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A 320 SRM 51-21-11 APLICATION OF PROTECTIVE TREATMENT TO METAL PARTS

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Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

1. General<br />

A. The following sections detail the necessary treatments for metal repair parts. The required paint coatings<br />

are given in Chapter <strong>51</strong>-23-<strong>11</strong> .<br />

B. The Table Below shows the original protection and choice of alternative solutions for field repairs only.<br />

NOTE: This table does not cover major part replacement.<br />

NOTE: CAA protection is recommended, especially in areas subject to corrosion, nevertheless chemical<br />

conversion coating or wash primer is acceptable although the level of protection is degraded<br />

versus CAA.<br />

MATERIAL<br />

Aluminum<br />

ORIGINAL PROTEC-<br />

TION FOR DETACH-<br />

ABLE REPAIR <strong>PARTS</strong><br />

<br />

REPAIR ALTERNAT-<br />

IVES<br />

General surface protection for corrosion prevention<br />

CAA unsealed + paint Chemical conversion<br />

<br />

coating + paint or wash<br />

Chemical conversion primer + paint <br />

coating + paint<br />

SAA unsealed + paint <br />

For surface protection of bonded repairs<br />

Hydrofluoric acid etching,<br />

Chemical conversion<br />

coating and Anti-corrosion<br />

Repair procedure<br />

calls for CAA Chapter<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> 2.A.(1) or<br />

TASK <strong>51</strong>-77-13-9<strong>11</strong>-013 ,<br />

Para 2. B. (2) (a)<br />

bonding primer method<br />

Acid etching and anti-corrosion<br />

bonding primer<br />

method<br />

Phosphoric acid non tank<br />

anodizing (PANTA) and<br />

anti-corrosion bonding<br />

primer method<br />

PARAGRAPH<br />

2.A<br />

TASK <strong>51</strong>-77-13-9<strong>11</strong>-013 ,<br />

Para 2. A. (2). (c)<br />

TASK <strong>51</strong>-77-13-9<strong>11</strong>-013 ,<br />

Para 2. A. (2). (d)<br />

TASK <strong>51</strong>-77-13-9<strong>11</strong>-013 ,<br />

Para 2. A. (2). (e)<br />

Table 001 - Protective Treatments on Aluminum<br />

If the required treatments are not practicable, refer to the column 'Repair Alternative'. Use the<br />

abbreviation 'CAA' for Chromic Acid Anodizing and 'SAA' for Sulfuric Acid Anodizing.<br />

Anodic coating is considered to be the superior protection.<br />

The application of wash primer is preferred in those areas that would be difficult to clean after the<br />

application of chemical conversion coating. This would prevent a chemical product being trapped between<br />

parts and subsequently causing corrosion.<br />

MATERIAL<br />

STEEL<br />

ORIGINAL PROTEC-<br />

TION FOR DETACH-<br />

ABLE REPAIR <strong>PARTS</strong><br />

<br />

Cadmium plating<br />

Cadmium plating + paint<br />

REPAIR ALTERNAT-<br />

IVES <br />

Brush cadmium plating<br />

Brush cadmium plating<br />

plus paint (primer<br />

PARAGRAPH<br />

2.B<br />

Print Date: December 29, 2016 Page 1 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

MATERIAL<br />

ORIGINAL PROTEC-<br />

TION FOR DETACH-<br />

ABLE REPAIR <strong>PARTS</strong><br />

<br />

Phosphating + paint<br />

Zinc spraying<br />

Silver plating<br />

Chrome plating<br />

REPAIR ALTERNAT-<br />

IVES <br />

or primer + top coat), or<br />

wash primer + primer +<br />

top coat if required.<br />

Phosphating or wash<br />

primer + paint<br />

Wash primer + paint<br />

None<br />

None<br />

PARAGRAPH<br />

Table 002 - Protective Treatments on Steel<br />

If the required treatments are not practicable, refer to the column 'Repair Alternative'. Use the<br />

abbreviation 'CAA' for Chromic Acid Anodizing and 'SAA' for Sulfuric Acid Anodizing.<br />

The repair alternatives in Table 002 are not allowed for bonded structure.<br />

MATERIAL<br />

Titanium<br />

ORIGINAL PROTEC-<br />

TION FOR DETACH-<br />

ABLE REPAIR <strong>PARTS</strong><br />

Anodizing<br />

Cadmium plating<br />

Nickel plating<br />

APPLICATION IN SITU<br />

PARAGRAPH<br />

not applicable 2.C<br />

2. Procedure<br />

Table 003 - Protective Treatments on Titanium<br />

A. Aluminum<br />

WARNING: BE CAREFUL WHEN YOU USE CHEMICAL MATERIALS. OBEY THE MATERIAL MAN-<br />

UFACTURER INSTRUCTIONS AND THE LOCAL REGULATIONS. MAKE SURE THAT<br />

THERE IS A GOOD FLOW <strong>OF</strong> AIR THROUGH THE WORK AREA. DO NOT BREATHE<br />

THE FUMES. DO NOT SMOKE. DO NOT USE THESE MATERIALS NEAR A FLAME,<br />

SPARKS OR SOURCES <strong>OF</strong> HEAT. USE <strong>PROTECTIVE</strong> CLOTHING, GOGGLES AND<br />

GLOVES. IF YOU GET ONE <strong>OF</strong> THESE MATERIALS ON YOUR SKIN OR IN YOUR<br />

EYES, FLUSH IT AWAY WITH A FLOW <strong>OF</strong> CLEAN WATER. IF YOU GET ONE <strong>OF</strong><br />

THESE MATERIALS IN YOUR MOUTH, GET IMMEDIATE MEDICAL AID. IN GENERAL,<br />

THESE MATERIALS ARE FLAMMABLE, POISONOUS AND SKIN IRRITATING.<br />

WARNING: PUT ON <strong>PROTECTIVE</strong> CLOTHING. ALL CHEMICAL COMPONENTS CAN CAUSE SKIN,<br />

EYE AND LUNG DAMAGE.<br />

(1). Chromic Acid Anodizing and Sulfuric Acid Anodizing (CAA, SAA, unsealed)<br />

(a) General<br />

1 CAA and SAA are galvanic procedures in which the surface of metal is given an oxide<br />

coating. The treatment increases the corrosion resistance of the material and gives a good<br />

surface for the adhesion of subsequent paint coatings.<br />

2 Make sure that subsequent paint coatings, if required, are applied within 16 hours after this<br />

treatment.<br />

(b) Safety Precautions<br />

Print Date: December 29, 2016 Page 2 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER’S INSTRUCTIONS FOR THE MATERIALS WHICH<br />

YOU USE FOR THE CLEANING PROCEDURES BEFORE YOU START WITH THE<br />

CAA PROCESS. THESE CLEANING AGENTS ARE DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. THESE CHEMICALS ARE POISONOUS AND DANGER-<br />

OUS.<br />

(c) Procedure<br />

1 For details of the CAA process and the necessary equipment refer to the PMS Chapter<br />

01-02-08 .<br />

2 For details of the SAA process and the necessary equipment refer to the PMS Chapter<br />

01-02-09 .<br />

(2). Application of Chemical Conversion Coating<br />

CAUTION:<br />

MAKE SURE THAT YOU REMOVE ALL MASKING MATERIAL FROM THE REPAIR<br />

AREA WHEN THE WORK IS COMPLETED. IT IS VERY IMPORTANT <strong>TO</strong> MAKE<br />

SURE THAT THERE IS NO MASKING MATERIAL ON THE PI<strong>TO</strong>T HEADS AND<br />

STATIC PORTS.<br />

(a) General<br />

1 The application of the product (Material No. 13-002 ), described in Paragraph 2.A.(2).(d) , is<br />

a non electrolytic process. It produces a protective coating and gives a good surface for the<br />

adhesion of the subsequent paint coatings. The product can be applied by brush, swab and<br />

immersion procedure. Brush application is suitable to field repairs.<br />

The use of ALODINE PEN <strong>11</strong>32 (Material No. 13-005 ) is a non electrolytic process driedin-place<br />

coating. It can be used as an alternative to pretreatment for painting (Material No.<br />

13-002 ) for small touch up repairs not exceeding 20000 mm² (31 in²), refer to Paragraph<br />

2.A.(2).(e) .<br />

2 Before you start with this procedure, make sure that the surface shows bright metal.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER’S INSTRUCTIONS WHEN YOU USE THE CLEANING<br />

AGENTS (MATERIAL NO. <strong>11</strong>-003 AND <strong>11</strong>-026). THESE CLEANING AGENTS ARE<br />

DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS WHEN YOU USE CHEMICAL CON-<br />

VERSION COATING (MATERIAL NO. 13-002). THIS PRODUCT IS POISONOUS.<br />

CAUTION:<br />

ENSURE THAT ALL MASKING MATERIALS ARE REMOVED FROM THE REPAIR<br />

AREA ON COMPLETION <strong>OF</strong> WORK, PAY SPECIAL ATTENTION <strong>TO</strong> PI<strong>TO</strong>T HEADS<br />

AND STATIC PORTS.<br />

(c) Materials<br />

Print Date: December 29, 2016 Page 3 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

