### Service Bulletin

LETTER OF TRANSMITTAL

SERVICE BULLETIN SAAB 340–27–097
REVISION 03, 19 APRIL 2012

TO : All holders of SAAB 340 SERVICE BULLETIN. This letter covers transmittal of the following Service Bulletin revision which should be included in the appropriate section of your folder. Revision 03 of Service Bulletin SAAB 340–27–097, 19 April 2012,”FLIGHT CONTROLS – STALL WARNING/IDENTIFICATION SYSTEM – PROVISION FOR IMPROVED STALL WARNING SYSTEM FOR ICING CONDITION”, cover sheet and 64 pages.

REASON FOR ISSUE
Procedure and material kit added for aircraft without TAWS.

Saab AB (Publ) Date: 19 April 2012 Support and Services Aircraft Services Division Technical Communication

Rolf Jönsson

# SERVICE BULLETIN

Number: SAAB 340–27–097 Date: 01 September 2011 Revision 03, 19 April 2012 Subject: FLIGHT CONTROLS – STALL WARNING/IDENTIFICATION SYSTEM – PROVISION FOR IMPROVED STALL WARNING SYSTEM FOR ICING CONDITION
Mod. No. 3311

64 pages

The content of this document is proprietary and confidential to Saab AB and may not: a) be used for any purpose other than those for which it was supplied; b) be copied or reproduced in whole or in part without the prior written consent of Saab AB; nor c) be disclosed to any third party without the prior written consent of Saab AB Support and Services Aircraft Services Division SE–581 88 Linköping Sweden Telephone: int+46 13 18 26 16 Telefax: int+46 13 18 41 83 Saab AB (Publ)

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### ATA CHAPTER: 27 FLIGHT CONTROLS – STALL WARNING/IDENTIFICATION SYSTEM – PROVISION FOR IMPROVED STALL WARNING SYSTEM FOR ICING CONDITION
Mod No. 3311

1. PLANNING INFORMATION

A. EFFECTIVITY (1) Aircraft: Aircraft Mfg. Serial No’s SAAB SF340A – 004–159. Aircraft Mfg. Serial No’s SAAB 340B – 160–169, 171–341, 343–361, 364–366, 368–371, 373–378, 380–384, 386–394, 396–404, 406–408, 410–430, 432–454, 456–459. NOTE : This Service Bulletin is not applicable for A/C POST Service Bulletin SAAB340–27–075 (Mod No 2650) or 340–27–085 (Mod No 2650, 2859) (Ice Speed Push Button). NOTE : This Service Bulletin is not applicable for A/C 367 and 372 (POST Service Bulletin SAAB340–23–073 Mod No 3142). FOR A/C With Basic Wingtip: NOTE : Service Bulletin SAAB 340–27–098 (Mod No 3312) completes the installation and activates the improved Stall Warning System for Icing Condition. (A/C with Basic Wingtip are A/C PRE Service Bulletin SAAB340–57–026 and PRE Service Bulletin SAAB340–57–030 and without Option 57:01) FOR A/C With Extended Wingtip: NOTE : Service Bulletin SAAB 340–27–099 (Mod No 3313) completes the installation and activates the improved Stall Warning System for Icing Condition. (A/C with Extended Wingtip are A/C POST Service Bulletin SAAB340–57–026 or POST Service Bulletin SAAB340–57–030 or with Option 57:01 installed) FOR A/C ALL (2) Spares: Not affected.

B. REASON Natural stall has in few cases been experienced in icing condition before stall warning. In order to prevent such unsafe condition a modified stall warning system has been developed. This Service Bulletin installs a provision for a modified stall warning system that includes stall warning curves that are optimized for operation in icing conditions.

C. DESCRIPTION This Service Bulletin gives instructions for: – removal of panels and units for access – modification of the instrument panel 1VU – installation of a illuminated push button switch at 1VU – installation of a blank label, to temporarily cover (hide) the push button switch, at 1VU – installation of a grounding block in the electrical center 305VU – installation of a grounding block in the electrical center 306VU

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Page 2 of 64 – installation of a relay console in the electrical center 305VU – installation of a relay console in the electrical center 306VU – installation of relay sockets and relays in the electrical center 305VU – installation of relay sockets and relays in the electrical center 306VU – installation of resistors and diodes – installation of clamp brackets – relocation of wires – installation of wires – parking of wires (to make the new system inoperative) – preparation for installation of a circuit breaker at 12VU – parking of a circuit breaker at 12VU – installation of removed access panels and units – functional and operational tests.

D. COMPLIANCE Mandatory This Service Bulletin is mandated by the European Aviation Safety Agency (EASA) through Airworthiness Directive No.: 2011–0219.

E. APPROVAL This Service Bulletin is developed and approved under the authority of DOA nr. EASA.21J.066.

F. MANPOWER Estimated time to complete this Service Bulletin is: 70 2 persons required for some of the structural modifications Total manhours: 70 Elapsed time (hours): 35 Labour cost at operators expense.

G. MATERIAL – COST AND AVAILABILITY Mod. Kit will be available 4 months after receipt of order.

H. TOOLING FOR A/C 220–459 – Heat tool. AA.400 Super Heater Mark II, or equivalent (For the MTC connectors 91VP–P2, 92VP–P2). FOR A/C ALL – Heat gun – Weight on wheels (WOW) switches operating tool, TDO 5–4650224.

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Page 3 of 64 Crimp tool Positioner Insert tool Removal tool Used for M22520/1–01 TH343 M81969/14–02 M81969/14–02 item 25: 35HL–J1, 36HL–J1, 37WH–J1, 50WH–J1, 7WHC–J1, 42WW–J1, 15GA–J1, 21GA–J1 M22520/2–01 M22520/2–06 M81969/14–01 item 26: 3WHC–P1, 3WH–P1, 4WH–P1 M22520/1–01 TH441–1 BL J1276–1 J1276–1 item 27: 4WHC, 5WHC, 6WHC, 9WHC, 305VN–G, 306VN–G, 306VT–R GMT232 item 28: 1VS–CA, 1VS–CB, 1VS–CC, 160VS–A, 201VS–VA, 203VS–VA, 292VS–A, 293VS–A, 305VS–GJ, 305VS–GK, 305VS–U, 305VS–UA, 306VS–FA, 306VS–V, 306VS–VA GMT232 item 29: 306VS–VB 47387 item 30: 2WHC:L/1, 36WH:L/1 47386 item 31: 2WHC, 1HL, 2HL

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Page 4 of 64 FOR A/C 079–459 Crimp tool Positioner Insert tool Removal tool Used for M22520/2–01 K817–2 CTA1160 item 32: 205VU–J17 M22520/2–01 K818–2 CTA1160 item 33: 205VU–P17
FOR A/C ALL

I. WEIGHT AND BALANCE Weight change +2.15 lb / +0.98kg Center of gravity STA 209.4 Change moment +4.50 lb.inch / +2.04 kg.inch 100

J. ELECTRICAL LOAD DATA Not affected. NOTE : The electrical load data will be affected post the activation Service Bulletins SAAB 340–27–098 (Mod No 3312) and SAAB 340–27–099 (Mod No 3313). FOR A/C With Basic Wingtip: Refer to Service Bulletin SAAB 340–27–098 (Mod No 3312). (A/C with Basic Wingtip are A/C PRE Service Bulletin SAAB340–57–026 and PRE Service Bulletin SAAB340–57–030 and without Option 57:01) FOR A/C With Extended Wingtip: Refer to Service Bulletin SAAB 340–27–099 (Mod No 3313). (A/C with Extended Wingtip are A/C POST Service Bulletin SAAB340–57–026 or POST Service Bulletin SAAB340–57–030 or with Option 57:01 installed) FOR A/C ALL

K. REFERENCES Aircraft Maintenance Manual (AMM) 06–30–00 Description / Operation 12–00–00 Servicing 24–00–00 Maintenance practices 25–11–05 Maintenance practices 34–23–10 Removal / Installation 34–24–10 Removal / Installation 34–24–15 Removal / Installation 34–25–05 Maintenance practices 39–10–42 Maintenance practices 39–40–40 Maintenance practices 39–40–45 Maintenance practices 39–50–10 Maintenance practices FOR A/C 079–459 Aircraft Maintenance Manual (AMM) 34–46–00–05 Adjustment / Test 34–46–25–04 Operational Test

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Page 5 of 64 34–46–30–04 Operational Test 34–46–35–04 Operational Test 34–60–00–05–2 Procedure 10
FOR A/C 220–459 Aircraft Maintenance Manual (AMM) 21–60–00–05 Adjustment / Test 24–20–00–05 Adjustment / Test 26–11–00–05 Adjustment / Test Procedure 1 26–13–00–05 Adjustment / Test 28–22–15–05 Adjustment / Test 30–10–00–05 Adjustment / Test 31–50–00–05 Part 1 Aural Visual36–11–00–02 Maintenance practices 36–23–00–05 Adjustment / Test 61–22–00–05 Adjustment / Test 71–00–00–05 Adjustment / Test Procedure 1 and 2
FOR A/C ALL Wiring Manual (WM) 20–00–00 Standard practices 20–20–15 Crimped sleeves 20–30–15 MTC Connectors
Structural Repair Manual (SRM) 51–20–42 surface treatment51–20–56 fillet sealing instructions51–40–21 rivet removal/installation 51–40–40 fastener hole and drill data 51–40–60 fastener spacing and edge margin data51–80–00 electrical bonding connection

L. OTHER PUBLICATIONS AFFECTED Aircraft Maintenance Manual (AMM) Illustrated Parts Catalog (IPC) Wiring Manual (WM)

2. ACCOMPLISHMENT INSTRUCTIONS

A. JOB SET–UP (1) Before you start the SB, make sure: – The modification kit contains the parts listed in the Service Bulletin – The local supply items listed in the Service Bulletin are available – The documentation is available – The special tools are available.

