WIRING MANUAL · LOT, Revision 3 Mar 01/13 Page 1 z SD3-60 AIRCRAFT WIRING MANUAL TO: Holders of...

0

WIRING MANUAL Ref. No. 360 I WM I

STATEMENT OF INITIAL CERTIFICATION

This manual complies with British Civil Airworthiness Requirements, Section A, Chapter A6· 2.

Signed u. ......... •

Date I /~W~. CAA Approval No. DAI/1665/40 . ................................... .

NOTE: The above certification does not apply to revisions or amendments made after the date of

initial certification by other approved Organisations. Revisions or amendments made by other approved Organisations must each be separately certified, and recorded on separate record sheets.

Short Brothers Limited P.O. Box 241, Airport Road

Belfast BT3 9DZ Northern Ireland Telephone: 0232 58444 Telex: 74688 Cables: Airport Belfast

@ SHORT BROTHERS LIMITED 1982

Mar 01/13LOT, Revision 3 Page 1

zSD3-60 AIRCRAFT WIRING MANUAL

TO: Holders of SD3-60 WIRING MANUAL - SH3686, SH3690 thru SH3694, SH3698 thru SH3704 SH3706, SH3707, SH3709 thru SH3713.

1.0.0.0

2.0.0.0LETTER OF TRANSMITTALREVISION NO.3

1. Summary of Revision

CHAP. 27: FLIGHT CONTROLS

CHAP. 33: LIGHTS

NOTE: The following instructions are for hard copy holders:-

2. Revision Action

Make sure that all previous revisions have been incorporated.

27-70-00 Revised due to Service Bulletin SD360-27-23.

33-42-00 Revised due to Service Bulletin SD360-33-25.

Remove and Destroy Insert Attached New

Equipment LIsts LEP page 1/2, 3 (Apr 01/11)Equipment List Chap 27 page 1/2(Apr 15/88)

Equipment List Chap 27 page 1/2(Mar 03/10)

Equipment List Chap 33 page 5/6(Jul 01/85)

Equipment List Chap 33 page 5/6(Mar 03/10)Chapter 27 LEP page 1 (Apr 01/11)

27-70-00 page 1 (Sep 02/89) 27-70-00 page 1 (Mar 02/10)27-70-00 page 101 (Sep 01/89) 27-70-00 page 101 (Mar 01/10)

Chapter 33 LEP page 1/2, 3 (Apr 01/11)33-42-00 page 1 (Feb 06/94) 33-42-00 page 1 (Mar 08/10)33-42-00 page 101 (Feb 03/94) 33-42-00 page 101 (Mar 03/10)

BOMBARDIER AEROSPACE

3. Records

SD3-60 AIRCRAFT WIRING MANUAL

Check that the contents of the Chapters agree with the List of Effective Pages.

Retain this Letter of Transmittal.

Please acknowledge receipt of this revision.

The technical content of this document is approved under the authority of DOA No. EASA.21J.068.

Signed ------,tU~ ___ Nk~1.VL .................. .

Issued by:

Date:

Bombardier Aerospace (Shorts) Aerospace Customer Support PO Box 241 Airport Road Belfast BT3 9DZ Northern Ireland

01 March 2013

Date 1:91 · ~«cH · 2ol3 ·································································

LOT, Revision 3 Page2 Mar 01/13

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WIRING MANUAl

LIST OF EFFECTIVE PAGES

SUBJECT

INTRODUCTION Tab Divider

List of Effective Pages

CONTENTS

INTRODUCTION

LETHAL WARNING

LIST OF CHAPTERS

PAGE DATE

1 Sept 1/82

1 Sept 1/82

1 Sept 1/82

2 Sept 1/82

3 Sept 1/82

4 Sept 1/82

1 Sept 1/82

1 Sept 1/82

INTRODUCTION List of Effective Pages

Page 1 Sept 1/82

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5ih)(Q)~ 503H60

WIRING MANUAL

INTRODUCTION

TABLE OF CONTENTS

SUBJECT

INTRODUCTION

General Companion Manuals Content Method of Using the Manual Effectivity Revisions Aircraft Modifications

PAGE EFFECTIVITY

1 All

INTRODUCTION -CONTENTS Page 1

Sept 1/B2

Slh©~ SD3H60

WIRING MANUAl

INTRODUCTION

Preliminary pages following this Introduction are as follows:-1. General

LETHAL WARNING This manual has been prepared generally in accordance with tl'1e Air Transport List of Chapters Association of America, Specification No.1 00 (ATA 1 00) to Revision 21 Standard.

Revisions to this manual will be prepared to whichever revision standard of ATA100 is effective at the time, where this is practicable.

Where necessary, information is included to comply with British Civil Airworthiness Requirements.

2. Companion manuals

Other manuals produced for the SD3-60 are:-

Maintenance Manual Crew Manual Illustrated Parts Catalogue Structural Repair Manual Maintenance Programme Information Letters and Service Bulletins Weight and Balance Manual Illustrated Tool and Equipment Manual Aircraft Recovery Manual

3. Content

The purpose of this manual is to illustrate all aircraft electrical circuits in the form of wiring and (in some cases) schematic diagrams, lists and charts, which, when used in conjunction with the aircraft Maintenance Manual, enable the trouble shooting ., and servicing of the electrical circuits during maintenance. To this end, the Section/ Chapter numbering system corresponds to that of the Maintenance Manual.

A. Preliminary pages

Preliminary pages preceding this Introduction are as follows:-

Title page, which includes a Statement of Certification Record of Revisions Record of Temporary Revisions Letters of Transmittal.

4. Method of using the manual

A. Chapterization

Chapters are allocated in accordance with ATA 100 and are listed in LIST OF CHAPTERS following this introduction.

B. Page numbering

c.

Pages are numbered consecutively within each subject. Blocks of page numbers are allocated for different subjects as follows:-

Page 1 - 100 Page 101 - 200

Equipment lists

...

... ... ----.. . ..

Wiring diagrams Schematic diagrams

The equipment lists provide a means of identifying items of equipment which appear on wiring diagrams. The components are listed under the circuit breakdown number in which they are employed and each item is referenced by a number corresponding to that which appears adjacent to the item on the appropriate wiring diagram. The list also indicates the description, maker, and the number off each item used. Circuit breakers and terminal blocks are not listed.

D. Equipment identification

The various items of electrical and radio equipment are identified by a system of letters and numbers which are marked on the cables to facilitate interconnection.

The numbers and letters are allocated as follows:-

( 1) Panels

Panels are identified according to the function of the equipment thereon. Thus all fascia or control panels are identified P, contactor panels C, and

Effectivity All

I NTROOUCTION Page 1

Sept 1/B2

Sih©~ SD3H60

distribution panels D. To distinguish between panels in the same category the identification letter is prefixed by a number.

Wherever possible the numbers are chosen so that the odd numbers indicate left hand panels and even numbers right.

(2) Circuit breakers

The circuit breakers which control and protect the supplies to the various systems are mounted on the five distribution panels 1 D, 30, 30, 50 and 60 and are numbered consecutively throughout the aircraft.

(3) Terminal blocks

The terminal blocks whether panel-mounted or attached to the aircraft structure are numbered consecutively. The numbers are prefixed TB when used for general services and RTB when used for radio circuits. Terminal block identification is shown on plastic tags secured by one of the fixing bolts.

(4) Panel-mounted equipment

Each item of panel-mounted equipment (other than circuit breakers or terminal blocks) is identified by a letter, or letters depending on the number of items on the panel (see fig.1 ). The letters are applied with Dymo·tape to the panels adjacent to the equipment. Each item is identified by the panel reference follow· ed by its identification letter or letters.

(5) Isolated equipment

Each item of isolated equipment is marked by Dymo·tape with the circuit code suffixed by a number which corresponds with the item number in the equipment list for that circuit.

Where a system has more than one identical component the c1rcuit code letters for each are prefixed by a number to distinguish between the components. Where possible, these numbers are chosen so the the odd numbers indicate components on the left and even numbers components on the right. Thus two items identified 1 PA37 and 2PA37 will both be item 37 in the equipment list for the circuit having the code PA the No. 1 item being located on the left and the No. 2 on the right.

In interests of power plant interchangeability identical engine-mounted components are given the same identifications without prefix numbers.

(6) Plugs and sockets

Effectivity : All

Plugs and sockets on larger component> are identified by the manufacturer.

Isolated plugs and sockets are positioned to provide wiring breaks which facilitate installation operations and are identified to indicate their positions. The plug and socket breaks between the fuselage and the inner wings are identified FB and those between the inner and outer wings WB the suffix L or R being added to indicate a left or right position.

WIRING MANUAL

Engine firewall breaks are marked FW, those on the firewall between the engine and the wing are suffixed from 1 to 4 and 13 each side and are further suffixed Land R for left and right engines respectively. The firewall plugs and sockets within the engine are marked FW followed by a number, identical in both engines.

(7) Cable assemblies

(a) Cable identification

The relevant identification information is stamped along the length of each cable.

In general each individual cable bears all the necessary information relevant to that cable i.e. origin, circuit code and destination (refer to figure 1 as a typical cable assembly for that diagram).

A cable bearing the ident 1 P·EE·A MH MH5·1 indicates that the cable is from pin A on a unit idented EE on panel 1 P, is terminated at terminal 1 on a remotely mounted unit MH5 and is associated with a circuit bearing a code MH.

Should any ident exceed the maximum number capable of being printed on a particular cable, reduction may have been made as follows:-

1P·EE-A MH5-1

or where necessary:-

1 PEE-A MH51

In both the latter cases the circuit code is dropped as the 'MH' of remote unit MH5 designates the associated circuit.

To illustrate a much more extreme example, a cable connected to a unit idented BB, on panel 1 P, at pin j on the unit connector and routed to a radio terminal block RTB8 at terminal 9, should ideally be stamped 1 P-88-j RNA RTB8-9. This involves seventeen characters (more than the Kingsley marker system capacity).

A printed ident sleeve, bearing '1 P-BB' would be placed over all the cables from unit BB electrical connector, adjacent to the loom origin and the following printed on the cable:- j RNA RTB8-9 which reduces the number of required printed characters.

Other cables are installed in the aircraft which are unsuitable for Kingsley marking e.g. co-axial antenna feeders, and these are marked with rubber idented sleeves.

I NT ADDUCTION Page 2

Sept 1/82

(b) Segregation

Sh©~ SIDl3H60

Cables are segregated in the aircraft according to voltage/current and source of supply as follows:-

Segregation group.

A B c D E F G H J

2BV d.c., 26V. a.c. left 28V d.c., and 26V a.c. right 115V, 400 Hz left 115V, 400 Hz right Antenna feeders 200V, 3 phase, 400 Hz left 200V, 3 phase, 400 Hz right 350V, 20kHz fluorescent lighting Microphone circuits

Segregation may be readily determined by reference to the associated schematic and wiring diagrams.

(8) Cable links

Adjoining terminals on terminal blocks are 'commoned' by solid copper links. Other terminals on the same block or plug are connected together by cable links. On each cable link a yellow marker, located at the middle, carries the terminal block or plug identification as appropriate; a white marker sleeve at each end of the link carrying the terminal or pin identification.

(9) Butt connectors

Butt (in-line crimped) connectors are used throughout the aircraft for various applications e.g. to change from one type, or size, of cable to another or to connect an item of equipment with flying leads into a circuit. Those butt connectors near the ends of cables are unmarked but those more remote are numbered and prefixed BC. These markings appear on a yellow sleeve at each end of the butt connector.

E. Wiring diagrams

The wiring diagrams are in the form of routeing charts and each is numbered to agree with the corresponding system number in the maintenance manual.

The routeing chart format (fig.1) consists of vertical columns headed with the titles of main aircraft areas e.g. flight compartment, front fuselage, wings etc.. These columns are sub-divided to show the panels and portions of the aircraft on which the various items of equipment are mounted. Other columns are used to show plug/ socket and firewall breaks.

