Atch_7_-_T.O._1C-130H-2-12JG-20-1.PDF

TO 1C-130H-2-12JG-20-1

TECHNICAL MANUAL

JOB GUIDE

ORGANIZATIONAL MAINTENANCE

GROUND HANDLING

LUBRICATION

USAF SERIES

ALL C-130

AIRCRAFT

ATOS/DLDSS

DISCLOSURE NOTICE - This information is furnished upon the condition that it will not be released to another nation without the specific authority of the Department of the Air Force of the United States, that it will be used for military purposes only, that individual or corporate rights originating in the information, whether patented or not, will be respected, that the recipient will report promptly to the United States, any known or suspected compro-mise, and that the information will be provided substantially the same degree of security afforded it by the Department of Defense of the United States. Also, regardless of any other markings on the document, it will not be downgraded or declassified without written approval of the originating United States agency.

DISTRIBUTION STATEMENT D - Distribution authorized to the Depart-ment of Defense and U.S. DoD contractors only (Administrative or Opera-tional Use) (30 September 1997). Refer other requests for this document to AFLCMC/WIUEG, Robins AFB, GA 31098.

WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.)

or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App.

2401 et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE - Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

Published under authority of the Secretary of the Air Force

14 DECEMBER 1990

CHANGE 42 - 15 OCTOBER 2015

BASIC AND ALL CHANGES HAVE BEEN MERGED TO MAKE THIS A COMPLETE PUBLICATION

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

LIST OF EFFECTIVE PAGES

NOTE: The portion of the text affected by the changes is indicated by a vertical line in the outer margins of the page.

Changes to illustrations are indicated by miniature pointing hands.

Dates of issue for original and changed pages are:

Original............................. 0.......... 14 December 1990 Change.............................. 1................... 27 May 1994 Change.............................. 2................... 27 July 1995 Change.............................. 3..........13 November 1995 Change.............................. 4................... 18 July 1996 Change.............................. 5.......... 31 December 1996 Change.............................. 6................31 March 1997 Change.............................. 7.........30 September 1997 Change.............................. 8.........30 September 1998 Change.............................. 9..............31 October 1998 Change.............................10..........30 November 1998 Change.............................11................... 31 July 1999 Change.............................12...............26 August 1999 Change.............................13.........30 September 1999 Change.............................14..................... 1 July 2000 Change.............................15................1 October 2001 Change.............................16..................... 1 July 2002 Change.............................17...............15 August 2002 Change.............................18..................1 March 2003 Change.............................19.................. 15 June 2003 Change.............................20...............15 August 2003 Change.............................21........... 15 February 2004 Change.............................22..................... 1 May 2004 Change.............................23.................1 August 2004 Change.............................24............1 November 2004 Change.............................25...............1 January 2005 Change.............................26..................1 March 2005 Change.............................27..............15 October 2005 Change.............................28..........15 November 2005 Change.............................29.................. 15 June 2006 Change.............................30..............15 October 2006 Change.............................31.................. 15 June 2007 Change.............................32...........1 September 2007 Change.............................33.................... 1 April 2008 Change.............................34.................. 15 June 2009 Change.............................35.......... 15 December 2009 Change.............................36............ 1 December 2010 Change.............................37..................... 1 July 2011 Change.............................38............. 1 February 2013 Change.............................39................... 15 July 2013 Change.............................40.................. 15 April 2014 Change.............................41................... 15 July 2014 Change.............................42..............15 October 2015

*Zero in this column indicates an original page

A Change 42 USAF

LIST OF EFFECTIVE PAGES (CONT)

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 116, CON-

SISTING OF THE FOLLOWING:

Page *Change Page *Change No. No. No. No.

