ut procedure tech

@A330NONDESTRUCTIVE TESTING MANUAL

CHAPTER 53 - FUSELAGE

TABLE OF CONTENTSREFERENCE SUBJECT

CHAPTER 53

53-00-01 SCRIBE MARK INSPECTION ON EXTERNAL SKIN/STRAPCIRCUMFERENTIAL AND LONGITUDINAL JOINTS

53-00-01 Descriptions

53-00-01-001-A General

53-00-01-002-A Preferred Inspection

53-00-01-01 Procedures

53-00-01-220-801-A-01 Scribe Mark Inspection on External Skin/Strap Circumferential andLongitudinal Joint

53-00-01-220-802-A-01 Scribe Mark Inspection on External Skin/Strap Circumferential andLongitudinal Joints

53-00-01-250-801-A-01 Scribe Mark Inspection on External Skin/Strap Circumferential andLongitudinal Joints

53-00-02 FASTENER ROWS(ONE OR MORE) IN ALUMINUM ALLOY PANEL


53-00-02-001-A General



53-00-02-250-801-A-01 Fastener Rows (one or more) in Aluminum Alloy Panel.

53-11-08 CIRCUMFERENTIAL JOINT AT FRAME 18 BETWEEN STGR3 ANDSTGR7, BUTT JOINT AND REAR PANEL, LH


53-11-08-001-A General



53-11-08-270-801-A-01 Circumferential Joint at FR18 between STGR3 and STGR7, Butt Jointand Rear Panel, LH

53-11-09 CIRCUMFERENTIAL JOINT AT FRAME 18 BETWEEN STGR11 ANDSTGR13, BUTT JOINT AND REAR PANEL, RH


53-11-09-001-A General



53-11-09-270-801-A-01 Circumferential Joint at FR18 between STGR11 and STGR13, Butt Jointand Rear Panel, RH

53-11-25 FR.17 ATTACHMENT TO BOTTOM SKIN FROM STGR48 TO STGR51,LH/RH


53-11-25-001-A Description

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REFERENCE SUBJECT



53-11-25-250-801-A-01 FR17 Attachment to Bottom Skin from STGR48 to STGR51, LH/RH

53-11-27 NLG DRAG STRUT FITTING ATTACHMENTS TO UPPER ANDFORWARD CANTED PANEL


53-11-27-001-A General



53-11-27-250-801-A-01 NLG Drag Strut Fitting Attachments to Upper and Forward Canted Panel

53-11-29 NOSE LANDING GEAR DOOR ACTUATOR FITTING BORES ON THEINBOARD AND OUTBOARD LUGS, RH ONLY


53-11-29-001-A General



53-11-29-250-801-A-01 Nose Landing Gear (NLG) Door Actuator Fitting Bores on the Inboardand Outboard Lugs, RH Side Only

53-11-30 FUSELAGE INTERNAL STRUCTURE, FRAME 16A AT CABIN FLOORLEVEL, LH/RH


53-11-30-001-A General (BEFORE MODIFICATION 44258S12992)

53-11-30-002-A Preferred Inspection (BEFORE MODIFICATION 44258S12992)


53-11-30-270-801-A-01 Fuselage Internal Structure, Frame 16A at Cabin Floor Level, LH/RH(BEFORE MODIFICATION 44258S12992)

53-11-31 FUSELAGE INTERNAL STRUCTURE, FRAME 16A JOINT AREABETWEEN STRINGERS 28 AND 30, LH/RH


53-11-31-001-A General



53-11-31-250-801-A-01 Fuselage Internal Structure, Frame 16A Joint Area Between Stringers 28and 30, LH/RH -- Procedure A

53-11-31-250-802-A-01 Fuselage Internal Structure, Frame 16A Joint Area Between Stringers 28and 30, LH/RH -- Procedure B

53-11-34 FUSELAGE INTERNAL, STRUCTURE, BOOMERANG FRAMES 11A TO16A ATTACHMENT TO SKIN, BETWEEN


53-11-34-001-A General



53-11-34-250-801-A-01 Fuselage Internal Structure, Boomerang Frames 11A to 16A Attachmentto Skin, between Stringers 46 and 47, LH/RH

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REFERENCE SUBJECT

53-11-35 REAR LOWER CORNER OF THE COCKPIT LATERAL WINDOW FRAME,FORWARD OF FR10, EXTERNAL SURFACE, LH/RH


53-11-35-001-A General



53-11-35-250-801-A-01 Rear Lower Corner of the Cockpit Lateral Window Frame, Forward ofFR10, External Surface, LH/RH

53-11-40 LATERAL FRAME 10 AT FLOOR LEVEL ATTACHMENT, ABOVECOCKPIT FLOOR, INTERNAL STRUCTURE, LH/RH





53-11-40-250-801-A-01 Lateral Frame 10 at Floor Level Attachment, Above Cockpit Floor,Internal Structure, LH/RH (BEFORE MODIFICATION 42829S12021)

53-11-42 FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTERLINEAND UPPER LATERAL SPLICING, SPLICE


53-11-42-001-A General


53-11-42-002-C Preferred Inspection


53-11-42-250-801-A-01 Frame 10 Upper Curved Member between Crown Centerline and UpperLateral Splicing, Splice Excluded, Internal Structure, LH/RH -- ProcedureA

53-11-42-250-802-A-01 Frame 10 Upper Curved Member between Crown Centerline and UpperLateral Splicing, Splice Excluded, Internal Structure, LH/RH -- ProcedureB

53-11-44 FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FR14AND CRUCIFORM FITTING, LH/RH


53-11-44-001-A General




53-11-44-270-801-A-01 Fuselage Internal Structure, Junction Area between FR14 and CruciformFitting, LH/RH -- Procedure A

53-11-44-270-802-A-01 Fuselage Internal Structure, Junction Area between FR14 and CruciformFitting, LH/RH -- Procedure B

53-11-45 CIRCUMFERENTIAL JOINT AT FRAME 19 BETWEEN STGR45 ANDSTGR47, BUTT JOINT AND REAR PANEL, RH


53-11-45-001-A General


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REFERENCE SUBJECT


53-11-45-250-801-A-01 Circumferential Joint at Frame 19 between STGR45 and STGR47, ButtJoint and Rear Panel, RH

53-11-48 CIRCUMFERENTIAL JOINT AT FRAME 18 BETWEEN STGR30 ANDSTGR32, BUTT JOINT AND REAR PANEL, LH


53-11-48-001-A General



53-11-48-270-801-A-01 Circumferential Joint at Frame 18 between STGR30 and STGR32, ButtJoint and Rear Panel, LH

53-11-55 FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 14C, FROM STGR9TO STGR12, LH/RH


