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SRM55-20-00 7.0.0.0ELEVATORS AND TABS - STRUCTURAL IDENTIFICATION

1. General

This section identifies the skin panels and structural components of the elevators, trim tabs and spring tabs. Details are given of: specific location; material specifications and related commercial designations; material thicknesses; limits of allowable damage; and approved repairs.

2. Construction

The elevators are of all metal construction consisting of a main and intermediate spar of full length with a leading edge spar broken at the hinge positions and a trailing edge spar broken in way of the tab horn. All spars are self flanged 2024-T42 material.

A 2024-T42 lipped angle stringer is located between the leading edge and main spars at both top and bottom surfaces.

Ribs are perpendicular to and intercostal with the spars and are self-flanged 2024-T42. Forward of the front spar the ribs have cut-outs to cater for the stringers.

Top, bottom and nose skins are chemi-etched 2024-T3 material with the nose skins housing the internal mass balance weights which extend over their entire length.

Fail safe 7075-T7351 tab hinge brackets are attached to the main spar.

The elevator tab is of similar construction to the rudder tab (Refer to 55-40-00, pb1.)

3. Structure Identification

The following pages contain diagrams and text to define the components, skin materials and thicknesses that comprise the Elevators and Tabs.

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Elevator structureFigure 1

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ITEM NO. MATERIAL THICKNESS/

GAUGE PART NO. DESCRIPTION

1 - - SD3-31-6039SD3-31-6040

ASSY L/E SPAR OUT/BD

2 - - SD3-31-6051SD3-31-6052

ASSY L/E SPAR CENTRE

3 - - SD3-31-6043SD3-31-6044

ASSY L/E SPAR IN/BD

4 - - SD3-31-6081 ASSY T/E SPAR IN/BD5 - - SD3-31-6077 ASSY T/E SPAR CENTRE6 - - SD3-31-6069 ASSY INTERMEDIATE SPAR7 - - SD3-31-6103

SD3-31-6104STRINGER ASSY IN/BD

8 - - SD3-31-6045SD3-31-6046

RIB ASSY IN/BD

9 - - SD3-31-6087 SUB SPAR RIB ASSY IN/BD10 - - SD3-31-6135

SD3-31-6136RIB ASSY OUT/BD

11 - - SD3-31-6115SD3-31-6116

ASSY HINGE RIB OUT/BD

12 - - SD3-31-6111SD3-31-6112

ASSY HINGE RIB IN/BD

13 - - SD3-31-6123SD3-31-6124

HINGE BRACKET ASSY

14 - - SD3-31-6179SD3-31-6180

SUPPORT RIB ASSY

15 - - SD3-31-6061SD3-31-6062

LANDING PLATE ASSY

16 - - SD3-31-6063SD3-31-6064

LANDING PLATE ASSY

17 - - SD3-31-6258 INTERMEDIATE RIB ASSY18 QQ-A-225/6

T35110.192" - WEDGE TRAILING EDGE

19 QQ-A-250/5 T42

0.032" - MAIN SPAR

20 QQ-A-250/5 T42

0.025" - SUB SPAR IN/BD

Key to Figure 1

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NOTE: Item 4 applies SH3601 thru SH3619 only.

Item 23 applies SH3620 & Subs.

21 QQ-A-250/5 T42

0.025" - RIB

22 QQ-A-250/5 T42

0.032" - RIB

23 - - SD3-31-6266 ASSY T/E SPAR IN/BD

ITEM NO. MATERIAL THICKNESS/

GAUGE PART NO. DESCRIPTION

Key to Figure 1

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Elevator SkinningFigure 2

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ITEM NO. MATERIAL THICKNESS/

GAUGE PART NO. DESCRIPTION

1 0.056" QQ-A-250/5 2024-T3

TOP SKIN

2 0.056" QQ-A-250/5 2024-T3

BOTTOM SKIN

3 0.056" QQ-A-250/5 2024-T3

NOSE L/EDGE SKIN

4 0.056" QQ-A-250/5 2024-T3

ACCESS PANEL

Key to Figure 2

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Elevator tabFigure 3

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ITEM NO. MATERIAL THICKNESS/

