introduccion al SRM ATR72

ATR42-400/500 - STRUCTURAL REPAIR MANUAL

INTRODUCTION 1.

General Policy A.

General This manual is in conformity with the Air Transport Association Specification number 2200 (ATA iSpec 2200). It provides descriptive information, instructions and specific data relative to the repair of the ATR structure. It contains damage acceptability criteria, the identification of structure materials and repair data applicable to the structural elements that are the most exposed to damage. It gives information on the standard repair procedures. All the data contained in this manual are approved by the authorities. The Structural Repair Manual is completed by the Illustrated Parts Catalog (IPC) which gives the list of replaceable structural elements. The Structural Repair Manual is laid out as follows: –

Chapter 51 : Aeronautical standards, standard practices, materials and general information on repairs

–

Chapters 52 through 57 : Specific structural chapters

The chapter numbers indicate an entire zone of the aircraft (for example : fuselage, wing, etc...), the section numbers indicate a sub-division of this zone (for example : fuselage nose section, wing center box), and the subject numbers indicate a component of this zone (for example : FWD pressure bulkhead, front spar, etc...) (See para. 4.A.). To obtain a separation of the topics, the following block pages are used : –

Description

–

Identification Figure

–

Allowable Damages

–

Repair

The Documentary Units (DU) are independently numbered and all the DU begin on a recto page. One page "PAGE LEFT BLANK INTENTIONALLY" is inserted if the DU finishes on a recto page. The LEP records all the DU and their interval of pages. After a revision, if a DU has an added or deleted pages, all the pages of the DU are numbered. B.

List of Effective Pages As noticed here-above the LEP records all the DUs and their interval of pages. It gives an overview of the parts revised. N, R or D indicates parts which are New, Revised or Deleted respectively.

C.

Manual Validity Manual designated as ATR42-400/500 series SRM (this manual) covers the ATR42-400/500 A/C -400, -500 series. This manual also covers ATR42-600 designation.

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D.

Data effectivity Data that has no effectivity designation shall be applicable to all the aircraft series covered by this manual. Effectivity designations are used to define the variants between the aircraft. Effectivity is expressed by MODIFICATION NUMBERS indicated : –

In the block effectivity at the top of the variant Figures.

–

In the Identification Tables, in the - OBSERVATION MOD/SB REPAIR column, in front of each item variant. Example: Be. 3667T3724 ; Solution Before Modification 3667T3724 Af. 3667T3724 ; Solution After Modification 3667T3724

–

In the Table of Contents, if a Configuration is created ('EFFEC' column) in front of each configuration ("a" or “b” on the AMTOSS code, see para. 6.A.). Example : The required configuration is specified at the bottom of the pages. The modifications concerned are given in the Table of Contents at the beginning of each ATA chapter.

The absence of modification number indicates commonality between all aircraft. The pages called "MODIFICATIONS/SERVICE BULLETINS LIST", placed - at the beginning of the chapter, give the effectivity of each Modification Number expressed in Standard Version (ST) and by Manufacturer Serial Number (MSN). NOTE :

E.

Revision of the manual The revision service is periodically provided. The revision is materialized by a "R" in the footer of the page. The latest revision date of the DU is shown in the footer. The revised text is shown by a bar located in the left hand margin of the pages. The HIGHLIGHTS section (in the begin of the manual) records the revised DU and their reasons of revision.

F.

Abbreviations used in the SRM The abbreviations used in the SRM are recorded in the "LIST OF ABBREVIATIONS".

G.

Symbols used in the repair drawings In order to simplify and clarify illustration of repair drawings, fastener symbols are as follows : SYMBOL

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Before all investigation on structure Items make sure that the validity is correct (before or after Modification, Service Bulletin retrofitted, etc...).

TYPE

Existing fastener not affected by the repair

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SYMBOL

TYPE

Existing fastener affected by the repair Rivet Blind fastener Bolt Countersunk fasteners (superimposed on other symbols)

Different diameters shall be represented by different symbols, as shown below: TYPE

SYMBOL

Rivet Blind fastener Bolt

2.

General technical principles A.

Description This section is a brief description of the chapter concerned.

B.

Identification Figure Chapters 52 through 57 include the identification of the materials used in the manufacture of the airplane. They indicate structural differences between airplanes of the same type which have been incorporated in production or retroactively, thus enabling the operator to identify the material of any significant component on any specific airplane in his fleet. Illustrations and text concerning the aircraft structure give description, material, and significant drawing numbers including appropriate assembly drawing numbers. Where applicable, material information define the finished heat treatment condition.

C.

Allowable damage Allowable damage is damage that allows an operator to continue operating an aircraft without any repairs other than local rework, and surface finish restoration.

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NOTE :

In the case of damage occurred on primary structure including PSE that go beyond SRM allowable limit, contact the manufacturer.

Wear Limits: Wear Limits on structural assemblies permit the assessment of in-service wear on single bolt and bolt-like parts, and also on attaching parts such as bearing and bushes. The limits are presented in tabular form in the Allowable Damage topic of the appropriate manual section and indicate when rectification is required so that the assembly can continue satisfactorily in service. D.

Repair (1) Definition of repair Repair instructions are intended to enable the operator to repair damage exceeding allowable damage limits. Several types of damage have been taken into account: –

Metallic materials: Corrosion; cracks; scratches; dents; scores; gouges: nicks; abrasion; etc.

–

Non-metallic materials: Flaking; perforation; delamination; scratches; score; separation; denting; etc.

The repair approach shown in the flowchart (Refer to Description 510001-03-001-A01) has to be followed NOTE :

In case of damage occurred in the areas where the structure is not regular, or joined with other components, and if any proximity criteria is defined in the concerned repair procedure, contact the manufacturer. There is not limit to the number of applications of a repair principle unless otherwise specified in the instructions, and provided that the geometry of the structure so permits. If damage occurred is closed to an existing repair, contact the manufacturer.

(2) Recommendations of repair WARNING :

IF THE REPAIR IS NOT LIMITED BY MAX. DIMENSION, THE SIZE IS DEFINED BY THE NUMBER OF FASTENERS SHOWN ON REPAIR SCHEME (SKETCH). PITCH AND EDGE MARGINS DEPEND ON FASTENER DIAMETERS WHEN THEY ARE NOT IMPOSED BY EXISTING STRUCTURE (REFER TO SRM 51-25-02 (FIT CONDITIONS OF BOLTS (TORQUE))). IN SUCH A CASE, IT COULD BE NECESSARY TO REMOVE PART OF THE COMPONENT THAT IS GREATER THAN THE OCCURRED DAMAGED AREA OR MAKE A DISPLACED SPLICE IN ORDER TO APPLY THE PRINCIPLE OF REPAIR AS DEFINED. 1. REPAIR PROXIMITY IN CASE OF MULTIPLE SIMULTANEOUS OR SUCCESSIVE DAMAGES, APPLICATION OF REPAIR PRINCIPLES CAN BE PERFORMED IF DAMAGE

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PROXIMITY CRITERIA AND GEOMETRY REQUESTED BY LEVEL OF REPAIRS IN THE CONCERNED REPAIR ARE MET. IN THE ABSENCE OF SPECIFIC CRITERIA, CONTACT THE MANUFACTURER.

2. REPAIR SHOWN IN THIS MANUAL ARE NOT APPLICABLE ON REPAIRS ALREADY PERFORMED. The repair application area is defined by precise structural references (frames, stringers, ribs, stiffeners, etc...). Repair schemes can be adapted to similar zones if: –

Note <> is absent

–

Damage is similar.

Before all repairs, an inspection must be performed in order to accurately determine extent of damage (Refer to SRM 51-00-01 (DEFECT/DAMAGE REPORTING)). Two kinds of repairs are defined: –

Standard repairs and processes valid for all structure defined in chapter 51.

–

Specific repairs relevant to an element (or an area) and described in the corresponding chapter or section.

Certain repairs are defined by means of graphs taking the following into account: –

type of damage

–

damage dimensions

–

damage area.

NOTE :

When repair instructions are not available, this does not mean that the concerned structure is not repairable. Sometimes it is not possible to give a standard repair, because the experience of inservice aircraft has not yet shown the necessity of such a repair. In certain cases an adapted repair design shall require an evaluation made by the aircraft manufacturer. As in-service experience shows the necessity, this manual shall be procedures updated for repetitive and typical issue so as to include new repairs. In the possible case of serious damage the information of this manual shall be completed by a direct link with a representative of the aircraft manufacturer support.

Temporary repairs, enabling limited service life are also defined in certain cases, and can be reported by a "TEMPORARY" in the title. When fatigue life of the repair is not stated in the repair principle, fatigue life has to be considered to be equal to the design life goal of the ATR which is 70000 cycles. Several solutions may be proposed for repairing given damage. In the case of cumulative damage, the repair must cover each type of damage. INTRODUCTION

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In the case where damage covers two areas, the repair retained will be the one corresponding to area comprising a flush criteria. 3.

Repair Components Kit. For the components given in the REPAIR MATERIAL tables of repair schemes, refer to "Index of Repair Drawing" or at the beginning of concerned chapter to check the drawing number, its description, location and figure number to be able to order the manufactured parts.

4.

How to use the manual A.

SRM Manual Breakdown Arrangement (Ref. Fig. 1)

B.

Identification Figure IDENTIFICATION FIGURE (Ref. Fig. 2)

COLUMNS DESCRIPTION 1 ITEM: Structural part item All required items, shown on the appropriate illustration, are listed in this column, in sequential order, beginning with Item Number 1 and continuing in steps of 5 (5, 10, 15, etc.). Structural components fitted in the same portion with different effectivities will be identified with an item number followed by a suffix letter A, B, C, etc. 2 DESCRIPTION: Structural part description This column contains the exact description of structural component shown in the appropriate illustrations. 3

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PART NUMBER Structural components will be given a manufacturer part number consisting of twelve characters. In general, the "as drawn" parts are LH. Where necessary, three additional characters are given for symmetrical item (RH item). If available, the appropriate standard (production methods) will be given here (Ref. Fig. 5 Sheet 1). MAT SPEC TREATMENT: Material and treatment of structure parts Material specification for metallic and/or non metallic components (Refer to SRM 51-30-00 (MATERIALS, ALTERNATIVES AND EQUIVALENTS GENERAL)) are listed in this column. Complicated composite components are identified in detail by number of plies, material thickness and ply direction given in an appropriate table in the figure.

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IDENTIFICATION FIGURE (Ref. Fig. 2)

COLUMNS DESCRIPTION 5 INTERCHANGEABILITY "IC" In the column is shown the interchangeability condition of a component (P/N). The interchangeability condition of concerned component is defined with one of following code numbers:

6

7

–

01: One way Interchangeability States that the post MOD item can be used to replace a pre MOD item without special action being required (not vice versa).

–

02: Two way Interchangeability Either the post MOD or pre MOD items can be used.

–

03: No Interchangeability The basic item and post MOD item are not interchangeable.

THK mm (in): Thickness of structural component Where necessary, information concerning the thickness of sheet metal component will be given in this column. The US/Imperial conversion (based on 1 in. = 25.4 mm) will be given in brackets. For machined metallic parts with variable thickness and composite materials, thicknesses are given by appropriate tables. OBSERVATIONS MOD/SB/REPAIR Information regarding the status "Before Modification" or "After Modification" or "Before or After Service Bulletin" shall appear in this column. A prefix letter shall be applied for Before/After/Mod/SB statement as follows: –

Be. = Before SB/Mod.

–

Af. = After SB/Mod.

In this column, the reference to a repair is given. The following indications may be used: –

For repair, see Pages REPAIR or

–

For repair, see XX-XX-XX Pages REPAIR

following the cases (XX-XX-XX for existing specific or general repairs Chapter/Section/Subject Number is inserted). Where no repair exists, the space is left blank. Should a repair be required and no information is given, a request must be sent to: ATR Structure Department 1, Alle Pierre Nadot 31712 BLAGNAC Cedex FRANCE Fax: + 33(0)562216290 E-mail: [email protected]

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IDENTIFICATION FIGURE (Ref. Fig. 2)

COLUMNS DESCRIPTION 8 ASSY DWG Drawings used for store issue of structural component.

C.

Allowable Damage (Ref. Fig. 3) The allowable damage procedure gives the related data applicable to the concerned area.

D.

Repair The repair procedure includes two parts: 1. the "JOB SET-UP INFORMATION" topic that gives all the information necessary to do the repair. This topic has the tables that follows: NOTE :

Only the tables applicable to the Repair are in the repair

TABLE REPAIR MATERIAL LIST

MATERIALS/CONSUMABLE LIST TOOLS LIST REFERENCED INFORMATION

DESCRIPTION This table records the repair material used to do the procedure. The materials are associated with a reference to the relevant chapter 51 for the standard procedure This table records the consumable used to do the procedure. The consumable are associated with a reference to the relevant chapter 51 for the standard procedure This table records the specific tool used to do the procedure. This table records the referenced information used to do the procedure.

2. The "PROCEDURE" topic that gives all the instructions to do the repair. The PROCEDURE topic is structured in subtask. E. 5.

AMTOSS Numbering The AMTOSS part numbers has a standard structure (Ref. Fig. 4)

Part Number Specification A.

Structure of A/C Manufacturer Part Number (Ref. Fig. 5) Suffix added to comply with manufacturing or spares requirements with the purpose of a more detailed definition not specified in the Drawing. The allocation of suffixes between Product Support and engineering/ Manufacturing is as follows:

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B.

