GRIMES AEROSPACE COMPANY

550 STATE ROUTE 55

URBANA, OHIO 43078

TO: HOLDERS OF COMPONENT MAINTENANCE MANUAL 33-40-59 FOR THE AIRCRAFT

NAVIGATIONAL LIGHT ANTI-COLLISION, FLASHTUBE, PART NUMBER 30-1033-ALL.

REVISION NO. 5 DATED FEBRUARY 1/06

HIGHLIGHTS

Pages which have been added or revised are outlined below together with the highlights of the revision.
Remove and insert the affected pages as listed and enter Revision No. 5 dated Feb 15/06 on the Record of
Revisions Sheet.

Page No. Description of Change Effectivity

T-1 Revised date. All Models

RR-1 Revised to reflect this revision. All Models

LEP-1 Revised to reflect this revision. All Models

101 Changed Variable Regulated Power Supply Part/Model Number and Cleaning All Models
Cloth Specification numbers. Added Adhesive (AD-053) to Materials List Table.

102 Added steps to make adjustment for flash rate and correct output power and to All Models
apply adhesive to potentiometer adjustment screws.

103 Table 103 text rolled to this page. All Models

301 Changed Cleaning Cloth Specification number. All Models

401 Changed Materials List Nomenclature and Specification numbers. Updated All Models
steps for Cleaning Procedures.

501, 601 Changed Cleaning Cloth Specification number. All Models

603-612 Removed steps for Surface Treatment Procedure which caused text to roll. All Models

606 Reversed contact part numbers in NOTE. All Models

613 Updated Grimes Aerospace Co. address and phone number. All Models

701 Deleted unneeded Table text reference and changed Cleaning Cloth All Models
Specification number.

702-707 Added text and tables for application of sealing compound (AD-330). All Models

708 Text rolled due to new tables added to previous pages. All Models

901 Changed Part/Model Number for Variable Regulated Power Supply. All Models

1005 Updated Grimes Aerospace Co. address and phone number. All Models

Highlights Page
33-40-59 Feb 1/06
 GRIMES AEROSPACE COMPANY
550 STATE ROUTE 55
URBANA, OHIO 43078

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PARTS LIST

AIRCRAFT NAVIGATIONAL LIGHT ANTI-COLLISION, FLASHTUBE

PART NUMBER(S)

30-1033-1 30-1033-19 30-1033-35 30-1033-53

30-1033-3 30-1033-21 30-1033-37 30-1033-55
30-1033-5 30-1033-23 30-1033-39 30-1033-57
30-1033-7 30-1033-25 30-1033-41 30-1033-59
30-1033-11 30-1033-27 30-1033-43 30-1033-61
30-1033-13 30-1033-29 30-1033-45 30-1033-63
30-1033-15 30-1033-31 30-1033-49 30-1033-65
30-1033-17 30-1033-33 30-1033-51 30-1033-67

This document and all information and expression

contained herein are the property of AlliedSignal Inc., are
loaned in confidence, and may not, in whole or in part, be
used, duplicated, or disclosed for any purpose without
prior written permission of AlliedSignal Inc. All rights
reserved.

Page T-1
33-40-59 Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

RECORD OF REVISIONS

Retain this record in the front of the manual. On receipt of revisions, insert revised pages in manual. Enter
revision number, date issued, date inserted and initials.

REV. DATE DATE REV. DATE DATE

NO. ISSUED INSERTED BY NO. ISSUED INSERTED BY

1 12/15/75 12/15/75 GMC

2 3/1/78 3/1/78 GMC

3 10/1/83 10/1/83 MRC

4 9/15/99 9/15/99 GAC

5 2/1/06

33-40-59 Page RR-1/RR-2

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

RECORD OF TEMPORARY REVISIONS

REV. ISSUE DATE DATE REV. ISSUE DATE DATE

NO. DATE INSRTD BY REMVD BY NO. DATE INSRTD BY REMVD BY

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Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

SERVICE BULLETIN LIST

SERVICE BULLETIN REVISION DATE BULLETIN

NUMBER NUMBER INCORPORATED INTO MANUAL

TIL 60 3/1/78

30-1033-33-0095 11/30/93

30-1033-33-SB01 1 1/15/98

30-1033-33-SB02 1 10/15/98

30-1033-33-SB03 4 9/15/99

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE

Title Page T-1 Feb 1/06 Assembly (Including 701 Feb 1/06
Record of Revisions RR-1 Feb 1/06 Storage) 702 Feb 1/06
RR-2 Blank 703 Feb 1/06
Record of Temporary RTR-1 Sep 15/99 704 Feb 1/06
Revisions RTR-2 Blank 705 Feb 1/06
Service Bulletin List SBL-1 Sep 15/99 706 Feb 1/06
SBL-2 Blank 707 Feb 1/06
List of Effective LEP-1 Feb 1/06 708 Feb 1/06
Pages LEP-2 Blank Special Tools, Fixtures 901 Feb 1/06
Table of Contents TC-1 Sep 15/99 and Equipment 902 Blank
TC-2 Blank Illustrated Parts List 1001 Sep 15/99
Introduction INT-1 Sep 15/99 1002 Sep 15/99
INT-2 Blank 1003 Sep 15/99
Description and 1 Sep 15/99 1004 Sep 15/99
Operation 2 Sep 15/99 1005 Feb 1/06
3 Sep 15/99 1006 Sep 15/99
4 Blank 1007 Sep 15/99
Testing and 101 Feb 1/06 1008 Sep 15/99
Fault Isolation 102 Feb 1/06 1009 Sep 15/99
103 Feb 1/06 1010 Sep 15/99
104 Sep 15/99 1011 Sep 15/99
105 Sep 15/99 1012 Sep 15/99
106 Blank 1013 Sep 15/99
Disassembly 301 Feb 1/06 1014 Sep 15/99
302 Sep 15/99 1015 Sep 15/99
303 Sep 15/99 1016 Sep 15/99
304 Blank 1017 Sep 15/99
Cleaning 401 Feb 1/06 1018 Sep 15/99
402 Blank 1019 Sep 15/99
Check 501 Feb 1/06 1020 Sep 15/99
502 Sep 15/99 1021 Sep 15/99
Repair 601 Feb 1/06 1022 Sep 15/99
602 Sep 15/99 1023 Sep 15/99
603 Feb 1/06 1024 Sep 15/99
604 Feb 1/06 1025 Sep 15/99
605 Feb 1/06 1026 Sep 15/99
606 Feb 1/06 1027 Sep 15/99
607 Feb 1/06 1028 Sep 15/99
608 Feb 1/06 1029 Sep 15/99
609 Feb 1/06 1030 Sep 15/99
610 Feb 1/06 1031 Sep 15/99
611 Feb 1/06 1032 Sep 15/99
612 Feb 1/06 1033 Sep 15/99
613 Feb 1/06 1034 Blank
614 Blank

33-40-59 Page LEP-1/LEP-2

Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

TABLE OF CONTENTS

SUBJECT PAGE

Introduction ................................................................................................................................................. INT-1

Description and Operation ................................................................................................................................. 1

Testing and Fault Isolation ............................................................................................................................. 101

Automatic Test Requirements (ATLAS) ....................................................................................... Not Applicable

Disassembly ................................................................................................................................................... 301

Cleaning ......................................................................................................................................................... 401

Check ............................................................................................................................................................. 501

Repair ............................................................................................................................................................. 601

Assembly (Including Storage) ........................................................................................................................ 701

Fits and Clearances ..................................................................................................................... Not Applicable

Special Tools, Fixtures and Equipment ......................................................................................................... 901

Illustrated Parts List ..................................................................................................................................... 1001

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Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

INTRODUCTION

This publication contains shop maintenance instructions with Illustrated Parts List (IPL) for the Aircraft
Navigational Light Anti-collision, Flashtube, part number 30-1033-ALL, manufactured by Grimes Aerospace
Company and hereafter referred to as the navigational light.

Service Bulletin 30-1033-33-SB03 introduces modifications to navigational lights PN 30-1033-61 and

30-1033-63 that change them, respectively, to PN 30-2675-1 and to PN 30-2676-1, CMM 33-42-21.

The instructions in this publication provide information necessary to do maintenance functions ranging from
simple checks and replacement to complete shop-type repair.

The instructions only apply to the navigational light part number listed above. Be sure the part number on the
navigational light is listed on the title page before performing any of these instructions.

This publication is written to the Air Transportation Association of America (ATA) Specification Number 100
and will be revised as necessary to show current information.

This publication is divided into sections as shown in the preceding Table of Contents. Also refer to the Table
of Contents for page location of each applicable section.

An explanation of how to use the Illustrated Parts List (IPL) is provided in the introduction of that section.

The following sections of this publication have been verified on the date(s) specified. Where actual
performance of the functions (tasks) cannot be performed prior to issuing a manual, those functions (tasks)
shall be verified by simulation. Any function (task) verified by simulation must be verified by actual
performance at the earliest possible time.

VERIFIED SECTION VERIFICATION DATE

Testing and Fault Isolation Verified by performance: August 13, 1999

Disassembly Verified by performance: August 13, 1999
Assembly Verified by performance: August 13, 1999

33-40-59 Page INT-1/INT-2

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

DESCRIPTION AND OPERATION

1. Description. (See Figure 1)

A. The navigational light is installed on aircraft to provide a flashing source of high-intensity illumination
to indicate aircraft position.

B. The navigational light uses a flashtube lamp assembly to provide illumination. The flashtube lamp
assembly fires at a rate of 40 to 60 flashes per minute and uses a parabolic reflector to control the
emitted light pattern. The flashtube lamp assembly is protected by a heat-resistant glass lens. The
glass lens provides the specified aviation color as per MIL-C-25050.

C. The navigational light has a Printed Circuit Board (PCB) assembly that provides voltage limiting,
timing and anti-afterglow circuitry.

2. Operation.

A. The navigational light requires a 28 Vdc input (Figure 2) from the aircraft electrical system. The
voltage is applied to the power conversion circuit. The output of the power conversion circuit is
applied to both the storage capacitors and control circuit. The control circuit is made up of voltage
limiting, timing and anti-afterglow circuits. The timing circuit provides a trigger to the flashtube, which
fires and provides a flashing source of illumination.

B. The 28 Vdc input is applied to the primary winding of transformer T1 (Figure 3) through choke L1.
Zener diode VR1 and capacitor C2 provide a 10 Vdc reference voltage to the timing and anti-
afterglow circuits.

C. The induced voltage on the secondary winding of T1 is applied to storage capacitors C9, C10, C11
and C12. These capacitors charge to 430-570 Vdc and discharge through the flashtube lamp DS1
to produce a 27 Joule, minimum, flash.

Aircraft Navigational Light Anti-Collision, Flashtube

Figure 1

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

D. A positive pulse is developed at operational amplifier U2 pin 2. The pulse is applied to the gate of a
Silicon Controlled Rectifier (SCR). SCR1 fires, discharging capacitor C7 through transformer T2,
which results in the storage caps discharging through DS1. Potentiometer R26 controls the timing of
the firing rate of flashtube lamp DS1. Potentiometer R26 and resistor R11 provide voltage limiting
for the PCB assembly.

Navigational Light Block Diagram

Figure 2

3. Leading Particulars. (Refer to Table 1)

Table 1. Leading Particulars

DESCRIPTION DATA

Dimensions:
Width ..................................................................................................................... 5.25 inches (133,4 mm)
Height PN 30-1033-1 through -55, -59 through -67 ............................................. 6.76 inches (171,7 mm)
PN 30-1033-57 ......................................................................................... 6.60 inches (167,6 mm)
Weight (approx) PN 30-1033-1 through -55, -59 through -67 ...................................... 2.75 pounds (1,25 kg)
PN 30-1033-57 ...................................................................................3.09 pounds (1,40 kg)
Operating Ranges:
Voltage ............................................................................................................................................. 28 Vdc
Brightness ................................................................................................................... 27 Joules, minimum

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

CR6 CR7
RED
+ 5 3
L1 C3 TPJ
ORN R1 R19 R20 T1 C14
1
VR1 R2 R5 R12 R14
R4 R13 Q2
R15 C9 + + C11
7 11 Q1 Q3
+ + 13 CR2
1 R23
U1 R6 CR3 10
U1 R21 CR9 DS1
- -
6 CR4 C10 + + C12 GREEN
C1 + C2 + R26 R11
R7 SCR1
R3 R9 R16 R17 C13 C7
T2
R22
R8 CR1

R28
5
+ CR5 4 R27
2 CR8
4 U1 R25 R24
- R10
+ + C4 + C5 + C15
C8 6
BLK
BLK
M32045

Navigational Light Schematic

Figure 3

33-40-59 Page 3/4

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

TESTING AND FAULT ISOLATION

1. General Information.

A. The following paragraphs provide information for testing and fault isolation of the navigational light.

B. Conduct all tests at a temperature of 65 to 85 °F (18 to 29 °C) and in the order presented, unless
otherwise noted. Failure of any test is cause for failure of the navigational light. Correct the fault
before testing is continued.

C. Refer to Table 101 for a list of special tools, fixtures and equipment needed for testing and fault
isolation. Refer to Table 102 for a list of materials needed for testing and fault isolation. Equivalent
substitutes are acceptable.

Table 101. Special Tools, Fixtures and Equipment List

NOMENCLATURE PART/MODEL USED FOR FIGURE

NUMBER NUMBER
Digital Multimeter Model 87 Testing and NA
(DMM) Fluke Corporation Fault Isolation
Everett, WA
(V02WJ6)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation
(0-45 Vdc, 6 amp min)

Table 102. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available
Adhesive (AD-053*) 162 General Electric Co.
Auburn, NY (V09214)
* Grimes Reference Only

2. Pretest Procedures.

A. Review any shipping tags or forms to determine cause for removal from aircraft.

B. Wipe the navigational light with a clean cloth to remove any dust, dirt or foreign material.

C. Visually inspect the navigational light for signs of missing, broken, bent or cracked parts. Damaged
parts shall be replaced before the navigational light is tested.

3. Test Setup.

A. Connect DMM positive lead to positive output terminal of DC power supply.

B. Connect DMM negative lead to negative output terminal of DC power supply.

C. Connect the DC power supply to the navigational light as follows:

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

(1) For models 30-1033-1, -11, -13, -19, -21, -35, -39, -51, -65 and -67, connect DC power supply
positive output to pin A and negative lead to pin B of input connector.

