CAUTION: DO NOT TRY TO PUSH THE INSERT INTO THE COMPONENT DURING INSTALLATION

(4) Hold the inserting tool at 90 degrees to the hole and wind the mandrel clockwise until the insert is installed in the hole to a depth of 0,20 to 0,38 mm (0.008 to 0.015 in).

NOTE: If you carefully pull the body of the inserting tool away from the insert and do not move the mandrel, you can do a check of the depth of the insert during installation.

NOTE: The depth of the insert is measured from the surface of the component to the top of the insert.

(5) When the insert is installed to the correct depth, wind the mandrel counterclockwise to remove the inserting tool from the insert.

(6) Install the applicable tang removal tool in the insert and put the end of the tool on the tang of the insert.

(7) Hit the tang removal tool with a 6 to 8 oz hammer to remove the tang.

(8) Make sure that the tang has broken off correctly then remove and discard the tang from the component.

(9) Apply the torque that follows to the screwlock insert and make sure that it does not cause the insert to move:

(a) Screwlock insert (800): 0,16 N.m (1.5 lbf.in).

(b) Screwlock insert (810): 0,11 N.m (1.0 lbf.in).

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 TASK-29-11-69-380-801-A01

5. Repair No. 2: Repair of Damaged Anodic Film

WARNING: ALOCROM 1200 CAN BE DANGEROUS TO PERSONS. PUT ON SAFETY GOGGLES, RUBBER GLOVES AND PROTECTIVE CLOTHES. PUT ON A RESPIRATOR WHEN YOU SPRAY THE MATERIAL. IF YOU GET ALOCROM 1200 ON YOUR SKIN, CLEAN WITH SOAP AND WATER. IF YOU GET ALOCROM 1200 IN YOUR EYES, FLUSH WITH CLEAN WATER AND GET MEDICAL HELP. REMOVE CONTAMINATION FROM PROTECTIVE EQUIPMENT BEFORE THEY ARE STORED OR DISCARDED.

CAUTION: ALOCROM 1200 CAN CAUSE DAMAGE TO LEAD, GLASS, TIN, GALVANISED IRON AND MILD STEEL. USE POLYETHYLENE OR STAINLESS STEEL CONTAINERS AND EQUIPMENT.

Use Alocrom 1200 to repair damaged anodic film as given in NGPS 30.

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

This page is intentionally left blank.

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 ASSEMBLY

TASK-29-11-69-99C-807-A01 1. General

A. Make sure that the area where you assemble the hydraulic filter manifold and the tools you use to assemble the hydraulic filter manifold are clean.

B. Make sure that all parts are cleaned before assembly.

C. Make sure that the items given in Table 7001 are available to replace parts discarded during disassembly (Refer to Table 7001 “TABLE-29-11-69-99A-809-A01”).

TABLE-29-11-69-99A-809-A01

Replacement Parts—Table 7001

IPL FIG-ITEM No. NOMENCLATURE QUANTITY

1-52 ‘O’ ring seal (2346H000-002) 2

1-52A ‘O’ ring seal (2346H000-003, 2346H000-004, 2346H000-005 and 2346H000-006)

1-56 Back-up ring 1

1-58 ‘O’ ring seal 1

1-60 Filter element 1

1-112 ‘O’ ring seal 2

1-114 ‘O’ ring seal 1

1-116 Back-up ring 1

1-118 ‘O’ ring seal 1

1-120 Filter element (2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 and 2346H000-006)

1-120A Filter element (2346H000-006) 1

1-172 ‘O’ ring seal (2346H000-002) 2

1-172A ‘O’ ring seal (2346H000-003, 2346H000-004, 2346H000-005 and 2346H000-006)