FOR CHAPTERS 52, 53 AND 55 SUFFIXES DEFINITION 00 Part to drawing 01 to 05 Production Part not 50 to drawing 51

60 to 89 Spare Part not to drawing and not stockable

REMARKS 00 = Part produced according to drawing 01 = Part with pilot hole 2.5 mm dia. (3/32 in.) as specified on drawing 02 = Undrilled part 03 = Increased perimeter and finished holes 04 = Increased perimeter and pilot holes 05 = Increased perimeter and not drilled 06 = Assy similar to drawing, but with different composition <3> 50 = Identical to drawing <1> 51 = Special specification <2> Numbering required for Product Support Breakout, but not applicable to production.

99 Spare Part to drawing and not stockable NOTE : Several suffixes are used by Spare Department to manufacture special P/ N. <1> and not as partially manufactured to allow the installation in the construction process. <2> referring some diversion from the manufactured one. NOTE :

C.

FOR CHAPTERS 54 AND 57 NOTE :

6.

<3> Means that for production needs the assy has to be manufactured with less or more components installed. The components not installed may be furnished to the customer separately.

For ATA Chapters 54 and 57, the delivery status of spare parts, not to drawing, is not univocally identified by suffix. In this case the desired delivery condition must be clearly mentioned on the part order (e.g. "UNDRILLED", "WITH PILOT HOLES", etc.).

ATA iSpec 2200 — Changes and Cross—References Table Between Before and After Conversion ATR Structural Repair Manual Conversion has been provided in order to switch from the old ATA100 specification to the new iSpec 2200 specification. ATR SRM Conversion is effective starting from June 2013 revision. A.

The Main Changement are:

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1. Old task numbers (example: chapter 53–00–00 Figure 437) are not used anymore. AMTOSS Code are the unique references which have to be used (example: 530000–300–837–A01).

2. Allowable damages are numbered 200 in the AMTOSS Code (and not either 300 as before). 3. Repairs are numbered 300 in the AMTOSS Code (and not either 400 as before). B.

Cross—References Table Between Before and After Conversion In order to facilitate the research of a task with different reference before and after the Conversion, a cross-reference table is provided. The tables includes the allowable damages and the repair procedures introduced in the manual until February 2013 revision. CHAPTER 52 Before Conversion

52–11–00 Fig 301

52–11–00 Fig 302 52–11–00 Fig 303

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Table 6: ALLOWABLE DAMAGE After Conversion (Refer to Damages 521100-200-801-A01) (Refer to Damages 521100-200-804-A01) (Refer to Damages 521100-200-805-A01) (Refer to Damages 521100-200-806-A01) (Refer to Damages 521100-200-802-A01) (Refer to Damages 521100-200-803-A01)

Title After Conversion AFT PASSENGER/CREW DOOR AFT PASSENGER/CREW DOOR ALLOWABLE SCRATCHES, SCORES AND ABRASIONS AFT PASSENGER/CREW DOOR ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS AFT PASSENGER/CREW DOOR ALLOWABLE DENTS IN SKIN PANELS (D≥E) AFT PASSENGER/ CREW DOOR SHOOT BOLT AFT PASSENGER/CREW DOOR COUNTERBALANCE SPRINGS

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Before Conversion

52–21–00 Fig 301

After Conversion

Title After Conversion

(Refer to Damages 522100-200-801-A01)

PASSENGER COMPARTMENT EMERGENCY EXIT PASSENGER COMPARTMENT EMERGENCY EXIT ALLOWABLE SCRATCHES, SCORES AND ABRASIONS

(Refer to Damages 522100-200-802-A01) (Refer to Damages 522100-200-803-A01) (Refer to Damages 522100-200-804-A01) (Refer to Damages 522200-200-801-A01)

52–22–00 Fig 301

(Refer to Damages 522200-200-802-A01) (Refer to Damages 522200-200-803-A01) (Refer to Damages 522200-200-804-A01)

52–31–00 Fig 301

52–31–00 Fig 302

52–42–00 Fig 301

52–42–00 Fig 302

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(Refer to Damages 523100-200-801-A01) (Refer to Damages 523100-200-803-A01) (Refer to Damages 523100-200-804-A01) (Refer to Damages 523100-200-805-A01) (Refer to Damages 523100-200-802-A01) (Refer to Damages 524200-200-801-A01) (Refer to Damages 524200-200-803-A01) (Refer to Damages 524200-200-804-A01) (Refer to Damages 524200-200-805-A01) (Refer to Damages 524200-200-802-A01)

PASSENGER COMPARTMENT EMERGENCY EXIT ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS PASSENGER COMPARTMENT EMERGENCY EXIT ALLOWABLE DENTS IN SKIN PANELS (D≥E)

FLIGHT COMPARTMENT OVERHEAD HATCH FLIGHT COMPARTMENT OVERHEAD HATCH ALLOWABLE SCRATCHES, SCORES AND ABRASIONS

FLIGHT COMPARTMENT OVERHEAD HATCH ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FLIGHT COMPARTMENT OVERHEAD HATCH ALLOWABLE DENTS IN SKIN PANELS (D≥E) CARGO COMPARTMENT DOOR CARGO COMPARTMENT DOOR ALLOWABLE SCRATCHES, SCORES AND ABRASIONS CARGO COMPARTMENT DOOR ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS CARGO COMPARTMENT DOOR ALLOWABLE DENTS IN SKIN PANELS (D≥E) CARGO DOOR HINGES (FUSELAGE AND DOOR SIDE) SERVICE DOOR SERVICE DOOR ALLOWABLE SCRATCHES, SCORES AND ABRASIONS SERVICE DOOR ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS SERVICE DOOR ALLOWABLE DENTS IN SKIN PANELS (D≥E) SERVICE DOOR SHOOT BOLT

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Before Conversion 52–82–00 Fig 301



NLG AFT DOORS

Table 7: REPAIR

Before Conversion 52–00–00 Fig 401 52–11–00 Fig 401 52–11–00 Fig 402 52–11–00 Fig 403 52–11–00 Fig 404 52–11–00 Fig 405

After Conversion


(Refer to Repair 520000-300-801-A01) (Refer to Repair 521100-300-801-A01) (Refer to Repair 521100-300-802-A01) (Refer to Repair 521100-300-803-A01) (Refer to Repair 521100-300-804-A01) (Refer to Repair 521100-300-805-A01)

52–11–00 Fig 406

(Refer to Repair 521100-300-806-A01)

REPAIR SCHEME FOR HOLE FILLING BY FASTENER ON THE DOORS SKIN AFT PASSENGER/CREW DOOR — SHOOT BOLT SURFACE REPAIR AFT PASSENGER/CREW DOOR — FWD BTM INTERNAL REPAIR AFT PASSENGER/CREW DOOR — AFT BTM INTERNAL REPAIR AFT PASSENGER/CREW DOOR — BOTTOM INTERNAL REPAIR AFT PASSENGER/CREW DOOR — REPAIR SCHEME FOR INNER SKIN TOP AFT AFT PASSENGER/CREW DOOR — REPAIR SCHEME FOR INNER SKIN FWD — UPPER SIDE

52–11–00 Fig 407

(Refer to Repair 521100-300-807-A01)

52–11–00 Fig 408

(Refer to Repair 521100-300-808-A01)

52–11–00 Fig 409

(Refer to Repair 521100-300-809-A01)

52–21–00 Fig 401

(Refer to Repair 522100-300-801-A01)

52–31–00 Fig 401 52–31–00 Fig 402

(Refer to Repair 523100-300-801-A01) (Refer to Repair 523100-300-802-A01)

52–31–00 Fig 403

(Refer to Repair 523100-300-803-A01)

52–31–00 Fig 404 52–31–00 Fig 405


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After Conversion

AFT PASSENGER/CREW DOOR — REPAIR SCHEME FOR INNER SKIN FWD — UPPER SIDE

AFT PASSENGER/CREW DOOR — CRACK REPAIR LAST STEP FWD SEMI AUTOMATIC HANDRAIL AFT PASSENGER CREW DOOR - INTERMEDIATE STEPS FWD AND AFT - CRACK REPAIR

PASSENGER COMPARTMENT EMERGENCY EXIT — LOCALIZED DENT - SKIN REPAIR BY EXTERNAL PATCH

CARGO COMPARTMENT DOOR — PAN REPAIR CARGO COMPARTMENT DOOR — FITTING FOR LOWERING ARTICULATION POINT REPAIR SCHEME FOR INTERCOSTAL REPAIR-CARGO DOOR STA6250, STA6174 REPAIR SCHEME FOR INTERCOSTAL REPAIR-CARGO DOOR REPAIR SCHEME FOR CARGO DOOR PAN REPAIR AT STRUT FITTING LOCATION Page 12

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Before Conversion 52–31–00 Fig 406 52–31–00 Fig 407

After Conversion



52–31–00 Fig 408

(Refer to Repair 523100-300-808-A01)

REPAIR SCHEME FOR CARGO DOOR PAN REPAIR AT STRUT FITTING LOCATION REPAIR SCHEME FOR INTERCOSTAL REPAIR-CARGO DOOR CARGO COMPARTMENT DOOR REPAIR SCHEME FOR INTERCOSTAL REPAIR STA6174, STA6250

52–31–00 Fig 409

(Refer to Repair 523100-300-809-A01)

52–31–00 Fig 410 52–41–00 Fig 401 52–42–00 Fig 401 52–42–00 Fig 402 52–42–00 Fig 403 52–42–00 Fig 404

(Refer to Repair 523100-300-810-A01) (Refer to Repair 524100-300-801-A01) (Refer to Repair 524200-300-801-A01) (Refer to Repair 524200-300-802-A01) (Refer to Repair 524200-300-803-A01) (Refer to Repair 524200-300-804-A01)

52–42–00 Fig 405

(Refer to Repair 524200-300-805-A01)

52–42–00 Fig 406 52–81–00 Fig 401


52–81–00 Fig 402

(Refer to Repair 528100-300-802-A01)

52–81–00 Fig 403 52–81–00 Fig 404 52–81–00 Fig 405 52–81–00 Fig 406

(Refer to Repair 528100-300-803-A01) (Refer to Repair 528100-300-804-A01) (Refer to Repair 528100-300-805-A01) (Refer to Repair 528100-300-806-A01)

52–82–00 Fig 401

(Refer to Repair 528200-300-801-A01)

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CARGO COMPARTMENT DOOR REPAIR SCHEME FOR INTERCOSTAL REPAIR STA6434.75, STA6619.5, STA6695.5, STA7065, STA7141

CARGO COMPARTMENT DOOR - PAN REPAIR - ACTUATOR FITTING AREA REPAIR SCHEME FOR AFT ACCESS DOOR SKIN AT FRAME 45 SERVICE DOOR — SHOOT BOLT SURFACE REPAIR (STEP BY STEP) SERVICE DOOR — PAN REPAIR ON FWD BTM SIDE SERVICE DOOR — PAN REPAIR ON AFT BOTTOM SIDE SERVICE DOOR — PAN REPAIR ON AFT BOTTOM SIDE SERVICE DOOR - REPAIR SCHEME FOR SERVICE DOOR LOWER FRONT AND REAR CORNER

SERVICE DOOR — REPAIR SCHEME FOR DAMAGED SKIN AT DOOR HINGE AREA MLG DOORS — METALLIC SANDWICH PANELS REPAIR MLG DOOR — REPAIR SCHEME FOR DAMAGE DOOR REAR EDGE — (OBSOLETE) MLG DOOR — REPAIR SCHEME FOR DEBONDING ON FOLDING DOOR EDGE MLG DOOR — REPAIR SCHEME EDGE SKIN DEBONDING MLG DOOR — OUTER SKIN REPAIR (LH/RH SIDE) MLG CORROSION REPAIR UNDER SEAL RETAINER (LH/RH) NLG DOORS — REPAIR AND REINFORCEMENT OF THE ANGLES OF AFT NLG DOORS

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After Conversion



52–82–00 Fig 404

(Refer to Repair 528200-300-804-A01)

NLG DOORS — REPAIR SCHEME FOR AFT DOOR CORE SKIN DEBOND NLG DOORS — REPAIR SCHEME FOR DAMAGED AFT DOOR REPAIR SCHEME TO REPLACE THE BUSHING OF AFT NLG DOOR HINGE FITTING (LH/RH)

CHAPTER 53 Table 8: ALLOWABLE DAMAGE

Before Conversion 53–00–00 Fig 301 53–00–00 Fig 302 53–00–00 Fig 303 53–00–00 Fig 304 53–00–00 Fig 305

(Refer to Damages 530000-200-801-A01) (Refer to Damages 530000-200-802-A01) (Refer to Damages 530000-200-803-A01) (Refer to Damages 530000-200-804-A01) (Refer to Damages 530000-200-805-A01)

53–00–00 Fig 306


After Conversion

(Refer to Damages 531100-200-801-A01) (Refer to Damages 531100-200-803-A01) 53–11–00 Fig 301


53–11–00 Fig 302

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Title After Conversion CARGO AREA FLOOR PANEL AISLE, ENTRY DOOR AND TOILET AREA FLOOR PANEL UNDER SEAT AREA FLOOR PANEL FUSELAGE STRUCTURE SEAT TRACK FUSELAGE STRUCTURE FLOOR BEAM FUSELAGE FLOOR PANELS ATTACHMENT WITH SEAT TRACKS AND FLOOR BEAMS (FROM FRAME 13 TO 39) - ALLOWABLE MISSING FASTENERS FUSELAGE NOSE SECTION STRUCTURE FUSELAGE NOSE SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS FUSELAGE NOSE SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS IN PRESSURIZED BULKHEADS FUSELAGE NOSE SECTION STRUCTURE — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FUSELAGE NOSE SECTION STRUCTURE — ALLOWABLE DENTS IN SKIN PANELS (VALID FOR D≥E) FUSELAGE NOSE SECTION STRUCTURE — STATIC AREA (LH AND RH)