Title A - C i ii Blank ii.1 ii.2 iii iv v vi Blank 1-1 1-2 - 1-3 1-4 1-5 1-6 - 1-7 1-8 1-9 1-10 1-11 1-12 - 1-13 1-14 Blank 1-15 - 1-17 1-18 1-19 1-20 1-21 1-22 1-23 - 1-24 1-25 - 1-28 1-29 1-30 Blank

1-31 1-32 1-33 1-34 1-35 1-36 1-36.1 1-36.2 Blank 1-37 - 1-39 1-40 Blank 1-41 1-42 1-43 1-44 1-45 - 1-47 1-48 1-48.1 1-48.2 Blank Added 1-49 1-50 1-51 1-52 1-52.1 1-52.2 Blank Added 1-53 1-54 - 1-55 1-56 1-56.1 Added 1-56.2 Blank Added 1-57 1-58

Change 42 B

LIST OF EFFECTIVE PAGES (CONT)

Page *Change Page *Change No. No. No. No.

1-59 1-60 - 1-61 1-62 1-63 - 1-64 1-64.1 Added 1-64.2 Blank Added 1-65 1-66 1-67 1-68 1-68.1 - 1-68.2 1-69 1-70 1-71 1-72 1-73 1-74 1-74.1 1-74.2 Blank 1-75 1-76 1-77 1-78 1-78.1 1-78.2 1-78.3 1-78.4 Added 1-79 1-80 - 1-81 Blank 1-82 1-83 - 1-84 Deleted 1-85 Blank 1-86 1-87 - 1-88 Added

C Change 42

TABLE OF CONTENTS

Function/Task Title S/S/SN

SAFETY SUMMARY

INTRODUCTION

Scope Use Arrangement Illustrations Safety and Health Hazards Improvement Reports Abbreviations and Acronyms Record of Applicable Time Compliance

Technical Orders

SECTION 1. LUBRICATION PROCEDURES

General Lubrication Requirements .........................12-20-01 Lubrication of Aileron Components .........................12-20-02 Lubrication of Rudder Components.........................12-20-03 Lubrication of Elevator Components .......................12-20-04 Lubrication of Flap Components..............................12-20-05 Lubrication of Flight Station Components..............12-20-06 Lubrication of Main Gear Components ...................12-20-07 Lubrication of Nose Gear Components....................12-20-08 Lubrication of Crew, Paratroop, Emergency

Exit, and 25MM Autoloading Access Door Components............................................................12-20-09

Lubrication of Ramp and Cargo Door Components............................................................12-20-10

Lubrication of Engine and Propeller Components............................................................12-20-11

Lubrication of Miscellaneous Components..............12-20-12

Change 42 i/(ii blank)

SAFETY SUMMARY

The following are general safety precautions and instruc-tions that must be understood and applied during many phases of operation and maintenance to ensure personnel safety and health and the protection of Air Force property.

Portions may be repeated elsewhere in this publication for emphasis.

ALIPHATIC NAPHTHA

Aliphatic naphtha is flammable and toxic to skin, eyes, and respiratory tract. Avoid skin and eye contact. Good general ventilation is normally adequate. Keep away from open flames or other sources of ignition.

HYDRAULIC FLUID, ENGINE OIL, LUBRICATING OIL, DRY

CLEANING SOLVENT

Use of Reformulated Dow Corning 321 or Perma-Silk Rac can cause respiratory track irritation. See local bioengineer-ing and safety for Personal Protection Equipment (PPE) requirements.

Hydraulic fluid, engine oil, lubricating oil, and dry cleaning solvent, are toxic to skin, eyes, and respiratory tract. Avoid skin and eye contact. Good general ventilation is normally adequate.

Isopropyl alcohol is flammable and toxic. Good general ven-tilation is normally adequate. Skin and eye protection is required. Avoid all sources of ignition.

MOLYBDENUM DISULFIDE GREASE

Molybdenum disulfide grease is toxic to eyes, skin, and respiratory tract. Eye and skin protection required. Unless waived by local Bioenvironmental Engineer, use in a well ventilated area.

Change 26 ii.1

SAFETY SUMMARY - Continued

SOLID FILM LUBRICANT, TEFLON SPRAY, AND CORRO-

SION PREVENTIVE COMPOUND

Solid film lubricant, teflon spray, and corrosion preventive compound are flammable and toxic. Good general ventila-tion is normally adequate. Skin and eye protection is required. Avoid all sources of ignition.