- Cleaning agent - Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

2 ALODINE 1200 or ALOCROME - Material No. 13-002 (Refer to CML)<br />

1200<br />

3 Concentrated nitric acid -<br />

4 Containers - Stainless steel or acid-resistant material<br />

5 Masking tape -<br />

6 Cotton cloth -<br />

7 Soft-bristle brushes - Fiber-bristled or nylon<br />

8 Hot-air dryer -<br />

9 SCOTCH-BRITE pads -<br />

- ALODINE 1000 or 1500 - Material No. 13-003 (Refer to CML)<br />

- ALODINE PEN <strong>11</strong>32 - Material No. 13-005 (Refer to CML)<br />

- SCOTCH-BRITE pads Type A fine - Local purchase<br />

(d) Application of Chemical Conversion Coating by Brushing<br />

1 Preparation of Brush Solution<br />

NOTE: Use either Material No. 13-002 (CCC yellow) or 13-003 (CCC colorless) in accordance<br />

with the areas to be repaired.<br />

Use pretreatment for painting (Material No. 13-003 ) on:<br />

- unpainted parts<br />

- non-painted area around static ports<br />

- parts where electrical bonding is required<br />

- when required in specific repair procedure<br />

a<br />

Mix the powder (Material No. 13-002 or 13-003 )) with deionized water in a plastic or<br />

stainless steel container at room temperature.<br />

NOTE: Use the applicable proportions as follows:<br />

Material No. 13-002 (ALODINE 1200 or ALOCROME 1200) The proportion to<br />

mix is 22 to 30 g in 1 liter of demineralized water. Contact time is 3 to 5 minutes.<br />

Material No. 13-003 (ALODINE 1000 or 15000) The proportion to mix is:<br />

For ALODINE 1500 10 to <strong>11</strong> g in 1 liter of demineralized water. Contact time is 1<br />

to 3 minutes.<br />

For ALODINE 1000 3 to 3.8 g in 1 liter of demineralized water. Contact time is 2<br />

to 5 minutes.<br />

NOTE: Refer to Chapter 01-01-18 for the definition of demineralized water.<br />

b<br />

Allow the solution to stand for a minimum of 1 hour before use.<br />

NOTE: You can disregard small amounts of insoluble material which may appear.<br />

2 Preparation Prior to Application<br />

a<br />

Mask all surfaces so that no solution can pass into adjacent splices, seams or voids.<br />

NOTE: Surfaces which are painted, anodized or have been previously treated with the<br />

product (Material No. 13-002 or 13-003 ) need not to be masked.<br />

b<br />

Abrade the surface to be treated with SCOTCH-BRITE pads.<br />

Print Date: December 29, 2016 Page 4 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

c Clean the area with a clean cotton cloth soaked in cleaning agent (Material No. <strong>11</strong>-003<br />

or <strong>11</strong>-026 ).<br />

3 Application<br />

WARNING: MATERIALS SOAKED IN CHEMICAL CONVERSION SOLUTION (MATERI-<br />

AL NO. 13-002) CONSTITUTE A FIRE HAZARD.<br />

a<br />

Apply the solution onto the surface of the metal with a brush or lint-free cloth or by<br />

immersion procedure. Keep the surface moist by successive applications until a golden<br />

yellow film is obtained for Material No. 13-002 or an iridescent film is obtained for<br />

Material No. 13-003 . Darker powdery deposits will result in poor paint adhesion.<br />

CAUTION:<br />

CAUTION:<br />

DO NOT ALLOW THE APPLIED FILM <strong>TO</strong> BECOME DRY BEFORE IT IS<br />

RINSED WITH WATER.<br />

WHEN YOU RINSE AND DRY THE S<strong>OF</strong>T NEW COATING, EXERCISE CARE<br />

NOT <strong>TO</strong> DAMAGE THE FILM.<br />

b<br />

c<br />

d<br />

CAUTION:<br />

Rinse the area thoroughly with demineralized running clean water (minimum 2 minutes).<br />

Dry off the area with hot (maximum 60° C (140° F)), oil free low-pressure air.<br />

Apply the required paint coatings as soon as possible but within 16 hours (Refer to<br />

Chapter <strong>51</strong>-23-<strong>11</strong> ).<br />

WEAR <strong>PROTECTIVE</strong> EQUIPMENT AND OBEY MANUFACTURER’S INSTRUCTIONS.<br />

(e) Application of Chemical Conversion by Pen<br />

NOTE: The use of ALODINE PEN <strong>11</strong>32 (Material No. 13-005 ) is a non-electrolytic process driedin-place<br />

coating. It can be used as an alternative to pretreatment for painting (Material<br />

No. 13-002 ) for small touch-up repairs not exceeding 20000 mm² (31 in²).<br />

1 Preparation prior to application<br />

a<br />

b<br />

Mask all the surfaces so that no solution can pass into adjacent splices, seams or voids.<br />

NOTE: Anodized areas or areas already treated with ALODINE PEN <strong>11</strong>32 (Material No.<br />

13-005 ) need not to be masked.<br />

Abrade the surface to be treated with SCOTCH-BRITE pads.<br />

c Clean the area with a clean cotton cloth soaked in cleaning agent (Material No. <strong>11</strong>-003<br />

or <strong>11</strong>-026 ).<br />

d<br />

2 Application<br />

a<br />

b<br />

Dry the surface.<br />

Activation of the pen<br />

Remove the cap, hold the pen with the felt tip downwards. Press the tip of the pen<br />

against a cotton cloth. This will open the valve, allowing ALODINE <strong>11</strong>32 to reach the<br />

application tip. A new unit should charge in 30 to 45 seconds. When the ALODINE wets<br />

the tip and the cotton cloth, release pressure. Unit is ready to use. The tip shall be not<br />

excessively wet prior to its use.<br />

Apply ALODINE <strong>11</strong>32 to the part with firm, smooth, even and continues strokes. Overlap<br />

each stroke by 50% to ensure full coverage.<br />

Print Date: December 29, 2016 Page 5 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

NOTE: Do not allow the solution to puddle. If it is the case, it will burn the surface and<br />

adhesion loss can occur.<br />

Do not use too much solution. Just wet the surface and the solution should not<br />

run, if the surface is held vertical.<br />

It is recommended that the application start and stop just outside the bare aluminum<br />

area.<br />

Do not rinse. Do not wipe.<br />

No solution breaks must be observed, repeat Paragraph 2.A.(2).(e).1 if solution<br />

breaks.<br />

c<br />

d<br />

Let it dry for 5 minutes and apply a second coat in 90° direction as described in<br />

Paragraph 2.A.(2).(e).2.b .<br />

Let it dry for 1 hour at ambient temperature.<br />

NOTE: Light brown color is acceptable. Color shades, lines or overlap marks are acceptable.<br />

e<br />

Apply the required primer within 4 hours maximum.<br />

NOTE: Replace the cap after use. To recharge the pen, repeat the activation process.<br />

Store the pens head up to avoid leaks.<br />

(3). Application of Wash Primer (Material No. 16-020 )<br />

(a) General<br />

1 The application of wash primer (Material No. 16-020 ) is a chemical pretreatment to increase<br />

the corrosion resistant properties of the metal and to give a good surface for the adhesion of<br />

further paint coatings.<br />

2 Wash primer (Material No. 16-020 ) is composed of a polyvinylbutyral basis and a hardener.<br />

The product must usually be thinned by a thinner to the appropriate viscosity for spray or<br />

brush application.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER’S INSTRUCTIONS WHEN YOU USE THE CLEANING<br />

AGENTS (MATERIAL NO. <strong>11</strong>-003 AND <strong>11</strong>-026). THESE CLEANING AGENTS ARE<br />

DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS WHEN YOU PREPARE AND APPLY<br />

WASH PRIMER (MATERIAL NO. 16-020). DO NOT LET ANY MATERIAL COME IN<br />

CONTACT WITH THE SKIN, EYES OR MOUTH. DO NOT INHALE VAPORS. WORK<br />

IN WELL VENTILATED AREA.<br />

CAUTION:<br />

ENSURE THAT ALL MASKING MATERIALS ARE REMOVED FROM THE REPAIR<br />

AREA ON COMPLETION <strong>OF</strong> WORK, PAY SPECIAL ATTENTION <strong>TO</strong> PI<strong>TO</strong>T HEADS<br />

AND STATIC PORTS.<br />

(c) Materials<br />

Print Date: December 29, 2016 Page 6 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 Cleaning agent - Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

2 Wash primer - Material No. 16-020 (Refer to CML)<br />

3 Application tool - According to manufacturer's instructions<br />

4 Masking tape and paper -<br />

5 Cotton cloth -<br />

B. Steel Alloys<br />

(d) Procedure<br />

1 Mask off the area, which is not to be treated, with masking tape and paper.<br />

2 Clean the area with a cotton cloth, soaked in cleaning agent (Material No. <strong>11</strong>-003 or<br />

<strong>11</strong>-026 ).<br />

NOTE: Make sure that the area shows a bright metal surface.<br />

3 Mix the wash primer solution according to the material manufacturer's instructions.<br />

4 Apply wash primer (Material No. 16-020 ) according to the material manufacturer's<br />

instructions.<br />

(1). Cadmium Plating<br />

(a) General<br />

NOTE: After application subsequent paint coatings must be applied within a period of<br />

16 hours. For the determination of the required paint coatings refer to Chapter<br />

<strong>51</strong>-23-<strong>11</strong> .<br />

1 Cadmium plating is a procedure in which the surface of the material is given a layer of<br />

cadmium. If corrosion occurs it will remove the thin layer first. This is referred to as sacrificial<br />

corrosion.<br />

2 There are two different procedures used to put the cadmium onto the surface of the material.<br />

The first method describes a cadmium plating procedure, in which the metal parts are put<br />

into several immersion baths. The second method describes the 'DALIC' Process, which is<br />

suitable for field repairs.<br />

3 Before you start the cadmium plating procedure, make sure that the parts are clean, show a<br />

bright metal surface and are free from corrosion (Refer to Chapter <strong>51</strong>-74-00 ).<br />

