Wiring Diagram for Beechcraft 99 Airliner
Beechcraft 99 Airliner · Wiring Diagram
Overview
This document is a wiring diagram specifically for the Beechcraft 99 Airliner. It serves as a reference for technicians and pilots to understand the electrical systems and wiring layout of the aircraft. The wiring diagram provides detailed illustrations and schematics that are essential for maintenance and troubleshooting of the aircraft's electrical components. It is crucial for ensuring the proper functioning of the aircraft's systems and for conducting repairs when necessary.
- Understand the layout of the electrical system in the Beechcraft 99 Airliner.
- Refer to the wiring schematics for accurate connections between components.
- Locate key electrical components easily with the provided diagrams.
- Use the troubleshooting guide for efficient diagnosis of electrical problems.
Document
Source
Originally published by www.bonanza.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Wiring Diagram
- Pages
- 10
- File size
- 629 KB
- Publisher
- www.bonanza.org
Most owners only have the POH. Here's the essential set for the Beechcraft 99 Airliner.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 99 Airliner to your watchlist and track it in one place.
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In this document
Electrical System Overview
This section provides a general description of the electrical system in the Beechcraft 99 Airliner, including the power sources, distribution, and major components.
Wiring Schematics
Detailed wiring schematics are included, showing the connections between various electrical components such as the battery, alternator, and avionics.
Component Locations
This section identifies the locations of key electrical components within the aircraft, aiding in maintenance and inspections.
Troubleshooting Guide
A troubleshooting guide is provided to assist technicians in diagnosing electrical issues based on symptoms and circuit diagrams.
Safety notes
- Always ensure the aircraft is powered down before performing any electrical work.
- Follow proper safety protocols when handling electrical components.
Full document text
Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL 24-30-03 ALTERNATOR (PRIOR TO INSTALLATION OF KIT 55-3025-1S) (Configuration 1) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 24-30-03 Page 1 01/29/99 B15 STARTER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL P54 J54 W32A20 - • 3 32 --] 91-02 91-19 [- +3 F26\XF26 K3A2 PIC2 -4 -] 24-40 74-30 [-K2A20 CR20 P23A20N K14 START RELAY • 24-33 24-34 P33A16-01. 