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Page 6 of 64 (2) Make the aircraft safe for maintenance: (a) Isolate the electrical power (Ref. AMM 24–00–00, maintenance practices). (3) Open for access (Ref. AMM 06–30–00) REF. FIG. 1 (a) Remove these exterior access panels: (Ref. AMM 06–30–00) – 117AL (electrical center L/H) – 118AR (electrical center R/H) – 210AL (windshield wiper LH) – 210AR (windshield wiper RH). (b) Remove the LH and the RH flight crew seat (Ref. AMM 25–11–05). (c) At the avionics rack:
1 Remove the access panels 210AZ and 220AZ (Ref. AMM 06–30–00). (d) In the flight compartment
1 Remove these access panels: (Ref. AMM 06–30–00) – 117BZ (floor panel) – 215BZ – 215DZ – 215FZ – 215GZ – 216BZ – 216DZ – 216FZ – 216GZ FOR A/C 004–219 – 215EZ remove if necessary for access to splice 293VS – 216EZ remove if necessary for access to splice 292VS. FOR A/C ALL
2 Loosen the screws that attach the access panel 215CZ to the structure and lower the panel.
3 Loosen the screws that attach the access panel 216CZ to the structure and lower the panel.
4 Loosen the screws that attach the circuit breaker panel 10VU to the structure and lower the panel.
5 Loosen the screws that attach the circuit breaker panel 11VU to the structure and lower the panel. 6 Loosen the screws that attach the circuit breaker panel 12VU to the structure and lower the panel. (e) At the instrument panels:
1 Remove the Multi Function Display (MFD 6FP) (Ref. AMM 34–25–05). (Only applicable for A/C with MFD installed).
2 If necessary for access, remove the LH and the RH Electronic Attitude Director Indicators (EADI 2FL and 2FM) (Ref. AMM 34–24–10).
3 If necessary for access, remove the LH and the RH Electronic Horizontal Situation Indicators (EHSI 3FL and 3FM) (Ref. AMM 34–24–15).
4 If necessary for access, remove the Flight Status Panel (51VU) (Ref. AMM 39–50–10).

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Page 7 of 64 5 If necessary for access, remove the Standby Horizon Indicator (3FN) (Ref. AMM 34–23–10). (f) Keep the removed units in a safe place.

B. MODIFICATION / INSTALLATION (1) Structural modifications / installations WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL CABLES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS. CAUTION : BE CAREFUL WHEN YOU DO STRUCTURAL MODIFICATIONS NEAR ELECTRICAL HARNESSES AND/OR MECHANICAL COMPONENTS. MAKE SURE THAT YOU COVER ELECTRICAL HARNESSES AND/OR MECHANICAL COMPONENTS ADJACENT TO THE WORK AREA. CLEAN AND INSPECT THE HARNESSES AND/OR THE MECHANICAL COMPONENTS WHEN THE MODIFICATION IS COMPLETED. DAMAGES TO THE WIRES OR THE MECHANICAL COMPONENTS CAN CAUSE SYSTEM MALFUNCTION. NOTE : For more data on the methods used to do the structural modification, see the: – SRM 51–20–42 for surface treatment – SRM 51–20–56 for fillet sealing instructions – SRM 51–40–21 for instructions on rivet removal/installation – SRM 51–40–40 for fastener hole and drill data. – SRM 51–40–60 for fastener spacing and edge margin data – SRM 51–80–00 for instructions on electrical bonding connection. (a) Modification of the instrument panel 1VU REF. FIG. 2 and 15
1 At the instrument panel 1VU, mark the position of the cut out for the push button switch 3WHC. Refer to figure 2 and to figure 15, Sheet 2 of 5, view L. WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
2 If necessary, remove units as applicable to be able to put the protective covers in a correct position at the work area.
3 Use protective covers to protect the work area from debris. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL WIRES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS.
4 Carefully make the cut out in the instrument panel 1VU. Break all sharp edges.

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Page 8 of 64 5 Remove all tools, protective covers and equipment from the work area.
6 Use a vacuum cleaner and remove all debris. Make sure the work area is clean. (b) Installation of the grounding blocks (23) REF. FIG. 15 Sheet 3 of 5 REF. FIG. 15 Sheet 5 of 5
1 In the electrical center 305VU: REF. FIG. 15 Sheet 3 of 5 view AB, and Sheet 5 of 5 view R–R and view P

a Loosen and lower the applicable relay consoles to get access to the location for the new grounding block 305VN–G (23). Refer to figure15, Sheet 3 of 5, view AB.
b In the electrical center 305VU at STA 203.5, mark the position for installation of the grounding block 305VN–G (23). Refer to figure15, Sheet 5 of 5, view R–R and view P. WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.

c Use protective covers to protect the work areas from debris. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL CABLES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS.
d Hold the grounding block (23) in position to the structure and drill the four holes in accordance with SRM 51–80–00 (Bonding of ground connection).

e Plain deburr if necessary.
f Use the four rivets BJ4–6 to install the grounding block (23) to the structure in accordance with SRM 51–80–00 (Bonding of ground connection). Refer to figure 15, Sheet 5 of 5, view P. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS.
g Apply fillet sealant PR 1422 B–1/2 (or equivalent) to the four rivets.
h Install the marker decal 305VN–G adjacent to the grounding block (23).
i Remove all tools, protective covers and equipment from the work area. j Use a vacuum cleaner and remove all debris. Make sure the work area is clean.
2 In the electrical center 306VU: REF. FIG. 15 Sheet 3 of 5 view AC, and Sheet 5 of 5 view T–T and view P

a Loosen and lower the applicable relay consoles to get access to the location for the new grounding block 306VN–G (23). Refer to figure15, Sheet 3 of 5, view AC.
b In the electrical center 306VU at STA 203.5, mark the position for installation of the grounding block 306VN–G (23). Refer to figure 15 Sheet 5 of 5 view T–T and view P.

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Page 9 of 64 WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.

c Use protective covers to protect the work areas from debris. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL CABLES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS. d Hold the grounding block (23) in position to the structure and drill the four holes in accordance with SRM 51–80–00 (Bonding of ground connection).

e Plain deburr if necessary. f Use the four rivets BJ4–6 to install the grounding block (23) to the structure in accordance with SRM 51–80–00 (Bonding of ground connection). Refer to figure 15, Sheet 5 of 5, view P. WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS.
g Apply fillet sealant PR 1422 B–1/2 (or equivalent) to the four rivets.
h Install the marker decal 306VN–G adjacent to the grounding block (23).
i Remove all tools, protective covers and equipment from the work area. j Use a vacuum cleaner and remove all debris. Make sure the work area is clean. (c) Installation of the clamp brackets (22) REF. FIG. 15 Sheet 5 of 5
1 In the electrical center 305VU: REF. FIG. 15 Sheet 5 of 5 view R–R WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS.

a In the electrical center 305VU at STA 203.5, use the cleaning agent MEK and clean the area for the three clamp brackets (22). b Attach the three clamp brackets (22). Use sealant PR 1422 B–1/2 or equivalent.
2 In the electrical center 306VU: REF. FIG. 15 Sheet 5 of 5 view T–T WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS.

a In the electrical center 306VU at STA 203.5, use the cleaning agent MEK and clean the area for the three clamp brackets (22). b Attach the three clamp brackets (22). Use sealant PR 1422 B–1/2 or equivalent.