4 It is recommended that cadmium plating is carried out by trained and approved personnel.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH MATERIAL WHICH YOU<br />

USE FOR CLEANING PROCEDURES BEFORE YOU START THE CADMIUM PLAT-<br />

ING. THESE CLEANING AGENTS ARE HARMFUL.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. THESE CHEMICALS ARE POISONOUS AND HARM-<br />

FUL.<br />

Print Date: December 29, 2016 Page 7 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

(c) Cadmium Plating (Immersion Procedure)<br />

1 For details of this cadmium-plating procedure and the necessary equipment refer to PMS<br />

Chapter 01-02-02 .<br />

(d) Cadmium Plating ('DALIC' Process) for steel with a maximum tensile strength of <strong>11</strong>00 N/mm ²<br />

(159 KSI).<br />

NOTE: Alternative procedures given in Paragraph 2.B.(1).(e) for steels and in Paragraph 2.B.(1).<br />

(f) for stainless steels.<br />

1 Materials and Equipment<br />

Contact AIRBUS to obtain the reference source for the 'DALIC' materials.<br />

NOTE: For the power supply you need a 'DALIC' rectifier. Dishes for the solutions must be<br />

made out of glass, polythene or porcelain material. For electrodes use 'DALIC' tampons<br />

which have to be prepared in accordance with the material manufacturer's instructions.<br />

2 Subsidiary Materials<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 'DALIC' cleaning and deoxidizing -<br />

solution<br />

2 'DALIC' cadmium/zinc passivating<br />

-<br />

solution<br />

3 Trichloroethane - Material No. <strong>11</strong>-026 (Refer to CML)<br />

4 Lint-free cloth -<br />

5 'DALIC' membrane -<br />

6 Masking tape -<br />

7 Brush or swab -<br />

8 Hot-air dryer -<br />

9 'DALIC' cadmium alkaline solution<br />

-<br />

10 'DALIC' cadmium acid solution - For all materials refer to the 'DALIC' instruction<br />

manual<br />

<strong>11</strong> 'DALIC' nickel epais solution -<br />

12 'DALIC' etch/activator solution -<br />

Number 4<br />

13 'DALIC' etch/activator solution -<br />

Number 3<br />

14 Aluminum oxide powder or<br />

Scotch-brite pads<br />

-<br />

3 How to Obtain the Correct Thickness<br />

The thickness of the deposited metal is controlled by the ampere-hour meter. It further<br />

depends upon the area to be plated and the specific plating factor. The specific plating factor<br />

gives the number of ampere hours required to produce a deposit in mm or inches onto a<br />

surface area of square centimeters or square inches.<br />

SOLUTION<br />

FAC<strong>TO</strong>R WHEN YOU FAC<strong>TO</strong>R WHEN YOU<br />

MEASURE IN (mm or cm) MEASURE IN (in)<br />

Nickel epais solution 1.282 <strong>21</strong>0<br />

Print Date: December 29, 2016 Page 8 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

SOLUTION<br />

FAC<strong>TO</strong>R WHEN YOU<br />

MEASURE IN (mm or cm)<br />

FAC<strong>TO</strong>R WHEN YOU<br />

MEASURE IN (in)<br />

Cadmium alkaline solution 0.488 80<br />

Cadmium acid solution 0.488 80<br />

Table 004 - Specific Plating Factor<br />

- Example: You have to plate an area of 25 cm² (3.875 in²) with cadmium alkaline solution.<br />

The required thickness is 0.015 mm. The correct ampere-hours setting is: 0.488 x 0.015 x<br />

25 = 0.183 ampere-hours<br />

- Example: You have to plate the same area with the same thickness, but you measure in<br />

inches. The thickness is 0.0006 in and the area has the size of 3.87 sq.in Determine the<br />

correct number of ampere-hours as follows: 80 x 0.0006 x 3.87 = 0.183 ampere-hours<br />

4 Inspection<br />

The cadmium deposit must be fine grain, smooth, and free from blisters, pitting, burns and<br />

other defects. Ensure that the cadmium deposit has good adherence to the metal surface.<br />

Check this with an adhesive tape. Put a strip of adhesive tape onto the treated surface and<br />

draw it quickly away. The adhesive tape must be free from cadmium particles.<br />

5 Procedure for non stainless steel<br />

a<br />

b<br />

Remove all grease from the repair area with a clean cloth soaked in trichloroethane<br />

(Material No. <strong>11</strong>-026 ).<br />

When the cleaning agent has evaporated, mask off all areas which are not to be treated.<br />

WARNING: CLEANING AND DEOXIDIZING SOLUTION IS HARMFUL.<br />

c<br />

d<br />

With a prepared tampon apply the cleaning and deoxidizing solution (Item 1 in the<br />

Table of Subsidiary Materials). Do this at cathodic plating polarity (see manufacturer's<br />

instructions) and 10 to 12 volts. Move the tampon in contact and over the surface until<br />

you get a regular clean surface which is free from water breaks. This should take about 5<br />

to 10 seconds per square inch (6.5 cm² (1.007 in²)).<br />

Rinse the area with clean cold running water.<br />

WARNING: CADMIUM ALKALINE SOLUTION IS DANGEROUS.<br />

e<br />

With a prepared tampon apply the cadmium alkaline solution (Item 9 in the Table of<br />

Subsidiary Materials). Do this at cathodic plating polarity and 8 to 12 volts. Move the<br />

tampon in contact with and over the surface until you get the required thickness. You<br />

should move the tampon at a speed of approximately 10 to 38 cm (4 to 15 in) per<br />

second.<br />

NOTE: For unspecified thickness, the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(d).3 .<br />

f<br />

g<br />

Rinse the area with clean cold running water.<br />

Abrade slightly the treated surface with a Scotch-brite pad or aluminum oxide and<br />

cotton wool. It will brighten the cadmium deposit before passivation and improve its<br />

appearance.<br />

WARNING: CADMIUM/ZINC PASSIVATING SOLUTION IS HARMFUL.<br />

Print Date: December 29, 2016 Page 9 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

h<br />

i<br />

Apply passivation solution (Item 2 in the Table of Subsidiary Materials) with a brush or<br />

swab to the plated surface. Allow the solution to remain in contact for 5 to 10 seconds<br />

until a yellow or gold appearance is obtained.<br />

Rinse the area with clean cold running water.<br />

CAUTION:<br />

THE PASSIVATED FILM IS RELATIVELY FRAGILE UNTIL DRY. AVOID<br />

<strong>TO</strong>UCHING IT BEFORE THE RELEVANT STEP IS COMPLETED.<br />

j<br />

Dry the repair area with a hot-air dryer at a maximum temperature of 50° C (122° F).<br />

NOTE: If step 2.B.(1).(d).5.j is impracticable, rinse with hot water to aid drying and<br />

gently dab the surface with soft clean tissues or clean cotton wool until the surface<br />

is dry.<br />

k Inspect the treated area as described in Paragraph 2.B.(1).(d).4 .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

6 Procedure for Stainless Steel<br />

a Do the steps 2.B.(1).(d).5.a to 2.B.(1).(d).5.d .<br />

WARNING: ETCH/ACTIVA<strong>TO</strong>R SOLUTION NUMBER 4 IS HARMFUL.<br />

b<br />

c<br />

With a prepared tampon apply the etching solution (Item 12 in the Table of Subsidiary<br />

Materials). Do this at a reversed polarity (anodically, see manufacturer's instructions)<br />

and 10 to 14 volts. Move the tampon in contact with and over the complete surface<br />

concerned. Continue until an evenly etched and smutted appearance is obtained.<br />

Rinse the area with clean cold running water.<br />

WARNING: ETCH/ACTIVA<strong>TO</strong>R SOLUTION NUMBER 3 IS HARMFUL.<br />

d<br />

e<br />

With a prepared tampon apply the etching solution (Item 13 in the Table of Subsidiary<br />

Materials). Do this at a reversed polarity (anodically, see manufacturer's instructions)<br />

and 10 to 12 volts. Move the tampon in contact with and over the complete surface<br />

concerned until the surface will not lighten further.<br />

Rinse the area with clean cold running water.<br />

WARNING: ETCH/ACTIVA<strong>TO</strong>R SOLUTION NUMBER 4 IS HARMFUL.<br />

f<br />

With a prepared tampon apply the etching solution (Item 12 in the Table of Subsidiary<br />

Materials). Do this at cathodically polarity (see manufacturer's instructions) and 10 to 12<br />

volts. Move the tampon in contact with and over the complete surface concerned for 2 to<br />

3 seconds per square inch (6.5 cm² (1.007 in²)).<br />

WARNING: NICKEL EPAIS SOLUTION IS DANGEROUS.<br />

g<br />

Move the tampon with nickel epais solution (Item <strong>11</strong> in the Table of Subsidiary Materials)<br />

over the moistened area at cathodically plating polarity (see manufacturer's instructions)<br />

and 6 to 10 volts, until 0.0025 mm (0.0001 in) has been deposited, refer to Paragraph<br />

2.B.(1).(d).3 .<br />

Print Date: December 29, 2016 Page 10 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

NOTE: Move the tampon at about 10 to 25 cm (4 to 10 in) per second.<br />

h<br />

Rinse the area with clean cold running water.<br />

WARNING: CADMIUM ACID SOLUTION IS DANGEROUS.<br />

i<br />

With a prepared tampon apply the cadmium acid solution (Item 10 in the Table of the<br />

Subsidiary Materials). Do this at the plating polarity (see manufacturer's instruction) and<br />