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WIRING MANUAl

FLIGHT COMPAP.TMENT

IP 2D

PllOU'INSTRUMENT PANEL RIGHT DISTRIBUTION PANEL

CONTROL UNIT . EE"

A

I GJ B I

--FUSElAGE

--fi'RZU-239 'P'RJ00-328

--

PRESSURE SWITCH

-

ORIG-IN CIRCUIT

CODE

j DESTINATION

Sih©~ SD3H60

lP-EE·A MH MH5-1 1P-EE·A MH MH5·1 ~-~------~~~~~----~~~~~----------

~

c,,.,,,.,.,_,"

~

1P·EE·A MH MH5·1 1P·EE·A MH MH5·1

1P·EE·C MH TB107.5 1 P-EE·C MH TB107·5

1P-EE·D MH TB107·6 1P-EE·D MH TB107-6

1P-EE·E MH TB129-4 1 P-EE·E MH TB129-4

1P-EE·F MH TB129-5 1P-EE-F MH TB129-5

Cable Identification Figure 2

F. Use of routeing charts

Any wire on the aircraft can be traced to its remote destination by first noting the terminal and circuit code sleeves (fig. 2), and then the destina-tion marker, which may be a few inches away. This last mentioned will identify the remote item of equipment to which the cable is connected. With this information available, it is only necessary to refer to the wiring diagram having the appropriate circuit code to determine the terminal to which the wire is connected at the remote end.

G. Schematic diagrams

These diagrams provide more detailed information in those cases where the circuits are too complicated for their operation to be obvious from their wiring diagrams.

5. Effectivity

A Contents/Aircraft Effectivity Chart is located at the beginning of each chapter, to enable the reader to establish whether the chapter is complete and has the appropriate issue of all pages. The left sides of the chart contains the Chapter Number and Title, and all the circuits of that chapter, complete with circuit code, ATA Ref, Figure and Page Number. The right side of the chart contains a number of columns, one for each aircraft of the fleet, in which the issue date of each page is quoted. The page dates relative to the first aircraft of the fleet are recorded in the leftmost column and subsequent aircraft are added, left to right, in order of aircraft delivery. Thus, when aircraft have a wiring difference, the chart shows more than one date against the particular page and the chapter contains all the pages listed.

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WIRING MANUAl

6. Revisions

Two types of revision will printed on yellow stock.

A. Normal

be issued; normal printed on white stock and temporary

Revisions will be made to this manual when necessary and manual holders will receive copies without request under the terms of agreement between Shorts and the manual holder. Each revision will contain a revised Contents/Aircraft Effectivity Chart for each chapter affected and a copy of each revised page referred to therein. Each revision will be covered by a LETTER OF TRANS-MITTAL which advises the holder what pages are to be removed and inserted. New or revised material will be indicated by a vertical line in the left hand margin, except when a section or chapter is re-issued in a completely revised form. A RECORD OF REVISIONS card is provided at the front of the Manual. As a means of avoiding a separate 'customer' revision system a revisiop affecting some aircraft only will be issued as a normal revision. In this instance a 'dummy' revision will be issued to holders whose books are unaffected and they will be asked to mark up the RECORD SHEET even though no change has been made to the content of their manual.

B. Temporary

Temporary revisions will be issued to notify operators, at the earliest opportunity, of important changes affecting safety and performance. A RECORD OF TEMP-ORARY REVISIONS card is provided at the front of the manual. The recording procedure is similar to that for normal revisions.

After the incorporation of a revision it is important for the operator to check the issue and date on each page of effected chapters against the Contents/Aircraft Effect-ivity Charts, the only documents to be used for checking the manual for correct contents.

7. Aircraft Modifications

To ensure that the information in this manual is compatible with the modification state of the aircraft, no information relating to Modifications issued after delivery of the aircraft will be incorporated retrospectively into this manual without the written assurance of the operator that he intends to embody a particular Modification. The only exceptions will be CAA Mandatory Modifications in which case the Manual will be revised according to the requirements of the Mandatory Modifications.

INTRODUCTION Page 4

Sept 1/82

Effectivity • All

LETHAL

WIRING MANUAL

ARNING

ELECTRICAL SYSTEM

1. SOME VOLTAGES USED ON THIS AIRCRAFT CAN BE DANGEROUS UNDER CERTAIN CIRCUMSTANCES. PERSONNEL SHOULD THEREFORE ENSURE THAT THE ELECTRICAL SYSTEM IS ELECTRICALLY SAFE BEFORE ANY SERVICING IS ATTEMPTED. WHERE IT IS ESSENTIAL THAT TESTS OR ADJUSTMENTS BE MADE WITH THE ELECTRICAL POWER SWITCHED ON, THE GREATEST CARE MUST BE EXERCISED.

HIGH ENERGY IGNITION UNITS

2. THE ENERGY STORED IN THE CAPACITORS OF THE HIGH ENERGY IGNITION UNITS CAN, UNDER CERTAIN CIRCUMSTANCES BE OF A LETHAL NATURE. NO SERVICING IS TO BE ATTEMPTED UNTIL AT LEAST SIX MINUTES HAVE ELAPSED FROM THE DISCONNECTION OF THE L.T. INPUT PLUG.

MICROWAVE RADIATION HAZARDS

3. THERE IS A MICROWAVE RADIATION HAZARD FROM CERTAIN EQUIPMENT IN THIS AIRCRAFT. TO AVOID INJURY TO HEALTH ALL PERSONNEL ARE TO KEEP CLEAR OF THE AREAS INDICATED WHEN WARNING NOTICES ARE DISPLAYED

REFER ALSO TO MAINTENANCE MANUAL 12-09-03

LETHAL WARNING Page 1

Seot 1/82

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Slh©@

SID3H60 WIRING

MANUAL

LIST OF CHAPTERS

INTRODUCTION EQUIPMENT LIST 21 Air Conditioning 22 Auto Flight 23 Communications 24 E Jectrical Power 25 Equipment/Furnishings 26 Fire Protection 27 Flight Controls 28 Fuel 29 Hydraulic Power 30 Ice and Rain Protection 31 Indicating/Recording Systems 32 Landing Gear 33 Lights 34 Navigation 38 Water/Waste 52 Doors 61 Propellers 73 Engine Fuel and Control 77 Engine Indicating 79 Oil 80 Starting

Yellow Tab Dividers are located at the beginning of each Chapter.

Blue Tab Dividers segregate the chapters as follows:

Airframe Systems- Chap. 21 thru Chap. 38 Structure- Chap. 52 Propeller- Chap. 61 Power Plant- Chap. 73 thru Chap. 80

LIST OF CHAPTERS Page 1

Sept 1/82

EFFECTIVITY:

1.0.0.09

CHAPTER CIRCUIT PAGE DATE

21 BASIC 1/2 FEB 14/83

3 SEP 01/82

SUPPLEMENTARY 1 ----

22 SUPPLEMENTARY 1 ----

23 BASIC 1/2 FEB 15/87

3 FEB 20/86

SUPPLEMENTARY 1/2 ----

3 ----

24 BASIC 1/2 FEB 14/83

3 JUN 30/86


25 BASIC 1 AUG 21/84


26 BASIC 1 FEB 15/87

27 BASIC 1 MAR 03/10

28 BASIC 1/2 JUL 12/83

3/4 SEP 01/82

5 OCT 08/85

29 BASIC 1 DEC 14/85

30 BASIC 1/2 SEP 10/83

3/4 OCT 09/85

5 JUL 12/83


31 BASIC 1 JUL 24/85


32 BASIC 1 NOV 02/84

33 BASIC 1/2 MAR 19/86

3/4 AUG 02/92

5/6 MAR 03/10

7 SEP 26/86


EQUIPMENT LISTS - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 1/2Apr 01/11

EFFECTIVITY:

34 BASIC 1/2 FEB 20/86

3/4 SEP 16/85

5/6 DEC 01/83

7 SEP 16/85

SUPPLEMENTARY 1/2 FEB 15/87

3 ----

38 BASIC 1 SEP 01/82


61 BASIC 1 OCT 13/87



77 BASIC 1 OCT 08/85



CHAPTER CIRCUIT PAGE DATE

EQUIPMENT LISTS - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 3Apr 01/11

EFFECTIVITY:

CIRCUIT CODE CH-SE-SU FIG PAGE DATE

AIR CONDITIONING HE 21-01-00 1 1/2 APR 05/89

3 APR 05/89

101 101 APR 05/89

GASPER BOOST AIR VALVES & FANS HM 21-02-00 1 1 APR 02/89

101 101 APR 01/89

MAIN FANS AND RAM AIR HR 21-03-00 1 1 APR 03/89

101 101 APR 02/89

RECIRCULATING FANS AND GROUND AIR INTAKE

HS 21-04-00 1 1 APR 04/89

101 101 APR 02/89

FLIGT DECK TEMPERATURE CONTROL HV 21-05-00 1 1 APR 03/89

101 101 APR 01/89

1ST AND 2ND PILOT'S FANS HL 21-51-00 1 1 APR 01/89

PASSENGER COMPARTMENT TEMPERATURE CONTROL

HU 21-61-00 1 1/2 APR 03/89

PASSENGER COMPARTMENT TEMPERATURE INDICATION

DE 2 3 ----

PASSENGER COMPARTMENT TEMPERATURE CONTROL

HU 101 101/2 APR 01/89

PASSENGER COMPARTMENT TEMPERATURE INDICATION

DE 102 103 ----

CHAPTER 21 - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 1Jun 01/97

EFFECTIVITY:

AUTOMATIC FLIGHT CONTROL SYSTEM (A.F.C.S.)

CA 22-12-00 1 1/2 ----

3/4 ----

5/6 ----

7/8 ----

9/10 ----

11/12 ----

13/14 ----

15/16 ----

17/18 ----

19/20 ----

21/22 ----

23/24 ----

25/26 ----

27/28 ----

A.F.C.S. DISENGAGE TONE WARNING CC 2 29/30 ----

ALTITUDE ALERTER SE 3 31 ----

ALTITUDE ALERTER SE 3 31/32 ----

ELECTRONIC HORIZONTAL SITUATION INDICATOR

FJ 4 33/34 ----

35/36 ----

37/38 ----

39 ----



EFFECTIVITY:

NO 1 VHF COMMUNICATION RV 23-11-00 1 1/2 FEB 03/94

NO 2 VHF COMMUNICATION 2 3 FEB 05/94

DUAL HF SYSTEM RC 23-14-00 1 1/2 ----

3/4 ----

5 ----

HF SYSTEM RC 23-14-00 1 1/2 ----

3 FEB 02/94

PASENGER ADDRESS SYSTEM RL 23-31-00 1 1/2 ----

3 ----

101 101 ----

PASSENGER ADDRESS AND TAPE PLAYER SYSTEM

RL 23-31-00 1 1 FEB 02/94

TAPE PLAYER RW 23-32-00 1 1 ----

101 101 ----

AUDIO SYSTEM RZ 23-51-00 1 1/2 FEB 16/94

3/4 FEB 12/94

5/6 FEB 01/94

7 FEB 01/94

7/8 ----

9 ----

101 101/2 FEB 03/94

103 FEB 04/94

103/4 ----

105 ----

VOICE RECORDER MF 23-71-00 1 1 FEB 04/94



EFFECTIVITY:

AC POWER SUPPLIES XA 24-21-00 1 1/2 JUN 30/87

3 JUN 30/87

101 101 NOV 11/86

DC POWER SUPPLIES-GENERATION PA 24-31-00 1 1/2 FEB 10/85

3/4 FEB 20/86

5 FEB 20/86

101 101 FEB 23/84

DC POWER SUPPLIES-DISTRIBUTION PA 24-32-00 1 1/2 FEB 14/83

3/4 JUN 30/86

5 ----

5/6 FEB 15/87

7 FEB 15/87

DC POWER SUPPLIES - (DISTRIBUTION AND ENGINE STARTING)

101 JUN 05/87

DC DISTRIBUTION PB 24-51-00 1 1/2 MAR 15/91

3 MAR 13/91



EFFECTIVITY:

DOMESTIC SERVICES HU 25-31-00 1 1 SEP 05/89

101 101 SEP 01/89

EMERGENCY LOCATOR TRANSMITTER WR 25-60-00 1 1 SEP 05/89



Sihlo«bi> WIRING SD3o60 MANUAL

EFFECTIVITY:

ENGINE FIRE WARNING WE 26-11-00 1 1 ----

1/2 SEP 04/89

3 MAR 15/91

101 101 SEP 03/89

BAGGAGE BAY SMOKE DETECTION WE 26-12-00 1 1 SEP 06/89

101 101 SEP 02/89

LAVATORY SMOKE DETECTION WE 26-13-00 1 1 SEP 02/89

101 101 SEP 01/89

ENGINE FIRE EXTINGUISHERS WC 26-21-00 1 1 SEP 02/89

101 101 SEP 02/89



EFFECTIVITY:

STALL WARNING WH 27-33-00 1 1/2 SEP 05/89

3 SEP 05/89

101 101 SEP 03/89

FLAP ACUMULATOR SOLONOID VALVE GE 27-51-00 1 1 SEP 02/89

FLAP POSITION INDICATORS DE 27-52-00 1 1 SEP 02/89

101 101 SEP 01/89

CONTROLS LOCKED WARNING WM 27-70-00 1 1 MAR 02/10

101 101 MAR 01/10


CHAPTER 27 - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 1Apr 01/11

EFFECTIVITY:

FUEL LEVELING VALVES & LOW LEVEL WARNING

QF 28-21-00 1 1 SEP 02/89

101 101 SEP 01/89

FUEL BOOSTER PUMPS QA 28-22-00 1 1 SEP 02/89

LOW FUEL & OIL PRESSURE WARNING SYSTEM

WD 28-41-00 1 1 SEP 03/89

101 101 SEP 02/89

FUEL CONTENTS GUAGES QB 28-42-00 1 1 SEP 02/89

FUEL FILTER BLOCKING WN 28-44-00 1 1 SEP 02/89

101 101 SEP 01/89

FUEL CROSSFEED SELECTED INDICATION WU 28-46-00 1 1 SEP 02/89

101 101 SEP 01/89

LOW FUEL LEVEL INDICATION WY 28-47-00 1 1 SEP 01/89

101 101 SEP 01/89



EFFECTIVITY:

HYDRAULIC CONTROL GA 29-11-00 1 1 SEP 02/89

101 101 SEP 01/89

LOW HYDRAULIC PRESSURE WARNING WP 29-31-00 1 1 SEP 02/89

HYDRAULIC FLUID CONTENTS GE 29-32-00 1 1 SEP 03/89

HYDRAULIC OVERHEAT WARNING WT 29-33-00 1 1 SEP 02/89

101 101 SEP 01/89

PUMP TEMPERATURE INDICATION GE 29-34-00 1 1 SEP 02/89

EMERGENCY PRESSURE INDICATION GH 29-35-00 1 1 SEP 02/89



EFFECTIVITY:

PNEUMATIC DE- ICING HK 30-11-00 1 1/2 JAN 05/92

3 JAN 04/92

101 101 JAN 04/92

EJECTOR VALVE HEATER MUFFS HP 30-12-00 1 1 JAN 03/92

101 101 JAN 01/92

ENGINE AIR INTAKE ANTI-ICING HC 30-21-00 1 1 JAN 02/92

101 101 JAN 01/92

INTAKE INERTIA ANTI-ICING ACTUATORS HD 30-22-00 1 1 JAN 03/92

101 101 JAN 02/92

PITOT & STATIC VENT HEATERS FE 30-31-00 1 1 JAN 03/92

101 101 JAN 02/92

WINDSHIELD HEATERS HH 30-41-00 1 1 JAN 05/92

101 101 JAN 04/92

WINDSHIELD WIPERS MA 30-42-00 1 1 JAN 03/92

101 101 JAN 01/92

RAIN REPELLENT SYSTEM MU 30-43-00 1 1 JAN 02/92

101 101 JAN 01/92

FIVE BLADE PROPELLER DE-ICING HA 30-61-00 1 1 JAN 03/92

101 101 JAN 02/92

SIX BLADE PROPELLER DE-ICING HA 30-62-00 1 1/2 ----

3 ----

101 101 ----

ICE DETECTOR WS 30-81-00 1 1 JAN 03/92

101 101 JAN 02/92



EFFECTIVITY:

FLIGHT DATA RECORDER ME 31-31-00 1 1 JUN 26/85

CENTRAL WARNING SYSTEM WL 31-50-00 1 1/2 OCT 08/85

3/4 JUN 30/86

5 JUN 30/85

101 101/2 JUN 30/85

103/4 SEP 01/82

105/6 SEP 01/82

107 JUN 24/85



EFFECTIVITY:

LANDING GEAR CONTROL & INDICATION CC 32-30-00 1 1/2 SEP 10/85

3 MAR 19/86

101 101 FEB 15/87

NOSEWHEEL STEERING GD 32-50-00 1 1 JUN 26/85

101 101 SEP 01/82



EFFECTIVITY:

ROOF PANEL & STANDBY COMPASS LIGHTING LG 33-12-00 1 1 FEB 02/94

MAIN INSTRUMENT PANEL LIGHTING LJ 33-13-00 1 1 ----

1/2 FEB 09/94

3 ----

3/4 FEB 01/94

5 FEB 03/94

101 101 FEB 03/94

SIDE PANEL & CONSOLE LIGHTING LK 33-14-00 1 1 FEB 02/94

101 101 FEB 01/94

FLIGT COMPARTMENT UTILITY LIGHTING LL 33-15-00 1 1 FEB 01/94

CENTRE CONSOLE LIGHTING LJ 33-16-00 1 1 FEB 02/94

101 101 FEB 01/94

PILOTS SPEED/POWER MEMORY BOARD LIGHTING

LU 33-18-00 1 1 FEB 01/94

1ST AND 2ND PILOTS MAP LIGHTS LZ 33-19-00 1 1 FEB 01/94

PASSENGER COMPARTMENT LIGHTING LB 33-21-00 1 1 FEB 02/94

101 101 FEB 01/94

READING & EMERGENCY LIGHTING LM 33-22-00 1 1/2 FEB 05/94

3/4 FEB 02/94

5 FEB 03/94

101 101/2 FEB 03/94

103 FEB 01/94

BREIFING SIGNS & CALL SYSTEMS WK 33-23-00 1 1 FEB 06/94

101 101 FEB 03/94

BAGGAGE COMPARTMENT LIGHTING LN 33-31-00 1 1 FEB 02/94

LANDING & TAXI LIGHTS LC 33-41-00 1 1 FEB 03/94

101 101 FEB 02/94

NAVIGATION AND STROBE LIGHTING LD 33-42-00 1 1 MAR 08/10

101 101 MAR 03/10


CHAPTER 33 - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 1/2Apr 01/11

EFFECTIVITY:

ANTI -COLLISION LIGHTS LE 33-43-00 1 1 FEB 02/94

101 FEB 01/94

ICE SPOTLIGHTS LA 33-44-00 1 1 FEB 03/94

LOGOGRAM ILLUMINATION LR 33-45-00 1 1 ----

FLIGHT COMPARTMENT EMERGENCY LIGHTING

LP 33-51-00 1 1 FEB 02/94

101 101 FEB 01/94

FLOOR PROXIMITY ESCAPE PATH LIGHTING LMA 33-52-00 1 1 FEB 02/94

101 101 FEB 01/94


CHAPTER 33 - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 3Apr 01/11

EFFECTIVITY:

AVIONICS COOLING MN 34-01-00 1 1 ----

101 101 ----

SENSITIVE AVIONIC SUPPLIES PBA 34-02-00 1 1/2 ----

3 ----

101 101 ----

ENCODING ALTIMETERS SC 34-12-00 1 1 FEB 10/85

HIGH SPEED WARNING WU 34-14-00 1 1 FEB 10/85

101 101 SEP 01/82

OUTSIDE AIR THERMOMETER DC 34-15-00 1 1 JUN 26/85

101 101 SEP 01/82

GYRO COMPASS FC 34-21-00 1 1/2 FEB 20/86

3 FEB 20/86

FLIGHT DIRECTOR FD 34-23-00 1 1/2 JUN 26/85

3/4 SEP 26/85

5/6 JUN 26/85

7 JUN 26/85

7/8 ----

ELECTRONIC HORIZONTAL SITUATION INDICATOR

FJ 34-23-00 2 9/10 ----

11/12 ----

13/14 ----

15 ----

STANDBY ATTITUDE GYRO, 1ST PILOT FE 34-24-00 1 1/2 FEB 20/86

STANDBY ATTITUDE GYRO, 2ND PILOT FE 2 3 FEB 10/85

VOR/ILS/MARKER BEACON SYSTEM RNA 34-31-00 1 1/2 SEP 01/82

3/4 JUN 30/86

5/6 FEB 10/85

7/8 JUN 30/86

9/10 FEB 10/85

11 FEB 15/87

WEATHER RADAR SB 34-41-00 1 1 NOV 11/86


CHAPTER 34 - CONTENTS/AIRCRAFT EFFECTIVITY CHARTSH3709 Page 1/2Jun 01/97

EFFECTIVITY:

GROUND PROXIMITY WARNING SYSTEM (GPWS)

RY 34-42-00 1 1 FEB 10/85

RADAR ALTIMETER SD 34-43-00 1 1 FEB 10/85

ALTITUDE ALERTER SE 34-44-00 1 1 JUN 30/86

NO 1 ADF SYSTEM RD 34-51-00 1 1/2 FEB 10/85

NO 2 ADF SYSTEM 2 3 ----

DME SYSTEM (WITH HOLD FACILITY) RB 34-52-00 1 1/2 JUN 10/85

DME SYSTEM (WITH HOLD FACILITY) 2 3 JUN 10/85

TWIN TRANSPONDER SYSTEM SA 34-53-00 1 1 JUN 26/85

E.H.S.I. (REF ONLY) FJ 34-61-00 1 1 ----



EFFECTIVITY:

WATER CLOSET PUMP HJ 38-31-00 1 1 MAR 31/84

101 101 SEP 01/82




EFFECTIVITY:

DOORS OPEN WARNING WA 52-71-00 1 1 MAY 06/89

101 101 MAY 04/89




EFFECTIVITY:

PITCH INDICATION & LBA SECONDARY STOP KD 61-21-00 1 1/2 MAY 05/89

3 MAY 05/89

101 101 MAY 04/89

AUTOFEATHER SYSTEM KC 61-22-00 1 1 MAY 05/89

101 101 MAY 04/89

PROPELLER OVERSPEED GOVERNOR TEST KB 61-23-00 1 1 MAY 05/89

PROPELLER SYNCRONIZATION KG 61-24-00 1 1 MAY 05/89

PROPELLER SYNCHROPHASING KF 61-25-00 1 1 ----

PROPELLER SPEED INDICATORS EF 61-41-00 1 1 MAY 05/89

101 101 MAY 04/89



EFFECTIVITY:

ENGINE FUEL BLOW DOWN KE 73-11-00 1 1 MAY 06/89

FUEL FLOWMETER INDICATORS QC 73-31-00 1 1 MAY 05/89




EFFECTIVITY:

RESERVE POWER SYSTEM QJ 76-13-00 1 1 MAY 05/89

101 101 MAY 05/89




EFFECTIVITY:

ENGINE TORQUE INDICATORS EB 77-11-00 1 1 MAY 05/89

GAS GENERATOR SPEED INDICATORS EG 77-12-00 1 1 MAY 05/89

101 101 MAY 04/89

INTER TURBINE TEMPERATURE INDICATORS ED 77-21-00 1 1 MAY 06/89

101 101 MAY 05/89



EFFECTIVITY:

OIL TEMPERATURE / PRESSURE INDICATORS EA 79-31-00 1 1 MAY 06/89

101 101 MAY 04/89




EFFECTIVITY:

ENGINE STARTING HA 80-10-00 1 1/2 FEB 15/87

3 FEB 15/87

101 101 SEP 01/82




EFFECTIVITY:

JUNCTION BOX JB1 - 91-10-00 1 1/2 SEP 10/85

3/4 NOV 11/86

5/6 NOV 11/86

7/8 NOV 11/86

9 NOV 11/86




DIAGRAM No.

