–860–806 TASK 24–32–00–710–801 TASK 24–42–00–720–801 TASK 24–21–00–710–801 TASK 26–21–00–720–801 TASK 26–21–00–720–802 TASK 27–12–00–720–801 TASK 28–21–15–710–801 TASK 28–21–20–710–801 TASK 28–21–25–710–801 TASK 28–21–30–710–801 TASK 28–22–30–710–801 TASK 28–22–35–710–801 TASK 28–41–10–710–802 TASK 28–41–10–720–801 TASK 28–41–15–710–801 TASK 30–10–00–710–802 TASK 30–10–00–720–802

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Page 4 of 41 TASK 32–30–00–720–801 TASK 32–32–00–720–802 TASK 32–61–10–710–801 TASK 32–61–25–830–801 TASK 33–41–15–701–801 TASK 33–42–10–710–801 TASK 33–44–10–710–801 TASK 33–47–15–710–801 TASK 36–11–10–710–801 TASK 36–11–25–710–801 TASK 36–11–30–720–801 TASK 36–20–20–710–802 TASK 49–00–00–710–801 TASK 54–16–10–000–801 TASK 54–16–10–400–801 TASK 61–21–20–710–801 TASK 71–00–00–860–805 TASK 75–10–00–700–801 TASK 76–20–00–720–801 Subtask12–10–29–942–004–B Subtask21–27–10–710–001 Subtask27–51–00–720–001 Subtask29–11–20–210–004 Subtask29–11–45–710–001 Subtask29–30–00–720–801 Subtask32–43–10–710–001 Subtask71–00–00–710–006 Subtask71–00–00–720–005 Wiring Diagram Manual (WDM) 20–00–00 20–20–05 20–20–35 20–30–00 Structural Repair Manual 51–20–45 51–33–00 51–80–00 Corrosion Prevention Manual (CPM) 20–20–50

L. OTHER PUBLICATIONS AFFECTED Maintenance Review Board Report (MRB) Maintenance Planning Document (MPD) Job Cards

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Page 5 of 41 2. ACCOMPLISHMENT INSTRUCTIONS
CAUTION : CAUTION: BE CAREFUL WHEN YOU DO WORK WITH THE HARNESSES: – MOVE THE HARNESS AS LITTLE AS POSSIBLE – ONLY DISASSEMBLE THE CABLE HARNESS WHEN THERE IS MAJOR CONTAMINATION – REMOVE ONLY THE CABLE TIES, LACING CORD AND CABLE CLAMPS NECESSARY – DO NOT USE THE CABLE HARNESS AS A HAND–HOLDS, STEPS OR SUPPORTS – DO NOT HANG INSPECTION LAMPS ON THE CABLE HARNESS. – IF YOU DO NOT FOLLOW THESE INSTRUCTIONS MORE DAMAGE TO THE CABLE HARNESS CAN OCCUR. CAUTION : BE CAREFUL WHEN YOU DO THE MODIFICATION OF THE HARNESS. MAKE SURE THAT YOU DO NOT DAMAGE THE EXISTING WIRES WHEN NEW WIRES ARE INSTALLED. CLEAN AND INSPECT THE AFFECTED HARNESS WHEN THE MODIFICATION IS COMPLETED. DAMAGES TO THE WIRES CAN CAUSE SYSTEM MALFUNCTION.
NOTE : All wiring changes are to be performed in accordance with the procedures in the WDM 20–00–00.
NOTE : The color of the lacing cord on the A and the B wire bundles gives the harness class and identification. The A harness is identified with white lacing cord and the B harness is identified with red/black lacing cord.
FOR A/C 042,043,044,046 and 055
NOTE : The connectors 131/132VP–J5/P5 have been replaced with feed throughs. However, the methods stated in this SB still apply.
FOR A/C ALL

A. JOB SET–UP (1) Before you start the SB, make sure: – The local supply items listed in the Service Bulletin are available – The documentation is available – The special tools are available. (2) Remove the electrical power (a) Remove the external AC power (Ref. AMM TASK 24–00–00–860–802), if supplied. (b) Disconnect the battery (Ref. AMM TASK 24–00–00–860–805). (3) Get access to the connectors in zone 191/192 REF. FIG. 1, 2 (a) Remove the access panels: – 191AL – 191CL – 191DB – 191EB – 191FB – 191GB – 192AR – 192CR – 192EB – 192FB. (4) Disconnect the connectors for the FWD center wing area

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Page 6 of 41 REF. FIG. 1, 2
(a) Disconnect these connectors at the LH forward center wing area:
– 7LA–P1 – 5GG–P1 – 21HP–P1 – 131VP–P1 – 131VP–P2 – 131VP–P3 – 131VP–P4 – 131VP–P5 – 131VP–P6 – 137VP–P1. (b) Disconnect these connectors at the RH forward center wing area:
– 6LA–P1 – 6GG–P1 – 22HP–P1 – 132VP–P1 – 132VP–P2 – 132VP–P3 – 132VP–P4 – 132VP–P5 – 132VP–P6. (c) Disconnect the connectors for the LH aft center wing area:
– 1DE–P1 – 2CM–P1 – 2CM–P2 – 5CN–P1 – 11MH–P1 – 14FD–J1 – 135VP–P1 – 135VP–P2 – 135VP–P3 – 138VP–P1. (d) Disconnect the connectors for the RH aft center wing area: – 2CP–P1 – 2CP–P2 – 2DE–P1 – 12MH–P1 – 14MJ–P1 (if extended water system option installed). – 26GA–P1 – 44HD–P1 – 136VP–P1 – 136VP–P2 – 136VP–P3.

