TO 1C-130A-6 - Attachment 7.pdf

Air Force Technical Order PDF 743 KB Posted Sep 12, 2009

Attached to: C-130 Aircraft Wash
Solicitation number: FA6703-09-R-0011
Issued by: Department of the Air Force Reserve Command

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TO 1C-130A-6

TECHNICAL MANUAL

AIRCRAFT SCHEDULED INSPECTION

AND MAINTENANCE INSTRUCTIONS

USAF SERIES

ALL C-130 AIRCRAFT

EXCEPT C-130J AIRCRAFT

F09603-02-D-0066

Changes in inspection requirements reflected in this publication are a result of analysis of statistical data generated through the data collection system prescribed by AFI 21-101.

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 compromise, 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 C – Distribution authorized to U.S. Government Agencies and their contractors (Administrative or Operational Use) (1 November 2003). Other requests for this document shall be referred to 580 ACSG/GFEAH, 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

1 NOVEMBER 2003

CHANGE 19 – 1 MARCH 2009

BASIC AND ALL CHANGES HAVE BEEN MERGED

TO MAKE THIS A COMPLETE PUBLICATION

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 shaded or screened areas, or by miniature pointing hands.

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.LIST OF EFFECTIVE PAGES

*Zero in this column indicates an original page.

USAF

Page *Change No. No.

Dates of issue for original and changed pages are:

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 238, CONSISTING OF THE FOLLOWING:

Original . . . . . . . . . . . . . 0 . . . . . . . . . . . 1 November 03 Change . . . . . . . . . . . . . 1 . . . . . . . . . . . . 1 February 04 Change . . . . . . . . . . . . . 2 . . . . . . . . . . . . . . . 1 April 04 Change . . . . . . . . . . . . . 3 . . . . . . . . . . . . . . . . 1 June 04 Change . . . . . . . . . . . . . 4 . . . . . . . . . . . . . . . 15 July 04 Change . . . . . . . . . . . . . 5 . . . . . . . . . . . 1 December 04 Change . . . . . . . . . . . . . 6 . . . . . . . . . . . . 15 January 05 Change . . . . . . . . . . . . . 7 . . . . . . . . . . . . . 15 March 05 Change . . . . . . . . . . . . . 8 . . . . . . . . . . . 1 December 05 Change . . . . . . . . . . . . . 9 . . . . . . . . . . . 15 February 06

Change . . . . . . . . . . . . . .10 . . . . . . . . . . . . . . . 1 July 06 Change . . . . . . . . . . . . . .11 . . . . . . . . . 15 September 06 Change . . . . . . . . . . . . . .12 . . . . . . . . . 20 December 06 Change . . . . . . . . . . . . . .13 . . . . . . . . . . . . . . 1 April 07 Change . . . . . . . . . . . . . .14 . . . . . . . . . 15 December 07 Change . . . . . . . . . . . . . .15 . . . . . . . . . . . 15 April 2008 Change . . . . . . . . . . . . . .16 . . . . . . . . . . . . 15 June 2008 Change . . . . . . . . . . . . . .17 . . . . . . . . 1 December 2008 Change . . . . . . . . . . . . . .18 . . . . . . . . . 1 February 2009 Change . . . . . . . . . . . . . .19 . . . . . . . . . . . 1 March 2009

Title A I

II – III

V Added VI Blank Added 1-A-001 1-A-002 Blank 1-B-001 1-B-002 Blank Added 1-C-001 1-C-002 Blank Added 1-D-001 1-D-002 Blank Added 1-E-001 1-E-002 Blank Added 1-F-001 1-F-002 Blank Added 1-G-001 1-G-002 Blank Added 1-H-001 1-H-002 Blank Added 1-J-001 Added 1-J-002 Blank Added 1-K-001 1-K-002 Blank Added 1-L-001 Added 1-L-002 Blank Added 1-M-001 1-M-002 Blank Added 1-N-001 1-N-002 Blank Added 1-P-001 1-P-002 Blank Added 2-A-001 2-A-002 – 2-A-004 2-A-004A 2-A-004B Blank 2-A-005 2-A-006 2-A-007