53-11-55-001-A General

53-11-60 FUSELAGE INTERNAL STRUCTURE, RADIUS OF LUGS ON UPPERCORNER OF PORTAL FRAME 15A, LH/RH


53-11-60-001-A General

53-11-62 FRAME 7 AND CROSS BEAM AT ATTACHMENT AREA


53-11-62-001-A General



53-11-62-250-801-A-01 Frame 7 and Cross Beam at Attachment Area (42 Fasteners)

53-11-63 NOSE LANDING GEAR MAIN ATTACHEMENT BEARING BORE, LH/RH


53-11-63-001-A General

53-11-64 NOSE LANDING GEAR BAY LATERAL PANELS, JUNCTION TO LOWERFRAME 17 FITTING, LH/RH


53-11-64-001-A General

53-11-65 FRAME 17 UPPER FREE FLANGE AT Y =+ /-750MM, SEAT RAILSTRUT / ATTACHMENT HOLES, LH/RH


53-11-65-001-A General



53-11-65-270-801-A-01 Frame 17 Upper Free Flange at Y=+/- 750 mm, Seat Rail StrutAttachment Holes, LH/RH

53-11-66 FUSELAGE INTERNAL STRUCTURE, UPPER CORNER OF PORTALFRAME FROM FRAME 11A TO 16A, LH/RH


53-11-66-001-A General


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REFERENCE SUBJECT


53-11-66-250-801-A-01 Fuselage Internal Structure, Upper Corner of Portal Frame from Frame11A to 16A, LH/RH

53-11-77 LONGITUDINAL JUNCTION CENTRAL AND LATERAL PANELS ATSTGR46, BETWEEN FR11 TO FR12A, LH/RH


53-11-77-001-A General

53-11-79 LOWER FRAME 17 FITTING AT Y750 FITTING JUNCTION, LH/RH


53-11-79-001-A General

53-11-82 INTER-STRINGER AREA AT CIRCUMFERENTIAL JUNCTION AT FR18 /FR19, FROM STGR1 TO STGR55 RH/LH


53-11-82-001-A General



53-11-82-250-801-A-01 Longitudinal Junction at STGR43 between FR18 and FR19, LH/RH

53-11-82-270-801-A-01 Longitudinal Junction at STGR43 between FR18 and FR19, RH

53-11-83 FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 13, TWO FIRSTRIVET ROWS BELOW STR9 FW, ON LATERAL PANEL, LF


53-11-83-001-A General (BEFORE MODIFICATION 53102S18264 AND BEFOREMODIFICATION 55534S18704)

53-11-83-002-A Preferred Inspection (BEFORE MODIFICATION 53102S18264 ANDBEFORE MODIFICATION 55534S18704)


53-11-83-250-801-A-01 Fuselage Circumferential Joint , Two First Rivet Rows Forward of FR13,below STGR9 FWD, LH/RH. BEFORE MODIFICATION 53102S18264AND BEFORE MODIFICATION 55534S18704

53-11-84 FUSELAGE EXTERNAL STRUCTURE, RIVET LINES AT UPPERLONGITUDINAL LAP JOINT (STGR9 AFT LEVEL) FROM


53-11-84-001-A General



53-11-84-250-801-A-01 Fuselage External Structure, Rivet Lines at Upper Longitudinal Lap Joint(STGR 9 AFT Level) from FR13 to FR13A and from FR14 to FR16A,LH/RH

53-11-86 FUSELAGE CIRCUMFERENCIAL JOINT AT 13, 3 RIVETS ROWS OFFORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/


53-11-86-001-A General



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REFERENCE SUBJECT

53-11-86-250-801-A-01 Fuselage Circumferential Joint at FR13, 8 Fasteners of Forward UpperPanel Above STGR9 Forward, LH/RH

53-11-88 FUSELAGE CIRCUMFERENTIAL JOINT, RIVET ROWS FOWARD OFFR13, FROM STGR9 AFT TO STGR26, EXCLUDING 5 RO


53-11-88-001-A General



53-11-88-250-801-A-01 Fuselage Circumferential Joint, Rivet Rows Forward of FR13 from STGR9AFT to STGR26, Excluding 5 Rows at STGR9 FWD Level, LH/RH.

53-21-16 FUSELAGE SKIN INTERNAL SURFACE UNDERNEATH ACOUSTICINSULATION PANELS FROM FR18 TO FR26.4


53-21-16-001-A General



53-21-16-250-801-A-01 Fuselage Skin Internal Surface Underneath Acoustic Insulation Panels fromFR18 to FR26.4

53-21-24 DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH


53-21-24-001-A General




53-21-24-270-801-A-01 Door 2 (Mid Passenger/Crew Door) Cut-out, Structure underneath theScuff Plate, LH/RH (AFTER SB A330-53-3086)

53-21-24-250-801-A-01 Door 2 (Mid Passenger/Crew Door) Cut-out, Structure underneath theScuff Plate, LH/RH

53-21-24-250-801-C-01 Door 2 (Mid Passenger/Crew Door) Cut-out, Structure underneath theScuff Plate, LH/RH

53-21-25 FUSELAGE SKIN AT DOOR 2(MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH


53-21-25-001-A General



53-21-25-270-801-A-01 Fuselage Skin at Door 2 (Mid Passenger/Crew Door) Cut-Out UpperCorners

53-21-25-250-801-A-01 Fuselage Skin at Door 2 (Mid Passenger/Crew Door) Cut-out UpperCorners

53-21-36 FUSELAGE INTERNAL SKIN UNDERNEATH ACOUSTIC INSULATIONPANELS, LH/RH


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REFERENCE SUBJECT

53-21-36-001-A General


53-21-36-003-A Alternative Inspection


53-21-36-250-801-A-01 Fuselage internal Skin underneath Acoustic Insulation Panels from FR18 toFR32 - PROCEDURE A

53-21-36-250-802-A-01 Fuselage internal Skin underneath Acoustic Insulation Panels from FR18 toFR32 - PROCEDURE B

53-21-37 LOWER SKIN OF LONGITUDINAL LAP JOINTS IN THE CRACKSTOPPER AREAS, EXTERNAL SURFACE


53-21-37-001-A General



53-21-37-250-801-A-01 Lower Skin of Longitudinal Lap Joints in Crack Stopper Areas, ExternalSurface

53-21-49 SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR26, FROMSTGR4 TO 6, STGR12 TO 14 AND STGR21 TO 22,


53-21-49-001-A General



53-21-49-270-801-A-01 Splice Plate at the Circumferential Splice at FR26, from STGR4 toSTGR6, STGR12 to STGR14 and STGR21 to STGR22, LH/RH