B. INSPECTION

NOTE : Only light corrosion that you can remove with isopropyl alcohol and ScotchBrite Type A very fine is acceptable.
(1) Do the inspection/cleaning of the EWIS (Ref. AMM TASK 20–70–00–200–801).

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Page 7 of 41 WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. (2) If there is contamination or corrosion of the EWIS, use a lint–free cloth and white spirit and remove any existing CPC.
NOTE : It is not necessary to remove the CPC if it is still visible, intact and tacky to touch. (a) Do an inspection of the connectors, backshells and braids for corrosion deposits. Look for: – White or gray/white deposits that indicate the presence of cadmium and/or aluminum corrosion – Blue/green deposits that indicate the presence of copper corrosion. (3) Do the inspection of the connectors, backshells and braids, LRUs and LRU connectors (a) Do an inspection of the connectors and backshells with drab olive cadmium plating
1 The olive drab chromate layer shall be almost 100 % complete and only minor defects in the layer are acceptable. There shall be no trace of corrosion or material defects. The defective parts shall be replaced and the harness repaired. Refer to the steps in D. CORRECTIVE ACTION.
2 Moderate or severe corrosion is not acceptable. The defective parts shall be replaced and the harness repaired. Refer to the steps in D. CORRECTIVE ACTION. (b) Do an inspection of the connectors with electroless nickel plating
1 The nickel coating must not show any corrosion deposits or material defects. Minor discoloration is acceptable. The defective parts shall be replaced and the harness repaired. Refer to the steps in D. CORRECTIVE ACTION.
2 Moderate or severe corrosion is not acceptable. Corrosion on nickel plated connectors and backshells is shown as flaking of the coating and the aluminium base material is visible and corroded. The defective parts shall be replaced and the harness repaired. Refer to the steps in D. CORRECTIVE ACTION. (c) For all connectors
1 Make sure the connectors, backshells and braids are not damaged and that they are securely attached.
2 Check the electrical bonding path, pigtail or braid to ground points.Make sure there is no damage or corrosion present and that they are securely attached.
3 Inspect the connector contacts:

a If the contacts are in the connector, look for any trace of corrosion.
b If the contacts are removed from the connector, look for corrosion and discoloration.
4 If: – There is light corrosion that can be removed, do the steps in C. CLEANING – There is moderate to heavy corrosion, do the necessary steps in D. CORRECTIVE ACTION. – The condition of the connector on the LRU is not acceptable, remove and replace the LRU. Refer to the steps in D. CORRECTIVE ACTION. (d) Do an inspection of the seals on the access panels
REF. FIG. 4
NOTE : The procedure that follows is applicable to the access panels 191DB, 191EB, 192EB, 191FB, 191GB and 192FB

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Page 8 of 41 1 Make sure that the seal (1) is in serviceable condition and that there are no cuts, nicks or tears. 2 Make sure the seal (1) is securely attached to the access panel (2). 3 If the seal (1) is damaged, replace the seal (1). Refer to D. CORRECTIVE ACTION (1) (f). 4 If the seal (1) is serviceable but not securely attached, re–attach the seal (1). Refer to D. CORRECTIVE ACTION (1) (f) 3

. (e) Please complete the Feedback Form and return to Saab REF. FIG. 6.

C. CLEANING NOTE : Only light corrosion that you can remove with isopropyl alcohol and ScotchBrite Type A very fine is acceptable. If you cannot remove the corrosion successfully, do the necessary steps in D. CORRECTIVE ACTION. (1) If necessary, use fine ScotchBrite Type A very fine to remove corrosion from the connectors, backshells and braid. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. (2) Use a lint free cloth and isopropyl alcohol to clean the connectors, backshells and braid.

D. CORRECTIVE ACTION (1) Do the necessary repair, as applicable (a) Repair the damaged shield wire as shown in (REF. FIG. 3) or WDM 20–20–35, as applicable. (b) Replace any LRUs necessary and make a note to perform the applicable post–installation test. (c) Repair the damaged braid as shown in (REF. FIG. 3). (d) Replace the connectors 1 If it is not possible to read the marking on the wires, tag and identify them before disconnection. This will help when the new connector is installed. 2 Use the correct connector, contacts and sealing plugs, as required, and replace the damaged connectors (Ref. WDM 20–30–00) and the material list. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. 3 Apply CPC (Ardrox AV–25) to the back of the backshell before assembly. Let the CPC (Ardrox AV–25) dry before you do the final assembly. (e) Repair damaged grounding or bonding (Ref. SRM 51–80–00). (f) Replace the seal on the access panel, if necessary. REF. FIG. 1 and 4 NOTE : The procedure that follows is applicable to the access panels 191DB, 191EB, 192EB, 191FB, 191GB and 192FB WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. 1 Use a non–metallic scraper and remove the old sealant from the access panel (2).