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Before Conversion

After Conversion



FUSELAGE FWD SECTION STRUCTURE


53–31–00 Fig 301


53–31–81 Fig 301


53–51–00 Fig 301


53–57–30 Fig 301 53–61–00 Fig 301

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(Refer to Damages 535730-200-801-A01) (Refer to Damages 536100-200-801-A01)

FUSELAGE FWD SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS FUSELAGE FWD SECTION STRUCTURE — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FUSELAGE FWD SECTION STRUCTURE — ALLOWABLE DENTS IN SKIN PANELS (VALID FOR D≥E)

FUSELAGE FWD SECTION STRUCTURE — WINDOW FRAME ALLOWABLE DAMAGES FUSELAGE FWD SECTION STRUCTURE SEAT TRACK AND FLOOR BEAM — ALLOWABLE DAMAGES REFERENCE CHAPTERS ICE SHIELD LH/RH FUSELAGE CENTER SECTION STRUCTURE FUSELAGE CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS

FUSELAGE CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS IN PRESSURIZED BULKHEAD FUSELAGE CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FUSELAGE CENTER SECTION STRUCTURE — ALLOWABLE DENTS IN SKIN PANELS (D≥E)

FUSELAGE CENTER SECTION STRUCTURE — WINDOW FRAME ALLOWABLE DAMAGES FUSELAGE CENTER SECTION STRUCTURE SEAT TRACK AND FLOOR BEAM — ALLOWABLE DAMAGES REFERENCE CHAPTERS MLG ATTACH FITTINGS - LH/RH FUSELAGE REAR CENTER SECTION STRUCTURE — ALLOWABLE DAMAGES

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Before Conversion

After Conversion



FUSELAGE REAR CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS

(Refer to Damages 536100-200-803-A01) (Refer to Damages 536100-200-804-A01) (Refer to Damages 536100-200-805-A01) (Refer to Damages 536100-200-806-A01) (Refer to Damages 536100-200-807-A01) (Refer to Damages 538100-200-801-A01) (Refer to Damages 538100-200-802-A01) 53–81–00 Fig 301


53–91–00 Fig 301 53–91–20 Fig 301 53–91–22 Fig 301 53–91–24 Fig 301

INTRODUCTION

R


FUSELAGE REAR CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS IN TOILET AND SERVICE POINT AREAS FUSELAGE REAR CENTER SECTION STRUCTURE — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FUSELAGE REAR SECTION STRUCTURE — ALLOWABLE DENTS IN SKIN PANELS (D≥E)

FUSELAGE REAR SECTION STRUCTURE — WINDOW FRAMES ALLOWABLE DAMAGES FUSELAGE REAR SECTION STRUCTURE — ALLOWABLE DAMAGES REFERENCE CHAPTERS FUSELAGE TAIL SECTION STRUCTURE FUSELAGE TAIL SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS

FUSELAGE TAIL SECTION STRUCTURE — ALLOWABLE SCRATCHES, SCORES AND ABRASIONS IN PRESSURIZED BULKHEAD FUSELAGE TAIL SECTION STRUCTURE — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS FUSELAGE TAIL SECTION STRUCTURE — ALLOWABLE DENTS IN SKIN PANELS (D≥E) RADOME, MLG FAIRING AND TAIL CONE AREAS

LANDING LIGHT TRANSPARENT COVER FAIRING SKIN PANELS STROBO LIGHT TRANSPARENT COVER

Page 16

Oct 01/14


After Conversion


53–00–00 Fig 401

(Refer to Repair 530000-300-801-A01)

53–00–00 Fig 402 53–00–00 Fig 403 53–00–00 Fig 404 53–00–00 Fig 405 53–00–00 Fig 406 53–00–00 Fig 407 53–00–00 Fig 408 53–00–00 Fig 409 53–00–00 Fig 410 53–00–00 Fig 411X

(Refer to Repair 530000-300-802-A01) (Refer to Repair 530000-300-803-A01) (Refer to Repair 530000-300-804-A01) (Refer to Repair 530000-300-805-A01) (Refer to Repair 530000-300-806-A01) (Refer to Repair 530000-300-807-A01) (Refer to Repair 530000-300-808-A01) (Refer to Repair 530000-300-809-A01) (Refer to Repair 530000-300-810-A01) (Refer to Repair 530000-300-811-A01)

FUSELAGE SKIN - REPAIR SCHEME FOR ELONGATED HOLES BY SHOULDER BUSHING

53–00–00 Fig 412

(Refer to Repair 530000-300-812-A01)

53–00–00 Fig 413

(Refer to Repair 530000-300-813-A01)

53–00–00 Fig 414 53–00–00 Fig 415 53–00–00 Fig 416 53–00–00 Fig 417


53–00–00 Fig 418

(Refer to Repair 530000-300-818-A01)

53–00–00 Fig 419

(Refer to Repair 530000-300-819-A01)

INTRODUCTION

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Table 9: REPAIR

Before Conversion

FUSELAGE SKIN - SMALL DAMAGE/EXTERNAL REPAIR FUSELAGE SKIN - SMALL DAMAGE/FLUSH REPAIR FUSELAGE SKIN - BETWEEN STRINGERS/EXTERNAL REPAIR FUSELAGE SKIN - BETWEEN STRINGERS/FLUSH REPAIR FUSELAGE SKIN - AT STRINGER/EXTERNAL REPAIR FUSELAGE SKIN - AT STRINGER/FLUSH REPAIR FUSELAGE SKIN - AT FRAME (WITH SKIN PAD)/EXTERNAL REPAIR FUSELAGE SKIN - AT FRAME (WITHOUT SKIN PAD)/EXTERNAL REPAIR FUSELAGE SKIN - AT FRAME (WITHOUT SKIN PAD)/FLUSH REPAIR FUSELAGE SKIN - AT STRINGER/TEMPORARY REPAIR FUSELAGE SKIN - AT STRINGER LOCATION/EXTERNAL REPAIR (TEMPORARY TO PERMANENT) FUSELAGE SKIN - AT STRINGER LOCATION/FLUSH REPAIR (TEMPORARY TO PERMANENT) FUSELAGE FRAME INNER FLANGE REPAIR FUSELAGE FRAME OUTER FLANGE REPAIR FUSELAGE FRAME - HEAVY DAMAGE FLANGE REPAIR FUSELAGE FRAME - FAIL SAFE ANGLE REPAIR FUSELAGE SEAT TRACK REPAIR (UPPER HORIZONTAL FLANGE REPLACEMENT)

FUSELAGE SEAT TRACK REPAIR (UPPER HORIZONTAL FLANGE + WEB REPLACEMENT) Page 17

Oct 01/14


Before Conversion

After Conversion


53–00–00 Fig 420

(Refer to Repair 530000-300-820-A01)

53–00–00 Fig 421 53–00–00 Fig 422


FUSELAGE SKIN - LONGITUDINAL LAP JOINT BETWEEN FRAMES (BOTH — SKINS ENDS DAMAGED)/EXTERNAL REPAIR

53–00–00 Fig 423

(Refer to Repair 530000-300-823-A01)

53–00–00 Fig 424

(Refer to Repair 530000-300-824-A01)

53–00–00 Fig 425

(Refer to Repair 530000-300-825-A01)

53–00–00 Fig 426

(Refer to Repair 530000-300-826-A01)

53–00–00 Fig 427 53–00–00 Fig 428 53–00–00 Fig 429

(Refer to Repair 530000-300-827-A01) (Refer to Repair 530000-300-828-A01) (Refer to Repair 530000-300-829-A01)

53–00–00 Fig 430

(Refer to Repair 530000-300-830-A01)

53–00–00 Fig 431 53–00–00 Fig 432


53–00–00 Fig 433

(Refer to Repair 530000-300-833-A01)

53–00–00 Fig 434

(Refer to Repair 530000-300-834-A01)

53–00–00 Fig 435

(Refer to Repair 530000-300-835-A01)

53–00–00 Fig 436

(Refer to Repair 530000-300-836-A01)

INTRODUCTION

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FUSELAGE SKIN - LONGITUDINAL LAP JOINT BETWEEN FRAMES/FLUSH REPAIR FUSELAGE SKIN - AT FRAME (WITH SKIN PAD)/FLUSH REPAIR FUSELAGE SKIN - REPAIR SCHEME FOR UPPER AND LOWER SKINS AT LONGITUDINAL LAP JOINT AND FRAMES/EXTERNAL REPAIR FUSELAGE SKIN - REPAIR SCHEME FOR UPPER SKIN AT LONGITUDINAL LAP JOINT BETWEEN FRAMES/EXTERNAL REPAIR FUSELAGE STRINGER FORMED STRINGER REPAIR FUSELAGE STRINGER - EXTRUSION STRINGER OUTSIDE SPECIAL STGR4 AND STGR5 REPAIR FUSELAGE STRINGER - TYPICAL EXTRUDED STRINGER REPAIR FUSELAGE FLOOR BEAM FLOOR CROSS BEAM REPAIR FUSELAGE CREASE BEAM - REPAIR SCHEME FUSELAGE SKIN - REPAIR SCHEME SKIN FOR HOLE WITH EXTERNAL DOUBLER

FUSELAGE SKIN - REPAIR SCHEME FOR SKIN HOLE WITH INTERNAL DOUBLER FUSELAGE SEAT TRACK REPAIR SCHEME FOR SPLICING FUSELAGE FRAME - REPAIR SCHEME FOR LOWER FR13 TO FR34 BETWEEN STGR17 LH/RH FUSELAGE FRAME - REPAIR SCHEME FOR CORROSION ON FRAMES — BETWEEN STGR17 LH/RH FUSELAGE SKIN - REPAIR SCHEME FOR HOLE FILLING BY FASTENER FUSELAGE FLOOR BEAM FRAMES/REPAIR SCHEME FOR FLOOR BEAM SPLICE Page 18

Oct 01/14



53–00–00 Fig 438


FUSELAGE FLOOR BEAM - FRAMES/ (Refer to Repair REPAIR SCHEME FOR FLOOR BEAM 530000-300-860-A01) Replaced by DWG S530R0022 issue B SPLICE AT SEAT TRACK - (OBSOLETE) (Refer to Repair FUSELAGE FLOOR BEAM - SPLICING 530000-300-837-A01) PRINCIPLE AT SEAT TRACK (RH SIDE) FUSELAGE COMPOSITE (Refer to Repair BONDED STRUCTURE FIBRELAM 530000-300-838-A01) SANDWICH PANEL REPAIR (Refer to Repair 530000-300-839-A01)

53–00–00 Fig 439

(Refer to Repair 530000-300-840-A01)

53–00–00 Fig 440 53–00–00 Fig 441


53–00–00 Fig 442

(Refer to Repair 530000-300-842-A01)

53–00–00 Fig 443

(Refer to Repair 530000-300-843-A01)

53–00–00 Fig 444

(Refer to Repair 530000-300-844-A01)

53–00–00 Fig 445

(Refer to Repair 530000-300-845-A01)

53–00–00 Fig 446

(Refer to Repair 530000-300-846-A01)

53–00–00 Fig 447

(Refer to Repair 530000-300-847-A01)

53–00–00 Fig 448

(Refer to Repair 530000-300-848-A01)

53–00–00 Fig 449

(Refer to Repair 530000-300-849-A01)

INTRODUCTION

R

After Conversion

FUSELAGE COMPOSITE SUPERFICIAL DAMAGE REPAIR FUSELAGE COMPOSITE IDENTATION CAUSING DAMAGE TO BOTH SKIN AND CORE

FUSELAGE COMPOSITE DELAMINATION REPAIR FUSELAGE COMPOSITE - FIBRELAM SANDWICH PANEL INSERT REMOVAL FUSELAGE FLOOR BEAM REPAIR SCHEME - FOR SPLICE AT SEAT TRACK RUN-OUT FUSELAGE SEAT TRACK REPAIR SCHEME FOR SEAT TRACK TO FLOOR BEAM JOINT

FUSELAGE FRAME - REPAIR SCHEME FOR FRAME FAIL SAFE ANGLE SPLICE (PRINCIPLE BETWEEN TWO ADJACENT STRINGERS) FUSELAGE FRAME - LWR FRAME INNER FLANGE SPLICING (FOR PARTIAL REPLACEMENT OF FRAME) AT STRINGER LEVEL - (OBSOLETE)

FUSELAGE COMPOSITE - REPAIR SCHEME TO INSTALL INSERT NTA12151 OR NTA12150 ON THE FLOOR PANEL WITH MISALIGNED/ELONGATED HOLE FUSELAGE STRINGER BONDED STRINGER/REPAIR BY STRINGER SPLICE

FUSELAGE STRINGER - BONDED STRINGER/DE-BONDED REPAIR FUSELAGE FLOOR BEAM - REPAIR SCHEME FOR UPPER AND LOWER FLANGE (APPLICABLE TO FLOOR BEAM MADE FROM NTA44770)

Page 19

Oct 01/14


Before Conversion

After Conversion


53–00–00 Fig 450

(Refer to Repair 530000-300-850-A01)

FUSELAGE COLD WORKED HOLE REPAIR SCHEME FOR FILLING BY FASTENER ON FUSELAGE FORMED FRAMES, STRINGERS, SEAT, TRACKS, FLOOR BEAMS AND STIFFENERS

53–00–00 Fig 451


53–00–00 Fig 452

(Refer to Repair 530000-300-852-A01)

53–00–00 Fig 453

(Refer to Repair 530000-300-853-A01)

53–00–00 Fig 454 53–00–00 Fig 455 53–11–00 Fig 401 53–11–10 Fig 401


53–11–10 Fig 402

(Refer to Repair 531110-300-802-A01)

53–11–10 Fig 403 53–11–10 Fig 404 53–11–10 Fig 405


53–11–10 Fig 406

(Refer to Repair 531110-300-806-A01)