FIGURE No.

SB & H Drg. No.

CIRCUIT CODE ITEM No. PART No.

AIRLINE STK No. DESCRIPTION VENDOR No. OFF

27-33 1 6132/E WH 23467

111213141617181920212224252627293031

MK 9WH10-3R9MR5-22KRL9809/G16F40796-202100-2CM-356Q-50-BB99-6304TP12-314-1046B3-00422TP12-7HDS14WH25-22R (±5%)W21-1KRTIL-1026B3017050CV7046 (or ZS106)MK5-2K7BZV-85-C22 (alternative BZX-61-C22)2N4400

Stick shakerResistorResistorRelayDiodeStall detectorHorn, model ‘S’FilamentRelay - current sensorIndicatorSwitchFilamentCap (Static/Stall)SwitchRelayResistor (25W, 22 Ohm)ResistorOpto isolatorCap (low/high)DiodeResistorZener diodeTransistor

AUECWelwynWelwynAAIRSafe FlightSafe FlightSafe FlightHartmanAerospace OpticsHoneywellAerospace OpticsAerospace OpticsHoneywellHellerman DeutschWelwynWelwynTexas InstrumentsAerospace OpticsFerrantiWelwynMullardMotorola

22484211242

1622242228222

27-51 1 6041/Aa GE 13

99211SE1-3/JE17

Solenoid valveMicroswitch

HTEHoneywell

11

27-52 1 6071/C DB 234

124210-250647/350647/4

IndicatorTransmitterTransmitter

KratosKratosKratos

111

27-70 1 6082/D and SB-SD360-27-16 andSB-SD360-27-23

WM 2345689

101112

DT-2RV212-A7S046001/C1SE1-3/JE17L10-706F/4014-1046H3-001899-630TDD-AYOG-1002RSE116661

Microswitch (2 pole)Solenoid (29V DC CONT)MicroswitchLinear actuatorDiodeFilament (type 6 28V, .024A)CaptionIndicator BodyTime delay relayRelay base

HoneywellLucasHoneywellPlesseyIRAerospace OpticsAerospace OpticsAerospace OpticsStruthers DunnStruthers Dunn

1211341111

Mar 03/10

EQUIPMENT LIST (BASIC) - CHAPTER 27Page 1/2

DIAGRAM No.

FIGURE No.

SB & H Drg. No.

CIRCUIT CODE ITEM No. PART No.

AIRLINE STK No. DESCRIPTION VENDOR No. OFF

33-23 1 6084/Aa WK 3

56789

1011121314151617

G80014SD3-18-64401PB5-T1TL1-31TP12-780/10/006480/10/1048 (clear)80/10/1048 (orange)80/10/064402/18416F/40RL9809/G1995/9182

Illuminated sign - LAVATORY(supplied with galley)Push/pull switchIlluminated sign (cabin)Push buttonSwitchSwitchLamp bodyCap (clear)Cap (orange)Earth tagLamp baseDiodeRelayFilament

Pepco Inc.Short Brothers LtdHoneywellHoneywellHoneywellThornThornThornThornThornI.R.A.A.Thorn

1

2413212312211

28

33-31 1 6057/B LN 345

30180B-23D16831TL1-3

LightFilament (white lens)Switch

GrimesG.E. (Netronic)Honeywell

442

33-41 1 6054/E LC 12389

1011

B-4150B1TP12-3Q4681GE4626101CC01AZS1062TP12-3

Taxi light housingSwitchLanding lightSealed beam unit (28V-150W)ContactorDiodeSwitch D.P.

GrimesHoneywellGrimesGen. E. (Aviquipo)E.C.E.E.C.E.Honeywell

1321221

33-42 1 6055/E andSB-SD360-33-25

LD 345667788

1TB12-330-0863-430-0863-330-0516-1 (Pre SB 33-25)30-1192-13 (Post SB 33-25)678 (Pre SB 33-25)692 (Post SB 33-25)60-3146-3 (Pre SB 33-25)60-2799-9 (Post SB 33-25)

SwitchLight assembly, right (green)Light assembly, left (red)Tail nav./Strobe assembly (white)Tail nav./Strobe assembly (white)LampLampPower unitPower unit

HoneywellGrimesGrimesGrimesGrimesGrimesGrimesGrimesGrimes

211113333

33-43 1 6056/Bb LE 56

1TP12-330-1033-5 (red lens)

SwitchRotating beacon

HoneywellGrimes

11

33-44 1 6018/A LA 134

1TL1-3H29025L588

SwitchLight assemblyFilament

HoneywellLucasRival Lamps

111

Mar 03/10

EQUIPMENT LIST (BASIC) - CHAPTER 33Page 5/6

~~ I

I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

9P AIR OOND

+

Q'o'ER ;;;_SSURE SYSTEM

+

DUCT l~ PRESSURE S)SfEM

'MRiliiiG LIGIHS

.,.

+

OVERHEAT PASSCOMP

+

, I 1

' r

' I I ' r '

'

r r '

r

EOMPARTHENT

. ' I I ' '

G

I I

WIRING MANUAL

' SHEET2

-IFF-Pi]

I I

I I I I I I I I I I I

,/ I

i I

L_____j + ,___,r---j I I "-~'---' )-- - - - --o ~I -=---{i{i})- -l: - --o /

I I I

IIHEI21 SPAR BO.X THERMOSTA.l LEFT

RIGHT WING

LEFT DUCT PRESSURE S'HITCH

WING BOX EOU•Pl AFTCFFIREWAll

" " I I I ' ' '

SPAR BOX THERMOSTAT RIGHT

j2HE12j

I I I I I I

I : I lmml

~-·~-~------------~1 ___ ¢ I I I I I I I I I I

' ' ' I I I I I I I I

RIGHT DUCT PRESSURE SWJTCH

I~ ~ 11 1_ lA'>'l-'ARKED CABLES A"RE KTCL SIZE 2~ fi:\ ® : I 2_ CABLESSHO'HNTHUS---ARE SUPPUEDWI1H EOUIPMEIIT ~RESERVE POWERSYSTEMI76-13·00lFIG1 F CENTRAL WARNING S~STEM (3J-SO-OC.) FIG. I I I I I

3 CABlES SfUNN THJS-·-AAE REF. ONLY ® PNEUYATIC DE!CING (30-11-00JFIG 1 ® I II I

I I I

.-._ CABLES MARI(ED EFG AftE EFGLASS

11

s SEGREG\rroN © FLIGHT co~P TEMP coNrROL(21-os-OOlFIG.I ®GASPER soosr AIR VALvEs &. FANs (21-oz- vo1, no 1 11

.. ,~~· n ~liM~-------==-. GROuP A 28'1 0 ClEFT @ W r rr Jl GROUPS 26'1 OC.RIGifT Q PASS (1)!.-t?_ TEt.IPCOIHROL !21·61·00lFIG1 Q) MAIN fAN & RAM AIR CONTROL {2!-03-00), FIG I

L_ _______ li~--------~=:=:=:=:=:=:=:=:=:=:=:=:=:=:=:([)~E~~tu~w~c;"'~';';";';'R~';''~"~"~'~·';''~·;"~·o;'~''~'u;'=:=:=:=:=:=:=:=:=:=:=:=:=:=:=:=:=:~ __ l: ______________________ _l~H~E~~~~j~i(il~ ll.ltiibCNif0'R~I,~J~Ul1jF\~ ~~~-----162, A66- A116, A119, A 121 - A125, A129- A 131,A133,A134, A 137- A 148,A151-A155 A UP 21-01-00

Pa;Je 1/2

Apr 5/89

28 V D.C. LEFT SHEDDING BUS BAR 2

)l SA I ~> 3 FLIGHT DECK CENTRAL WARNING SYSTEM ili 90

TEMPERATURE CONTROIL-~----1 (31-50-00), FIG 101 (21-0S-00), FIG 101 /;-~-"~-~\

PRESS URE SWITCH 'HE I' i-® r---~1 I B : ih .,..: INDICATOR: ,

WIRING MANUAL

~---~---..----------~9P----------,--------~~~LI~G~~~~~~~H~========~~==========2~C==========~===============~FUS~El~==============~ RIGHT IN PANEL AIR CONDITIONING PANEL FRAME 7' RIGHT EQUIPMENT BAY PANEL 89- 146 LEFT

I I GASPER BOOST - r- I I2C liC-PJI I2C -Pi VALVES AND • • I -P ,19P· II I \ I = I FAN SWITCH ffi I I I I t.!.!J;:I =-DI....,DD::-E-,S 'AS' I

I 0 @fu~~--0JTJJ0--!_ ________ _:I__ _____ ~ s s 1---+-.:;.! ~l~ ~E,J.~A ~b~ IC I I r- I E209 STATION 89-146 RIGHT 1101 ~lsi I

I 101 ~ !1 !11---__:.l ______ ____:_l ---+-----'---Hf-------l 1

1 ,. 20 (!__ ? (n (,~"

I f--1! • 1--_.!_ ________ _:__ __ -+--'-----t-+--------' ~ r J TJ

I 10 : I L__~l--++----+. --+___!,___!!14'---1~ ' " v 10WL1

~-tm~m~-~---------------j~29~ r.;, I '- I • I I --® t.!!.J 'AU' :----1 ~ I ..... I I I I 4~~0UI .@::~--1 y y 1---.:..._1 ...::;E2:,:::08:___ ______ ---I B

I RIGHT OPTIC ,. . I I I @) 'AV' DIODES I INDICATOR I i\?c): ,.--10.,..:19~1-,sl 'AL' . I I -'~ ~T---i_~a ~gt---T--------------1 A

I I~ I BC442 I I I I I ~~ ~y y~~~--------~~----~,:.___ _________ ~1-----------------~D I -- I f-----1 :l :l f----1:------------:-1 ____ :._____ _______ ~-------~~

E

LEFT GASPER BOOST VALVE

RIGHT GASPER BOOST VALVE

I 10)..!--_J I I UNMARKED CABLES ARE KTCL-1-24 ""' f8\ CABLES MARKED WITH Nos ARE loiiNYVIN SIZES

I I= I I 10WL1 .).!:!.) SEGREGATION'- GROUP '8 28V. D.C. RIGHT ® PASSENGER COMPARTMENT TEMPERATURE CONTROL ( 21 - 61 - 00 ),FIG.1 I I (e) I ~..____, p p 1---_:_ ____________ ---i 33 l.-' / ® MAIN FAN & RAM AIR CONTROL I (21-03-00~ FIG I I I I @CENTRAL WARNING SYSTEiol (31-50-001 FIG.I (21 .-------;-~:-;-;-;-------i I I I © LANDING GEAR CONTROL (32- 30-001 FIG.1 .1 AND INDICATION =i"': ·

I @ AIR CONDITIONING CONTROL (21-D1-DOI,FIG.1 lu .. IF-j!G 1 .,.... ' .. ':=.'~- BOU';..: •• ,~ & INDICATION ln1' 11 1 All" .vc: AN[ rAN:::l LA62-.A6-6U-P~----------~L---------~----~~--~~--------~--~~~21-02-00

Page 1

Apr 2/89

CENTRAL WARNING SYSTEM (31-50-00),FIG.lOI

ALL A/C

VIEW OF

INDICATOR SCREEN

WIRING MANUAL

,. ________________________ 28jj,Vi. D.C. GROUND SERVICES B;;,U;;SB·A·R------------------------~

LEFT OPTIC INDICATOR

,------~

I I I I

I I d L------·

DIODES

L...T--T---T---'i-1-' , I

I

I

I. I SHUT I

OPEN

I I I I

I

I I 1 I L-------- ----- _J

LEFT GASPER BOOST VALVE

209 SA 211 SA 210 '=-J

ISA AIR CONDITIONING CONTROL & INDICATION r---

9P AIR CONDITIONING

SWITCH 'H'