53-21-49-250-801-A-01 Splice Plate at the Circumferential Splice at FR26, from STGR4 toSTGR6, STGR12 to STGR14 and STGR21 to STGR22, LH/RH

53-21-50 FUSELAGE LONGITUDINAL BUTT JOINT AT STGR9, BETWEEN FR31AND 37.1


53-21-50-001-A General



53-21-50-250-801-A-01 Fuselage Longitudinal Butt Joint at STGR9, between FR31 and FR37.1

53-21-51 EXTERNAL SKIN OF LONGITUDINAL LAP JOINT AT STGR22,BETWEEN FR37.1 AND 38


53-21-51-001-A General



53-21-51-250-801-A-01 External Skin of Longitudinal Lap Joint at STGR22, between FR37.1 andFR38, LH/RH

53-21-53 FUSELAGE OUTFLOW VALVE DOUBLER EXTERNAL SURFACE,BETWEEN FR32 AND 33, FROM STGR45 TO 49, LH ONLY


53-21-53-001-A General


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REFERENCE SUBJECT


53-21-53-250-801-A-01 Fuselage Outflow Valve Doubler External Surface, between FR32 andFR33, from STGR45 to STGR49, LH only

53-21-56 FUSELAGE CIRCUMFERENTIAL SPLICE AT FR37.1, FROM STGR13 TOCROWN CENTER LINE, LH/RH


53-21-56-001-A General

53-21-56-001-C General



53-21-56-250-801-A-01 Fuselage Circumferential Splice at FR37.1, from STGR13 to Crown CenterLine, LH/RH

53-21-56-250-801-C-01 Fuselage Circumferential Splice at FR37.1, from STGR9 to STGR13,LH/RH

53-21-57 FUSELAGE CIRCUMFERENTIAL SPLICE AT FR31, FROM STGR9 TO 15,LH/RH


53-21-57-001-A General



53-21-57-270-801-A-01 Fuselage Circumferential Splice at FR31, from STGR9 to STGR15, LH/RH

53-21-57-250-801-A-01 Fuselage Circumferential Splice at FR31, from STGR9 to STGR15, LH/RH

53-21-58 FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH


53-21-58-001-A General

53-21-58-001-C General




53-21-58-270-801-C-01 Fuselage Circumferential Splice at FR 37.1, from STGR9 to STGR 13,LH/RH


53-21-58-250-801-C-01 Fuselage Circumferential Splice at FR 37.1, from STGR9 to STGR 13,LH/RH

53-21-64 FWD FUSELAGE CARGO DOOR ACTUATOR SUPPORT BEAMBETWEEN FR22 AND 23


53-21-64-001-A General



53-21-64-250-801-A-01 FWD Fuselage Cargo Door Actuator Support Beam between FR22 andFR23

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REFERENCE SUBJECT

53-21-65 FUSELAGE LONGITUDINAL BUTT JOINT AT STGR9, BETWEEN FR31AND 37.1


53-21-65-001-A General



53-21-65-250-801-A-01 Fuselage Longitudinal Butt Joint at STGR9, between FR31 and FR37.1(AFTER MODIFICATION 46636D40649)

53-21-82 FRAME AND FRAME COUPLING FROM FR 20 TO FR 26/28 AT STR21,RH


53-21-82-001-A General

53-21-83 FUSELAGE SKIN AND CIRCUMFERENTIAL SPLICE AT FR31 BETWEENSTRG6 AND CROWN CENTER LINE, LH/RH


53-21-83-001-A General



53-21-83-250-801-A-01 Fuselage Skin and Circumferential Splice at FR31 between STGR6 andCrown Center Line, LH/RH

53-21-84 FUSELAGE LONGITUDINAL BUTT JOINT BETWEEN FR18 AND FR20 ATSTGR28 RH AND STGR39 RH


53-21-84-001-A General



53-21-84-250-801-A-01 Fuselage Longitudinal Butt Joint between FR18 and FR20 at STGR28 RHand STGR39 RH - Procedure A

53-21-84-250-802-A-01 Fuselage Longitudinal Butt Joint between FR18 and FR20 at STGR28 RHand STGR39 RH - Procedure B

53-21-85 FRAMES AND FRAME COUPLINGS FROM FR20 TO FR25 RH, BETWEENSTGR20 AND STGR23


53-21-85-001-A General



53-21-85-250-801-A-01 Frames and Frame Couplings from FR20 to FR25 RH, between STGR20and STGR23

53-21-85-270-801-A-01 Frames and Frame Couplings from FR20 to FR25 RH, between STGR20and STGR23

53-30-09 FUSELAGE CIRCUMFERENCIAL BUTT JOINT AT FR45, BETWEEN STGR3 AND 5, AND BETWEEN STGR 11 AND 13, LH/RH


53-30-09-001-A General


Page 9Jan 01/15

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REFERENCE SUBJECT


53-30-09-260-801-A-01 Fuselage Circumferential Butt Joint at FR45, between STGR3 and 5, andbetween STGR11 and 13, LH/RH

53-30-09-250-801-A-01 Fuselage Circumferential Butt Joint at FR45, between STGR3 and 5, andbetween STGR11 and 13, LH/RH

53-30-10 FUSELAGE CIRCUMFERENCIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH


53-30-10-001-A General



53-30-10-250-801-A-01 Fuselage Circumferential Joint at FR45 from Crown Centerline toSTGR17, LH/RH

53-30-12 FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER4 TO 5, LH/ RH


53-30-12-001-A General



53-30-12-260-801-A-01 Fuselage Circumferential Joint at FR54 from STGR4 to STGR5, LH/RH(64 Fastener Positions)

53-30-12-250-801-A-01 Fuselage Circumferential Joint at FR54 from STGR4 to STGR5, LH/RH(64 Fastener Positions)

53-30-13 FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANELSTIFFENER JUNCTION AT FRAME 48 CLEAT AT Y2093,Y2227


53-30-13-001-A General



53-30-13-250-801-A-01 Fuselage Internal Structure, Canted Pressure Panel Stiffener Junction onFR48 cleat at Y=2093, Y=2227 and Y=2361, LH/RH

53-30-14 MAIN LANDING GEAR BAY, LOWER FLANGE OF GANTRY Y1456, 20FASTENERS AFT OF FRAME 47 DATUM, LH/RH


53-30-14-001-A General



53-30-14-250-801-A-01 Main Landing Gear Bay, Lower Flange of Gantry Y=1456, 20 FastenersAft of FR47 Datum, LH/RH.

53-30-14-250-801-C-01 Main Landing Gear Bay, Lower Flange of Gantry Y=1456, 20 FastenersAft of Frame 47 Datum, LH/RH.