GAUGE PART NO. DESCRIPTION

1 - - SD3-31-6261SD3-31-6262

L/E ASSY - BONDED

2 QQ-A-250/5 2024-T3

0.012" - SKIN

3 QQ-A-250/5 2024-T42

0.040" - SPAR CHANNEL

4 AEROWEB A1-24-6

- - HONEYCOMB CORE

5 QQ-A-250/5 2024-T42

0.040" - LEADING EDGE

6 QQ-A-250/5 2024-T3

0.050" - REINFORCING STRIP

7 7075-T7351 - - ELEV. TAB DRIVE BKT.8 7075-T7351 - - ELEV. TAB MASTER HNG.9 7075-T7351 - - ELEV. TAB HINGE

10 QQ-A-250/5 2024-T42

0.025" - COVER BKT (BAL.WT)

11 QQ-A-250/5 2024-T42

0.016" - COVER BAL WEIGHT

12 G.E.C. HEAVY ALLOY

0.25" - BALANCE WEIGHT

13 L65 0.25" - BALANCE WEIGHT14 S.534 0.064" - BALANCE WEIGHT

Key to Figure 3

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SRM55-20-00 8.0.0.0ELEVATORS AND TABS - ALLOWABLE DAMAGE

1. General

The following pages define the allowable damage limitations for the aircraft Elevators and Tabs.

The limitations are given in tabular form as follows:

- Elevator Skin. Refer to Table 101.- Elevator Leading Edge Skin. Refer to Table 102.- Elevator Spar Web and Rib Web. Refer to Table 103.

Definitions of types of damage. Refer to 51-10-00, pb1.

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NOTE: ts = thickness of skintk = thickness of doubler

TYPE OF DAMAGE 'D' MAX. DEPTH

'L'LENGTH

MIN.EDGEDIST.

INCHES

MIN. DIM.FROM

LINES OF FASTENERS

OTHER LIMITATIONS REMEDIAL ACTION REQUIRED

Isolated Dents(1) Basic skin(2) Basic skin and doubler

1.50 x ts 1.50 x td

10D min.10D min.

1.00 1.00

1.001.00

Dents smooth and free of cracks.For skin with bonded doubler no delaminations allowed. No dents allowed in skin at rib stations, along spar flanges or on stringer.

If beyond limits, repair is required.

Gouges, nicks,scratches and surface corrosion.(1) Basic skin(2) Basic skin and doubler

0.10 x ts 0.10 x td

0.50 max. 0.50 max.

--

--

Must not extend over more than two adjacent fasteners, except where damage does not exceed depth of cladding.

Clean up damageRefer to 51-10-00, pb1.

If beyond limits, repair is required.

Punctures - - - - - Repair is required

Cracks - - - - - Repair is required.

Allowable damage - Elevator skinTable 101

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NOTE: tl = thickness of leading edge skin

TYPE OF DAMAGE 'D' MAX. DEPTH

'L'LENGTH

MIN.EDGEDIST.

INCHES

MIN. DIM.FROM

LINES OF FASTENERS

OTHER LIMITATIONS REMEDIAL ACTION REQUIRED

Isolated Dents 1.00 x tl 10D min. 1.00 1.00 Dents smooth and free from cracks.No dents allowed in skin at rib station or along spar flanges

If beyond limits, repair is required.

Gouges, nicks,scratches andsurface corrosion.

0.10 x tl 0.50 max. - - Must not extend over more than two adjacent fasteners, except where damage does not exceed depth of cladding.

Clean up damageRefer to 51-10-00, pb1.

If beyond limits, repair is required.

Punctures - - - - - Repair is required.

Cracks - - - - - Repair is required.