DEPRESSURIZED/DEACTIVATE HYDRAULIC SYSTEM

Prior to lubricating flight control components depressurize the auxiliary and utility hydraulic system in accordance with TO 1C-130H-2-05JG-00-1, 05-00-14 or TO 1C-130(M)H-2-05JG-00-1, 05-00-14. In addition, deactivate the auxiliary and utility hydraulic system in accordance with TO 1C-130H-2-05JG-00-1, 05-00-16 or TO

1C-130(M)H-2-05JG-00-1, 05-00-16.

ii.2 Change 37

INTRODUCTION

NOTE All references (if any), in this manual, pertaining to MC-130W airplanes shall now be known as AC-130W airplanes. Any Technical Order (TO) ref-erences to the 1C-130(M)W series shall apply to the corresponding 1C-130(A)W TO. Technical Orders in the 1C-130(M)W series will be transitioned to 1C-130(A)W TO numbers as changes are made to the TO.

NOTE It is very important that the following information be read carefully before using this job guide manual.

This introduction describes the use and arrangement of the manual.

SCOPE.

This manual provides illustrated organizational level main-tenance procedures for lubricating the C-130.

The complete listing of the OMMS is located in TO

1C-130H-2-00GE-00-1.

USE.

This manual has been developed for lubricating the C-130 airplane. Illustrations are provided as a more effective way of using the manual for lubrication tasks.

ARRANGEMENT.

Instructions in this manual are arranged in a function/task format. A task begins with a text page to identify the com-ponents being lubricated. The remaining pages in the task are illustrations of lubrication points.

A function is made up of a task or series of tasks and illus-trations which support lubrication of a system or component.

All steps within a task must be accomplished to complete the task. All tasks within a function must be accomplished to complete the function.

Change 38 iii

Lubrication procedures only locate and WARNING identify lubrication requirements.

These procedures do not give detailed instructions for access or system oper-ation. Observe all system operating procedures and safety precautions in the appropriate maintenance manuals when a system needs to be operated.

Failure to comply could cause injury to personnel and damage to the airplane.

ILLUSTRATIONS.

Illustrations include a location view of equipment and the name for each component part to be lubricated. The name of each lubrication point is identified and located with an index arrow. Each lubrication point includes a symbol to represent the type and method of lubrication. When neces-sary, delta notes are used when further details about the lubrication type or method is required.

Door and actuator positions, control settings, and indication displays shown on illustrations may not match the actual equipment configuration during lubrication.

SAFETY AND HEALTH HAZARDS.

Lubrication activities involve the use of some hazardous lubricants. Also, movement of control surfaces or landing gear can easily injury a mechanic. See Safety Summary for warnings that apply to this volume.

IMPROVEMENT REPORTS.

Recommendations for improvements to this technical order shall be submitted on AFTO Form 22, Technical Manual (TM) Change Recommendation and Reply. Complete AFTO Form 22 in accordance with TO 00-5-1.

iv Change 20

ABBREVIATIONS AND ACRONYMS.

The following abbreviations and acronyms are used in this manual:

NTS Negative Torque System

S/S/SN System/Subsystem/Sub-subsystem Number

RECORD OF APPLICABLE TIME COMPLIANCE TECHNICAL

ORDERS.

The record of applicable time compliance technical orders is a list of all Time Compliance Technical Orders (TCTO) which affect the technical content (text or illustration) of this manual.

Only current TCTO are listed. A TCTO is deleted from the list when any of the following occurs:

a. The equipment configuration to which the TCTO is applicable is no longer covered in the manual.

b. The TCTO is rescinded.

c. The TCTO is superseded or replaced.

TCTO No. Title TCTO Date

1C-130-2031 Installation of 4 Sep 2013 Square Observer Window Paratroop Door on Selected C-130 Aircraft

Change 42 v/(vi blank)

SECTION 1

LUBRICATION PROCEDURES

1-1. GENERAL LUBRICATION REQUIREMENTS.