1-175 ‘O’ ring seal 1

1-178 ‘O’ ring seal 1

1-180 Filter element 1

1-200 ‘O’ ring seal 1

1-210 Back-up ring 1

1-220 ‘O’ ring seal 1

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

1-240 ‘O’ ring seal 1

1-260 ‘O’ ring seal 1

1-310 ‘O’ ring seal 1

1-320 ‘O’ ring seal 1

1-330 Back-up ring 1

1-380 ‘O’ ring seal 1

1-390 ‘O’ ring seal 1

1-400 Back-up ring 1

1-450 ‘O’ ring seal 1

1-460 ‘O’ ring seal 1

1-470 Back-up ring 1

1-490 ‘O’ ring seal 1

1-510 ‘O’ ring seal 1

1-530 ‘O’ ring seal 1

1-550 Back-up ring 1

1-550A Back-up ring 1

1-560 ‘O’ ring seal 1

1-560A ‘O’ ring seal 1

1-570 Back-up ring 1

1-570A Back-up ring 1

1-580 ‘O’ ring seal 1

1-580A ‘O’ ring seal 1

1-600 ‘O’ ring seal 1

1-620 Back-up ring 1

1-630 ‘O’ ring seal 1

1-640 Back-up ring 1

1-650 ‘O’ ring seal 1

1-760 Back-up ring 1

IPL FIG-ITEM No. NOMENCLATURE QUANTITY

Replacement Parts (Sheet 2 of 2)—Table 7001

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 D. Each installation SUBTASK of these assembly procedures can be done independently.

E. All item numbers in parenthesis relate to IPL Figure 1.

F. Test the non-return valve (540 or 540A), check valve (610) and the three differential pressure indicators (270, 340 and 410) as given in TESTING AND FAULT ISOLATION before assembly.

TASK-29-11-69-94A-804-A01 2. Materials

The materials necessary for assembly are given in Table 7002 (Refer to Table 7002 “TABLE-29-11-69-99A-810-A01”).

TABLE-29-11-69-99A-810-A01 Assembly Materials—Table 7002

TASK-29-11-69-94B-803-A01 3. Special Tools and Equipment

The special tools and equipment given in Table 7003 are necessary for the procedures given in this Section (Refer to Table 7003 “TABLE-29-11-69-99A-811-A01”).

TABLE-29-11-69-99A-811-A01

Special Tools and Equipment for Assembly—Table 7003 NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Hydraulic fluid, phosphate ester

AS1241 Type IV Class I Commercially available

Lockwire MS20995C32 Commercially available

Assembly Materials —Table 7002

NOMENCLATURE PART No./TYPE USE

Assembly bullet 3422T000 Installation of ‘O’ ring seals and back-up rings

Open end crowfoot wrench, 7/8 inch AF

STARTRITE E2030 Installation of pressure transducer

Special Tools and Equipment for Assembly —Table 7003

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

TASK-29-11-69-400-801-A01 4. Procedure

SUBTASK-29-11-69-410-002-A01 A. Installation of Bypass Valve

WARNING: HYDRAULIC FLUID CAN BE DANGEROUS TO PERSONS. KEEP AWAY FROM OPEN FLAMES OR SOURCES OF IGNITION. DO NOT GET THE HYDRAULIC FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHES AND EYE PROTECTION.

NOTE: A shim (745) can be used on the by-pass valve (740) to adjust the cracking pressure as given in TESTING AND FAULT ISOLATION.

(1) Lubricate a new ‘O’ ring seal (750) with hydraulic fluid. Install a new back-up ring (760) and the ‘O’ ring seal (750) on the assembly bullet.

(2) Install the assembly bullet on the bypass valve (740) and move the back-up ring (760) and the ‘O’ ring seal (750) to the bypass valve (740).

(3) Install the bypass valve (740) in the manifold assembly (790) and tighten to a torque of 38,4 to 42,9 N.m (340 to 380 lbf.in).

SUBTASK-29-11-69-410-003-A01

B. Installation of Pressure Transducer

(1) Lubricate a new ‘O’ ring seal (710) with hydraulic fluid. Install the ‘O’ ring seal (710) on the pressure transducer (700).