Allowable damage - Elevator leading edge skinTable 102

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NOTE: ts = thickness of skintr = thickness of rib.

TYPE OF DAMAGE 'D' MAX. DEPTH

'L'LENGTH

MIN.EDGEDIST.

INCHES

MIN. DIM. FROM

LINES OF FASTENERS

OTHER LIMITATIONS REMEDIAL ACTION REQUIRED

Isolated Dents.(1) Spar web(2) Rib web

1.50 x ts1.00 x tr

10D min. 10D min.

- 1.000.75

Dents smooth and free from cracks.

If beyond limits, repair is required.

Nicks, scratchessurface corrosionand abrasions.(1) Spar web(2) Rib web

0.10 x ts 0.10 x tr

0.50 max. 0.50 max.

--

--

Not to extend over more than two adjacent fasteners except where damage does not exceed depth of cladding.

Clean up damageRefer to 51-10-00, pb1.

If beyond limits, repair is required.

Punctures - - - - - Repair is required.

Cracks - - - - -(a)Radiating from lightening holes

(a) Repair.Refer to 51-70-00, pb1.

(b)Other cracks (b) Repair is required.

Allowable damage - Elevator spar web and rib webTable 103

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SRM55-20-00 9.0.0.0ELEVATOR AND TRIM TABS - REPAIRS

1. General

The following pages contain details of approved repairs to the elevator and trim tabs.

Reference must also be made to CHAPTER 51, for further information regarding structural damage and repair practices of a general nature.

It is to be noted that due to the similarity in construction of the Elevator to the Horizontal Stabiliser, some of the approved repairs are applicable to both assemblies.

CAUTION: THESE REPAIRS MAY AFFECT THE FATIGUE CRITICAL BASELINE STRUCTURE.REFER TO 51-00-01 FOR FURTHER INFORMATION ON FCBS AND PROCEDURES TO BE FOLLOWED, PRIOR TO INCORPORATING ANY OF THESE REPAIRS.

2. List of approved repairs for Elevators and Trim Tabs

Skin Repairs - Patches. Refer to 55-10-00, Figure 201.

Skin Repair. Refer to 55-10-00, Figure 202.

Stringer Repairs. Refer to 55-10-00, Figure 203.

Trailing Edge Repairs. Refer to 55-10-00, Figure 204.

Typical Rib Repairs. Refer to 55-10-00, Figure 205.

Leading Edge Repair. Refer to 55-10-00, Figure 206.

Replacement of Elevator Tab Inbd Hinge Bracket, and Hinge Bearing Sub Assembly. Refer to Figure 201.

- Alternative fasteners. Refer to 51-40-00, pb1.- Alternative Materials. Refer to 51-31-00, pb1.

Information regarding the repainting of the aircraft following repairs to the structure. Refer to 51-23-00, pb1.

CAUTION: REPAINTING OF CONTROL SURFACES MAY IN SOME CASES NECESSITATE REBALANCING. REFER TO 55-20-10, PB1.

As a guide, light sanding prior to a single spray coat would not require surfaces to be rebalanced. Overspraying or additional spraying will require balance to be verified.

Feb 01/10

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Replacement of Elevator Tab Inbd Hinge Bracket & Hinge Bearing Sub AssyFigure 201

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SRM55-20-00 10.0.0.0ELEVATOR AND ELEVATOR TAB - INSPECTION/CHECK

1. Check wear limits at hinge points

Tabulated data of in-service wear limits for the elevator and elevator tab hinge points are presented as follows:

- Elevator inboard hinge. Refer to Figure 601.- Elevator outboard Hinge. Refer to Figure 602.- Elevator tab outboard hinge. Refer to Figure 603 (Sheet 1).- Elevator tab inboard hinge. Refer to Figure 604 (Sheet 1).