(2) For models 30-1033-3, -7, -23, -25, -27, -29, -33, -37, -41, -43, -49, -53, -55, -57, -59, -61 and
-63, connect DC power supply positive output to pin A and negative lead to pin C of input
connector.

(3) For models 30-1033-5 and -31, connect DC power supply positive output to positive terminal
and negative lead to negative terminal of input terminal board.

(4) For models 30-1033-15, -17 and -45, connect DC power supply positive output to red wire of
the power conversion circuit and negative lead to black wire of the power conversion circuit.

4. Testing.

A. Set DC power supply power switch to ON position and adjust for 28 Vdc output. The navigational
light will flash at a rate of 40-60 flashes per minute.

B. If the flash rate is not 40-60 flashes per minute, adjust potentiometer R26 (IPL Figure 3, 135) until
flash rate is correct.

C. Adjust potentiometer R16 (130) to set voltage level for correct output power of 27 to 29 joules.

WARNING: ADHESIVE IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

D. Apply adhesive (AD-053) to the adjustment screws of potentiometers R16 (130) and R26 (135).
Wipe excess with clean cloth. Allow adhesive to cure for four hours at room temperature.

E. Set DC power supply power switch to OFF position.

F. Disconnect the DC power supply from the navigational light.

5. Post Test Procedures.

A. If navigational light passed all the tests, prepare it for shipment or storage. Refer to ASSEMBLY,
section 701, for details.

B. If navigational light did not pass all the tests, repair or replace defective parts, then repeat all tests.
Refer to Fault Isolation, paragraph 6, for details.

6. Fault Isolation. (Refer to Table 103)

NOTE: Refer to the IPL for illustrations of the navigational light. Numbers in parentheses ( ) refer
to item numbers on the illustration.

A. Measure test points on PCB as indicated by Table 103.

B. When measuring signals at test points, set oscilloscope to NON-INVERTING. Set the VOLTS/DIV
and TIME/DIV settings as specified for each test point.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 103. Fault Isolation

FAULT PROBABLE CAUSE CORRECTIVE ACTION

Navigational light does not flash. Bad quartz flashtube Replace quartz flashtube (30).
(30, IPL Figure 4). Refer to REPAIR, section 601,
for detailed instructions.
Defective wiring harness. Repair wiring harness. Refer to
REPAIR, section 601, for detailed
instructions.
Defective component(s). Troubleshoot navigational light.
Refer to Figures 3 and 101 for
troubleshooting information.

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Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Troubleshooting Guide (Sheet 1 of 2)

Figure 101

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Troubleshooting Guide (Sheet 2 of 2)

Figure 101

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Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

DISASSEMBLY

1. General Information.

A. The following paragraphs provide information for disassembly of the navigational light.

B. Disassemble only to the extent required to replace defective parts, unless complete overhaul is
required. Before disassembly, wipe exterior surfaces with a clean cloth to remove dust, dirt or other
foreign materials.

C. Do not remove threaded inserts. Refer to CHECK, section 501, for details.

D. Do not disassemble riveted parts. Refer to REPAIR, section 601, to determine whether part(s) can
be replaced.

E. Do not remove electrical wires unless repair or replacement is required. Tag electrical wires before
removal.

F. Refer to Table 301 for a list of materials needed for disassembly. Equivalent substitutes are
acceptable.

Table 301. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available

2. Disassembly of Navigational Light.

NOTE: Refer to IPL Figure 2 for an illustration of the navigational light. Numbers in parentheses ( )
refer to item numbers on the illustration.

A. Remove the lens assembly (-20) as follows:

(1) For all models, except 30-1033-27, perform following steps:

(a) Remove three screws (15) and lens retainer (10) from housing (330).

(b) Remove lens assembly (-20) and gasket (65) from housing (330).

(2) For model 30-1033-27, perform following steps:

(a) Remove retainer band (-10A) and lens assembly (-20) from housing (330).

(b) Remove three screws (115), mounting ring (110) and gasket (105) from housing (330).

B. Disassemble the lens assembly (-20) as follows:

(1) Remove screw (25), lockwasher (30), drain tube (35 or -35A) and washer (50) from lens (60).

(2) Remove threaded insert (40) and teflon washer (45) from lens (60).

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

CAUTION: THIS HALOGEN CYCLE LAMP IS PRESSURED AND MAY SHATTER. DO NOT
OPERATE IN EXCESS OF RATED VOLTAGE. PROTECT LAMP AGAINST
ABRASIONS AND SCRATCHES. REMOVE GREASE OR FINGERPRINTS WITH A
GREASE-FREE SOLVENT. WEAR PROTECTIVE EYEGLASSES AND CLOTHING
WHEN HANDLING LAMP. TURN POWER OFF WHEN INSTALLING AND ALLOW
TO COOL BEFORE REMOVING. DISPOSE OF LAMP WITH CARE.

C. Remove flashtube lamp assembly (DS1) (100) from housing (330) as follows:

(1) Mark wires and ring terminals attached to flashtube lamp assembly (DS1) (100) with location
information.

(2) Remove wires and ring terminals from flashtube lamp assembly (DS1) (100).

D. Remove the mounting flange (125) or adapter (-125C) as follows:

NOTE: Models 30-1033-21, -25 and -45 do not have gasket.

(1) Remove gasket (120) from mounting flange (125) or adapter (-125C).

NOTE: All models except 30-1033-21 and -25 have mounting flange. Model 30-1033-21
has an adapter. Model 30-1033-25 does not have a mounting flange or adapter
installed.

(2) Remove sealing compound from three screws (130).

(3) Remove three screws (130) and mounting flange (125) or adapter (-125C) from housing (330).

E. Disassemble the light subassembly (-1 or -2) as follows:

(1) Remove the base (265) and Printed Circuit Board (PCB) assembly (275) from housing (330) as
follows:

(a) Remove sealing compound from three screws (270) and seam where base (265) meets
housing (330).

(b) Remove three screws (270), one screw (295), PCB assembly (275) and base (265) from
housing (330).

(2) Remove sealing compound from four screws (325).

(3) Remove four screws (305), two retainer assemblies (300) and two capacitor assemblies
(-310A) from housing (330).

(4) Remove sealing compound from screws (280 and 290) that secure the base (265) to PCB
assembly (275) brackets.

NOTE: Models 30-1033-1 through -27 use a screw and nut to secure PCB assembly
bracket to base. All other models have nutplate installed on bracket.

(5) For models 30-1033-1 through -27, remove screw (280), nut (285) and screw (290) that secure
PCB assembly (275) brackets to base.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

(6) For all other models, remove screw (280) and screw (290) that secure PCB assembly (275)
brackets to base.

F. Remove sealing compound residue from housing (330), base (265) and mounting flange (125) or
adapter (-125C). Refer to CLEANING, section 401, for details

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Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

CLEANING

1. General Information.

A. The following paragraphs provide information for cleaning the navigational light.

B. Refer to Table 401 for a list of materials needed for cleaning. Equivalent substitutes are acceptable.

Table 401. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Aqueous Cleaner Armakleen M-HP II Safety Kleen Systems, Inc.
Columbia, SC (V30530)
Cleaning Cloth A-A-59323 Commercially Available
Soft, Natural Bristle Brush None Commercially Available
Sharp Knife None Commercially Available

2. Cleaning Procedures.

NOTE: Refer to IPL Figure 2 for an illustration of the navigational light. Numbers in parentheses ( )
refer to item numbers on the illustration.

A. Clean metal parts in aqueous cleaner. Use a soft, natural bristle brush to remove ground-in
deposits.

B. Use sharp knife to remove sealing compound residue from housing (330), base (265) and mounting
flange (125) or adapter (-125C). Make a clean cloth moist with aqueous cleaner and use it to
remove the remaining adhesive/sealant residue from parts.

C. Except for printed circuit boards, clean electrical parts with a clean cloth dipped in aqueous cleaner
to remove dirt, dust, and unwanted material.

D. Clean printed circuit boards with a dry, clean cloth to remove dirt or dust.

WARNING: WHEN YOU USE COMPRESSED AIR, KEEP THE AIR PRESSURE AT OR BELOW
30 PSI (207 KPA). IF YOU DO NOT OBEY THIS RECOMMENDATION, THERE IS A
RISK OF INJURY OR DEATH.

E. Dry the parts with compressed air or clean with a clean cloth and dry the parts in the air.

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Feb 1/06
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

CHECK

1. General Information.

A. The following paragraphs provide information for a check of each part in the navigational light.

B. Complete checks in accordance with the standard requirements and checks listed in the following
paragraphs, unless otherwise specified.

C. Refer to Table 501 for a list of materials needed for checks. Equivalent substitutes are acceptable.

Table 501. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available

2. Standard Requirements.

A. Clean the parts before performing any check. Refer to CLEANING, section 401, for details.

B. Use 2X magnification and an amplified light to check the parts.

C. Repair or replace the parts that exceed limits. Refer to REPAIR, section 601, for details. Use parts
within limits for assembly. Refer to ASSEMBLY, section 701, for details.

3. Standard Checks.

NOTE: Refer to IPL Figure 2 for an illustration of the navigational light. Numbers in parentheses ( )
refer to item numbers on the illustration.

A. Examine parts for nicks, gouges, scratches or small burrs. If any are deeper than 0.03 inch
(0,76 mm), replace part. Minor damage may be repaired.

B. Examine parts for corrosion. If deeper than 0.03 inch (0,76 mm) or more than 20 percent of surface
is damaged, replace part. Minor damage may be repaired.

C. Examine painted parts for scratches, peeling, flaking or chipping. If more than 20 percent of surface
is damaged, replace part. Minor damage may be repaired.

D. Examine threaded parts with a thread gage for distortion or stripping. If not a Class 3 fit, replace
part.

E. Examine threaded inserts for stripping and tight fit. If damaged or loose, replace part.

F. Examine electrical parts for cracks, distortion, bent pins or signs of burned connections. If damaged,
replace parts.

G. Examine electrical wires for cracks, breaks or deterioration of insulation. If damaged, replace wires.

H. Examine lens (60) for cracks. If damaged, replace lens (60).

I. Examine drain tubes (35 or 195) for debris. Clean as required.

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PART NUMBER 30-1033

J. Examine guide (320) for distortion or cracks. If damaged, replace guide (320).

K. For model 30-1033-49, inspect lens assembly (-20) and navigational light to ensure Service Bulletin
SB 30-1033-33-0095 procedures have been performed.

L. For model 30-1033-59, inspect navigational light to ensure Service Bulletin 30-1033-SB01
procedures have been performed.

M. For models 30-1033-61 and -63, inspect Printed Circuit Board (PCB) assembly (275) to ensure
Service Bulletin 30-1033-33 SB02 procedures have been performed.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

REPAIR

1. General Information.

A. The following paragraphs provide information for repair of parts in the navigational light.

B. Limit repair procedures to correction of minor defects or damage, paint touch-up and replacement of
parts. Refer to CHECK, section 501, for details.

CAUTION: HEAT SENSITIVE PARTS. USE A HEAT SINK; APPLY HEAT FOR A MAXIMUM OF
10 SECONDS AT A TEMPERATURE NOT TO EXCEED 300 °F (149 °C) TO AVOID
DAMAGE.

C. Apply solder in accordance with MIL-STD-454. Remove excess with a clean cloth.

D. Use conformal coating to seal solder connections and electronic parts in accordance with
MIL-STD-275.

E. Use same color and type to replace electrical wires. Strip insulation 0.25 inch (6,35 mm). Use solder
to tin end, then attach to another component.

F. Install rivets in accordance with MIL-R-47196.

CAUTION: DO NOT USE CROCUS CLOTH ON ALUMINUM PARTS. CLOTH CONTAINS IRON
OXIDE, WHICH CAUSES RAPID OXIDATION OF ALUMINUM.

G. Use aluminum oxide abrasive cloth on aluminum parts. Use crocus cloth on steel parts

H. Refer to Table 601 for a list of materials needed for repair. Equivalent substitutes are acceptable.

Table 601. Materials List (Sheet 1 of 3)

NOMENCLATURE SPECIFICATION MANUFACTURER

Aluminum Oxide Abrasive Cloth P-C-451 (400 grade) Commercially Available
Cable M27500-20RC2506 Commercially Available
Cement Weldwood Contact Cement Commercially Available
Cleaning Cloth A-A-59323 Commercially Available
Conformal Coating MIL-I-46058, Type AR Commercially Available
Contact M39029/58-396 Commercially Available
Contact M39029/4-110 Commercially Available
Contact M39029/4-111 Commercially Available
Crocus Cloth P-C-458 (600 grade) Commercially Available
Electrical Solder SN63 WRMAP-3 Commercially Available
Heat Shrink Tubing M23053/4-201-0 Commercially Available

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PART NUMBER 30-1033

Table 601. Materials List (Sheet 2 of 3)

NOMENCLATURE SPECIFICATION MANUFACTURER

Heat Shrink Tubing M23053/5-104-0 Commercially Available
Masking Tape 0.75 in. (19 mm) wide Commercially Available
Paint (PA-5992*) MIL-C-85285, color 16492 Commercially Available
Paint (PA-826*) P-7033-A Vanguard Paints and Finishes, Inc.
Marrietta, OH
(V63717)
Primer (PR-1055*) 515X336 base Courtaulds Aerospace
910X458 catalyst Mojave, CA
(V85570)
Primer (PR-104*) Fed Spec. TT-P-1757 Commercially Available
Sealant SWS-835 Stauffer SWS Silicones
Matawan, NJ
(V07607)
Sealing Compound (AD-330*) MIL-S-8802 Commercially Available
Seal Plug MS27488-20 Commercially Available
Solder Shield M83519/1-4 Commercially Available
Splice M33519/1-1 Commercially Available
Ring Terminal 31879 Amp, Inc.
Middletown, PA (V00779)
Ring Terminal (TE-089*) 36151 Amp, Inc.
Middletown, PA (V00779)
Ring Terminal (TE-145*) 36149 Amp, Inc.
Middletown, PA (V00779)
Ring Terminal (TE-190*) 36158 Amp, Inc.
Middletown, PA (V00779)
Tape (TT-260*) 1.0 in. (25,4 mm) wide, Commercially Available
insulation, vinyl, pressure
sensitive rubber adhesive - non
thermosetting, black 7/10 mils
overall thickness
Thinner (PA-090*) Xylene Vanguard Paints and Finishes, Inc.
Marrietta, OH (V63717)
Ty-Rap MS3367-4-4 Commercially Available
Wash Primer (PR-124*) MIL-C-8514 Commercially Available
Wire (WI-256*), Red and Black MIL-W-22759/16 Commercially Available
*Grimes reference only.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 601. Materials List (Sheet 3 of 3)

NOMENCLATURE SPECIFICATION MANUFACTURER

Wire (WI-292*), Red MIL-W-16878/5 Commercially Available
Wire M22759/34-200 Commercially Available
*Grimes reference only.