1. General Information. Lubricated surfaces shall be cleaned of moisture, solvents, and contaminants. Never apply lubri-cant over rusted or corroded surfaces. Do not allow body moisture or other agents to contact highly polished surfaces before lubrication. Contact with moisture may cause corro-sion on the polished surfaces. Throughout this manual, speci-fication numbers not preceded by MIL are to be interpreted as Federal Specification numbers.

2. Solid Film Lubrication. The application of solid-film lubri-cant is a manufacturing step that involves cleaning, spraying, and baking. When the film is permanently damaged, the part should be completely refinished or replaced. Solid-film lubri-cant can be identified by a dark gray color which will rub off slightly.

Molybdenum disulfide is flammable and WARNING toxic to skin, eyes, and respiratory tract.

Avoid skin and eye contact. Good general ventilation is normally adequate. Keep away from open flames or other sources of ignition.

Solid-film lubricated parts should not be treated with a wet lubricant. It is permissible to treat undamaged lubricated parts with molybdenum disulfide, Specification MIL-M-7866.

If molybdenum disulfide is used to lubricate the area, a permanent record shall be made and the area inspected frequently.

3. Lubrication Application. Lubricants shall be applied as follows:

a. Clean and dry grease guns and oil cans before filling.

12-20-01 1-1

Aliphatic naphtha is flammable and WARNING toxic to skin, eyes, and respiratory tract. Avoid skin and eye contact.

Good general ventilation is normally adequate. Keep away from open flames or other sources of ignition.

b. Clean brushes with aliphatic naphtha and dry thoroughly before use.

c. Clean surfaces thoroughly with aliphatic naph-tha for better adhesion before applying a brush or spray-on type lubricant.

d. Use clean lubricants only.

e. Wipe grease fittings, oil holes, etc. with clean, dry cloths before lubricating.

f. Remove dirt or rust from surfaces to be lubricated.

g. If practical, work moving parts to ensure thor-ough lubrication.

h. Force grease into fittings until old grease is forced out unless otherwise noted. Old caked grease has a tendency to attract moisture causing corrosion.

i. Fill oil holes to nearly full. Add oil until level does not drop. Squirt-oil cans are recommended for oil application.

j. Clean excess lubricant from all but the work-ing surfaces.

1-2 Change 29

Isopropyl alcohol is flammable and WARNING toxic. Good general ventilation is nor-mally adequate. Skin and eye protec-tion is required. Avoid all sources of ignition.

CAUTION Do not use MIL-PRF-680 Type II solvent on door seals. Only use aliphatic naph-tha or isopropyl alcohol.

k. Clean rubber door seals with aliphatic naphtha or isopropyl alcohol only. Do not allow solvent to dry on door seals. Wipe seals with a separate, clean cloth before solvent has a chance to dry. Repeat as necessary until door seals are clean. Lubricate natural or neoprene rubber (black color) with molybdenum disulfide only. Silicone rubber door seals do not require lubrication.

l. Use Stewart-Warner Corporation nozzle (part No. 314150) on grease guns when applying lubricant to an NAS516 grease fitting.

m. Use Alemite hydraulic coupler (part No.

6304-B) on grease guns when applying lubricant to grease fittings MS15000 through MS15006.

n. Piano-type hinges are lubricated with solid film lubricant except for aileron, rudder, and elevator trim tabs. On LOX servicing door hinges, use MIL-G-27617 Type I, II, or III grease. If trim tabs are binding, remove, clean, and lubricate hinge pins with Specification VV-L-800 lubri-cating oil. Reinstall hinge pin and wipe off excess oil.

Replace hinge pin if solid film lubricant is worn away.

Install new pin with Specification MIL-C-16173, Grade 4 corrosion preventative compound.