(2) Install the pressure transducer (700) in the manifold assembly (790). Use the open end crowfoot wrench to tighten to a torque of 20,3 to 22,6 N.m (180 to 200 lbf.in).

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 SUBTASK-29-11-69-410-004-A01

C. Installation of Check Valve

(1) Lubricate a new ‘O’ ring seal (650) with hydraulic fluid. Install the ‘O’ ring seal (650) on the check valve (610).

(2) Lubricate a new ‘O’ ring seal (630) with hydraulic fluid. Install a new back-up ring (640), the ‘O’ ring seal (630) and a new back-up ring (620) on the check valve (610).

(3) Install the check valve (610) in the manifold assembly (790) and tighten to a torque of 96,6 to 106,8 N.m (855 to 945 lbf.in).

SUBTASK-29-11-69-410-005-A01 D. Installation of Non-return Valve

(1) Lubricate a new ‘O’ ring seal (580 or 580A) with hydraulic fluid. Install the ‘O’ ring seal on the non-return valve (540 or 540A).

(2) Lubricate a new ‘O’ ring seal (560 or 560A) with hydraulic fluid. Install a new back-up ring (570 or 570A), the ‘O’ ring seal (560 or 560A) and a new back-up ring (550 or 550A) in the groove of the non-return valve (540 or 540A).

(3) Install the non-return valve (540 or 540A) in the manifold assembly (790, 790A or 790B) and tighten to a torque of 129 to 142 N.m (1140 to 1260 lbf.in).

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

SUBTASK-29-11-69-410-006-A01 E. Installation of Pressure Switches

NOTE: The installation procedure for the two pressure switches (500 and 590) is the same.

(1) Lubricate a new ‘O’ ring seal (510 or 600) with hydraulic fluid. Install the ‘O’ ring seal (510 or 600) on the pressure switch (500 or 590).

(2) Install the pressure switch (500 or 590) in the manifold assembly (790) and tighten to a torque of 15,3 to 16,4 N.m (135 to 145 lbf.in).

SUBTASK-29-11-69-410-007-A01

F. Installation of Differential Pressure Indicators

NOTE: The installation procedure for the three differential pressure indicators (270, 340 and 410) is the same.

(1) If removed, install the protective cap (300, 370 or 440) on the differential pressure indicator (270, 340 or 410).

(2) Lubricate a new ‘O’ ring seal (320, 390 or 460) with hydraulic fluid. Install a new back-up ring (330, 400 or 470) and the ‘O’ ring seal (320, 390 or 460) on the assembly bullet.

(3) Install the assembly bullet on the differential pressure indicator (270, 340 or 410) and move the back-up ring (330, 400 or 470) and the ‘O’ ring seal (320, 390 or 460) to the widest groove of the differential pressure indicator (270, 340 or 410).

(4) Lubricate a new ‘O’ ring seal (310, 380 or 450) with hydraulic fluid. Install the ‘O’ ring seal (310, 380 or 450) in the thinner groove of the differential pressure indicator (270, 340 or 410).

(5) Install the differential pressure indicator (270, 340 or 410) and the clamp ring (290, 360 or 430) on the manifold assembly (790) and align their holes.

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (6) Install the four screws (280, 350 or 420) and measure and record the run-down torque

of each screw. The value must be more than 0,17 N.m (1.5 lbf.in).

(7) If the value is not more than 0,17 N.m (1.5 lbf.in), replace the screws (280, 350 or 420) and the screwlock inserts (810) and start this procedure again. Refer to REPAIR for replacement of screwlock inserts.

(8) If the value is more than 0,17 N.m (1.5 lbf.in), calculate the correct torque necessary for each screw (280, 350 or 420) with this formula:

1,2 N.m (11 lbf.in) + run-down torque = correct torque ± 0,1 N.m (1 lbf.in) (9) Tighten each screw (280, 350 or 420) to its calculated torque.