2-A-008 2-A-008A 2-A-008B Blank 2-A-009 – 2-A-010 2-A-011 2-A-012 2-A-012A 2-A-012B Blank 2-A-013 2-A-014 2-A-015 2-A-016 2-A-016A 2-A-016B Blank 2-A-017 2-A-018 2-A-018A – 2-A-018B 2-A-018C 2-A-018D 2-A-019 – 2-A-020 2-A-020A – 2-A-020B 2-A-020C 2-A-020D 2-A-021 2-A-022 – 2-A-023 2-A-024 2-A-024A – 2-A-024B 2-A-025 – 2-A-028 2-A-028A 2-A-028B Added 2-B-001 – 2-B-003 2-B-004 Blank 2-C-001 2-C-002 Blank 2-D-001 2-D-002 – 2-D-003 2-D-004 Blank 2-E-001 2-E-002 Blank 2-F-001 2-F-002 2-F-003 – 2-F-004

3-A-001 – 3-A-002 3-A-002A Added 3-A-002B Blank Added 3-A-003 – 3-A-004 3-A-004A Added 3-A-004B Blank Added 3-A-005 – 3-A-006 3-A-006A 3-A-006B Blank Added 3-A-007 – 3-A-008 3-A-008A 3-A-008B Blank Added 3-A-009 – 3-A-012 4-A-001 4-A-002 Blank 4-A-003 – 4-A-118 Deleted

A Change 19

T.O. 1C-130A-6

Change 11 I

TABLE OF CONTENTS

SECTION AND PART PAGE

Forward-------------------------------------------------------------------------------------------------------- ii

SECTION I

PART A ASIP INSPECTIONS FOR AC-130H AIRCRAFT --------------------------------------------------------- 1-A-001

PART B ASIP INSPECTIONS FOR AC-130U AIRCRAFT --------------------------------------------------------- 1-B-001

PART C ASIP INSPECTIONS FOR C-130E AIRCRAFT------------------------------------------------------------ 1-C-001

PART D ASIP INSPECTIONS FOR C-130H AIRCRAFT ----------------------------------------------------------- 1-D-001

PART E ASIP INSPECTIONS FOR EC-130E AIRCRAFT---------------------------------------------------------- 1-E-001

PART F ASIP INSPECTIONS FOR EC-130H AND TC-130H---------------------------------------------------- 1-F-001

PART G ASIP INSPECTIONS FOR HC-130N AND HC-130P AIRCRAFT------------------------------------ 1-G-001

PART H ASIP INSPECTIONS FOR LC-130H AIRCRAFT---------------------------------------------------------- 1-H-001

PART J ASIP INSPECTIONS FOR MC-130E AIRCRAFT--------------------------------------------------------- 1-J-001

PART K ASIP INSPECTIONS FOR MC-130H AIRCRAFT -------------------------------------------------------- 1-K-001

PART L ASIP INSPECTIONS FOR MC-130P AIRCRAFT--------------------------------------------------------- 1-L-001

PART M ASIP INSPECTIONS FOR MC-130W AIRCRAFT-------------------------------------------------------- 1-M-001

PART N ASIP INSPECTIONS FOR NC-130H AIRCRAFT --------------------------------------------------------- 1-N-001

PART P ASIP INSPECTIONS FOR WC-130H AIRCRAFT -------------------------------------------------------- 1-P-001

SECTION II

PART A Special Inspections ---------------------------------------------------------------------------------------------- 2-A-001

PART B Inspection Requirements for PDM Extension ------------------------------------------------------------ 2-B-001

PART C Functional Check Flight ---------------------------------------------------------------------------------------- 2-C-001

PART D Historical Documents AFTO Forms 95 and 44 --------------------------------------------------------- 2-D-001

PART E Special Inspections (CIE)--------------------------------------------------------------------------------------- 2-E-001

PART F Special Inspection for Desert Operations and High Utilization ------------------------------------- 2-F-001

SECTION III

PART A Replacement Schedule------------------------------------------------------------------------------------------ 3-A-001

SECTION IV

PART A Base Level Repair Restrictions ------------------------------------------------------------------------------- 4-A-001

1. PURPOSE AND SCOPE.

This manual contains complete requirements for accomplishing scheduled maintenance on the C-130 aircraft during its entire service life. It establishes inspection, accessory replacement and functional check flight requirements for the airframe and airborne equipment. The requirements prescribed by this manual are primarily those which are technical in nature and the conditions listed are intended to direct attention to known problem areas where defects or malfunctions would prevent the items from performing their designed functions within prescribed limits. These requirements are developed for new aircraft through maintenance engineering experience and comparison of similar installations on in-service aircraft.