'-0 0 I , 5

~· I • :.J I

INDICATOR G' BC 760

@ 7

r!- (4)1 .!.. :=:t BC762

~I 3

I BC 764 A

(a)__l ~

1\62,1'66-UP

FLIGHT COMPARTMENT

RIGHT 2C RIGHT

PANEL EQUIPMENT BAY EQUIPMENT PANEL

I I I I RElAY 0 I lrB44 I

'H'

Q)l lcp 0 I l>c- P41 •

I I _l

I I _G) 0, E E

I I I

WIRING MANUAL

20 R I GH 1

DISTRIBUTION PANEL

I 212 I 60 28V D.C. 12 2 1 GROUND SERVICES

BUSBAR RIGHT 2C-S41 25A

I

I 12 I I I JOC·SII

30 c

WEIGHT

FUSELAGE FUSELAGE FAIRING

FORWARD FAIRING

PLUG BREAK FRAME 74-148

I I

I I I FF-P2 '

IFF -52 I I I FAN I I 12 ,

A A A

I I B ( '-® I I I ~o I I llOC-PII SWITCH RELAY I 12 , o· I~ I I I ~ _l_ I I•P-P I 9P-SI I

I I • • I I I I I ~ I I I I .1'2) 0< 2BV D.C. T T 2 I GROUND 5Ef;l:VICES I I I 5A BUSBAR RIGHT •

0 I I EXD B I I I I

EE EE BB BB I I I I FF FF I I I I

GG GG

I I I I p p I I I I I I I I I I I I

I I I I pp pp

I I I I I

10 Wll

I 0 I I q q 25 I I I I I I I I I I

NOTES

All UNMARKED CABLES ARE KTCL-1-24 @ GASPER BOOST AIR VALVES & FANS I 21..()2-00 ),FIG. I CABLES WITH Nos. ONLY SHOWN ARE MINYVIN SIZE

SEGREGATION:· GROUP '8 28V O.C.RIGHT ® AIR CONDITIONING.CONTAOL & INDICATION- ( 21-01 -00 I,FIG.1 @ CENTRAL WARNING SYSTEM 131-50-00) Fl G.1 ® PASSENGER COMP! TEMP CONTROL (21-61-00) F /G. 1 © LANDING GEAR CONTROL & INDICATION ( 32·30-QO ),FIG.1

r.,, 1 I I I I 0 I@ I : E3 I I L- - J I

I IFF-PI IFF-SI

I ~

p p

I N N

I f f -

I I I I

R R

I I I I I I I

FIG. HR 1

I I I I I I RAM AIR VALVE ~ I I I A I I

B

D

I ~o I < ,_ c ~

I I I I

E

I I I I I I

I I I

WI R lNG DIAGRAM S03-06-6029, ISSUE'c'

MAIN RAM AIR

FAN & CONTROL

21-03-00 Page 1

Apr 3/89

A62,A66-UP

212

28V. D.C. GROUND SERVICES BUSBAR-RIGHT

25A

GASPER BOOST AIR VALVES & FANS

(21-02-00) FIG 101

211

AIR CONDITIONING CONTROL---------~ & INDICATION ( 21-0HlO J. FIG.IOI

WIRING MANUAL

PASSENGER COMPARTMENT TEMPERATURE CONTROL (21-61-00), FIG 10 I

RAM AIR VALVE

' ----MAIN FAN I A SWITCH r-------------------~:~-~--~0

r---~~ON IB I ~~-~~--------~------------~·~~---

L--'- t )RAM ·•ilf---

WIRING MANUAL

FUSELAGE

9p 30( RIGHT RIGHT 2 ( DISTRIBUTION PANEL EQUIPMENT

FLIGHT COMPARTMENT 20 FORWARD FAIRING

PLUG BREAK FRAMES 7li-180

I I I I

112, · .1l----'1~ k k 1-----<

I I I I I I

A62,A66-A 160

T

714 I F F r-1~· ... I~ I I !A ~~~ '-GJI.ill::i- H H I K K

BC 778

I : j/ I I

r; ~NOTES f3"P-Pi ALL UNMARKED CABLES ARE KTCL-1-2l. ~ CABLES WITH Nos ONLY SHOWN ARE MINYVIN SIZE

19P-S1 SEGREGATION:- GROUP 'a' 28V D.C. RIGHT

0 CENTRAL WARNING SYSTEM (31-50-00) FIG l (2)

I I

I I I

I I

I I

I I

I I I I I

I

E 218

I -

I 1----'----1 --Jel

I

i 9HBC I

I ~~--~-c..· _...J

FAN

IHSBI

GROUND AIR INTAKE VALVE

j!HsJI

RE-CIRCULATION AIR INTAKE VALVE

12HS31

:i(~v.J,.-1 I 11 1~ ~-~w:.,.,1 1=Ricc-NG~oo-:l A"""G;o-RA;:-;-M,------------1

I 503-06-6019. ISSUE ' ' I HS FjG. §~o~~8U~~TII~fA~~-D

21-04-00 Page 1

Apr 4/89

A33-A160

WIRING MANUAL

'1----- 28 V D.C. GROUND SERVICES BUSBAR \

ril 208 ~ ~ SA

\'f

,---- 1- --[

2 5 [RECIRCULATION

(_A 207 ~SA

"' I ... ---- I SWITCH GNO -·AlA - OFF """

__::.:.:.::.__:.:.::.__~- : 3 ' flooy .., 4 • J •.

INDICATOR 'c •

-t-

r;-;12 -- 3' 4 1 I I I A I I I I '.::/ I I I I ~ l• -

WIRING MANUAL

FLIGHT COMPARTMENT

9P lC STATION 5-54 FRAME 74

AIR CONDITIONING PANEL LEFT EQUIPNENT PANEL

FLIGHT COMPARTMENT I I I TEMPERATURE CONTROLLER I I I I HV 6 I I I I

I I I I I I I I I

F

I I I G

I i I FLIGHT COMPARTNENT I I AUTO I MANUAL SWITCH IC -52 I I ..... / IC -P2 I -0 I K ~ T~l I FLIGHT COMPARTMENT I I E2 H I

TEMPERATURE SENSOR I 2 N N n n ,,

]lit•· [!] (1\1 I I I HV3 I I J I I I

I I D A I ® I ' I I ' E

I B

I Fl...IGHT I

I 'L' COMPARTMENT I I SELECTOR I I I '-0 I A

I I I I

I I • I c I I m ~ I I I I I I ' ' I I I I I I loiAHUAL I I I 'N' CCNTROL I I SYrTTCH , I

rPl '

I I I I I [!) I I I

L 1 p p

I I I I I ... I 2..

J J

I I I .JI 7 B

19P-~2~ I I 19~-521 I I I I I I I I

I NOTES

I 1 ALL UNMARKED CABLES ARE KTCL-1-24 2 SEGREGATION - GROUP A 28 V DC LEFT I 3. CABLES SHOWN THUS--- ARE REF. ONLY

I ® AIR CONDITIONING CONTROL ANn ltDCATION {21-01-00)FIG.I I I I I

A62.A66-UP

I I I I I I I I I I I

I I I I

I I I I I I I I I I I I I

FUSELAGE

1D FORWARD FAIRING FRAf.E 7.4-122

LEFT DISTRIBUTION PANEL PLUG BREAK

I I FLIGHT COMPARTMENT I I DUCT TEMPERATURE SENSOR I HV2 I

FF- 51 FF- PI

I I \ ..1.. I I L L A I I

K K B I I I I

1 I I I • ' '2 7) I I / 5A '-'--I I 28V D.C. SHEDDING BUSBAR LEFT I • • I I A I I I I • • I

I I I I I • 0 I I I I I I FLIGHT COMPARTMENT AClUATOR I ' 0 I I HV5 I I

I I I I

d d B

I I • • A I I

p 1!. D I I E•9

•Ill r I I c I I E I I I I I I I I I I I

WIRING DIAGRAM 503- oe;- 6064 ISSUE 'C~'

FIG. FLIGHT COMPARTMENT HV 1 TEMPERATURE CONTRO_!:

21-05-00 Page 1

Apr 3/89

ALL A/C

'

WIRING MANUAL

28VO.C. SHEDDING BUS BAR LEFT

(). SA }1 90 ®'

I

FLIGHT COMPARTMENT AIR CONDITIONING CONTROL &

INDICATION ( 21 · 01 • 00 ),FIG.l

AUTO I MANUAL SWITCH r ~;I I, 'I I

MANUAL 1'-of r\oJ..:I_c:A.:_UT-'-0_:_ _______ _ ~...-__ ~...J

MANUAL CONTROL

SWITCH

HOT

r- -,--, I ) I 13 d Li> __ ~ ...J COOL

,---1

l L

K

FLIGHT COMPARTMENT

TEMPERATURE CONTROLLER

----

~---+------------------------~M

-, I I I I I .-------------------------~·

r''' r"· C A E B 0

I I I I L ______ ..J

ACTUATOR

OEHCAJFG _j

0 A 8 Ch 0 A 8 c I . I I I I I I I L------...J L-----...J

FLIGHT COMPARTMENT FLIGHT COMPAATMENT

TEMPERATURE SENSOR OUC T TEMPERATURE SENSOR

-f 3 2 I

I ~ I I < : I ? I I L---j

FLIGHT COMPARTMENT

SELECTOR

SCHEMATIC . . '

SDJ-06-6064, JSSUECb

HV FIG FLIGHT COMPARTMENT 1 01 TEMPERATURE CONTROL

21-05-00 Page 101

Apr l/89

STATION 37· 5 LEFT

II H L2 I ON/OFF SWITCH

0

I I H L I I 2 I~ PILOTS FAN T B 125

\ --"-'-- -0 :.{V

/ BR -- 2

,...._ E 185

-~

NOTES

1. UNMARKED CABLES ARE KTCL -I - 24.

2. CORES SHOWN THUS -----ARE SUPPLIED

AS TAILS WITH EQUIPMENT.

J. SEGREGATION:- GROUP 'A' 28 V D.C. LEFT.

GROUP 'a' 28 V D.C. RIGHT.

0 JST&2~o PILOT'S MAP liGHTS (33-19-00) FIG.1

A1-A160

I

I I

I I

I

I

I I

I I

I

I

I I 2 H ll I 2'iD PILOTS FAN

I I \

I J I I

I I

I

I

Sih©~ SlD3Jo60

WIRING MANUAL

FLIGHT COMPARTMENT

STATION 37• 5 RIGHT

I 2HL2 I ON/ OFF SWITCH

0

0" '-" T B 126

_ BL --(1' '-" kD

BR 2 -

E 186

--~

10 LEFT DISTRIBUTION

I

I I I I I 75

T I ~ '. 5A 1

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20 PANEL RIGHT DISTRIBUTION PANEL

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WIRING DIAGRAM 503- 06- 60n ISSUE

1Ab

1

FIG w & 2ND 1 PILOTS FANS

21-51-00 Page 1

Apr l/89

WIRING MANUAL

GHT COMPARTMENT ~~------------~

_l____1Q____ Ne2!1ATT£RY ~~~ ~~~~~--~B~A~V~--~~~ ----------"F~R~A~M-E=-~7~4-"1~220-----------~----------~·~·~A~M~E0-4~4~7--~·~0~8----------_, ~PANEL AIR STAT! ONS ....

