Installation of the Fuel Filter Element [IAE]

TASK 73-12-42-400-010-B
Installation of the Fuel Filter Element

WARNING: DO NOT LET ENGINE OIL STAY ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.

WARNING: BE CAREFUL NOT TO GET AIRCRAFT FUEL IN YOUR MOUTH OR IN YOUR EYES. IF YOU GET FUEL ON YOUR SKIN OR ON YOUR CLOTHES, FLUSH IT IMMEDIATELY WITH WATER. IF NECESSARY, GET MEDICAL HELP. AIRCRAFT FUEL IS POISONOUS.

WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

CAUTION: DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.

ZONE: 210
ZONE: 400
FIN: 2000EM1 ** ON A/C NOT FOR ALL

1. Reason for the Job
This TASK is for V2500-A5 engines.
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 95 and 85 lbf.in (1.07 and 0.96 m.daN )
No specific	Torque wrench: range to between 120 and 110 lbf.in (1.36 and 1.24 m.daN )

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.V02-119)	corrosion-resistant steel lockwire
(Material No.V02-147)	lockwire
(Material No.V10-077)	lubricant (engine oil)

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
210	CKPT,FWD COMPT BHD TO FLT COMPT BULKHEAD
400	POWER PLANT, NACELLES AND PYLONS
FOR [1000EM1] (ENGINE-1)
437AL, 438AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
4	SEALING RING	AIPC 73-12-42-80-040
3	FUEL FILTER ELEMENT	AIPC 73-12-42-80-050
5	SEALING RING	AIPC 73-12-42-80-070

E. Referenced Information

REFERENCE	DESIGNATION
TASK 70-23-11-911-013-A	General Torque Tightening Techniques
TASK 70-23-13-911-010-A	Procedures for the Installation of Preformed Packings
TASK 70-40-11-911-014-A	Locking Devices General Information
TASK 71-00-00-710-012-B	Test No.3 : Idle Leak Check
TASK 71-13-00-010-010-A	Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-010-A	Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
Fuel Filter Element

3. Job Set-up
Subtask 73-12-42-860-051-A ** ON A/C NOT FOR ALL

A. Aircraft Maintenance Configuration
(1) On the center pedestal, on the ENG panel 115VU, make sure that the WARNING NOTICE(S) is in position to tell persons not to start the engine.
(2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that the WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).

Subtask 73-12-42-010-053-A ** ON A/C NOT FOR ALL

B. Make sure that the fan cowl doors are open (Ref. AMM TASK 71-13-00-010-010):
(1) FOR [1000EM1] (ENGINE-1)
437AL 438AR.
(2) FOR [1000EM2] (ENGINE-2)
447AL 448AR.

Subtask 73-12-42-630-051-A ** ON A/C NOT FOR ALL

C. Make sure that the cover is removed from the Fuel Cooled Oil Cooler (FCOC).

4. Procedure
Subtask 73-12-42-420-055-A ** ON A/C NOT FOR ALL

A. Installation of the Fuel Filter Element.

POST SBE 79-0086

(1) Carefully install the new AIPC 73-12-42-80-050 FUEL FILTER ELEMENT (3) into the opening of the FCOC housing.

NOTE: Make sure that the fuel filter element is in the correct position in the FCOC housing.

END OF POST SBE 79-0086

Subtask 73-12-42-210-063-A ** ON A/C NOT FOR ALL

B. Do an inspection of the cap assembly (8), FCOC mating faces.

POST SBE 79-0086

(1) Examine the cap assembly (8) mating face.
(a) If damaged, reject the FCOC.
(2) Examine the sealing ring location on the cap assembly (8).
(a) If damaged, reject the FCOC.
(3) Examine the FCOC mating face.
(a) If damaged, reject the FCOC.

END OF POST SBE 79-0086

Subtask 73-12-42-410-056-A ** ON A/C NOT FOR ALL

C. Installation of the Cap Assembly

POST SBE 79-0086

(1) Lubricate the new AIPC 73-12-42-80-040 SEALING RING (4) with the V10-077lubricant (engine oil) and install the sealing ring (4) in the groove of the cap assembly (8) (Ref. AMM TASK 70-23-13-911-010). Make sure that the sealing ring is not twisted when you install it.
(2) Make sure that the end seal outer diameter of the fuel filter element is aligned with the internal diameter of the cap assembly.
(3) Put the cap assembly (8) in position on the flange of the fuel cooled oil-cooler.
(4) Make sure that the cap assembly (8) is correctly installed and the holes are aligned.
(5) Install the washers (2) and the nuts (1), initially with your hand. Gradually tighten the nuts in a symmetrical sequence so a single nut is never subjected to the total spring force on the cap assembly.
(6) TORQUE the nuts to between 95 and 85 lbf.in (1.07 and 0.96 m.daN )

adhering strictly (Ref. AMM TASK 70-23-11-911-013). Torque the nuts evenly and smoothly in a symmetrical sequence. This will ensure that the components move together gradually and do not become damaged (Ref. AMM TASK 70-23-11-911-013).
(7) Install the fuel drain plug (6).
(8) Lubricate the new AIPC 73-12-42-80-070 SEALING RING (5) with the clean V10-077lubricant (engine oil) and install the sealing ring (5) on the fuel drain plug (6) (Ref. AMM TASK 70-23-13-911-010).
(9) Install the fuel drain plug (6) on the fuel plug (7).
(10) TORQUE the fuel drain plug to between 120 and 110 lbf.in (1.36 and 1.24 m.daN )

(Ref. AMM TASK 70-23-11-911-013).

WARNING: USE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.

(11) Safety the fuel drain plug to the fuel plug either with the lockwire (Material No.V02-147) or the corrosion-resistant steel lockwire (Material No.V02-119) (Ref. AMM TASK 70-40-11-911-014).

END OF POST SBE 79-0086

5. Close-up
Subtask 73-12-42-410-051-A ** ON A/C NOT FOR ALL

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR.
(b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
(3) Remove the WARNING NOTICE(S).

Subtask 73-12-42-865-056-A ** ON A/C NOT FOR ALL

B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
FOR FIN: 1000EM1 (ENGINE1)
49VU	FUEL/LP VALVE/MOT1/ENG1	1QG	A08
121VU	FUEL/LP VALVE/MOT2/ENG1	3QG	M25
FOR FIN: 1000EM2 (ENGINE2)
49VU	FUEL/LP VALVE/MOT1/ENG2	2QG	A09
121VU	FUEL/LP VALVE/MOT2/ENG2	4QG	M26

Subtask 73-12-42-790-051-A ** ON A/C NOT FOR ALL

C. Do an idle leak check of the FCOC housing (Ref. AMM TASK 71-00-00-710-012). Leaks are not permitted.

[Rev.10 from 2021] 2026.04.01 07:30:44 UTC