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Page 9 of 41 2 Use a lint–free cloth soaked with MEK and clean the area where the old seal was installed. 3 Apply the PR 1431–G Type 1 sealant to the access panel (2) and put the seal (1) in position for installation.
4 Remove the unwanted sealant from the area and let the sealant dry. (2) Do the manual check of the wiring (Ref. WDM 20–20–05). (3) Apply the CPC to the connectors (a) Prepare the surface before you apply the CPC (Ardrox AV–25) (Ref. CPM–20–20–50). (b) Put the protective cover in position below the connectors. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. (c) Apply the CPC (Ardrox AV–25) to the connectors as shown in FIG. 5. (d) Let the CPC (Ardrox AV–25) dry. (e) Remove all the tools and the equipment from the work area. Make sure the work is clean. (4) Connect the connectors for the FWD center wing area REF. FIG. 1, 2 (a) Connect these connectors at the LH forward center wing area: – 7LA–P1 – 5GG–P1 – 21HP–P1 – 131VP–P1 – 131VP–P2 – 131VP–P3 – 131VP–P4 – 131VP–P5 – 131VP–P6 – 137VP–P1. (b) Connect these connectors at the RH forward center wing area: – 6LA–P1 – 6GG–P1 – 22HP–P1 – 132VP–P1 – 132VP–P2 – 132VP–P3 – 132VP–P4 – 132VP–P5 – 132VP–P6. (c) Connect the connectors for the LH aft center wing area: – 1DE–P1 – 2CM–P1 – 2CM–P2 – 5CN–P1 – 11MH–P1 – 14FD–J1 – 135VP–P1 – 135VP–P2 – 135VP–P3 – 138VP–P1.

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Page 10 of 41 (d) Connect the connectors for the RH aft center wing area: – 2CP–P2 – 2DE–P1 – 12MH–P1 – 14MJ–P1 (if extended water system option installed) – 44HD–P1 – 26GA–P1 – 136VP–P1 – 136VP–P2 – 136VP–P3. (5) Apply the CPC (Ardrox AV–25) to the EWIS (a) Prepare the surface before you apply the CPC (Ardrox AV–25) (Ref. CPM 20–20–50).
WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIAL(S). YOU MUST OBEY THE OPERATOR’S AND MANUFACTURER’S HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIAL (S) CAN CAUSE INJURY OR DEATH TO PERSONS. (b) After inspection and the EWIS is restored to a serviceable condition apply CPC (Ardrox AV–25) to the braids and pigtail braid to the grounding points. (c) Let the CPC (Ardrox AV–25) dry. (d) Remove the protective cover from below the connectors.

E. OPERATIONAL TEST (1) Connect the battery (Ref. AMM TASK 24–00–00–860–806). (2) Do the applicable operational or functional test for connectors that have been disconnected as given in the table below. NOTE : Additional manual test for system HD are given in Paras 3 to 6 that follow the table.
NOTE : In addition to the tests listed here, you must do the applicable operation or functional tests of any LRUs that have been replaced.

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Page 11 of 41 CONNECTORS DISCONNECTED SYSTEM DESIGNATOR RELATED AMM TEST/INDICATION SYSTEM TITLE WDM REF

131VP–J1 HQ AMM Subtask 21–27–710–001 Nacelle Ventilation 21–50–00

PA AMM 24–32–00–710–801 DC Battery Power System 24–32–00

QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

QM Self Indicating with Engine Start Fuel Distribution Pumps 28–20–20

MH/ML AMM Subtask 29–30–00–720–801 Hydraulic Valve, Electrical /Hydraulic P 29–10–00

AMM Subtask 29–11–45–710–001 y Pumps

131VP–J1 HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

GA/GAA AMM 32–61–10–710–801 (WOW) Landing Gear Extension and Retraction 32–30–00

AMM 32–30–00–720–801 (D–Lock)
LB AMM 33–42–10–710–801 Nav Lights 33–42–00

LE AMM 33–44–10–710–801 Wing Inspection Lights 33–44–00

LC AMM 33–47–15–710–801 Strobe Lights 33–47–00

KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 HQ AMM Subtask 21–27–10–710–001 Nacelle Ventilation 21–50–00

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Page 12 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 131VP–J2 WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

XA AMM 24–21–00–710–801 Main AC Generation System 24–21–00

TF Self Indicating (EICAS/MDS) Engine Data Acquisition System 31–41–00

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Page 13 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 131VP–J3 QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

GG AMM Subtask 32–43–10–710–001 Anti–Skid 32–43–00

DG AMM 32–61–25–820–801 Landing Gear Indicating System 32–60–00

LA AMM 33–41–15–701–801 Landing and Taxi Lights 33–41–00

HD AMM 36–11–10–710–801 Pneumatic Distribution 36–10–00

AMM 36–20–20–710–802 AMM 36–11–25–710–801 AMM 36–11–30–720–801 Perform tests shown in E. OPERATIONAL TEST Paras 2 thru 7. KF AMM 61–21–20–710–801 Propeller Control 61–20–00

KC AMM Subtask 71–00–00–720–005 Engine Power Management Unit 76–11–15

KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805(Engine start performed x 2 to calibrate FADEC A and B)