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Elevator Inboard HingeFigure 601

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FIG.601REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

A

OD 1

ID 2

0.4985(12.6619)

0.5120(13.0048)

0.4995(12.6873)

0.5280(13.4112)

0.0125(0.3175)

0.0295(0.7493)

B

OD 3

ID 4

0.9359(23.7719)

0.9375(23.8125)

0.9367(23.7922)

0.9383(23.8328)

0.0008(0.0203)

0.0024(0.0610)

0.9351(23.7515)

0.9375(23.8125)

0.9367(23.7922)

0.9391(23.8531)

0.0040 (0.1016)

C

OD4

ID 5

1.0639(27.0231)

1.0625(26.9875)

1.0647(27.0434)

1.0637(27.0180)

-0.0022(-0.0559)

-0.0002(-0.0051)

D

OD 2

ID 3

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7510(19.0754)

0.0020 (0.0508)

E

OD 2

ID 7

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7485(19.0119)

0.7495(19.0373)

0.7495(19.0373)

0.7505(19.0627)

0.0020 (0.0508)

F

OD 7

ID 6

1.8745(47.6123)

1.8736(47.5894)

1.8750(47.6250)

1.8742(47.6047)

-0.0014(-0.0356)

-0.0003(-0.0076)

G

OD 2

ID 10

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7485(19.0119)

0.7495(19.0373)

0.7495(19.0373)

0.7505(19.0627)

0.0020 (0.0508)

Elevator Inboard Hinge, Table of Fits and ClearancesTable 601 (Sheet 1)

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H

OD 10

ID 9

0.9359(23.7719)

0.9375(23.8125)

0.9367(23.7922)

0.9383(23.8328)

0.0008(0.0203)

0.0024(0.0610)

0.9351(23.7515)

0.9375(23.8125)

0.9367(23.7922)

0.9391(23.8531)

0.0040 (0.1016)

J

OD 9

ID 8

1.0639(27.0231)

1.0625(26.9875)

1.0647(27.0434)

1.0637(27.0180)

-0.0022(-0.0559)

-0.0002(-0.0051)

FIG.601REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

Elevator Inboard Hinge, Table of Fits and ClearancesTable 601 (Sheet 1) (Continued)

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Elevator Outboard HingeFigure 602

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FIG.602REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

A

OD 1

ID 2

0.4985(12.6619)

0.5120(13.0048)

0.4995(12.6873)

0.5280(13.4112)

0.0125(0.3175)

0.0295(0.7493)

B

OD 3

ID 4

0.9359(23.7719)

0.9375(23.8125)

0.9367(23.7922)

0.9383(23.8328)

0.0008(0.0203)

0.0024(0.0610)

0.9350(23.7490)

0.9375(23.8125)

0.9367(23.7922)

0.9391(23.8531)

0.0040 (0.1016)

C

OD4

ID 5

1.0639(27.0231)

1.0625(26.9875)

1.0647(27.0434)

1.0637(27.0180)

-0.0022(-0.0559)

-0.0002(-0.0051)

D

OD 2

ID 3

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7485(19.0119)

0.7495(19.0373)

0.7495(19.0373)

0.7505(19.0627)

0.0020 (0.0508)

E

OD 2

ID 7

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7485(19.0119)

0.7495(19.0373)

0.7495(19.0373)

0.7505(19.0627)

0.0020 (0.0508)

F

OD 7

ID 6

1.8745(47.6123)

1.8736(47.5894)

1.8750(47.6250)

1.8742(47.6047)

-0.0014(-0.0356)

-0.0003(-0.0076)

G

OD 2

ID 10

0.7490(19.0246)

0.7495(19.0373)

0.7495(19.0373)

0.7500(19.0500)

0.0000(0.0000)

0.0010(0.0254)

0.7485(19.0119)

0.7495(19.0373)

0.7495(19.0373)

0.7505(19.0627)

0.0020 (0.0508)

Elevator Outboard Hinge, Table of Fits and ClearancesTable 602

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H

OD 10

ID 9

0.9359(23.7719)

0.9375(23.8125)

0.9367(23.7922)