2. Standard Repair Procedures.

CAUTION: DO NOT CHANGE SURFACE FINISH OR PART SHAPE, OR EXCEED WEAR LIMITS.
FAILURE TO COMPLY CAN RESULT IN PREMATURE FAILURE OF THE PART.

A. Remove minor surface corrosion with correct abrasive cloth for material.

B. Remove nicks, gouges, scratches or small burrs as follows:

(1) Remove any raised material with a very fine file.

(2) Blend damaged area into adjacent surfaces.

(3) Polish areas with correct abrasive cloth for material.

3. Surface Finish Procedure. This procedure shall be used for touch-up of scratches and minor surface
defects. If complete surface finish is required, replace part.

A. Repair area, if required. Refer to Standard Repair Procedures, paragraph 2, for details.

B. Apply chemical film to surface, if required. Refer to Surface Treatment Procedure, paragraph 3, for
details.

C. If not already done, cover areas not to be treated with masking tape.

D. For models 30-1033-23, -41 and -43, apply surface finish as follows:

WARNING: PRIMER IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

(1) Apply wash primer (PR-124) as follows:

(a) Mix and thin wash primer in accordance with manufacturer’s instructions.

(b) Apply one coat of wash primer to damaged area with a brush. Allow to air dry four hours.

(c) When dry, check finish is smooth and free of defects.

WARNING: PRIMER IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

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(2) Apply yellow zinc chromate primer (PR-104) as follows:

(a) Mix and thin yellow zinc chromate primer in accordance with manufacturer’s instructions.

(b) Apply one coat of yellow zinc chromate primer to damaged area with a brush. Allow to air
dry four hours.

(c) When dry, check finish is smooth and free of defects.

WARNING: PAINT IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

(3) Apply olive drab paint (PA-826) as follows:

(a) Mix and thin paint in accordance with manufacturer’s instructions. Use xylene thinner for
thinning paint.

(b) Apply one coat of paint to damaged area with a brush. Allow to air dry four hours.

(c) When dry, apply a second coat of paint. Allow to air dry four hours.

(d) When dry, remove masking tape and check finish is smooth, free of defects and blends
into other surfaces.

E. For models 30-1033-61 and -63, apply surface finish as follows:

WARNING: PRIMER IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

(1) Apply primer (PR-1055) as follows:

(a) Mix and thin primer in accordance with manufacturer’s instructions.

(b) Apply one coat of primer to damaged area with a brush. Allow to air dry four hours.

(c) When dry, check finish is smooth and free of defects.

WARNING: PAINT IS FLAMMABLE AND TOXIC TO EYES, SKIN AND RESPIRATORY

TRACT. SKIN AND EYE PROTECTION REQUIRED. AVOID REPEATED OR
PROLONGED CONTACT. USE ONLY IN WELL-VENTILATED AREAS. KEEP
AWAY FROM OPEN FLAMES OR OTHER SOURCES OF IGNITION.

(2) Apply gray urethane paint (PA-5992) as follows:

(a) Mix and thin paint in accordance with manufacturer’s instructions.

(b) Apply one coat of paint to damaged area with a brush. Allow to air dry four hours.

(c) When dry, apply a second coat of paint. Allow to air dry four hours.

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PART NUMBER 30-1033

(d) When dry, remove masking tape and check finish is smooth, free of defects and blends
into other surfaces.

4. Repair of Wiring Harness.

NOTE: Refer to the IPL for illustrations of the navigational light. Numbers in parentheses ( ) refer
to item numbers on the illustration.

A. Replace PCB assembly (275, IPL Figure 2) as follows:

(1) Unsolder wires from PCB assembly (275).

(2) Solder wires to replacement PCB assembly (275). Coat solder joints with conformal coating.

B. Replace capacitor assembly (-310A) as follows:

(1) Cut the wires as close to the ring terminal as possible.

(2) Strip insulation 0.25 inch (6,35 mm) from wires. Use solder to tin wire ends.

(3) Install new ring terminal (TE-190) on wires and crimp in place.

C. Replace green wire on PCB assembly (275) as follows:

(1) Unsolder damaged wire from PCB assembly (275) terminal (240, IPL Figure 3).

(2) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire ends.

(3) Install new ring terminal (TE-089) on wire and crimp in place.

(4) Solder replacement wire to terminal (240). Coat joint with conformal coating.

D. Replace red wire on PCB assembly (275, IPL Figure 2) connected to capacitor assembly (-310A) as
follows:

(1) Unsolder damaged wire from PCB assembly (275) terminal (240, IPL Figure 3).

(2) Cut the red wires as close to the ring terminal as possible.

(3) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire ends.

(4) Install new ring terminal (TE-190) on wires and crimp in place.

(5) Solder replacement wire to terminal (240). Coat joint with conformal coating.

E. Replace orange wire on PCB assembly (275, IPL Figure 2) terminal board as follows:

(1) Unsolder damaged wire from PCB assembly (275) terminal (240, IPL Figure 3).

(2) For all models except 30-1033-5, -13, -53, -55, -59, -61 and -63, perform following steps:

(a) Remove contact from connector plug position A.

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(b) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire
ends.

NOTE: Models 30-1033-49 and -57 use M39029/4-111 contact. Model 30-1033-51
uses M39029/4-110 contact. All other models with connector have contacts
provided with connector.

(c) Install new contact on replacement wire.

(d) Install contact in connector plug position A.

(3) For models 30-1033-53, -55, -59, -61 and -63, perform following steps:

(a) Cut the wire as close to splice as possible.

(b) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire
ends.

(c) Install splice on wire end and solder in place. Coat joint with conformal coating.

(4) For models 30-1033-5 and -31, perform following steps:

(a) Unsolder orange wire from terminal board (210, IPL Figure 2) positive terminal.

(b) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire
ends.

(c) Solder orange wire to terminal board (210) positive terminal. Coat joint with conformal
coating.

(5) Solder replacement wire to terminal (240, IPL Figure 3). Coat joint with conformal coating.

F. Replace black wire connected to capacitor (C3) (70) as follows:

(1) Unsolder damaged wire from capacitor (C3) (70).

(2) For models 30-1033-1, -3, -7, -11, -13, -19, -21, -23, -25, -27, -29, -33, -35, -37, -39, -41, -43,
-49, -51, -57, -65 and -67, perform following steps:

(a) Remove screw (235, IPL Figure 2), two lockwashers (240), two ring terminals and two
nuts (245) from base (265).

(b) Strip insulation 0.25 inch (6,35 mm) from wire ends. Use solder to tin wire ends.

(c) Install new ring terminal (TE-190) on wires and crimp in place.

(d) Secure two ring terminals to base (265) with screw (235), two lockwashers (240) and two
nuts (245).

(3) For models 30-1033-15, -17, -45, -53, -55, -59, -61 and -63, perform following steps:

(a) Remove screw (235), two lockwashers (240), ring terminals and two nuts (245) from base
(265).

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(b) Cut the wire as close to the ring terminal as possible.

(c) Strip insulation 0.25 inch (6,35 mm) from wire ends. Use solder to tin wire ends.

(d) Install new ring terminal (TE-145) on wires and crimp in place.

NOTE: Models 30-1033-59, -61 and -63 have three ring terminals installed on
screw.

(e) Secure two or three ring terminals to base (265) with screw (235), two lockwashers (240)
and two nuts (245).

(4) For models 30-1033-5 and -31, perform following steps:

(a) Unsolder black wire from terminal board (210) negative terminal.

(b) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire
ends.

(c) Solder black wire to terminal board (210) negative terminal. Coat joint with conformal
coating.

(5) Solder replacement wire to capacitor C3 (70, IPL Figure 3). Coat joint with conformal coating.

G. For all models except 30-1033-5, -15, -17, -31 and -45, replace connector (P1) (135, IPL Figure 2)
as follows:

(1) Remove connector (P1) (135) as follows:

(a) For all models except 30-1033-53, -55, -59, -61 and -63, remove orange wire and contact
from connector pin A.

(b) For models 30-1033-53, -55, -59, -61 and -63, remove white wire and contact from
connector pin A.

(c) For models 30-1033-1, -11, -13, -19, -21, -35, -39, -51, -65 and -67, remove black wire
and contact from connector pin B.

(d) For models 30-1033-3, -7, -23, -25, -27, -29, -33, -37 -41, -43, -49 and -57, remove black
wire and contact from connector pin C.

(e) For models 30-1033-53, -55, -59, -61 and -63, remove blue wire and contact from
connector pin C.

(f) For models 30-1033-59, -61 and -63, remove black wire and ring terminal from
backshell (-185).

(2) Install connector (P1) (135) as follows:

(a) For all models except 30-1033-53, -55, -59, -61 and -63, install orange wire and contact in
connector pin A.

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(b) For models 30-1033-53, -55, -59, -61 and -63, install white wire and contact in connector
pin A.

(c) For models 30-1033-1, -11, -13, -19, -21, -35, -39, -51, -65 and -67, install black wire and
contact in connector pin B.

(d) For models 30-1033-3, -7, -23, -25, -27, -29, -33, -37, -41, -43, -49 and -57, install black
wire and contact in connector pin C.

(e) For models 30-1033-53, -55, -59, -61 and -63, install blue wire and contact in connector
pin C.

(f) For models 30-1033-59, -61 and -63, secure black wire and ring terminal from cable to
backshell (-185).

H. For models 30-1033-15, -17 and -45, replace connecting wires as follows:

(1) Replace black wire from screw (235) as follows:

(a) Remove screw (235), two lockwashers (240), ring terminals and two nuts (245) from
base (265).

(b) Thread 24 in. (61,0 cm) long replacement wire (WI-256) through grommet (-230) in
base (265).

(c) Strip insulation 0.25 inch (6,35 mm) from replacement wire ends. Use solder to tin wire
ends.

(d) Install new ring terminal (TE-145) on wire at end that will attach to screw (235) and crimp
in place.

(e) Secure two ring terminals to base (265) with screw (235), two lockwashers (240) and two
nuts (245).

(2) Replace red wire on PCB assembly (275) as follows:

(a) Unsolder damaged wire from PCB assembly (275) terminal (240, IPL Figure 3). Remove
wire from base (265, IPL Figure 2).

(b) Thread 24 in. (61,0 cm) long replacement wire (WI-256) through grommet (-230) in
base (265).

(c) Solder replacement wire to PCB assembly (275) terminal (240, IPL Figure 3). Coat joint
with conformal coating.

I. For models 30-1033-5 and -31, replace terminal board (210, IPL Figure 2) as follows:

(1) Unsolder orange wire from positive terminal of terminal board (210).

(2) Unsolder black wire from negative terminal of terminal board (210).

(3) Remove two screws (205), spacers (220) and cover (200) from terminal board (210).

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PART NUMBER 30-1033

(4) Remove two screws (215) and jumper (225) from terminal board (210).

(5) Remove terminal board attaching hardware and terminal board (210) from base (265).

(6) Position new terminal board (210) on base (265) and secure with attaching hardware.

(7) Install two screws (215) and jumper (225) on terminal board (210).

(8) Position cover (200) on terminal board (210). Secure cover (200) with two screws (205) and
spacers (220).

(9) Solder orange wire on positive terminal of terminal board (210). Coat joint with conformal
coating.

(10) Solder black wire on negative terminal of terminal board (210). Coat joint with conformal
coating.

J. For models 30-1033-53, -55, -59, -56 and -63, replace cable as follows:

(1) For models 30-1033-59, -56 and -63, loosen backshell (-185) and move away from connector
(P1)(-135J).

(2) Remove contacts from connector (P1) (-135G, -135H or -135J).

(3) Remove connector (P1) (-135G, -135H or -135J) from cable.

NOTE: Models 30-1033-53 and -55 have two ring terminals installed on screw. Models
30-1033-59, -61 and -63 have three ring terminals installed on screw.

(4) Remove screw (235), two lockwashers (240), two or three ring terminals and two nuts (245)
from base (265).

NOTE: Model 30-1033-55 has cable exit through housing. Models 30-1033-53, -59, -61
and -63 have cable exit through base.

(5) Remove sealing compound, Ty-Raps, grommet (-230A) and old cable from base (265) or
housing (330).

(6) Install new grommet (-230A) on base (265) or housing (330).

NOTE: Model 30-1033-53 has 13.0 in. (33,0 cm) long cable. Model 30-1033-55 has 8.0
in. (20,3 cm) long cable. Models 30-1033-59, -61 and -63 have 20.0 in. (50,8
cm) long cable.

(7) Install replacement cable through grommet (-230A) in base (265) or housing (330).

(8) Install tape on cable where it contacts the grommet (-235A). Install heat shrink tubing over tape
and secure with two Ty-Raps. See Figure 601 for details.

WARNING: SEALING COMPOUND IS HIGHLY FLAMMABLE. AVOID INHALATION OF

VAPORS AND CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

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(9) Coat cable, grommet (-235A), tape and ty-raps with sealing compound. Wipe excess with clean
cloth. Allow sealing compound to cure for four hours at room temperature.

Cable Installation
Figure 601

(10) For models 30-1033-53 and -55, perform following steps:

(a) Strip cover from non-connector end of cable. Use care to not cut ground shield braid.

(b) Prepare a ground wire by stripping insulation 0.25 inch (6,35 mm) from wire ends. Use
solder to tin wire ends.

(c) Install new ring terminal (TE-145) on ground wire and crimp in place.

(d) Solder ground wire to cable ground shield braid.

(e) Install heat shrink tubing on wire and ground shield. Leave ring terminal uncovered.

(11) For models 30-1033-59, -61 and -63, perform following steps:

(a) Strip cover from both cable ends. Use care to not cut ground shield braid.

(b) Prepare two ground wires by stripping insulation 0.25 inch (6,35 mm) from wire ends. Use
solder to tin wire ends.

(c) Install new ring terminal (TE-145) on one end of ground wire and crimp in place.

(d) Solder ground wire to both ends of cable ground shield braid.

(e) Install heat shrink tubing on ground wire on non-connector end of cable.