8 to 10 volts. Move the tampon in contact with and over the surface until you get the<br />

required thickness. You should move the tampon at a speed of approximately 15 to 61<br />

cm (6 to 24 in) per second.<br />

NOTE: For unspecified thickness, the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(d).3 .<br />

j Do steps 2.B.(1).(d).5.f thru 2.B.(1).(d).5.k .<br />

(e) Cadmium brush plating (or pad cadmium plating DALIC process) for steels (excluding stainless<br />

steels) with a maximum tensile strength of 1420 N/mm² (205 KSI).<br />

NOTE: This process is to be used to repair damaged protective treatment film not exceeding 700<br />

mm² (1.085 in²). The process is not allowed on any steel with carburized areas<br />

For larger surface perform multiple repairs.<br />

This process must be carried out by trained and approved personnel. An operator training<br />

service is available from the solution suppliers.<br />

1 Equipment<br />

- Power supply: Variable rectifier 30 volt 20 amp minimum fitted with voltmeter, ammeter,<br />

ampere hour meter, reversing switch and on/off switch.<br />

- Dishes for solutions glass polyethylene or porcelain flat bottom dishes of convenient size.<br />

- Electrodes: Use DALIC or DALIC UK or SIFCO tampons which have to be prepared in<br />

accordance with the material manufacturer's instructions. For optimum deposit speed area<br />

and shape of the anode must be determined by the area and the shape of the part to be<br />

plated the size should be s/6 < S < s/3 for SIFCO solution and s/8 < S < s/5 for DALIC<br />

solution where "s" is the area to be treated and "S" the area of the anode.<br />

- Hot air dryer (oil free).<br />

2 Repair Materials<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 Cleaning Agent AR Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

2 Lint free cloth, cotton wool AR Local Purchase<br />

3 Abrasive Paper - Silicon Carbide<br />

(grade 120)<br />

4 Abrasive Paper - Aluminum Oxide<br />

AR Local Purchase<br />

(grade <strong>320</strong> - water resistant)<br />

or finer or red SCOTCH-BRITE<br />

pads<br />

5 Masking tape AR PVC insulating tape or 3M No. 470 or aluminum<br />

tape Material No. 08-052 (Refer to<br />

CML)<br />

6 Brush or Swab AR Local Purchase<br />

Print Date: December 29, 2016 Page <strong>11</strong> of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

7 De-mineralized Water AR<br />

8 Aluminium Oxide Powder (80 microns)<br />

AR DALIC Reference CC<strong>11</strong>5<br />

9 Brush Plating Tools (use graphite<br />

anode) and Bonnets<br />

AR Separate anodes, bonnets and solution<br />

must be used at each stage of the<br />

process .Do not use steel tools containing<br />

more than 5% of chromium<br />

10 DALIC Cadmium plating Solution AR<br />

2023<br />

<br />

<strong>11</strong> Chromic finish solution AR<br />

<br />

12 SIFCO Cadmium LHE<br />

<br />

13 SIFCO Passivating Solution<br />

<br />

Code <strong>11</strong>028 from DALIC Code DPS6123<br />

from DALIC UK<br />

Passivateur No. 2 Code 10033 from DAL-<br />

IC Cadmium/Zinc Passivating Code DFS<br />

8010 from DALIC UK<br />

Code SPS 5070 from SIFCO<br />

Code SSS 3002 from SIFCO<br />

Storage conditions: Keep away from humidity and light at a temperature between 5° C<br />

to 30° C. Recommended shelf life is three years in original container except dalic solution<br />

2023 one year.<br />

DALIC 41, Rue des Eaux, B.P. 90139 35501 VITRE - France Tel: (33)<br />

2.99.75.53.80 Fax: (33) 2.99.74.49.31 service@dalicworld.com<br />

DALIC UK Ltd South Lodge House, 68-70 Frogge Street Ickleton<br />

(South Cambridge Shire) CB 10-1 SH - UK Tel: 0 1799 532 002 Fax: 0<br />

1799 532 003 info.dalicuk@tiscali.co.uk<br />

Storage conditions: <strong>21</strong>° C to 43° C RH 30 to 90, keep away from humidity and light<br />

at a temperature between 5° C to 30° C. Recommended shelf life is three years in original<br />

container and one year for SIFO5070.<br />

SIFCO applied surface concepts 16, rue de la Noue Guimante<br />

Lots 22/23 PA de la Courtilliere 77400 Saint-Thibault des Vignes<br />

www.electrolyseautampon.com<br />

3 How to obtain the correct thickness<br />

The thickness of the deposited metal is controlled by the ampere-hour meter. It further<br />

depends upon the area to be plated and the specific plating factor. The specific plating factor<br />

gives the number of ampere hours required to produce a deposit in mm or inches onto a<br />

surface area of square centimeters or square inches.<br />

SOLUTION<br />

FAC<strong>TO</strong>R FOR<br />

MEASUREMENT<br />

IN (mm)<br />

FAC<strong>TO</strong>R FOR<br />

MEASUREMENT<br />

IN (in)<br />

DALIC Code 2023 0.4 70<br />

SIFCO SPS 5070 0.4 70<br />

Table 005 - Specific Plating Factor<br />

Example 1:<br />

You have to plate an area of 25 cm² (3.875 in²) with SPS 5070 cadmium LHE plating<br />

solution. The required thickness is 0.015 mm. The correct ampere hours setting is: 0.4 x<br />

0.015 x 25 = 0.15 ampere hours.<br />

Example 2:<br />

Print Date: December 29, 2016 Page 12 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

You have to plate the same area with the same thickness but you measure in inches. The<br />

thickness is 0.0006 in and the area has the size of 3.87 sq.inch. Determine the correct<br />

number of ampere hours as follows: 70 X 0.0006 X 3.87 = 0.162 ampere-hours.<br />

4 Inspection<br />

The cadmium deposit must be fine grain, smooth and free from blisters, pitting, burns and<br />

other defects. Ensure that the cadmium deposit has good adherence to the metal surface.<br />

Check this with an adhesive tape. Put a strip of adhesive tape onto the treated surface and<br />

draw it quickly away. The adhesive tape must be free from cadmium particles. For more<br />

information refer to PMS Chapter 01-02-<strong>21</strong> .<br />

5 Procedure<br />

a<br />

b<br />

c<br />

d<br />

Remove all grease from the repair area (minimum one inch outside the repair area) with<br />

a clean cloth soaked in cleaning agent (Material No. <strong>11</strong>-003 or <strong>11</strong>-026 ) and wipe dry<br />

with a clean cloth or absorbent paper.<br />

Mask as necessary to define the area to be plated. If the area was already plated with<br />

cadmium, the brush plating must overlap the existing cadmium by about 4 mm (0.157<br />

in), refer to Figure 001 .<br />

Brush Plating Procedure<br />

Use one of the alternative procedures given in Paragraph 2.B.(1).(e).5.d and 2.B.(1).<br />

(e).5.e .<br />

Using SIFCO solutions<br />

NOTE: Prepare the work place with all the items. Start the power pack, adjust the<br />

voltage to 20 V and the current to the maximum and ensure the power pack is<br />

set in 'forward' polarity. Set the bonnet on the plating tool. Wet it first with demineralised<br />

water, squeeze with hand and paper, then place the electrode in the<br />

cadmium solution.<br />

- Manually abrade the area to be plated using a water wetted abrasive paper (<strong>320</strong><br />

grade or finer) or fine SCOTCH-BRITE pad and water. Feather the edge as shown on<br />

Figure 001 .<br />

- Rinse with demineralized water. Wipe with a clean wet cloth and wipe dry with a clean<br />

cloth.<br />

- Before switching on the current, wipe the area to be treated with a pad dampened<br />

with the plating solution (Item 12) or soak a tampon with the plating solution and start<br />

the appropriate tampon movement over the plating area. Ensure you have a liquid<br />

break free condition otherwise repeat 2.B.(1).(e).5.d Paragraph 2.<br />

- Using a prepared tampon move the tampon and apply plating solution at forward<br />

current cathodic plating polarity (part connected to (-) terminal and electrode (+) see<br />

manufacturer's instructions), plate at 15 to 20 V until a visible layer of cadmium is<br />

deposited, then reduce voltage to 8 to 14 V. Move the tampon in contact and over the<br />

surface and until you get the required thickness (see the required ampere hours in<br />

Paragraph 2.B.(1).(e).4 at a speed of approximately 6 to 24 m/min or 20 to 80 feet per<br />

minute. During plating do not allow the surface to dry and move the tampon to avoid<br />

the deposit to darken (burning).<br />

NOTE: For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(e).4 .<br />

- Rinse the area with clean cold running water.<br />

- Apply passivating solution (Item 13) with a brush or swab to the plated surface.<br />

Allow the solution to remain in contact for 15 to 30 seconds until a yellow or gold<br />

appearance is obtained.<br />

Print Date: December 29, 2016 Page 13 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F) or gently dab the surface with soft clean tissues, absorbent paper or<br />

clean cotton wool.<br />

- Inspect the treated areas as described in Paragraph 2.B.(1).(e).4 .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. The solutions, rinsing water<br />

and used bonnets must be processed or destroyed by an approved organization.<br />