PASSENGER COMPARTMENT TEMPERATURE COHTROllErR:;-;-:;-,

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AUTO/MANUAl SWITCH 'A' I • I

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AIR CONOJTIONING CONTROL & INDICATION (21..01-00),FI G.101 ~----------~'~,~----~

MAIN FAN & RAM AIR CONTROL SYSTEM {lJ-03-00J. FIG.101

CENTRAL WARNING SYSTEM DIM/BRIGHT & TEST SWITCHES

( 31-50-00 ) ,FIG.101 (2}

ALL A/C

PASSENGER COMPARTMENT ''------'1- GASPER BOOST AIR VALVES & MANUAL CONTROL SWITCH FANS (21-02·00), FIG.IOI

•IILI-----~-, II• ., HOT r - - - - - - - - -,

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,--; -------

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3 -l I PASSENGER COMPARTMENT

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11 2 1 AUTO/MANUAL SWITCH I

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PASSENGER COMPARTMENT TEMPERATURE CONTROLLER

G "\--------- -------,

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BY- PASS VALVE I ACTUATOR I

L ------ --- -- --

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5 I -- - I

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PILOT TEMPERATURE _.-J~==~=I~------~=-=-11/:___j_ _ __L_~ SElECTOR i '--,',--_2 __ -,1 _ _jf- j i -'----,-3 ---2 ---,1-..Jf- l

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UNIT

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,.-NOTES

FOR NOTES & CROSS- REFS REF£ R TO SHEET. 2-

A91 - A107,A109 - A115

2P

PILOTS AVIONICS PANEL

"l'!'?--28V D.C. INPUT I

JJ FREQ_ SEL COM _ A 2

FREQ_ SEL • ~ 117 \OM Hz 7

FREQ SEL D " FRED SEL A ~ 6 IMHz 5 " 4

~~EQ_ SEL ! REO SEL

0-IMHz ~ 12 " It

FRED_ SEL E

~REO. SEL C 21 O-OIMHz FREO. SEL 0 9

SQUELCH nc;~1 ~ J2

AUDIO IN HI

AUDIO IN/OUT LO lw AUDIO OUT HI

CHASSIS GNO.

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PANEL LIGHT HI I ' PANEL LIGHT LO 9

2SVD.C0UT I 2

XMT. LAMP LO 12

DIM REf HI SV D.C. " DIM CONTROL I"

WIRING MANUAL

FLIGHT COMPARTMENT

BE HI NO PANEL I P

J B 1 No. I AVIONICS BAY

I ~ I I " ·-@ I IRZ12·N· I

If ' I I J1RV2J4J5J 9 TRANSCEIVER

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[!] I I 20 28V DC INPUT

I j ' ' ' FREQ. SEL COM E I

CONTROL {'REO. SEL : 8

UNIT "' c 7

FREQ. SEl 0 :I I SEL A

~ 6

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SEL I

'FRED. SEL

~ 11 D 111

SEl '.:: SEL C SEL _ D 9

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IP

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WIRING MANUAL

COMPARTMENT

No.2 AVIONICS BAY

20 2RZ12- N- 4-0 ,--r P101

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113 14 1

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AUDIO IN/OUT LD

AUDIO our HI I" L '-J'lf j' ' I ~~:1''' CHASSIS GND 7 MJ C. HI.

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LD -2RZ12- N- 24 PANEL LIGHT 9 I I -H- 37-

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I~ I

All UNMARKED CABlES ARE KTCL-1-24

-' CABLES SHOWN THUS ARE KTCL-IMS-24 DIM REF. HI sv o.c. 18 ® CABLES WITH Nos. ONLY SHOWN ARE MINYYIN SIZE ©J)- I I BXEJ 1 2T ~~ CABLES SHOWN THUS# TO SE TWISTED ·=t I I I TOGETHER ALONG THEIR ENTIRE LENGTH I ® ' ' OJM CONTROL SEGREGATION GROUP B 28 V O.C. RiGHT. & 5C A.C. RIGHT. I

® .F) AUO!O SYSTEM ( 23-5!-00 l FIG. I. I ®

XMT. LAMP HI

lJ 2RZ12·N· 8

MAIN INSTRUMENT PANEL UGKTTNG (33-13-00),FIG.l :;r ' I I © CENTRAL WARNING SYSTEM (31- 50-00). FIG. I I @ AOF SYSTEM (34 -51- OO).FIG.I. I I ® VORI!LS MARKER BEACON SYSTEM (34-31-00J.FIG.I.

I I 0 TWIN TRANSPONDERS ( )4 ·53· OO!FJG.\ I

A91 - A94.A96- A104,A106,A107,A109- A111,A115

20

RIGHT DISH! PANEL

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FUSELAGE

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WIRING DrAG RAM SDJ-06-6231 ISSUE),~Q

RV FIG. L V.H.F SHT.2 SYSTEM.

23-11-00 Page 3

Feb 05/94

SHEET 1

ADJACENT TO IP PANEl

IHFPBI* (s) (P) MINYVIN 12

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No.2 AVIONICS BAY

121?2121

® I 2RZ3 I I I( \!A'f'"''~~( ~H 9

WIRING MANUAL

FUSELAGE CENTRE DUCT 60 RIGHT DIST. PNL. FRAME 74·483 3D DJST.P

• 12P ATTENDANTS SW. PNL FRAME 508

PVM ~ ~~ W·'''r-,-,CD·S< ~ : 28V D.C. R'GHT f-~~~----'---il;;J I ® RTBsS{ij : I : I I : I CONTRCL PANEL

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r HOlES UHioiARKEO CABlES ARE KTCL-1·2~

CABLES SH:lWN THUS .: ARE KTCL-IMS-24

CABLES WITH No$_ ONlY SHOHN ARE MINYVIH SIZE

CABLES SHOWN THJS/ 0 ARE KTCL-2MS-24 SEGREGATION;- GROUP 'A' 2E!V O.C., 26V A.C. LEFT

GROUP 'ff 28V O.C., 26V A.C. RIGHT GROUP 'J" M!C CABLES

® ®

AI.IDlO SYSTEM (23-51·00~ FIG_!

lOW FUEL & Oil PRESSURE WNG. ( 28-~I -00 ).FIG. I

© BRIEFING SYSTEioiS

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CABlES Sf!O'J'."N THUS ---- ARE SVPPUEO AS TAllS V.1TH EQI.IIP,.-Ef!T

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WIRING DIAGRAM SOl- 06- 623B

FIG. I SHT 4 AUDIO SYSTEM

23-51-00 Page 7

Feb 01/94

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-NOTES-----------------------------, UNMARKED CABLES ARE KTCL- 1 -24

CABLES SHOWN THUS =>;='=~':ARE KTCL-lMS-24

CABLES SHOWN THUS ~~-~~~ARE K T C L- 2MS-24

2M51 CABLES SHOWN THUS ----- ARE REF. ONLY

SEGREGATION:- GROUP 'B' ZBV D.C. RIGHT GROUP '0' liSV A.C. RIGHT

0 AUDIO SYSTEM {23-51-00), FIG. I ® CONTROLS LOCKED WARNING (27-70-00), FIG.t CD CENTRAL WARNING SYSTEM (31-50-00), FIG. I ® FLIGHT DATA RECORDER (31-31-00), FIG. 1 0 A. C. POWER SUPPLIES (24-21-00), FIG. I ® PASSENGER AOORESS (23-Jl-00), FIG. I

I . A I .. s

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WIRING MANUAL

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Page 1

Feb 04/94

4P ROOF lD LEFT DISTRIBUTION PANEL

WIRING MANUAL

FLIGHT COMPARTMENT

FRAME 54 LEFT lEFT BATTERY BAY

20 RIGHT DISTRIBUTION PANEL 54 RIGHT RIGHT EQUIPMENT BAY

'c.~ ~!~r-----~--------~--~~~~--------~-------~-------------~------------------------------------'-------~-~-~~%~~--4~''" ~ 'o T ~a~ 'E' [I] LEFT INVERTER I EH _

ELECTRICAL PAC,NE:.:L~=c-~-;o FRS 54-74

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XA ~~~f.1 503- OS ISSUE ' 0 4_

A.C. POWER SUPPLIES

24-21-00 Page 1/2

June 30/87

® FLIGHT DIRECTOR (3'-23-00), FIG.I ®ENGINE TORQUE INDICATORS (77-11-00), FIG. I

© VOR/ILS/ MARKER BEACON SYSTEM (34-31-00), FIG. I

® GROUND PROXIMITY WARNING SYSTEt-1 (34-42-00), FIG.! ® FliGHT DATA RECORDER (31-31-00), FIG.! ® FUEL BOOSTER PUMPS (26 -22 -00), FIG. I ® ROOF PANEL & STANDBY COMPASS LIGHTING (33-12-QO), FIG.I ® WEATHER RADAR (34-41-00), FIG. I 0 ICE DETECTOR (30-61-00}, FIG.! ® VOICE RECORDER (23-71-00),FIG.I ® STANDBY ATTITUDE GYRO - 1sT PILOT (34-14-00), FIG, I ® CENTRAL WARNING SYSTEM (31-S0-00). FIG. I

® STANDBY ATTITUDE GYRO -2ND PILOT (34 -24 -00}, FIG. 2 ® MAIN INSTRUMENT PANEL LIGHTING (33-13-00 FlG.l) ® CENTRE CONSOLE LIGHTING (33·1&·00) FIG.!

WIRING MANUAL

r----NOT£5--------------------------------------------------, 1. UNMARKED CABLES ARE KTCL-1 -24

2. CABLES WITH NUMBERS ARE MINYVIN SIZE

3. CABLES SHOWN THUS-=-=.. 20

ARE KTCL-!MS -24

4. CABLES SHOWN THUS=..;;;~;:. ARE MINYVIN METSHEATH SIZE 20

5. DIOO ES CONNECTED ACROSS TERMINALS XI & X2 OF RELAYS ITEM IS

MUST HAVE THE RED BAND ON DIODE NEAREST TERMINAl X1

6. SEGREGATION:- GROUP'A 28V.O.C.lEFT

26 V. D.C. lEFT

5 V. A.C. lEFT

GROUP 'C' liS V. A/:.. lEFT

GROUP 'a' 28 V. D.C. RIGHT

26V. A.C. RIGHT

5 Y. A£. RIGHT

GROUP '[J' 115 V. A.C. RIGHT

WIRING DIAGRAM SD 3-06-6051, ISSUE 'Da.'

XA Fl G.1 C W SHTZ A .. PO ER SUPPLIES

24-21-00 Page3

June 30/87

.....:~ 84 H \r SA 83 H JOA 175 H SA

v

RIGHT 28 V ESSENTIAL

WIRING MANUAL

BUSBAR

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RIGHT INVERTER OUTPUT RELAY

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I I w ,@; W 1 INDICATOR I I w 11!;:,. !.@w

1 I 1 .. , "' I

:1~ I""' I T· I I -~ y I I y ~ I ~WHITE 2 I a_., I I if~-~ : YELLOW 1 r:- __ "':..__1 I ___ ::_-~---- I GREEN4 I OFF a. ~~ A·C I 'I'' I ON -....r-- jll'" L- _A..:llQ__ - _I 'FG' RoGHT INVERTER FAilURE