53-30-16 FUSELAGE CIRCUMFERENTIAL JOINT AT FR38 FROM CROWNCENTRELINE TO STGR3 AND FROM STGR5 TO STGR11, LH/RH


53-30-16-001-A General

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REFERENCE SUBJECT



53-30-16-250-801-A-01 Fuselage Circumferential Joint at FR38, From Crown Centerline to STGR3and From STGR5 to STGR11, External Surface, LH/RH

53-30-18 FRAME CIRCUMFERENTIAL JOINT AT FR54, FROM CROWNCENTRELINE TO STGR4 LH/RH AND FROM STGR5 TO STGR11,


53-30-18-001-A General



53-30-18-250-801-A-01 Fuselage Circumferential Joint at FR54, from Crown Centerline to STGR4and from STGR5 to STGR11, External Surface, LH/RH

53-30-19 FUSELAGE CIRCUMFERENTIAL BUTT JOINT STRAP RADIUS AT FR38,FROM CENTRELINE TO STGR8 (EXCLUDING AREA


53-30-19-001-A General



53-30-19-250-801-A-01 Fuselage Circumferential Butt Strap Radius at FR38, from Centerline toSTGR8 (Excluding Area between STGR3 and STGR5), LH/RH.

53-30-20 FLOOR BEAM Y1959 LOWER INBOARD FLANGE BETWEEN FR47 ANDFR48, LH/RH


53-30-20-001-A General (BEFORE MODIFICATION 42418S11867 AND BEFOREMODIFICATION 42418S11929)

53-30-20-002-A Preferred Inspection (BEFORE MODIFICATION 42418S11867 ANDBEFORE MODIFICATION 42418S11929)


53-30-20-250-801-A-01 Lower Flange and Radius of Floor Beam at Y1959 between FR47 andFR48, LH/RH (BEFORE MODIFICATION 42418S11867 AND BEFOREMODIFICATION 42418S11929)

53-30-21 RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 AND Y=450, AT FR53.2, LH


53-30-21-001-A General

53-30-21-002-G Preferred Inspection


53-30-21-250-801-B-01 Radii of Tee Fittings Connecting Hydraulic Bracket to Vertical BeamsY=953 and Y=450, below Pressure Floor, at Pressure Bulkhead FR53.2,LH

53-30-21-220-801-A-01 RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 AND Y=450, AT FR53.2, LH

53-30-22 FUSELAGE LONGITUDINAL LAP JOINT AT STR 5 FROM FR 38 TO FR45, LH/RH


53-30-22-001-A General

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REFERENCE SUBJECT



53-30-22-270-801-A-01 Fuselage Longitudinal Lap Joint at STGR5, from FR38 to FR45, LH/RH

53-30-24 FUSELAGE LONGITUDINAL LAP JOINT AT STR 13 FROM FR 38 TO 45,LH/RH


53-30-24-001-A General




53-30-25 FUSELAGE LONGITUDINAL LAP JOINT AT STR 13 FROM FR 45 TO53.3, LH/RH


53-30-25-001-A General



53-30-25-270-801-A-01 Fuselage Longitudinal Lap Joint at STGR13 from FR45 to FR53.3, LH/RH

53-30-26 FUSELAGE LONGITUDINAL LAP JOINT AT STR 22 FROM FR 38 TO 45,LH/RH


53-30-26-001-A General




53-30-27 FUSELAGE LONGITUDINAL LAP JOINT AT STR 22 FROM FR 45 TO 53,3LH/RH


53-30-27-001-A General



53-30-27-270-801-A-01 Fuselage Longitudinal Lap Joint at STGR22, from FR45 to FR53.3,LH/RH

53-30-51 STRAP AT STGR31 LONGITUDINAL JUNCTION BETWEEN FR53.1 ANDFR53.2,LH/RH


53-30-51-001-A General



53-30-51-270-801-A-01 Strap at STGR31 Longitudinal Junction between FR53.1 and FR53.2,LH/RH

53-30-52 MAIN LONGERON EXTENSION BETWEEN FR53.2 AND FR53.3, LH/RH


53-30-52-001-A General


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REFERENCE SUBJECT


53-30-52-270-801-A-01 Main Longeron Extension between FR53.2 and FR53.3, LH/RH

53-31-05 FUSELAGE INTERNAL STRUCTURE, FASTENER HOLE AREA ABOVESTRINGER 28 AT FRAME 39.1 WEB JUNCTION ON





53-31-05-270-801-A-01 Fuselage Internal Structure, Fastener Hole Area above STGR28 at FR39.1Web Junction on Hoist Fitting, LH/RH(BEFORE MODIFICATION40391S10374)

53-31-06 FUSELAGE EXTERNAL STRUCTURE, FASTENERS AREA BETWEENSTR18 AND STR22, FROM FR38 TO 53.3, LH/RH


53-31-06-001-A General



53-31-06-250-801-A-01 Fuselage External Structure, Fasteners Area at Window Frames Junctionon Fuselage Skin between STGR18 and STGR22, from FR38 to FR53.3,LH/RH

53-31-07 FUSELAGE INTERNAL STRUCTURE, FR39 TO FR39.2 WEB HOLE AREAJUST BELOW STGR28 AND FR39 TO 39.2 FASTENERS


53-31-07-001-A General



53-31-07-270-801-A-01 Fuselage Internal Structure, FR39 to FR39.2 Web Hole Area just belowSTGR28 and Fasteners Area at Frames Junction below STGR29 Level,LH/RH

53-31-07-250-801-A-01 Fuselage Internal Structure, FR39 to FR39.2, Web Hole Area just belowSTGR28 and Fasteners Area at Frames Junction below STGR29 Level,LH/RH

53-31-09 FUSELAGE LONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME38 TO 53.3 ATSTRINGER 13 FROM FRAME 38 TO 47 AND


53-31-09-001-A General



53-31-09-250-801-A-01 Fuselage Longitudinal Lap joint at STGR5 from FR38 to FR53.3, atSTGR13 from FR38 to FR47 and at STGR22 from FR43 to FR53.3,Excluding 3 Rivet Rows Forward and Aft FR45 Level, LH/RH

53-31-11 FUSELAGE EXTERNAL STRUCTURE, FIRST FASTENER ROW AREAABOVE STRINGER 39 BETWEEN FRAMES 53.2 AND 53.3


53-31-11-001-A General

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REFERENCE SUBJECT



53-31-11-270-801-B-01 Fuselage External Structure, First Fasteners Row Area above STGR39between FR53.2 and FR53.3, LH/RH

53-31-12 FUSELAGE EXTERNAL STRUCTURE, LONGITUDINAL JOINT ATSTRINGER 39 AHEAD OF FRAME 53.2, LH / RH


53-31-12-001-A General



53-31-12-270-801-B-01 Fuselage External Structure, Longitudinal Joint at STGR39 ahead ofFR53.2, LH/RH