25-11 [ PITA18 P31A20 P29A20 W24 5A FI5/XF15 5A F16/XF 15 E56A20 77-20 E55A20 50A F2/XF2 P8D8 P8B8 24-50 W22 W25 50A +4° F3/XF3 P6A8 AVIONICS BUS 02. 03.04 W20 -P2A4N- -P BTIO BATTERY R34 SHUNT CR24 1 80A K15 BATTERY FIXE MASTER -P8A4 CR25 RELAY A16 ALT OUT SENSOR -4-P20A20-24-40 -P3A4N- LP3816- BAT GND F2 FI AUX 9 e-P64A18-] 24-31 -P25A20 →→→→ OPTIONAL 100 AMP ALT I • — P53A20 P54A20N CII P8A4 P25A20-5A ÞJPR20,01 F31/XF31 +2 RED -P25A20 STANDARD AUX F2 GRN PI6A20 -] 33-10 BLK - PI8A20N GS3 G18 ALTERNATOR ו - WIT -P64A18- -] 24-31 P80 J80 OFF -P4A20 -P5A20N I 529 BATTERY SWITCH ON 91-15 - L SUBPANEL 5A -P25A20→ F31/XF31 G18 ALTERNATOR 2 REFER TO APPLICABLE AVIONICS DIAG FOR MODE OF CONNECTION. 03 WHEN OPTIONAL DUAL NAV IS USED REFER TO DIAG 24-51. 04 WHEN OPTIONAL SINGLE NAV IS USED REFER TO DIAG 24-52. 4 USED ON ACFT WITH EXTERNAL POWER OPTION ♦3 USED ON ACFT CE-919. CE-923. CE-925 & CE-927 ONLY ♦2 WIRE AS SHOWN EA-158 ONLY ON ACFT EA-6 & AFT NOT USED • ON ACFT HAVING OPTIONAL CONTROL WHEEL CLOCK INSTALLED. REF DIAGRAM 25-12 REPLACES REF DIAGRAM 25-11. WIRE LENGTH MUST BE KEPT LESS THAN 3-INCHES. ° WIRE LENGTH MUST BE KEPT LESS THAN 6-INCHES. GS4 CE24F 982522AA 24-30-03 Page 2 01/29/99 ALTERNATOR (PRIOR TO INSTALLATION OF KIT 55-3025-1S) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (Configuration 1) REFERENCE DESIGNATOR PART NUMBER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL DESCRIPTION INSTL ZONE CODE USABLE ON A16 36-380000-3 BT10 36-380059-1 BT10 PS12-11 24-30-03 (Configuration 1) SENSOR-ALTERNATOR OUT BATTERY (ALTN FOR PS12-11) BATTERY (ALTN FOR 36-380059-1) 222 1 222 1 222 1 B15 MHJ-4003 MOTOR-STARTER (ALTN FOR 637847) 410 1 B15 637847 MOTOR-STARTER (ALTN FOR MHJ-4003) 410 1 CR20 1.5KE51CA TRANSZORB-START RELAY 222 1 CR24 1N4007 DIODE-BATTERY MASTER RELAY (SUPERSEDED BY 132408-22) 222 1 CR24 132408-22 DIODE-BATTERY MASTER RELAY (SUPERSEDES 222 1 1N4007) CR25 1N4007 DIODE-BATTERY MASTER (SUPERSEDED BY 132408- 222 1 22) CR25 132408-22 DIODE-BATTERY MASTER (SUPERSEDES 1N4007) 222 1 C11 39D507G050GL4 CAPACITOR-ALTERNATOR (OPTL) 410 3 F1 FLLB LIMITER-ELECTRIC, ALTERNATOR OUTPUT 222 1 F15 AGC5 F16 AGC5 FUSE-AMMETER FUSE-AMMETER 222 1 222 1 F2 FLLA LIMITER-ELECTRICAL BUS 222 1 F26 AGC5 FUSE-START ANNUNCIATOR (OPTL) 222 2 F3 FLLA LIMITER-AVIONICS BUS 222 1 F31 AGC5 FUSE-ALTERNATOR AUXILIARY OUTPUT 410 1 GS3 131270-3 GROUND STUD-FIREWALL 221 1 GS4 AN3-5A GROUND STUD-LOWER FIREWALL 222 1 G18 642056A2 ALTERNATOR, 100 AMP(W/ CLUTCH)(ALTN FOR ALV9407) 410 1 G18 641668 G18 ALT9422 G18 642056 ALTERNATOR, 50 AMP (ALTN FOR ALT9422) ALTERNATOR, 50 AMP (ALTN FOR 641668) ALTERNATOR, 100 AMP (WITHOUT CLUTCH) 410 410 1 410 1 G18 642056A2 J80 204814-1 ALTERNATOR, 100 AMP (WITH CLUTCH) RECEPTACLE-GROUNDING