SUBTASK-29-11-69-410-008-A01 G. Installation of Unions

NOTE: The installation procedure for the seven unions (230, 250, 480, 520, 660, 680 and 720) is the same.

(1) Lubricate a new ‘O’ ring seal (240, 260, 490, 530, 670, 690 or 730) with hydraulic fluid.

Install the ‘O’ ring seal (240, 260, 490, 530, 670, 690 or 730) on the union (230, 250, 480, 520, 660, 680 or 720).

(2) Install the union (230, 250, 480, 520, 660, 680 or 720) in the manifold assembly (790) and tighten to the torque that follows:

(a) Reducer union (230): 80,2 to 89,3 N.m (710 to 790 lbf.in).

(b) Union (250): 18,1 to 20,3 N.m (160 to 180 lbf.in).

(d) Union (520): 48,0 to 53,7 N.m (425 to 475 lbf.in).

(e) Union (660): 96,6 to 106,8 N.m (855 to 945 lbf.in).

(f) Union (680): 28,8 to 32,2 N.m (255 to 285 lbf.in).

(g) Union (720): 11,9 to 13,0 N.m (255 to 285 lbf.in).

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

SUBTASK-29-11-69-410-009-A01

H. Installation of System Relief Valve

(1) Lubricate a new ‘O’ ring seal (220) with hydraulic fluid. Install the ‘O’ ring seal (220) on the assembly bullet.

(2) Install the assembly bullet on the system relief valve (190) and move the ‘O’ ring seal (220) to the groove above the thread of the system relief valve (190).

(3) Lubricate a new ‘O’ ring seal (200) with hydraulic fluid. Install a new back-up ring (210) and the ‘O’ ring seal (200) in the groove on the body the system relief valve (190).

(4) Install the system relief valve (190) in the manifold assembly (790) and tighten to a torque of 53,7 to 59,3 N.m (475 to 525 lbf.in).

SUBTASK-29-11-69-410-013-A01

I. Installation of Pressure Shut-off Valve

(1) Lubricate new ‘O’ ring seals (52), (54) and (58) with hydraulic fluid.

(2) Install the ‘O’ ring seal (58) and back-up ring (56) in the manifold assembly (790).

(3) Install the ‘O’ ring seal (54) on the shut-off valve piston (25).

(4) Install two ‘O’ ring seals (52) in their slots on the shut-off valve piston (25) for 2346H000-002.

(5) Install one ‘O’ ring seal (52) on the shut-off valve piston (25) for 2346H000-003, 2346H000-004, 2346H000-005 or 2346H000-006.

(6) Install the cup washer (28), spring (26), shut-off valve piston (25) and shut-off stop (22) in the manifold (790).

(7) Install the stop bolt (23) and measure and record the run-down torque. The value must be more than 0,45 N.m (4 lbf.in).

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (8) If the value is not more than 0,45 N.m (4 lbf.in), replace the stop bolt (23) and start this

procedure again.

(9) If the value is more than 0,45 N.m (4 lbf.in), calculate the correct torque necessary for the stop bolt (23) with this formula:

2,825 N.m (25 lbf.in) + run-down torque = correct torque ± 0,225 N.m (2 lbf.in) (10) Tighten the stop bolt (23) to its calculated torque.

SUBTASK-29-11-69-410-014-A01

J. Installation of Case Drain Shut-off Valve

(1) Lubricate new ‘O’ ring seals (112), (114) and (118) with hydraulic fluid.

(2) Install the ‘O’ ring seal (118) and back-up ring (116) in the manifold assembly (790).

(3) Install the ‘O’ ring seal (114) on the shut-off valve piston (86).

(4) Install the two ‘O’ ring seals (112) in their respective slots on the shut-off valve piston (86).

(5) Install the spring (88), shut-off valve piston (86) and shut-off stop (82) in the manifold (790).

(6) Install the stop bolt (84) and measure and record the run-down torque. The value must be more than 1,13 N.m (10 lbf.in).