53-31-13 FUSELAGE EXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME 47,FROM BELOW STRINGER 22 TO ABOVE STRINGER


53-31-13-001-A General



53-31-13-270-801-A-01 Fuselage External Structure, Fasteners Rows at FR47, from belowSTGR22 to above STGR24 Level, LH/RH

53-31-14 FUSELAGE INTERNAL STRUCTURE, FR47 WEB AT JUNCTION WITHSTABILIZER STGR20 TO 23, LH/RH


53-31-14-001-A General



53-31-14-270-801-A-01 Fuselage Internal Structure, FR47 Web at Junction with StabilizerSTGR20 to STGR23, LH/RH

53-31-38 FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM INBOARD FLANGEAT Y=1959,LH/RH


53-31-38-001-A General (AFTER MODIFICATION 42418S11867)

53-31-38-002-A Preferred Inspection (AFTER MODIFICATION 42418S11867)


53-31-38-260-801-A-01 Fuselage Internal Structure, Floor Beam Inboard Flange at Y=1959,LH/RH (AFTER MODIFICATION 42418S11867)

53-31-40 FUSELAGE INTERNAL STRUCTURE, FR53.2BULKHEAD FORWARDFACE, ANGLE SPLICE AT STGR42, LH/RH


53-31-40-001-A General



53-31-40-250-801-A-01 Fuselage Internal Structure, FR53.2 Bulkhead Forward Face, Angle Spliceat STGR42, LH/RH

Page 14Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT

53-31-45 EXTERNAL INSPECTION OF THE LONGITUDINAL BUTT JOINT ATSTGR31 LEVEL FROM FR53.3 TO FR54, LH/RH





53-31-45-250-801-A-01 External Inspection of the Longitudinal Butt Joint at STGR31 Level fromFR53.3 to FR54, LH/RH (BEFORE MODIFICATION 49202S16307)

53-31-51 FR40 FRONT FITTING AT STGR21 LEVEL, LH/RH


53-31-51-001-A General



53-31-51-270-801-A-01 FR40 Front Fitting at STGR21 Level, LH/RH

53-31-52 INTERNAL INSPECTION OF STGR31 BETWEEN FR53.7 TO FR53.8 ATFILLET FAIRING LEVEL, LH/RH


53-31-52-001-A General



53-31-52-270-801-A-01 Internal Inspection of STGR31 between FR53.7 to FR53.8 at Fillet FairingLevel, LH/RH

53-31-56 FUSELAGE INTERNAL STRUCTURE, SPLICE AT FRAME JUNCTIONSBETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3


53-31-56-001-A General



53-31-56-270-801-A-01 Fuselage Internal Structure, Splice at Frame Junctions between STGR32and STGR33 at FR53.3 to FR54, LH/RH

53-31-61 FUSELAGE INTERNAL STRUCTURE, SPLICING AREA AT FRAMES 53 TO53.2 BETWEEN STRINGERS 24 AND 26, LH/RH


53-31-61-001-A General



53-31-61-270-801-A-01 Fuselage Internal Structure, Splicing Area at Frames 53 to 53.2 betweenStringers 24 and 26, LH/RH - Procedure A

53-31-61-270-802-A-01 Fuselage Internal Structure, Splicing Area at Frames 53 to 53.2 betweenStringers 24 and 26, LH/RH - Procedure B

53-31-62 MAIN LANDING GEAR BAY, LOWER FLANGE OF GANTRY Y1456, 40FASTENERS FORWARD AND AFT FR48 DATUM, LH/RH


53-31-62-001-A General

53-31-62-001-D General

Page 15Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT



53-31-62-270-801-A-01 Main Landing Gear Bay, Lower Flange of Gantry Y1456, 40 FastenersForward and AFT FR48 Datum, LH/RH

53-31-62-270-801-D-01 Main Landing Gear Bay, Lower Flange of Gantry Y=1456, 40 FastenersForward and AFT FR48 Datum, LH/RH

53-31-78 FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM INBOARD FLANGERADIUS AT Y1959, FROM FRAME 47 TO FRAME 48, LH/RH


53-31-78-001-A General



53-31-78-250-801-A-01 Fuselage Internal Structure, Floor Beam Inboard Flange Radius atY=1959, from Frame 47 to Frame 48, LH/RH

53-31-81 SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE BTW FR 53.6 AND53.7 AT DOOR TYPE A AND AT DOOR TYPE 1, LH/


53-31-81-001-A General



53-31-81-250-801-A-01 Splice Plate at the Circumferential Splice between FR53.6 and FR53.7,LH/RH

53-31-82 LOWER SKIN OF LONGITUDINAL LAP JOINT IN CRACK STOPPERAREA AT STGR5, BETWEEN FR53.3 AND 54


53-31-82-001-A General



53-31-82-250-801-A-01 Lower Skin of Longitudinal Lap Joint in Crack Stopper Area at Stringers 5LH/RH, between FR53.3 and FR54, External Surface

53-31-87 LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FR48 ANDFR49, Y-1456 AND Y+1456


53-31-87-001-A General



53-31-87-270-801-A-01 Large Membranes around 6 Fasteners between FR48 and FR49, at Y-1456and Y+1456

53-31-87-270-802-A-01 Large Membranes around 6 Fasteners between FR48 and FR49, at Y-1456and Y+1456

53-31-89 FWD LOWER SHELL PANEL BTW STGR35 AND 36, LHS, FROM FR39.2TO 40 INERTING SYSTEM CROSSING AREA


53-31-89-001-A General



Page 16Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT

53-31-89-250-801-A-01 Fwd Lower Shell Panel between STGR35 and STGR36, LH side, fromFR39.2 to FR40 at Inerting System Crossing Area



53-31-94 FUSELAGE SKIN AT DOOR 3 (EMMERGENCY/PASSENGER/CREWDOOR) CUT-OUT UPPER CORNERS


53-31-94-001-A General



53-31-94-270-801-A-01 Fuselage Skin at Door 3 (Emergency/Passenger Crew Door) Cut-OutUpper Corners, LH/RH (AFTER SB 53-3023 OR AFTERMODIFICATION 42351D19526)

53-31-94-250-801-A-01 Fuselage Skin at Door 3 (Emergency/Passenger Crew Door) Cut-OutUpper Corners, LH/RH

53-31-94-250-803-B-01 Fuselage Skin at Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out Upper Corners, LH/RH

53-31-94-250-803-C-01 Fuselage Skin at Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out Upper Corners, LH/RH

53-31-94-250-803-D-01 Fuselage Skin at Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out Upper Corners, LH/RH