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Page 10 of 64 (d) Prepare for installation of the relay consoles (1) and (6)
1 In the electrical center 305VU: REF. FIG. 13

a Use a heat gun and install two pieces of edge string (5) on the relay console (1) in accordance with FIG. 13 view B. (bench work).
b Use four rivets BJ4–5 to install the panel fastener (4) to the bracket (2). Install in accordance with FIG. 13 view A and D. (bench work).

c Use four rivets BJ4–5 to install the panel fastener (4) to the bracket (3). Install in accordance with FIG. 13 view A and D. (bench work). WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
d Use protective covers to protect the work area in the electrical center 305VU from debris.

e In the electrical center 305VU, mark the position for the bracket (2) and the bracket (3). Use the relay console (1) as a template. Refer to figure 13 view A. NOTE : It is important to install the brackets (2 and 3) in the correct position in accordance with the measurement given in figure 13 view A. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL CABLES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS.
f Drill and deburr the six holes for the brackets (2) and (3).
g Use six rivets BJ5–5 to install the bracket (2) and the bracket (3) to the structure. Install in accordance with figure 13 view A. FOR A/C With Option 231–1 (Portable Oxygen Bottle) REF. FIG. 13 view C WARNING : BE CAREFUL WHEN YOU USE THE CONSUMABLE MATERIALS. YOU MUST OBEY THE MANUFACTURERS HEALTH AND SAFETY INSTRUCTIONS. THE CONSUMABLE MATERIALS CAN CAUSE INJURY OR DEATH TO PERSONS.
h In the electrical center 305VU, use the cleaning agent MEK and clean the flanges of the reinforcement bracket for the portable oxygen bottle.
i Use a heat gun and install two pieces of edge string (5) on the flanges of the reinforcement bracket in accordance with FIG. 13 view C. FOR A/C ALL j Temporarily install the relay console (1).
k Remove all tools, protective covers and equipment from the work area.
l Use a vacuum cleaner and remove all debris. Make sure the work area is clean.
2 In the electrical center 306VU: REF. FIG. 14

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Page 11 of 64 a Use a heat gun and install three pieces of edge string (5) on the relay console (6) in accordance with FIG. 14 view B. (bench work). b Use four rivets BJ4–5 to install the panel fastener (4) to the bracket (2). Install in accordance with FIG. 14 view A and C. (bench work).

c Use four rivets BJ4–5 to install the panel fastener (4) to the bracket (3). Install in accordance with FIG. 14 view A and C. (bench work). WARNING : MAKE SURE ALL THE ELECTRICAL COMPONENTS IN THE WORK AREA ARE PROTECTED BEFORE YOU START THE STRUCTURAL WORK. SWARF AND WORK DEBRIS CAN CAUSE DAMAGE OR SHORT–CIRCUITS. INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
d Use protective covers to protect the work area in the electrical center 306VU from debris.

e In the electrical center 306VU, mark the position for the bracket (2) and the bracket (3). Use the relay console (6) as a template. Refer to figure 14 view A. NOTE : It is important to install the brackets (2 and 3) in the correct position in accordance with the measurement given in figure 14 view A. CAUTION : MAKE SURE BEFORE DRILLING AND CUTTING THAT YOU HAVE ENOUGH CLEARANCE TO STRUCTURE AND ELECTRICAL CABLES BEHIND. CUTTING TOOLS CAN CAUSE DAMAGE TO THE MATERIALS. f Drill and deburr the six holes for the brackets (2) and (3).
g Use six rivets BJ5–5 to install the bracket (2) and the bracket (3) to the structure. Install in accordance with figure 14 view A.
h Temporarily install the relay console (6).
i Remove all tools, protective covers and equipment from the work area. j Use a vacuum cleaner and remove all debris. Make sure the work area is clean. (2) Electrical modifications / installations 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 WM 20–00–00. (a) Installation of the relay sockets (19 and 21)
1 In the electrical center 305VU: REF. FIG. 15 Sheet 4 of 5 view AD

a Remove the relay console (1) and put it on a suitable work bench.
b At the relay console (1), install the relay sockets 21GA–J1 (19) and 7WHC–J1 (19).

c At the rear side of the relay console (1), install the marker decal 21GA–J1 adjacent to the relay socket 21GA–J1.
d At the rear side of the relay console (1), install the marker decal 7WHC–J1 adjacent to the relay socket 7WHC–J1.

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Page 12 of 64 e At the relay console (1), install the relay socket 35HL–J1 (21). f At the rear side of the relay console (1), install the marker decal 35HL–J1 adjacent to the relay socket 35HL–J1.
g Install the relay console (1) in the electrical center 305VU. NOTE : At installation of the wires to the relay sockets, (21GA–J1, 7WHC–J1 and 35HL–J1) make sure that you have sufficient length and routing of the wires to be able to loosen and lower the relay console (1) for future installations.
2 In the electrical center 306VU: REF. FIG. 15 Sheet 4 of 5 view AE

a Remove the relay console (6) and put it on a suitable work bench. b At the relay console (6), install the relay socket 50WH–J1 (19).

c At the rear side of the relay console (6), install the marker decal 50WH–J1 adjacent to the relay socket 50WH–J1. d At the relay console (6), install the relay socket 36HL–J1 (21).

e At the rear side of the relay console (6), install the marker decal 36HL–J1 adjacent to the relay socket 36HL–J1. f Install the relay console (6) in the electrical center 306VU. NOTE : At installation of the wires to the relay sockets, (50WH–J1 and 36HL–J1) make sure that you have sufficient length and routing of the wires to be able to loosen and lower the relay console (6) for future installations. (b) Installation of the resistors (16) and the diodes (17) REF. FIG. 15 Sheet 2 of 5 view E REF. FIG. 15 Sheet 4 of 5 view D and view J FOR A/C 200–459 1 At the terminal track 3VT (located at the area in front of the instrument panel 3VU), remove and discard the dummy block (112) from the terminal track 3VT. Refer to figure 15 Sheet 2 of 5 view E. FOR A/C ALL
2 At the terminal track 3VT (located at the area in front of the instrument panel 3VU), install the terminal block diode 9WHC (17). Refer to figure 15 Sheet 2 of 5 view E. NOTE : If the terminal track 3VT is to full to install 9WHC, remove and discard any dummy block from 3VT to provide space for 9WHC. Refer to figure 15 Sheet 2 of 5 view E. 3 Install the marker decal 9WHC at the terminal block for 9WHC.
4 In the electrical center 305VU, at 305VT, install the terminal block diode 5WHC (17). Refer to figure 15 Sheet 4 of 5 view J.
5 Install the marker decal 5WHC at the terminal block for 5WHC. 6 In the electrical center 306VU, at 306VT, install the terminal block resistor 4WHC (16). Refer to figure 15 Sheet 4 of 5 view D.
7 Install the marker decal 4WHC at the terminal block for 4WHC. 8 In the electrical center 306VU, at 306VT, install the terminal block resistor 6WHC (16). Refer to figure 15 Sheet 4 of 5 view D.

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Page 13 of 64 9 Install the marker decal 6WHC at the terminal block for 6WHC. FOR A/C 079–459 PRE SB340–34–139 (c) Assembling and installation of the MTC–connectors 205VU–J17 (232) and 205VU–P17 (235) REF. FIG. 15 Sheet 5 of 5 view S–S NOTE : Do the final assembling and installation of the MTC–connectors 205VU–J17/–P17 in conjunction with installation of the wires, Ref step 2.C.(1)(h) NOTE : For maintenance practices of the MTC connectors, Ref. WM 20–30–15. 1 Install two dummy wafers (234) and the wafer for 205VU–J17 (233) into the receptacle for 205VU–J17 (232). 2 Install the polarization pins in the key position DB (Ref. WM 20–30–15). NOTE : The polarization pins are part of the receptacle (232). 3 Install the marker decal 205VU–J17 on the receptacle (232). 4 Install two dummy wa fers (234) and the wafer for 205VU–P17 (236) into the plug housing for 205VU–P17 (235). 5 Install the polarization pins in the key position DB (Ref. WM 20–30–15). NOTE : The polarization pins are part of the plug housing (235). 6 Install the marker decal 205VU–P17 on the plug housing (235). NOTE : Install and connect the connectors 205VU–J17/–P17 after installation of the wires. Ref step 2.C.(1)(h)
7 Connect 205VU–P17 to 205VU–J17. 8 In the avionics rack, remove the two connector mounting screws NAS1101–06–30 and the two washers that attach the connectors 205VU–J16/P16, –J15/P15, –J14/P14, –J13/P13 to the plate, REF. FIG. 15 Sheet 5 of 5 view S–S. 9 Discard the two screws NAS1101–06–30, keep the washers. 10 Use the screws NAS1101–06–36 (237) and the two removed washers and install the connectors 205VU–J17/P17 and 205VU–J16/P16, –J15/P15, –J14/P14, –J13/P13 to the plate in the avionics rack. FOR A/C ALL (d) Installation of the push button switch 3WHC (15) REF. FIG. 15 Sheet 2 of 5 view L NOTE : In this Service Bulletin the push button switch is connected and installed, but then covered by a blank label. Removal of the blank label and activation of the push button switch is in the activation Service Bulletins SB340–27–098 and SB340–27–099. 1 At the instrument panel 1VU, put the push button switch 3WHC (15) in position. Refer to figure 15 Sheet 2 of 5 view L. NOTE : Do not attach the push button switch at this step. (The push button switch is attached to the instrument panel 1VU after connection of the wires. Step 2.C.(3). (e) Temporary installation of the circuit breaker 2WHC (14) REF. FIG. 15 Sheet 3 of 5 NOTE : In this Service Bulletin, the circuit breaker is connected but then safetied, insulated, parked and stowed. The final installation and activation of the circuit breaker is in the activation Service Bulletins SB340–27–098 and SB340–27–099.