Contaminated packaging if not re-used with the same product is also special<br />

waste to be sent to an approved organization for recycling or disposal.<br />

e DALIC Solution 2023<br />

NOTE: Prepare the work place with all the items. Start the power pack, adjust the<br />

voltage to 20 V and the current to the maximum and ensure the power pack is<br />

set in 'forward' polarity. Set the cover material on the plating tool. Wet it first with<br />

demineralised water, squeeze with hand and paper, then place the electrode in<br />

the cadmium solution.<br />

- Lightly dry abrade the area to be treated using 120 grade abrasive paper (around 3<br />

perpendicular cross pattern)<br />

- Re-apply aluminium or PVC masking tape.<br />

- Hand abrade area to be cadmium plated using 120 grade paper and water.<br />

- Clean with clean cloth dampened with demineralized water.<br />

- Lightly manually abrade the area using aluminium oxide powder, water and cotton<br />

wool.<br />

- Rinse with de-mineralized water.<br />

- Clean with clean cotton wool or clean cloth dampened with demineralized water,<br />

ensure that there is no longer black residues on the cloth.<br />

- Rinse with demineralized water.<br />

NOTE: Do not swab DALIC cadmium solution on the area to be plated.<br />

- Connect the piece to (-) terminal and the electrode to (+) terminal (red plug, +) to the<br />

power supply pack.<br />

- Plate at 20 V until 12 to 15% of the total current quantity calculated is reached.<br />

- Repeat 2.B.(1).(e).5.e Paragraph 3 thru Paragraph 8 to remove the first cadmium<br />

layer.<br />

- Set to 0 the current quantity meter.<br />

- Plate again at 20 V until 12 to 15% of the total current quantity calculated is reached<br />

then reduce to <strong>11</strong> V until the required current quantity is reached.<br />

NOTE: Ensure fast electrode movement to prevent 'burning' of the deposit (use a speed<br />

of around 25 m/min (80 feet / min). Put the electrode on the tape and start to<br />

move the electrode over the surface, sweep the surface very quickly.<br />

For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(e).4 .<br />

- Rinse with clean cold running water.<br />

- Remove the masking.<br />

- Rinse with water.<br />

- Dry with hot air dryer.<br />

- Clean with cleaning agent (Material No. <strong>11</strong>-026 ).<br />

Print Date: December 29, 2016 Page 14 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

- Apply passivating solution (Item <strong>11</strong>) with a brush or swab to the plated surface. Allow<br />

the solution to remain in until a yellow or gold appearance is obtained.<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F) or gently dab the surface with soft clean tissues, absorbent paper or<br />

clean cotton wool.<br />

- Inspect the treated areas as described in 2.B.(1).(e).5.e Paragraph 4.<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. The solutions, rinsing water<br />

and used bonnets must be processed or destroyed by an approved organization.<br />

Contaminated packaging if not re-used with the same product is also special<br />

waste to be sent to an approved organization for recycling or disposal.<br />

(f)<br />

Cadmium brush plating (or pad cadmium plating DALIC process) for stainless steels with<br />

maximum tensile strength of <strong>11</strong>00 N/mm² (159 KSI).<br />

NOTE: This process must be carried out by trained and approved personnel. An operator training<br />

service is available from the solution suppliers.<br />

1 Equipment<br />

- Power supply: variable rectifier minimum fitted with voltmeter, ammeter, ampere-hour<br />

meter, reversing switch and on/off switch.<br />

- Dishes for solutions glass polyethylene or porcelain flat bottom dishes of convenient size.<br />

- Electrodes: Use DALIC, DALIC UK or SIFCO tampons which have to be prepared in<br />

accordance with the material manufacturer's instructions. For optimum deposit speed area<br />

and shape of the anode must be determined by the area and the shape of the part to be<br />

plated. The size should be s/6 < S < s/3 where "s" is the area to be treated and "S" the<br />

area of the anode.<br />

- Hot air dryer (oil free).<br />

2 Repair Materials<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 Cleaning Agent AR Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

2 Lint free cloth, cotton wool AR Local Purchase<br />

3 Abrasive Paper - Silicon Carbide<br />

(grade 120)<br />

4 Abrasive Paper - Aluminum Oxide<br />

AR Local Purchase<br />

(grade <strong>320</strong> - water resistant)<br />

or finer or red SCOTCH-BRITE<br />

pads<br />

5 Masking Tape AR PVC insulating tape or 3M No. 470 or aluminum<br />

tape Material No. 08-052 (Refer to<br />

CML)<br />

6 Brush or Swab AR Local Purchase<br />

7 De-mineralized Water AR<br />

8 Aluminium Oxide Powder (80 microns)<br />

AR DALIC Reference CC<strong>11</strong>5<br />

9 Brush Plating Tools (use graphite<br />

anode) and Bonnets<br />

AR<br />

Separate anodes, bonnets and solution<br />

must be used at each stage of the<br />

Print Date: December 29, 2016 Page 15 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

process .Do not use steel tools containing<br />

more than 5% of chromium<br />

10 DALIC Cadmium plating Solution AR<br />

2023<br />

<br />

<strong>11</strong> Chromic finish solution AR<br />

<br />

12 ATTAQUE No. 3<br />

<br />

13 ATTAQUE No. 2<br />

<br />

14 NICKELAGE EP<br />

<br />

15 SIFCO Cadmium LHE<br />

<br />

16 SIFCO Passivating Solution<br />

<br />

17 SIFCO Electrolytic Degreasing<br />

Solution<br />

<br />

18 Nickel Plating Solution<br />

<br />

19 ACTIVA<strong>TO</strong>R No. 4<br />

<br />

20 ACTIVA<strong>TO</strong>R No. 1<br />

<br />

AR<br />

AR<br />

AR<br />

AR<br />

Code <strong>11</strong>028 from DALIC Code DPS6123<br />

from DALIC UK<br />

Passivateur No. 2 Code 10033 from DAL-<br />

IC Cadmium/Zinc Passivating Code DFS<br />

8010 from DALIC UK<br />

Code 10005 from DALIC or DCN ETCH-<br />

ING Code DPR 5075 from DALIC UK<br />

Code 10004 from DALIC or ACTIVAT-<br />

OR/ETCH No. 3 Code DPR5003 from<br />

DALIC UK<br />

Code <strong>11</strong>028 FROM DALIC or Nickel<br />

EPAIS Code DPS6340 from DALIC UK<br />

Code SPS 5070 from SIFCO<br />

Code SSS 3002 from SIFCO<br />

Code SCM 4100 from SIFCO<br />

Code SPS 5600 from SIFCO<br />

Code SCM 4250 from SIFCO<br />

Code SCM 4200 from SIFCO<br />

Storage conditions: Keep away from humidity and light at a temperature between 5° C<br />

to 30° C. Recommended shelf life is three years in original container.<br />

DALIC 41, Rue des Eaux, B.P. 90139 35501 VITRE - France Tel: (33)<br />

2.99.75.53.80 Fax: (33) 2.99.74.49.31 service@dalicworld.com<br />

DALIC UK Ltd South Lodge House, 68-70 Frogge Street Ickleton<br />

(South Cambridge Shire) CB 10-1 SH - UK Tel: 0 1799 532 002 Fax: 0<br />

1799 532 003 info.dalicuk@tiscali.co.uk<br />

Storage conditions: <strong>21</strong>° C to 43° C RH 30 to 90, keep away from humidity and light<br />

at a temperature between 5° C to 30° C. Recommended shelf life is three years in original<br />

container.<br />

SIFCO applied surface concepts 16, rue de la Noue Guimante Lots<br />

22/23 PA de la Courtilliere 77400 Saint-Thibault des Vignes http://<br />

www.electrolyseautampon.com<br />

3 How to obtain the correct thickness<br />

The thickness of the deposited metal is controlled by the ampere-hour meter. It further<br />

depends upon the area to be plated and the specific plating factor. The specific plating factor<br />

gives the number of ampere-hours required to produce a deposit in mm or inches onto a<br />

surface area of square centimeters or square inches.<br />

SOLUTION<br />

FAC<strong>TO</strong>R FOR MEASURE-<br />

MENT<br />

IN (mm)<br />

DALIC Code 2023 0.4 70<br />

FAC<strong>TO</strong>R FOR MEASURE-<br />

MENT<br />

IN (in)<br />

Print Date: December 29, 2016 Page 16 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

SOLUTION<br />

FAC<strong>TO</strong>R FOR MEASURE-<br />

MENT<br />

IN (mm)<br />

SIFCO SPS 5070 0.4 70<br />

NICKEL EP/EPAIS 1.78 290<br />

Nickel SPS 5600 1.5 250<br />

FAC<strong>TO</strong>R FOR MEASURE-<br />

MENT<br />

IN (in)<br />

Table 006<br />

Example 1:<br />

You have to plate an area of 25 cm² (3.875 in²) with SPS 5070 cadmium LHE plating<br />

solution. The required thickness is 0.015 mm, the correct ampere hours setting is: 0.4 x<br />

0.015 x 25 = 0.15 ampere-hours.<br />

Example 2:<br />

You have to plate the same area with the same thickness, but you measure in inches. The<br />

thickness is 0.0006 in and the area has the size of 3.87 sq.inch. Determine the correct<br />

number of ampere hours as follows: 70 x 0.0006 x 3.87 = 0.162 ampere-hours.<br />

4 Inspection<br />

The cadmium deposit must be fine grain, smooth and free from blisters, pitting, burns and<br />

other defects. Ensure that the cadmium deposit has good adherence to the metal surface.<br />

Check this with an adhesive tape. Put a strip of adhesive tape onto the treated surface and<br />

draw it quickly away. The adhesive tape must be free from cadmium particles. Refer to PMS<br />

Chapter 01-02-<strong>21</strong> for more information.<br />

5 Procedure<br />

a<br />

b<br />

c<br />

Remove all grease from the repair area (minimum one inch outside the repair area) with<br />

a clean cloth soaked in cleaning agent (Material No. <strong>11</strong>-003 or <strong>11</strong>-026 ) and wipe dry<br />

with a clean cloth or absorbent paper.<br />

Mask as necessary to define the area to be plated. If the area was already plated with<br />

cadmium, the brush plating must overlap the existing cadmium by about 4 mm (0.157<br />

in), refer to Figure 001 .<br />

Brush Plating Procedure<br />

Use one of the alternative procedures given in Paragraph 2.B.(1).(f).5.d and 2.B.(1).<br />