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Page 14 of 41 CONNECTORS DISCONNECTED SYSTEM DESIGNATOR RELATED AMM TEST/INDICATION SYSTEM TITLE WDM REF

131VP–J4 WG AMM 26–21–00–720–801 Fire Detection APU/ SAU 26–10–00

WF AMM 26–21–00–720–801 Overheat Detection Tailpipe 26–12–00

WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

EB Fuel Measuring System 28–41–00

AMM 28–21–25–710–801 Fuelling Panel

AMM 28–41–15–710–801 Fuel Quantity

AMM 28–41–10–720–801 Low Level Sensor

HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

GG AMM Subtask 32–43–10–710–001 Anti–Skid 32–43–00

FC/FCA/FCB/FF/ FFA/FFB Self–Indicating AHRS/IRS 34–27–00

KF AMM 61–21–20–710–801 Propeller Control 61–20–00

EA Self–Indicating at Engine Start and EICAS Fuel Pressure and Temperature 73–30–00

131VP–J5 MH/ML AMM 29–30–00–720–801 Hydraulic Valve, Electrical /Hydraulic P 29–10–00

AMM Subtask 29–11–45–710–001 y Pumps

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Page 15 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 131VP–J5 HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

EA Self–Indicating at Engine Start and EICAS Fuel Pressure and Temperature 73–30–00

EC Self–Indicating at Engine Start Fuel Flow System 73–31–00

HL AMM 75–10–00–700–801 Engine Anti–Icing 75–10–00

DB/DBA AMM Subtask 12–10–29–942–004 –B Hydraulic Indicating 29–30–00

AMM Subtask 29–11–20–210–004 ED Self Indicating with Engine Start Oil Temp/Pressure Indicating 79–30–00

131VP–J6 KA AMM 71–00–00–710–006 Engine Power Control 76–10–00

AMM 71–00–00–720–005 AMM 76–20–00–720–801
132VP–J1 PA AMM 24–32–00–710–801 DC Battery Power System 24–32–00

QM Self Indicating with Engine Start Fuel Distribution Pumps 28–20–20

MH/ML AMM Subtask 29–30–00–720–801 Hydraulic Valve, Electrical/Hydraulic P 29–10–00

AMM Subtask 29–11–45–710–001 y Pumps

132VP–J1 HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

LE AMM 33–44–10–710–801 Wing Inspection Lights 33–44–00

LC AMM 33–47–15–710–801 Strobe Lights 33–47–00

KA AMM 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801

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Page 16 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 132VP–J2 WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

TF Self Indicating (EICAS/MDS) Engine Data Acquisition System 31–41–00

XA AMM 24–21–00–710–801 Main AC Generation System 24–21–00

GA/GAA AMM 32–61–10–710–801 (WOW) Landing Gear Extension and Retraction 32–30–00

AMM 32–30–00–720–801 (D–Lock)
LB AMM 33–42–10–710–801 Nav Lights 33–42–00

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Page 17 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 132VP–J3 QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

GG AMM Subtask 32–43–10–710–001 Anti–Skid 32–43–00

DG AMM 32–61–25–820–801 Landing Gear Indicating System 32–60–00

LA AMM 33–41–15–701–801 Landing and Taxi Lights 33–41–00

LB AMM 33–42–10–710–801 Nav Lights 33–42–00

HD AMM 36–11–10–710–801 Pneumatic Distribution 36–10–00

AMM 36–20–20–710–802 AMM 36–11–25–710–801 AMM 36–11–30–720–801 Perform tests shown in E. OPERATIONAL TEST Paras 2 thru 7. KF AMM 61–21–20–710–801 Propeller Control 61–20–00

KC AMM Subtask 71–00–00–720–005 Engine Power Management Unit 76–11–15

KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805 (Engine start performed x 2 to calibrate FADEC A and B)

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Page 18 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 132VP–J4 WG AMM 26–21–00–720–801 Fire Detection APU/ SAU 26–10–00

WF AMM 26–21–00–720–801 Overheat Detection Tailpipe 26–12–00

WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

EB Fuel Measuring System 28–41–00

AMM 28–21–25–710–801 Fuelling Panel

AMM 28–41–15–710–801 Fuel Quantity

AMM 28–41–10–720–801 Low Level Sensor

HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

GG AMM Subtask 32–43–10–710–001 Anti–Skid 32–43–00

FC/FCA/FCB/FF/ FFA/FFB Self–Indicating AHRS/IRS 34–27–00

EA Self–Indicating at Engine Start and EICAS Fuel Pressure and Temperature 73–30–00

132VP–J5 RL/RLA AMM 23–42–00–720–801 pos (a), (b), (c), and (h) to (k) Audio Integrating 23–51–00

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Page 19 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 132VP–J5 QA Fuel Distribution Valves 28–20–10

AMM 28–21–15–710–801 Refuel Shut–Off Valves AMM 28–21–20–710–801 Defuel Valve

AMM 28–41–10–710–802 Overfill Sensor

AMM 28–22–30–710–801 Crossfeed Valve

AMM 28–22–35–710–801 Interconn Valve

EB Fuel Measuring System 28–41–00

AMM 28–21–25–710–801 Fuelling Panel

AMM 28–41–15–710–801 Fuel Quantity

AMM 28–41–10–720–801 Low Level Sensor

MH/ML AMM 29–30–00–720–801 Hydraulic Valve, Electrical/Hydraulic Pumps 29–10–00

AMM Subtask 29–11–45–710–001 HP/HPA AMM 30–10–00–710–802 Airfoil De–Icing System 30–10–00

