## Dornier 328

Revision Transmittal Sheet 328 Support Services

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany e-mail gsc.op@328suppor t.de

Model Dornier 328 No. SB-328-76-486

Date of Issue Apr 07, 2010

Page 1 of 1 

### Revision Transmittal Sheet

This sheet transmits Revision 3 to Service Bulletin SB-328-76-486, titled:

Engine Controls – Modification of Power Lever Assem bly and introduction of Crew Aural

Alerting Device.

This is a complete Revision. This SB has been repri nted in its entirety. All previous editions

must be destroyed.

NOTE: This Revision does require further action.

Reason for Revision:

Page 2: Manpower corrected.

Page 11: Material List corrected.

Page 29, 30: Figure 17, 18. corrected.

NOTE: The changes are marked with revision marker a t the right hand page margin.

This Revision Transmittal Sheet is Part of SB-328-7 6-486 Revision 3.Page 2 of 30 SB-328-76-486R3

Manpower

Access: 11 Mhrs.

Modification: 60 Mhrs.

Close-up: 9 Mhrs.

Functional checks: 19 Mhrs.

Total: 99 Mhrs. (based on an experienced modific ation crew)

Material

According to Material Parts List.

Special Tools

Not necessary.

Weight and Balance

The changes of weight and moment differ depending w hether options 040-011, 235K001

and SB-328-30-231 are installed or not installed. T he corresponding values are given in

the table below. The appropriate change of weight a nd moment must be incorporated into

the Basic Weight and Balance Record of the WBM.

Option Option SB Change of Weight Change of Moment

040-011 235K001 328-30-

231 (kg) (lb) (kg m) (1000 lb in)

Standard A/C 4,952 10,917 17,757 1,541



### x 5,252 11,579 18,867 1,638



### x 5,122 11,292 18,551 1,610



### x x 5,422 11,953 19,661 1,706



### x 4,722 10,410 17,005 1,476



### x x 5,022 11,072 18,115 1,572



### x x 4,892 10,785 17,799 1,545 installed

Option / SB



### x x x 5,192 11,446 18,909 1,641

Electrical Load Data

Max. 2 A on NON ESS BUS1 = 1PP

Max. 2 A on NON ESS BUS2 = 5PP

References

Not affected.

Other Publications Affected

Airplane Flight Manual (AFM)

Airplane Maintenance Manual (AMM)

Airplane Operating Manual (AOM)

Aircraft Illustrated Parts Catalogue (AIPC).

Maintenance Review Board Report (MRB)

Weight and Balance Manual (Equipment List)

Wiring Manual (WM)

Quick Reference Handbook Check list (QRH)

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 3 of 30 

# SB

Reporting

Compliance of this Service Bulletin must be reporte d to 328 Support Services GmbH

Customer Services Department using the Compliance R eport for Configuration Control.



### 2.ACCOMPLISHMENT INSTRUCTIONS

CAUTION: Obey Safety Precautions and General Mainte nance Practices

according to AMM JIC Chapter 00.

CAUTION: Obey the following SRM chapters:

51-40-10, ’Drill and hole data’

51-41-20, ’Rivet installation and removal - metal s tructure’

51-41-30, ’Rivet installation and removal - non-met al structure’

51-40-11, ‘Fastener hole and drill data - metal str ucture’

51-40-12, ’Fastener hole and drill data - non-metal structure’

51-41-41, ’Alternative rivets - metal structure’

51-41-42, ’Alternative rivets - non-metal structure ’

51-21-00, ’Cleaning processes’

51-22-00, ’Sealing’

51-77-32, ’Composite sandwich structures’

51-90-00; ‘Surface protection’

51-93-00, ‘Paint Repair’

CAUTION: For modification to aircraft electrical wi ring refer to Maintenance

Practices according to Wiring Manual Chapter 20.

Obey the Aircraft Electrical Bonding Maintenance Pr actices

according to the AMM JIC 20-28-00.Page 4 of 30 SB-328-76-486R3

A Preparation

(1) Make the aircraft safe for maintenance accordin g to AMM JIC 00-30-01.

(2) Remove engine control box according to AMM JIC 76-11-04.

(3) Remove LH and RH side panel according to AMM JI C 25-12-02 as required to

get access to modification area.

(4) Remove rack panels LH and RH according to AMM J IC 25-12-03 as required

to get access to modification area.

(5) Open necessary floors/panels according to AMM J IC 06-40-00 as required to

get access to modification area.