(f).5.e .<br />

d SIFCO Solution SPS 5070<br />

NOTE: Prepare the work place with all the tools and solutions.<br />

Use a different and identified tool for each solution.<br />

First wet with demineralised water the bonnets set on the plating tools then<br />

squeeze with hand and paper and let soak with solution for a minimum of 2<br />

minutes.<br />

The treatment must be achieved in totality without interruption.<br />

- Manually abrade the area to be plated using a water wetted abrasive paper (<strong>320</strong><br />

grade or finer) or fine SCOTCH-BRITE pad and water or aluminum oxide powder on a<br />

water moistened swab. Feather the edge as shown on Figure 001 .<br />

- Rinse with demineralized water.<br />

- Electrolytically clean with deoxidizing solution (Item 27) at 10 to 20 volts forward<br />

current.<br />

- Rinse with demineralized water ensuring a water break free surface.<br />

- Anodically etch with solution ACTIVA<strong>TO</strong>R No. 4 SCM 4250 (Item 19) at 8 to 15 volts<br />

reverse current.<br />

- Rinse with demineralized water.<br />

Print Date: December 29, 2016 Page 17 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

- Cathodically etch with solution ACTIVA<strong>TO</strong>R No. 1 SCM 4200 (Item 20) at 8 to 15<br />

volts forward current.<br />

- Do not allow to dry. Plate without delay a layer of nickel using plating solution (Item<br />

18) at 6 to 10 volts for the ampere minutes required to obtain 5 microns (2 to 7<br />

microns).<br />

- Rinse with de-mineralized water.<br />

- Do not allow to dry. Before switching on the current, wipe the area to be treated with<br />

a pad dampened with the plating solution (Item 15) or soak a tampon with the plating<br />

solution and start the appropriate tampon movement over the plating area.<br />

- Using a prepared tampon move the tampon and apply plating solution at forward<br />

current or cathodic plating polarity ( part (-) and tool (+)) see manufacturer's<br />

instructions (Item 15). Plate at 8 V and move the tampon in contact and over<br />

the surface and until you get the required thickness (for required ampere-hours<br />

refer to Paragraph 2.B.(1).(f).5.e . During plating move the tampon at a speed of<br />

approximately 6-24 m/min or 20-80 feet per minute. During plating do not allow the<br />

surface to dry and move the tampon to avoid the deposit to darken (burning).<br />

NOTE: For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(f).3 ).<br />

- Rinse the area with cold running water.<br />

- If required for appearance abrade slightly the treated surface with a SCOTCH-BRITE<br />

pad or aluminum oxide and cotton wool. It will brighten the cadmium deposit before<br />

passivation.<br />

- Apply passivating solution (Item 16) with a brush or swab to the plated surface. Allow<br />

the solution to remain in contact until a yellow or gold appearance is obtained.<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F) or gently dab the surface with soft clean tissues or absorbent paper<br />

or clean cotton wool.<br />

- Inspect the treated area as described in Paragraph 2.B.(1).(e).5.d .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. The solutions, rinsing water<br />

and used bonnets must be processed within the firm or destroyed by an<br />

approved organization. Contaminated packaging if not re-used with the same<br />

product is also special waste to be sent to an approved organization for recycling<br />

or disposal<br />

e DALIC Solution 2023<br />

NOTE: Prepare the work place with all the tools and solutions.<br />

Use a different and identified tool for each solution.<br />

First wet with demineralised water the bonnets set on the plating tools then<br />

squeeze with hand and paper and let soak with solution for a minimum of 2<br />

minutes.<br />

The treatment must be achieved in totality without interruption.<br />

- Manually abrade the area to be plated using a water wetted abrasive paper (220<br />

grade), feather the edges as shown on Figure 001 . Clean with demineralized water<br />

and several cloths or papers without drying the surface.<br />

- Manually abrade the area using a water wetted red abrasive sponge, clean with<br />

demineralized water and several cloths or papers without drying the surface.<br />

Print Date: December 29, 2016 Page 18 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

(2). Phosphating<br />

(a) General<br />

- Manually abrade the area using alumina powder and a wetted cotton wool piece,<br />

clean carefully with demineralized water and several cloths or papers without drying<br />

the surface. The surface in final must be free from residues.<br />

NOTE: Before switching on the current, wipe the area to be treated with a tampon<br />

soaked with the indicated solution (Item 12) and start the appropriate tampon<br />

movement over the plating area.<br />

- Etch with ATTAQUE No. 3 Solution at <strong>11</strong> V, reverse polarity (part (+) and tool (-)),<br />

apply 0.25 Ah/dm² of area to be treated.<br />

- Rinse with de-mineralized water.<br />

- Etch for cleaning with ATTAQUE No. 2 solution (Item 13) at <strong>11</strong> V, reverse polarity<br />

(part (+) and tool (-)), apply 0.25 Ah/dm² of area to be treated.<br />

- Rinse with de-mineralized water.<br />

- Plate a nickel under layer with the NICKELAGE EP Solution (Item 14) at 6 to 10V,<br />

cathodic plating polarity or forward current (part (-) and tool (+)), for the ampere<br />

minutes required to obtain 5 microns (2 to 7 microns).<br />

- Rinse with de-mineralized water.<br />

- Plate around 3 µm cadmium with CADMIUM 2023 solution (Item 10) at 6 V, cathodic<br />

plating polarity or forward current (part (-) and tool (+)) then increase to 8 V to achieve<br />

the required thickness (see the required ampere-hours in Paragraph 2.B.(1).(f).5.e .<br />

During plating move the tampon at a speed of approximately 6 to 24 m/min or 20 to<br />

80 feet/minute. During plating do not allow the surface to dry and move the tampon to<br />

avoid the deposit to darken (burning).<br />

NOTE: For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(f).5.e .<br />

- Rinse the area with clean cold running water.<br />

- Apply passivating solution (Item <strong>11</strong>) with a piece of cotton wool. Do soft and regular<br />

movements on the plated surface for 15 to 30 seconds until a yellow or gold colour is<br />

obtained.<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F).<br />

- Inspect the repair as described in Paragraph 2.B.(1).(e).5.d .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. These solutions, rinsing water<br />

and used bonnets must be disposed by an approved organization. Contaminated<br />

packaging if not re-used with the same product is also special waste to be<br />

sent to an approved organization for recycling or disposal.<br />

1 The phosphorisation is a procedure in which the surface of the metal is given a layer of<br />

phosphoric acid solution. You do this with a brush when the parts are installed or you can put<br />

them into a phospheric bath.<br />

2 This protective treatment is necessary after the removal of corrosion or when a repair<br />

procedure breaks the original surface protection. All corrosion and the paint coatings must<br />

be removed until a clean metallic surface is obtained, before you start with phosphating.<br />

Before brush phosphating, the corrosion can be removed mechanically. When the parts are<br />

Print Date: December 29, 2016 Page 19 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

phosphated in a bath and strongly oxidized, the corrosion must be removed by abrasive<br />

blasting (Refer to Chapter <strong>51</strong>-74-00 ).<br />

3 For the required paint coatings after this treatment refer to Chapter <strong>51</strong>-23-<strong>11</strong> .<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER’S INSTRUCTIONS WHEN YOU USE THE CLEANING<br />

AGENTS (MATERIAL NO. <strong>11</strong>-003 AND <strong>11</strong>-026). THESE CLEANING AGENTS ARE<br />

DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS WHEN YOU USE THE PHOSPHORIC<br />

SOLUTION (MATERIAL NO. 05-041 OR 05-042). THESE PHOSPHORIC SOLUTIONS<br />

ARE DANGEROUS.<br />

(c) Brush Phosphating of Steel Parts in Installed Position<br />

1 Materials<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 Phosphoric solution - Material No. 05-042 (Refer to CML)<br />

2 Cleaning agent - Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

3 Cheese cloth -<br />

4 Brush -<br />

5 Masking tape -<br />

6 Hot-air dryer -<br />

2 Procedure<br />

a<br />

Clean and remove grease from the repair area with a clean cloth, soaked in cleaning<br />

agent (Material No. <strong>11</strong>-003 or <strong>11</strong>-026 ).<br />

b Mask all adjacent surfaces on which the phosphoric solution (Material-Number 05-042 )<br />

can possibly cause damage.<br />

WARNING: PHOSPHORIC SOLUTION (MATERIAL NO. 05-042) IS DANGEROUS.<br />

c<br />

Apply a large quantity of phosphoric solution (Material No. 05-042 ) with a brush or a<br />

clean cloth. Permit the solution to penetrate for 10 minutes.<br />

d<br />

e<br />

NOTE: The surface must, when treated correctly, show a grey-white color. Do the phosphating<br />

procedure again if necessary.<br />

Clean the surface with a clean cloth, soaked in water.<br />

Dry the area with hot air.<br />

f Apply the required paint coatings (Refer to Chapter <strong>51</strong>-23-<strong>11</strong> ).<br />

(d) Phosphating of Steel Parts by Immersion in a Phosphoric Bath<br />

1 For details of this treatment and the necessary equipment refer to PMS Chapter 01-01-10 .<br />

(3). Hard Chromium Plating<br />

(a) General<br />

Print Date: December 29, 2016 Page 20 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