4. Lubricants. See the table of lubricants for a particular application.

5. Lubrication Symbols. See the table of lubrication sym-bols for a particular application.

Change 29 1-3

Federal/ NATO Military Num- Specification/ Type of

Symbol ber Part Number Lubricant

LTG MIL-L-23699 Lubricating oil, aircraft turbine engines

GIA MIL-G-23827 Grease. Aircraft and in-struments gear and actua-tor screws

OGP MIL-L-7870 Lubricating oil. General purpose, low temperature

MDO DOD-L-25681 Lubricating oil, Molybde-num disulfide, high tem-perature

OHA MIL-H-83282 Hydraulic fluid

OHC MIL-H-6083 Hydraulic equipment pre- Type I servative fluid

ASG MIL-M-7866 Molybdenum disulfide

GEL MIL-G-7421 Grease. Extreme low tem-perature

MDG MIL-G-21164 Grease. Molybdenum di-sulfide (low and high tem-peratures)

WTR MIL-G-81322 Grease. General purpose, wide temperature range

GG MIL-C-16173, Grease. Corrosion Preven- Grade 4 tive Compound

1-4 Change 8

Federal/ Military

Specification/ Type of Symbol NATO Part Number Lubricant

SFD PERMA-SLIK Solid film lubricant.

RAC Aerosol

REFORMULAT- Solid film lubricant.

ED DOW CORN- Aerosol

ING 321

DC321-NEW Solid film lubricant.

(LIQUID) Liquid

MIL-PRF-63460 Solid film lubricant.

Liquid

OAI MIL-L-6085 Instrument oil

PL VV-L-800 Preservative lubricating oil

PO A-A-50493 Penetrating oil

TSL MIL-L-63460 Teflon spray lubricant

GAI MIL-G-27617 Grease. Aircraft and in- Type I, II, or III strument (liquid oxygen parts and area lubri-cant)

OLG MIL-L-6086 Lubricating oil, gear, pe- (Grade M) troleum base

CPC SUPER CORR A Corrosion Preventative Compound/Lubricant Aerosol

SD-2 MIL-PRF-680 Degreasing Solvent

Change 39 1-5

1-6

1-2. LUBRICATION OF AILERON COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

12-20-02 1-7

1-2-1. LUBRICATE AILERON COMPONENTS.

1-8 Change 3

1-2-1. (Continued).

Change 11 1-9

1-2-1. (Continued)

1-10 Change 29

1-3. LUBRICATION OF RUDDER COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

12-20-03 1-11

1-3-1. LUBRICATE RUDDER COMPONENTS.

1-12 Change 32

1-3-1. (Continued)

Change 32 1-13/(1-14 blank)

1-4. LUBRICATION OF ELEVATOR COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

12-20-04 1-15

1-4-1. LUBRICATE ELEVATOR COMPONENTS.

1-16

1-4-1. (Continued).

1-17

1-4-1. (Continued)

1-18 Change 29

1-5. LUBRICATION OF FLAP COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

12-20-05 1-19

1-5-1. LUBRICATE FLAP COMPONENTS.

1-20 Change 34

1-5-1. (Continued).

Change 19 1-21

1-5-1. (Continued)

1-22 Change 33

Change 19 1-23

1-24 Change 19

1-6. LUBRICATION OF FLIGHT STATION COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

12-20-06 1-25

1-6-1. LUBRICATE FLIGHT STATION COMPONENTS.

1-26

1-6-1. (Continued).

1-27

1-28

Change 26 1-29/(1-30 blank)

1-7. LUBRICATION OF MAIN GEAR COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explanation of symbols, and general lubrication requirements.

Refer to the following list for specific lubrication tasks:

Main gear 1-7-1 Main gear doors 1-7-2 Main skis (LC-130H 1-7-3 only)

12-20-07 1-31

1-7-1. LUBRICATE MAIN GEAR COMPONENTS.

1-32 Change 39

Change 22 1-33

1-7-1. (Continued).

1-34 Change 3

Change 16 1-35

1-36 Change 19

Change 6 1-36.1/(1-36.2 blank)

1-7-2. LUBRICATE MAIN GEAR DOOR COMPONENTS.