0.9383(23.8328)

0.0008(0.0203)

0.0024(0.0610)

0.9350(23.7490)

0.9375(23.8125)

0.9367(23.7922)

0.9390(23.8506)

0.0040 (0.1016)

J

OD 9

ID 8

1.0639(27.0231)

1.0625(26.9875)

1.0647(27.0434)

1.0637(27.0180)

-0.0022(-0.0559)

-0.0002(-0.0051)

FIG.602REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

Elevator Outboard Hinge, Table of Fits and ClearancesTable 602 (Continued)

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Elevator Tab Outboard HingeFigure 603 (Sheet 1)

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FIG.603REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

A

OD2

ID 5

0.3737(9.4920)

0.3750(9.5250)

0.3744(9.5098)

0.3759(9.5479)

0.0006(0.0152)

0.0022(0.0559)

0.3737(9.4920)

0.3750(9.5250)

0.3744(9.5098)

0.3759(9.5479)

0.0022(0.0559)

B

OD 1

ID 2

02485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005 (0.0127)

0.0024 (0.0610)

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0024(0.0610)

C

OD4

ID 3

0.6557(16.6548)

0.6550(16.6370)

0.6562(16.6675)

0.6555(16.6497)

-0.0012(-0.0305)

-0.0002(-0.0051)

D

OD 1

ID 4

0.2485(6.3119)

0.2495(6.3373)

0.2495(6.3373)

0.2500(6.3500)

0.0000 (0.0000)

0.0015 (0.0381)

0.2485(6.3119)

0.2495(6.3373)

0.2495(6.3373)

0.2500(6.3500)

0.0015(0.0381)

E

OD 1

ID 6

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005 (0.0127)

0.0024 (0.0610)

0.2485(6.3119)0.2500

(6.3500)

0.2495(6.3373)0.2509

(6.3729)

0.0024(0.0610)

F

OD 1

ID 5

02485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005 (0.0127)

0.0024 (0.0610)

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0024(0.0610)

Elevator Tab Outboard Hinge, Table of Fits and Wear LimitsTable 603

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Elevator Tab Inboard HingeFigure 604 (Sheet 1)

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FIG.604REF.LTR

ITEMNo.

ORIGINAL MANUFACTURING LIMITS IN-SERVICE WEAR LIMITS

DIMENSION lnches

(Millimetres)

ASSEMBLYCLEARANCES

Inches(Millimetres)

DIMENSION LIMITS Inches

(Millimetres)

MAX. ALLOW.

CLEAR�CE Inches

(mm) MIN. MAX. MIN. MAX. MIN. MAX.

A

OD 6

ID 2

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005(0.0127)

0.0024(0.0610)

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0024(0.0610)

B

OD 6

ID 1

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005(0.0127)

0.0024(0.0610)

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0024 (0.0610)

C

OD 6

ID 3

0.2485(6.3119)

0.2495(6.3373)

0.2495(6.3373)

0.2500(6.3500)

0.0000(0.0000)

0.0015(0.0381)

0.2485(6.3119)

0.2495(6.3373)

0.2495(6.3373)

0.2500(6.3500)

0.0015 (0.0381)

D

OD3

ID 4

0.6557(16.6548)

0.6550(16.6370)

0.6562(16.6675)

0.6555(16.6497)

-0.0012(-0.0305)

-0.0002(-0.0051)

E

OD 6

ID 5

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0005(0.0127)

0.0024(0.0610)

0.2485(6.3119)

0.2500(6.3500)

0.2495(6.3373)

0.2509(6.3729)

0.0024 (0.0610)

F

OD 5

ID 2

0.3737(9.4920)

0.3750(9.5250)

0.3744(9.5098)

0.3759(9.5479)

0.0006(0.0152)

0.0022(0.0559)

0.3737(9.4920)

0.3750(9.5250)

0.3744(9.5098)

0.3759(9.5479)

0.0022 (0.0559)