53–11–24 Fig 401

(Refer to Repair 531124-300-801-A01)

INTRODUCTION

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FUSELAGE CREASE BEAM - SPLICING PRINCIPLE OF INNER CHORD AT FR19 FUSELAGE CREASE BEAM - SPLICING PRINCIPLE OF INNER CHORD AT FR20 FUSELAGE CREASE BEAM - SPLICING PRINCIPLE OF INNER CHORD AT FR21 FUSELAGE CREASE BEAM - SPLICING PRINCIPLE OF INNER CHORD AT FR31 OR FR32 OR FR33 FUSELAGE FLOOR BEAM SPLICING PRINCIPLE AT STATION STA6427.3, STA6887.7, STA7348, STA10076 AND STA15959 FUSELAGE SEAT TRACK REPAIR SCHEME FOR SEAT TRACK SPLICING AT FLOOR BEAM

FUSELAGE FLOOR BEAM - SPLICING PRINCIPLE AT FR36 NEAR BL0 FUSELAGE FLOOR BEAM SPLICING PRINCIPLE AT FR36 REPAIR SCHEME FOR FUSELAGE SKIN/OIL CANNING REPAIR SCHEME FOR DAMAGED WEB CHORD AND SPLICE PLATE REPAIR SCHEME FOR DAMAGED BULKHEAD CHORD BETWEEN BL0 AND BL475 - LH/RH SIDE REPAIR SCHEME FOR BURN FR1 WEB REPAIR SCHEME FOR DAMAGED FR1 WEB AT STA2962 REPAIR BULKHEAD STIFFENERS CORROSION LOWER WEB FRAME 1 CORROSION REPAIR (LH/RH) BETWEEN BL187.5 AND BL350

REPAIR SCHEME FOR DAMAGED SKIN BETWEEN FR5 AND FR6 AND FROM WL2327.5 TO WL2640.4

Page 20

Oct 01/14


Before Conversion

After Conversion


53–11–28 Fig 401

(Refer to Repair 531128-300-801-A01)

53–11–28 Fig 402 53–11–28 Fig 403 53–11–28 Fig 405

(Refer to Repair 531128-300-802-A01) (Refer to Repair 531128-300-802-B01) (Refer to Repair 531128-300-805-A01)

REPAIR SCHEME FOR LOWER PANEL AT FR9 AND BETWEEN STGR11 AND STGR12A

53–11–28 Fig 406

(Refer to Repair 531128-300-806-A01)

53–11–28 Fig 407 53–11–28 Fig 408 53–11–31 Fig 401 53–11–40 Fig 401 53–11–40 Fig 402X

(Refer to Repair 531128-300-807-A01) (Refer to Repair 531128-300-808-A01) (Refer to Repair 531131-300-801-A01) (Refer to Repair 531140-300-801-A01) (Refer to Repair 531140-300-802-A01)

53–11–40 Fig 403

(Refer to Repair 531140-300-803-A01)

53–31–21 Fig 401

(Refer to Repair 533121-300-801-A01)

53–31–26 Fig 401

(Refer to Repair 533126-300-801-A01)

53–31–26 Fig 402

New Repair moved from 53–11–28 Fig.404 to 53–31–26 Fig.402 (Refer to Repair 533126-300-802-A01)

53–31–50 Fig 401 53–31–81 Fig 401 53–33–00 Fig 401 53–51–40 Fig 401 INTRODUCTION

R


REPAIR SCHEME FOR SKIN CORROSION AT “DME 2” ANTENNA LOCATION REPAIR SCHEME FOR SKIN CORROSION AT “DME 2” ANTENNA LOCATION RH LOWER AFT PANEL REPAIR GROUND POWER BOX RH LOWER AFT PANEL DOUBLER FOR EXTERNAL DC POWER RECEPTACLE REPAIR

RH LOWER AFT PANEL POWER BOX CRACK REPAIR RH LOWER AFT SKIN PANEL REPAIR BETWEEN FR7 AND FR8 AT BL800 REPAIR SCHEME FOR CRACK OF LOWER SILL BETWEEN NODES 6/7 REPAIR SCHEME FOR DAMAGED TEE FLOOR BEAM SPLICE AT STA4426/FR7 TEMPORARY REPAIR SCHEME FOR CRACK ON LH/RH FRAME 5 AT STA3982.5 PERMANENT REPAIR SCHEME FOR FUSELAGE FRAME 5 BETWEEN STGR11 AND NODE 6 (LH/RH) CROWN PANEL - REPAIR SCHEME FOR SKIN CORROSION AT ADF1 AND ADF2 ANTENNA LOCATION (COLLINS)

REPAIR SCHEME FOR FUSELAGE LOWER SKIN CORROSION BETWEEN FR19 AND FR20 AT BL0 UNDER TCAS ANTENNA REPAIR SCHEME FOR SKIN CORROSION AT DME1 ANTENNA LOCATION CHORD CREASE BEAM REPAIR REPAIRS FOR METALLIC ICE SHIELD REPAIR SCHEME FOR SEAT TRACK SPLICING REPAIR SCHEME FOR CRACK ON FR26/ STGR13 (LH/RH) - (OBSOLETE) Page 21

Oct 01/14



After Conversion


(Refer to Repair 535300-300-801-A01)

53–57–30 Fig 401

(Refer to Repair 535730-300-801-A01)

SEAT TRACKS - REPAIR SCHEME FOR SEAT TRACK SPLICING REPAIR SCHEME FOR CORROSION BLEND OUT ALLOWABLE DAMAGE ON TRUSS SHEAR MEMBER LUGS, F/ S AND R/S MLG FITTINGS LUGS AND F/S AND R/S STRUTS LUGS

53–57–70 Fig 401

(Refer to Repair 535770-300-802-A01)

53–61–25 Fig 401

(Refer to Repair 536125-300-801-A01)

53–61–40 Fig 401

(Refer to Repair 536140-300-801-A01)

53–61–40 Fig 402

(Refer to Repair 536140-300-802-A01)

53–61–40 Fig 403 53–61–40 Fig 404 53–61–40 Fig 405


53–61–40 Fig 406

(Refer to Repair 536140-300-806-A01)

53–61–40 Fig 407

(Refer to Repair 536140-300-807-A01)

53–61–40 Fig 408 53–63–00 Fig 401


53–67–70 Fig 401

(Refer to Repair 536770-300-801-A01)

53–81–40 Fig 401

(Refer to Repair 538140-300-801-A01)

INTRODUCTION

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(Refer to Repair 535770-300-801-A01)

KEEL BEAM PLATE REPAIR LH/ RH SIDE BETWEEN FRAME 25 AND FRAME 27 AT STRINGER 21 (4 CASES) MLG BULKHEADS - KEEL BEAM PLATE REPAIR LH/RH BETWEEN FRAME 25 AND FRAME 27 AT STRINGER 21 (4 CASES) LH LATERAL LOWER PANEL - REPAIR SCHEME FOR PAX DOOR SURROUND SKIN AT SHOOT BOLT LOCATION LH/RH SIDE REPAIR SCHEME FOR FRAMES 30, 31, 33 AND 34 SPLICING LH AND RH BETWEEN STRINGERS 10 AND 11 REPAIR SCHEME FOR FLOOR BEAM REPLACEMENT BY SPLICE AT FRAME 41 (STA19149) LH AND RH SIDE

REPAIR SCHEME FOR FRAME 36 SPLICING LH AND RH AT STRINGER 18 REPAIR SCHEME FOR FRAME 38 SPLICING LH AND RH AT STRINGER 18 REPAIR SCHEME FOR FRAME 39 SPLICING LH AND RH AT STRINGER 18 FRAMES - STA17319/FR36 REPAIR SCHEME FOR LOCAL REINFORCEMENT BETWEEN STGR14 AND STGR15 (RH/LH SIDE) REPAIR SCHEME FOR LOWER FRAME 40 SPLICING BETWEEN STGR19 LH AND STGR19 RH

FLOOR BEAM CORROSION REPAIR AT STA19149/FR41 RH SIDE SEAT TRACKS - REPAIR SCHEME FOR SEAT TRACK SPLICING FRAMES - STA17459/FR37 REPAIR SCHEME FOR LOCAL REINFORCEMENT BETWEEN STGR14 AND STGR15 (RH SIDE)

FRAME - REPAIR SCHEME FOR A LIGHT CORROSION ON FRAME 44 (STA 20425) Page 22

Oct 01/14


Before Conversion 53–81–40 Fig 402 53–83–00 Fig 401 53–91–21 Fig 401 53–91–21 Fig 402

After Conversion

Title After Conversion FRAME - REPAIR SCHEME FOR A HEAVY CORROSION ON FRAME 44 (STA 20425) SEAT TRACKS - REPAIR SCHEME FOR SEAT TRACK SPLICING

53–91–22 Fig 401 53–91–42 Fig 401 53–91–43 Fig 401

(Refer to Repair 538140-300-802-A01) (Refer to Repair 538300-300-801-A01) (Refer to Repair 539121-300-801-A01) (Refer to Repair 539121-300-802-A01) (Refer to Repair 539121-300-803-A01) (Refer to Repair 539121-300-804-A01) (Refer to Repair 539122-300-801-A01) (Refer to Repair 539142-300-801-A01) (Refer to Repair 539143-300-801-A01)

53–91–43 Fig 402

(Refer to Repair 539143-300-802-A01)

53–91–80 Fig 401

(Refer to Repair 539180-300-801-A01)

53–91–21 Fig 403

RADOME REPAIR RADOME PAINTING RADIO ELECTRIC INSPECTION INSTALLATION OF LIGHTNING PROTECTION AND INSPECTION WING TO FUSELAGE FAIRING SKIN PANELS - REPAIR REPAIR SCHEME FOR FLANGE RIB 29 LH AND RH SIDE REPAIR SCHEME FOR MLG FAIRING FRAME 27A (LH/RH) SMALLER DAMAGE REPAIR SCHEME FOR MLG FAIRING FRAME 27A (LH AND RH) BIGGER DAMAGE MISCELLANEOUS - MLG FAIRING RIB REPAIR

CHAPTER 54 Before Conversion 54–11–61 Fig 301 Config 1 54–11–61 Fig 301 Config 2 54–21–61 Fig 301 Config 1 54–21–61 Fig 301 Config 2

INTRODUCTION

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Table 10: ALLOWABLE DAMAGE After Conversion



TUBULAR MOUNT

(Refer to Damages 541161-200-801-B01)

TUBULAR MOUNT


TUBULAR MOUNT


TUBULAR MOUNT

Page 23

Oct 01/14


Before Conversion 54–11–61 Fig 401 Config 1 54–11–61 Fig 401 Config 2 54–11–61 Fig 402 Config 1 54–11–61 Fig 402 Config 2 54–11–62 Fig 401 Config 1 54–11–62 Fig 401 Config 2 54–12–61 Fig 401 Config 1 54–12–61 Fig 401 Config 2 54–12–61 Fig 402 Config 1 54–12–61 Fig 403 Config 1 54–12–61 Fig 402 Config 2 54–12–61 Fig 404 Config 1 54–12–61 Fig 405 Config 1 54–12–61 Fig 406 Config 1

INTRODUCTION

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Table 11: REPAIR After Conversion


(Refer to Repair 541161-300-801-A01)

REPAIR SCHEME FOR A SUPERFICIAL SMOOTHING ON FORWARD TUBULAR MOUNT

(Refer to Repair 541161-300-801-B01) (Refer to Repair 541161-300-802-A01) (Refer to Repair 541161-300-802-B01) (Refer to Repair 541162-300-801-A01)

REPAIR SCHEME FOR A SUPERFICIAL SMOOTHING ON FORWARD TUBULAR MOUNT REPAIR SCHEME FOR A CALIBRATED SMOOTHING ON FORWARD TUBULAR MOUNT REPAIR SCHEME FOR A CALIBRATED SMOOTHING ON FORWARD TUBULAR MOUNT

ATTACH FITTINGS — REPAIR SCHEME FOR FWD BEAM ATTACHMENT JUNCTION SHACKLE (ELONGATED HOLES)

(Refer to Repair 541162-300-801-B01)

ATTACH FITTINGS — REPAIR SCHEME FOR FWD BEAM ATTACHMENT JUNCTION SHACKLE (ELONGATED HOLES)

(Refer to Repair 541261-300-801-A01)

COWLS AND FAIRINGS — REPAIR SCHEME FOR DAMAGED COWL

(Refer to Repair 541261-300-801-B01)

COWLS AND FAIRINGS — REPAIR SCHEME FOR DAMAGED COWL

(Refer to Repair 541261-300-802-A01)

COWLS AND FAIRINGS — REPAIR SCHEME FOR CRACKS ON OUTLET ASSY - AIR

(Refer to Repair 541261-300-803-A01)

COWLS AND FAIRINGS — REPAIR SCHEME FOR CRACK ON AFT EDGING

(Refer to Repair 541261-300-803-B01)

COWLS AND FAIRINGS — REPAIR SCHEME FOR CRACK ON AFT EDGING

(Refer to Repair 541261-300-804-A01)

OIL COOLER DUCT — REPAIR SCHEME FOR CRACKS ON UPPER SURFACE AT ATTACHMENT HOLES

(Refer to Repair 541261-300-805-A01)

OIL COOLER DUCT — REPAIR SCHEME FOR CRACKS, CHIPPING AND ELONGATION AT ATTACHMENT HOLES

(Refer to Repair 541261-300-806-A01)