1 Hard chromium plating is a procedure in which the surface of the material is given a<br />

chromium layer.<br />

2 Hard chromium plating is required when:<br />

- the original chromium layer becomes thinner by friction than is permitted,<br />

- or the material under the chromium layer is corroded.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR THE MATERIALS WHICH YOU<br />

USE FOR CLEANING PROCEDURES BEFORE HARD CHROMIUM PLATING.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE.<br />

(c) Procedure<br />

For details of hard chromium plating and the necessary equipment refer to PMS Chapter<br />

01-02-<strong>11</strong> .<br />

(4). Silver Plating<br />

(a) General<br />

1 Silver Plating is a procedure in which the surface of the material is given a layer of silver. You<br />

do this with the silver electrolytic process. Silver plating is used for its electrical conductive<br />

properties and its resistance to fretting corrosion under hot conditions.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR THE MATERIALS WHICH YOU<br />

USE FOR CLEANING PROCEDURES BEFORE SILVER PLATING. THESE MATERI-<br />

ALS ARE DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. SOME <strong>OF</strong> THESE MATERIALS CONTAIN IRRITANTS.<br />

(c) Procedure<br />

For details of silver plating and the necessary equipment refer to PMS Chapter 01-02-01 .<br />

(5). Zinc Spraying<br />

(a) General<br />

1 Zinc spraying is a procedure in which the surface of the metal is given a zinc layer. This<br />

can be necessary when the steel repair parts touch aluminum components and galvanic<br />

corrosion can occur.<br />

2 The zinc layer is a type of sacrificial protection. The corrosion effects initially damage the zinc<br />

layer and not the material below the protective layer.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

Print Date: December 29, 2016 Page <strong>21</strong> of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR THE MATERIALS WHICH YOU<br />

USE FOR CLEANING PROCEDURES BEFORE ZINC SPRAYING. THESE MATERI-<br />

ALS ARE DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS WHEN YOU SPRAY ZINC WITH A<br />

SPRAY GUN. THE <strong>METAL</strong>LIC DUST IN THE AIR IS HIGHLY EXPLOSIVE. MAKE<br />

SURE THAT YOU DO THE SPRAYING PROCEDURE IN A GOOD VENTILATED<br />

AREA. USE <strong>PROTECTIVE</strong> CLOTHES FOR ALL <strong>PARTS</strong> <strong>OF</strong> YOUR BODY AND DO<br />

NOT INHALE THE <strong>METAL</strong>LIC DUST.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS WHEN YOU USE PROPANE OR<br />

ACETYLENE GAS. BOTH GASES ARE HIGHLY FLAMMABLE.<br />

(c) Procedure<br />

For details of zinc spraying and the necessary equipment refer to PMS Chapter 01-02-24 .<br />

(6). Vacuum Cadmium Plating<br />

C. Titanium<br />

(a) General<br />

1 Vacuum cadmium plating is a procedure in which the surface of the metal is given a layer<br />

of cadmium. This layer of cadmium is a type of sacrificial protection. The corrosion effects<br />

initially damage the cadmium and not the metal under the protective layer.<br />

2 This procedure is specially used for high-tensile steels with a tensile strength more than 1450<br />

N/mm ² (<strong>21</strong>0 KSI). Other procedures of cadmium plating are not permitted for high-tensile<br />

steel because of the embrittlement of the material.<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR THE MATERIAL WHICH YOU<br />

USE FOR THE CLEANING PROCEDURES BEFORE VACUUM CADMIUM PLATING.<br />

THESE CLEANING AGENTS ARE DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. THESE CHEMICALS ARE POISONOUS AND DANGER-<br />

OUS.<br />

(c) Procedure<br />

For details of vacuum cadmium plating and the necessary equipment refer to PMS Chapter<br />

01-02-38 .<br />

(1). Anodizing<br />

(a) General<br />

1 Anodizing of titanium is a procedure in which the surface of the material is given a very<br />

thin anodic coating. This protective treatment decreases galvanic corrosion when it is<br />

used without further protections. This coating gives a good surface for the adhesion of dry<br />

lubricants.<br />

2 This protective treatment is necessary when titanium touches other metals and galvanic<br />

effects have to be prevented.<br />

3 Make sure that the required paint coatings are supplied within 16 hours after this treatment.<br />

Print Date: December 29, 2016 Page 22 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

(b) Safety Precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR THE MATERIAL WHICH YOU<br />

USE FOR THE CLEANING PROCEDURE BEFORE ANODIZING. THESE CLEANING<br />

AGENTS ARE DANGEROUS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. THESE CHEMICALS ARE DANGEROUS.<br />

(c) Procedure<br />

For details of anodizing titanium and the necessary equipment refer to PMS Chapter 01-02-10 .<br />

D. Copper Alloys<br />

(1). Cadmium Plating<br />

(a) General<br />

1 There are two different procedures used to put cadmium onto the surface of the material.<br />

The first method describe a cadmium plating procedure, in which the metal parts are put into<br />

several immersion baths. The second method describes the portable plating DALIC process,<br />

which is suitable for field repairs.<br />

2 Before you start the cadmium plating procedure, make sure that the parts are clean, show a<br />

bright metal surface and are free from corrosion, refer to Chapter <strong>51</strong>-74-00 .<br />

3 It is recommended that cadmium plating is carried out by trained and approved personnel.<br />

(b) Safety precautions<br />

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERI-<br />

AL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH MATERIAL WHICH YOU<br />

USE FOR CLEANING PROCEDURES BEFORE YOU START THE CADMIUM PLAT-<br />

ING. THESE CLEANING AGENTS ARE HARMFUL.<br />

WARNING: OBEY THE MANUFACTURER INSTRUCTIONS FOR EACH CHEMICAL WHICH YOU<br />

USE IN THIS PROCEDURE. THESE CHEMICALS ARE POISONOUS AND HARM-<br />

FUL.<br />

(c) Cadmium plating immersion procedure in accordance with AMS-QQ-P-416 Type II.<br />

NOTE: Use class 2 thickness unless otherwise noted in repair instructions/drawing.<br />

(d) Cadmium brush plating (or pad cadmium plating DALIC process) for copper alloys<br />

NOTE: This process must be carried out by trained and approved personnel, an operator training<br />

service is available from the solution suppliers.<br />

1 Equipment<br />

Power supply: variable rectifier minimum fitted with voltmeter, ammeter, ampere-hour meter,<br />

reversing switch and on/off switch.<br />

Dishes for solutions glass polyethylene or porcelain flat bottom dishes of convenient size.<br />

Print Date: December 29, 2016 Page 23 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

Electrodes: Use DALIC or DALIC UK or SIFCO tampons which have to be prepared in<br />

accordance with the material manufacturer's instructions, for optimum deposit speed area<br />

and shape of the anode must be determined by the area and the shape of the part to be<br />

plated the size should be s/6 < S < s/3 where "s" is the area to be treated and "S" the area of<br />

the anode.<br />

Hot air dryer (oil free)<br />

2 Materials<br />

ITEM NOMENCLATURE QTY MATERIAL/REMARKS<br />

1 Cleaning Agent AR Material No. <strong>11</strong>-003 or <strong>11</strong>-026 (Refer to<br />

CML)<br />

2 Lint free cloth, cotton wool AR Local Purchase<br />

3 Abrasive Paper - Aluminum Oxide<br />

AR Local Purchase<br />

(grade <strong>320</strong> - water resistant)<br />

or finer<br />

4 Masking tape AR PVC insulating tape or 3M No. 470 or aluminum<br />

tape Material No. 08-052 (Refer to<br />

CML)<br />

5 Brush or Swab AR Local Purchase<br />

6 De-mineralized Water AR<br />

7 SCOTCH-BRITE pads - red AR Local Purchase<br />

8 Aluminium Oxide Powder (80 microns)<br />

AR DALIC Reference CC<strong>11</strong>5<br />

9 Brush Plating Tools (use graphite<br />

anode) and Bonnets<br />

AR<br />

10 DALIC Cadmium plating Solution AR<br />

2023<br />

<br />

<strong>11</strong> Chromic finish solution AR<br />

<br />

12 Cleaning de-oxidizing solution<br />

<br />

13 ATTAQUE No. 2<br />

<br />

14 SIFCO Cadmium LHE<br />

<br />

15 SIFCO Passivating Solution<br />

<br />

16 SIFCO Electrolytic Degreasing<br />

Solution<br />

<br />

17 Etching dismutting solution<br />

<br />

AR<br />

AR<br />

Separate anodes, bonnets and solution<br />

must be used at each stage of the<br />

process .Do not use steel tools containing<br />

more than 5% of chromium<br />

Code <strong>11</strong>028 from DALIC Code DPS6123<br />

from DALIC UK<br />

Passivateur No. 2 Code 10033 from DAL-<br />

IC Cadmium/Zinc Passivating Code DFS<br />

8010 from DALIC UK<br />

DECA Z from DALIC Code 10007<br />

Code 10004 from DALIC or ACTIVAT-<br />

OR/ETCH No. 3 Code DPR5003 from<br />

DALIC UK<br />

Code SPS 5070 from SIFCO<br />

Code SSS 3002 from SIFCO<br />

Code SCM 4100 from SIFCO<br />

SCM 4350 from SIFCO<br />

Storage conditions: Keep away from humidity and light at a temperature between 5° C<br />

to 30° C. Recommended shelf life is three years in original container.<br />

DALIC 41, Rue des Eaux, B.P. 90139 35501 VITRE - France Tel: (33)<br />

2.99.75.53.80 Fax: (33) 2.99.74.49.31 service@dalicworld.com<br />

Print Date: December 29, 2016 Page 24 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