(6) Remove equipment in cockpit center console as n ecessary according to the

relevant AMM JIC ́s to get space enough for installa tion of summing amplifiers.

(7) Remove micro air data computer 1FA/11FA accordi ng to AMM JIC 34-11-01.

(8) Remove audio panel 1 & 2, according to AMM JIC 23-51-00.

(9) Remove 3rd audio control panel when installed a ccording to observer audio

controls maintenance practices AMM JIC 23-51-23.

(10) Remove C/B side-panel 10VE (RH) according to A MM JIC 31-12-08.

(11) Remove C/B side-panel 11VE (LH) according to A MM JIC 31-12-09.

(12) Remove relay support 20VE according to AMM JIC 31-12-16.

B Modification

(1) Install new wiring harness (item no. 2) for Pow er Lever Aural Alert System

along existing wiring harnesses according to Fig. 1 – 9.

(2) Modification of CB side-panel 10VE (refer to Fi g.10, 17, 18)

(a) Install circuit breaker 16KW (item-no. 6) in CB side-panel according to Fig.10

and stick placard (item no. 11) beside circuit brea ker 16KW on backside of CB

side-panel.

(b) Exchange existing placard by new placard (item no. 10, 10a, or 10b) at front

side of CB side-panel.

(c) Connect circuit breaker 16KW at contact rail (i tem no. 7a) and wire harness

(item no. 3) and cover contact rail with shrink tub e on unused CB places.

(d) Connect wire harness (item no. 3) at receptacle 10VE*A according Fig.10 and

17, 18.

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 5 of 30 

# SB

(e) Restore wire harness in CB side-panel.

(3) Modification of CB side-panel 11VE (refer to Fi g.11, 17, 18)

(a) Install circuit breaker 15KW (item-no. 6) in CB side-panel according to Fig.11

and stick placard (item no. 9) beside circuit break er 15KW on backside of CB

side-panel.

(b) Exchange existing placard by new placard (item no. 12) at front side of CB

side-panel.

(c) Connect circuit breaker 15KW at contact rail (i tem no. 7) and wire harness

(item no. 4).

(d) Connect wire harness (item no. 4) at receptacle 11VE*A according Fig.10 and

17, 18.

(e) Restore wire harness in CB side-panel.

(4) Modification of relay support 20VE (refer to Fi g.12, 17, 18)

(a) Position relay sockets 3KWA and 4KWA ( part of wiring harness item no. 5) in

relay support as shown in Fig.12 and transfer attac hment holes from relay

sockets to relay support 20VE; hole diameter 5,3 mm = 0.209 inch.

(b) Remove relay sockets 3KWA and 4KWA and restore surface protection of

relay support.

(c) Install wire harness (item no. 5) with relay so ckets 3KW and 4KW in relay

support and connect wire harness at receptacle 20VE A and 20VEB according

to wiring diagram Fig. 17, 18.

(d) Restore wire harness in relay support.

(e) Install relay 3KW/ 4KW with placards (item no. 13-15) on relay support.Page 6 of 30 SB-328-76-486R3

(5) Installation of summing amplifiers 101RZ and 11 1RZ

NOTE: The installation is described for one summing amplifier, but has to

be performed with both amplifiers 101RZ and 111RZ.

Note: Ensure electrical bonding from summing amplif ier to structure;

refer to AMM JIC 20-28-00 method 410.

(a) Pre-complete summing amplifier (item no. 16) wi th angle (item no. 17); use

attachment material item no. 18 and position pre-co mpleted unit in center

console according Fig. 14.

(b) Transfer attachment holes from pre-completed un it to center console; hole

diameter according SRM for rivet item no. 20.

(c) Remove pre-completed unit and restore surface p rotection of center console.

(d) Install pre-completed unit (summing amplifier i tem no. 16 and two angles item

no. 17) in center console according Fig. 14, use ri vets item no.20.

(e) Install placards (item no. 26, 27) at summing a mplifiers.

(6) Installation of summing amplifier 131RZ

NOTE: The installation is only necessary, if option 235K001 (3 rd audio

panel) is installed in a/c.

NOTE: Ensure electrical bonding from summing amplif ier to structure;

refer to AMM JIC 20-28-00 method 410; use existing bonding

point.

(a) Position summing amplifier 131RZ in avionic rac k RH near 3 rd audio panel

according Fig.15

(b) Transfer attachment holes from summing amplifie r to avionic rack RH; hole

dia. 3,6 mm = 0.141 inch and restore surface protec tion.