AMM 30–10–00–720–801 y

KF AMM 61–21–20–710–801 Propeller Control 61–20–00

EA Self–Indicating at Engine Start and EICAS Fuel Pressure and Temperature 73–30–00

EC Self–Indicating at Engine Start Fuel Flow System 73–31–00

HL AMM 75–10–00–700–801 Engine Anti–Icing 75–10–00

ED Self Indicating with Engine Start Oil Temp/Pressure Indicating 79–30–00

DB/DBA AMM Subtask 12–10–29–942–004 –B Hydraulic Indicating 29–30–00

AMM Subtask 29–11–20–210–004

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Page 20 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 132VP–J6 KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 KC AMM Subtask 71–00–00–720–005 Engine Power Management Unit 76–11–15

135VP–J1 WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

CC AMM 27–12–00–720–801 Trim Control System 27–00–20

DE AMM 27–12–00–720–801 Trim and Flaps Indication 27–00–30

CM/CP Self Indicating with Engine Start PECS 27–31–00

CN AMM Subtask 27–51–00–720–001 pos (b) Flap Control System 27–51–00

WA AMM 28–21–30–710–801 Fuel Fire Valves 28–20–30

GB 32–32–00–720–802 Emergency Landing Gear Extension 32–32–00

MA/MAA AMM 49–00–00–710–801 APU Control System 49–00–00

KF AMM 61–21–20–710–801 Propeller Control 61–20–00

KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805 (Engine start performed x 2 to calibrate FADEC A and B)

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Page 21 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 135VP–J2 WG AMM 26–21–00–720–801 Fire Detection APU/ SAU 26–10–00

WF AMM 26–21–00–720–801 Overheat Detection Tailpipe 26–12–00

CM/CP Self Indicating with Engine Start PECS 27–31–00

MH/ML AMM Subtask 29–11–45–710–001 Hydraulic Valve, Electrical/Hydraulic P 29–10–00

AMM 29–30–00–720–801 y Pumps

TA Self Indicating (EICAS) Flight Data Recorder 31–31–00

KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805 (Engine start performed x 2 to calibrate FADEC A and B)
XA AMM 24–21–00–710–801 Main AC Generation System 24–21–00

135VP–J3 KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 KC AMM Subtask 71–00–00–720–005 Engine Power Management Unit 76–11–15

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Page 22 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 136VP–J1 WB AMM 26–21–00–720–801 /802 Fire Extinguishing Engine 26–21–00

CC AMM 27–12–00–720–801 Trim Control System 27–00–20

DE AMM 27–12–00–720–801 Trim and Flaps Indication 27–00–30

CM/CP Self Indicating with Engine Start PECS 27–31–00

WA AMM 28–21–30–710–801 Fuel Fire Valves 28–20–30

GB AMM 32–32–00–720–802 Emergency Landing Gear Extension 32–32–00

KF AMM 61–21–20–710–801 Propeller Control 61–20–00

KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805 (Engine start performed x 2 to calibrate FADEC A and B)

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Page 23 of 41 CONNECTORS DISCONNECTED WDM REF SYSTEM TITLE RELATED AMM TEST/INDICATION SYSTEM DESIGNATOR 136VP–J2 WG AMM 26–21–00–720–801 Fire Detection APU/ SAU 26–10–00

WF AMM 26–21–00–720–801 Overheat Detection Tailpipe 26–12–00

CM/CP Self Indicating with Engine Start PECS 27–31–00

MH/ML AMM Subtask 29–11–45–710–001 Hydraulic Valve, Electrical/Hydraulic P 29–10–00

AMM 29–30–00–720–801 y Pumps

TA Self Indicating (EICAS) Flight Data Recorder 31–31–00

KS AMM Subtask 71–00–00–720–005 Cranking 80–10–00

AMM 71–00–00–860–805 (Engine start performed x 2 to calibrate FADEC A and B)
XA AMM 24–21–00–710–801 Main AC Generation System 24–21–00

136VP–J3 KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 KC AMM Subtask 71–00–00–720–005 Engine Power Management Unit 76–11–15

137VP–J1 KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801 138VP–J1 KA AMM Subtask 71–00–00–710–006 Engine Power Control 76–10–00

AMM Subtask 71–00–00–720–005 AMM 76–20–00–720–801

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Page 24 of 41 (3) Left bleed overtemperature test (131VP–J3 only) (a) Remove the center cowl (Ref. AMM TASK54–16–10–000–801). (b) Supply the external AC power (Ref. AMM TASK 24–00–00–860–801).