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(f) Install new ring terminal (TE-089) on connector end ground wire and crimp in place.

(g) Install solder shield over cable to cover ground wire and cable ground shield braid.

(12) Strip insulation 0.25 inch (6,35 mm) from replacement cable wire ends. Use solder to tin wire
ends.

NOTE: Models 30-1033-53 and -55 use contacts supplied with connector. Models 30-
1033-59, -61 and -63 use M39029/58-396 contact.

(13) Install contacts on cable wires that will be installed in connector (P1) (-135G, -135H or -135J).

(14) For models 30-1033-59, -61 and -63, perform following steps:

(a) Install backshell (-185) on cable.

(b) Install white wire and contact in connector (P1) (-135J) pin A.

(c) Install blue wire and contact in connector (P1) (-135J) pin C.

(d) Install seal plugs in unused connector pin holes.

(e) Slide backshell (-185) down cable and secure to connector (P1) (-135J).

(f) Secure ground wire and ring terminal (TE-089) from cable to backshell (-185).

(15) For models 30-1033-53 and -55, perform following steps:

(a) Install white wire and contact in connector (P1) (-135G or -135H) pin A.

(b) Install blue wire and contact in connector (P1) (-135G or -135H) pin C.

NOTE: Models 30-1033-53 and -55 have two ring terminals installed on screw. Models
30-1033-59, -61 and -63 have three ring terminals installed on screw.

(16) Install ring terminal (TE-145) on blue wire of cable. Crimp in place.

(17) Install two or three ring terminals on screw (235).

(18) Secure screw (235) to base (265) with two lockwashers (240) and two nuts (245).

(19) Install white wire of cable in splice with orange wire and solder in place. Coat joint with
conformal coating.

5. Repair of Flashtube Lamp Assembly.

NOTE: Refer to IPL Figure 4 for an illustration of the flashtube lamp assembly. Numbers in
parentheses ( ) refer to item numbers on the illustration.

A. Replace the quartz flashtube lamp assembly as follows:

(1) Remove sealant from trigger coil assembly (T2) (70).

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(2) Remove nut (10), lockwasher (15) and spacer (20) from lamp assembly.

(3) Remove reflector (5) and spacer (20) from lamp assembly.

(4) Remove clamp (25) from quartz flashtube (30).

WARNING: THIS HALOGEN CYCLE LAMP IS PRESSURED AND MAY SHATTER. DO

NOT OPERATE IN EXCESS OF RATED VOLTAGE. PROTECT LAMP
AGAINST ABRASIONS AND SCRATCHES. REMOVE GREASE OR
FINGERPRINTS WITH A GREASE-FREE SOLVENT. WEAR PROTECTIVE
EYEGLASSES AND CLOTHING WHEN HANDLING LAMP. TURN POWER
OFF WHEN INSTALLING AND ALLOW TO COOL BEFORE REMOVING.
DISPOSE OF LAMP WITH CARE.

(5) Remove quartz flashtube (30) from clamp (35).

(6) Remove barrier (65) in trigger coil assembly (T2) (70).

(7) If required, prepare replacement quartz flashtube (30) as follows:

(a) Strip insulation 0.25 inch (6,35 mm) from black wire (WI-256) ends. Use solder to tin wire
ends.

(b) Strip insulation 0.25 inch (6,35 mm) from red wire (WI-292) ends. Use solder to tin wire
ends.

WARNING: THIS HALOGEN CYCLE LAMP IS PRESSURED AND MAY SHATTER.

DO NOT OPERATE IN EXCESS OF RATED VOLTAGE. PROTECT LAMP
AGAINST ABRASIONS AND SCRATCHES. REMOVE GREASE OR
FINGERPRINTS WITH A GREASE-FREE SOLVENT. WEAR
PROTECTIVE EYEGLASSES AND CLOTHING WHEN HANDLING LAMP.
TURN POWER OFF WHEN INSTALLING AND ALLOW TO COOL
BEFORE REMOVING. DISPOSE OF LAMP WITH CARE.

(c) Solder wires to quartz flashtube (30). Coat joints with conformal coating.

WARNING: THIS HALOGEN CYCLE LAMP IS PRESSURED AND MAY SHATTER. DO

NOT OPERATE IN EXCESS OF RATED VOLTAGE. PROTECT LAMP
AGAINST ABRASIONS AND SCRATCHES. REMOVE GREASE OR
FINGERPRINTS WITH A GREASE-FREE SOLVENT. WEAR PROTECTIVE
EYEGLASSES AND CLOTHING WHEN HANDLING LAMP. TURN POWER
OFF WHEN INSTALLING AND ALLOW TO COOL BEFORE REMOVING.
DISPOSE OF LAMP WITH CARE.

(8) Install new quartz flashtube(30) on clamp (35).

(9) Install clamp (25) on quartz flashtube (30).

(10) Check clamp (25) for fit on quartz flashtube (30). If required, remove clamp (25), bend fingers
to ensure proper fit and reinstall on quartz flashtube (30).

(11) Install spacer (20), reflector (5) and spacer (20) and secure with lockwasher (15) and nut (10).

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WARNING: SEALANT IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

(12) Install barrier (65) in trigger coil assembly (T2) (70).

(13) Inject sealant in trigger coil assembly (T2) (70) cavity. Wipe excess sealant with clean cloth.
Allow sealant to cure for four hours at room temperature.

(14) Install ring terminals on wire ends and crimp in place.

B. Replace reflectors (45) as follows:

(1) Remove damaged reflector (45) from trigger coil assembly (T2) (70).

WARNING: CEMENT IS HIGHLY FLAMMABLE. AVOID INHALATION OF VAPORS AND

CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

(2) Coat replacement reflector (45) with cement and install on trigger coil assembly (T2) (70). Wipe
excess cement with clean cloth.

(3) Replacement of Identification Plate.

NOTE: Grimes Aerospace Company does not authorize replacement of the identification plate.
For further information, contact a Grimes Aerospace representative at the following
address:

Grimes Aerospace Company

550 State Route 55
Urbana, OH 43078-1059
Telephone: (937) 484-2000
FAX: (937) 484-2101
SITA: DAYFLCR

6. Post Repair Procedures.

A. Clean parts. Refer to CLEANING, section 401, for details.

B. Wrap parts in a clean cloth to avoid contamination until ready for assembly.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

ASSEMBLY (INCLUDING STORAGE)

1. General Information.

A. The following paragraphs provide information for assembly (including storage) of the navigational
light.

B. Examine the parts for damage. Refer to CHECK, section 501, for details.

C. Repair the parts before assembly. Refer to REPAIR, section 601, for details.

D. Refer to Table 701 for a list of materials needed for assembly (including storage). Equivalent
substitutes are acceptable.

Table 701. Materials List

NOMENCLATURE SPECIFICATION MANUFACTURER

Cleaning Cloth A-A-59323 Commercially Available
Cushion and Dunnage PPP-C-1752, Unicellular, Commercially Available
Polyethylene Foam
Desiccant MIL-D-3464 Commercially Available
Masking Tape ¾ Inch Wide Commercially Available
Plastic Bag None Commercially Available
Sealing Compound (AD-330) MIL-S-8802 Commercially Available
Ty-Rap MS3367-4-4 Commercially Available
Wrapping Material MIL-B-121, Grade A Commercially Available
Unit Container PPP-B-636, Type CF or SF, Commercially Available
Class Weather Resistant

2. Assembly of Navigational Light.

NOTE: Refer to IPL Figure 2 for an illustration of the navigational light. Numbers in parentheses ( )
refer to item numbers on the illustration.

A. Assemble the light subassembly (-1 or -2) as follows:

(1) Position two capacitor assemblies (-310A) in housing (330). Ensure insulators are installed in
capacitor assemblies (-310A).

(2) Position two retainer assemblies (300) on two capacitor assemblies (-A310) and check for
proper fit. Secure retainer assemblies (300) in place with four screws (325).

(3) Install the Printed Circuit Board (PCB) assembly (275) on base (265) as follows:

(a) Use screw (290) to secure base (265) to PCB assembly (275) bracket.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

NOTE: Models 30-1033-1 through -27 use screw and nut to secure PCB bracket to
base. All other models have nutplate installed on bracket.

(b) For models 30-1033-1 through -27, use screw (280) and nut (285) to secure the base
(265) to PCB assembly (275) bracket. For all other models, use screw (280) to secure the
base (265) to PCB assembly (275) bracket.

(4) Install PCB assembly (275) and base (265) in housing (330). Ensure PCB assembly (275) is
properly installed in guide (320) during installation.

(5) Secure PCB assembly (275) in housing (330) with screw (295).

(6) Secure base (265) to housing (330) with three screws (270).

WARNING: SEALING COMPOUND IS HIGHLY FLAMMABLE. AVOID INHALATION OF

VAPORS AND CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

(7) Install sealing compound (AD-330) on three screws (270), seam where base (265) meets
housing (330), and four screws (305). Wipe excess sealing compound with clean cloth. Allow
sealing compound to cure at room temperature for four hours.

B. Install the mounting flange (125) or adapter (-125C) as follows:

NOTE: All models except 30-1033-21 and -25 have a mounting flange. Model 30-1033-21
has an adapter. Model 30-1033-25 does not have a mounting flange or adapter
installed.

(1) Position mounting flange (125) or adapter (-125C) on housing (330) and secure with three
screws (130).

WARNING: SEALING COMPOUND IS HIGHLY FLAMMABLE. AVOID INHALATION OF

VAPORS AND CONTACT WITH SKIN. OBSERVE FIRE PRECAUTIONS.

(2) Install bead of sealing compound around top and bottom joints of mounting flange. Wipe
excess adhesive with clean cloth. Allow adhesive to cure at room temperature for four hours.

NOTE: Models 30-1033-21, -25 and -45 do not have gaskets.

(3) Install gasket (120) on mounting flange (125) or adapter (-125C) and secure with Ty-Raps.

CAUTION: THIS HALOGEN CYCLE LAMP IS PRESSURED AND MAY SHATTER. DO NOT
OPERATE IN EXCESS OF RATED VOLTAGE. PROTECT LAMP AGAINST
ABRASIONS AND SCRATCHES. REMOVE GREASE OR FINGERPRINTS WITH A
GREASE-FREE SOLVENT. WEAR PROTECTIVE EYEGLASSES AND CLOTHING
WHEN HANDLING LAMP. TURN POWER OFF WHEN INSTALLING AND ALLOW
TO COOL BEFORE REMOVING. DISPOSE OF LAMP WITH CARE.

CAUTION: SEALANT IS VERY FLAMMABLE. DO NOT BREATHE THE VAPORS OR TOUCH

SEALANT WITH BARE SKIN. OBEY FIRE PRECAUTIONS.

3. For models 30-1033-1 and -7, apply a fillet of sealing compound (AD-330) to the items listed in Table
701. Wipe excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 701. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (265)
Housing (Bottom) (-315)

4. For models 30-1033-3, -23, -29, -37, -41, -43, and -49, apply a fillet of sealing compound (AD-330) to the
items listed in Table 702. Wipe excess with clean cloth. Allow sealing compound to cure for four hours at
room temperature.

Table 702. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (265)
Housing (Bottom) (-315)
Connector (135), (-135B), (-135D)

5. For models 30-1033-5 and -31, apply a fillet of sealing compound (AD-330) to the items listed in Table
703. Wipe excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 703. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265B)
Housing (Bottom) (-315)

6. For model 30-1033-51, apply a fillet of sealing compound (AD-330) to the items listed in Table 704. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 704. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265A)
Housing (Bottom) (-315A)

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

7. For model 30-1033-57, apply a fillet of sealing compound (AD-330) to the items listed in Table 705. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 705. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265C)
Housing (-315)
Flange (Top only) (-125A)

8. For models 30-1033-11, -13, -19, -21, -25, -27, -35, and -39, apply a fillet of sealing compound (AD-330)
to the items listed in Table 706. Wipe excess with clean cloth. Allow sealing compound to cure for four
hours at room temperature.

Table 706. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (265)
Housing (Bottom) (-315)

9. For models 30-1033-15, -17, and -45, apply a fillet of sealing compound (AD-330) to the items listed in
Table 707. Wipe excess with clean cloth. Allow sealing compound to cure for four hours at room
temperature.

Table 707. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265D)
Housing (Bottom) (-315)

10. For model 30-1033-33, apply a fillet of sealing compound (AD-330) to the items listed in Table 709. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 709. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (265)
Housing (Bottom) (-315)

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

11. For model 30-1033-53, apply a fillet of sealing compound (AD-330) to the items listed in Table 710. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 710. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265E)
Housing (Bottom and Top) (-315)
Screw (-280B)
Screw (-130A)
Screws (270) and (295)
Screw (235) and (290)
Screw (305)
Flange (Top only) (-125E)
Grommet (Inside and Outside) (-230A)

12. For model 30-1033-55, apply a fillet of sealing compound (AD-330) to the items listed in Table 711. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 711. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265F)
Housing (Bottom and Top) (-315B)
Screw (-280B)
Screw (-130A)
Screws (270) and (295)
Screw (235) and (290)
Screw (305)
Flange (Top only) (-125F)
Grommet (Inside and Outside) (-230A)

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

13. For model 30-1033-63, apply a fillet of sealing compound (AD-330) to the items listed in Table 712. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 712. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265E)
Housing (-315C)
Screw (-235) and (290)
Screw (305)
Screws (-130A)
Screw (270) and (295)
Flange (Top and Bottom) (-125G)
Grommet (Inside and Outside) (-230A)

14. For model 30-1033-61, apply a fillet of sealing compound (AD-330) to the items listed in Table 713. Wipe
excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

Table 713. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (-265G)
Housing (-315C)
Screw (270) and (295)
Screw (305)
Screws (-130A)
Screw (-235) and (290)
Screw (-280B)
Flange (Top and Bottom) (-125G)
Grommet (Inside and Outside) (-230A)

15. For models 30-1033-65 and -67, apply a fillet of sealing compound (AD-330) to the items listed in Table
714. Wipe excess with clean cloth. Allow sealing compound to cure for four hours at room temperature.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 714. Sealing Compound Areas

NOMENCLATURE IPL ITEM NUMBER

Base (265)
Housing (Bottom and Top) (-315)
Screw (290)
Screw (305)
Screw (-130A)
Screw (270) and (295)
Flange (Top only) (125)
Lens Retainer (Fill in cavities) 10

A. Install flashtube lamp assembly (DS1) (100) as follows:

(1) Position mounting ring (110) and gasket (105) on housing (330) and secure with three
screws (115).