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# 340–27–097

Page 14 of 64 1 At the RH circuit breaker panel 12VU, temporary remove the cover from position S–28. NOTE : The cover is reinstalled in step 2.C.(2) (Parking of the circuit breaker 2WHC). 2 At the RH circuit breaker panel 12VU, temporary install the circuit breaker 2WHC (14) at position S–28 (Ref. AMM 39–10–42). NOTE : The temporary installation of the circuit breaker is to get the correct length on the wires connected to the circuit breaker. 3 At the rear side of the RH circuit breaker panel 12VU, install the marker decal 2WHC adjacent to the circuit breaker 2WHC. (3) Relocation of wires (REF. FIG. 15) 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 WM 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 004–219 (a) Relocate these wires: REF. FIG. 3 and 4

Wire No: Class: From: Contact: To: Contact: Remarks: HL13–24* A 292VS 36HL–J1:X2 item 25 * (+ 2500mm) HL25–24* A 293VS 35HL–J1:X2 item 25 * (+ 3000mm) HL64–24 A 292VS 292VS–A ** item 28 ** splice together with HL89 and HL3004 HL67–24 A 293VS 293VS–A *** item 28 *** splice together with HL91 and HL3001 HL89–24 A 292VS (discard 292VS) 292VS–A   splice together with HL64 and HL3004 HL91–24 A 293VS (discard 293VS) 293VS–A ** * *** splice together with HL67 and HL3001
NOTE : *) Extend the existing wires HL13–24 and HL25–24 with marked wires and unmarked butt splices (28) supplied in the Material Kit. NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. FOR A/C 220–459 (b) Relocate these wires:

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# 340–27–097

Page 15 of 64 REF. FIG. 5 and 6

Wire No: Class: From: Contact: To: Contact: Remarks: HL64–24* A 92VP–P2:B1 36HL–J1:X2 item 25 * (+ 2500mm) HL67–24* A 91VP–P2:A20 35HL–J1:X2 item 25 * (+ 3000mm)
NOTE : *) Extend the existing wires HL64–24 and HL67–24 with marked wires and unmarked butt splices (28) supplied in the Material Kit. NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. NOTE : For maintenance practices of the MTC connectors, Ref. WM 20–30–15. FOR A/C ALL (c) Relocate these wires: REF. FIG. 7 and 8

Wire No: Class: From: Contact: To: Contact: Remarks: WH311–24 A 306VT–R:H 306VS–FA ** item 28 ** splice together with WH3000 and WH3003 WH375–24* A 42WW–J1:C2 50WH–J1:C2 item 25 * (+1000mm) WH376–24* A 42WW–J1:C3 50WH–J1:C3 item 25 * (+1000mm)
NOTE : *) Extend the existing wires WH375–24 and WH376–24 with marked wires and unmarked butt splices (28) supplied in the Material Kit. NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. (d) Relocate these wires: REF. FIG. 9 and 10

Wire No: Class: From: Contact: To: Contact: Remarks: GA83–24 A 15GA–J1:X1 305VS–GJ * item 28 * splice together with GA3002 and GA3004 GA84–24 A 15GA–J1:X2 305VS–GK ** item 28 ** splice together with GA3001 and GA3003
NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15.

C. INSTALLATION (1) Installation of wires (REF. FIG. 15) 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 WM 20–00–00.

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# 340–27–097

Page 16 of 64 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 004–219 (a) Install these new wires:
REF. FIG. 4

Wire No: Class: From: Contact: To: Contact: Remarks: HL3001–24 A 293VS–A *** 35HL–J1:A2 item 25 *** splice together with HL67 and HL91 HL3004–24 A 292VS–A ** 36HL–J1:A2 item 25 ** splice together with HL64 and HL89

NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15.
FOR A/C 220–459 (b) Install these new wires:
REF. FIG. 6

Wire No: Class: From: Contact: To: Contact: Remarks: HL3006–24 A 35HL–J1:A2 item 25 91VP–P2:A20 solder item 34 HL3007–24 A 36HL–J1:A2 item 25 92VP–P2:B1 solder item 34

NOTE : For maintenance practices of the MTC connectors, Ref. WM 20–30–15.
FOR A/C ALL (c) Install these new wires:
FOR A/C 004–219 REF. FIG. 4
FOR A/C 220–459 REF. FIG. 6
FOR A/C ALL

Wire No: Class: From: Contact: To: Contact: Remarks: HL3000–24 A 1HL item 31 35HL–J1:X1 item 25 HL3002–24 A 305VN–G:4 item 27 35HL–J1:A1 item 25 HL3003–24 A 2HL item 31 36HL–J1:X1 item 25 HL3005–24 A 306VN–G:3 item 27 36HL–J1:A1 item 25
(d) Install these new wires:
REF. FIG. 8

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Page 17 of 64 Wire No: Class: From: Contact: To: Contact: Remarks: WH3000–24 A 306VS–FA * 306VT–R:H item 27 * splice together with WH3003 and WH311 WH3003–24 A 306VS–FA * 50WH–J1:X1 item 25 * splice together with WH3000 and WH311 WH3004–24 A 42WW–J1:C2 item 25 50WH–J1:X2 item 25 WH3005–24 A 42WW–J1:C1 item 25 306VN–G:1 item 27
NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. (e) Install these new wires: REF. FIG. 10

Wire No: Class: From: Contact: To: Contact: Remarks: GA3001–24 A 305VS–GK ** 21GA–J1:X2 item 25 ** splice together with GA84 and GA3003 GA3002–24 A 305VS–GJ * 21GA–J1:X1 item 25 * splice together with GA83 and GA3004 GA3003–24 A 305VS–GK ** 15GA–J1:X2 item 25 ** splice together with GA84 and GA3001 GA3004–24 A 305VS–GJ* 15GA–J1:X1 item 25 * splice together with GA83 and GA3002
NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. (f) Install these new wires: FOR A/C 004–078 REF. FIG. 11 FOR A/C 079–459 REF. FIG. 12 FOR A/C ALL

Wire No: Class: From: Contact: To: Contact: Remarks: WHC1–24 A 1VS–CC item 28 3WHC–P1:7 item 26 WHC2–24 A 306VS–VA item 28 50WH–J1:B3 item 25 WHC3–24 A 306VS–VB item 29 50WH–J1:B2 item 25 WHC4–24 A 306VS–VA 4WHC–702 item 27

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Page 18 of 64 Wire No: Remarks: Contact: To: Contact: From: Class: WHC5–24 A 306VS–VB 6WHC–701 item 27 WHC6–24 A 305VS–UA item 28 7WHC–J1:C2 item 25 WHC7–24 A 305VS–U item 28 7WHC–J1:X2 item 25 WHC8–24 A 305VS–U 7WHC–J1:A2 item 25 WHC9–24 A 1VS–CB item 28 3WHC–P1:8 item 26 WHC10–24 A 1VS–CB 3WHC–P1:9 item 26 WHC11–24 A 1VS–CA item 28 3WHC–P1:6 item 26 WHC12–24 A 1VS–CA 3WHC–P1:5 item 26 WHC13–24 A 1VS–CC 3WHC–P1:4 item 26 WHC14–24 A 1VS–CC 9WHC – item 27 WHC15–24 A 1VS–CC 5WHC – item 27 WHC19–24 A 306VS–VB 4WHC:701 item 27 WHC20–24 A 306VS–V item 28 6WHC:702 item 27 WHC21–24 A 306VS–VB 50WH–J1:A2 item 25 WHC22–24 A 306VS–V 50WH–J1:A3 item 25 WHC23–24 A 306VN–G:2 item 27 36HL–J1:B1 item 25 WHC24–24 A 305VS–U 36HL–J1:B2 item 25 WHC25–24 A 305VS–U 35HL–J1:B2 item 25 WHC26–24 A 305VN–G:2 item 27 35HL–J1:B1 item 25 WHC27–24 A 305VS–UA 7WHC–J1:B2 item 25 WHC28–24 A 305VS–UA 7WHC–J1:A1 item 25 WHC29–24 A 305VN–G:1 item 27 37WH–J1:B2 item 25 WHC30–24 A 37WH–J1:B1 item 25 5WHC + item 27 WHC31–24 A 3WHC–P1:A2 item 26 21GA–J1:A2 item 25 WHC32–24 A 160VS–A item 28 3WHC–P1:A3 item 26 WHC33–24 A 1VS–CB 306VS–V WHC34–24 A 1VS–CA 306VS–VA WHC35–24 A 160VS–A 306VS–VB WHC36–16 A 2WHC:L/1 item 30 36WH:911 * item 30 * WHC37–24 A 160VS–A 2WHC item 31 WHC40–24 A 305VN–G:3 item 27 305VS–UA WHC48–24 A 21GA–J1:A3 item 25 7WHC–J1:X1 item 25
NOTE : *) Install the terminal lug (30) to the wire, insulate the terminal lug with shrink sleeve (supplied in the kit). Park and stow this end adjacent to the circuit breaker 36WH. (36WH:L/1). NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. FOR A/C 004–078 (g) Install these new wires:

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Page 19 of 64 REF. FIG. 11

Wire No: Class: From: Contact: To: Contact: Remarks: WHC16–24 A 7WHC–J1:C1 item 25 4WH–P1:911 ** item 26 ** WHC17–24 A 7WHC–J1:B1 item 25 3WH–P1:911 * item 26 * WHC18–24 A 201VS–VA item 28 4WH–P1:911 ** item 26 ** WHC38–24 A 9WHC + item 27 201VS–VA WHC39–24 A 201VS–VA 3WH–P1:911 * item 26 *
NOTE : *) Install the contact (26) to the wire, insulate the contact with shrink sleeve (supplied in the kit). Park and stow this end adjacent to 3WH–P1. NOTE : **) Install the contact (26) to the wire, insulate the contact with shrink sleeve (supplied in the kit). Park and stow this end adjacent to 4WH–P1. NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. FOR A/C 079–459 (h) Install these new wires: REF. FIG. 12