ACTION RESULT (c) Connect a shorting wire between19HD–P1:A–B. On the PED, the amber caution L BLD OVTEMP is shown. On the AIR COND panel: – The FAULT caption comes on in the L BLD switch – The FAULT caption comes on in the L HP switch. (d) Remove the shorting wire from between 19HD–P1:A–B. On the PED, the amber L BLD OVTEMP caution goes off after 20 seconds. On the AIR COND panel: – The FAULT caption goes off in the L BLD switch – The FAULT caption goes off in the L HP switch
(4) Right bleed overtemperature test (131VP–J3 only)

ACTION RESULT (a) Connect a shorting wire between 20HD–P1:A–B On the PED, the amber caution R BLD OVTEMP is shown. On the AIR COND panel: – The FAULT caption comes on in the R BLD switch – The FAULT caption comes on in the R HP switch. (b) Remove the shorting wire from between 20HD–P1:A–B On the PED, the amber caution R BLD OVTEMP goes off after 20 seconds. On the AIR COND panel: – The FAULT caption goes off in the R BLD switch – The FAULT caption goes off in the R HP switch.
(5) Do the left bleed overpressure test (131VP–J3 only)

ACTION RESULT (a) Connect a shorting wire between 21HD–P1:A–B. On the PED, the amber caution L BLD OVPRESS is shown. On the AIR COND panel: – The FAULT caption comes on in the L BLD switch – The FAULT caption comes on in the L HP switch.

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Page 25 of 41 ACTION RESULT (b) Remove the shorting wire from between 21HD–P1:A–B. On the PED, the amber caution L BLD OVPRESS goes off after 20 seconds. On the AIR COND panel: – The FAULT caption goes off in the L BLD switch – The FAULT caption goes off in the L HP switch.

(6) Do the right bleed overpressure test (131VP–J3 only)

ACTION RESULT (a) Connect a shorting wire between 22HD–P1:A–B. On the PED, the amber caution R BLD OVPRESS is shown. On the AIR COND panel: – The FAULT caption comes on in the R BLD switch – The FAULT caption comes on in the R HP switch. (b) Remove the shorting wire from between 22HD–P1:A–B. On the PED, the amber caution R BLD OVPRESS goes off after 20 seconds. On the AIR COND panel: – The FAULT caption goes off in the R BLD switch – The FAULT caption goes off in the R HP switch. (c) Remove the external AC power (Ref. AMM TASK 24–00–00–860–802)

F. JOB CLOSE–UP (1) Close the access to the connectors in the FWD center wing area REF. FIG. 1, 2 (a) Remove all the tools and the equipment from the work area. Make sure the work is clean. (b) Install the access panels: – 191AL – 191CL – 191DB – 191EB – 191FB – 191GB – 192AR – 192CR – 192EB – 192FB. (c) Remove all the tools and the equipment from the work area. Make sure the work is clean.

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Page 26 of 41 (2) Install the center cowl, if removed (a) Remove all the tools and the equipment from the work area. Make sure the work is clean. (b) Install the center cowl (Ref. AMM TASK 54–16–10–400–801). (c) Remove all the tools and the equipment from the work area. Make sure the work is clean.

3. MATERIAL INFORMATION

A. Maximum list of potential parts required to do the modification:

Item Part Number Qty Nomenclature Designation Remarks
4 – 1 7353500–139 1 Seal – 191EB 4 – 1 7353500–140 1 Seal – 192EB 4 – 1 7353500–131 1 Seal – 191FB 4 – 1 7353500–132 1 Seal – 192FB 4 – 1 7353500–197 1 Seal – 191GB 4 – 1 7353500–195 1 Seal – 191DB – – – MS27468T23B53SN 4 Receptacle 131VP–J1, 132VP–J1, 135VP–J1, 136VP–J1. –

– – – MS27467T23B53PN 4 Plug 131VP–P1, 132VP–P1, 135VP–P1, 136VP–P1. –

– – – MS27468T23B53SA 2 Receptacle 131VP–J2, 132VP–J2. –
– – – MS27467T23B53PA 2 Plug 131VP–P2, 132VP–P2. –
– – – MS27468T23B35SN 2 Receptacle 131VP–J3, 132VP–J3. –
– – – MS27467T23B35PN 2 Plug 131VP–P3, 132VP–P3. –
– – – MS27468T23B53SB 2 Receptacle 131VP–J4, 132VP–J4. –
– – – MS27467T23B53PB 2 Plug 131VP–P4, 132VP–P4. –

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Page 27 of 41 Item Remarks Designation Nomenclature Qty Part Number
– – – 901–35541–22–11–5 5 12 Backshell 131VP–P1, 131VP–P2, 131VP–P3, 131VP–P4, 131VP– P5, 132VP–P1, 132VP–P2, 132VP–P3, 132VP–P4, 132VP–P5, 135VP–P1, 136VP–P1. –

– – – MS27468T23B35SA 2 Receptacle 131VP–J5, 132VP–J5. –

– – – MS27467T23B35PA 2 Plug 131VP–P5, 132VP–P5. –

– – – MS27468T17B26SN 4 Receptacle 131VP–J6, 132VP–J6, 135VP–J3, 136VP–J3. –

– – – MS27467T17B26PN 4 Plug 131VP–P6, 132VP–P6, 135VP–P3, 136VP–P3. –

– – – 901–35541–16–08– 55 4 Backshell 131VP–P6, 132VP–P6, 135VP–P3, 136VP–P3. –

– – – MS27467T9B98B 6 Plug 6LA–P1, 7LA–P1, 5GG–P1, 6GG–P1, 11MH–P1, 12MH–P1. –

– – – 901–35541–08–04– 55 7 Backshell 6LA–P1, 7LA–P1, 5GG–P1, 6GG–P1, 11MH–P1, 12MH–P1, 26GA–P1. –