(7) If the value is not more than 1,13 N.m (10 lbf.in), replace the stop bolt (84) and start this procedure again.

(8) If the value is more than 1,13 N.m (10 lbf.in), calculate the correct torque necessary for the stop bolt (84) with this formula:

1,125 N.m (10 lbf.in lbf.in) + run-down torque = correct torque ± 0,125 N.m (1 lbf.in) (9) Tighten the stop bolt (84) to its calculated torque.

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

SUBTASK-29-11-69-410-015-A01

K. Installation of Return Shut-off Valve

(1) Lubricate new ‘O’ ring seals (172), (175) and (178) with hydraulic fluid.

(2) Install the ‘O’ ring seal (178) in the manifold assembly (790).

(3) Install the ‘O’ ring seal (175) on the shut-off valve piston (145).

(4) Install two ‘O’ ring seals (172) in their slots on the shut-off valve piston (145) for 2346H000-002.

(5) Install one ‘O’ ring seal (172) on the shut-off valve piston (145) for 2346H000-003, 2346H000-004, 2346H000-005 or 2346H000-006.

(6) Install the cup washer (148), spring (146), shut-off valve piston (145) and shut-off stop (142) in the manifold (790).

(7) Install the stop bolt (143) and measure and record the run-down torque. The value must be more than 0,45 N.m (4 lbf.in).

(8) If the value is not more than 0,45 N.m (4 lbf.in), replace the stop bolt (143) and start this procedure again.

(9) If the value is more than 0,45 N.m (4 lbf.in), calculate the correct torque necessary for the stop bolt (143) with this formula:

2,825 N.m (25 lbf.in) + run-down torque = correct torque ± 0,225 N.m (2 lbf.in) (10) Tighten the stop bolt (143) to its calculated torque.

SUBTASK-29-11-69-410-010-A01 L. Installation of Locking Levers

NOTE: The installation procedure for the three locking levers (30, 90 and 150) is the same.

(1) Install the spring (50, 110 or 170) and the locking lever (30, 90 or 150) on the manifold assembly (790) and loosely attach with the shoulder bolt (40, 100 or 160).

(2) Measure and record the run-down torque of the shoulder bolt (40, 100 or 160). The value must be more than 0,17 N.m (1.5 lbf.in).

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 (3) If the value is not more than 0,17 N.m (1.5 lbf.in), replace the shoulder bolt (40, 100 or

160) and the screwlock insert (800) and start this procedure again. Refer to REPAIR for replacement of screwlock inserts.

(4) If the value is more than 0,17 N.m (1.5 lbf.in), calculate the correct torque necessary for the shoulder bolt (40, 100 or 160) with this formula:

1,2 N.m (11 lbf.in) + run-down torque = correct torque ± 0,1 N.m (1 lbf.in) (5) Tighten the shoulder bolt (40, 100 or 160) to its calculated torque.

SUBTASK-29-11-69-410-011-A01 M. Installation of Filter Elements

NOTE: The installation procedure for the three filter elements (60, 120 and 180) is the same.

(1) Remove the retaining ring (15, 75 or 135) from the bowl assembly (20, 80 or 140).

Install the filter element (60, 120 or 180) in the bowl assembly (20, 80 or 140) and attach with the retaining ring (15, 75 or 135).

(2) Lubricate the threads of the bowl assembly (20, 80 or 140) with hydraulic fluid. Push and hold the locking lever (30, 90 or 150) and install the bowl assembly (20, 80 or 140) in the manifold assembly (790). Tighten the bowl assembly (20, 80 or 140) with your hand.

(3) Release the locking lever (30, 90 or 150) and make sure that it engages fully with one of the serrations in the bowl assembly (20, 80 or 140). If necessary, adjust the position of the bowl assembly (20, 80 or 140) until the locking lever (30, 90 or 150) engages satisfactorily.