Wire No: Class: From: Contact: To: Contact: Remarks: WHC16–24 A 7WHC–J1:C1 item 25 205VU–P17:A6 item 33 WHC17–24 A 7WHC–J1:B1 item 25 205VU–P17:A7 item 33 WHC38–24 A 9WHC + item 27 205VU–P17:A5 item 33 WHC41–24 A 203VS–VA item 28 205VU–J17:A5 item 32 WHC44–24 A 203VS–VA 4WH–P1:911 ** item 26 ** WHC45–24 A 205VU–J17:A6 item 32 4WH–P1:911 ** item 26 ** WHC46–24 A 203VS–VA 3WH–P1:911 * item 26 * WHC47–24 A 205VU–J17:A7 item 32 3WH–P1:911 * item 26 *
NOTE : *) Install the contact (26) to the wire, insulate the contact with shrink sleeve (supplied in the kit). Park and stow this end adjacent to 3WH–P1. NOTE : **) Install the contact (26) to the wire, insulate the contact with shrink sleeve (supplied in the kit). Park and stow this end adjacent to 4WH–P1. NOTE : For maintenance practices of the MTC connectors, Ref. WM 20–30–15. NOTE : For maintenance practices of the butt splices, Ref. WM 20–20–15. FOR A/C ALL (2) Parking of the circuit breaker 2WHC REF. FIG. 15 Sheet 3 of 5 view K (a) At the RH circuit breaker panel 12VU (position S–28), remove the circuit breaker 2WHC (14) from the circuit breaker panel. (2WHC was temporarily installed at step 2.B.(2)(e). ) (b) At the RH circuit breaker panel 12VU (position S–28), reinstall the cover. (The cover was temporarily removed at step 2.B.(2)(e). ) (c) Use a cable–tie to safety the circuit breaker 2WHC in open position. (d) Use the shrink sleeve (supplied in the kit) to insulate the circuit breaker 2WHC.

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# 340–27–097

Page 20 of 64 (e) Park and stow the circuit breaker 2WHC to the adjacent harness below the circuit breaker panel 12VU. NOTE : The wire WHC36–16 (electrical power to 2WHC) is parked and stowed at the circuit breaker 36WH (10VU). (3) Deactivation of the push button switch 3WHC REF. FIG. 15 Sheet 2 of 5 view L (a) Attach the push button switch 3WHC (15) to the instrument panel 1VU. (b) At the instrument panel 1VU, install the blank label (13) on top of the push button switch 3WHC to cover (hide) the push button switch 3WHC. NOTE : The wire WHC36–16 (electrical power to 3WHC) is parked and stowed at the circuit breaker 36WH (10VU). (4) Installation of relays (18 and 20) (a) In the electrical center 305VU: REF. FIG. 15 Sheet 4 of 5 view AD
1 At the relay console (1) at 7WHC–J1, install the relays 21GA (18) and 7WHC (18). (Ref. AMM 39–40–45).
2 At the front side of the relay console (1), install the marker decal 21GA adjacent to the relay 21GA.
3 At the front side of the relay console (1), install the marker decal 7WHC adjacent to the relay 7WHC.
4 At the relay console (1) at 35HL–J1, install the relay 35HL (20). (Ref. AMM 39–40–40).
5 At the front side of the relay console (1), install the marker decal 35HL adjacent to the relay 35HL.
6 At the relay console (1), use silicon tape and a strap to attach the wires to the relay console (1). Refer to figure 15 Sheet 4 of 5 view AD. NOTE : When you attach the wires to the relay console (1), make sure that you have sufficient length and routing of the wires to be able to loosen and withdraw the relay console (1) for future installations. (b) In the electrical center 306VU: REF. FIG. 15 Sheet 4 of 5 view AE
1 At the relay console (6) at 50WH–J1, install the relay 50WH (18). (Ref. AMM 39–40–45).
2 At the front side of the relay console (6), install the marker decal 50WH adjacent to the relay 50WH.
3 At the relay console (6) at 36HL–J1, install the relay 36HL (20). (Ref. AMM 39–40–40).
4 At the front side of the relay console (6), install the marker decal 36HL adjacent to the relay 36HL.
5 At the relay console (6), use silicon tape and a strap to attach the wires to the relay console (6). Refer to figure 15 Sheet 4 of 5 view AE. NOTE : When you attach the wires to the relay console (6), make sure that you have sufficient length and routing of the wires to be able to loosen and withdraw the relay console (6) for future installations. (5) In the electrical center 306VU, install the convoluted tubing (7) on the harness to the existing relay consoles in accordance with FIG. 15 Sheet 3 of 5 view H–H.

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Page 21 of 64 (6) Restore all affected wiring in accordance with the procedures in the wiring manual, Ref. WM 20–00–00. (7) Install the marker plates and the marker decals as applicable at the related items and locations. (8) Remove all the tools and equipment from the work area. Make sure the work area is clean. (9) Installation of removed units (a) Install the Multi Function Display (MFD 6FP) (Ref. AMM 34–25–05). (Only applicable for A/C with MFD installed). (b) If removed, install the LH and the RH Electronic Attitude Director Indicators (EADI 2FL and 2FM) (Ref. AMM 34–24–10). (c) If removed, install the LH and the RH Electronic Horizontal Situation Indicators (EHSI 3FL and 3FM) (Ref. AMM 34–24–15). (d) If removed, install the Flight Status Panel (51VU) (Ref. AMM 39–50–10). (e) If removed, install the Standby Horizon Indicator (3FN) (Ref. AMM 34–23–10). (10) Close the access: REF. FIG. 1 (a) Put the circuit breaker panel 10VU in position at the structure and tighten the screws. (b) Put the circuit breaker panel 11VU in position at the structure and tighten the screws. (c) Put the circuit breaker panel 12VU in position at the structure and tighten the screws. (d) Hold the access panel 215CZ in position to the structure and tighten the screws. (e) Hold the access panel 216CZ in position to the structure and tighten the screws. (f) In the electrical center 305VU, hold the loosened relay consoles in position and tighten the dzus fasteners. (g) In the electrical center 306VU, hold the loosened relay consoles in position and tighten the dzus fasteners. (h) Install the exterior access panels: – 117AL (electrical center L/H) – 118AR (electrical center R/H) – 210AL (windshield wiper LH) – 210AR (windshield wiper RH). (11) Install the LH and the RH flight crew seat (Ref. AMM 25–11–05). (12) Remove all the tools and equipment from the work area. Make sure the work area is clean.

D. FUNCTIONAL AND OPERATIONAL TEST NOTE : Do the tests that follows in order to test the connection of the wires in the connectors and the splices that has been opened during installation. (1) Prepare the aircraft for test (a) Supply the 28 VDC external power (Ref. AMM 12–00–00, servicing). (b) On the overhead panel DC ELEC (32VU), set the switches L AVION, R AVION and ESS AVION to ON. (c) On the overhead panel AC/DC ELEC (33VU), set the switch INVERTER to ON (1 or 2). If the AC/DC ELEC panel does not have the switch INVERTER, set the switch MAIN INV to position ON.

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Page 22 of 64 FOR A/C 220–459 (2) Do the functional test of the aural and visual alerts (Ref. AMM 31–50–00–05, Part 1). (3) Do this operational test of the AC Power–Inverter 1 :

ACTION RESULT (a) On the overhead panel AC/DC ELEC (33VU), set the switch INVERTER (or MAIN INV) to OFF. On the overhead panel AC/DC ELEC (33VU), the indicator light INVERTER
comes on. (b) On the overhead panel AC/DC ELEC (33VU), set the switch INVERTER to position 1. If the AC/DC ELEC panel does not have the switch INVERTER, set the switch MAIN INV to ON. On the overhead panel (33VU) the indicator light INVERTER goes off.

FOR A/C ALL (4) If the Standby Horizon Indicator was removed (for access), do the functional test of the Standby Horizon Indicator (Ref. AMM 34–23–10–05). (5) Do this operational test of the Engine Anti–Icing System:

ACTION RESULT (a) On the overheadpanel ENGINE (42VU), set the L/R ENGINE (Anti Ice) to ON. At the center instrument panel, on the flight status panel (51VU), the blue advisory light L/R ENG ANTI–ICE comes on. (b) On the overheadpanel ENGINE (42VU), set the L/R ENGINE (Anti Ice) to OFF. (6) Do this operational test of the relay function for the flight–idle stop (FI STOP) indicator light:

ACTION RESULT (a) Set the aircraft in ground configuration (L and R main landing–gear down and locked, weight on wheels). (b) At the L and R main landing–gear, install the WOW operating tool (TDO 5–4650224) on the WOW switches 5GA and 6GA, to set the aircraft in flight position. On the flight status panel 51VU, make sure the blue flight–idle stop (FI STOP) indicator light is not on.