(2) Position gasket (65) on housing (330).

(3) Install wires and ring terminal on flashtube lamp assembly (DS1) (100) at locations marked
during DISASSEMBLY, section 301. Secure with screws.

B. Assemble the lens assembly (-20) as follows:

(1) Install threaded insert (40) and teflon washer (45) in lens (60).

(2) Install lockwasher (30), drain tube (35 or -35A) and washer (50) on lens (60) and secure with
screw (25).

C. Install the lens assembly (-20) as follows:

(1) For all models except 30-1033-27, install lens assembly (20) and gasket (65) on housing (330)
and secure with three screws (15).

(2) For model 30-1033-27, install lens assembly (20) and gasket (65) on mounting ring (110) and
secure with retainer band (-10A).

D. If the navigational light is painted, ensure all applications of sealing compound have paint applied.
Refer to REPAIR, section 601, for detailed instructions.

E. Test the navigational light. Refer to TESTING AND FAULT ISOLATION, section 101, for details.

16. Storage. Pack the navigational light as follows:

A. Wipe the navigational light with a clean cloth to remove dust, dirt and foreign material.

B. Preserve the navigational light in accordance with MIL-P-116, Method 1-A-8.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

C. Wrap the navigational light in wrapping material and place in plastic bag.

D. Place cushion and dunnage material, desiccant and the navigational light in unit container, then seal
with masking tape.

E. Mark outside of unit container in accordance with MIL-STD-129. Also include overhaul date and
location.

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

SPECIAL TOOLS, FIXTURES AND EQUIPMENT

1. General Information.

A. The following paragraphs provide information for special tools, fixtures and equipment used for
overhaul of the navigational light.

B. Refer to Table 901 for a list of this equipment. These items may be purchased from Grimes
Aerospace Company, the original manufacturer or, in some cases, locally manufactured. Refer to
the referenced figure for details. Equivalent substitutes are acceptable.

Table 901. Special Tools, Fixtures and Equipment List

NOMENCLATURE PART/MODEL USED FOR FIGURE

NUMBER NUMBER
Digital Multimeter Model 87 Testing and NA
(DMM) Fluke Corporation Fault Isolation
Everett, WA
(V02WJ6)
Variable Regulated Commercially Available Testing and NA
Power Supply Fault Isolation
(0-45 Vdc, 6 amp min)

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

ILLUSTRATED PARTS LIST

1. General Information.

A. The Illustrated Parts List (IPL) provides a breakdown of assemblies, subassemblies and detail parts
of the aircraft navigational light. All parts are listed, except for parts which lose their identities by
being permanently fastened to other parts or are part of an assembly not subject to disassembly.

B. Bulk materials such as safety or electrical wire and tape, and consumable materials such as
adhesives, sealants, lubricants, solder, paint and primer are not included in the detailed parts lists.
These materials are identified in the materials list at the beginning of each section.

C. To find a part number when the part number is unknown, locate the part on the illustration and note
the item number. Locate the item number on the detailed parts list. The part number will be shown
on the same line. In some instances there are gaps in item number sequence and the item numbers
are not continuously sequential.

2. Explanation of Columns, Terms and Symbols in the Illustrated Parts List (IPL).

A. FIG. & ITEM NO. column: The figure and item numbers key the detailed parts list to the applicable
illustration. The first number represents the figure number of the illustration. The item number
corresponds to an item number on the illustration.

(1) An item number not on the illustration is identified by a dash (-) preceding the item number.
This can indicate the following:

(a) When two or more visually alike parts are listed in sequence, only the first part is
illustrated. The illustration, however, is applicable to both parts.

(b) When detail parts of an assembly or installation are separately illustrated, the resulting
assembly may be illustrated as an assembly by bracketing the detail parts and identifying
the bracket as the assembly. If brackets are not used, the detail parts are illustrated, but
the assembly is not.

(2) An item number followed by an alphabetical character such as A, B, C, etc., indicates the part
listed is similar to the same item number without the alphabetical character. The difference
could be each part is used for a different next higher assembly (NHA) or is an equivalent part.
This will be noted in the NOMENCLATURE or EFF CODE columns.

B. PART NUMBER column: This column contains the original manufacturer’s part number of the
assembly, subassembly or detail part listed. Part numbers in this IPL are those of Grimes
Aerospace Company, Urbana, Ohio (V72914) or are standard parts unless a Commercial and
Government Entity (CAGE) code appears in the NOMENCLATURE column. Refer to paragraph 4
for details. The following phrases may be used in this column:

„ “ORDER NHA” is used when no part number exists for the part listed or when it is preferable to
order an assembly rather than detail parts. ORDER NHA items which have no part numbers
are not procurable and should not be ordered. The next higher assembly, however, is
procurable and may be ordered.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

„ “NONPROC” followed by an assigned number (for example NONPROC123) is used when no

part number exists for the assembly. NONPROC assemblies are not procurable and may not
be ordered. However, the detail parts of the assembly are procurable and may be ordered,
unless otherwise specified.

„ “REF” followed by an assigned number (for example REF001) is used when the part number is
more than fifteen digits. The original part number with more than fifteen digits is listed in the
NOMENCLATURE column and is the part number to be used when ordering the part.

C. AIRLINE STOCK NO. column: This column is reserved for airline part numbers and accommodates
eleven numbers.

D. NOMENCLATURE column: This column identifies the parts being listed by noun name followed by
modifiers when applicable. This column also provides the following information:

(1) The relationship of each listed item to its next higher assembly (NHA) is shown by an indenture
code. Each listed item is placed in the NOMENCLATURE column one indenture (one dot) to
the right of the assembly to which it belongs. Items at equal indentures are all components of a
single assembly or subassembly. An example of the indenture code system is shown below:

12 3 4 5 6 7

Assembly or Installation Descriptive Title

. Assembly
. Attaching Parts for Assembly
. . Detail Parts for Assembly
. . . Subassembly
. . . Attaching Parts for Subassembly
. . . . Detail Parts for Subassembly
. . . . . Sub-Subassembly
. . . . . Attaching Parts for Sub-Subassembly
. . . . . . Detail Parts for Sub-Subassembly

(2) Symbols used, with the exception of effectivity and CAGE codes, are as follows:

(ATTACHING PARTS) Designates start of each group of attaching parts.

-------*------- Designates end of each group of attaching parts.

(3) The following phrases may be used in this column:

„ “DELETED” identifies a part no longer used.

„ “SUPERSEDED” identifies a part no longer authorized for use.

„ “REPLACES” or “REPLACES ITEM XXX” identifies this part is newer and therefore more
desirable than the “REPLACED” part. However, either may be used.

„ “REPLACED” or “REPL BY ITEM XXX” identifies this part is older and therefore less
desirable than the “REPLACES” part. However, either may be used.

„ “ALTN PART FOR ITEM XXX” identifies this part as an alternative. However, either part
may be used and neither is more desirable than the other.

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

„ “TPN” precedes a True Part Number with all dashes, slashes, spaces and/or symbols
assigned by the original manufacturer of the part. This is the part number to be used
when ordering the part.

E. EFF CODE column: This column establishes part relationship with assemblies, which are essentially
the same, but have minor variations. These assemblies are the end items on the detailed parts list
and are assigned reference letters such as A, B, C, D, etc. Subassemblies or detail parts, which are
not common to all configurations, but are associated with one or more of the coded end items, carry
the letter or letters assigned to the end item(s) with which they are associated. If a part is common
to all end items, the EFF CODE column is blank.

F. UNITS PER ASSY column: This column shows the quantity of each item required for the next higher
subassembly, assembly or installation outline. Quantities shown for attaching parts are the number
required for the related part, subassembly or assembly and, therefore, may not be the total quantity
used for the end item of the detailed parts list. The following letters may be used in this column:

„ “AR” indicates “as required” and refers to variable quantity items such as shims, spacers or
similar items.

„ “RF” indicates "reference" and refers to items and their quantities which are listed elsewhere
and are provided here as a reference only.

„ "NP" indicates "non-procurable" and refers to items which are not procurable and may not be
ordered.

3. Abbreviations. Standard abbreviations used in the IPL agree with MIL-STD-12, except as noted below:

Abbreviation Definition

None

4. Commercial and Government Entity (CAGE) Codes.

A. CAGE codes, preceded by the capital letter "V" (V12345), are used to identify the original
manufacturer of non-Grimes Aerospace Company (V72914) components. CAGE codes are listed in
the NOMENCLATURE column, except for the government codes below, which are not listed:

V96906 Military Standard (prefix MS)

V88044 Army/Navy Standard (prefix AN)
V80205 National Aircraft Standard (prefix NAS)

B. The following CAGE codes are listed in this IPL:

VK1196 Zetex Plc.

Fields New Rd.
Chadderton Oldham Lancs, OL9 8NP
United Kingdom

V01556 Emhart Fastening System Group

Helicoil Div.
510 River Rd.
Shelton, CT 06484

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

V04222 AVX Corp.

867 19th Ave. S.
Myrtle Beach, SC 29578

V04713 Motorola Inc.

Semiconductor Products Sector
5005 E McDowell Rd.
Phoenix, AZ 85008

V05277 Westinghouse Electric Corp.

Semiconductor Div.
Hills St.
Youngwood, PA 15697

V11139 Deutsch Co.

Engineered Connecting Devices
5733 W. Whittier Ave.
Hemet, CA 92545

V13103 Thermalloy Co, Inc.

2021 W. Valley View Ln.
Dallas, TX 75381

V14433 ITT Semiconductor Div.

West Palm Beach, FL 33401

V15873 Motorola, Inc.

400 W. Main St.
Arcade, NY 14009

V18310 Concord Electronics Corp.

30 Great Jones St.
New York, NY 10012

V25403 Philips Circuit Assemblies

100 Providence Pike
Slatersville, RI 02876

V27194 Teccor Electronics, Inc.

Semiconductor Div.
1801 Hurd Dr.
Irving, TX 75038

V56289 Sprague Electric Co.

678 Main St.
Sanford, ME 04073

V59610 Souriau, Inc.

Valencia, CA 91354

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PART NUMBER 30-1033

V66958 SGS-Thomson Microelectronics, Inc.

1000 E. Bell Rd.
Phoenix, AZ 85022

V71279 Interconnection Products, Inc.

2601 S. Garnsey St.
Santa Ana, CA 92707

V73138 Bi Technologies Corp.

4200 Bonita Pl.
Fullerton, CA 92635

V77820 Amphenol Corp.

Amphenol Aerospace
Bendix Connectors OPNS
40-60 Delaware St.
Sidney, NY 13838

V86577 Precision Metal Products, Inc.

Peabody, MA 01960

V91265 Goshen Rubber Co., Inc.

1525 S. 10th St.
Goshen, IN 46526

V96905 L and W Mfg. Corp.

Indianapolis, IN

V99942 N A P SMD Technology, Inc.

5. Overhaul. The navigational light may be returned to Grimes Aerospace (V72914) for overhaul. For
further information, contact a Grimes Aerospace representative at the following address:

Grimes Aerospace Company

550 State Route 55
Urbana, OH 43078-1059
Telephone: (937) 484-2000
FAX: (937) 484-2101
SITA: DAYFLCR

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 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1001. Reference Designator Index

REFERENCE FIG./ REFERENCE FIG./ REFERENCE FIG./

DESIGNATOR ITEM DESIGNATOR ITEM DESIGNATOR ITEM
C1 3-60 L1 3-100 R16 3-130
C1 3-60A P1 2-135 R17 3-190
C1 3-60B P1 2-135A R19 3-180
C2 3-65 P1 2-135B R20 3-200
C3 3-70 P1 2-135C R21 3-185
C4, C5 3-75 P1 2-135D R22 3-195
C7 3-80 P1 2-135E R23, R24 3-155
C7 3-80A P1 2-135F R25 3-190
C8 3-85 P1 2-135G R26 3-135
C9-C12 2-310 P1 2-135H R27, R28 3-205
C9-C12 2-310A P1 2-135J SCR1 3-210
C13 3-90 R1 3-140 SCR1 3-210A
C13 3-90A R2, R3 3-145 TB1 2-210
C13 3-90B R4 3-150 T2 4-65
C14 3-95 R5 3-200 Q1 3-215
C15 3-90B R6 3-145 Q1 3-215A
CR1-CR5 3-110 R7 3-155 Q2 3-220
CR6, CR7 3-115 R8 3-145 Q2 3-220A
CR6, CR7 3-115A R9 3-160 Q3 3-50
CR8 3-110 R10 3-145 Q3 3-50A
CR9 3-125 R11 3-165 T1 3-230
DS1 2-100 R12 3-170 T1 3-230A
DS1 2-100A R13 3-145 U1 3-105
DS1 4-1 R14 3-200 VR1 3-120
DS1 4-1A R15 3-175

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COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 1 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
A3934 2 -80 NP
A4253-1 2 -75 NP
A7632-2 2 105 1
A7635A 2 -10A 1
A7794 2 -5A 2
A7794 2 195 2
A7941 2 -95 NP
A8918-1 2 120 1
A8966-1 2 -90 NP
A9292-1 2 -55 NP
A9292-3 2 50 1
BUW50 3 -50A 1
BYV96E 3 -115A 2
B8-3APLN29500 2 -135A NP
B8917-10 2 -125A 1
B8917-11 2 -125B 1
B8917-9 2 125 1
CB1055S 3 -250
DDM103 3 75 2
DD102 3 95 1
D38999-26FA99PN 2 -135J 1
GRC614 2 -230 1
JAN2N2222A 3 -215A 1
MCR22-6 3 -210A 1
MS20426A2-3 2 325 2
MS21042-04 2 145 4
MS21042-04 2 285 1
MS21042-06 3 40 1
MS27488-16 2 -165
MS27488-20 2 -170
MS3101F10SL3P 2 -135H 1
MS3102R10SL3P 2 135 1
MS3116F10-6P 2 -135G 1
MS3120E8-4P 2 -135D 1
MS3470L12-3P 2 -135E 1
MS3470L8-3P 2 -135F 1
MS35206-211 2 190 2
MS35206-212 2 15 3
MS35206-213 2 280 NP
MS35206-214 2 -15A 3
MS35206-215 2 -280A 1
MS35206-216 2 -280B 1
MS35206-225 2 25 1
MS35206-226 2 -70 NP
MS35206-226 2 -290A 1
MS35206-227 3 25 1