OIL COOLER DUCT — REPAIR SCHEME FOR CRACKS ON UPPER SURFACE

Page 24

Oct 01/14


Before Conversion 54–12–61 Fig 403 Config 2 54–12–61 Fig 407 Config 1 54–12–61 Fig 408 Config 1 54–12–61 Fig 404 Config 2 54–12–61 Fig 409 Config 1 54–12–61 Fig 405 Config 2 54–12–61 Fig 410 Config 1 54–12–61 Fig 406 Config 2 54–12–61 Fig 411 Config 1 54–12–61 Fig 407 Config 2 54–21–61 Fig 401 Config 1 54–21–61 Fig 401 Config 2 54–21–61 Fig 402 Config 1 54–21–61 Fig 402 Config 2 54–22–61 Fig 401 Config 1 INTRODUCTION

R

After Conversion


(Refer to Repair 541261-300-806-B01)

OIL COOLER DUCT — REPAIR SCHEME FOR CRACKS ON UPPER SURFACE

(Refer to Repair 541261-300-807-A01)

OIL COOLER DUCT — REPAIR SCHEME FOR WEARS ON UPPER SURFACE

(Refer to Repair 541261-300-808-A01)

COWL AND FAIRING — REPAIR SCHEMES FOR CRACK ON UPPER COWL AT CENTER CUT OUT

(Refer to Repair 541261-300-808-B01)

COWL AND FAIRING — REPAIR SCHEMES FOR CRACK ON UPPER COWL

(Refer to Repair 541261-300-809-A01)

COWL AND FAIRING — REPAIR SCHEMES FOR CRACK ON SKIN OF UPPER COWL AT CORNER

(Refer to Repair 541261-300-809-B01)

COWL AND FAIRING — REPAIR SCHEMES FOR CRACK ON SKIN OF UPPER COWL

(Refer to Repair 541261-300-810-A01)

COWL AND FAIRING — REPAIR SCHEMES FOR THE EDGING CRACK ON UPPER COWL

(Refer to Repair 541261-300-810-B01) (Refer to Repair 541261-300-811-A01)

COWL AND FAIRING — REPAIR SCHEMES FOR THE EDGING CRACK ON UPPER COWL COWL AND FAIRING — REPAIR SCHEME FOR UPPER COWL COMPONENTS REPLACEMENT

(Refer to Repair 541261-300-811-B01)

COWL AND FAIRING — REPAIR SCHEME FOR UPPER COWL COMPONENTS REPLACEMENT

(Refer to Repair 542161-300-801-A01)

REPAIR SCHEME FOR A SUPERFICIAL SMOOTHING ON REAR TUBULAR MOUNT

(Refer to Repair 542161-300-801-B01)

REPAIR SCHEME FOR A SUPERFICIAL SMOOTHING ON REAR TUBULAR MOUNT

(Refer to Repair 542161-300-802-A01)

REPAIR SCHEME FOR A CALIBRATED SMOOTHING ON REAR TUBULAR MOUNT

(Refer to Repair 542161-300-802-B01)

REPAIR SCHEME FOR A CALIBRATED SMOOTHING ON REAR TUBULAR MOUNT

(Refer to Repair 542261-300-801-A01)

REPAIR SCHEME FOR DAMAGED EDGE ON LATERAL PANEL

Page 25

Oct 01/14


Before Conversion 54–22–61 Fig 401 Config 2 54–22–61 Fig 402 Config 1 54–22–61 Fig 402 Config 2 54–22–61 Fig 403X Config 1 54–22–61 Fig 403X Config 2 54–22–61 Fig 404 Config 1 54–22–61 Fig 405X Config 1 54–22–61 Fig 405X Config 2 54–22–61 Fig 405 Config 1 54–22–61 Fig 405 Config 2 54–22–61 Fig 403 Config 1 54–22–61 Fig 403 Config 2 54–22–61 Fig 406 Config 1 54–22–61 Fig 407 Config 1 54–22–61 Fig 404 Config 2 INTRODUCTION

R

After Conversion


(Refer to Repair 542261-300-801-B01)

REPAIR SCHEME FOR DAMAGED EDGE ON LATERAL PANEL

(Refer to Repair 542261-300-802-A01)

REPAIR SCHEME FOR CRACK ON FIREWALL DEFINITION OF ZONES

(Refer to Repair 542261-300-802-B01)

REPAIR SCHEME FOR CRACK ON FIREWALL DEFINITION OF ZONES

(Refer to Repair 542261-300-803-A01)

TEMPORARY REPAIR SCHEME FOR CRACK ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-803-B01)

TEMPORARY REPAIR SCHEME FOR CRACK ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-804-A01)

REPAIR SCHEME FOR CRACK ON REINFORCING ANGLE

(Refer to Repair 542261-300-805-A01)

TEMPORARY REPAIR SCHEME FOR CRACK ON FRONT FIREWALL PANEL

(Refer to Repair 542261-300-805-B01)

TEMPORARY REPAIR SCHEME FOR CRACK ON FRONT FIREWALL PANEL

(Refer to Repair 542261-300-806-A01)

REPAIR SCHEME FOR CRACK ON FRONT FIREWALL PANEL

(Refer to Repair 542261-300-806-B01)

REPAIR SCHEME FOR CRACK ON FRONT FIREWALL PANEL

(Refer to Repair 542261-300-807-A01)

REPAIR SCHEME FOR CRACK ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-807-B01)

REPAIR SCHEME FOR CRACK ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-808-A01)

REPAIR SCHEME FOR PERFORATION ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-809-A01)

REPAIR SCHEME FOR PERFORATION ON UPPER FIREWALL PANEL

(Refer to Repair 542261-300-810-A01)

REPAIR SCHEME FOR CRACK ON FIREWALL PANEL

Page 26

Oct 01/14


Before Conversion

After Conversion


54–32–61 Fig 401

(Refer to Repair 543261-300-801-A01)

FAIRING STRUCTURE - REPAIR SCHEME FOR DELAMINATION ON LOWER SURFACE OF ENGINE NACELLE

CHAPTER 55 Before Conversion 55–00–00 Fig 301 Config 1 55–00–00 GENERAL Config 2

Table 12: ALLOWABLE DAMAGE After Conversion



HORIZONTAL AND VERTICAL STABILIZER — DAMAGE TYPE AND DEFECT DESCRIPTION


HORIZONTAL AND VERTICAL STABILIZER DAMAGE TYPE AND DEFECT DESCRIPTION


C/E VERTICAL STABILIZER — ALLOWABLE DAMAGE


C/E HORIZONTAL STABILIZER — MULTISPAR BOX — ALLOWABLE DAMAGES


C/E VERTICAL AND HORIZONTAL STABILIZER JOINTS — ALLOWABLE DAMAGES

55–00–00 TABLE 1 Config 2 55–00–00 Fig 301 Config 2 55–00–00 Fig 302 Config 2 55–00–00 Fig 303 Config 2 55–00–00 Fig 324 Config 2 55–00–00 TABLE 2 Config 2 55–00–00 Fig 305 Config 2 55–00–00 Fig 306 Config 2 55–00–00 Fig 323 Config 2 55–00–00 TABLE 3 Config 2 INTRODUCTION

R

Page 27

Oct 01/14


Before Conversion 55–00–00 Fig 307 Config 2

After Conversion


55–00–00 Fig 308 Config 2 55–00–00 Fig 309 Config 2 55–00–00 Fig 310 Config 2 55–00–00 Fig 311 Config 2 55–00–00 Fig 312 Config 2 55–00–00 Fig 313 Config 2 55–00–00 Fig 314 Config 2 55–00–00 Fig 315 Config 2 55–00–00 Fig 316 Config 2 55–00–00 Fig 317 Config 2 55–00–00 Fig 318 Config 2 55–00–00 Fig 319 Config 2 55–00–00 Fig 320 Config 2 55–00–00 Fig 321 Config 2

INTRODUCTION

R

Page 28

Oct 01/14



After Conversion



HORIZONTAL STABILIZER — SPAR BOX

(Refer to Damages 551100-200-803-A01) 55–11–00 Fig 301


55–11–00 Fig 302 Config 1 and Config 2 55–12–30 Fig 301 55–20–00 Fig 301

INTRODUCTION

R

HORIZONTAL STABILIZER — SPAR BOX — ALLOWABLE DENTS IN SKIN PANELS (VALID FOR D≥E) HORIZONTAL STABILIZER — SPAR BOX — ALLOWABLE DENTS IN HONEYCOMB SKIN PANEL


HORIZONTAL STABILIZER — SPAR BOX — DAMAGE TYPES AND REPAIRS


HORIZONTAL STABILIZER LEADING EDGE SKIN PANELS ELEVATOR AND TABS COMPOSITE PARTS - ALLOWABLE DAMAGE


55–31–00 Fig 302 Config 1 and Config 2

HORIZONTAL STABILIZER — SPAR BOX — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS


(Refer to Damages 553100-200-803-A01) 55–31–00 Fig 301

HORIZONTAL STABILIZER — SPAR BOX — ALLOWABLE SCRATCHES, SCORES AND ABRASION

VERTICAL STABILIZER SPAR BOX VERTICAL STABILIZER — SPAR BOX — ALLOWABLE SCRATCHES, SCORES AND ABRASION

HORIZONTAL STABILIZER — SPAR BOX — ALLOWABLE SCRATCHES IN MACHINED AND EXTRUDED PARTS VERTICAL STABILIZER — SPAR BOX — ALLOWABLE DENTS IN SKIN PANEL (VALID FOR D≥E)


VERTICAL STABILIZER — SPAR BOX — ALLOWABLE DENTS IN HONEYCOMB SKIN PANEL


VERTICAL STABILIZER SPAR BOX FOR IMPACT DAMAGES TYPES AND REPAIRS

Page 29

Oct 01/14





RUDDER COMPOSITE PART ALLOWABLE DAMAGE RUDDER TAB

Table 13: REPAIR

Before Conversion 55–00–00 General

After Conversion


(Refer to Repair 550000-300-817-A01)

STABILIZERS — GENERAL — REPAIRS

55–00–00 Fig 401

(Refer to Repair 550000-300-801-A01)

55–00–00 Fig 402 55–00–00 Fig 403 55–00–00 Fig 404 55–00–00 Fig 405


55–00–00 Fig 406


55–00–00 Fig 407

(Refer to Repair 550000-300-807-A01)

55–00–00 Fig 408

(Refer to Repair 550000-300-808-A01)

55–00–00 Fig 409

(Refer to Repair 550000-300-809-A01)

55–00–00 Fig 410

(Refer to Repair 550000-300-810-A01)

55–00–00 Fig 411

(Refer to Repair 550000-300-811-A01)

INTRODUCTION

R

After Conversion

STABILIZER GENERAL — DEBONDED METALLIC SKIN AND HONEYCOMB CORE REPAIR

REPAIR OF SKIN REPAIR OF SKIN

DAMAGE TO ONE AND HONEYCOMB DAMAGE TO ONE AND HONEYCOMB

METALLIC CORE METALLIC CORE

REPAIR TO METALLIC SANDWICH PANEL REPAIR OF DENTS IN METAL HONEYCOMB STRUCTURE RUDDER, ELEVATOR AND TABS — GRAPHITE COMPOSITE STRUCTURE — REPAIR — PROCEDURE COMMON TO TYPICAL REPAIR FIGURE RUDDER, ELEVATOR AND TABS — REPAIR A — SEPARATION SKIN CORE AND DELAMINATION RUDDER, ELEVATOR AND TABS — REPAIR B — PERFORATING AND NON PERFORATING DAMAGE

RUDDER, ELEVATOR AND TABS — REPAIR C — SANDWICH STRUCTURE PERFORATING DAMAGE RUDDER, ELEVATOR AND TABS — REPAIR D1 AND REPAIR D2 — SEPARATION SKIN CORE DAMAGE

RUDDER, ELEVATOR AND TABS — REPAIR E1 AND REPAIR E2 — PERFORATING DAMAGE SANDWICH ZONE RUDDER, ELEVATOR AND TABS — REPAIR F — DENT ON SANDWICH STRUCTURE

Page 30

Oct 01/14


Before Conversion

After Conversion


55–00–00 Fig 412

(Refer to Repair 550000-300-812-A01)

RUDDER, ELEVATOR AND TABS — REPAIR G — DENT ON SANDWICH STRUCTURE

55–00–00 Fig 413

(Refer to Repair 550000-300-813-A01)

55–00–00 Fig 414

(Refer to Repair 550000-300-814-A01)

55–00–00 Fig 415

(Refer to Repair 550000-300-815-A01)

55–11–00 Fig 401 Config 1

(Refer to Repair 551100-300-801-A01)

HORIZONTAL STABILIZER — SPAR BOX — REPAIRS

(Refer to Repair 551100-300-802-A01)

REPAIR FOR LIGHT DAMAGES FOR RESIN FILLING

(Refer to Repair 551100-300-803-A01)

REPAIR FOR LIGHT DAMAGES BY RESIN FILLING AND EXTRA PLIES

(Refer to Repair 551100-300-804-A01)

HOT BOND REPAIR FOR NONPERFORATING DAMAGE ON PANEL EDGE CLOSE TO REAR SPAR

55–11–00 Fig 401 Config 2 55–11–00 Fig 402 Config 2 55–11–00 Fig 403 Config 2 55–11–00 Fig 404 Config 2 55–11–00 Fig 405 Config 2 55–11–00 Fig 406 Config 2 55–11–00 Fig 407 Config 2 55–11–00 Fig 408 Config 2 55–11–00 Fig 409 Config 2 INTRODUCTION

R


RUDDER, ELEVATOR AND TABS — REPAIR H1 AND REPAIR H2 — DENT ON SANDWICH STRUCTURE

RUDDER, ELEVATOR AND TABS — REPAIR K — NON PERFORATING DAMAGE RUDDER, ELEVATOR AND TABS — REPAIR L1 AND REPAIR L2 — NON PERFORATING DAMAGE OR DELAMINATION