BLOCK 410 1 231 1 K14 6041H190 RELAY-START 222 1 K15 6041H189 RELAY-BATTERY MASTER 222 1 P80A 200838-3 PLUG-GROUNDING BLOCK 231 1 P80B 201224-1 STRAIN RELIEF 231 1 P80C 201328-1 P80D 200333-1 P80E 203618-1 SOCKET CONTACT SOCKET CONTACT JACKSCREW 231 1 231 1 231 1 R34 MS91586-2 SHUNT-50 AMP 131 1 R34 MS91586-6 SHUNT-100 AMP (OPTL) 222 1 S29 35-380053-21 SWITCH-BATTERY 240 1 W11 002-369014-3 BUS BAR-ALTERNATOR (USED WITH 50 AMP ALTERNA- 410 1 TOR) W20 36-364001-27 W22 002-361016-7 W24 36-364001-13 BUS BAR-SHUNT, AVIONICS LIMITER BUS BAR-SHUNT, ELECTRIC LIMITER BUS BAR-START RELAY 222 1 222 1 222 1 W25 36-364001-19 BUS BAR-BATTERY MASTER 222 1 XF1 FSH LIMITER BASE 222 1 XF15 4532 FUSEHOLDER-AMMETER/CLOCK 222 1 XF2 FSH LIMITER BASE-ELECTRICAL BUS 222 1 XF26 60-369025-2 FUSEHOLDER-START ANNUNCIATOR LIGHT 222 2 XF3 FSH LIMITER BASE-AVIONICS BUS 222 1 24-30-03 Page 3 01/29/99 B15 +3 F26\XF26 K3A2 STARTER 74-30 [-K2A20 Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL P54 J54 W32A20 ♦ 3 32 --] 91-02 91-19 - CR20 P23A20N K14 START RELAY 24-33 P33A16—♦1· 24-34 25-11 [ -PIA18- -P2A4N-ID-PIA2- PIC2 _ 4 -] 24-40 P31A20 P29A20 W24 5A FIB/XF15 5A F16/XF15 E56A20 77-20 E55A20 50A F2/XF2 50A P8D8 P888 24-5 24-50 W22 W25 P6A8 AVIONICS BUS F3/XF3 02. 03.04 W20 - 1 ⚫ - P53A20 P54A20N BTIO BATTERY R34 SHUNT CR24 1 80A CII K15 BATTERY P8A4 FI/XFI MASTER -P8A4 CR25 RELAY BAT GND -P3816- F2 FI -P25A20- 5A ÞJPR2001 RED F31/XF31 -P25A20- STANDARD °° G18 ALTERNATOR AUX F22 WIT -P64A18- -] 24-31 GRN PI6A20 -] 33-10 A16 ALT OUT SENSOR -4-P20A20- 0-] 24-40 BLK PI8A2ON GS3 P80 J80 OFF -P4A20- 1529 BATTERY SWITCH • P5A20N- ON FF 91-15 - -P3A4N- -e-P64A18-] 24-31 AUX P25A20→ L SUBPANEL OPTIONAL 100 AMP ALT I 5A þ-P25A20→ F31/XF31 ♦2 G18 ALTERNATOR *2 REFER TO APPLICABLE AVIONICS DIAG FOR MODE OF CONNECTION. 03 WHEN OPTIONAL DUAL NAV IS USED REFER TO DIAG 24-51. 04 WHEN OPTIONAL SINGLE NAV IS USED REFER TO DIAG 24-52. . 4 USED ON ACFT WITH EXTERNAL POWER OPTION 3 USED ON ACFT CE-919. CE-923, CE-925 & CE-927 ONLY 2 WIRE AS SHOWN EA-158 ONLY 1 ON ACFT EA-6 & AFT NOT USED ON ACFT HAVING OPTIONAL CONTROL WHEEL CLOCK INSTALLED. REF DIAGRAM 25-12 REPLACES REF DIAGRAM 25-11. WIRE LENGTH MUST BE KEPT LESS THAN 3-INCHES. WIRE LENGTH MUST BE KEPT LESS THAN 6-INCHES. 24-30-03 Page 4 01/29/99 GS4 CE24F 982522AA ALTERNATOR (PRIOR TO INSTALLATION OF KIT 55-3025-1S) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (Configuration 1) REFERENCE DESIGNATOR PART NUMBER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL DESCRIPTION 24-30-03 (Configuration 1) USABLE INSTL ZONE CODE ON XF31 HDJ-A FUSEHOLDER-ALTERNATOR AUXILIARY OUTPUT (ALTN 410 1 FOR HHJ-A) XF31 HHJ-A