– – – MS3456W10SL–4S 2 Plug 21HP–P1, 22HP–P1. –

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Page 28 of 41 Item Remarks Designation Nomenclature Qty Part Number – – – 311AS001N1001 2 Backshell 21HP–P1, 22HP–P1. –

– – – MS27656T11B35B 2 Receptacle 137VP–J1, 138VP–J1. –

– – – MS27467T11B35A 2 Plug 137VP–P1, 138VP–P1. –

– – – 901–35541–10–06– 55 4 Backshell 137VP–J1, 137VP–P1, 138VP–J1, 138VP–P1. –

– – – MS27468T21B41SN 2 Receptacle 135VP–J2, 136VP–J2. –

– – – MS27467T21B41A 2 Plug 135VP–P2, 136VP–P2. –

– – – 901–35541–20–10– 55 2 Backshell 135VP–P2, 136VP–P2. –

– – – MS27656T9B35SD 2 Receptacle 2CM–J1, 2CP–J1. –

– – – 901–35541–08–05– 55 5 Backshell 2CM–J1, 2CM–J2, 2CP–J1, 2CP–J2, 5CN–P1. A/C 004–049 PRE SB 27–024

901–35541–12–06– 55 1 Backshell 5CN–P1 A/C 50 and up or POST SB 27–024. – – – MS27656T9B35S 2 Receptacle 2CM–J2, 2CP–J2. –

– – – MS3476W10–6B 2 Plug 1DE–P1, 2DE–P1. –

– – – 311AS001N1002 2 Backshell 1DE–P1, 2DE–P1. –

– – – MS27467T9B35B 1 Plug 5CN–P1 A/C 004–049 PRE SB 27–024 – – – MS27467T13B98SN 1 Plug 5CN–P1 A/C 050 and up or POST SB 27–024 – – – MS27467T11B98SN 1 Plug 44HD–P1
– – – 901–35541–10–05– 55 1 Backshell 44HD–P1 –

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Page 29 of 41 Item Remarks Designation Nomenclature Qty Part Number – – – MS27467T9B35SN 2 Plug 26GA–P1, 14MJ–P1. 14MJ–P1 Extended water system option.

– – – 21741R–08–04–4–0 0–55Z 1 Backshell 14MJ–P1 14MJ–P1 Extended water system option.
– – – MS27468T15B19SC 1 Receptacle 14FD–J1 –
– – – M39029/56–351 A/R Socket – 5CN–P1 (POST SB27–024), 5GG–P1, 6GG–PL1, 6LA–P1, 7LA–P1, 11MH–P1, 12MH–P1, 14FD–P1, 44HD–P1, 131VP–J1, 131VP–J2, 131VP–J4, 131VP–J6, 132VP–J1, 132VP–J2, 132VP–J4, 132VP–J6, 135VP–J1, 135VP–J2, 135VP–J3, 136VP–J1, 136VP–J2, 136VP–J3.
– – – M39029/58–363 A/R Pin – 131VP–P1, 131VP–P2, 131VP–P4, 131VP–P6, 132VP–P1. 132VP–P2, 132VP–P4, 132VP–P6, 135VP–P1, 135VP–P2, 135VP–P3, 136VP–P1, 136VP–P2, 136VP–P3.

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Page 30 of 41 Item Remarks Designation Nomenclature Qty Part Number – – – M39029/58–360 A/R Pin – 131VP–P3, 131VP–P5, 132VP–P3, 132VP–P5, 137VP–P1, 138VP–P1. – – – M39029/56–348 A/R Socket – 2CM–J1, 2CP–J1, 2CM–J2, 2CP–J2, 5CN–P1 (PRE SB 27–024) 26GA–P1,14MJ–P1 (Extended water system option), 131VP–J3, 131VP–J5, 132VP–J3, 132VP–J5, 137VP–J1, 138VP–J1. – – – M39029/30–217 A/R Socket – 21HP–P1, 22HP–P1 – – – M39029/5–115 A/R Socket – 1DE–P1, 2DE–P1. – – – MS27488–22 A/R Sealing Plug – Black – Size 22 – – – MS27488–20 A/R Sealing Plug – Red – Size 20

B. Local supply

Item Part Number Qty Nomenclature Designation Remarks – – – Scotch Tape No 92 A/R – – – – – – Nitto 665 A/R Silicon Tape – – – – – 000W280 A/R Braiding Tape – Raychem

or – – – 23–50225 A/R EMC Braiding Tape Tecknit – – – Viton–E A/R Shrink Tube – For braid tails. O/T – – – RW–200–E A/R Shrink Tube – For braid tails. – – – 214L0002 A/R EMI Band – – – – – – A/R Cable–Ties – –

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Page 31 of 41 Item Remarks Designation Nomenclature Qty Part Number
– – – Ardrox AV–25 A/R Corrosion Preventive Compound – Previously Dinitrol AV–25

– – – – A/R Isopropyl Alcohol – – – A/R Solder – – – – – – A/R Lacing Cord – – – – – – A/R Lint–Free Cloth – – – – – ScotchBrite Type A Very Fine A/R – – –

– – – – A/R White Spirit – Fed. Std. P–D–689 Type 1 – – – PR 1431–G Type 1 A/R Sealant – MIL–S–81733 Type IV–12 – – – RAY–101–10,0 A/R Tubular Braid All connectors, minus 131VP, 132VP, 135VP, 136VP. – – – RAY–101–20,0 A/R Tubular Braid For connectors 131VP, 132VP, 135VP, 136VP.