HOT BOND REPAIR FOR NONPERFORATING DAMAGE ON THE SKIN AT SPAR CAP

METAL PATCH REPAIR FOR PERFORATING DAMAGE ON FRONT SPAR CAP — FIRST REPAIR SOLUTION METAL PATCH REPAIR FOR PERFORATING DAMAGE ON FRONT SPAR CAP — SECOND REPAIR SOLUTION

(Refer to Repair 551100-300-807-A01)

METAL PATCH REPAIR FOR PERFORATING DAMAGE ON THE SKIN AT SPAR CAP

(Refer to Repair 551100-300-808-A01)

METAL PATCH REPAIR FOR FRONT AND REAR SPAR WEBS CUT OUT

(Refer to Repair 551100-300-809-A01)

REPAIR SCHEME FOR NONPERFORATING DAMAGE ON THE SKIN BETWEEN TWO SPARS

(Refer to Repair 551100-300-810-A01)

HOT BOND REPAIR FOR NONPERFORATING DAMAGE ON THE SKIN BETWEEN TWO SPARS Page 31

Oct 01/14


Before Conversion 55–11–00 Fig 410 Config 2 55–11–40 Fig 401 Config 2 55–12–20 Fig 401 55–20–00 Fig 401 55–31–00 Fig 401 55–31–10 Fig 401 Config 2 55–31–30 Fig 401 Config 2 55–31–30 Fig 403 Config 2 55–31–30 Fig 404 Config 2 55–31–30 Fig 405 Config 2 55–31–30 Fig 406 Config 2 55–31–30 Fig 402 Config 2 55–31–30 Fig 407 Config 2 55–34–20 Fig 401X 55–40–00 Fig 401 55–41–00 Fig 403

After Conversion


(Refer to Repair 551100-300-811-A01)

METAL PATCH REPAIR FOR NON-PERFORATING DAMAGE ON THE SKIN AT SPAR CAP

(Refer to Repair 551140-300-801-A01)

REAR SPAR UPPER GROUNDING STRIP CORROSION REPAIR


HORIZONTAL STABILIZER LEADING EDGE - RIB CRACK REPAIR (LH/RH) RUDDER, ELEVATOR AND TABS COMPOSITE PARTS — REPAIRS

(Refer to Repair 553110-300-801-A01)

REAR SPAR GROUNDING STRIP CORROSION REPAIR

(Refer to Repair 553130-300-805-A01)

REPAIR FOR LIGHT DAMAGES BY RESIN FILLING

(Refer to Repair 553130-300-801-A01)

METAL PATCH REPAIR FOR NON-PERFORATING DAMAGE ON SKIN BETWEEN TWO STRINGERS


VERTICAL STABILIZER SPAR BOX

HOT BOND REPAIR FOR NONPERFORATING DAMAGE ON THE SKIN BETWEEN TWO STRINGERS METAL PATCH REPAIR FOR PERFORATING DAMAGE ON SKIN BETWEEN TWO STRINGERS

(Refer to Repair 553130-300-804-A01)

METAL PATCH REPAIR FOR PERFORATING DAMAGE AT SKIN/STRINGERS LOCATION

(Refer to Repair 553130-300-806-A01)

REPAIR FOR LIGHT DAMAGES BY RESIN FILLING AND EXTRA PLIES

(Refer to Repair 553130-300-807-A01)

METAL PATCH REPAIR FOR FRONT AND REAR SPAR WEBS CUT OUT


TEMPORARY REPAIR OF A SMALL CRACK ON FIN TIP RIB RUDDER, ELEVATOR AND TABS COMPOSITE PARTS — REPAIRS RUDDER SKIN REPAIR AT TAB COUNTERBALANCE ARM CUT — OUT

CHAPTER 56

INTRODUCTION

R

Page 32

Oct 01/14



Table 14: ALLOWABLE DAMAGE After Conversion (Refer to Damages 561000-200-801-A01) (Refer to Damages 562100-200-801-A01)

Title After Conversion FLIGHT COMPARTMENT CABIN WINDOW - ALLOWABLE DAMAGES

Table 15: REPAIR

Before Conversion

After Conversion


56–00–00 Fig 401

(Refer to Repair 560000-300-801-A01)

WINDOWS GENERAL COCKPIT WINDSHIELD AND CABIN WINDOWS REPAIR

56–10–00 Fig 401

(Refer to Repair 561000-300-801-A01)

56–10–00 Fig 402

(Refer to Repair 561000-300-802-A01)

56–10–00 Fig 403

(Refer to Repair 561000-300-803-A01)

56–10–00 Fig 404

(Refer to Repair 561000-300-804-A01)

SPS - MAIN WINDSHIELDS (SPSATR42– 1–1–1 OR SPSATR42– 2–1–1 OR SPSATR42–1–2–2 OR SPSATR42–2– 2–2) ERODED AND/ OR DEBONDED WEATHER SEAL REPAIR

PPG - MAIN WINDSHIELDS (NP-158801– 3/4) ERODED AND/ OR DEBONDED MOISTURE SEAL REPAIR PPG - MAIN WINDSHIELDS (NP-158801– 1/2) ERODED AND/ OR DEBONDED MOISTURE SEAL REPAIR PPG - FOWARD SIDE WINDOWS (NP-158862–3/4) ERODED AND/OR DEBONDED MOISTURE SEAL REPAIR

CHAPTER 57


57–12–10 Fig 301


57–12–10 Fig 302 57–12–10 Table 301

FRONT SPAR UPPER/LOWER CHORDS ALLOWABLE DAMAGES ON VERTICAL AND HORIZONTAL FLANGES


FRONT SPAR TOP FLANGE ALLOWABLE DAMAGES ON STRIP SLAT

INTRODUCTION

R

Table 16: ALLOWABLE DAMAGE


After Conversion

Title After Conversion SPAR EXTRUSION SPAR WEB

Page 33

Oct 01/14


Before Conversion

After Conversion


57–12–20 Fig 301


REAR SPAR UPPER/LOWER CHORDS ALLOWABLE DAMAGES ON VERTICAL AND HORIZONTAL FLANGES

57–13–00 Fig 301 57–14–10 Fig 301


57–14–12 Fig 301


57–22–00 Fig 301 57–22–00 Fig 302 57–23–00 Fig 301 57–24–00 Fig 301 57–24–10 Fig 301 57–31–10 Fig 301 57–40–00 Fig 301 57–52–10 Fig 301 Config 1 and Config 2

(Refer to Damages 572200-200-801-A01) (Refer to Damages 572200-200-802-A01) (Refer to Damages 572300-200-801-A01) (Refer to Damages 572400-200-801-A01) (Refer to Damages 572410-200-801-A01) (Refer to Damages 573110-200-801-A01) (Refer to Damages 574000-200-801-A01)

ALLOWABLE DAMAGES ON SHEET METAL RIBS (WEB AND RIB FLANGES) SKIN AND STIFFENERS - FUEL OUTFLOW DEFLECTOR ANGLE UPPER SURFACE SKINS — REMOVABLE AND FIXED PANELS


INBOARD FLAP STRUCTURE DEFINITION OF ZONES


INBOARD FLAP STRUCTURE SANDWICH CONSTRUCTION ZONE (FLAKING IMPACT)


INBOARD FLAP STRUCTURE MONOLITH CONSTRUCTION ZONES 5 AND 6 (FLAKING IMPACT)

57–12–20 Fig 302

57–52–10 Fig 302 Config 1 and Config 2 57–52–10 Fig 303 Config 1 and Config 2

INTRODUCTION

R

REAR SPAR TOP FLANGE ALLOWABLE DAMAGES ON STRIP SLAT REAR SPAR STRUCTURAL DEFECT/DAMAGE REPORT ALLOWABLE DAMAGES ON SHEET METAL RIBS (WEB AND RIB FLANGES) UPPER SURFACE SKIN REMOVABLE PANELS - - ALLOWABLE BLENDING LIMITS OF HOUSING SURFACE OF THE ACCESS DOOR SPAR EXTRUSION SPAR WEB

WING TIP LIGHT TRANSPARENT COVER COMPOSITE LEADING EDGE

Page 34

Oct 01/14


Before Conversion 57–52–10 Fig 304 Config 1 and Config 2 57–52–10 Fig 305 Config 1 and Config 2 57–52–10 Fig 306 Config 1 and Config 2 57–52–10 Fig 307 Config 1 and Config 2 57–52–10 Fig 308 Config 1 and Config 2 57–52–10 Fig 309 Config 1 and Config 2

57–52–10 Table 301 Config 1 and Config 2 57–52–10 Fig 310 Config 1 and Config 2 57–52–20 Fig 301 Config 1 57–52–20 Fig 301 Config 2 INTRODUCTION

R

After Conversion



INBOARD FLAP STRUCTURE SANDWICH CONSTRUCTION ZONE (SCORES, SCRATCHES)


INBOARD FLAP STRUCTURE MONOLITH CONSTRUCTION ZONES 5 AND 6 (SCORES, SCRATCHES)


INBOARD FLAP STRUCTURE SANDWICH CONSTRUCTION ZONE (CRUSHING)


INBOARD FLAP STRUCTURE (DELAMINATION)


INBOARD FLAP STRUCTURE (SEPARATION - SKIN/CORE)


INBOARD FLAP STRUCTURE (CHIPPING - SKIN/CORE)


INBOARD FLAP STRUCTURE SUMMARY


INBOARD FLAP STRUCTURE PICK-UP FITTINGS AND FITTINGS AT RIB 5


CAM GUIDE (WEAR)


CAM GUIDE (WEAR)

Page 35

Oct 01/14



After Conversion



CORROSION ON FLAP CAM GUIDES

57–52–20 Fig 302 Config 2



57–53–10 Fig 301


57–53–10 Fig 302


57–53–10 Fig 304 57–53–10 Fig 306 57–53–10 Fig 307 57–53–10 Fig 308

(Refer to Damages 575310-200-803-A01) (Refer to Damages 575310-200-804-A01) (Refer to Damages 575310-200-805-A01) (Refer to Damages 575310-200-806-A01) (Refer to Damages 575310-200-807-A01) (Refer to Damages 575310-200-808-A01) (Refer to Damages 575310-200-809-A01)

57–53–10 Fig 309 57–53–10 Fig 310 57–53–20 Fig 301 CONFIG 1 57–53–20 Fig 301 CONFIG 2 57–53–20 Fig 302 CONFIG 1 57–53–20 Fig 302 CONFIG 2 57–61–10 Fig. 301 Config 1 57–61–10 Fig. 301 Config 2 INTRODUCTION

R

OUTBOARD FLAP STRUCTURE - DEFINITION OF ZONES OUTBOARD FLAP STRUCTURE - SANDWICH CONSTRUCTION ZONE (FLAKING IMPACT)

OUTBOARD FLAP STRUCTURE SANDWICH CONSTRUCTION ZONE (SCORES) OUTBOARD FLAP STRUCTURE SANDWICH CONSTRUCTION ZONE (CRUSHING) OUTBOARD FLAP STRUCTURE (DELAMINATION) OUTBOARD FLAP STRUCTURE (SEPARATION - SKIN/CORE) OUTBOARD FLAP STRUCTURE (CHIPPING - SKIN/CORE) OUTBOARD FLAP STRUCTURE SUMMARY OUTBOARD FLAP STRUCTURE FITTINGS AT RIB 14 AND RIB 18


CAM GUIDE (WEAR)


CAM GUIDE (WEAR)






COMPLETE STRUCTURE — EVALUATION OF REPAIRABILITY COMPLETE STRUCTURE AILERON BOX - DEFINITION OF ZONES


COMPLETE STRUCTURE — EVALUATION OF REPAIRABILITY

Page 36

Oct 01/14


Before Conversion 57–61–10 Fig. 302 Config 1 57–61–10 Fig. 303 Config 1 57–61–10 Fig. 304 Config 1 57–61–10 Fig. 305 Config 1 57–61–10 Fig. 306 Config 1 57–61–10 Fig. 307 Config 1 57–61–10 Fig. 308 Config 1 57–61–10 Fig. 309 Config 1 57–61–10 Fig. 310 Config 1 57–61–10 Fig. 311 Config 1 57–61–10 Fig. 312 Config 1 57–61–10 Fig. 313 Config 1 57–61–10 Fig. 314 Config 1 57–61–10 Fig. 302 Config 2 57–61–10 Fig. 308 Config 2 INTRODUCTION

R

After Conversion



COMPLETE STRUCTURE TAB — DEFINITION OF ZONES


COMPLETE STRUCTURE HORN - DEFINITION OF ZONES


COMPLETE STRUCTURE AILERON BOX (SCORE/SCRATCH)


COMPLETE STRUCTURE AILERON BOX (PERFORATING IMPACT)


COMPLETE STRUCTURE AILERON BOX (FLAKING/ PERFORATING IMPACT OR NOT)


COMPLETE STRUCTURE AILERON BOX (DELAMINATION, SEPARATION)


COMPLETE STRUCTURE TAB (SCORE/SCRATCH)


COMPLETE STRUCTURE TAB (FLAKING/ PERFORATING IMPACT OR NOT)


COMPLETE STRUCTURE TAB (DELAMINATION, SEPARATION)


COMPLETE STRUCTURE HORN (SCORE, SCRATCH)


COMPLETE STRUCTURE HORN (FLAKING/ PERFORATING IMPACT OR NOT)


COMPLETE STRUCTURE HORN (DELAMINATION, SEPARATION)


COMPLETE STRUCTURE HORN (CRUSHING)


COMPLETE STRUCTURE SPRING TAB SKIN PANEL (DELAMINATION)


COMPLETE STRUCTURE SPRING TAB SKIN PANEL (SCORE, SCRATCH)