1-37

1-7-2. (Continued).

1-38

1-7-3. LUBRICATE MAIN SKI COMPONENTS.

1-39/(1-40 blank)

1-8. LUBRICATION OF NOSE GEAR COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

Refer to the following list for specific lubrication tasks:

Nose gear 1-8-1 Nose gear doors 1-8-2 Nose ski (LC-130H only) 1-8-3 Nose steering control cable 1-8-4

12-20-08 Change 26 1-41

1-8-1. LUBRICATE NOSE GEAR COMPONENTS.

1-42

1-8-1. (Continued)

Change 35 1-43

1-8-1. (Continued).

1-44 Change 19

1-8-2. LUBRICATE NOSE GEAR DOOR COMPONENTS.

1-45

1-8-2. (Continued).

1-46

1-8-3. LUBRICATE NOSE SKI COMPONENTS.

1-47

1-8-3. (Continued)

1-48 Change 2

1-8-4. LUBRICATE NOSE STEERING CONTROL CABLE

COMPONENTS.

Change 35 1-48.1/(1-48.2 blank)

1-9. LUBRICATION OF CREW, PARATROOP,

EMERGENCY EXIT, AND 25MM AUTOLOADING

ACCESS DOOR COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

Refer to the following list for specific lubrication tasks:

Crew door 1-9-1 Paratroop door (Except 1-9-2 C-130H airplanes AF90-1057 and up and airplanes modified by

TO 1C-130-2031,

AC-130W, HC-130N/P,

or MC-130H/P air-planes).

Paratroop door (Air- 1-9-2A planes AF90-1057 and up and airplanes modi-fied by TO 1C-130-2031, AC-130W, HC-130N/P, or MC-130H/P air-planes).

Emergency exit door 1-9-3 25MM Autoloading ac- 1-9-4 cess door

12-20-09 Change 42 1-49

1-9-1. LUBRICATE CREW DOOR COMPONENTS.

1-50 Change 29

1-9-1. (Continued).

Change 9 1-51

1-9-2. LUBRICATE PARATROOP DOOR COMPONENTS

(EXCEPT C-130H AIRPLANES AF90-1057 AND UP AND AIR-

PLANES MODIFIED BY TO 1C-130-2031, AC-130W,

HC-130N/P, OR MC-130H/P AIRPLANES).

1-52 Change 42

1-9-2. (Continued)

Change 27 1-52.1/(1-52.2 blank)

1-9-2A. LUBRICATE PARATROOP DOOR COMPONENTS

(AIRPLANES AF90-1057 AND UP AND AIRPLANES MODI-

FIED BY TO 1C-130-2031, AC-130W, HC-130N/P, OR

MC-130H/P AIRPLANES).

Change 42 1-53

1-9-3. LUBRICATE EMERGENCY EXIT DOOR COMPO-

NENTS.

1-54 Change 9

1-9-3. (Continued).

Change 9 1-55

1-9-3. (Continued).

1-56 Change 34

1-9-4. LUBRICATE 25MM AUTOLOADING ACCESS

DOOR COMPONENTS.

Change 7 1-56.1/(1-56.2 blank)

1-10. LUBRICATION OF RAMP AND CARGO DOOR

COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

Refer to the following list for specific lubrication tasks:

Ramp 1-10-1 Cargo door (Except 1-10-2 AC-130W, EC-130H, and MC-130H Airplanes) Cargo door (AC-130W, 1-10-3 EC-130H, and MC-130H Airplanes)

12-20-10 Change 42 1-57

1-10-1. LUBRICATE RAMP COMPONENTS.

1-58

1-10-1. (Continued).

Change 9 1-59

1-10-2. LUBRICATE CARGO DOOR COMPONENTS

(EXCEPT AC-130W, EC-130H, AND MC-130H AIRPLANES).

1-60 Change 42

1-10-2. (Continued)

Change 42 1-61

1-10-2. (Continued).

1-62 Change 9

1-10-2. (Continued).