33-40-59 Page 1007

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 2 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
MS35206-228 2 205 2
MS35206-228 2 290 1
MS35206-228 3 -35A 1
MS35206-229 2 215 NP
MS35206-229 3 35 1
MS35206-231 2 -215A 2
MS35338-136 2 240 2
MS35338-41 2 30 1
MS35338-41 2 -85 NP
MS35338-41 4 15 1
MS35489-4 2 -230A 1
MS35649-262 4 10 1
MS35649-264 2 245 2
MS51863-21 2 130 NP
MS51863-215 2 140 4
MS51863-216 2 -140A 4
MS51957-12 2 115 3
MS51957-26 2 -130A 3
MS51957-30 2 235 1
M38527-08-043P 3 -225A 1
M39029-4-110 2 -155
M39029-4-111 2 -150
M39029-58-363 2 -160
M85049-38-9W 2 -185 1
PMT2R22K400 3 80 NP
PTO2E8-4P 2 -135C NP
REF001 3 -40A 1
REF002 3 60 NP
SC359 2 305 4
SC727 2 270 3
SC727 2 295 1
SK047C224KAA 3 -60A 1
SK047C224KAA 3 -80A 1
SR215E224MAA 3 -60B 1
S4001MS3 3 210 NP
ZTX849 3 -220A 1
1D3-8B 3 240 NP
1N4731 3 -125A 1
1N4740A 3 120 1
1N5399 3 115 NP
1N751A 3 125 NP
10-214-2-01 3 -240A 4
11661 2 40 1
11706-3 2 -35A 1
14828 3 55 1
150D685X9035B2 3 65 1
17489 2 -195A 2

33-40-59 Page 1008

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 3 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
192P473X9200 3 -90A 1
192P473X9200 3 90B 2
192P47392 3 -90 NP
2N2222 3 215 NP
2N2222 3 220 NP
25-0918-21 2 -60D 1
25-0918-21C 2 60 1
25-0918-21C3 2 -60F 1
25-0918-21C5 2 -60G 1
25-0918-23 2 -60C 1
25-0918-23C 2 -60A 1
25-0921-1 2 -60E 1
25-0956-23C 2 -60B 1
30-1033-1 1 -1 RF
30-1033-11 1 -1D RF
30-1033-13 1 -1E RF
30-1033-15 1 -1F RF
30-1033-17 1 -1G RF
30-1033-19 1 -1H RF
30-1033-21 1 -1J RF
30-1033-23 1 -1K RF
30-1033-25 1 -1L RF
30-1033-27 1 -1M RF
30-1033-29 1 -1N RF
30-1033-3 1 -1A RF
30-1033-31 1 -1P RF
30-1033-33 1 -1Q RF
30-1033-35 1 -1R RF
30-1033-37 1 -1S RF
30-1033-39 1 -1T RF
30-1033-41 1 -1U RF
30-1033-43 1 -1V RF
30-1033-45 1 -1W RF
30-1033-49 1 -1X RF
30-1033-5 1 -1B RF
30-1033-51 1 -1Y RF
30-1033-53 1 -1Z RF
30-1033-55 1 -2 RF
30-1033-57 1 -2A RF
30-1033-59 1 -2B NP
30-1033-61 1 -2C RF
30-1033-63 1 -2D RF
30-1033-65 1 -2E RF
30-1033-67 1 -2F RF
30-1033-7 1 -1C RF
31-0981-1 1 -20
31-1604-11 4 40 1

33-40-59 Page 1009

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 4 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
31-1604-9 4 5 1
31-2101-5 4 45 2
31-2622-1 4 25 1
31-2622-5 4 35 1
31-2836-1 4 65 1
31-3196-1 2 200 1
31-3318-1 2 -315 1
31-3318-13 2 -315C 1
31-3318-3 2 330 1
31-3318-3 2 -330B 1
31-3318-3 2 -330C 1
31-3318-5 2 -330A 1
31-3318-7 2 -315A 1
31-3318-9 2 -315B 1
31-3319-1 2 265 1
31-3319-11 2 -265C 1
31-3319-13 2 -265E 1
31-3319-15 2 -265F 1
31-3319-17 2 -265G 1
31-3319-3 2 -265A 1
31-3319-5 2 -265B 1
31-3319-9 2 -265D 1
31-3320-1 2 300 2
31-3321-1 2 310 NP
31-3321-3 2 -310A 2
31-3322-1 3 5 1
31-3323-1 3 20 NP
31-3323-3 3 -20A
31-3323-5 3 -20B 1
31-3324-1 3 245 NP
31-3325-1 2 275 NP
31-3325-1 3 -1 NP
31-3325-11 2 -275C 1
31-3325-11 3 -1C RF
31-3325-5 2 -275A NP
31-3325-5 3 -1A NP
31-3325-7 2 -275B 1
31-3325-7 3 -1B RF
31-3326-1 1 35 1
31-3326-1 2 -1 RF
31-3326-11 1 -35N 1
31-3326-11 2 -1E RF
31-3326-13 1 -35P 1
31-3326-13 2 -1F RF
31-3326-15 1 -35U 1
31-3326-15 2 -1G RF
31-3326-17 1 -35V 1
31-3326-17 2 -1H RF

33-40-59 Page 1010

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 5 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
31-3326-19 1 -35S 1
31-3326-19 2 -1J RF
31-3326-21 1 -35X 1
31-3326-21 2 -1K RF
31-3326-23 1 -35Y 1
31-3326-23 2 -1L RF
31-3326-25 1 -36A 1
31-3326-25 2 -1M RF
31-3326-3 1 -35A 1
31-3326-3 2 -1A RF
31-3326-5 1 -35B 1
31-3326-5 2 -1B RF
31-3326-7 1 -35C 1
31-3326-7 2 -1C RF
31-3326-9 1 -35K 1
31-3326-9 2 -1D RF
31-3328-1 1 -10
31-3353-1 2 100 1
31-3353-1 4 -1 RF
31-3353-3 2 -100A 1
31-3353-3 4 -1A RF
31-3492-1 3 30 1
31-3492-5 3 30
31-3694-1 4 70 1
31-3762-5 1 -30
31-3851-1 2 10 1
31-3851-3 2 -10B 1
31-3881-1 1 -35D 1
31-3881-1 2 -1N RF
31-3881-11 1 -35J 1
31-3881-11 2 -1T RF
31-3881-17 1 -35L 1
31-3881-17 2 -1U RF
31-3881-19 1 -35M 1
31-3881-19 2 -1V RF
31-3881-25 1 -35Q 1
31-3881-25 2 -1W RF
31-3881-27 1 -35R 1
31-3881-27 2 -1X RF
31-3881-29 1 -35T 1
31-3881-29 2 -1Y RF
31-3881-3 1 -35E 1
31-3881-3 2 -1P RF
31-3881-31 1 -35W 1
31-3881-31 2 -1Z RF
31-3881-33 1 -35Z 1
31-3881-33 2 -2 RF

33-40-59 Page 1011

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 6 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
31-3881-35 1 -36 1
31-3881-35 2 -2A RF
31-3881-37 1 -36B 1
31-3881-37 2 -2B RF
31-3881-39 1 -36C 1
31-3881-39 2 -2C RF
31-3881-41 1 -36D 1
31-3881-41 2 -2D RF
31-3881-43 1 -36E 1
31-3881-43 2 -2E RF
31-3881-5 1 -35F 1
31-3881-5 2 -1Q RF
31-3881-7 1 -35G 1
31-3881-7 2 -1R RF
31-3881-9 1 -35H 1
31-3881-9 2 -1S RF
31-4079-1 2 -20 1
31-4079-17 2 -20E 1
31-4079-29 2 -20B 1
31-4079-3 2 -20A 1
31-4079-31 2 -20G 1
31-4079-33 2 -20H 1
31-4079-5 2 -20D 1
31-4079-7 2 -20C 1
31-4079-9 2 -20F 1
31-4346-1 1 15 NP
31-4431-1 2 -125D 1
31-5921-1 2 -120B 1
31-7980-1 2 -125E 1
31-7988-1 2 110 1
31-7997-1 2 -125F 1
31-8224-1 2 -125G 1
31-8225-1 2 -120C 1
31-8244-1 2 250 1
31879 3 -265
31901 2 -175
3585-06CN0138 4 60 1
36149 2 -180
41-0782-1 2 -125C 1
41-1035-1 2 -120A 1
41-1191-3 2 260 1
41-1192-1 2 255 1
41-1225-1 1 -5
41-1225-1 2 5 2
41-1457-7 2 35 1
43-02-37 3 235 1
55-0206-21 3 10 NP

33-40-59 Page 1012

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Table 1002. Numerical Index (Sheet 7 of 7)

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NO. NUMBER NO. REQUIRED
55-0207-01 3 -10A 1
55-0211-25PB 4 50 1
55-0211-26PB 4 55 2
55-0225-10R03F 3 205 2
55-0225-10015A 3 -255
55-0225-10015D 3 180 1
55-0225-30R03F 3 195 1
55-0283-1 4 30 1
55-0283-3 4 -30A 1
55-0363-1 3 50 1
55-0382-1025CS 3 190 2
55-0382-1025DS 3 140 1
55-0382-1045CS 3 145 6
55-0382-1055CS 3 155 3
55-0382-2215CS 3 185 1
55-0382-2225CS 3 160 1
55-0382-2255DS 3 175 1
55-0382-3345CS 3 170 1
55-0382-4725CS 3 200 3
55-0382-4745CS 3 165 1
55-0382-6835CS 3 150 1
55-0478-14 3 105 1
55-0679-1051AF 3 85 1
55-0712-1 3 100 1
55-0713-1 3 230 1
55-0713-5 3 -230A 1
55-0997-1 3 110 6
55-1037-151AJ14 3 70 1
60-0258-3 2 45 1
60-1521-9 3 45 1
60-2227-1 4 20 3
60-2485-1 2 220 2
60-5023-3 2 65 2
601-J 2 225 1
601-2104-1 2 210 1
61-1606-1 1 25 1
66-2513-3 3 15 1
72XWR10K 3 130 1
72XWR500K 3 135 1
7717-157T 3 225 NP
7717158T 3 -260
81-0849-9 2 320 1
851-00-R8-3APN50 2 -135B 1
86-0512-1 2 -65A NP
86-0512-3 2 -65B NP

33-40-59 Page 1013

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Aircraft Navigational Light

IPL Figure 1

33-40-59 Page 1014

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 -1 30-1033-1 NAVIGATIONAL LIGHT A RF

-1A 30-1033-3 NAVIGATIONAL LIGHT B RF
-1B 30-1033-5 NAVIGATIONAL LIGHT C RF
-1C 30-1033-7 NAVIGATIONAL LIGHT D RF
-1D 30-1033-11 NAVIGATIONAL LIGHT E RF
-1E 30-1033-13 NAVIGATIONAL LIGHT F RF
-1F 30-1033-15 NAVIGATIONAL LIGHT G RF
-1G 30-1033-17 NAVIGATIONAL LIGHT H RF
-1H 30-1033-19 NAVIGATIONAL LIGHT J RF
-1J 30-1033-21 NAVIGATIONAL LIGHT K RF
-1K 30-1033-23 NAVIGATIONAL LIGHT L RF
-1L 30-1033-25 NAVIGATIONAL LIGHT M RF
-1M 30-1033-27 NAVIGATIONAL LIGHT N RF
-1N 30-1033-29 NAVIGATIONAL LIGHT P RF
-1P 30-1033-31 NAVIGATIONAL LIGHT Q RF
-1Q 30-1033-33 NAVIGATIONAL LIGHT R RF
-1R 30-1033-35 NAVIGATIONAL LIGHT S RF
-1S 30-1033-37 NAVIGATIONAL LIGHT T RF
-1T 30-1033-39 NAVIGATIONAL LIGHT U RF
-1U 30-1033-41 NAVIGATIONAL LIGHT V RF
-1V 30-1033-43 NAVIGATIONAL LIGHT W RF
-1W 30-1033-45 NAVIGATIONAL LIGHT X RF
-1X 30-1033-49 NAVIGATIONAL LIGHT (MODIFIED PER Y RF
SB 30-1033-33-0095)
-1Y 30-1033-51 NAVIGATIONAL LIGHT Z RF
-1Z 30-1033-53 NAVIGATIONAL LIGHT AA RF
-2 30-1033-55 NAVIGATIONAL LIGHT AB RF
-2A 30-1033-57 NAVIGATIONAL LIGHT (MODIFIED PER AC RF
SB 30-1033-33-0095)
-2B 30-1033-59 NAVIGATIONAL LIGHT (REWORKED TO ITEM 2C OR AD NP
2D PER SB 30-1033-33-SB01)
-2C 30-1033-61 NAVIGATIONAL LIGHT (MODIFIED PER SB 30-1033- AE RF
33-SB01) (MODIFIED PER SB 30-1033-33-SB02)
(MODIFY TO PART NUMBER 30-2675-1 PER
SB 30-1033-33-SB03) (SEE CMM 33-42-21)
-2D 30-1033-63 NAVIGATIONAL LIGHT (MODIFIED PER AF RF
SB 30-1033-33-SB01) (MODIFIED PER SB 30-1033-
33-SB02) (MODIFY TO PART NUMBER 30-2676-1
PER SB 30-1033-33-SB03) (SEE CMM 33-42-21)
-2E 30-1033-65 NAVIGATIONAL LIGHT AG RF
-2F 30-1033-67 NAVIGATIONAL LIGHT AH RF

- Item Not Illustrated

33-40-59 Page 1015

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 -5 41-1225-1 . DELETED
-10 31-3328-1 . DELETED
15 31-4346-1 . PLATE, IDENTIFICATION L,V,W NP
-20 31-0981-1 . DELETED
25 61-1606-1 . PLATE, INSTRUCTION B, L, 1
P, V,
W, Z
-30 31-3762-5 . DELETED
35 31-3326-1 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR A 1
DETAILS)
-35A 31-3326-3 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR B 1
DETAILS)
-35B 31-3326-5 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR C 1
DETAILS)
-35C 31-3326-7 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR D 1
DETAILS)
-35D 31-3881-1 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR E 1
DETAILS)
-35E 31-3881-3 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR F 1
DETAILS)
-35F 31-3881-5 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR G 1
DETAILS)
-35G 31-3881-7 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR H 1
DETAILS)
-35H 31-3881-9 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR J 1
DETAILS)
-35J 31-3881-11 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR K 1
DETAILS)
-35K 31-3326-9 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR L 1
DETAILS)
-35L 31-3881-17 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR M 1
DETAILS)
-35M 31-3881-19 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR N 1
DETAILS)
-35N 31-3326-11 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR P 1
DETAILS)
-35P 31-3326-13 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR Q 1
DETAILS)
-35Q 31-3881-25 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR R 1
DETAILS)
-35R 31-3881-27 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR S 1
DETAILS)
-35S 31-3326-19 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR T 1
DETAILS)