(c) Install summing amplifier 131RZ (item no. 16a) in RH avionic rack according

Fig. 15; use attachment material item no. 21-23.

(d) Stick placard (item no. 24) near summing amplif ier, refer to Fig. 15.

(7) Modification for audio panel LH (refer Fig. 17, 18)

(a) Eject wire RZ022E24 out of plug 1RZ*B pin A and *A, extract wire out of wiring

harness till splice SP1350/SP1351 (refer to WM 23-4 1-00).

(b) Route wire RZ022E24 to summing amplifier 101RZ and connect wire

according Fig. 17, 18.

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 7 of 30 

# SB

(8) Modification for audio panel RH (refer Fig. 17, 18)

(a) Eject wire RZ126E24 out of plug 11RZ*B pin A an d *A, extract wire out of

wiring harness till splice SP1350/SP1351 (refer to WM 23-42-02/04).

(b) Route wire RZ126E24 to summing amplifier 111RZ and connect wire

according Fig. 17, 18.

(9) Modification for third audio panel (refer Fig. 17, 18)

NOTE: The modification is only necessary, if option 235K001 (third audio

panel) is installed in a/c.

(a) Refer to para B (7) and B (8) and open wire har ness at splice SP1350/1351 in

center console (refer to WM 23-41-00).

(b) Cut splice SP1350/1351 and connect existing wir es with wire RZ022G24 (part

of item no. 2) by use of new splice (provided with item no. 2), refer to Fig. 17,

18.

(10) Structural modification for installation of gr ound connector 114VVNS.

(a) Check if SB-328-30-231 is installed or not. If it is installed continue with (b) if

not continue with (20)

(b) Drill holes and install rivet nuts (item no. 28 ) according Fig. 16; use rivets item

no. 29.

NOTE: Ensure electrical bonding from rivet nut to s tructure; refer to AMM

JIC 20-28-00 method 41.

(c) Install ground connector 114VVNS at structure u sing attachment material item

no. 30, 31, refer to Fig. 16

NOTE: Ensure electrical bonding from ground connect or to structure; refer

to AMM JIC 20-28-00 method 410.Page 8 of 30 SB-328-76-486R3

(d) Install placard (item no. 25) at 114VVNS.

(11) Connect wire harness (item, no. 2) at all equi pment according to Fig. 17, 18.

(12) If 3rd audio panel (option 235K001) is not ins talled, store plug 131RZ*A and

residual wires in the area of third summing amplifi er in an adequate additional

plastic cap on the plug 131RZ and secure at existin g wire harness.

(13) Restore all wiring harness in modification are a and perform a continuity check

of newly installed wiring.

(14) Install the modified engine control box accord ing to AMM JIC 76-11-04.

(a) Position the modified engine control box (item no. 1, 1a or 1b) in the flight

compartment and align it with the attachment points in the floor.

(b) Install the Emergency/Parking Brake Handle acco rding to AMM JIC 32-43-01.

(c) Connect all electrical connectors according to Fig. 17, 18 and AMM JIC

76-11-04.

(d) Continue to install the modified engine control box according to AMM JIC

76-11-04.

(15) Re-install audio panel 1 & 2 (and 3rd when equ ipped) according to AMM JIC

23-51-00 (and 23-51-23).

(16) Reinstall Micro Air Data Computer 1FA/11FA acc ording to AMM JIC 34-11-01.

(17) Install C/B Side-Panel 10VE (RH) according to AMM JIC 31-12-08.

(18) Install Relay Support 20VE according to AMM JI C 31-12-16.

(19) In addition to necessary adjustment and tests described in the current AMM

JIC 76-11-04, 31-12-08, 31-12-09 and 31-12-16; perf orm also functional test

procedure of power lever aural alert system accordi ng to AMM JIC 76-12-00

and passenger address system – functional test JIC 23-31-00.

If step (20) was necessary, perform an operational test of the cockpit window

heating system according to AMM JIC 30-42-00.

(20) Installation of mounting adapter

(a) Remove existing heat controllers 6HF and 26 HF according to AMM JIC 30-

42-02.

(b) Perform step (10.b).

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 9 of 30 

# SB

(c) Install mounting adapter (item no. 31,32) on ex isting mounting profiles with

screw and washer (item no. 33,34) according to Fig . 7a.