(c) Remove the WOW operating tool from the L main landing–gear WOW switch 5GA. On the flight status panel 51VU, make sure the blue flight–idle stop (FI STOP) indicator light comes on. (d) Remove the WOW operating tool from the R main landing–gear WOW switch 6GA.
FOR A/C 079–459 POST Service Bulletin SAAB 340–34–139 (Mod No 3069) (7) Operational test of the Terrain Awareness and Warning System (TAWS)

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Page 23 of 64 (a) Do the operational test of the TAWS (Ref. AMM 34–46–00–05). (b) Do the operational test of the TERRAIN INHIBIT Switch (Ref. AMM 34–46–25–04). (c) Do the operational test of the TERR AWARE and the G/S INHIBIT Pushbutton Switches (Ref. AMM 34–46–30–04). FOR A/C 079–459 POST Service Bulletin SAAB 340–34–166 (Mod No 3167) (d) Do the operational test of the Steep Approach Pushbutton Switch (Ref. AMM 34–46–35–04) FOR A/C 079–459 POST Service Bulletin SAAB 340–34–136 (Mod 3034) (8) Do the operational test of the NPA/GPS System (Ref. AMM 34–60–00–05–2, Procedure 10) FOR A/C 220–299 (9) Do this operational test of the Left Nacelle Air–Intake Indicating–Lamp:

ACTION RESULT (a) On the overhead panel TEST 1 (19VU), set and hold the LAMPS/UPR/LWR switch to UPR. On the overhead panel TEST 3 (54VU), the L INTAKE lamp comes on.

(b) Release the LAMPS/UPR/LWR switch.

FOR A/C 220–459 (10) Do this operational test of the Avionics–Rack Air–Distribution:

ACTION RESULT (a) On the overhead panel DC ELEC (32VU), set the switches L AVION, R AVION and ESS AVION to OFF. (b) On the overhead panel DC ELEC (32VU), set the ESS AVION switch to ON. The avionics ventilation fan (7HN) operates. ( Feel by hand at the avionics rack manifold that the avionics ventilation fan moves air through the avionics rack.) (c) On the overhead panel DC ELEC (32VU), set the ESS AVION switch to OFF. The avionics ventilation fan (7HN) stops.

(d) On the overhead panel DC ELEC (32VU), set the switches L AVION, R AVION and ESS AVION to ON. (11) Do the operational test of the Engine–Nacelle Fire–Detection System (Ref. AMM 26–11–00–05, Procedure 1). (12) Do the operational test of the Smoke Detectors (Ref. AMM 26–13–00–05). (13) Do the operational test of the Bleed–Air–Duct Leak–Detection System (Ref. AMM 36–23–00–05). (14) Do this operational test of the Fuel Quantity Indicators:

ACTION RESULT

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Page 24 of 64 (a) On the overhead panel TEST 1 (19VU), set and hold the FUEL test switch to L. On the center instrument panel and on the wing refuel/defuel panel, the left FUEL QTY indicators shows 1000 ± 50 lbs. (455 ± 23 kg). (b) Release the FUEL test switch to the center position. The left FUEL QTY indicators shows the fuel quantity in left tank.

(c) On the overhead panel TEST 1 (19VU), set and hold the FUEL test switch to R. On the center instrument panel and on the wing refuel/defuel panel, the right FUEL QTY indicators shows 1000 ± 50 lbs. (455 ± 23 kg). (d) Release the FUEL test switch to the center position. The right FUEL QTY indicators shows the fuel quantity in right tank. (15) Do the operational test of the Fuel–Distribution Standby DC Boost–Pump (Ref. AMM 28–22–15–05). Do the test for both the LH and the RH side. (16) Do this operational test of the Flap Control System: WARNING : BE CAREFUL WHEN YOU OPERATE THE FLAPS. MAKE SURE THAT PERSONS ARE NOT NEAR THE FLAPS WHEN THE FLAPS OPERATES. THE FLAPS CAN CAUSE INJURY TO PERSONS. CAUTION : BE CAREFUL WHEN YOU OPERATE THE FLAPS. MAKE SURE THE AREA BELOW THE FLAPS IS CLEAR. DAMAGE TO THE FLAPS CAN OCCUR WHEN YOU LOWER THE FLAPS.

ACTION RESULT (a) On the center pedestal, make sure the flap control lever is in the UP position. (b) On the center pedestal, at panel 27VU, set the hydraulic pump switch to OVRD. The two pointers on the flap position indicator shows 0 °

.
(c) Move the flap control lever to the 15 ° position. The two pointers on the flap position indicator shows 15 °

. (d) On the overhead panel TEST 1 (19VU), press and hold the FLAPS test switch. On the TEST 1 panel (19VU), the FLAPS test light come on.

(e) Continue to press and hold the FLAPS test switch and move the flap control lever to the 20 ° position. – The two pointers on the flap position indicators do not respond – On the CWP, the FLAPS caution light start to flash – On the TEST 1 panel (19VU), the FLAPS test light start to flash. (f) Continue to press and hold the FLAPS test switch and move the flap control lever to the UP position. – The two pointers on the flap position indicators do not respond – On the CWP, the FLAPS caution light start to flash – On the TEST 1 panel (19VU), the FLAPS test light start to flash.

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Page 25 of 64 ACTION RESULT (g) On the overhead panel TEST 1 (19VU), release the FLAPS test switch. – The two pointers on the flap position indicator shows 0 ° – On the CWP, the FLAPS caution light goes off – On the TEST 1 panel (19VU), the FLAPS test light goes off.
NOTE : Do the tests that follows with the engines running. (17) Start the engines (Ref. AMM 71–00–00–05). (18) Do the operational test of the AC generating and distribution system (Ref. AMM 24–20–00–05). (19) Do this operational test of the Pitot/Static Heating: (a) On the RH circuit breaker panel 12VU, open these circuit breakers

LABEL POS C/B PROBE HEAT / STBY PITOT / PWR S–26 3HG PROBE HEAT / STBY PITOT / CONTROL S–27 7HG

ACTION RESULT (b) On the overhead panel ICE PROTECTION (21VU), make sure the STBY PITOT switch is set to OFF. On the overhead panel, ICE PROTECTION (21VU), the STBY PITOT lamp comes on. NOTE : If you need to reset the lamp, push in one of the MASTER CAUTION switches on the LH/RH glareshield panel. (c) On the RH circuit breaker panel 12VU, close these circuit breakers

LABEL POS C/B PROBE HEAT / STBY PITOT / PWR S–26 3HG PROBE HEAT / STBY PITOT / CONTROL S–27 7HG

ACTION RESULT (d) On the overhead panel ICE PROTECTION (21VU), set the STBY PITOT switch to ON. On the overhead panel ICE PROTECTION 21VU, the indication lamp STBY PITOT goes off. (e) On the overhead panel ICE PROTECTION (21VU), set the STBY PITOT switch to OFF. (20) Do this operational test of the Propellers De–icing System:
ACTION RESULT (a) On the overhead panel ICE PROTECTION (21VU), set the R PROP switch to MAX. – At the center instrument panel, on the flight status panel (51VU), the R PROP DE–ICE lamp comes on – On the overhead panel ICE PROTECTION (21VU), make sure the R PROP warning lamp is off.

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Page 26 of 64 ACTION RESULT (b) On the RH circuit breaker panel 12VU, open the R PROPELLER/ PWR ØC circuit breaker (P–23) for approximately two minutes. – On the central warning panel 3WW, the amber ICE PROT warning lamp flashes – On the overhead panel ICE PROTECTION (21VU), the R PROP warning lamp comes on. (c) On the RH circuit breaker panel 12VU, close the R PROPELLER/ PWR ØC circuit breaker (P–23). (d) On the overhead panel ICE PROTECTION (21VU), set the R PROP switch to OFF, and then set the switch to MAX. – On the central warning panel 3WW, the amber ICE PROT warning lamp goes off – On the overhead panel ICE PROTECTION (21VU), the R PROP warning lamp goes off – On the flight status panel (51VU), the L PROP DE–ICE lamp 36HJ comes on. (e) On then overhead panel ICE PROTECTION (21VU), set the R PROP switch to OFF. On the flight status panel (51VU), the R PROP DE–ICE lamp goes off.

(21) Do the operational test of the Temperature Control System (Ref. AMM 21–60–00–05). (22) Do the operational test of the Pneumatic Air–Supply Distribution System (Ref. AMM 36–11–00–02). (23) Do the operational test of the Airfoil De–Icing System (Ref. AMM 30–10–00–05). (24) Do the operational test of the Autocoarsen System (Ref. AMM 61–22–00–05). (25) Shut down the engines (Ref. AMM 71–00–00). FOR A/C ALL (26) Remove the electrical power (Ref. AMM 12–00–00). (27) Remove all the tools and equipment from the work area. Make sure the work area is clean.

E. JOB CLOSE–UP (1) Remove all the tools and equipment from the work area. Make sure the work area is clean. (2) Close the access: REF. FIG. 1 (a) At the avionics rack, install the access panels 210AZ and 220AZ. (b) In the flight compartment:
1 Install the access panels: – 117BZ (floor panel) – 215BZ – 215DZ – 215FZ – 215GZ – 216BZ – 216DZ – 216FZ

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Page 27 of 64 – 216GZ. FOR A/C 004–219 2 If removed, install these access panels: – 215EZ – 216EZ. FOR A/C ALL (3) Remove all the tools and equipment from the work area. Make sure the work area is clean.