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FUSEHOLDER-ALTERNATOR AUXILIARY OUTPUT (ALTN 410 1 FOR HDJ-A) NOTE REFER TO THE ALTERNATOR (G18) INSTALLED IN THE AIRPLANE FOR THE CORRECT PART NUMBER. CODES OF EFFECTIVITY 1. E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (PRIOR TO INSTALLATION OF KIT 55-3025-1S) 2. CE-919, CE-923, CE-925 AND CE-927 (PRIOR TO INSTALLATION OF KIT 55-3025-1S) 3. E-1519 THRU E-1765; CE-862 THRU CE-928; D-10248 THRU D-10353; EA-6 THRU EA-158 (PRIOR TO INSTALLA- TION OF KIT 55-3025-1S) 24-30-03 Page 5 01/29/99 Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL 24-30-03 ALTERNATOR (AFTER INSTALLATION OF KIT 55-3025-1S) (Configuration 2) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 24-30-03 Page 1 01/29/99 -P8A4 B15 Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL • 3 F26\XF26 K3A2 STARTER 74-30 [-K2A20 P54 J54 W32A20 • 3 32 --] 91-02 91-19 CR20 P23A20N K14 START RELAY 24-33 24-34 [P33A16-01 PIC2 -] 24-40 P31A20 5A FI5/XF 15 E56A20 77-20 P29A20 5A E55A20 W24 F16/XF 15 50A F2/XF2 50A P8D8 P8B8 24-50 W22 W25 P6A8 AVIONICS BUS 02. 03.04 F3/XF3 25-11 [ -PITA18- -P2A4N- -ɖi|D-PIA2- W20 BTIO BATTERY R34 SHUNT • — P53A20 Ko P54A20N CR24 1 CII 80A K15 BATTERY MASTER RELAY P8A4 FI/XFI BATGND LP3816-F2 -P3A4N- P64A18-324-31 F AUX -P25A20 OPTIONAL 100 AMP ALT -P8A4 15A P25A20 CR25 F317XF31 G18 ALTERNATOR A16 ALT OUT SENSOR -◆4-P20A20- -] 24-40 -P25A20- 5A JPR201 F31/XF31 ♦2 RED -P25A20- 1 STANDARD °° AUX F2 22) G18 ALTERNATOR FIO WIT -P64A18- HK GRN - PI6A20 -] 33-10 BLK PI8A20N GS3 -] 24-31 P80 J80 OFF -P4A20 P5A20N- 1 $29. BATTERY SWITCH ON 91-15 - L SUBPANEL 05 -P3A4N- G18 BAT GO °° LP3816-F2 FI P64A18324-31- ALTERNATOR HIRED -P25A20- AUX; AUX P25A20 +5 OPTIONAL 100 AMP ALT STANDARD G18 ALTERNATOR -WIT -P64A18-24-31 •5 PC BOARD FUSE PER S.B. 2016 USED ON KIT 55-3025-IS PER S.B.2016 GS4 ◆4 USED ON ACFT WITH EXTERNAL POWER OPTION 3 USED ON ACFT CE-919, CE-923, CE-925 & CE-927 ONLY 2 WIRE AS SHOWN EA-158 ONLY 1 ON ACFT EA-6 & AFT NOT USED • ON ACFT HAVING OPTIONAL CONTROL WHEEL CLOCK INSTALLED. REF DIAGRAM 25-12 REPLACES REF DIAGRAM 25-11. ⚫ WIRE LENGTH MUST BE KEPT LESS THAN 3-INCHES. ° WIRE LENGTH MUST BE KEPT LESS THAN 6-INCHES. 02 REFER TO APPLICABLE AVIONICS DIAG FOR MODE OF CONNECTION. 03 WHEN OPTIONAL DUAL NAV IS USED REFER TO DIAG 24-51. 