Note: Before installation, make sure, the surface protection for bonding

on existing mounting profile and new mounting ada pter must be

performed as shown at fig.7a according to AMM JIC 2 0-28-00.

Ensure electrical bonding from rivet nut to structu re; refer to AMM JIC 20-

28-00 method 41.

(d) Install old controllers and connector bracket w ith screws and washers (item

no.34,36) according to fig.7a and reconnect all con nectors.

Reinstall the cable brackets again on the controlle r with screws and washers

(item no.35,36).

(e) Continue with step (10.c) to step (19).

C Close-up

(1) Perform a foreign object inspection in and arou nd the modification area.

(2) Reinstall LH and RH side panel according to AMM JIC 25-12-02 as required.

(3) Reinstall rack panels LH and RH according to AM M JIC 25-12-03 as required.

(4) Reinstall all opened floors/panels according to AMM JIC 06-40-00.

(5) Reinstall the crew seats in the cockpit accordi ng to AMM JIC 25-11-01.

(6) Return the aircraft to a serviceable condition.

NOTE: All tests and checks have been described abov e to ensure proper

function of all systems after this modification wit h the aircraft on

ground. Compliance with the tasks fulfils all requi rements to bring

the aircraft back into an airworthy state. It is up to the operator and

the local authority to decide whether to reconfirm the functionality

of affected systems in flight is required.Page 10 of 30 SB-328-76-486R3



### 3.MATERIAL INFORMATION

Item-No. P/N: Qty. Nomenclature Remarks

1 001A761A1010010 1 Engine control box 3005up to 30 79

1a 001A761A1010012 1 Engine control box 3080 and up

1b 001A761A1010014 1 Engine control box Option 040- 011 only

2 001A909A1261000 1 Wire harness

2a 001A909A1261002 1 Wire harness Option 040-011 on ly

3 001A904A7109008 1 Wire harness 10VE Cut cable len gth A/R

4 001A904A7119016 1 Wire harness 11VE Cut cable len gth A/R

5 001A904A1209002 1 Wire harness 20VE

6 EN2495-02AU 2 Circuit breaker 15KW,16KW

7 001A311A5106202 1 Rail 11VE

7a 001A311A5306212 1 Rail 10VE

8 DIN137-B4-FST-B3P 2 Spring washer

9 001A311A5259224 1 Placard 15KW

10 001A311A5251260 1 Placard

10a 001A311A5251262 1 Placard

10b 001A311A5251264 1 Placard 10VE depending of

current CB installation

11 001A311A5159234 1 Placard 16KW

12 001A311A5151278 1 Placard 11VE

13 FLR300-D4A-2A2 2 Relay 3KW, 4KW

14 001A904A1203282 1 Placard 3KW

15 001A904A1203284 1 Placard 4KW

16 990-3338-000 2 Summing amplifier 01RZ,111RZ

16a 990-3338-000 1 Summing amplifier 131RZ

(option235K001 only)

17 001A251A5306000 4 Angle

18 NAS1101E06-5 8 Screw

19 Left blank

20 CR3523P-4-2 12 Rivet

21 MS21043-06 4 Nut (option235K001 only)

22 AN960-6L 4 Washer (option235K001 only)

23 NAS1101E06-6 4 Screw (option235K001 only)

24 001A902A3203248 1 placard 131RZ

(option235K001 only)

25 001A907A1110370 1 Placard 114VVNS

26 001A907A1110372 1 Placard 101RZ

27 001A907A1110374 1 Placard 111RZ

28 MS21052L08 2 Rivet nut

29 DON299-2400 4 Rivet Alternative see

SRM 51-41-41

30 NAS1096-2-8 2 Screw

31 NAS620-8L 2 Washer

32 001A304A3001000 1 Mounting Adapter

33 001A304A3001001 1 Mounting Adapter

34 NAS 1096-3-10 12 Screw

35 NAS 1096-3-12 2 Screw

36 AN960-10L 14 Washer only used if SB-328-

30-231 is not installed

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 11 of 30 

# SB

37 MS39029/57-357 A/R Socket pin for Audio

Panel connector

38 MS39029/63-368 4 Socket pin for

Summing Amplifier

connector

39 MS39029/11-144 A/R Pin for PSEU

connector Note:

Normally this should

be part of the

connector, use this if

required.