They are refined and changed during the service life of the aircraft by continually evaluating the performance of the equipment, results of scheduled maintenance, and through study of factual operating data for the primary use of the aircraft. The interval between the accomplishment of a requirement is intended to be the longest period of time that an item or component can safely operate without an inspection or observation. When the aircraft is operated in other than the primary purpose or major use class the requirements have been adjusted accordingly, if necessary, and the requirements identified as to class of operation. These requirements and inspection intervals are the maximum and should never be exceeded. Local conditions (type of missions, special utilization, geographical locations, etc.) may dictate more frequent inspection or replacement or more thorough inspections. Therefore, commands, local commanders and their maintenance officers are expected to exercise their prerogative to increase the frequency or scope of any requirements, as required.

1.1 LIMITATIONS. This manual does not

contain detailed instructions for troubleshooting to find causes for malfunctioning, nor does it contain instructions for repair, adjustment, or other means of rectifying defective conditions.

Proper installation of a piece of equipment or accessory is not necessarily within the scope of this manual as adequacy and completeness or installation will have been determined at the time of installation.

Further, it does not normally contain informative or precautionary data such as notes, cautions, and warnings. Applicable portions of the appropriate maintenance manuals should be consulted to obtain the maintenance instructions as they are beyond the scope of this manual.

1.2 APPLICABILITY. This manual and work

cards may pertain to part or all types and series of a model of aircraft and may therefore, contain requirements applicable to specific equipment that is not installed on individual aircraft. When this situation is encountered, those requirements that are not applicable should be disregarded.

1.3 PERFORMANCE OF INSPECTIONS.

The inspections prescribed by this manual will be accomplished at specified periods by Air Force organizational activities with assistance provided by intermediate maintenance and specialized repair activities when required. Compliance with the provisions of this manual is required to assure that latent defects are discovered and corrected before malfunctions or serious failures occur.

III

2. INSPECTION REQUIREMENTS.

The inspection requirements establish what equipment is to be inspected, when it is to be inspected, and what conditions are to be sought. The requirements are designed to direct the attention of maintenance personnel to components and areas (or zones) where defects are suspected to occur due to usage under normal operating conditions.

They are not intended to provide coverage for routine cleaning, washing, etc., nor are they designed to lead to the detection of isolated discrepancies that may occur on a one time basis, or discrepancies that are the result of carelessness, abuse, or poor maintenance practices. During accomplishment of the specific requirements directed by this manual, maintenance personnel should observe both the equipment being inspected and, in each designated zone, the components within that zone for any of the requirements.

2.1 REPLACEMENT SCHEDULE. The

replacement schedule directs replacement of items at a specific time whose failure would compromise safety of flight beyond reasonable limits or definitely cause a mission to abort. Also considered are any high cost items whose failure would result in condemnation and any short life items which would require frequent occurrence of unscheduled maintenance. Items not listed will be known as “condition items” and will be replaced only when necessary.

2.2 FUNCTIONAL CHECK FLIGHT

(FCF). The conditions requiring functional check flight in this manual augment the requirements specified in to 1- 1-300 and establish the requirements for the aircraft to which this manual pertains.

They are designed to assure the aircraft is operational and capable of mission accomplishment after completion of certain scheduled or unscheduled maintenance.

Detailed procedures are contained in the applicable acceptance and functional check flight procedures manual.

2.3 REPAIR RESTRICTIONS. Repair

restrictions, lists items (by work unit code, nomenclature, federal stock class (FSC), and part number) for which base level repair restrictions have been established, and describes the repairs which are not authorized.

2.4 HISTORICAL DOCUMENTS. The

historical documents section of chapter 2 contains a listing of all airplane components that require preparation of AFTO forms.

The forms provide a permanent record of events or conditions encountered during the use of the equipment. The information documented in these forms will be used to plan required logistic and maintenance procedural support.

2.5. TIME REQUIREMENTS. The times in

man minutes for accomplishment of requirements in sections II and III reflect only the time required for inspection or replacements. These times do not include time required to gain access to the equipment to facilitate accomplishment.

Those factors (personnel and equipment shortages, lack of parts, adverse working conditions, and qualifications of personnel) which will directly affect the length of time for any scheduled maintenance are not included because they cannot be accurately predicted.

IV Change 14

3. DEFINITIONS OF TERMS.

For clarification, the following definitions are given.

A. Specified -- refers to a definite amount, operation, or limitation that has been established and is contained in applicable directives.

B. Evidence -- is an indication of an existing or impending unsatisfactory condition.

C. Security -- means the component is properly mounted or attached to related equipment, including applicable safety wiring.

D. Accessible -- is the term applied to equipment that may be inspected without further disassembly or removal of panels, cowling, etc., Other than those required to accomplish the more specific requirements applicable to the particular inspections.