INDICATOR /SWITCH

tR'iNVl VISIBLE WHITE ~YELLOW

375 ~ lA v

RIGHT /VOLT FREQUENCY METER

'se' ---1--T-fO ~"

~~~====1 I)( ATF~y A. C. POWER SUPPLIES

24-21-00 Page 101

Nov 11/86

NOTES:-

UNMARKED CABLES ARE MINYVIN 20

CABLES WITH Nos ONLY SHOWN ARE MINYVIN SIZE

CABLES MARKED K24 ARE KTC L-1-24

CABLES SHOWN THUS=::.:::::. ARE KTCL-IMS-24

CABLES MARKED 'EFG' ARE EFGLAS SIZE

CABLES MARKED 'NVA( ARE NYVINAL SIZE

CABLES MARKED 'TSA( ARE TERSILAL SIZE

CABLES SHOWN THUS ARE MINYVIN METSHEATH 16

CABLES MARKED 'EFGM 16' ARE EFGLAS METSHEATH 16

CABLES SHOWN THUS @ARE TO BE SEGREGATED FROM ALL OTHER CABLES BY RUNNING EACH ONE IN CONDUIT ALONG

THEIR ENTIRE LENGTH.

CABLES SHOWN THUS* ARE TO BE IMMACULATE

DIODES CONNECTED ACROSS TERMINALS X I & X2 AND X3 & X4 OF CONTACTORS (ITEMS 21 & 22) MUST HAVE THE RED BAND ON DIODE NEAREST X2 & X4 RESPECTIVELY.

SEGREGATION:- GROUP 'tf. 28V. D.C. LEH GROUP 'fi 28V. D.C. RIGHT

WIRING MANUAL

® D.C. POWER SUPPLIES (DISTRIBUTION), (24-32-00), FIG.!

® ENGINE STARTING (ao-1o-oo), FIG.!

© GAS GENERATOR SPEED INDICATORS (77-12-00), FIG.!

@ CENTRAL WARNING SYSTEM (31-50-00}, FIG.!

® ENGINE AIR INTAKE ANTI-ICING (30-21-00), FIG.!

® A.C. POWER SUPPLIES (24·21·00), FIG.1

@ A.C. POWER SUPPLIES (24·21-00). FIG. 1

WIRING DIAGRAM 503-06-6048, ISSUE'F'

PA FIG.I SHT. I

D.C. POWER SUPPLIES (GENERATION)

24-31-0 0 Page 1/2

Feb 10/85

WIRING MANUAL

~==~==~~==~ITF'Lilli~ffill~C~O~~~~~~:~N~======~======~~====~~ ~ ~~~~~~llilw~ FR22 1P j No1 4P ROOF 21C h-*r 1C LEFT 1-----"~-------i_;;;' ~;~.; STN L'""' 19C ZONE 1 STNS112-122 LEFT p~ MAIN ~lA~~(S ELECTRKAL PANEL ~ o!-------LE_FT_E_UU_IP_ME_NT_PA_NE_L ___ L"_"R:::."BA::._Y___JL_ __ ST_NS_7_4-_B9_---; 5TN5 ;::-;,.- r~-'-'--~_L_ ___ __L_ __ -1 . -r=~~____::_:_~~=---±~+--~ ~ 1 1 1 -_ , , n"ffi 1

1 1

I I I I ~ A ~ I ;€ SA 0 I I I ' y ~~=-'--'---------, I 1 I I ~ (1:~ I I I ~-------+t====*~~~======~l c cl-+-1 ----~ I I I I I I I I LEFT1 I®~ I I I

I GENERATOR ""' I I I TEST SWITCH [%(I)'----, LEFT I I I I I I LEFT I I I I ----' LEFT

'

I ~"-i}!+..J 8csal I 1 I . ~ AMMETER 1';:: IAHBERI " I f1C- HiMi] ' I (=v- JJ:l~l~ 'f~·::H~*~fsH~UNT

·cw•·j€>!+-. : :·"~-~p·l1_w __ l,._l~-·l·_·l _ _ll _ _j:L_

WIRING MANUAL

~----------------------~-1 11 CQ~~NI~T~========~~========~=:~=+====~~F~'L~~·~~~~~~~==~~@BH~TF~NG~INF~,9cr·~~ I I

;b. I I I ~CD~..;-· -j ll ll [_J _ _I_ _ _L~~=~. r1 12J!r,\ ~I L l l I @] ld ;.; ,_ RIGHT ~ ~"" . ! I I I I TB~ I~ ®/} I F F~~=+=A~@'""'l.~ '

(24·32·00) FIG. 101

I AMMETER

RIGHT UN!l TERM"

BIB TO CBSS

RlGHT U~~cR'~;~~' UNIT TERM'- ~-~ LEFT GENERATOR SLAVE RELAY TERM~ 22

GEN L

(019)

{24·32·00), FJG_101

CURRENT TR,A.NSFQF.'1ER

3PA15

CURRENT TRANSFORMER

'1PA15'

TO CB No_S

LEFT

SERVICES BUSBAR

TO GROUND SUPPLY CONTACTOR TERHh 6, SEE {21d2-00J FIG.101 PREVENTS PARALLELING OF GS & GENERATOR

LEFT GENERATCR CONTROL

4P

LEFT GENERATOR TRIP

0/VOLTS

LEFT ENGINE START -~-------1 SWITCH TERM~ 4 (24 ·32 ·00), FIG.IOI

BUS-BAR ENGmE "'f""-"1-t--~========~ TO LEFT LINE CONTACTOR SLAVE RELAY TERM'= b (24·3HOt FIG.101

TEST 11Wl2-P1

LEFT STARTER

,GENE[3:AT0R PA17

LEFT AMMETER SHUNT

* THESE CABlES TO HAVE ADDITIONAL PROTECTION

TO (811

I

WIRING MANUAL

CONTROL & PROTECTION UNITS _LEFJ ~IGH. T

AA AA -, -J

R

u

' ' T

I I '

I v =t= ~ N

' I

I ' I

ESS SERVICES BUSBAR

SA ~1154 RIGHT GENfRATOR CONTROL r,j] '/- 4P ON~! OFF '

COUPLE 1

RIGHT G~NE,RATOR

TRIP 1 !,!":] ,, 1

10 5 RESET

6 ,l.!__J

OIVOUS TEST ':oTJ 1 1b1 I

GND. FAULT 'u{-2c

I RIGHT

1LJ GENERATOR ,uc RESET •II RE~AY p CR-2C

b

9 (08) 27

22(- PI

TO GROUND SUPPLY CONTACT OR G101 TERI+ 6, SEE {24-32-00I_FI

(PREVENTS PARALLELINU OF

RIGHT MAIN BUSBAR

' II II II

CURRENT TRANSFORMER '4PA15'

CB 155

RIGHT VOLT I

+-_____ LEFT UNDERVOLTAGE

UNIT TERM'- T8123- 3

RIGHT

~-~-LEFT UNDERVOLTAGE UNIT TER* TB123 -2

{24-32-00) FIG_ 101

TO LB No.155

RIGHT GENERATOR FAILURE SLAVE RELAY TERM'= b (24-32-00), FIG. 101

Pq---~~~Jfi!~~froil:========:::--tr.:.,t ENGINE BUS-BAR TO RIGHT LINE SLAVE RELAY TERM\- b (24-32-00), FJG_IOI

+-------RIGHT ENGINE START

SWITCH TERM!. 4 {24-32-00). FIG.101

I

I

' I

RIGHT AMMETER SHUNT

I

_j

RIGHT STARTER ~ENE~TOR

PA17

PA 101

STARTER RUNNING (016) WARNING (GREEN)

12WL2-P1

(GENERATION l

24-31-00 Page 101

Feb 23/84

NOTES:-

UNMARKED CABLES ARE KTCL-1-24.

CABLES MARKED 'N' ARE NYVIN SIZE.

CABLES WITH NOS ONLY SHOWN ARE MINYVIN SIZE.

CABLES SHOWN THUS --- ARE KTCL-IMS-24.

CABLES SHOWN THUS---- ARE REF. ONLY.

CABLES SHOWN THUS @ ARE TO BE SEGREGATED FROM ALL OTHER CABLES BY RUNNING EACH CABLE IN A CONDUIT ALONG THEIR ENTIRE LENGTH .

CABLES MARKED THUS * ARE TO BE IMMACULATE. DIODES CONNECTED ACROSS TERMINALS 3 & 4 OF CONTACTORS (ITEMS 33, 34 & 35) MUST HAVE RED BAND ON DIODE NEAREST TO TERMINAL 3.

SEGREGATION:- GROUP 'A' 28 V D.C. LEFT. GROUP 'B' 28 V D.C. RIGHT.

DIODES COtJNECTED ACROSS 1'ERMfNALS C g. Co, OF RELAYS ID-'K' & 2().:1-\• ,-0 HAVE REI> BAND ON !:>lODE NEAP.E:ST TO TERMINAL C

WIRING MANUAL

® CENTRAL WARNING SYSTEM

® D. C. DISTRIBUTION

© ENGINE STARTING

@ 0. C. POWER SUPPLIES (GENERATION)

® REFER TO SHEET 2

® REFER TO SHEET 3

@ READING & EMERGENCY LIGHTING

® LANDING GEAR CONTROL & INDICATION

(31-50-00), FIG.1

(24-51-00 ), FIG.!

(80-10-00), FIG. 1

( 24- 31- 00 l, FIG. 1

(33 -22-00 ), FIG. 1

(32- 30-00 )1 FIG. 1

WIRING DIAGRAM 503-06-6049 ISSUE 'Ad'

p A FIG. 1. SHT.1.

D.C. POWER SUPPLIES ( DISTRIBUTION )

24-32-00 Page 1/2

Feb 14/83

"

\1\_ 10 I•

I I " ( 1-!TJ I IS E71

E d I•

'

I

HTBI E71 ")--'--'"'--:-(] ''· I• --

LEFT BATTERY 1 fi:\ (i' 1 (:! \ 17

1:1:~1:1"a , ""-"~" '~

'r I (C) QkJCD~ lj, ~ 8 (i) 1---:------:7 11WL2 ~ 'iAI

__ J

I I ·~ I i:;l'~~ I I ~ .

I I I

I I

' I

'~u I ~ , I

- I

I

J I)--~

' ~ I j !.2) l...:J"~ SHEDDitlG ~) BIJSBAR

@ 0 "'"

I

(')

I ~I

I

IJ' ; FOR NOTE5 REFER TO 511EET 1 I""' I

I

LEFT EOUIP~Hlf P.

NOSE

h '

I I I

I I I

I

I

I

I

WIRING MANUAL

FLI ~T

""""" '"" ~ "'"' ~

J ! II : C==tt ', ~· JA!. I WARNING ~1 ... , I I I ! I I

I

I I I I

!§II I I I .,

' ' I

I I

I I I I I

I I

I _( ~) [® 0® C' I ~~i~' I . 00~

Tal 1 I Tl( 1 •z\. ti•E2

10 ,2 I 11•E4 I

j MTB2 E72

I 1 I 16 i-c::t•·

E74 I I 16 I @J-10 -:--"'---;-01 I•

I

I I I I

I I I

I I

I

I

' ''" ------~1 ~~'T·~--"-"_'"_"_·"~

-:-IC-52-1 I SHEET 4

DIODE I

" ( >)-C-.L... ' 154 -.11

i ' .-+---t-t--- '

GREEN ~ ( I '"'I ·li RED I 0>71-------'

I I EW

8LACK 10) 1 9 OVERVOLTAGE

' ~ CETECTOR

PANEL JOC

NOTES I [ REFER 10 SHEET 1

24-32-00 Page 5/6

Feb 15/87

WIRING MANUAL

r--------------------------------------cf~L"IG~H~Tr-~coM~npA~R~T~MTrE~NnT~-------------------------------------,

I

I I I I I

I I I I I

I I I I

I I I

I I

I I

I I

2 c 1 c RIGHT EQUIPMENT PANEL STATION 54-74 LEFT EQUIPMENT PANEL

I I I

I I

1C-52 1C-P2

BC2324 I ~ ! SHE ~T 3 -------:-

1-1 t t 1----------,

RELAY 'R' ~ I I I I TB 43 CD G)

" Q 2C-P2 2C-S2 I :; ~ ((23~>-i,--'

\ L I • G) rb), RELAY 'A o'- 3 ~ r?i\ 1'-

SHEET 3 ·----18 Bl-1-------lr r ~---[, ~23~111 ~

RELAY 'Ac'- 7 SHEET 3 -----1

RELAY 'B'-4 SHEET -3 ------1

I I y II-