NOTE : Equivalent materials can be used for listed items, Ref. SRM 51–33–00.

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Page 32 of 41 

### THIS PAGE INTENTIONALLY LEFT BLANKService Bulletin29 March 2010Revision 01, 18 August 20102000–92–006Page 33/34 of 41B18398BBFWDVIEWLOOKINGUPWARDS131VP–J2/P2131VP–J1/P1131VP–J5/P5131VP–J3/P3131VP–J4/P4131VP–J6/P6132VP–J6/P6132VP–J4/P4132VP–J3/P3132VP–J2/P2132VP–J1/P1132VP–J5/P5136VP–A136VP–J1/P1136VP–J2/P2 136VP–J3/P3 14FD–J1135VP–J3/P3135VP–J2/P2 135VP–J1/P1135VP–AA – AB – BZONE191/192CONNECTORS191GB191DB193ABSTA642STA541.5191AL191FB193CL191EB191CL192EB192CR192AR192FB194CRAASTA 642 LOOKING AFTSTA 541.5 LOOKING FWDAccess Panels/Component Location – Center Wing FairingFIG. 1

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Date Month Year
Revison X, Date Month Year 

# 2000–XX–XXX

Page 34Service Bulletin29 March 2010Revision 01, 18 August 20102000–92–006Page 35/36 of 41B184051DE–P1 (LHS)2DE–P1 (RHS)VIEW LOOKING FWD AT REAR SPARVIEW LOOKING AFT AT FRONT SPARLHS SHOWN RHS OPPOSITEComponent Location – Front/Rear SparFIG. 2

### Service Bulletin

Date Month Year
Revison X, Date Month Year 

# 2000–XX–XXX

Page 36Service Bulletin29 March 2010Revision 01, 18 August 20102000–92–006Page 37/38 of 41B18400STEP 1STEP 2STEP 3STEP 4STEP 5FILL BACKSHELL ENTRYWITH SILICONE TAPE NITTO 665THE WIRE BUNDLE SHALL BE 100%COVERED WITH SCOTCH TAPE NO. 92Braid RepairFIG. 3

### Service Bulletin

Date Month Year
Revison X, Date Month Year 

# 2000–XX–XXX

Page 38

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Page 39 of 41 1

2

B18455 NOTE: ACCESS PANEL 191EB SHOWN. 191DB, 192EB. 191FB, 191GB AND 192FB ARE SIMILAR.
Seal – Inspection/Replacement FIG. 4

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Page 40 of 41 B18395 APPLY ARDROX AV–25 IN PLUG CAVITY BEFORE CONNECTION WITH RECEPTACLE APPLY ARDROX AV–25 ON OUTSIDE AREA BEFORE CONNECTION WITH PLUG APPLY ARDROX AV–25 IN PLUG CAVITY BEFORE CONNECTION WITH RECEPTACLE AVOID ARDROX AV–25 IN PIN OR SOCKET AVOID ARDROX AV–25 IN PIN OR SOCKET

PLUG RECEPTACLE

APPLY CPC AV–25 IN BACKSHELL BEFORE INSTALLED ON CONNECTOR

BACKSHELL

CPC Application – Connectors FIG. 5

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Page 41 of 41 B18427 Conn Conn Conn Level Conn Level 0123 0123 0123 0123 1DE–P1

12MH–P1 131VP–P4 135VP–J1 2CM–J1

14FD–J1 131VP–P5 135VP–J2 2CM–J2 14MJ–P1 131VP–P6 135VP–J3

2CP–J1 21HP–P1 132VP–J1 135VP–P1

2CP–J2 22HP–P1 132VP–J2 135VP–P2

2DE–P1 26GA–P1 132VP–J3 135VP–P3

5GG–P1 131VP–J1 132VP–J4 136VP–J1

5CN–P1 131VP–J2 132VP–J5 136VP–J2 131VP–J3 132VP–J6 136VP–J3 131VP–J4 132VP–P1 136VP–P1 6GG–P1 131VP–J5 132VP–P2 136VP–P2 6LA–P1 131VP–J6 132VP–P3 136VP–P3 7LA–P1 131VP–P1 132VP–P4 137VP–J1 11MH–P1 131VP–P2 132VP–P5 137VP–P1 44HD–P1 131VP–P3 132VP–P6 138VP–J1 138VP–P1 Please identify the level of corrosion found on each connector in the table below

Level

Please return the completed feedback form to: Saab Aerotech Aircraft Services Division SE–581 88 Linköping Service Engineering E–mail: Saab2000.techsupport@saabgroup.com Fax: +46 13 18 4874 Operator
A/C No:

Date: Corrosion levels: 0 = None, 1 = Low, 2 = Moderate, 3 = Severe 

### Feedback Form – SB 2000–92–006

Any other observations/comments:

Feedback Form FIG. 6