Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 1 of 41

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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2000–92–006

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.
Service Bulletin

29 March 2010

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2000–92–006

Page 3 of 41

Crimp tool Positioner Insert tool Removal tool Used for

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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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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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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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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29 March 2010

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2000–92–006

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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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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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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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(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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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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CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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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CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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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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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 15 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 16 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 17 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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)
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 18 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 19 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 20 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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)
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 21 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 22 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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)
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 23 of 41

CONNECTORS

DISCONNECTED

RELATED AMM SYSTEM TITLE WDM REF

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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.
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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.
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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.

–
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 27 of 41

Item Part Number Qty Nomenclature Designation Remarks

– – – 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.

–
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 28 of 41

Item Part Number Qty Nomenclature Designation Remarks

– – – 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 –
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 29 of 41

Item Part Number Qty Nomenclature Designation Remarks

– – – 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.
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 30 of 41

Item Part Number Qty Nomenclature Designation Remarks

– – – 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 – –
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

Page 31 of 41

Item Part Number Qty Nomenclature Designation Remarks

– – – 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.
Service Bulletin

29 March 2010

Revision 1, 18 August 2010

2000–92–006

Page 32 of 41

THIS PAGE INTENTIONALLY LEFT BLANK
Service Bulletin

29 March 2010Revision 01, 18 August 2010

2000–92–006

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B18398

B

B

FWD

VIEW

LOOKING

UPWARDS

131VP–J2/P2

131VP–J1/P1

131VP–J5/P5

131VP–J3/P3

131VP–J4/P4

131VP–J6/P6

132VP–J6/P6

132VP–J4/P4 

136VP–A

136VP–J1/P1

136VP–J2/P2 136VP–J3/P3 14

A – AB – B

ZONE 191/192

CONNECTORS

191GB

191DB

193AB

STA

642

STA

541.5

191AL

191FB

193CL

191EB

191CL

192EB

192CR

192AR

192FB

194CR

A

A

STA 642 LOOKING AFT

STA 541.5 LOOKING FWD

Access Panels/Component Location – Center Wing Fairing

FIG. 1
Service Bulletin

Date Month Year

Revison X, Date Month Year

2000–XX–XXX

Page 34
Service Bulletin

29 March 2010Revision 01, 18 August 2010

2000–92–006

Page 35/36 of 41

B18405

1DE–P1 (LHS)

2DE–P1 (RHS)

VIEW LOOKING FWD AT REAR SPAR

VIEW LOOKING AFT AT FRONT SPAR

LHS SHOWN RHS OPPOSITE

Component Location – Front/Rear Spar

FIG. 2
Service Bulletin

Date Month Year

Revison X, Date Month Year

2000–XX–XXX

Page 36
Service Bulletin

29 March 2010Revision 01, 18 August 2010

2000–92–006

Page 37/38 of 41

B18400

STEP 1STEP 2STEP 3

STEP 4STEP 5

FILL BACKSHELL ENTRYWITH SILICONE TAPE NITTO 665

THE WIRE BUNDLE SHALL BE 100%COVERED WITH SCOTCH TAPE NO. 92

Braid Repair

FIG. 3
Service Bulletin

Date Month Year

Revison X, Date Month Year

2000–XX–XXX

Page 38
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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
Service Bulletin

29 March 2010

Revision 01, 18 August 2010

2000–92–006

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