SUBTASK-29-11-69-700-001-A01 N. Testing

Do the main assembly tests given in TESTING AND FAULT ISOLATION.

SUBTASK-29-11-69-410-012-A01 O. Installation of Lockwire

(1) Safety the system relief valve (190) to the manifold assembly (790) with lockwire.

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

(2) Safety the pressure switch (500) to the manifold assembly (790) with lockwire.

(3) Safety the pressure switch (590) to the manifold assembly (790) with lockwire.

(4) Safety the pressure transducer (700) to the manifold assembly (790) with lockwire.

(5) Safety the bypass valve (740) to the manifold assembly (790) with lockwire.

SUBTASK-29-11-69-620-001-A01 P. Preservation

Do the preservation procedure given in STORAGE.

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 FITS AND CLEARANCES

TASK-29-11-69-99C-808-A01 1. General

Fits and clearances are not applicable to the hydraulic filter manifold.

TASK-29-11-69-820-801-A01 2. Run-down Torque Values

Run-down torque values for the attaching parts of the hydraulic filter manifold are shown in Table 8001 (Refer to Table 8001 “TABLE-29-11-69-99A-812-A01”).

TABLE-29-11-69-99A-812-A01

Run-down Torque Values—Table 8001

TASK-29-11-69-820-802-A01 3. Torque Values

Torque values for the components of the hydraulic filter manifold are shown in Table 8002 (Refer to Table 8002 “TABLE-29-11-69-99A-813-A01”).

NOMENCLATURE IPL FIG-ITEM No. RUN-DOWN TORQUE - N.m (lbf.in)

Bolt, stop 1-23 0,45 (4)

Bolt, shoulder 1-40 0,17 (1.5)

Bolt, stop 1-84 1,13 (10)

Bolt, shoulder 1-100 0,17 (1.5)

Bolt, stop 1-143 0,45 (4)

Bolt, shoulder 1-160 0,17 (1.5)

Screw, socket head cap 1-280 0,17 (1.5)

Screw, socket head cap 1-350 0,17 (1.5)

Screw, socket head cap 1-420 0,17 (1.5)

Run-down Torque Values —Table 8001

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

TABLE-29-11-69-99A-813-A01

Torque Values—Table 8002

NOMENCLATURE IPL FIG-ITEM No. TORQUE VALUE - N.m (lbf.in)

Bolt, stop 1-23 2,60 to 3,05 (23 to 27) + run-down torque

Bolt, shoulder 1-40 1,1 to 1,3 (10 to 12) + run-down torque

Bolt, stop 1-84 1,00 to 1,25 (9 to 11) + run-down torque

Bolt, shoulder 1-100 1,1 to 1,3 (10 to 12) + run-down torque

Bolt, stop 1-143 2,60 to 3,05 (23 to 27) + run-down torque

Bolt, shoulder 1-160 1,1 to 1,3 (10 to 12) + run-down torque

System relief valve 1-190 53,7 to 59,3 (475 to 525)

Reducer union 1-230 80,2 to 89,3 (710 to 790)

Union 1-250 18,1 to 20,3 (160 to 180)

Screw, socket head cap 1-280 1,1 to 1,3 (10 to 12) + run-down torque Screw, socket head cap 1-350 1,1 to 1,3 (10 to 12) + run-down torque Screw, socket head cap 1-420 1,1 to 1,3 (10 to 12) + run-down torque

Union 1-480 18,1 to 20,3 (160 to 180)

Pressure switch 1-500 15,3 to 16,4 (135 to 145)

Union 1-520 48,0 to 53,7 (425 to 475)

Non-return valve 1-540 129 to 142 (1140 to 1260)

Non-return valve 1-540A 129 to 142 (1140 to 1260)

Pressure switch 1-590 15,3 to 16,4 (135 to 145)

Check valve 1-610 96,6 to 106,8 (855 to 945)

Union 1-660 96,6 to 106,8 (855 to 945)