Page 37

Oct 01/14


Before Conversion 57–61–10 Fig. 309 Config 2

After Conversion



COMPLETE STRUCTURE SPRING TAB TRAILING EDGE (CRUSHING)

Table 17: REPAIR

Before Conversion

After Conversion


57–12–10 Fig 401X

(Refer to Repair 571210-300-801-A01)

FRONT SPAR - TEMPORARY REPAIR SCHEME FOR CRACK AND CORROSION ON LOWER AND UPPER SPAR FLANGES

57–12–10 Fig 401

(Refer to Repair 571210-300-802-A01)

57–12–10 Fig 402


57–12–10 Fig 403


57–12–10 Fig 404

(Refer to Repair 571210-300-805-A01)

57–12–20 Fig 401X

(Refer to Repair 571220-300-801-A01)

57–12–20 Fig 401

(Refer to Repair 571220-300-802-A01)

57–12–20 Fig 402

(Refer to Repair 571220-300-803-A01)

57–13–10 Fig 401

(Refer to Repair 571310-300-801-A01)

57–13–10 Fig 402

(Refer to Repair 571310-300-802-A01)

INTRODUCTION

R

FRONT SPAR - REPAIR SCHEME FOR CRACK AND CORROSION ON LOWER AND UPPER SPAR FLANGES FRONT SPAR REPAIR SCHEME FOR CHAFING ON UPPER FRONT SPAR STRIP SLAT

FRONT SPAR — LOWER STRIP REPAIR BETWEEN THE RIBS 10 AND 11 (LH SIDE) — REPAIR A FRONT SPAR — LOWER STRIP REPAIR BETWEEN THE RIBS 11 AND 12 (LH SIDE) — REPAIR B FRONT SPAR — LOWER STRIP REPAIR BETWEEN THE RIBS 10 AND 11 (RH SIDE) — REPAIR C FRONT SPAR — LOWER STRIP REPAIR BETWEEN THE RIBS 11 AND 12 (RH SIDE) — REPAIR D

FRONT SPAR LOWER STRIP BLEND OUT (LH/RH) BETWEEN THE RIBS 10/11 AND RIBS 11/12

REAR SPAR TEMPORARY REPAIR SCHEME FOR CRACK AND CORROSION ON LOWER AND UPPER SPAR FLANGES REAR SPAR REPAIR SCHEME FOR CRACK AND CORROSION ON LOWER AND UPPER SPAR FLANGES

REPAIR SCHEME FOR CHAFING ON UPPER REAR SPAR STRIP SLAT RIBS STRUCTURE — REPAIR SCHEME FOR CRACK ON WING RIB FLANGE (DAMAGE BETWEEN STIFF. 3 THRU 5) RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB FLANGE (DAMAGE BETWEEN STIFF. 4 THRU 5) Page 38

Oct 01/14


Before Conversion

After Conversion


57–13–10 Fig 403

(Refer to Repair 571310-300-803-A01)

57–13–10 Fig 404

(Refer to Repair 571310-300-804-A01)

RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB FLANGE (DAMAGE BETWEEN STIFF. 6 THRU 8)

57–14–10 Fig 401

(Refer to Repair 571410-300-801-A01)

57–14–10 Fig 402

(Refer to Repair 571410-300-802-A01)

57–14–10 Fig 403

(Refer to Repair 571410-300-803-A01)

57–14–10 Fig 404

(Refer to Repair 571410-300-804-A01)

57–14–12 Fig 401

(Refer to Repair 571412-300-801-A01)

57–14–20 Fig 401

(Refer to Repair 571420-300-801-A01)

57–14–20 Fig 402

(Refer to Repair 571420-300-802-A01)

57–22–00 Fig 401

(Refer to Repair 572200-300-801-A01)

57–23–10 Fig 401 57–23–10 Fig 402 57–23–10 Fig 403 57–23–10 Fig 404


57–24–00 Fig 401X

(Refer to Repair 572400-300-801-A01)

57–24–00 Fig 401

(Refer to Repair 572400-300-802-A01)

INTRODUCTION

R

RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB WEB UPPER SURFACE SKIN — REPAIR SCHEME FOR CORROSION ON SKIN PANELS

UPPER SURFACE SKIN — REPAIR SCHEME FOR CORROSION ON REMOVABLE PANELS BETWEEN RIB 0 AND RIB 8 REPAIR SCHEME FOR CORROSION ON REMOVABLE PANELS BETWEEN RIB 8 AND RIB 13 UPPER SURFACE SKIN — REPAIR SCHEME FOR CRACK ON SKIN PANELS STIFFENERS

REMOVABLE PANELS REPAIR SCHEME FOR HOUSING SURFACE ON THE ACCESS DOORS

LOWER SURFACE SKIN REPAIR SCHEME FOR CRACK ON LOWER SURFACE PANEL STIFFENER DAMAGE (CRACK) CUTOUT DEPTH 15 mm (0.591 in.) MAX. LOWER SURFACE SKIN REPAIR SCHEME FOR CRACK ON LOWER SURFACE PANEL STIFFENER DAMAGE (CRACK) CUTOUT DEPTH 8mm (0.315 in.) MAX. SPARS (FRONT AND REAR) — REPAIR SCHEME FOR SPAR WEB FLANGE RIB23 TO RIB30

RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB FLANGE RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB FLANGE RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB FLANGE RIBS STRUCTURE - REPAIR SCHEME FOR CRACK ON WING RIB WEB SKINS AND STIFFENERS TEMPORARY REPAIR FOR FUEL OUTFLOW DEFLECTOR ANGLE

SKINS AND STIFFENERS - REPAIR FOR FUEL OUTFLOW DEFLECTOR ANGLE

Page 39

Oct 01/14


Before Conversion

After Conversion


57–24–11 Fig 401

(Refer to Repair 572411-300-801-A01)

UPPER FIXED PANELS RIB 13 TO RIB 23 - REPAIR SCHEME FOR CRACK ON STIFFENERS BETWEEN RIB 14 TO RIB 18 (CRACK ON TWO SIDES OF STIFFENER)

57–24–11 Fig 402

(Refer to Repair 572411-300-802-A01)

57–24–20 Fig 401

(Refer to Repair 572420-300-801-A01)

57–24–20 Fig 401X

(Refer to Repair 572420-300-802-A01)

57–24–20 Fig 402

(Refer to Repair 572420-300-803-A01)

57–24–20 Fig 402X

(Refer to Repair 572420-300-804-A01)

57–24–20 Fig 403

(Refer to Repair 572420-300-805-A01)

57–24–20 Fig 404

(Refer to Repair 572420-300-806-A01)

57–24–20 Fig 405

(Refer to Repair 572420-300-807-A01)

57–40–00 Fig. 402 57–40–00 Fig. 403 57–40–00 Fig. 404

(Refer to Repair 574000-300-801-A01) (Refer to Repair 574000-300-802-A01) (Refer to Repair 574000-300-803-A01) (Refer to Repair 574000-300-804-A01) (Refer to Repair 574000-300-805-A01)

57–40–00 Fig. 405

(Refer to Repair 574000-300-806-A01)

57–40–00 Fig. 401

INTRODUCTION

R

UPPER FIXED PANELS RIB 13 TO RIB 23 — REPAIR SCHEME FOR CRACK ON STIFFENERS BETWEEN RIB 18 TO RIB 21 (CRACK ON ONE SIDE AT STIFFENER)

LOWER SURFACE SKIN - REPAIR SCHEME FOR CRACK ON SKIN PANEL AT RIB/STIFFENER INTERSECTION LOWER SURFACE SKIN - TEMPORARY REPAIR SCHEME FOR CRACK ON SKIN PANEL AT RIB/ STIFFENER INTERSECTION LOWER SURFACE SKIN REPAIR SCHEME FOR CRACK ON SKIN PANEL RECESS

LOWER SURFACE SKIN TEMPORARY REPAIR SCHEME FOR CRACK ON SKIN PANEL RECESS

LOWER SURFACE SKIN - REPAIR SCHEME FOR CRACK ON STIFFENERS LOWER SURFACE SKIN REPAIR SCHEME FOR CRACK ON SKIN PANEL AND STIFFENER LOWER SURFACE SKIN - REPAIR SCHEME FOR CRACK ON SKIN PANEL AND STIFFENER AT RIB/ STIFFENER INTERSECTION LEADING EDGES - REPAIRS LEADING EDGES - PLIES ON KEVLAR FABRIC IDENTIFICATION LEADING EDGES - REPAIR FOR PICK-UP (SCHEME A) LEADING EDGES - REPAIR FOR PUNCHING, NOTCH (SCHEME B) LEADING EDGES - REPAIR FOR SEPARATION (SCHEME C) LEADING EDGES - REPAIR FOR INDENTATION ON SANDWICH STRUCTURE (SCHEME D) Page 40

Oct 01/14


Before Conversion 57–40–00 Fig. 406 57–40–00 Fig. 407 57–40–00 Fig. 408

After Conversion



57–43–10 Fig. 401

(Refer to Repair 574310-300-801-A01)

LEADING EDGE - REPAIR FOR PICK UP (SCHEME E) LEADING EDGES - REPAIR FOR DELAMINATION (SCHEME F) LEADING EDGES - REPAIR FOR PUNCHING, NOTCH (SCHEME H) COMPLETE STRUCTURE - REPAIR SCHEME FOR DELAMINATION (BETWEEN RIB 20 AND RIB 21)

57–43–10 Fig. 402

(Refer to Repair 574310-300-802-A01)

57–43–10 Fig. 403

(Refer to Repair 574310-300-803-A01)

57–52–10 Fig. 401 Config 1 and Config 2 57–52–10 Fig. 402 Config 1 and Config 2 57–52–10 Fig. 403 Config 1 and Config 2 57–52–10 Fig. 404 Config 1 and Config 2 57–52–10 Fig.405 Config 1 and Config 2 57–52–10 Fig. 406 Config 1 and Config 2 INTRODUCTION

R

(Refer to Repair 575210-300-801-A01)

COMPLETE STRUCTURE - REPAIR SCHEME FOR DELAMINATION (BETWEEN RIB 21 AND RIB 22) COMPLETE STRUCTURE REPAIR SCHEME FOR CORROSION (BETWEEN RIB 21 AND RIB 30) INBOARD FLAP STRUCTURE - REPAIR

(Refer to Repair 575210-300-802-A01)

INBOARD FLAP STRUCTURE - TEMPORARY REPAIR FOR FLAKING, IMPACT ON SANDWICH CONSTRUCTION (SCHEME AX)

(Refer to Repair 575210-300-803-A01)

INBOARD FLAP STRUCTURE REPAIR FOR FLAKING, IMPACT ON SANDWICH CONSTRUCTION (SCHEME A)

(Refer to Repair 575210-300-804-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR FLAKING, PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575210-300-805-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR SCORES, SCRATCHES ON SANDWICH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575210-300-806-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575210-300-807-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR SCORES, SCRATCHES ON MONOLITH CONSTRUCTION (SCHEME B1X) Page 41

Oct 01/14


Before Conversion 57–52–10 Fig. 407 and Config 2 Config 1 57–52–10 Fig. 408 Config 1 and Config 2 57–52–10 Fig. 409 Config 1 and Config 2 57–52–10 Fig. 410 Config 1 and Config 2 57–52–10 Fig. 411 Config 1 and Config 2 57–52–10 Fig. 412 Config 1 and Config 2 57–52–10 Fig. 413 Config 1 and Config 2 57–52–10 Fig. 414 Config 1 and Config 2 57–52–10 Fig. 415 Config 1 and Config 2

INTRODUCTION

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After Conversion


(Refer to Repair 575210-300-808-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR FLAKING ON TRAILING EDGE ON SANDWICH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575210-300-809-A01)

INBOARD FLAP STRUCTURE - REPAIR FOR FLAKING, PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575210-300-810-A01)

INBOARD FLAP STRUCTURE REPAIR FOR SCRATCHES, SCORES ON SANDWICH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575210-300-811-A01)

INBOARD FLAP STRUCTURE - REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575210-300-812-A01)

INBOARD FLAP STRUCTURE REPAIR FOR SCRATCHES, SCORES ON MONOLITH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575210-300-813-A01)

INBOARD FLAP STRUCTURE REPAIR FOR FLAKING, IMPACT ON TRAILING EDGES (SCHEME B1)

(Refer to Repair 575210-300-814-A01)

INBOARD FLAP STRUCTURE - REPAIR FOR PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B2)

(Refer to Repair 575210-300-815-A01)

INBOARD FLAP STRUCTURE - REPAIR FOR NON-PERFORATING IMPACT OF 4 PLIES ZONE (SCHEME B3)

(Refer to Repair 575210-300-816-A01)


Page 42

Oct 01/14


Before Conversion 57–52–10 Fig. 416 Config 1 and Config 2 57–52–10 Fig. 417 Config 1 and Config 2 57–52–10 Fig. 418 Config 1 and Config 2 57–52–10 Fig. 419 Config 1 and Config 2 57–52–10 Fig. 420 Config 1 and Config 2 57–52–10 Fig. 421 Config 1 and Config 2 57–52–10 Fig. 422 Config 1 and Config 2 57–52–10 Fig. 423 Config 1 and Config 2 57–52–10 Fig. 424 Config 1 and Config 2

INTRODUCTION

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After Conversion


(Refer to Repair 575210-300-817-A01)


(Refer to Repair 575210-300-818-A01)

INBOARD FLAP STRUCTURE REPAIR FOR IMPACT HOLE ON 4 PLIES ZONE (SCHEME B4)

(Refer to Repair 575210-300-819-A01)


(Refer to Repair 575210-300-820-A01)


(Refer to Repair 575210-300-821-A01)

INBOARD FLAP STRUCTURE - REPAIR FOR PERFORATING IMPACT ON SANDWICH CONSTRUCTION SCHEME B5

(Refer to Repair 575210-300-822-A01)