E. Jacked -- requires aircraft be jacked, with wing in a no-load condition IAW T.O. 1C-130A-3.

F. Not jacked -- requires the wing be self-supporting.

G. Excessive -- is a term used to describe conditions when specific limitations have not been established. A condition is excessive if it has progressed to the degree that, if not corrected, could result in failure or malfunction of the component prior to the next scheduled action that would direct attention to the condition.

H. Hard Landing -- any landing that exceeds the the allowable decent rate at touchdown as published in the C-130 flight manuals.

I. Retorque -- requires that at least the minimum torque be applied to ensure that bolts have not loosened since the last installation.

J. Initial Inspection – requires an initial inspection after the accumulation of a specified number of airframe hours. If the requirement exempts the requirement for specific number of airframes then the inspection is due at the end of that exemption i.e. NA for the first 4800 hours. In this case the first inspection would be due at 4800 hours.

K. WEAR INDICATION – The end of service life is accompanied by excessive wear which is indicated by displaced material, ruts and grooves, misalighnment and malfunctioning equipment. The areas mainly affected are attaching points of structural members subject to varying loads and points of relative motion. When inspecting for wear damage, particular attention should be given to bushings, hinges, tracks, fasteners, and fittings. Wear damage is expected, but evidences of rapid or excessive wear should warrant a complete inspection of related and attaching equipment.

Evidence of excessive wear damage may be indicated in any of the following ways:

a. Elongated or Enlarged Holes.

b. Bent, Broken or Deformed Fasteners.

c. Brineling or Failed Material.

d. Misalignment.

e. Binding, Sticking or Erratic Movement of

Equipment.

f. Squeaks, Rattles or Chatter.

g. Improper Seating.

4. UPDATES.

Changes and supplements to this manual will be published when necessary to add, delete, or change frequency or scope of requirements. Such changes will be based on factual data accumulated as a result of maintenance experience with the aircraft and equipment. Recommendations proposing changes to this manual should be submitted on AFTO Form 22 in accordance with T.O. 00-5-1 to WR-ALC/LUTD, Robins

AFB, GA, 31098.

Change 11 V/(VI blank)

5. ADDITIONAL INSPECTION

REQUIREMENTS THAT ARE ASSOCIATED

WITH THIS TECHNICAL ORDER ARE

INCLUDED IN THE FOLLOWING

TECHNICAL ORDERS:

1C-130A-6WC-10 (Preflight) 1C-130A-6WC-11 (Thru-Flight) 1C-130A-6WC-12 (Basic Postflight) 1C-130A-6WC-13 (Preflight/Postflight combined 1C-130A-6WC-14 (Home Station Check) 1C-130A-6WC-15 (Minor and Major Isochronal)

Change 12 1-A-001/(1-A-002 blank)

INTRODUCTION

C-130 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) INSPECTIONS

1. THIS SECTION CONSISTS OF FOURTEEN PARTS WHICH PROVIDE THE INSPECTION REQUREMENTS OF THE C-130 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) AS OUTLINED IN MIL-HDBK-1530 AND AFI 63-1001. THESE INSPECTION REQUIREMENTS SHALL BE ACCOMPLISHED AFTER THE ACCRUAL OF A SPECIFIED NUMBER OF AIRFRAME HOURS. EARLY ACCOMPLISHMENT OF THESE INSPECTIONS IS AUTHOIRIZED AS LOCAL SCHEDULING OR MISSION DICTATES. THE AIRCRAFT SHALL BE REMOVED FROM SERVICE UNTIL THESE INSPECTIONS ARE ACCOMPLISHED. THE INTERVAL MAY BE EXTENDED BY 10% WHEN NECESSARY TO MEET MISSION REQUIREMENTS. WAIVERS TO THESE REQUIREMENTS WILL BE SUBMITTED AS A REQUEST FOR TECHNICAL ASSISTANCE IAW T.O. 00-25-107 (SEE HTTPS://C130AIRCAT.ROBINS.AF.MIL/).