- Item Not Illustrated

33-40-59 Page 1016

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

1 -35T 31-3881-29 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR U 1

DETAILS)
-35U 31-3326-15 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR V 1
DETAILS)
-35V 31-3326-17 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR W 1
DETAILS)
-35W 31-3881-31 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR X 1
DETAILS)
-35X 31-3326-21 . LIGHT SUBASSEMBLY (MODIFIED PER Y 1
SB 30-1033-33-0095) (SEE IPL FIGURE 2 FOR
DETAILS)
-35Y 31-3326-23 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR Z 1
DETAILS)
-35Z 31-3881-33 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AA 1
DETAILS)
-36 31-3881-35 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AB 1
DETAILS)
-36A 31-3326-25 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AC 1
DETAILS)
-36B 31-3881-37 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AD,AF 1
DETAILS)
-36C 31-3881-39 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AE 1
DETAILS)
-36D 31-3881-41 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AG 1
DETAILS)
-36E 31-3881-43 . LIGHT SUBASSEMBLY (SEE IPL FIGURE 2 FOR AH 1
DETAILS)

- Item Not Illustrated

33-40-59 Page 1017

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Light Subassembly
IPL Figure 2

33-40-59 Page 1018

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 -1 31-3326-1 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR A RF

NHA)
-1A 31-3326-3 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR B RF
NHA)
-1B 31-3326-5 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR C RF
NHA)
-1C 31-3326-7 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR D RF
NHA)
-1D 31-3326-9 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR E RF
NHA)
-1E 31-3326-11 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR F RF
NHA)
-1F 31-3326-13 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR G RF
NHA)
-1G 31-3326-15 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR H RF
NHA)
-1H 31-3326-17 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR J RF
NHA)
-1J 31-3326-19 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR K RF
NHA)
-1K 31-3326-21 LIGHT SUBASSEMBLY (MODIFIED PER L RF
SB 30-1033-33-0095) (SEE IPL FIGURE 1 FOR
NHA)
-1L 31-3326-23 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR M RF
NHA)
-1M 31-3326-25 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR N RF
NHA)
-1N 31-3881-1 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR P RF
NHA)
-1P 31-3881-3 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR Q RF
NHA)
-1Q 31-3881-5 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR R RF
NHA)
-1R 31-3881-7 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR S RF
NHA)
-1S 31-3881-9 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR T RF
NHA)
-1T 31-3881-11 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR U RF
NHA)
-1U 31-3881-17 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR V RF
NHA)
-1V 31-3881-19 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR W RF
NHA)
-1W 31-3881-25 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR X RF
NHA)

- Item Not Illustrated

33-40-59 Page 1019

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 -1X 31-3881-27 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR Y RF

NHA)
-1Y 31-3881-29 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR Z RF
NHA)
-1Z 31-3881-31 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AA RF
NHA)
-2 31-3881-33 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AB RF
NHA)
-2A 31-3881-35 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AC RF
NHA)
-2B 31-3881-37 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AD RF
NHA)
-2C 31-3881-39 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AE RF
NHA)
-2D 31-3881-41 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AF RF
NHA)
-2E 31-3881-43 LIGHT SUBASSEMBLY (SEE IPL FIGURE 1 FOR AG RF
NHA)
5 41-1225-1 . COVER, DRAIN HOLE (MODIFIED PER A-M, 2
SB 30-1033-33-SB01) P-AC,
AE-AG
-5A A7794 . TUBE, DRAIN (TPN A-7794) AC 2
10 31-3851-1 . RETAINER, LENS (MODIFIED PER A-M, 1
SB 30-1033-33-0095) P-AB,
AD-AG
-10A A7635A . BAND, RETAINER (TPN A-7635A) N 1
(MODIFIED PER SB 30-1033-33-0095)
-10B 31-3851-3 . RETAINER, LENS AC 1
(ATTACHING PARTS)
15 MS35206-212 . SCREW, PAN HEAD A-M 3
-15A MS35206-214 . SCREW, PAN HEAD (MODIFIED PER P-AG 3
SB 30-1033-33-0095)
-------*-------
-20 31-4079-1 . LENS ASSEMBLY (RED) A-C,E, 1
K,M,U,
W,Z-AB,
AE
-20A 31-4079-3 . LENS ASSEMBLY (WHITE/CLEAR) D,F-J, 1
(MODIFIED PER SB 30-1033-33-0095) L,T,Y
-20B 31-4079-29 . LENS ASSEMBLY (WHITE/CLEAR) N 1
(MODIFIED PER SB 30-1033-33-0095)
-20C 31-4079-7 . LENS ASSEMBLY (WHITE/CLEAR) P,R 1
-20D 31-4079-5 . LENS ASSEMBLY (RED) Q,S,X 1
-20E 31-4079-17 . LENS ASSEMBLY (RED/WHITE) V 1
-20F 31-4079-9 . LENS ASSEMBLY (RED) AC,AD 1

- Item Not Illustrated

33-40-59 Page 1020

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2-20G 31-4079-31 . LENS ASSEMBLY (RED) AF 1

-20H 31-4079-33 . LENS ASSEMBLY (RED) AG 1
25 MS35206-225 . . SCREW, PAN HEAD A-M, 1
P-AB,
AE-AG
30 MS35338-41 . . WASHER, LOCK A-M, 1
P-AB,
AE-AG
35 41-1457-7 . . TUBE, DRAIN A-M, 1
P-AG
-35A 11706-3 . . TUBE, DRAIN N 1
(ATTACHING PARTS)
40 11661 . . INSERT, THREADED 1
45 60-0258-3 . . WASHER, TEFLON 1
50 A9292-3 . . WASHER, FLAT (TPN A-9292-3) 1
-------*-------
-55 A9292-1 . . DELETED NP
60 25-0918-21C . . LENS (RED) A-C,E, 1
K,M,U,W,
Z-AE
-60A 25-0918-23C . . LENS (WHITE/CLEAR) D,F-J, 1
L,T,Y
-60B 25-0956-23C . . LENS (WHITE/CLEAR) N 1
-60C 25-0918-23 . . LENS (WHITE/CLEAR) P,R 1
-60D 25-0918-21 . . LENS (RED) Q,S,X 1
-60E 25-0921-1 . . LENS (RED/WHITE) V 1
-60F 25-0918-21C3 . . LENS (RED) (TPN 25-0918-21C-3) AF 1
-60G 25-0918-21C5 . . LENS (RED) (TPN 25-0918-21C-5) AG 1
65 60-5023-3 . GASKET (MODIFIED PER SB 30-1033-33-SB01) 2
-65A 86-0512-1 . DELETED NP

-65B 86-0512-3 . DELETED NP

-70 MS35206-226 . DELETED NP
-75 A4253-1 . DELETED NP
-80 A3934 . DELETED NP
-85 MS35338-41 . DELETED NP
-90 A8966-1 . DELETED NP
-95 A7941 . DELETED NP
100 31-3353-1 . FLASHTUBE LAMP ASSEMBLY (DS1) A-S,V-X, 1
(SEE IPL FIGURE 4 FOR DETAILS) AA
-100A 31-3353-3 . FLASHTUBE LAMP ASSEMBLY (DS1) T,U,Y,Z, 1
(SEE IPL FIGURE 4 FOR DETAILS) AB-AG

- Item Not Illustrated

33-40-59 Page 1021

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 105 A7632-2 . GASKET (TPN A-7632-2) N 1

(MODIFIED PER SB 30-1033-33-0095)
110 31-7988-1 . RING, MOUNTING (MODIFIED PER N 1
SB 30-1033-33-0095)
(ATTACHING PARTS)
115 MS51957-12 . SCREW, PAN HEAD (MODIFIED PER N 3
SB 30-1033-33-0095)
-------*-------
120 A8918-1 . GASKET (TPN A-8918-1) A-D,F,G, 1
L,N-W,
Y-AA,
AC,AF,
AG
-120A 41-1035-1 . GASKET E,H,J 1
-120B 31-5921-1 . GASKET AB 1
-120C 31-8225-1 . GASKET (MODIFIED PER SB 30-1033-33-SB01) AD,AE 1
125 B8917-9 . FLANGE, MOUNTING (TPN B-8917-9) A,C,D,G, 1
P-W,
Y-AA,
AF,AG
-125A B8917-10 . FLANGE, MOUNTING (TPN B-8917-10) B,F,L,N 1
-125B B8917-11 . FLANGE, MOUNTING (TPN B-8917-11) E,H,J 1
-125C 41-0782-1 . ADAPTER K 1
-125D 31-4431-1 . FLANGE, MOUNTING X 1
-125E 31-7980-1 . FLANGE, MOUNTING AB 1
-125F 31-7997-1 . FLANGE, MOUNTING AC 1
-125G 31-8224-1 . FLANGE, MOUNTING AD,AE 1
(ATTACHING PARTS)
130 MS51863-21 . SCREW, PAN HEAD (SUPSD BY ITEM 130A) NP
-130A MS51957-26 . SCREW, PAN HEAD (SUPSDS ITEM 130) 3
-------*-------
135 MS3102R10SL3P . CONNECTOR (TPN MS3102R10SL-3P) (P1) A,D,J,P, 1
Q,T-Z,
AF,AG
-135A B8-3APLN29500 . CONNECTOR (V11139) (CO-094 - V72914) (P1) NP
(SUPSD BY ITEM 135B)
-135B 851-00-R8-3APN50 . CONNECTOR (V59610) (CO-094 - V72914) (P1) B,E,F,H 1
(SUPSDS ITEM 135A)
-135C PTO2E8-4P . CONNECTOR (V77820) (TPN PTO2E-8-4P) (CO- NP
104 - V72914) (P1) (SUPSD BY ITEM 135D)
-135D MS3120E8-4P . CONNECTOR (P1) (SUPSDS ITEM 135C) K 1
-135E MS3470L12-3P . CONNECTOR (LESS CONTACTS) (P1) L,N 1
-135F MS3470L8-3P . CONNECTOR (LESS CONTACTS) (P1) M 1

- Item Not Illustrated

33-40-59 Page 1022

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 -135G MS3116F10-6P . CONNECTOR (P1) AB 1

-135H MS3101F10SL3P . CONNECTOR (P1) AC 1
-135J D38999-26FA99PN . CONNECTOR (P1) AD,AE 1
(ATTACHING PARTS)
140 MS51863-215 . SCREW, PAN HEAD A,B,D-F, 4
H-N
-140A MS51863-216 . SCREW, PAN HEAD P,Q,T-Z, 4
AF,AG
145 MS21042-04 . NUT, HEX A,B,D-F, 4
H-N,P,Q,
T-Z,
AF,AG
-------*-------
-150 M39029-4-111 . DELETED (MOVE TO REPAIR SECTION)
-155 M39029-4-110 . DELETED (MOVE TO REPAIR SECTION)
-160 M39029-58-363 . DELETED (MOVE TO REPAIR SECTION)
-165 MS27488-16 . DELETED (MOVE TO REPAIR SECTION)
-170 MS27488-20 . DELETED (MOVE TO REPAIR SECTION)
-175 31901 . DELETED
-180 36149 . DELETED (MOVE TO REPAIR SECTION)
-185 M85049-38-9W . BACKSHELL AD,AE 1
190 MS35206-211 . SCREW, PAN HEAD T,U,Y,Z, 2
AF,AG
195 A7794 . TUBE, DRAIN (TPN A-7794) A-S,V-X, 2
AA
-195A 17489 . TUBE, DRAIN T,U,Y,Z, 2
AF,AG
200 31-3196-1 . COVER C,G 1
(ATTACHING PARTS)
205 MS35206-228 . SCREW C,G 2
-------*-------
210 601-2104-1 . BOARD, TERMINAL (V75382) (TE-616 - V72914) C,G 1
(TB1)
(ATTACHING PARTS)
215 MS35206-229 . SCREW, PAN HEAD (SUPSD BY ITEM 215A) C,G NP
-215A MS35206-231 . SCREW, PAN HEAD (SUPSDS ITEM 215) C,G 2
220 60-2485-1 . SPACER C,G 2
-------*-------
225 601-J . JUMPER (V75382) (TE-788 - V72914) C,G 1
-230 GRC614 . GROMMET (V91265) (GR-060 - V72914) R,S,AA 1
-230A MS35489-4 . GROMMET AB-AE 1

- Item Not Illustrated

33-40-59 Page 1023

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 235 MS51957-30 . SCREW, PAN HEAD R,S, 1

AA-AE
240 MS35338-136 . WASHER, LOCK R,S, 2
AA-AE
245 MS35649-264 . NUT, HEX R,S, 2
AA-AE
250 31-8244-1 . WASHER (MODIFIED PER SB 30-1033-33-SB01) AE 1
255 41-1192-1 . DIAPHRAGM (MODIFIED PER AE 1
SB 30-1033-33-SB01)
260 41-1191-3 . HOUSING (MODIFIED PER SB 30-1033-33-SB01) AE 1
265 31-3319-1 . BASE A,D,J,P, 1
Q,T-Z,
AF,AG
-265A 31-3319-3 . BASE B,E,F,H, 1
K,M
-265B 31-3319-5 . BASE C,G 1
-265C 31-3319-11 . BASE L,N 1
-265D 31-3319-9 . BASE R,S,AA 1
-265E 31-3319-13 . BASE AB,AD 1
-265F 31-3319-15 . BASE AC 1
-265G 31-3319-17 . BASE (MODIFIED PER SB 30-1033-33-SB01) AE 1
(ATTACHING PARTS)
270 SC727 . SCREW, FLAT HEAD (TPN SC-727) 3
-------*-------
275 31-3325-1 . PRINTED CIRCUIT BOARD ASSEMBLY (SUPSD NP
BY ITEM 275B) (SEE FIGURE 3 FOR
DETAILS)
-275A 31-3325-5 . PRINTED CIRCUIT BOARD ASSEMBLY (SUPSD NP
BY ITEM 275C) (SEE FIGURE 3 FOR
DETAILS)
-275B 31-3325-7 . PRINTED CIRCUIT BOARD ASSEMBLY (SUPSDS A-Q,T-Z, 1
ITEM 275) (SEE FIGURE 3 FOR DETAILS) AB-AG
-275C 31-3325-11 . PRINTED CIRCUIT BOARD ASSEMBLY (SUPSDS R,S,AA 1
ITEM 275A) (SEE FIGURE 3 FOR DETAILS)
(ATTACHING PARTS)
280 MS35206-213 . SCREW, PAN HEAD (SUPSD BY ITEM 280A) A-N NP
-280A MS35206-215 . SCREW, PAN HEAD (SUPSDS ITEM 280) A-N 1
-280B MS35206-216 . SCREW, PAN HEAD P-AG 1
285 MS21042-04 . NUT A-N 1
290 MS35206-228 . SCREW, PAN HEAD A,B,D-F, 1
H-AG
-290A MS35206-226 . SCREW, PAN HEAD C,G 1
295 SC727 . SCREW, FLAT HEAD (TPN SC-727) 1
-------*-------