53-31-95 DOOR 3 (EMMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH


53-31-95-001-A General



53-31-95-270-801-A-01 Door 3 (Emergency/Passenger Crew Door) Cut-Out, Structure underneaththe Scuff Plate, LH/RH (AFTER SB 53-3023 OR AFTERMODIFICATION 42351D19526)

53-31-95-250-801-A-01 Door 3 (Emergency/Passenger Crew Door) Cut-Out, Structure underneaththe Scuff Plate, LH/RH

53-31-95-250-803-B-01 Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out, Structureunderneath the Scuff Plate, LH/RH

53-31-95-250-803-C-01 Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out, Structureunderneath the Scuff Plate, LH/RH

53-31-95-250-803-D-01 Door 3 (Large Emergency/Passenger/Crew Door) Cut-Out, Structureunderneath the Scuff Plate, LH/RH

53-31-96 MAIN LANDING GEAR BAY, CATENARIES SKINS AT JUNCTION WITHGANTRIES Y1456, BETWEEN FR48 AND FR49 LH/RH


53-31-96-001-A General


Page 17Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT


53-31-96-270-801-A-01 Main Landing Gear Bay, Catenaries Skins at Junction with GantriesY1456, Outside Board, and Y1959, Inside Board, between FR48 andFR49, LH/RH

53-41-04 SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH /RH


53-41-04-001-A General



53-41-04-270-801-A-01 Splice Plate at Circumferential Skin Splice at FR58, from STGR 4 toSTGR6, STGR12 to STGR14 and STGR21 to STGR22, LH/RH

53-41-04-250-801-A-01 Splice Plate at Circumferential Skin Splice at FR58, from STGR4 toSTGR6, STGR12 to STGR14 and STGR21 to STGR22, LH/RH

53-41-07 SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR72, ATINTERSECTION OF LAP JOINTS, LH/RH


53-41-07-001-A General



53-41-07-270-801-A-01 Splice Plate at Circumferential Skin Splice at FR72, from STGR3 toSTGR7, and STGR11 to STGR13, at Intersection of Lap Joints andCircumferential Skin Splice, LH/RH

53-41-07-250-801-A-01 Splice Plate at Circumferential Skin Splice at FR72, from STGR3 toSTGR7, and STGR11 to STGR13, at Intersection of Lap Joints andCircumferential Skin Splice, LH/RH

53-41-13 LOWER SKIN OF LONGITUDINAL LAP JOINT IN SPECIFIC CRACKSTOPPER AREAS AT STGR13, 17, 22 AND 24


53-41-13-001-A General



53-41-13-250-801-A-01 Lower Skin of Longitudinal Lap Joint in the Crack Stopper Areas ExternalSurface, at STGR13 and STGR22 LH/RH from FR54 to FR72 and atSTGR17 and STGR24 LH/RH from FR76 to FR80

53-41-15 LOWER SKIN OF LONGITUDINAL LAP JOINT IN SPECIFIC CRACKSTOPPER AREAS AT STGR5 AND 6, EXTERNAL


53-41-15-001-A General



53-41-15-250-801-A-01 Lower Skin of Longitudinal Lap Joint in the Crack Stopper Areas atSTGR5, from FR54 to FR72 and at STGR6, from FR72 to FR80, LH/RH,External Surface

53-41-16 LOWER SKIN OF LONGITUDINAL LAP JOINT IN CRACK STOPPERAREAS AT STGR44, EXTERNAL SURFACE

Page 18Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT


53-41-16-001-A General



53-41-16-250-801-A-01 Lower Skin of Longitudinal Lap Joint in Crack Stopper Areas at STGR44LH/RH, from FR 54 to FR 55, External Surface

53-41-17 LOWER SKIN OF LONGITUDINAL LAP JOINT AT STGR 54 LH, FROMFR54 TO 58, EXTERNAL SURFACE


53-41-17-001-A General



53-41-17-270-801-A-01 Lower Skin of Longitudinal Lap Joint at STGR54, LH between FR54 andFR58

53-41-31 DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS


53-41-31-001-A General



53-41-31-250-801-A-01 Door 4 (AFT Passenger/Crew Door) Cut-Out Upper Corners

53-41-32 DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE LH/RH


53-41-32-001-A General



53-41-32-250-801-A-01 Door 4 (AFT Passenger/Crew Door) Cut-Out, Structure Underneath theScuff Plate, LH/RH

53-41-36 FUSELAGE SKIN OF AFT CARGO COMPARTMENT DOOR CUT-OUT ATUPPER REAR AND LOWER FWD CORNERS


53-41-36-001-A General (BEFORE MODIFICATION 41045D18651)

53-41-36-002-A Preferred Inspection (BEFORE MODIFICATION 41045D18651)


53-41-36-250-801-A-01 Fuselage Skin of AFT Cargo Compartment Door Cut-Out at Upper Rearand Lower FWD Corners, External Surface (BEFORE MODIFICATION41045D18651)

53-41-55 TORSION BOX LONGITUDINAL BEAM ADJACENT TO RUNOUT OFCORNER DOUBLER BTW FR73A AND 74, LH/RH


53-41-55-001-A General



53-41-55-250-801-A-01 Torsion Box Longitudinal Beam Adjacent to Run Out of Corner DoublerBetween FR73A and FR74, LH/RH

Page 19Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT

53-41-64 AFT FUSELAGE, CARGO DOOR ACTUATOR SUPPORT BEAM BETWEENFR61 AND 62


53-41-64-001-A General



53-41-64-250-801-A-01 AFT Fuselage Cargo Door Actuator Support Beam Between FR62 andFR63 (AFTER MODIFICATION 44072D40405 AND BEFOREMODIFICATION 45489D40883)

53-41-66 SKIN AROUND VHF2 ANTENNA CUT-OUT BETWEEN FR 54 AND 55


53-41-66-001-A General

53-41-66-002-A General




53-41-66-270-801-A-01 Skin Around VHF2 Antenna Cut-Out between FR54 and FR55, fromSTGR51 to STGR52, LH (ON A/C MSN 0320, 0324, 0326, 0328, 0330,0334, 0336 AND 0339)

53-41-66-250-801-A-01 Skin Around VHF2 Antenna Cut-Out between FR54 and FR55, fromSTGR56 to STGR57, RH AFTER MODIFICATION 46025D42061 ANDBEFORE MODIFICATION 46849D42376

53-41-82 FRAMES AND FRAME COUPLINGS FROM FR60 TO FR64 BETWEENSTGR20 AND STGR23, RH


53-41-82-001-A General



53-41-82-250-801-A-01 Frame and frame couplings from FR60 to FR64 between STGR20X andSTGR23, RH

53-41-82-270-801-A-01 Frames and frame couplings from FR60 to FR64 between STGR20X andSTGR23, RH

53-51-00 THE FLANGE AND THE LONGITUDINAL DOUBLER OF THE VERTICALTAIL ATTACHMENT FITTING


53-51-00-001-A General



53-51-00-250-801-A-01 The Flange of the Vertical Tail Attachment Fitting at FR80 in the Areabetween STGR2A and STGR5A, LH/RH -- PROCEDURE A

53-51-00-250-802-A-01 Longitudinal Doubler for the Vertical Tail Attachment Fittings in the Areaat FR84 and FR86 Between STGR2 and STGR3 and Between STGR4 andSTGR5A, LH/RH -- PROCEDURE B.