04 WHEN OPTIONAL SINGLE NAV IS USED REFER TO DIAG 24-52. CE24F 982548AA 24-30-03 Page 2 01/29/99 ALTERNATOR (AFTER INSTALLATION OF KIT 55-3025-1S) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (Configuration 2) REFERENCE DESIGNATOR PART NUMBER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL DESCRIPTION USABLE INSTL ZONE ON CODE A16 BT10 36-380000-3 36-380059-1 BT10 PS12-11 24-30-03 (Configuration 2) SENSOR-ALTERNATOR OUT BATTERY (ALTN FOR PS12-11) BATTERY (ALTN FOR 36-380059-1) 222 1 222 1 222 1 B15 MHJ-4003 MOTOR-STARTER (ALTN FOR 637847) 410 1 B15 637847 MOTOR-STARTER (ALTN FOR MHJ-4003) 410 1 CR20 1.5KE51CA TRANSZORB-START RELAY 222 1 CR24 1N4007 DIODE-BATTERY MASTER RELAY (SUPERSEDED BY 132408-22) 222 1 CR24 132408-22 DIODE-BATTERY MASTER RELAY (SUPERSEDES 222 1 1N4007) CR25 1N4007 DIODE-BATTERY MASTER (SUPERSEDED BY 132408- 222 1 22) CR25 132408-22 DIODE-BATTERY MASTER (SUPERSEDES 1N4007) 222 1 C11 39D507G050GL4 CAPACITOR-ALTERNATOR (OPTL) 410 3 F1 FLLB LIMITER-ELECTRIC, ALTERNATOR OUTPUT 222 1 F15 AGC5 F16 AGC5 FUSE-AMMETER FUSE-AMMETER 222 1 222 1 F2 FLLA LIMITER-ELECTRICAL BUS 222 1 F26 AGC5 FUSE-START ANNUNCIATOR (OPTL) 222 2 F3 FLLA LIMITER-AVIONICS BUS 222 1 F31 AGC5 FUSE-ALTERNATOR AUXILIARY OUTPUT 410 1 GS3 131270-3 GROUND STUD-FIREWALL 221 1 GS4 AN3-5A GROUND STUD-LOWER FIREWALL 222 G18 642056A2 ALTERNATOR, 100 AMP(W/ CLUTCH)(ALTN FOR ALV9407) 410 G18 641668 G18 ALT9422 G18 642056 ALTERNATOR, 50 AMP (ALTN FOR ALT9422) ALTERNATOR, 50 AMP (ALTN FOR 641668) ALTERNATOR, 100 AMP (WITHOUT CLUTCH) 410 410 1 410 1 G18 642056A2 J80 204814-1 ALTERNATOR, 100 AMP (WITH CLUTCH) RECEPTACLE-GROUNDING BLOCK 410 231 1 K14 6041H190 RELAY-START 222 1 K15 6041H189 RELAY-BATTERY MASTER 222 1 P80A 200838-3 PLUG-GROUNDING BLOCK 231 1 P80B 201224-1 STRAIN RELIEF 231 1 P80C 201328-1 SOCKET CONTACT 231 1 P80D 200333-1 P80E 203618-1 R34 MS91586-2 SOCKET CONTACT JACKSCREW SHUNT-50 AMP 231 1 231 1 131 1 R34 MS91586-6 SHUNT-100 AMP (OPTL) 222 1 S29 35-380053-21 SWITCH-BATTERY 240 1 W11 002-369014-3 BUS BAR-ALTERNATOR (USED WITH 50 AMP ALTERNA- 410 1 TOR) W20 36-364001-27 W22 W24 002-361016-7 36-364001-13 BUS BAR-SHUNT, AVIONICS LIMITER BUS BAR-SHUNT, ELECTRIC LIMITER 222 1 222 1 BUS BAR-START RELAY 222 1 W25 36-364001-19 BUS BAR-BATTERY MASTER 222 1 XF1 FSH LIMITER BASE 222 1 XF15 4532 FUSEHOLDER-AMMETER/CLOCK 222 1 XF2 FSH LIMITER BASE-ELECTRICAL BUS 222 1 XF26 60-369025-2 FUSEHOLDER-START ANNUNCIATOR LIGHT 222 2 XF3 FSH LIMITER BASE-AVIONICS BUS 222 1 24-30-03 Page 3 01/29/99 -P8A4 B15 STARTER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL +3 F26\XF26 K3A2 P54 J54 W32A20 ♦ 3 32 ---] 91-02 91-19- 74-30-1 K2A20 CR20 P23A20N K14 START RELAY • 24-33 [P33A16-01 24-34 PIC2 4 -] 24-40 P31A20 P29A20 5A FIBAFIS 5A E56A20 77-20 E55A20 W24 F16/XF15 P8D8 50A F2/XF2 50A P8B8 -] 24 24-50 W22 W25 P6A8 AVIONICS BUS F3/XF3 02.03.04 25-11 [ PIIA18- -P2A4N—ɖ|I|D-P1A2- W20 BTIO BATTERY R34 SHUNT • P53A20 Ko P54A20N CR24 CII 80A K15 P8A4 BATTERY FI/XFI MASTER BATGND