3. MATERIAL INFORMATION

A. Modification Kit No SAAB 340–27–097–01 contains: NOTE : The Modification Kit contains the items for several configurations of the Saab 340. Some items (wires and contacts) are only applicable for some of the aircraft. Where an item has a specific effectivity it is given in the Remarks column. Items without aircraft effectivity listed in the Remarks column are effective for all aircraft.
Item Part Number Qty Nomenclature Designation Remarks 1 7239305–823 1 Relay console – At 305VU 2 7239305–091 2 Bracket – For the relay consoles (1) and (6) 3 7239305–092 2 Bracket – For the relay consoles (1) and (6) 4 7239224–103 4 Panel fastener – For the relay consoles (1) and (6) 5 TPEM–7 700mm Edge string – For the relay consoles (1) and (6) (and for the optional oxygen bottle) 6 7239305–824 1 Relay console – At 306VU 7 HCTE–1250–0– BLACK 100MM Convoluted tubing – At 306VU

– MS20470AD4–5 16 Rivet BJ4–5 – To attach the panel fasteners(4) to the brackets (2) and (3) – MS20470AD5–5 12 Rivet BJ5–5 – To attach the brackets (2) and (3) to structure – MS20470AD4–6 8 Rivet BJ4–6 – To attach 305VN–G and 306VN–G (23)

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Page 28 of 64 Item Remarks Designation Nomenclature Qty Part Number 13 7292183–009 1 Blank label – At 1VU, to cover 3WHC 14 MS3320–5 1 Circuit breaker 2WHC At 12VU15 4668–59 1 Illuminated pushbutton switch 3WHC At 1VU

16 7239791–512 2 Term block resistor 4WHC, 6WHC At 306VT 17 YHLZD–8 2 T.B. Diode 5WHC, 9WHC At 305VU and 3VT 18 M83536–6–022L O/T M83536–6–022M 3 Relay 21GA, 7WHC, 50WH At 305VU and 306VU

19 RSE120060 O/T S220A4A0 3 Relay socket 21GA–J1, 7WHC–J1, 50WH–J1 At 305VU and 306VU

20 M83536–2–024L O/T M83536–2–024M 2 Relay 35HL, 36HL At 305VU and 306VU

21 RSE120050 O/T S210A4A0 2 Relay socket 35HL–J1, 36HL–J1 At 305VU and 306VU

22 TY3–G1 6 Clamp bracket – At 305VU and 306VU 23 YHLZG–16–1 2 Grounding block 305VN–G, 306VN–G At 305VU and 306VU 25 M39029/101–553 44 Contact 15GA–J1, 21GA–J1, 35HL–J1, 36HL–J1, 37WH–J1, 50WH–J1, 7WHC–J1, 42WW–J1 26 M39029/57–354 16 Contact 3WHC–P1, 3WH–P1, 4WH–P1 27 YHMM22–2DB8 17 Contact 4WHC, 5WHC, 6WHC, 9WHC, 305VN–G, 306VN–G, 306VT–R

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Page 29 of 64 Item Remarks Designation Nomenclature Qty Part Number 28 D–436–36 18 Butt splice 201VS–VA, 203VS–VA, 292VS–A, 293VS–A, 1VS–CA, 1VS–CB, 1VS–CC, 160VS–A, 305VS–GJ, 305VS–GK, 305VS–U, 305VS–UA, 306VS–FA, 306VS–V, 306VS–VA, Unmarked splices qty. 4 201VS–VA valid for A/C 004–078. 203VS–VA valid for A/C 079–459. 292VS–A and 293VS–A valid for A/C004–219.

(Unmarked splices qty. 4 to extend wires WH375 & WH376 and HL13 & HL25 or HL64 & HL67) 29 D–436–37 1 Butt splice 306VS–VB 30 MS25036–153 2 Terminal lug 2WHC:L/1, 36WH:L/1 31 MS25036–146 3 Terminal lug 2WHC, 1HL, 2HL 32 CTA–0166 3 MTC–Contact 205VU–J17 Valid for A/C 079–459 33 CTA–0165 3 MTC–Contact 205VU–P17 Valid for A/C 079–459 34 CTA–0036 1 Butt solder sleeve kit 91VP–P2, 92VP–P2 Valid for A/C 220–459 – RNF–100 3/16 1 Marker sleeve (GA) 305VS–GJ

– RNF–100 3/16 1 Marker sleeve (GA) 305VS–GK

– RNF–100 3/16 1 Marker sleeve (WH) 306VS–FA

– RNF–100 3/16 1 Marker sleeve (HL) 292VS–A Valid for A/C 004–219 – RNF–100 3/16 1 Marker sleeve (HL) 293VS–A Valid for A/C 004–219 – RNF–100 3/16 1 Marker sleeve (WHC) 201VS–VA Valid for A/C 004–078 – RNF–100 3/16 1 Marker sleeve (WHC) 203VS–VA Valid for A/C 079–459

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Page 30 of 64 Item Remarks Designation Nomenclature Qty Part Number
– RNF–100 3/16 1 Marker sleeve (WHC) 1VS–CA

– RNF–100 3/16 1 Marker sleeve (WHC) 1VS–CB

– RNF–100 3/16 1 Marker sleeve (WHC) 1VS–CC

– RNF–100 3/16 1 Marker sleeve (WHC) 160VS–A

– RNF–100 3/16 1 Marker sleeve (WHC) 305VS–U

– RNF–100 3/16 1 Marker sleeve (WHC) 305VS–UA

– RNF–100 3/16 1 Marker sleeve (WHC) 306VS–V

– RNF–100 3/16 1 Marker sleeve (WHC) 306VS–VA

– RNF–100 3/16 1 Marker sleeve (WHC) 306VS–VB

– RNF–100 3/16 200mm Shrinkable tubing – At the 4 unmarked splices. – RNF–100 1/8 200mm Shrinkable tubing – For parking of contacts at 3WH–P1 and 4WH–P1. – RNF–100 1/4 100mm Shrinkable tubing – For parking of terminal lug at C/B 36WH. – RNF–100 1 200mm Shrinkable tubing – For parking of C/B 2WHC. – – 1 Marker decal 21GA – – 2 Marker decal 2WHC – – 1 Marker decal 3WHC – – 1 Marker decal 4WHC – – 1 Marker decal 5WHC – – 1 Marker decal 6WHC – – 1 Marker decal 7WHC – – 1 Marker decal 9WHC – – 1 Marker decal 1HL – – 1 Marker decal 2HL – – 1 Marker decal 35HL

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Page 31 of 64 Item Remarks Designation Nomenclature Qty Part Number
– – 1 Marker decal 36HL – – 1 Marker decal 36WH – – 1 Marker decal 50WH – – 1 Marker decal 305VN–G – – 1 Marker decal 306VN–G – – 1 Marker decal 21GA–J1 – – 1 Marker decal 3WH–P1 – – 1 Marker decal 4WH–P1 – – 1 Marker decal 37WH–J1 – – 1 Marker decal 50WH–J1 – – 1 Marker decal 7WHC–J1 – – 1 Marker decal 35HL–J1 – – 1 Marker decal 36HL–J1 – – 1 Marker decal 42WW–J1 – – 1 Marker decal 91VP–P2 – – 1 Marker decal 92VP–P2 – – 1 Marker decal 205VU–J17 – – 1 Marker decal 205VU–P17
– 6127432–016 O/T IT18R.NN901 13 Marker plate – at 2WHC, 3WHC, 36WH, 1HL, 2HL, 3WH–P1, 4WH–P1, 37WH–J1, 42WW–J1, 91VP–P2, 92VP–P2, 205VU–J17, 205VU–P17 – 55T9081–16–9 1700mm Wire WHC36–1601 ( AWG16 ) – 55T8015–24–9 2000mm Wire GA3001–2401 – 55T8015–24–9 2000mm Wire GA3002–2401 – 55T8015–24–9 300mm Wire GA3003–2401 – 55T8015–24–9 300mm Wire GA3004–2401 – 55T8015–24–9 1000mm Wire WH375–2401 – 55T8015–24–9 1000mm Wire WH376–2401 – 55T8015–24–9 300mm Wire WH3000–2401 – 55T8015–24–9 1500mm Wire WH3003–2401

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Page 32 of 64 Item Remarks Designation Nomenclature Qty Part Number
– 55T8015–24–9 1500mm Wire WH3004–2401
– 55T8015–24–9 1200mm Wire WH3005–2401 – 55T8015–24–9 2500mm Wire HL13–2401 Valid for A/C 004–219 – 55T8015–24–9 3000mm Wire HL25–2401 Valid for A/C 004–219 – 55T8015–24–9 2500mm Wire HL64–2401 Valid for A/C 220–459 – 55T8015–24–9 3000mm Wire HL67–2401 Valid for A/C 220–459 – 55T8015–24–9 2500mm Wire HL3000–2401 – 55T8015–24–9 3000mm Wire HL3001–2401 Valid for A/C 004–219 – 55T8015–24–9 1700mm Wire HL3002–2401
– 55T8015–24–9 2500mm Wire HL3003–2401 – 55T8015–24–9 2500mm Wire HL3004–2401 Valid for A/C 004–219 – 55T8015–24–9 1700mm Wire HL3005–2401 – 55T8015–24–9 3000mm Wire HL3006–2401 Valid for A/C 220–459 – 55T8015–24–9 2500mm Wire HL3007–2401 Valid for A/C 220–459 – 55T8015–24–9 300mm Wire WHC1–2401 – 55T8015–24–9 500mm Wire WHC2–2401 – 55T8015–24–9 500mm Wire WHC3–2401 – 55T8015–24–9 1500mm Wire WHC4–2401 – 55T8015–24–9 1500mm Wire WHC5–2401 – 55T8015–24–9 300mm Wire WHC6–2401 – 55T8015–24–9 300mm Wire WHC7–2401 – 55T8015–24–9 300mm Wire WHC8–2401 – 55T8015–24–9 300mm Wire WHC9–2401 – 55T8015–24–9 300mm Wire WHC10–2401 – 55T8015–24–9 300mm Wire WHC11–2401 – 55T8015–24–9 300mm Wire WHC12–2401 – 55T8015–24–9 300mm Wire WHC13–2401 – 55T8015–24–9 1500mm Wire WHC14–2401 – 55T8015–24–9 5500mm Wire WHC15–2401