I ~------jq q~-------~ I - -

~-------'-1 -Js sf---- 1c-'P'-22 © I I I

I I

I

I I

I

I I I I

I

I I I I I

I I

I I I I I

I

I I

I

WIRING DIAGRAM 503-06-6049/ J& SP3-03-645b/A

PA FIG.1 D.C. POWER SUPPLIES SHT. 4 ( 0 IS T R I B U T I 0 N l

24-32-00 Page 7

Feb 15/87

CENTRAL WARNING SYSTEH

01-50· OOJ, f!G.101

AVIONIC SUS-BAR ~ ....... 401

L..---6,.1?----l- D.C. OISHt r !lf.·st-ooJ

lEFT GENERA TOO FAILURE SLAVE RELAY 'J'·lC

'F(·4P lOAD SHEU SWITCH ·LEFT

TO lEFTT8~:~.T·voorAGE UNIT TERH i" 114·31·00), FIG 101

TAIL BAJTW BUS-SAR

WIRING MANUAL

ESSENTIAL SERVIC5 RELAYS

'&-1c

l2C-P1 1010)

START

""" -!-+~----- ----!+----------={!~

'u'-2(

RIGHT START MASTER

tr·4P

GROUND SER\IICES BUS-BAR

20

ffiOUND SUPPLY CONNECTOR

I 124·3I·OOJ, FIG 101

CONTACTm 'o'-zc

101 RIGHT ELECTRICAL

RIGHT START

MA~~r: ~~\TCH

'(-2[

RIGHT STARTER CONTACTOR TERI+ X2

z

WITH Off-liNE 'f 2(

{31·50·00JFIG 101

SA

UNIT

24-32-00 Page 101

June 5/87

75;.

" < • ~ ~ • ~

w 10 u

>

" w ~ SA

" BLOW

. ". [2]

10

r·

0 ENGI~

I

17\C -•~--~-O~A~ G£NR CONTROL ~- (!) ~ (l) FIE LO

•

j j

10

2D-C8162 SHEET 2

10

LEFT ESSENTIAL sERVI'::ES

TRANSFER RELAY SA

'

< SA "

FTII w z w 0

u

" > •

NOTES ------------0

FOR NOTES & CROSS -REFS

REFER TO SHEET 2

VHF I

FA55Et;'3ER EM G. z LTG SUPPLY

E.L.T

BATT. !NDIC"'-

SA E

®

OIST

WIRING MANUAL

---cDID)----

SA

SA

5A

SA

SA

SA

SA

SA

SA

" < • ~ ~ • ~

w u

> " w ~

" SA < ~

z w ~ ~ w

~ ~

AY 'H', TERM I,

SHEET 2

"

*

" < ~ ~ ~

~

0 _ VALVE z

0 0 w I

• u 0

> I • N

I

p B FIG. I S HT. I

DISTRIBUTION PAt4El

D. C. D STRIBUTION

24-51-00 Page 1/2

Mar 15/91

c;ND SUPPLY PLUG 00AGS JNOS GNO SUPPLY PLUG IS~ GROUND SUPPLY CONTL

FT13

0 z 0 0 w I ~

u 0

> • ~

sr'ev

lA "'

t FT. tS

lA

0 z

' I "' 0

lA w HAP > " • <

m " • 0 m

u z w 0 • w ,

" " 0 w

z

' I ~ w " 0 , w ' • " > u z w

< " > 0 " 0 u

• w > w

• w 0 z "'

E~IT

j w ~ ~ < " FWD. EXIT

NOTES

CABLES WITH NO$. ONLY SHOWN ARE MiNYVlH SIZES CABLES SHOWN THUS~--·-·- ARE REF. Om.Y * THESE CABLES TO BE IMMACULATE ALONG

THEIR ENTIRE LENGTH.

® D.C. POWER SUPPliES (DISTl!.) (24-32-00 )1 FIG. I.

" '

® READING & EMERGENCY l!GHTifiG {33-22-00)1 FIG. I.

CD ®

m

~

5A < ' z w • • w u 0

> m ~

0 z z I 0 w > u z w 0 • w > w u 0

> • N I

' ' AFT_ 12~ EMG LTG

1 SUPPlY

'

l

oD DISTRI6UTI0~1 PANEl

"' V-H-f l

PB

"

"

10.

• < m • " m

> • w • ' z w , ' • < " > 0 u

• w 0 z w • ~ < "

I

24-51-00 Page 3

Mar 13/91

30 TAIL DISTRIBUTION PANEL

28V D.C. PASSENGER COMPARTMENT SERVICES BUSBAR

12P ATTENDANTS SWITCH PANEL

No.1 BEVERAGE ~ CONTAINER SWITCH CD

PLUG BREAK

'12P·

53 PJ

WIRING MANUAL

FUSELAGE

STN 458-475

G/FB2

GALLEY STN 498-508

No.1 BEVERAGE CONTAJI£R

s p cr 7-5A ®r---...:._------H~ 3::..1}+-------:-J G G f-7-----------j F F - - - - - - - - - +

E.lo.0.2 TB163

.1'~ ,16'--\Ji) I 20 .------

2}----lK K r-- -, I .,.,.

4'L

28V D.C. PASSENGER COMPARTMENT SERVICES BUSBAA

No.1 BEVERAGE (r:sT( "'6(r:7,-(8""( (3 I I I CONTAINER LAMP

No.2 BEVERAGE CONTAINER LAMP

G Gr--_!_ __ j I

J J r----~--1

I I

'/ '12P' ~ ~~~~N·~(=s=(6~(=7=(=8~(~2~o-~::1~----2o~--------~(:

()1 I I I I

)? I I 20 E~J I I

'12P' -br--"16"---- I I No. 2 BEVERAGE CONTAINER

No.2 BEVERAGE \t' 0 53 PJ -;- 1 I ~ CONTAINER SW1TCH IQ;'l+--------'--l H H f--,--------------1 H H - - -,--,- - +

cr 7-SA @f-------------11n..G); I I CD I L---

ENTRANCE SWITOl y

r:---,

GALLEY LIGHT SWITOl

'p' 0 @10 01

1 0 5 r.--1 -£!!'--'Co( -------- I

~ 24 24 {!)

.28V 0 C. PASSENGER COMPARTMENT SERVICES' BUSBAR I 10 0 1 ---~ CD

'12P •

P1 51

DO DO

.--Nores--------------------------, 1 CABLES SHOWN THUS ---ARE

REFERENCE ONLY AND SUPPLIED WITH GALLEY

2 UNMARKED CABLES ARE MINYVIN 18 CABLES WITH No.16 SHOWN ARE MINYVIN 16 CABLES WITH No.20 SHOWN ARE MINYVIN 20 CABLES WITH No.24 SHOWN ARE KTCL-1-24

3 CABLES SHOWN THUS a2T ARE TO BE TWISTED TOGETHER Z

4 SEGREGATION:-GROUP'B 28V DC RIGHT

A62,A66- AUP

PASSENGER COMPARTMENT nvo LEVEL LIGHTING (·33-21-00 )

1 FIG. 1

24 L

1 I I I

Lt---------1 I I I .__ 24 ---

24 -----

-= BALLAST • UNIT I HJ10 I

-tB1 CD+-~---------, ® ~-~-------~ I @ ~-~--..,2T I 12T

J..C:\ ~ 24 I V:' · .... r'-='-.::....,____.._I.YI..::.....J 1- - - 1 GALLEY rusE ; I

- - - - _I 'ENDA : 6 ~ '·END a· L fD Oi- j(HJ4(11(

H J FIG 1

WIRING DIAGRAM SDJ-06-6087 ISSUE C

GALLEY DOMESTIC SERVICES

25-31-00 Page 1

Sept 5/89

WIRING MANUAL

( 28 V DC PASSENGER COMPARTMENT SERVICES BUS BAR I I I

133 1-

'0

r -- --l I 2

I I I I

OFF 1'd o' 1 L _____ j ON

N~l BEVERAGE CONTAINER ,- -1 I I

INDICATOR I I No I LAMP

~ I I I I I I I I L_ _ j

A1- A4,A6- P8, A10- A14, A17- A42, A48, A51- UP

;0 134 f- 7·5A

~

I - -, 2 I

I I

I I OFF I'd c/ I

L-- _J ON

I I I I I I

J... ,.J 1 1

( -128 f-i SA

' -'( 2 ) T

12P-'E' I r-- -)--! I ~ I I I \ I --- '-.)

ENTRANCE SWITCH

~ PASSENGER COMPARTMENT

lWO LEVEL LIGHTING ( 33 ·21·QO ), FIG.101

No2 BEVERAGE CONTAINER ,- -l I I I I INDICATOR

No2 LAMP I I I I I I I I I I L _ _j

--

GALLEY LIGHT SWITCH

,---; -1 I 'I I I I

I 0 ' I L-- -- _J

BALLAST UNIT

r< -+ - , n(.)--',-----------, : 0 5 2 ;()-~-------, 1 o' 'o~1 ---JI/I•·

•lilf--1 --~1 o- '0 1 L_- __ :_j

HJ FIG. 101

/

'

TUBE

SCHEMATIC 503-06-6087 ISSUE 'Ao'

GALLEY DOMESTIC SERVICES

25-31-00 Page 101

Sept 1/89

FLIGHT COMPARTMENT

1P

WIRING MANUAL

BEHIND PANEL 1P 1D PILOTS INSTRUMENT PANEL JBI LEFT DISTRIBUTION PANEL

CIRCUIT BOARD 0 ~r 'H HI

0 25106 _1. ( FERRANTI ) 11 r:'::!!. --@ H H : 14 ~

I

I 41~ (O·~SW} 1 VOEF 61-12 PT6 EQUIPMENT WIRE vvvv

19 7:~~ (O~SW) I ~'r

yy v v I 67 I TRANSMITTER L ON LIGHT

')., I 'GH' SA cb -.'::((! A A T10 ITT ITT ... r'( I si6171 28 v DC

r '!!> BCY 70 2N4400 r- ~ BATTERY BUS BAR

I I liT I ( 30925A ZF 4 ·7 P

~

I I I 3·9 K (O·SW) T,!_ I AAA I ••••

~

OEF 61-12 PT 6 -..; T 12 EQUIPMENT WIRE 4~K{0•25W) 11

.AAA ~ ~ ~ •vvv

l

r-NOTES -... UNMARKED CABLES ARE KTCL-1-14 A

CABLE SHOWN THUS ====IS CORNE & MARGOLIN 'r'

IO TBI JTO ' • A' 28 V SEGREGATION:- GROUP D.C. LEFT

REMOTE CONTROL ® CENTRAL WARNING. SYSTEM SWITCH (Jf- so-oo) FIG. 1 SHEET 1. [j]

A62, A66 - A76, A77 - A86, A90 - A94, A96 -A 111, A 116 - A150

FRM 508

" [RF I

1!1. 'I 0 0

REAR FUSELAGE

ROOF STA liONS 508 - 536 • 5

ANTENNA

jWRIIj

~ I I I I

I I I jWR9 I I I EMERGENCY LOCATOR TRANSMITTER

I I jWRZj11j I I

I I - - -r ---------L

E64

-

WR

r Jn L r J Ji L

WIRING DIAGRAM 503-06-6216. ISSUE 'G'

FIG EMERGENCY LOCATOR 1 TRANSMITTER

25-60-00 Page 1

Sept 5/89

NOTES:

1. UNMARKED CABLES ARE KTCL-1-24

2. CABLES WITH Nos. SHOWN ARE MINYVIN SIZE

3. CABLES SHOWN THUS 'ECM52' ARE ECM52 SIZE 16

4. CABLES SHOWN THUS UFX20 ARE UNIFLEXGLAS SIZE 20

5.

6.

A78, A80- UP

TO BE GROUNDED TO MOUNTING SCREW OF FIREVVIRE

"END TERMINATION"

SEGREGATION:- GROUP 'A' 28V D.C. LEFT GROUP 'B' 28V D.C. RIGHT

I I

CW8

FIRE L

PTOC

v

1CW13'

FIRE

WIRING MANUAL · LOT, Revision 3 Mar 01/13 Page 1 z SD3-60 AIRCRAFT WIRING MANUAL TO: Holders of...

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Transcript of WIRING MANUAL · LOT, Revision 3 Mar 01/13 Page 1 z SD3-60 AIRCRAFT WIRING MANUAL TO: Holders of...