LP3816-F2 Fi -P3A4N- -P64A18-324-31 AUX P25A20 15A P25A20+ CR25 RELAY -P25A20- 5A JPR2001 RED F31/XF31 -P25A20- Ο AUX F2 F22) FIO G18 ALTERNATOR WII -P64A18-24-31 STANDARD GRN - PI6A20 -] 33-10 A16 ALT OUT SENSOR BLK PI8AZON GS3 OPTIONAL 100 AMP ALT F31/XF31 2 G18 -4-P20A20- ALTERNATOR -] 24-40 P80 J80 OFF -P4A20- P5A20N- FF | $29 BATTERY SWITCH L SUBPANEL ON 91-15 -- P8A4 +5 -P3A4N- G18 BAT GND °° LP3816 F2 -P64A18324-31- ALTERNATOR F RED -P25A20- AUX AUX P25A20 +5 OPTIONAL 100 AMP ALT STANDARD G18 ALTERNATOR WII -P64A18-24-31 ♦5 PC BOARD FUSE PER S.B. 2016 USED ON KIT 55-3025-IS PER S.B.2016 GS4 4 USED ON ACFT WITH EXTERNAL POWER OPTION 3 USED ON ACFT CE-919, CE-923. CE-925 & CE-927 ONLY 2 WIRE AS SHOWN EA-158 ONLY ⚫ 1 ON ACFT EA-6 & AFT NOT USED . ON ACFT HAVING OPTIONAL CONTROL WHEEL CLOCK INSTALLED. REF DIAGRAM 25-12 REPLACES REF DIAGRAM 25-11. WIRE LENGTH MUST BE KEPT LESS THAN 3-INCHES. WIRE LENGTH MUST BE KEPT LESS THAN 6-INCHES. 02 REFER TO APPLICABLE AVIONICS DIAG FOR MODE OF CONNECTION. 03 WHEN OPTIONAL DUAL NAV IS USED REFER TO DIAG 24-51. 04 WHEN OPTIONAL SINGLE NAV IS USED REFER TO DIAG 24-52. CE24F 982548AA 24-30-03 Page 4 01/29/99 ALTERNATOR (AFTER INSTALLATION OF KIT 55-3025-1S) E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (Configuration 2) REFERENCE DESIGNATOR PART NUMBER Raytheon Aircraft BEECH BONANZA WIRING DIAGRAM MANUAL DESCRIPTION USABLE INSTL ZONE CODE ON 24-30-03 (Configuration 2) FUSEHOLDER-ALTERNATOR AUXILIARY OUTPUT (ALTN FUSEHOLDER-ALTERNATOR AUXILIARY OUTPUT (ALTN FOR HDJ-A) XF31 HDJ-A FOR HHJ-A) XF31 HHJ-A Y1A Y1B 55-3025-1S Y1C 58-360006-1 Y1D 58-361015-1 Y1E WF2K10R Y1F 9505-08 THE FOLLOWING COMPONENTS ARE PART OF KIT 55-3025-1S AND COMPLY WITH S.B. 2016. KIT, PRINTED CIRCUIT BOARD FUSE ASSEMBLY (CON- SISTS OF PARTS AND INSTRUCTIONS TO INSTALL A PRINTED CIRCUIT BOARD FUSE DIRECTLY ON THE AUXILIARY OUTPUT TERMINAL OF THE ALTERNATOR) ALTERNATOR CONTROL RESISTOR ASSEMBLY- ALTERNATOR FUSE (A COMPONENT PART OF KIT 55-3025-1S) (SUPERSEDES 58-361014-1) PRINTED CIRCUIT BOARD (A COMPONENT PART OF KIT 55-3025-1S) RESISTOR, FUSIBLE (A COMPONENT PART OF KIT 55-3025-1S) NUTSERT (A COMPONENT PART OF KIT 55-3025-1S) NOTE REFER TO THE ALTERNATOR (G18) INSTALLED IN THE AIRPLANE FOR THE CORRECT PART NUMBER. CODES OF EFFECTIVITY 410 1 410 1 1. E-1519 THRU E-1765; CE-862 THRU CE-928; CJ-150 THRU CJ-155; D-10248 THRU D-10353; EA-6 THRU EA-158 (AFTER INSTALLATION OF KIT 55-3025-1S) 2. CE-919, CE-923, CE-925 AND CE-927 (AFTER INSTALLATION OF KIT 55-3025-1S) 1 1 1 1 1 3. E-1519 THRU E-1765; CE-862 THRU CE-928; D-10248 THRU D-10353; EA-6 THRU EA-158 (AFTER INSTALLATION OF KIT 55-3025-1S) 24-30-03 Page 5 01/29/99