(Refer to Repair 575210-300-823-A01)

INBOARD FLAP STRUCTURE REPAIR FOR PERFORATING IMPACT ON 6 PLIES ZONE (SCHEME B6)

(Refer to Repair 575210-300-824-A01)


(Refer to Repair 575210-300-825-A01)

INBOARD FLAP STRUCTURE TEMPORARY REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B7X)

Page 43

Oct 01/14



INTRODUCTION

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After Conversion


(Refer to Repair 575210-300-826-A01)

INBOARD FLAP STRUCTURE REPAIR FOR TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B7)

(Refer to Repair 575210-300-827-A01)

INBOARD FLAP STRUCTURE REPAIR FOR TRAVERSING IMPACT ON TRAILING EDGE (SCHEME B8)

(Refer to Repair 575210-300-828-A01)

INBOARD FLAP STRUCTURE — REPAIR FOR TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B9)

(Refer to Repair 575210-300-829-A01)

INBOARD FLAP STRUCTURE REPAIR FOR TRAVERSING IMPACT ON TRAILING EDGE (SCHEME C)

(Refer to Repair 575210-300-830-A01)

INBOARD FLAP STRUCTURE REPAIR FOR DELAMINATION (SCHEME E1)

(Refer to Repair 575210-300-831-A01)

INBOARD FLAP STRUCTURE REPAIR FOR DELAMINATION (SCHEME E2)

(Refer to Repair 575210-300-832-A01)

INBOARD FLAP STRUCTURE REPAIR FOR SKIN/HONEYCOMB SEPARATION (SCHEME F1)

(Refer to Repair 575210-300-833-A01)

INBOARD FLAP STRUCTURE REPAIR FOR DAMAGED TRAILING EDGE (IMPACT)

(Refer to Repair 575210-300-834-A01)

INBOARD FLAP STRUCTURE REPAIR OF FLAP RIB ATTACH FITTINGS

Page 44

Oct 01/14


Before Conversion 57–52–20 Fig. 401 Config 1 57–53–10 Fig. 401 Config 1 and Config 2 57–53–10 Fig. 402 Config 1 and Config 2 57–53–10 Fig. 403 Config 1 and Config 2 57–53–10 Fig. 404 Config 1 and Config 2 57–53–10 Fig. 405 Config 1 and Config 2 57–53–10 Fig. 406 Config 1 and Config 2 57–53–10 Fig. 407 Config 1 and Config 2 57–53–10 Fig. 408 Config 1 and Config 2

INTRODUCTION

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After Conversion


(Refer to Repair 575220-300-801-A01)

REPAIR SCHEME ON CAM GUIDE

(Refer to Repair 575310-300-801-A01)

TEMPORARY REPAIR FOR FLAKING, IMPACT ON SANDWICH CONSTRUCTION (SCHEME AX)

(Refer to Repair 575310-300-802-A01)

REPAIR FOR FLAKING, IMPACT ON SANDWICH CONSTRUCTION (SCHEME A)

(Refer to Repair 575310-300-803-A01)

TEMPORARY REPAIR FOR FLAKING, PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575310-300-804-A01)

TEMPORARY REPAIR FOR SCORES, SCRATCHES ON SANDWICH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575310-300-805-A01)

TEMPORARY REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575310-300-806-A01)

TEMPORARY REPAIR FOR SCORES, SCRATCHES ON MONOLITH CONSTRUCTION (SCHEME B1X)

(Refer to Repair 575310-300-807-A01)

TEMPORARY REPAIR FOR FLAKING ON TRAILING EDGE (SCHEME B1X)

(Refer to Repair 575310-300-808-A01)

REPAIR FOR FLAKING, PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B1)

Page 45

Oct 01/14



INTRODUCTION

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After Conversion


(Refer to Repair 575310-300-809-A01)

REPAIR FOR SCRATCHES, SCORES ON SANDWICH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575310-300-810-A01)

REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575310-300-811-A01)

REPAIR FOR SCRATCHES, SCORES ON MONOLITH CONSTRUCTION (SCHEME B1)

(Refer to Repair 575310-300-812-A01)

REPAIR FOR FLAKING, IMPACT ON TRAILING EDGES (SCHEME B1)

(Refer to Repair 575310-300-813-A01)

REPAIR FOR PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B2)

(Refer to Repair 575310-300-814-A01)

REPAIR FOR NON-PERFORATING IMPACT ON 4 PLIES ZONE (SCHEME B3)

(Refer to Repair 575310-300-815-A01)


(Refer to Repair 575310-300-816-A01)


(Refer to Repair 575310-300-817-A01)

REPAIR FOR IMPACT HOLE ON 4 PLIES ZONE (SCHEME B4)

Page 46

Oct 01/14



INTRODUCTION

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After Conversion


(Refer to Repair 575310-300-818-A01)


(Refer to Repair 575310-300-819-A01)


(Refer to Repair 575310-300-820-A01)

REPAIR FOR PERFORATING IMPACT ON SANDWICH CONSTRUCTION (SCHEME B5)

(Refer to Repair 575310-300-821-A01)


(Refer to Repair 575310-300-822-A01)

REPAIR FOR PERFORATING IMPACT ON 6 PLIES ZONE (SCHEME B6)

(Refer to Repair 575310-300-823-A01)


(Refer to Repair 575310-300-824-A01)

TEMPORARY REPAIR FOR FLAKING, TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B7X)

(Refer to Repair 575310-300-825-A01)

REPAIR FOR TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B7)

(Refer to Repair 575310-300-826-A01)

REPAIR FOR TRAVERSING IMPACT ON TRAILING EDGE (SCHEME B8)

Page 47

Oct 01/14


Before Conversion 57–53–10 Fig. 427 Config 1 and Config 2

After Conversion


(Refer to Repair 575310-300-827-A01)

REPAIR FOR TRAVERSING IMPACT ON MONOLITH CONSTRUCTION (SCHEME B9)

(Refer to Repair 575310-300-828-A01)

REPAIR FOR TRAVERSING IMPACT ON TRAILING EDGE (SCHEME C)

(Refer to Repair 575310-300-829-A01)

REPAIR FOR DELAMINATION (SCHEME E1)

(Refer to Repair 575310-300-830-A01)

REPAIR FOR DELAMINATION (SCHEME E2)

(Refer to Repair 575310-300-831-A01)

REPAIR FOR SKIN/HONEYCOMB SEPARATION (SCHEME F1)

(Refer to Repair 575310-300-832-A01)

OUTBOARD FLAP STRUCTURE REPAIR FOR TEAR ON LOWER PANEL OUTER SKIN (RIB20 AND TRAILING EDGE ANGLE)

(Refer to Repair 575310-300-833-A01)

REPAIR OF FLAPS RIB ATTACH FITTINGS

57–53–20 Fig 401

(Refer to Repair 575320-300-801-A01)

REPAIR SCHEME ON CAM GUIDE

57–54–10 Fig. 401

(Refer to Repair 575410-300-801-A01)

57–54–20 Fig. 401

(Refer to Repair 575420-300-801-A01)

57–53–10 Fig. 428 Config 1 and Config 2 57–53–10 Fig. 429 Config 1 and Config 2 57–53–10 Fig. 430 Config 1 and Config 2 57–53–10 Fig. 43 Config 1 and Config 2 57–53–10 Fig 432 Config 1 and Config 2 57–53–10 Fig 433 Config 1 and Config 2

INTRODUCTION

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UPPER SURFACE TRAILING EDGE REPAIR SCHEME FOR DAMAGED EDGE AT LH RIB 13 LOWER SURFACE TRAILING EDGE REPAIR SCHEME FOR DAMAGED OUTER FACE

Page 48

Oct 01/14


Before Conversion 57–61–10 Fig. 401 config 1 57–61–10 Fig. 401 config 2 57–61–10 Fig. 402 config 1 and Config 2 57–61–10 Fig. 403 config 1 and Config 2

57–61–10 Fig. 404, 405, 406 and 407 config 1 and Config 2 57–61–10 Fig. 408 config 1 and Config 2 57–61–10 Fig. 409 config 1 and Config 2 57–61–10 Fig. 410 config 1 57–61–10 Fig. 411 config 1 57–61–10 Fig. 412 config 1

INTRODUCTION

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After Conversion (Refer to Repair 576110-300-801-A01) (Refer to Repair 576110-300-802-A01)

Title After Conversion GENERAL INSTRUCTIONS RENEWAL OF LIGHTNING PROTECTION

(Refer to Repair 576110-300-801-B01)

GENERAL INSTRUCTIONS

(Refer to Repair 576110-300-803-A01)

TEMPORARY REPAIR FOR IMPACT ON SANDWICH STRUCTURE (SCHEME AX)

(Refer to Repair 576110-300-804-A01)

REPAIR SCHEME A

(Refer to Repair 576110-300-805-A01)

REPAIR SCHEME ON AILERON BOX (SCHEME B1)

(Refer to Repair 576110-300-806-A01)


(Refer to Repair 576110-300-807-A01)


(Refer to Repair 576110-300-812-A01)

REPAIR SCHEME ON TAB (SCHEME C1)

(Refer to Repair 576110-300-813-A01)

REPAIR SCHEME FOR AILERON AND TAB (SCHEME C2)

(Refer to Repair 576110-300-814-A01)


Page 49

Oct 01/14


Before Conversion 57–61–10 Fig. 413 and 414 config 1 57–61–10 Fig. 415 config 1

57–61–10 Fig. 416, 417, 418 and 419 Config 2 57–61–10 Fig. 416 and 417 config 1 57–61–10 Fig. 418 config 1 57–61–10 Fig. 419 config 1 57–61–10 Fig. 420 config 1 and Config 2 57–61–10 Fig. 421 config 1 57–61–10 Fig. 422 config 1 and Config 2 57–61–10 Fig. 423 config 1 and Config 2 57–61–10 Fig. 424 config 1 and Config 2

INTRODUCTION

R

After Conversion


(Refer to Repair 576110-300-816-A01)

REPAIR SCHEME ON AILERON BOX (SCHEMES C4)

(Refer to Repair 576110-300-817-A01)


(Refer to Repair 576110-300-817-B01)

REPAIR SCHEME ON AILERON BOX (SCHEMES D)

(Refer to Repair 576110-300-819-A01)

REPAIR SCHEME ON AILERON BOX (SCHEME D1, D2, D3)

(Refer to Repair 576110-300-820-A01)

REPAIR SCHEME ON AILERON BOX (SCHEME D4)

(Refer to Repair 576110-300-821-A01)

REPAIR SCHEME ON AILERON BOX (SCHEME D5)

(Refer to Repair 576110-300-822-A01)

REPAIR SCHEME ON HORN (SCHEME E1)

(Refer to Repair 576110-300-823-A01)

REPAIR SCHEME ON TAB (SCHEME E2)

(Refer to Repair 576110-300-824-A01)

REPAIR SCHEME ON AILERON BOX (SCHEME F)

(Refer to Repair 576110-300-825-A01)

REPAIR SCHEME ON HORN (SCHEME G1)

(Refer to Repair 576110-300-826-A01)


Page 50

Oct 01/14


Before Conversion 57–61–10 Fig. 425 config 1 and Config 2 57–61–10 Fig. 426 config 1 and Config 2 57–61–10 Fig. 427 and 428 config 1 and Config 2 57–61–10 Fig. 429 config 1 and Config 2

INTRODUCTION

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After Conversion


(Refer to Repair 576110-300-827-A01)


(Refer to Repair 576110-300-828-A01)


(Refer to Repair 576110-300-830-A01)

COMPLETE STRUCTURE - WET LAY-UP. REPAIR SCHEME ON HORN (SCHEME G5, G6)

(Refer to Repair 576110-300-831-A01)

PROCEDURE FOR REPLACEMENT OF AILERON LIGHTNING PROTECTION STRIPS

Page 51

Oct 01/14


ATA Chapter Organization FIGURE 1/SHT-000000-INT-001-001-01

INTRODUCTION

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Page 52

Oct 01/14


Assembly Identification FIGURE 2 (Sheet 1)/SHT-000000-INT-001-002-01

INTRODUCTION

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Page 53

Oct 01/14


Assembly Identification FIGURE 2 (Sheet 2)/SHT-000000-INT-001-002-02

INTRODUCTION

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Page 54

Oct 01/14


Allowable Damage FIGURE 3/SHT-000000-INT-001-006-01

INTRODUCTION

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Page 55

Oct 01/14


Section Numbering System FIGURE 4 (Sheet 1)/SHT-000000-INT-001-003-01

INTRODUCTION

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Page 56

Oct 01/14


Task Structure Element FIGURE 4 (Sheet 2)/SHT-000000-INT-001-003-02

INTRODUCTION

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Page 57

Oct 01/14


Figure Structure Element FIGURE 4 (Sheet 3)/SHT-000000-INT-001-003-03

INTRODUCTION

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Page 58

Oct 01/14


P/N Structure Element FIGURE 5/SHT-000000-INT-001-005-01 Technical Specification: The A/C manufactured part numbers has a standard structure. During the construction process, each single P/N is manufactured according to the drawing but may be not completed to allow the installation on the assy structure. Two characters (Technical Specification) specifying the delivery condition that permits the right installation of component have to be added. The two characters to manufacture the part according to the drawing and manufacturing process requirements are 00 (following Tables give the suffixes for the most used delivery condition). NOTE :

When customer demand a delivery condition different from current produced one, the lead time to get the part could be deferred.

INTRODUCTION

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Page 59

Oct 01/14


Legal/Environmental Notice FIGURE 6/SHT-000000-INT-001-004-01

INTRODUCTION

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Page 60

Oct 01/14

introduccion al SRM ATR72

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