Union 1-680 28,8 to 32,2 (255 to 285)

Pressure transducer 1-700 20,3 to 22,6 (180 to 200)

Union 1-720 11,9 to 13,0 (255 to 285)

Bypass valve 1-740 38,4 to 42,9 (340 to 380)

Bypass valve 1-740A 38,4 to 42,9 (340 to 380)

Torque Values —Table 8002

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 SPECIAL TOOLS, FIXTURES AND EQUIPMENT

TASK-29-11-69-99C-809-A01 1. General

A. This Section gives a full list of special tools, fixtures, equipment and materials that are necessary for the procedures given in this manual.

B. Unless specified, the special tools, fixtures, equipment and materials shown are available from:

Honeywell Aerospace Yeovil Product Support Engineering Mail Box 702

Bunford Lane Yeovil BA20 2YD UK

Tel: +44 (0) 1935 446729 Fax: +44 (0) 1935 446581 TASK-29-11-69-94B-804-A01

2. Special Tools, Fixtures and Equipment

The special tools and equipment given in Table 9001 are necessary for the procedures given in this manual (Refer to Table 9001 “TABLE-29-11-69-99A-814-A01”).

TABLE-29-11-69-99A-814-A01

Special Tools, Fixtures and Equipment—Table 9001

NOMENCLATURE PART No./TYPE SUPPLIER

Flexible hoses - Commercially available

Shut-off valves (quantity 8) - Commercially available

Connection blanks - Commercially available

Pressure gauge,

0 to 31028 kPa (0 to 4500 psi)

- Commercially available

Drip spouts (quantity 3) - Commercially available

Special Tools, Fixtures and Equipment (Sheet 1 of 5)—Table 9001

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

Pressure/return filter element blank

5688K000

Case drain filter element blank

5689K000

Flowmeter, 0 to 75 l/min (0 to 20 US gpm)

Filter, 3 micron. Installed in the pressure supply line, upstream of the manifold assembly

- Commercially available

Voltmeter - Commercially available

Low resistance ohmmeter - Commercially available

Test fixture 5697K000

Pressure gauge, 0 to 35000 kPa (0 to 5000 psi)

- Commercially available

Pressure gauges, 0 to 750 kPa (0 to 100 psi)

(quantity 2)

- Commercially available

Pressure gauge, 0 to 100 kPa (0 to 10 psi)

- Commercially available

Flowmeter, 0 to 100 l/min (0 to 20 US gpm)

- Commercially available

Test fixture TBD

Test fixture 5747K000-001

NOMENCLATURE PART No./TYPE SUPPLIER

Special Tools, Fixtures and Equipment (Sheet 2 of 5)—Table 9001

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

Extracting tool 1227-06 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Inserting tool 3551-06 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Inserting tool 3551-2 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Tang removal tool 3580-06 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Tang removal tool 3580-2 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Plug tap 06CPB Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

NOMENCLATURE PART No./TYPE SUPPLIER

Special Tools, Fixtures and Equipment (Sheet 3 of 5)—Table 9001

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

Plug tap 2CPB Armstrong Fastening Systems Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Bottoming tap 06CBB Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Bottoming tap 2CBB Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Thread gauge 1440-06 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

(VK1012)

Thread gauge 1440-2 Armstrong Fastening Systems

Foster Street

Stoneferry Business Park Hull

East Yorkshire HU8 8BT UK

NOMENCLATURE PART No./TYPE SUPPLIER

Special Tools, Fixtures and Equipment (Sheet 4 of 5)—Table 9001

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006

TASK-29-11-69-94A-805-A01 3. Materials

The materials necessary for maintenance are given in Table 9002 (Refer to Table 9002 “TABLE-29-11-69-99A-815-A01”).