Change 42 1-63

1-10-3. LUBRICATE CARGO DOOR COMPONENTS

(AC-130W, EC-130H, AND MC-130H AIRPLANES).

1-64 Change 42

1-10-3. (Continued).

Change 7 1-64.1/(1-64.2 blank)

1-11. LUBRICATION OF ENGINE AND PROPELLER

COMPONENTS.

1. When lubricating NTS bracket 738338-1 refer to TO

1C-130H-2-61JG-20-1, 61-20-32.

2. Refer to 12-20-01 for a listing of lubricants, explanation of symbols, and general lubrication requirements.

12-20-11 Change 41 1-65

1-11-1. LUBRICATE ENGINE AND PROPELLER

COMPONENTS.

1-66 Change 35

1-11-1. (Continued)

Change 31 1-67

1-68 Change 24

Change 29 1-68.1

1-68.2 Change 29

1-12. LUBRICATION OF MISCELLANEOUS

COMPONENTS.

Refer to 12-20-01 for a listing of lubricants, explana-tion of symbols, and general lubrication requirements.

Refer to the following list for specific lubrication tasks:

Air deflector doors 1-12-1 Toilets 1-12-2 Life rafts 1-12-3 Flight station and scanner sta- 1-12-4 tion seats Ground test checkout valve 1-12-5 Paratroop anchor arm 1-12-6 Inflight refueling pod 1-12-7 Integrated Air Refueling System 1-12-7A Pod (MC-130H airplanes) Lubrication of nose radome 1-12-9 shock struts (HC-130P and

WC-130H)

RF switch hoist (MC-130H) 1-12-13 Condenser door actuating mech- 1-12-14 anism (EC-130H airplanes) Air handler pillow block bear- 1-12-15 ings (EC-130H Airplanes before

TCTB 1EC-130H (RF)-100)

12-20-12 Change 42 1-69

1-12-1. LUBRICATE AIR DEFLECTOR DOOR

COMPONENTS.

1-70 Change 29

1-12-2. LUBRICATE TOILET COMPONENTS.

Change 17 1-71

1-12-3. LUBRICATE LIFE RAFT COMPONENTS.

1-72

1-12-4. LUBRICATE FLIGHT STATION AND SCANNER STA-

TION SEAT COMPONENTS.

Change 17 1-73

1-12-4. (Continued)

1-74 Change 27

1-12-4. (Continued)

Change 42 1-74.1/(1-74.2 blank)

1-12-4. (Continued).

Change 7 1-75

1-12-5. LUBRICATE GROUND TEST CHECKOUT VALVE

COMPONENTS.

1-76 Change 30

1-12-5. (Continued)

Change 29 1-77

1-12-6. LUBRICATE PARATROOP ANCHOR ARM

COMPONENTS.

1-78 Change 19

1-12-7. LUBRICATE INFLIGHT REFUELING POD

COMPONENTS.

Change 36 1-78.1

1-12-7A. LUBRICATE INTEGRATED AIR REFUELING

SYSTEM POD COMPONENTS (MC-130H AIRPLANES).

1-78.2 Change 38

1-12-7A. (Continued)

Change 29 1-78.3

1-78.4 Change 28

All data on pages 1-80 and 1-81 deleted.

Change 42 1-79/(1-80 blank)

1-12-9. LUBRICATION OF NOSE RADOME SHOCK STRUTS

(HC-130P AND WC-130H).

All data on pages 1-83 through 1-85 deleted.

(1-81 blank)/1-82 Change 42

1-12-13. LUBRICATE RF SWITCH HOIST (MC-130H AIR-

PLANES ONLY).

(1-85 blank)/1-86 Change 42

1-12-14. LUBRICATE CONDENSER DOOR ACTUATING

MECHANISMS (EC-130H AIRPLANES).

Change 20 1-87

1-12-15. LUBRICATE AIR HANDLER PILLOW BLOCK

BEARINGS (EC-130H AIRPLANES BEFORE TCTB

1EC-130H(RF)-100).

1-88 Change 20