53-51-09 HORIZONTAL STABILIZER HINGE SUPPORT MEMBERS AND UPPERAND LOWER ATTACHMENT LUGS OF FR91 LH/RH

Page 20Jan 01/15

T.O.C.

Revision n: 80


REFERENCE SUBJECT


53-51-09-001-A General



53-51-09-270-801-A-01 Horizontal Stabilizer Hinge Support Members and Upper and LowerAttachment Lugs of FR 91 LH/RH - PROCEDURE A

53-51-09-270-802-A-01 Horizontal Stabilizer Hinge Support Members and Upper and LowerAttachment Lugs of FR 91 LH/RH - PROCEDURE B

53-56-10 THS SUPPORT RODS AT FR91


53-56-10-001-A General



53-56-10-250-801-A-01 THS Support Rods at FR91

53-58-01 APU MOUNTS, SUSPENSION TIE-RODS AND ATTACHMENTBRACKETS


53-58-01-001-A General



53-58-01-250-801-A-01 APU Mounts, Suspension Tie-Rods and Attachment Brackets

Page 21Jan 01/15

T.O.C.

Revision n: 80


CHAPTER 53 - FUSELAGE

LIST OF EFFECTIVE CONTENTREFERENCE CHG CODE REVISION DATE

CHAPTER 53 Oct 01/12

53-00-01 Jan 01/10

53-00-01-001-A Jan 01/10

53-00-01-002-A Jan 01/10

53-00-01-220-801-A-01 Jan 01/10

53-00-01-221-001-A Jan 01/10

53-00-01-222-001-A Jan 01/10

53-00-01-971-001-A Jan 01/10

Figure 53-00-01-991-001-A Jan 01/10

Figure 53-00-01-991-001-A SHEET 01 Jan 01/10

Figure 53-00-01-991-002-A Jan 01/10


Figure 53-00-01-991-003-A Jan 01/10


Figure 53-00-01-991-004-A Jan 01/10


Figure 53-00-01-991-005-A Jan 01/10


Figure 53-00-01-991-006-A Jan 01/10


Figure 53-00-01-991-007-A Jan 01/10


Figure 53-00-01-991-008-A Jan 01/10


Figure 53-00-01-991-009-A Jan 01/10


Figure 53-00-01-991-010-A Jan 01/10


Figure 53-00-01-991-011-A Jan 01/10


Figure 53-00-01-991-012-A Jan 01/10


Figure 53-00-01-991-013-A Jan 01/10


53-00-01-220-802-A-01 Nov 01/10

Page 1Jan 01/15

L.E.C.

Revision n: 80


REFERENCE CHG CODE REVISION DATE

53-00-01-221-002-A Nov 01/10

53-00-01-224-001-A Nov 01/10

53-00-01-222-002-A Nov 01/10

53-00-01-971-004-A Jan 01/10

Figure 53-00-01-991-014-A Jan 01/10


Figure 53-00-01-991-015-A Jan 01/10


Figure 53-00-01-991-016-A Jan 01/10


Figure 53-00-01-991-017-A Jan 01/10


Figure 53-00-01-991-019-A Jan 01/10


Figure 53-00-01-991-020-A Jan 01/10


Figure 53-00-01-991-021-A Nov 01/10

Figure 53-00-01-991-021-A SHEET 01 Nov 01/10

Figure 53-00-01-991-033-A Nov 01/10


Figure 53-00-01-991-034-A Nov 01/10


Figure 53-00-01-991-035-A Nov 01/10


Figure 53-00-01-991-036-A Nov 01/10


Figure 53-00-01-991-037-A Nov 01/10


53-00-01-250-801-A-01 Nov 01/10

53-00-01-251-001-A Nov 01/10

53-00-01-252-001-A Nov 01/10

53-00-01-253-001-A Nov 01/10

53-00-01-971-005-A Jan 01/10

53-00-01-943-001-A Jan 01/10

Figure 53-00-01-991-022-A Jan 01/10


Figure 53-00-01-991-023-A Nov 01/10


Figure 53-00-01-991-024-A Jan 01/10

Page 2Jan 01/15

L.E.C.

Revision n: 80




Figure 53-00-01-991-025-A Nov 01/10


Figure 53-00-01-991-026-A Jan 01/10


Figure 53-00-01-991-027-A Jan 01/10


Figure 53-00-01-991-038-A Nov 01/10


Figure 53-00-01-991-028-A Jan 01/10


Figure 53-00-01-991-029-A Jan 01/10


Figure 53-00-01-991-030-A Nov 01/10


Figure 53-00-01-991-031-A Nov 01/10


Figure 53-00-01-991-032-A Nov 01/10


53-00-02 Apr 01/08

53-00-02-001-A R Jan 01/15

53-00-02-002-A R Jan 01/15

53-00-02-250-801-A-01 R Jan 01/15

53-00-02-254-001-A R Jan 01/15

53-00-02-251-001-A R Jan 01/15

53-00-02-252-001-A R Jan 01/15

53-00-02-253-001-A R Jan 01/15

53-00-02-971-001-A R Jan 01/15

Figure 53-00-02-991-001-A R Jan 01/15

Figure 53-00-02-991-001-A SHEET 01 R Jan 01/15

Figure 53-00-02-991-002-A R Jan 01/15


Figure 53-00-02-991-003-A R Jan 01/15


Figure 53-00-02-991-004-A R Jan 01/15


Figure 53-00-02-991-005-A R Jan 01/15


Figure 53-00-02-991-006-A R Jan 01/15

Page 3Jan 01/15

L.E.C.