TABLE-29-11-69-99A-815-A01 Materials—Table 9002 Open end crowfoot

wrench, 7/8 inch AF

STARTRITE E2030 Startrite Designs Limited Courteney Road

NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Test fluid, phosphate ester hydraulic fluid

AS1241 Type IV Class I (Skydrol LD IV)

Commercially available

Cloth (must not contain lint) DEF1410 Commercially available

Isopropyl alcohol - Commercially available

Aqueous cleaning solution (refer to NGPS 256 Method 1C for mixture)

- Commercially available

Alkaline cleaning solution (refer to NGPS 256 Method 2 for mixture)

- Commercially available

Polyethylene bags - Commercially available

PVC or polyethylene gloves

Materials (Sheet 1 of 2)—Table 9002

NOMENCLATURE PART No./TYPE SUPPLIER

Special Tools, Fixtures and Equipment (Sheet 5 of 5)—Table 9001

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

Alocrom 1200 MIL-C-5541 DTD900/4413

ICI Paints Decorative Wexham Road Slough

Berks SL2 5DS UK

Hydraulic fluid, phosphate ester

AS1241 Type IV Class I Commercially available

Lockwire MS20995C32 Commercially available

Paper, waxed - Commercially available

Label, identification - Commercially available

Desiccant - Commercially available

Container, cardboard - Commercially available

Packing material, protective

- Commercially available

Tape, adhesive - Commercially available

NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Materials (Sheet 2 of 2)—Table 9002

COMPONENT MAINTENANCE MANUAL

Part No. 2346H000-002, 2346H000-003, 2346H000-004, 2346H000-005 AND 2346H000-006 STORAGE

TASK-29-11-69-99C-810-A01 1. General

A. This Section contains the procedures necessary for preservation, packing and storage.

B. The hydraulic fluid used for preservation must be clean to NAS1638, Table 1, Class 5 or better.

C. All item numbers in parenthesis relate to IPL Figure 1.

TASK-29-11-69-94A-806-A01 2. Materials

The materials necessary for preservation, packing and storage are given in Table 15001 (Refer to Table 15001 “TABLE-29-11-69-99A-816-A01”).

TABLE-29-11-69-99A-816-A01

Preservation, Packing and Storage Materials—Table 15001 NOTE: Equivalent alternatives can be used for these items.

NOMENCLATURE PART No./TYPE SUPPLIER

Hydraulic fluid, phosphate ester

AS1241 Type IV Class I Commercially available

Paper, waxed - Commercially available

Label, identification - Commercially available

Bag, polyethylene - Commercially available

Desiccant - Commercially available

Container, cardboard - Commercially available

Packing material, protective

- Commercially available

Tape, adhesive - Commercially available

Preservation, Packing and Storage Materials —Table 15001

RELEASED FOR THE EXCLUSIVE USE BY: COPA AIRLINES

TASK-29-11-69-620-801-A01 3. Preservation

A. Flush the hydraulic filter manifold with hydraulic fluid.

B. Drain all hydraulic fluid from the hydraulic filter manifold.

C. Put some new, clean hydraulic fluid in the hydraulic filter manifold to almost fill the assembly.

D. Install a protective cap (820) on the return inlet union (520).

E. Install a protective cap (820) on the non-return valve (540).

F. Install a protective cap (820) on the pressure outlet union (660).

G. Install the protective cap (830) on the return outlet union (230).

H. Install a protective cap (840) on the case drain outlet union (250).

I. Install a protective cap (840) on the case drain inlet union (480).

J. Install a protective cap (840) on the check valve (610).

K. Install a protective cap (840) on the ground service pressure union (680).

L. Install the protective cap (850) on the reservoir fill union (720).

TASK-29-11-69-530-801-A01 4. Packing

A. Put waxed paper around the unit.

B. Write a label with all the applicable data for the unit.

C. Put the unit, the label and some desiccant in a polyethylene bag. Make sure that the label can be read when all items are in the bag.

D. Remove unwanted air from the bag and seal the opening of the bag with heat.

E. Put the bag in a cardboard container with material for protection.

In document CMM 29-11-69 (Page 70-102)