SP1350

SP 1351 40 D436-82 3

SP 1677

41 D436-83 1 SP1363 Splice material

42 006-1169-16 or

M39029-4-112 A/R Socket for

connection 11VE*A Special AWG16 socket

usable for AWG22

wire

43 006-1168-16 or

M39029-5-117 A/R Pin for connector

11VEA Special AWG16 pin

usable for AWG22

wire

The following expendables to be provided by operato r and/or ordered separately (not

part of the Kit):

Item-No. P/N: Qty. Nomenclature Remarks

MIL-T-43435 A/R Lacing tape CML No. 05-142

MS3367-1-9 A/R TY -rap

DWQ-575X-XXX A/R Coppermesh WM 20-14-02

DR25-TW 1⁄2-0 A/R Shrink sleeve

diameter 1⁄2

“ CML No. 05-179Page 12 of 30 SB-328-76-486R3 Wiring Installation side view

Fig. 1

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 13 of 30 

# SB

Wiring Installation top view

Fig. 2Page 14 of 30 SB-328-76-486R3 View from Fig 1 (Frame 10 seen in flight direction)

Fig. 3 see Fig.4

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 15 of 30 

# SB

View from Fig. 3 (frame 10/11 RH)

Fig. 4Page 16 of 30 SB-328-76-486R3 View from Fig. 2 (frame 4 – 10 LH)

Fig. 5

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 17 of 30 

# SB

View from Fig. 1 (frame 4 looking forward)

View from Fig. 1 (frame 3 looking forward)

Fig. 6Page 18 of 30 SB-328-76-486R3 View from Fig. 6

Fig. 7

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 19 of 30 

# SB

Fig. 7aPage 20 of 30 SB-328-76-486R3 View from Fig. 7 to LH

View from Fig. 7 to RH

Fig. 8

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 21 of 30 

# SB

View from Fig. 2 (frame 4 – 10 LH)

Fig. 9Page 22 of 30 SB-328-76-486R3 C/B Panel 10VE

Fig.10

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 23 of 30 

# SB

C/B Panel 11VE

Fig. 11Page 24 of 30 SB-328-76-486R3 Relay Support 20VE

Fig. 12

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 25 of 30 

# SB

Center console

Fig. 13Page 26 of 30 SB-328-76-486R3 Installation summing amplifiers 101RZ(LH), 111RZ(RH )

Fig. 14

## Dornier 328

Service Bulletin 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany

Model Dornier 328 Rev. No. 3 No. SB-328-76-486

Rev. Date. Apr 07, 2010 Date of Issue Jul 15, 2009

Page 27 of 30 

# SB

Installation summing amplifiers 131RZ

Fig. 15Page 28 of 30 SB-328-76-486R3 Installation of ground connector 114VVNS

(detail from Fig. 7)

Fig. 16Page 29 of 30 SB-328-76-486R3Wiring DiagramFig. 17Page 30 of 30 SB-328-76-486R3Wiring Diagram for option 040-011 (Mod.30 a/c) onlyFig. 18

## Dornier 328/328J

Compliance Report 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany e-mail gsc.op@328support .de 

# CR

Please complete this Compliance Form for each aircr aft only when it is applicable,

and mail or fax to:

Attention: Dept. P1

328 Support Services GmbH

Customer Services

P.O.B. 1252

D-82231 Wessling

Telefax +40 (0) 8153 88111- 6565

From Company:

___________________________________________________ __________________________________

___________________________________________________ __________________________________

AOT No.: Rev.: Title:

ASB No.: Rev.: Title:

SB No.: Rev.: Title:

EO No.: Rev.: Title:

Aircraft Serial Number:

______________________________________________ _______________________________ Operator:

_________________________________________________ _______________________________________________ Total Flight Hours: Total Landings:

________________________ ___________________ ______ Date of compliance:

______________________________________________ _______________________________

Comments:

__________________________________________________ _______________________________________

___________________________________________________ ___________________________________________________ ______

___________________________________________________ ___________________________________________________ ______

__________________ _________________________ ______ Date Authorized signature

## Dornier 328/328J

In Service Technical Information 328 Support Services GmbH

Customer Services Global Support Center

P. O. Box 1252 Phone +49 (0) 8153 88111-6666

D-82231 Wessling Telefax +49 (0) 8153 88111-6565

Fed. Rep. of Germany e-mail gsc.op@328support .de

Model Dornier 328/328J Rev. No. No.

Rev. Date. Date of Issue

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Relevant and legally binding is the printed docum ent.