Revision n: 80




Figure 53-00-02-991-007-A R Jan 01/15



Figure 53-00-02-991-008-A R Jan 01/15


53-11-08 Oct 01/14

53-11-08-001-A Oct 01/14

53-11-08-002-A Oct 01/14

53-11-08-270-801-A-01 Oct 01/14

53-11-08-271-012-A Oct 01/14

53-11-08-272-001-A Oct 01/14

53-11-08-273-001-A Oct 01/14

53-11-08-971-001-A Oct 01/14

53-11-08-943-001-A Oct 01/14

Figure 53-11-08-991-002-A Oct 01/14

Figure 53-11-08-991-002-A SHEET 01 Oct 01/14

Figure 53-11-08-991-003-A Oct 01/14


Figure 53-11-08-991-004-A Oct 01/14


Figure 53-11-08-991-005-A Oct 01/14



Figure 53-11-08-991-006-A Oct 01/14


53-11-09 Oct 01/14

53-11-09-001-A Oct 01/14

53-11-09-002-A Oct 01/14

53-11-09-270-801-A-01 Oct 01/14

53-11-09-271-001-A Oct 01/14

53-11-09-272-001-A Oct 01/14

53-11-09-273-001-A Oct 01/14

53-11-09-971-001-A Oct 01/14

53-11-09-943-001-A Oct 01/14

Figure 53-11-09-991-001-A Oct 01/14



Page 4Jan 01/15

L.E.C.

Revision n: 80



Figure 53-11-09-991-002-A Oct 01/14



Figure 53-11-09-991-003-A Oct 01/14


Figure 53-11-09-991-004-A Oct 01/14


Figure 53-11-09-991-005-A Oct 01/14



53-11-25 Apr 01/08

53-11-25-001-A R Jan 01/15

53-11-25-002-A R Jan 01/15

53-11-25-250-801-A-01 R Jan 01/15

53-11-25-254-001-A R Jan 01/15

53-11-25-251-001-A R Jan 01/15

53-11-25-252-001-A R Jan 01/15

53-11-25-253-001-A R Jan 01/15

53-11-25-971-001-A R Jan 01/15

Figure 53-11-25-991-001-A R Jan 01/15


Figure 53-11-25-991-002-A R Jan 01/15


Figure 53-11-25-991-003-A R Jan 01/15


Figure 53-11-25-991-004-A R Jan 01/15


53-11-27 Apr 01/08

53-11-27-001-A R Jan 01/15

53-11-27-002-A R Jan 01/15

53-11-27-250-801-A-01 R Jan 01/15

53-11-27-254-001-A R Jan 01/15

53-11-27-251-001-A R Jan 01/15

53-11-27-252-001-A R Jan 01/15

53-11-27-253-001-A R Jan 01/15

53-11-27-971-001-A R Jan 01/15

Figure 53-11-27-991-001-A R Jan 01/15


Page 5Jan 01/15

L.E.C.

Revision n: 80



Figure 53-11-27-991-002-A R Jan 01/15


Figure 53-11-27-991-003-A R Jan 01/15


Figure 53-11-27-991-004-A R Jan 01/15


53-11-29 Apr 01/08

53-11-29-001-A R Jan 01/15

53-11-29-002-A R Jan 01/15

53-11-29-250-801-A-01 R Jan 01/15

53-11-29-254-001-A R Jan 01/15

53-11-29-251-001-A R Jan 01/15

53-11-29-252-001-A R Jan 01/15

53-11-29-253-001-A R Jan 01/15

53-11-29-971-001-A R Jan 01/15

Figure 53-11-29-991-001-A R Jan 01/15



Figure 53-11-29-991-002-A R Jan 01/15


Figure 53-11-29-991-003-A R Jan 01/15


Figure 53-11-29-991-004-A R Jan 01/15


53-11-30 Apr 01/08

53-11-30-001-A R Jan 01/15

53-11-30-002-A R Jan 01/15

53-11-30-270-801-A-01 R Jan 01/15

53-11-30-274-001-A R Jan 01/15

53-11-30-271-001-A R Jan 01/15

53-11-30-272-001-A R Jan 01/15

53-11-30-273-001-A R Jan 01/15

53-11-30-971-001-A R Jan 01/15

53-11-30-943-001-A R Jan 01/15

Figure 53-11-30-991-001-A R Jan 01/15


Figure 53-11-30-991-002-A R Jan 01/15


Page 6Jan 01/15

L.E.C.

Revision n: 80



Figure 53-11-30-991-003-A R Jan 01/15


Figure 53-11-30-991-004-A R Jan 01/15


Figure 53-11-30-991-005-A R Jan 01/15



53-11-31 Apr 01/08

53-11-31-001-A Oct 01/14

53-11-31-002-A Oct 01/14

53-11-31-250-801-A-01 Oct 01/14

53-11-31-254-001-A Oct 01/14

53-11-31-251-001-A Oct 01/14

53-11-31-252-001-A Oct 01/14

53-11-31-253-001-A Oct 01/14

53-11-31-971-001-A Oct 01/14

Figure 53-11-31-991-001-A Oct 01/14


Figure 53-11-31-991-002-A Oct 01/14


Figure 53-11-31-991-003-A Oct 01/14


53-11-31-250-802-A-01 Oct 01/14

53-11-31-254-003-A Oct 01/14

53-11-31-251-003-A Oct 01/14

53-11-31-252-003-A Oct 01/14

53-11-31-253-003-A Oct 01/14

53-11-31-971-003-A Oct 01/14

Figure 53-11-31-991-007-A Oct 01/14


Figure 53-11-31-991-008-A Oct 01/14


Figure 53-11-31-991-009-A Oct 01/14


53-11-34 Apr 01/08

53-11-34-001-A R Jan 01/15

53-11-34-002-A R Jan 01/15

53-11-34-250-801-A-01 R Jan 01/15

Page 7Jan 01/15

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53-11-34-254-001-A R Jan 01/15

53-11-34-251-001-A R Jan 01/15

53-11-34-252-001-A R Jan 01/15

53-11-34-253-001-A R Jan 01/15

53-11-34-971-001-A R Jan 01/15

Figure 53-11-34-991-001-A R Jan 01/15


Figure 53-11-34-991-002-A R Jan 01/15


Figure 53-11-34-991-003-A R Jan 01/15


Figure 53-11-34-991-004-A R Jan 01/15


53-11-35 Apr 01/08

53-11-35-001-A Jul 01/10

53-11-35-002-A Jul 01/10

53-11-35-250-801-A-01 Jul 01/10

53-11-35-254-001-A Jul 01/10

53-11-35-251-001-A Jul 01/10

53-11-35-252-001-A Jul 01/10

53-11-35-253-001-A Jul 01/10

53-11-35-971-001-A Jul 01/10

Figure 53-11-35-991-001-A Jul 01/10

Figure 53-11-35-991-001-A SHEET 01 Jul 01/10

Figure 53-11-35-991-002-A Jul 01/10


Figure 53-11-35-991-003-A Jul 01/10


53-11-40 Apr 01/08

53-11-40-001-A R Jan 01/15

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Figure 53-21-58-991-001-A R Jan 01/15

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