DALIC UK Ltd South Lodge House, 68-70 Frogge Street Ickleton<br />

(South Cambridge Shire) CB 10-1 SH - UK Tel: 0 1799 532 002 Fax: 0<br />

1799 532 003 info.dalicuk@tiscali.co.uk<br />

Storage conditions: <strong>21</strong>° C to 43° C RH 30 to 90, keep away from humidity and light<br />

at a temperature between 5° C to 30° C. Recommended shelf life is three years in original<br />

container.<br />

SIFCO applied surface concepts 16, rue de la Noue Guimante Lots<br />

22/23 PA de la Courtilliere 77400 Saint-Thibault des Vignes http://<br />

www.electrolyseautampon.com<br />

3 How to obtain the correct thickness<br />

The thickness of the deposited metal is controlled by the ampere-hour meter. It further<br />

depends upon the area to be plated and the specific plating factor. The specific plating factor<br />

gives the number of ampere-hours required to produce a deposit in mm or inches onto a<br />

surface area of square centimeters or square inches.<br />

SOLUTION<br />

FAC<strong>TO</strong>R FOR<br />

MEASUREMENT<br />

IN (mm)<br />

FAC<strong>TO</strong>R FOR<br />

MEASUREMENT<br />

IN (in)<br />

DALIC Code 2023 0.4 70<br />

SIFCO SPS 5070 0.4 70<br />

Table 007 - Specific Plating Factor<br />

Example 1:<br />

You have to plate an area of 25 cm² (3.875 in²) with SPS 5070 cadmium LHE plating<br />

solution. The required thickness is 0.015 mm, the correct ampere hours setting is: 0.4 x<br />

0.015 x 25 = 0.15 ampere-hours.<br />

Example 2:<br />

You have to plate the same area with the same thickness, but you measure in inches. The<br />

thickness is 0.0006 in and the area has the size of 3.87 sq.inch. Determine the correct<br />

number of ampere hours as follows: 70 x 0.0006 x 3.87 = 0.162 ampere-hours.<br />

4 Inspection<br />

The cadmium deposit must be fine grain, smooth and free from blisters, pitting, burns and<br />

other defects. Ensure that the cadmium deposit has good adherence to the metal surface.<br />

Check this with an adhesive tape. Put a strip of adhesive tape onto the treated surface and<br />

draw it quickly away. The adhesive tape must be free from cadmium particles. Refer to PMS<br />

Chapter 01-02-<strong>21</strong> for more information.<br />

5 Procedure<br />

a<br />

b<br />

c<br />

Remove all grease from the repair area (minimum one inch outside the repair area) with<br />

a clean cloth soaked in cleaning agent (Material No. <strong>11</strong>-003 or <strong>11</strong>-026 ) and wipe dry<br />

with a clean cloth or absorbent paper.<br />

Mask as necessary to define the area to be plated. If the area was already plated with<br />

cadmium, the brush plating must overlap the existing cadmium by about 4 mm (0.157<br />

in), refer to Figure 001 .<br />

Brush Plating Procedure<br />

Use one of the alternative procedures given in Paragraph 2.D.(1).(d).5.d and 2.D.(1).<br />

(d).5.e .<br />

d SIFCO Solution SPS 5070<br />

NOTE: Prepare the work place with all the tools and solutions.<br />

Use a different and identified tool for each solution.<br />

Print Date: December 29, 2016 Page 25 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

First wet with demineralised water the bonnets set on the plating tools then<br />

squeeze with hand and paper and let soak with solution for a minimum of 2<br />

minutes.<br />

The treatment must be achieved in totality without interruption.<br />

- Manually abrade the area to be plated using a water wetted abrasive paper (180<br />

grade) or aluminum oxide powder on a water moistened swab. Feather the edge as<br />

shown on Figure 001 .<br />

- Rinse with de-mineralized water.<br />

- Electrolytically clean with deoxidizing solution (Item 16) at 10 to 15 volts forward<br />

current.<br />

- Rinse with de-mineralized water ensuring a water break free surface.<br />

- Before switching on the current, wipe the area to be treated with a pad dampened<br />

with the etching solution (Item 17) or soak a tampon with the plating solution and start<br />

the appropriate tampon movement over the plating area.<br />

- Anodically etch with solution SCM 4350 at 10 to 15 volts reverse current.<br />

- Rinse with cold clean running water.<br />

- Do not allow to dry. Before switching on the current, wipe the area to be treated with<br />

a pad dampened with the plating solution (Item 14) or soak a tampon with the plating<br />

solution and start the appropriate tampon movement over the plating area.<br />

- Using a prepared tampon move the tampon and apply plating solution at forward<br />

current or cathodic plating polarity (part (-) and tool (+)) see manufacturer's<br />

instructions (Item 14). Plate at 6 to 20 V and move the tampon in contact and over<br />

the surface and until you get the required thickness (for required ampere-hours<br />

refer to Paragraph 2.B.(1).(f).5.e . During plating move the tampon at a speed of<br />

approximately 6 to 24 m/min or 20 to 80 feet per minute. During plating do not allow<br />

the surface to dry and move the tampon to avoid the deposit to darken (burning).<br />

NOTE: For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in), refer to Paragraph 2.B.(1).(f).5.e .<br />

- Rinse the area with cold running water.<br />

- Apply passivating solution (Item 15) with a brush or swab to the plated surface. Allow<br />

the solution to remain in contact until a yellow or gold appearance is obtained.<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F) or gently dab the surface with soft clean tissues or absorbent paper<br />

or clean cotton wool.<br />

- Inspect the treated area as described in Paragraph 2.B.(1).(e).5.d .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. The solutions, rinsing water<br />

and used bonnets must be processed within the firm or destroyed by an<br />

approved organization. Contaminated packaging if not re-used with the same<br />

product is also special waste to be sent to an approved organization for recycling<br />

or disposal.<br />

e DALIC Solution 2023<br />

NOTE: Prepare the work place with all the tools and solutions.<br />

Use a different and identified tool for each solution.<br />

First wet with demineralised water the bonnets set on the plating tools then<br />

squeeze with hand and paper and let soak with solution for a minimum of 2<br />

minutes.<br />

Print Date: December 29, 2016 Page 26 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

The treatment must be achieved in totality without interruption.<br />

- Manually abrade the area to be plated using a water wetted abrasive paper (180<br />

grade) or aluminum oxide powder on a water moistened swab. Feather the edge as<br />

shown on Figure 001 .<br />

- Clean with de-mineralized water and several cloths or papers without drying the<br />

surface.<br />

- Cathodically clean with cleaning/deoxidizing solution DECA Z solution (Item 12) at 12<br />

to 15 volts forward current.<br />

- Rinse with cold clean running water ensuring a water break free surface.<br />

- Anodically etch with etch ACTIVA<strong>TO</strong>R solution No. 3 (Item 13) at 12 to 15 volts,<br />

reverse polarity (part (+) and tool (-)).<br />

- Rinse with cold clean running water.<br />

- Swab cadmium 2023 plating solution and apply to the surface area to be treated.<br />

- Saturate tampon with cadmium 2023 solution and apply to the surface area to be<br />

treated.<br />

- Cadmium plate with the cadmium solution (Item 10) at 8 to 10 V, cathodic plating<br />

polarity or forward current (part (-) and tool (+)) to achieve the required thickness (for<br />

required ampere-hours refer to Paragraph 2.B.(1).(f).5.e . During plating move the<br />

tampon at a speed of approximately 6 to 24 m/min or 20 to 80 feet/minute. During<br />

plating do not allow the surface to dry and move the tampon to avoid the deposit to<br />

darken (burning).<br />

NOTE: For unspecified thickness the deposit must average between 0.015 mm (0.0006<br />

in) and a minimum of 0.01 mm (0.0004 in) refer Paragraph 2.B.(1).(f).5.e .<br />

- Rinse the area with cold running water.<br />

- Apply passivating solution (Item <strong>11</strong>) with a piece of cotton wool. Do soft and regular<br />

movements on the plated surface for 15 to 30 seconds until a yellow or gold<br />

appearance is obtained.<br />

- Rinse the area with clean cold running water.<br />

- Dry the repair area with an air blast or with a hot air dryer at a maximum temperature<br />

of 50° C (122° F).<br />

- Inspect the treated area as described in Paragraph 2.B.(1).(e).5.d .<br />

NOTE: Make sure that the required paint coatings are applied within 16 hours.<br />

NOTE: Do not return used solutions in original containers. The solutions, rinsing water<br />

and used bonnets must be processed within the firm or destroyed by an<br />

approved organization. Contaminated packaging if not re-used with the same<br />

product is also special waste to be sent to an approved organization for recycling<br />

or disposal.<br />

Print Date: December 29, 2016 Page 27 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

DAMAGED AREA<br />

PLATING DAMAGED IN THIS AREA<br />

NS6 <strong>51</strong> <strong>21</strong> <strong>11</strong> 0 AAM0 00 0<br />

BLENDING AREA<br />

AT LEAST 4mm (0.157in.)<br />

TRANSITION AREA<br />

Figure 001 (sheet 1) / <strong>51</strong>-<strong>21</strong>-<strong>11</strong> Typical surface preparation<br />

Print Date: December 29, 2016 Page 28 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.


Customer : ENV<br />

Type : A<strong>320</strong><br />

Rev. Date : Nov 01, 2016<br />

<strong>51</strong>-<strong>21</strong>-<strong>11</strong> Application of Protective Treatment to Metal Parts<br />

Manual : <strong>SRM</strong><br />

Selected effectivity :<br />

End of document<br />

Print Date: December 29, 2016 Page 29 of 29<br />

© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

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