A. PART A CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE AC-130H.

B. PART B CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE AC-130U.

C. PART C CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE C-130E.

D. PART D CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE C-130H.

E. PART E CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE EC-130E.

F. PART F CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE EC-130H AND TC-130H.

G. PART G CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE HC-130N AND HC-130P.

H. PART H CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE LC-130H.

J. PART J CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE MC-130E.

K. PART K CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE MC-130H.

L. PART L CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE MC-130P.

M. PART M CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE MC-130W.

N. PART N CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE NC-130H.

P. PART P CONTAINS RECURRING ASIP INSPECTION REQUIREMENTS FOR THE WC-130H.

2. WHEN A CHANGE TO SECTION I (ASIP INSPECTIONS) RESULTS IN AN OVERDUE INSPECTION (DUE TO AN ADDED INSPECTION REQUIREMENT OR A DECREASE IN AN INSPECTION INTERVAL), A RED DASH ENTRY SHALL BE MADE IN THE AFTO FORM 781A.

THE RED DASH SHALL BE UPGRADED TO A RED X CONDITION WHEN ANY OF THE FOLLOWING CONDITIONS OCCUR.

A. THE AIRCRAFT ACCUMULATES TWICE THE SPECIFIED FLIGHT HOUR INTERVAL SINCE THE MOST RECENT ACCOMPLISHMENT

OF THE INSPECTION

B. THE AIRCRAFT ENTERS HOME STATION CHECK OR ISOCHRONAL INSPECTION

C. 35 DAYS HAVE ACCRUED SINCE THE RECEIPT OF THE T.O. 1C-130A-6 CHANGE.

PART A

ASIP INSPECTIONS FOR AC-130H AIRCRAFT

WORK

UNIT

CODE

PARA-

GRAPH ASIP INSPECTION

MIN-

UTES

RESERVED

PART B

ASIP INSPECTIONS FOR AC-130U AIRCRAFT

WORK

UNIT

CODE

PARA-

GRAPH

ASIP INSPECTION MIN-

UTES

1. EVERY 80 AIRFRAME HOURS FOR AIRCRAFT WITH MORE THAN 24,000 EQUIVALENT BASELINE

HOURS (EBH) SINCE RAINBOW FITTING OEM INSTALLATION OR REPLACEMENT. EVERY 400

AIRFRAME HOURS FOR AIRCRAFT WITH LESS THAN 24,000 EBH SINCE RAINBOW FITTING

OEM INSTALLATION OR REPLACEMENT. THE DATE OF RAINBOW FITTING REPLACEMENT CAN

BE FOUND BY REVIEWING AFTO 95 RECORDS. EBH VALUES ON CURRENT AND REPLACE-

MENT DATE CAN BE FOUND AT THE AIRCAT WEBSITE - HTTPS://C130AIRCAT.ROBINS.AF.MIL.

N/A TO AIRCRAFT WITH FEWER THAN 8,500 EBH SINCE RAINBOW FITTING OEM INSTALLATION

OR REPLACEMENT.

115BA

115BB

A. INSPECT CENTER WING UPPER AND LOWER RAINBOW FITTINGS, LEFT AND RIGHT SIDES,

IAW TO 1C-130A-36 (CHANGE 47 OR SUBSEQUENT), INSPECTION CW-17 AND CW-18. PER-

FORM INSPECTIONS LISTED AS SCAN 1 AND SCAN 2 ONLY. INSPECTION OF THE UPPER AND

LOWER RAINBOW FITTINGS IS A SAFETY OF FLIGHT CRITICAL INSPECTION REQUIRED BY

THE C-130 AIRCRAFT STRUCTURAL INSPECTION PROGRAM (ASIP). REPORT RESULTS OF

INSPECTION VIA ICARR SOFTWARE IAW TO 1C-130A-23 AND 1C-130A-36.

2. EVERY 50 AIRFRAME HOURS AFTER PREVIOUS INSPECTION IF PERFORMED EXTERNALLY OR

550 AIRFRAME HOURS IF PREVIOUS INSPECTION PERFORMED INTERNALLY. PERFORM

EITHER INSPECTION A OR B. USE ICARR SOFTWARE TO MAKE INPUTS TO THE AUTOMATED

INSPECTION, CORROSION, REPAIR AND AIRCRAFT TRACKING (AIRCAT) DATABASE. THIS IS AN

AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) REQUIREMENT. SEE HTTPS://

C130AIRCAT.ROBINS.AF.MIL/ FOR PROGRAM, INSTRUCTIONS AND INFORMATION ON ICARR.

N/A AFTER COMPLIANCE WITH TCTO 1C-130-1872 OR TCTO 1C-130-1900.