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Page 33 of 64 Item Remarks Designation Nomenclature Qty Part Number
– 55T8015–24–9 4500mm Wire WHC16–2401 Use 3000 mm for A/C 079–459 – 55T8015–24–9 4500mm Wire WHC17–2401 Use 3000 mm for A/C 079–459 – 55T8015–24–9 500mm Wire WHC18–2401 Valid for A/C 004–078 – 55T8015–24–9 1500mm Wire WHC19–2401 – 55T8015–24–9 1500mm Wire WHC20–2401 – 55T8015–24–9 500mm Wire WHC21–2401 – 55T8015–24–9 500mm Wire WHC22–2401 – 55T8015–24–9 1700mm Wire WHC23–2401 – 55T8015–24–9 2200mm Wire WHC24–2401 – 55T8015–24–9 300mm Wire WHC25–2401 – 55T8015–24–9 1700mm Wire WHC26–2401 – 55T8015–24–9 300mm Wire WHC27–2401 – 55T8015–24–9 300mm Wire WHC28–2401 – 55T8015–24–9 1700mm Wire WHC29–2401 – 55T8015–24–9 2200mm Wire WHC30–2401 – 55T8015–24–9 5500mm Wire WHC31–2401 – 55T8015–24–9 3500mm Wire WHC32–2401 – 55T8015–24–9 4500mm Wire WHC33–2401 – 55T8015–24–9 4500mm Wire WHC34–2401 – 55T8015–24–9 1200mm Wire WHC35–2401 – 55T8015–24–9 1200mm Wire WHC37–2401 – 55T8015–24–9 6000mm Wire WHC38–2401 Use 4500 mm for A/C 079–459 – 55T8015–24–9 300mm Wire WHC39–2401 Valid for A/C 004–078 – 55T8015–24–9 1500mm Wire WHC40–2401

– 55T8015–24–9 1000mm Wire WHC41–2401 Valid for A/C 079–459 – 55T8015–24–9 1500mm Wire WHC44–2401 Valid for A/C 079–459 – 55T8015–24–9 2200mm Wire WHC45–2401 Valid for A/C 079–459 – 55T8015–24–9 1300mm Wire WHC46–2401 Valid for A/C 079–459

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Page 34 of 64 Item Remarks Designation Nomenclature Qty Part Number
– 55T8015–24–9 2000mm Wire WHC47–2401 Valid for A/C 079–459 – 55T8015–24–9 300mm Wire WHC48–2401

FOR A/C 079–459 PRE SB340–34–139

B. Modification Kit No SAAB 340–27–097–02 contains:

Item Part Number Qty Nomenclature Designation Remarks 232 MTC100–JH–2–R22 1 Receptacle 205VU–J17 233 MTCP–122–20P1 1 Insert pin A1B1 (Wafer) – 205VU–J17

234 CHA–0124 4 Dummy Wafer – 205VU–J17/P17 235 MTC100–JH–2–P22 1 Plug Housing 205VU–P17 236 MTCP–122–20S1 1 Insert socket A1B1 (Wafer) – 205VU–P17

237 NAS1101–06–36 2 Screw – for 205VU–J17 – – 1 Marker decal 205VU–J17 – – 1 Marker decal 205VU–P17

FOR A/C ALL

C. Local supply FOR A/C ALL
Item Part Number Qty Nomenclature Designation Remarks – NITTO 665 AR Silicone tape – – – AR Lacing cord – – – AR Cable–tie – – – AR Alodine 1500 – – PR 1422 B–1/2 A/R Sealant – MIL–S–8802 Type II, Class B–1/2– Methyl–Ethyl–Ketone (MEK) A/R Cleaning agent – TT–M–261

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

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Page 35 of 64 D. Removal FOR A/C 200–459
Item Part Number Qty Nomenclature Designation Remarks 112 YHLZ1–C–7 1 Dummy block 3VT

FOR A/C 079–459 PRE SB340–34–139

– NAS1101–06–30 2 Screw – at 205VU

FOR A/C ALL

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Page 36 of 64 A30716 215BZ 216BZ
215CZ 216CZ

215FZ 216FZ 215DZ 216DZ 10 VU

215GZ 11VU 215EZ 216EZ

12VU

216GZ 117AL 210AL

118AR 210AR 117BZ

STA 186.0 STA 215.0 A

210AZ

AVIONIC

RACK 220AZ

VIEW A

Access Panels – Location FIG. 1

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Page 37 of 64 6.12 0.04 in (155.5 1 mm)

3.96 0.04 in (100.5 1 mm)

0.689 0.01 in (17.5 0.25 mm) (0.8 mm) R 0.0315 in (TYP 4 PLCS)

SQUARE A30715 Center Instrument Panel 1VU – Modification of Panel 1VU for Installation of Push Button Switch 3WHC FIG. 2

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Page 38 of 64      

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### Service Bulletin

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Page 39 of 64      

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### Service Bulletin

01 September 2011

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### Service Bulletin

01 September 2011

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# 340–27–097

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01 September 2011

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01 September 2011

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### Service Bulletin

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Page 44 of 64 A30883 " "







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### Service Bulletin

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Page 45 of 64 A30884 !
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### Service Bulletin

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Page 46 of 64 

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### Service Bulletin

Date Month Year

Revison X, Date Month Year 

# 340–XX–XXX

Page 48Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 49/50 of 64A30948

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### Service Bulletin

Date Month Year

Revison X, Date Month Year 

# 340–XX–XXX

Page 50Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 51/52 of 64AIR DIST. REF8.47 in (215.1 mm)1.97 in(50.0 mm)4.18 in(106.2 mm)0.20 in(5.0 mm)A30699USE ITEM 01AS TEMPLATEVIEW C ONLY APPLICABLEFOR A/C WITH OPTION231–1 PORTABLE OXYGENBOTTLE INSTALLEDElectrical Center 305VU – Installation of Relay ConsoleFIG. 13

### Service Bulletin

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Page 52Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 53/54 of 64MAKE SURE THERE IS CLEARANCEBETWEEN FLANGE ON RELAY CONSOLEAND STATIC PRESSURE TUBE0.20 in(5.0 mm)8.47 in (215.1 mm)1.97 in(50.0 mm)4.18 in(106.2 mm)06A30700COMP. PRESS. REFAIR DIST. REFElectrical Center 306VU – Installation of Relay ConsoleFIG. 14

### Service Bulletin

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Page 54Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 55/56 of 64A31109Flight Compartment – Component Location and Wire RoutingFIG. 15 (Sheet 1 of 5)

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Page 56Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 57/58 of 64A3071411INSTALL BLANK LABEL ITEM 13 ON TOPOF THE PUSH BUTTON SWITCH 3WHCFlight Compartment – Component Location and Wire RoutingFIG. 15 (Sheet 2 of 5)

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Page 58Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 59/60 of 6415GA RefA/C 004–37915GA RefA/C 380–459TO VIEW AE TO VIEW AD7INSTALL CONVOLUTEDTUBE ON HARNESS TOEXISTING RELAY CONSOLESA30711LOCATION:S281122SECURE C/B 2WHC IN OPEN POSITION. INSULATE WITHSHRINK SLEEVE AND STOW BEHIND C/B PANEL 12VUPARK AND STOW WIRE WHC36–1601 BEHINDC/B PANEL 10VU ADJACENT TO C/B 36WHFlight Compartment and Electrical Center – Component Location and Wire RoutingFIG. 15 (Sheet 3 of 5)

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Page 60Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 61/62 of 64A30990TO VIEWH–HTO VIEWH–HTO VIEWH – H21GA21GA–J1TO VIEWH – HElectrical Center – Component Location and Wire RoutingFIG. 15 (Sheet 4 of 5)

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Date Month Year

Revison X, Date Month Year 

# 340–XX–XXX

Page 62Service Bulletin01 September 2011Revision 03, 19 April 2012340–27–097Page 63/64 of 64A311100.790.79 in(20 20 mm)0.16+0 in–0.20 in(4+0 mm)–5 mm)Electrical Center and Avionics Rack – Component Location and Wire RoutingFIG. 15 (Sheet 5 of 5)

### Service Bulletin

Date Month Year

Revison X, Date Month Year 

# 340–XX–XXX

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