STRUCTURAL REPAIR MANUAL FUSELAGE DIAGRAMS — … · Installation F.F.M.S. - FS 133 - FS 193 Top 159B10221 0.040 ALCLAD 2024-T3 9 Skin Assembly and Installation Fuselage - RH FS

FUSELAGE DIAGRAMS — STRUCTURAL IDENTIFICATION

1. Fuselage — Diagrams, Materials, Illustrations and Part Number Identification

A. General

The following item numbers are used in conjunction with Figure 1.

Fuselage

ITEM DESCRIPTION DWG. REF. GAGE MATERIAL EFFECT

1 Skin Installation - FuselageForward Section - FS 44 - FS79

159B10203 0.050 ALCLAD 2024-T42

2 Skin Installation - FS 44 3/8 -FS 85 3/8

1159B21110 0.050 ALCLAD 2024-T3

3 Skin Installation - FuselageForward Section FS 85

1159B21111 0.050 ALCLAD 2024-T3

4 Skin Assembly - FuselageForward Section - FS 12311/16 - FS 145 LH

159B10243 0.050 ALCLAD 2024-T3

5 Skin Installation - CockpitEnclosure

1159B30201 0.050 ALCLAD 2024-T42

6 Skin Installation - ForwardSection FS 114.06 - FS 145,LH

1159B30242 0.050 ALCLAD 2024-T42

7 Skin Installation - AssemblyFS 145 - FS 193

1159B20241 0.063 /0.040 (3)

ALCLAD 2024-T42

8 Skin Panel Assembly andInstallation F.F.M.S. - FS 133 -FS 193 Top

159B10221 0.040 ALCLAD 2024-T3

9 Skin Assembly and InstallationFuselage - RH FS 133 - FS193

1159B20222 0.040 ALCLAD 2024-T42

10 Skin Assembly and InstallationFuselage Forward Mid SectionFS 133 - FS 193 Bottom

1159B20223 0.050 ALCLAD 2024-T3

11 Skin Installation - FuselageMid Section FS 193 - FS 297

1159B41226 0.040 ALCLAD 2024-T3

12 Skin Installation and Assembly- Fuselage Forward MidSection FS 145 - FS 193,Stinger 4 - Stringer 11 LH

1159B20224 0.050 ALCLAD 2024-T3

13 Skin Assembly and Installation- Fuselage Mid

1159B40225 0.040 ALCLAD 2024-T3

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ITEM DESCRIPTION DWG. REF. GAGE MATERIAL EFFECT

14 Skin Installation - Upper, FS181.00 - FS 345.875

1159B43128 0.040 (1) ALCLAD 2024-T3

15 Skin Installation - FuselageMid Section, FS 193 - FS321.5

1159B40227 0.040 ALCLAD 2024-T3

16 Skin Installation - FS 297 - FS345 7/8

1159B21100 0.040 (1) ALCLAD 2024-T3

17 Skin Installation - FS 345 7/8 -FS 452 1/2

1159B21210 0.040 ALCLAD 2024-T3

18 Skin Installation - FS 345 7/8 -FS 452 1/2

1159B21211 0.040 (2) ALCLAD 2024-T3

19 Skin Installation - FS 451 5/16- FS 498 Upper

1159B21310 0.040 ALCLAD 2024-T3

20 Skin Installation and AssemblyAft Mid

1159B41311 0.040 ALCLAD 2024-T42

21 Skin Installation - Fuselage -Aft Mid Section FS 498 - FS580 Top

1159B21314 0.040 ALCLAD 2024-T42

22 Skin Installation - Fuselage AftMid Section FS 498 - FS 580LH

1159B31315 0.040 ALCLAD 2024-T42

23 Skin Installation - Fuselage AftMid Section FS 498B - FS580 RH

1159B31316 0.040 ALCLAD 2024-T42

24 Skin Installation - Fuselage AftMid Section - FS 498 - FS580 Bottom

1159B41317 0.040 ALCLAD 2024-T42

25 Skin Installation - Fuselage AftMid

1159B31318 0.040 ALCLAD 2024-T42

26 Skin Installation - Fuselage AftMid Section

1159B31319 0.050 ALCLAD 2024-T42

27 Skin Installation - FS 580 - FS635 Bottom

1159B31321 ALCLAD 2024-T42

28 Skin Installation - FS 635 - FS713 Top

1159B21510 0.063 /0.040 (3)

ALCLAD 2024-T42

29 Installation - Fuselage TailSection FS 635.00 - FS713.50 Side

1159B41511 0.063 /0.040 (3)

ALCLAD 2024-T42

30 Skin Installation - FS 635 - FS713 Bottom

1159B21513 0.063 /0.040 (3)

ALCLAD 2024-T42

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ITEM DESCRIPTION DWG. REF. GAGE MATERIAL EFFECT

31 Skin Installation - FuselageTail FS 713 - FS 757 Bottom

1159B41517 0.063 /0.040 (3)

ALCLAD 2024-T42

32 Skin Installation - Tail FS 713- FS 757

1159B21515 0.063 /0.040 (3)

ALCLAD 2024-T42

33 Skin Installation - Tail SectionFS 757

1159B21521 0.063 /0.040 (3)

ALCLAD 2024-T42

34 Skin Installation - FuselageTail FS 757.563 - FS 812.50Side

1159B21519 0.063 /0.040 (3)

ALCLAD 2024-T42

(1) Additional 0.032 doubler inside skin.(2) Additional 0.050 doubler inside skin.(3) Skin thickness 0.063 chem-milled to 0.040.