- Item Not Illustrated

33-40-59 Page 1024

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

2 300 31-3320-1 . RETAINER ASSEMBLY 2

(ATTACHING PARTS)
305 SC359 . SCREW, FLAT HEAD (TPN SC-359) 4
-------*-------
310 31-3321-1 . CAPACITOR ASSEMBLY (C9-C12) (SUPSD BY NP
ITEM 310A)
-310A 31-3321-3 . CAPACITOR ASSEMBLY (C9-C12) (SUPSDS 2
ITEM 310)
-315 31-3318-1 . HOUSING ASSEMBLY A-L, 1
N-AB,
AF,AG
-315A 31-3318-7 . HOUSING ASSEMBLY M 1
-315B 31-3318-9 . HOUSING ASSEMBLY AC 1
-315C 31-3318-13 . HOUSING ASSEMBLY AD,AE 1
320 81-0849-9 . . GUIDE 1
(ATTACHING PARTS)
325 MS20426A2-3 . . RIVET 2
-------*-------
330 31-3318-3 . . HOUSING A-L, 1
N-AB,
AF,AG
-330A 31-3318-5 . . HOUSING M 1
-330B 31-3318-3 . . HOUSING AC 1
-330C 31-3318-3 . . HOUSING AD,AE 1

- Item Not Illustrated

33-40-59 Page 1025

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

REF ITEM REF ITEM REF ITEM REF ITEM

DES NUMBER DES NUMBER DES NUMBER DES NUMBER
C1 60 CR9 125 R12 170 R26 135
C2 65 L1 100 R13 145 R27, R28 205
C3 70 R1 140 R14 200 SCR1 210
C4, C5 75 R2, R3 145 R15 175 Q1 215
C7 80 R4 150 R16 130 Q2 220
C8 85 R5 200 R17 190 Q3 50
C13 90B R6 145 R19 180 T1 230
C14 95 R7 155 R20 200 U1 105
C15 90B R8 145 R21 185 VR1 120
CR1-CR5 110 R9 160 R22 195
CR6, CR7 115 R10 145 R23, R24 155
CR8 110 R11 165 R25 190

Printed Circuit Board Assembly

IPL Figure 3

33-40-59 Page 1026

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 -1 31-3325-1 PRINTED CIRCUIT BOARD ASSEMBLY (SUPSD BY A NP

ITEM 1B) (SEE IPL FIGURE 2 FOR NHA)
-1A 31-3325-5 PRINTED CIRCUIT BOARD ASSEMBLY (SUPSD BY B NP
ITEM 1C) (SEE IPL FIGURE 2 FOR NHA)
-1B 31-3325-7 PRINTED CIRCUIT BOARD ASSEMBLY (SUPSDS C RF
ITEM 1) (SEE IPL FIGURE 2 FOR NHA)
-1C 31-3325-11 PRINTED CIRCUIT BOARD ASSEMBLY (SUPSDS D RF
ITEM 1A) (SEE IPL FIGURE 2 FOR NHA)
5 31-3322-1 . BRACKET 1
(ATTACHING PARTS)
10 55-0206-21 . SCREW, PAN HEAD (SUPSD BY ITEM 10A) NP
-10A 55-0207-01 . SCREW, PAN HEAD (SUPSDS ITEM 10) 1
15 66-2513-3 . NUT 1
-------*-------
20 31-3323-1 . BRACKET (SUPSD BY ITEM 20B) NP
-20A 31-3323-3 . DELETED
-20B 31-3323-5 . BRACKET (SUPSDS ITEM 20) 1
(ATTACHING PARTS)
25 MS35206-227 . SCREW, PAN HEAD 1
-------*-------
30 31-3492-1 . BRACKET 1
30 31-3492-5 . DELETED
(ATTACHING PARTS)
35 MS35206-229 . SCREW, PAN HEAD A,B 1
-35A MS35206-228 . SCREW, PAN HEAD C,D 1
40 MS21042-06 . NUT A,B 1
-40A REF001 . TERMINAL, SOLDER (V71279) (TE-595 - V72914) C,D 1
(TPN 572-4851-01-05-16)
-------*-------
45 60-1521-9 . INSULATOR 1
50 55-0363-1 . TRANSISTOR (Q3) A, B 1
-50A BUW50 . TRANSISTOR (V66958) (TR-2375 - V72914) (Q3) C, D 1
55 14828 . INSULATOR 1
60 REF002 . CAPACITOR, 0.22 µF, 500 V A, B NP
(TPN 8131-050-651-224M) (C1)
(SUPSD BY ITEM 60B)
-60A SK047C224KAA . CAPACITOR, 0.22 µF, 500 V (V96095) C 1
(CA-968 - V72914) (MODIFIED PER
SB 30-1033-33-SB02) (C1)

- Item Not Illustrated

33-40-59 Page 1027

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 -60B SR215E224MAA . CAPACITOR, 0.22 µF, 50 V (V04222) A, B, D 1

(CA-326 - V72914) (C1) (SUPSDS ITEM 60)
65 150D685X9035B2 . CAPACITOR, 6.8 µF, 35 V (V56289) 1
(CA-489 - V72914) (C2)
70 55-1037-151AJ14 . CAPACITOR, 150 µF, 50 V (C3) 1
75 DDM103 . CAPACITOR, 0.1 µF, 150 V (V99942) 2
(TPN DDM-103) (CA-212 - V72914) (C4, C5)
80 PMT2R22K400 . CAPACITOR, 0.22 µF, 400 V (V14433) (C7) NP
(SUPSD BY ITEM 80A)
-80A SK047C224KAA . CAPACITOR, 0.22 µF, 500 V (V96095) 1
(CA-968 - V72914) (C7) (SUPSDS ITEM 80) -
(MODIFIED PER SB 30-1033-33-SB02)
85 55-0679-1051AF . CAPACITOR, 1.0 µF, 50 V (C8) 1
-90 192P47392 . CAPACITOR, 0.047µF, 200 V (V56289) (C13) A,B NP
(SUPSD BY ITEM 90A)
-90A 192P473X9200 . CAPACITOR, 0.047 µF, 200 V (V56289) A,B 1
(CA-274 - V72914) (C13) (SUPSDS ITEM 90)
90B 192P473X9200 . CAPACITOR, 0.047 µF, 200 V (V56289) C, D 2
(CA-274 - V72914) (C13, C15)
95 DD102 . CAPACITOR, 0.001 MF, 1000 V (V99942) 1
(CA-186 - V72914) (C14)
100 55-0712-1 . CHOKE (L1) 1
105 55-0478-14 . COMPARATOR, QUAD (U1) 1
110 55-0997-1 . DIODE (CR1-CR5, CR8) 6
115 1N5399 . DIODE (V05277) (RC-490 - V72914) (CR6, CR7) NP
(SUPSD BY ITEM 115A)
-115A BYV96E . DIODE (V25403) (TPN BYV96-E) (CR6, CR7) 2
(RC-485 - V72914) (SUPSDS ITEM 115)
120 1N4740A . DIODE (V04713) (RC-635 - V72914) (VR1) 1
125 1N751A . DIODE (V04713) (RC-620 - V72914) (CR9) NP
(SUPSD BY ITEM 125A) (MODIFIED PER
SB 30-1033-33-SB02)
-125A 1N4731 . DIODE, ZENER (V15873) (RC-604 - V72914) 1
(VR2) (SUPSDS ITEM 125) (MODIFIED PER
SB 30-1033-33-SB02)
130 72XWR10K . POTENTIOMETER, 10 K OHM, 1/2 W (V73138) 1
(RH-239 - V72914) (R16)
135 72XWR500K . POTENTIOMETER, 500 K OHM, 1/2 W (V73138) 1
(RH-275 - V72914) (R26)
140 55-0382-1025DS . RESISTOR, FIXED, 1.0 K OHM, 5%, 1/2 W (R1) 1
145 55-0382-1045CS . RESISTOR, FIXED, 100 K OHM, 5%, 1/4 W 6
(R2, R3, R6, R8, R10, R13)
150 55-0382-6835CS . RESISTOR, FIXED, 6.8 K OHM, 5%, 1/4 W (R4) 1

- Item Not Illustrated

33-40-59 Page 1028

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 155 55-0382-1055CS . RESISTOR, FIXED, 1 M OHM, 5%, 1/4 W 3

(R7, R23, R24)
160 55-0382-2225CS . RESISTOR, FIXED, 2.2 K OHM, 5%, 1/4 W (R9) 1
165 55-0382-4745CS . RESISTOR, FIXED, 470 K OHM, 5%, 1/4 W (R11) 1
170 55-0382-3345CS . RESISTOR, FIXED, 330 K OHM, 5%, 1/4 W (R12) 1
175 55-0382-2255DS . RESISTOR, FIXED, 2.2 M OHM, 5%, 1/2 W (R15) 1
180 55-0225-10015D . RESISTOR, FIXED, 1 K OHM, 2 1/4 %, 5 W (R19) 1
185 55-0382-2215CS . RESISTOR, FIXED, 220 OHM, 5%, 1/4 W (R21) 1
190 55-0382-1025CS . RESISTOR, FIXED, 1 K OHM, 5%, 1/4 W 2
(R17, R25)
195 55-0225-30R03F . RESISTOR, FIXED, 30 OHM, 3%, 3 W (R22) 1
200 55-0382-4725CS . RESISTOR, FIXED, 4.7 K OHM, 5%, 1/4 W 3
(R5, R14, R20)
205 55-0225-10R03F . RESISTOR, FIXED, 10 OHM, 3%, 3 W (R27, R28) C, D 2
210 S4001MS3 . RECTIFIER, SILICON CONTROLLED (V27194) NP
(RC-880 - V72914) (SCR1) (SUPSD BY
ITEM 210A) (MODIFIED PER
SB 30-1033-33-SB02)
-210A MCR22-6 . RECTIFIER, SILICON CONTROLLED (V04713) 1
(RC-350 - V72914) (SCR1) (SUPSDS
ITEM 210) (MODIFIED PER
SB 30-1033-33-SB02)
215 2N2222 . TRANSISTOR (V04713) (TR-115 - V72914) (Q1) NP
(SUPSD BY ITEM 215A)
-215A JAN2N2222A . TRANSISTOR (Q1) (SUPSDS ITEM 215) 1
220 2N2222 . TRANSISTOR (V04713) (TR-115 - V72914) (Q2) NP
(SUPSD BY ITEM 220A)
-220A ZTX849 . TRANSISTOR (VK1196) (TR-0916 - V72914) (Q2) 1
(SUPSDS ITEM 220)
225 7717-157T . PAD, MOUNTING (USED UNDER Q1 AND Q2) NP
(V13103) (TR-343 - V72914)
(SUPSD BY ITEM 225A)
-225A M38527-08-043P . PAD, MOUNTING (USED UNDER Q1) 1
(SUPSDS ITEM 225)
230 55-0713-1 . TRANSFORMER (T1) A, B 1
-230A 55-0713-5 . TRANSFORMER (T1) C, D 1
235 43-02-37 . INSULATOR (USED UNDER T1) (V13103) 1
(TR-355 - V72914)
240 1D3-8B . TERMINAL (V86577) (TE-524 - V72914) NP
(SUPSD BY ITEM 240A)
-240A 10-214-2-01 . TERMINAL (V18310) (TE-524 - V72914) 4
(SUPSDS ITEM 240)
245 31-3324-1 . BOARD, PRINTED CIRCUIT NP

- Item Not Illustrated

33-40-59 Page 1029

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

3 -250 CB1055S . DELETED

-255 55-0225-10015A . DELETED
-260 7717158T . DELETED
-265 31879 . DELETED (MOVED TO REPAIR SECTION)

- Item Not Illustrated

33-40-59 Page 1030

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

This page left blank intentionally.

33-40-59 Page 1031

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

Flashtube Lamp Assembly

IPL Figure 4

33-40-59 Page 1032

Sep 15/99
 GRIMES AEROSPACE COMPANY
COMPONENT MAINTENANCE MANUAL
PART NUMBER 30-1033

FIG. & UNITS

ITEM AIRLINE NOMENCLATURE EFF PER
NO. PART NUMBER STOCK NO. 1 2 3 4 5 6 7 CODE ASSY

4 -1 31-3353-1 FLASHTUBE LAMP ASSEMBLY (DS1) (SEE IPL A RF

FIGURE 2 FOR NHA)
-1A 31-3353-3 FLASHTUBE LAMP ASSEMBLY (DS1) (SEE IPL B RF
FIGURE 2 FOR NHA)
5 31-1604-9 . REFLECTOR 1
(ATTACHING PARTS)
10 MS35649-262 . NUT 1
15 MS35338-41 . WASHER, LOCK 1
-------*-------
20 60-2227-1 . SPACER 3
25 31-2622-1 . CLAMP 1
30 55-0283-1 . FLASHTUBE, QUARTZ A 1
-30A 55-0283-3 . FLASHTUBE, QUARTZ B 1
35 31-2622-5 . CLAMP 1
40 31-1604-11 . REFLECTOR 1
45 31-2101-5 . REFLECTOR 2
50 55-0211-25PB . SCREW, PAN HEAD 1
55 55-0211-26PB . SCREW, PAN HEAD 2
60 3585-06CN0138 . INSERT (V01556) (TPN 3585-06CN-0138) 1
65 31-2836-1 . BARRIER 1
70 31-3694-1 . TRIGGER COIL ASSEMBLY (T2) 1

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