1152L 1152M

A. EXTERNAL INSPECTION OF THE LOWER FORWARD CENTER WING SPAR CAP FROM WS 168

TO WS 177: WITH THE AREA CLEAN AND DEPAINTED, PERFORM AN EDDY CURRENT SURFACE

SCAN OF THE EXPOSED PORTION OF THE LOWER FORWARD CENTER WING SPAR CAP FROM

WS 168 TO THE LOWER ENGINE NACELLE AT APPROXIMATE WS 177, LEFT AND RIGHT, IAW TO

1C-130A-36 PARAGRAPH 2-30.1 THROUGH PARAGRAPH 2-30.10 WITH FREQUENCY SET AT 200

KHZ. ALTERNATE EQUIPMENT SHALL NOT BE USED. THIS SECTION OF SPAR CAP IS EXTER-

NALLY ACCESSIBLE WITHOUT REMOVAL OF ANY PANELS. IT IS LOCATED BETWEEN THE AFT

EDGE OF THE LEADING EDGE HINGE AND THE FORWARD EDGE OF THE CENTER WING

LOWER FORWARD WING PLANK. THE INSPECTION AREA IS SIMILAR TO THE AREA SHOWN IN

TO 1C-130A-3 FIGURE 57-30-02 VIEW C. THE BEAM CAP LABEL ARROW POINTS TO THIS

EXPOSED AREA. THE VIEW SHOWN IN THIS FIGURE IS FOR AN UPPER SPAR CAP.

1152L 1152M

B. INTERNAL INSPECTION OF THE LOWER FORWARD CENTER WING SPAR CAP FROM WS 168 TO

WS 177: (INSIDE THE OUTBOARD AUXILIARY TANK CAVITY): WITH THE AREA CLEAN AND

DEPAINTED, PERFORM AN EDDY CURRENT SURFACE SCAN OF THE INTERNAL HORIZONTAL

AND VERTICAL FLANGES OF THE LOWER FORWARD CENTER WING SPAR CAP FROM WS 168

TO THE WS 178 RIB, LEFT AND RIGHT, IAW TO 1C-130A-36 PARAGRAPH 2-30.1 THROUGH PARA-

GRAPH 2-30.10 WITH FREQUENCY SET AT 200 KHZ. ALTERNATE EQUIPMENT SHALL NOT BE

USED. REFERENCE TO 1C-130A-36 FIGURE 4-38 FOR LOCATION.

Change 18 1-B-001/(1-B-002 blank)

PART C

ASIP INSPECTIONS FOR C-130E AIRCRAFT

WORK

UNIT

CODE

PARA-

GRAPH

ASIP INSPECTION MIN-

UTES

1. EVERY 270 AIRFRAME HOURS FOR AIRCRAFT WITH MORE THAN 24,000 EQUIVALENT BASE-

LINE HOURS (EBH) SINCE RAINBOW FITTING OEM INSTALLATION OR REPLACEMENT. EVERY

675 AIRFRAME HOURS FOR AIRCRAFT WITH LESS THAN 24,000 EBH SINCE RAINBOW FITTING

OEM INSTALLATION OR REPLACEMENT. THE DATE OF RAINBOW FITTING REPLACEMENT CAN

BE FOUND BY REVIEWING AFTO 95 RECORDS. EBH VALUES ON CURRENT AND REPLACE-

MENT DATE CAN BE FOUND AT THE AIRCAT WEBSITE - HTTPS://C130AIRCAT.ROBINS.AF.MIL.

N/A TO AIRCRAFT WITH FEWER THAN 8,500 EBH SINCE RAINBOW FITTING OEM INSTALLATION

OR REPLACEMENT.

115BA

115BB

A. INSPECT CENTER WING UPPER AND LOWER RAINBOW FITTINGS, LEFT AND RIGHT SIDES,

IAW TO 1C-130A-36 (CHANGE 47 OR SUBSEQUENT), INSPECTION CW-17 AND CW-18. PER-

FORM INSPECTIONS LISTED AS SCAN 1 AND SCAN 2 ONLY. INSPECTION OF THE UPPER AND

LOWER RAINBOW FITTINGS IS A SAFETY OF FLIGHT CRITICAL INSPECTION REQUIRED BY

THE C-130 AIRCRAFT STRUCTURAL INSPECTION PROGRAM (ASIP). REPORT RESULTS OF

INSPECTION VIA ICARR SOFTWARE IAW TO 1C-130A-23 AND 1C-130A-36.

2. EVERY 100 AIRFRAME HOURS AFTER PREVIOUS INSPECTION IF PERFORMED EXTERNALLY

OR 1100 AIRFRAME HOURS IF PREVIOUS INSPECTION PERFORMED INTERNALLY. PERFORM