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Fuselage Skin Thickness LocatorFigure 1 (Sheet 1 of 3)

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Fuselage Skin Thickness LocatorFigure 1 (Sheet 2 of 3)

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23 22

21

24 27

30

26

25

28

29

32

31

33

34

29715C01

Fuselage Skin Thickness LocatorFigure 1 (Sheet 3 of 3)

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2. Stringers — Diagrams, Materials, Illustrations and Part Number Identification

A. General

See Table 1 and Table 2 and Figure 2 and Figure 3 for stringer location and material.

Table 1: Stringer Location

INTERSECTION OF STRINGER CENTER LINE AND SKIN AT AIR PASSAGE

STGR BUTT LINE WATER LINESPACEALONG

CONTOUR

1 0.000 147.000 0.000

2 7.535 146.392 7.568

3 14.849 144.643 7.541

4 21.791 141.643 7.551

5 28.213 137.590 7.602

6 33.854 132.603 7.537

7 38.657 126.733 7.593

8 41.529 122.007 5.533

9 43.643 117.444 5.031

10 45.524 111.687 6.060

11 46.646 105.754 6.042

12 46.999 99.678 6.091

13 46.574 93.686 6.011

14 45.638 88.767 5.010

15 43.638 83.238 5.796

16 41.105 77.210 6.654

17 37.615 71.820 6.426

18 33.922 67.468 5.712

19 28.614 62.714 7.132

20 22.647 58.816 7.135

21 16.158 55.865 7.135

22 8.998 53.869 7.441

23 3.000 53.069 6.052

CL 0.000 53.000 0.000

NOTE: Stringers 1 - 13 remain constant section from FS 193 - FS 498.

Stringers 14 - 16, stringer 18 - 21 and stringer 23 remain constant section from FS 193 - FS321.5.

Stringers 17 and 22 remain constant section from FS 193 - FS 287.5.

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Stringer locations in fuselage constant sections only.

StringersFigure 2

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Table 2: Stringer Material

ITEM(1) PROCESS MATERIAL THICKNESS

A ALCLAD 2014-T6 0.025

B ALCLAD 2014-T6 0.032

C ALCLAD 2014-T6 0.040

D ALCLAD 2014-T6 0.050

E ALCLAD 2014-T6 0.063

F ALCLAD 2014-T6 0.071

G ALCLAD 2014-T6 0.0710.080

H ALCLAD 2014-T6 0.0500.080

I ALCLAD 2014-T60.0250.0500.080

J ALCLAD 2014-T60.0500.0710.100

K ALCLAD 2014-T6 0.063

L ALCLAD 2014-T42 0.040

M ALCLAD 2014-T42 0.071

N ALCLAD 2014-T42 0.025

O ALCLAD 2014-T42 0.0320.040

P AL. AL. EXTRUSION 2024-T35117075-T6511DIE No. 249910136-1702

Q AL. AL. EXTRUSION 2024-T3511 DIE No. 2499

R Contact Gulfstream Technical Operations for information.

S ALCLAD 2014-T6 0.0400.063

T ALCLAD 2014-T42 0.050

U ALCLAD 2014-T6 0.0320.040

V ALCLAD 7075-T6 0.050

W ALCLAD 7075-T6 0.040

X ALCLAD 2014-T6 0.080

Y ALCLAD 7075-T62 0.090

Z ALCLAD 7075-T6 0.063

(1) See Figure 3 for item location.

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Stringer SchematicFigure 3

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3. Pressure Bulkhead — Diagram, Illustration and Part Number Identification

A. Pressure Bulkhead

See Figure 4 for pressure bulkhead repair.

NOTE: For additional information and drawing numbers see 1159B31396 or contact GulfstreamTechnical Operations.

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Flat Pressure BulkheadFigure 4

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GIV STRUCTURAL REPAIR MANUALLIST OF EFFECTIVE PAGESTABLE OF CONTENTSINTRODUCTIONCHAPTER 51 STRUCTURES GENERALCHAPTER 52 DOORSCHAPTER 53 FUSELAGEList Of Effective PagesTable Of Contents53-00-01 FUSELAGE DIAGRAMSStructural IdentificationFuselage - Diagrams, Materials, Illustrations and Part Number IdentificationStringers - Diagrams, Materials, Illustrations and Part Number IdentificationPressure Bulkhead - Diagram, Illustration and Part Number Identification

53-00-02 FUSELAGE REPAIRS53-02-00 FUSELAGE ANTENNA INSTALLATIONS53-34-01 TORQUE BOX REPAIR

CHAPTER 54 NACELLES AND PYLONSCHAPTER 55 STABILIZERSCHAPTER 56 WINDOWSCHAPTER 57 WINGS