Installation of the Aileron

TASK 27-14-41-400-001-A
Installation of the Aileron

WARNING: MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.

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

CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:

DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.

CAUTION: THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.

ZONE: 575
ZONE: 675

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 4M (13 FT)
No specific	1	CRANE 100KG (220 LB)
No specific	AR	SAFETY BARRIER(S)
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 0.13 and 0.11 m.daN (11.50 and 9.73 lbf.in )
No specific	Torque wrench: range to between 5.2 and 4.7 m.daN (38.35 and 34.66 lbf.ft )
No specific	Torque wrench: range to between 8.0 and 7.5 m.daN (59.00 and 55.31 lbf.ft )
98D27104000001	1	GUIDE CONE-AILERON
98D27104001000	1	FRAME-LIFTING ASSEMBLY,AILERON

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.03GBB1)	Synthetic Oil base Grease-General Purpose Clay Thickened -
(Material No.03GBC1)	Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. -
(Material No.06LCG9)	Non Hardening Jointing Putty-Medium Temp. Area - -
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.12ACC1)	Corrosion Preventive Compound-Heavy Duty Soft Film -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
575	AFT OUTBD SE OF WING AND TE FIXED STRUCT
675	AFT OUTBD SE OF WING AND TE FIXED STRUCT
575AT, 575KB, 575LB, 575MB, 590AB, 590BB, 675AT, 675KB, 675LB, 675MB, 690AB, 690BB

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
65	COTTER PINS	AIPC 27-14-05-20-080
104	COTTER PIN	AIPC 27-14-05-31-110
82	COTTER PIN	AIPC 27-14-05-31-110
65	COTTER PINS	AIPC 27-14-85-21-050
104	COTTER PIN	AIPC 27-14-85-31-100
82	COTTER PIN	AIPC 27-14-85-31-100

E. Referenced Information

REFERENCE	DESIGNATION
TASK 20-28-00-912-802-A	Electrical Bonding - General Maintenance Procedure
TASK 23-61-41-400-001-A	Installation of the Static Discharger
TASK 27-14-00-710-001-A	Operational Test of the Aileron and Hydraulic Actuation
TASK 27-14-00-820-001-A	Adjustment of the Aileron
TASK 27-50-00-866-009-A	Retraction of the Flaps on the Ground
TASK 27-50-00-866-009-A-01	Retraction of the Flaps/Slats on the Ground
TASK 29-10-00-863-001-A	Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-863-003-A	Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart
TASK 29-10-00-863-003-A-01	Pressurize the Blue Hydraulic System with the Blue Electric Pump
TASK 29-10-00-864-001-A	Depressurize the Green Hydraulic System
TASK 29-10-00-864-003-A	Depressurize the Blue Hydraulic System
TASK 29-14-00-614-001-A	Depressurization of the Hydraulic Reservoirs
TASK 29-23-00-863-001-A	Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
TASK 57-51-37-000-005-A	Removal of the Access Panels 575KB(675KB), 575LB(675LB), 575MB(675MB)
TASK 57-51-37-000-007-A	Removal of the Access Panel
TASK 57-51-37-400-005-A	Installation of the Access Panels 575KB(675KB), 575LB(675LB), 575MB(675MB)
TASK 57-51-37-400-007-A	Installation of the Access Panel
TASK 12-22-00-00	LUBRICATION - DESCRIPTION AND OPERATION
Aileron - Location and Detail
Aileron Attachment - Hinges and Actuators
Aileron - Upper and Lower Seals

3. Job Set-up
Subtask 27-14-41-941-053-A

A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the WARNING NOTICE(S) to tell persons not to operate the flight controls is in position.

Subtask 27-14-41-860-051-A

B. Aircraft Maintenance Configuration

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

(1) Make sure that the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-009).
(2) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is on the flap/slat control lever.
(3) Make sure that the Green and the Blue Hydraulic systems are depressurized (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-003).
(4) Make sure that the applicable hydraulic reservoir is depressurized (Ref. AMM TASK 29-14-00-614-001).
(5) Make sure that the ACCESS PLATFORM 4M (13 FT) is in position below the applicable zone 575(675).
(6) Make sure that the applicable access panels are removed (Ref. AMM TASK 57-51-37-000-007), (Ref. AMM TASK 57-51-37-000-005):

For the left wing, panels 575AT 575MB 575KB 575LB 590AB 590BB
For the right wing, panels 675AT 675MB 675KB 675LB 690AB 690BB.

Subtask 27-14-41-865-051-A

C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B11
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
** ON A/C ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20

4. Procedure

CAUTION: BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:

DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.

Subtask 27-14-41-420-053-C

A. Preparation for Installation

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

(1) Use a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean:

The head of each bolt (84), (95) and (97)
The nuts (75), (106) and (107)
The ends of the bonding straps (77), (90) and (99).

(2) Clean the component interfaces and/or the adjacent areas with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Lubricate these parts with Non Hardening Jointing Putty-Medium Temp. Area - - (Material No.06LCG9) :

For hinge No.s 2 and 3, the bushes (70)
The bushes (78), (91) and (100)
The hinge pins (71) and (92)
The flanged bushes (66)
The pins (67)
The installed bushes in the attachment brackets.

Subtask 27-14-41-420-051-C

B. Install the Bushes in the Hinges
(1) For hinge No. 1, install the bush (78).
(2) For hinge No.s 2 and 3, install the bushes (70) and (78).
(3) For hinge No.s 4 and 5, install the bushes (91) and (100).

Subtask 27-14-41-560-050-A

C. Preparation of a Replacement Component
(1) If it is necessary to replace the aileron, install the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON:
(a) Make sure that the side plates on the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON are correctly installed.
(b) Make sure that the adjuster assemblies on the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON are as far apart as possible.
(2) Lift the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON with the CRANE 100KG (220 LB) and put the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON around the aileron, at the same distance from each end.

NOTE: The weight of the aileron and the brackets is 50 kg (110.23 lb).

(3) To lock the lifting frame assembly:

CAUTION: DO NOT TIGHTEN THE ADJUSTER ASSEMBLIES ON THE LIFTING FRAME TOO MUCH OR YOU WILL DAMAGE THE AILERON.

(a) Tighten the adjuster assemblies on the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON to lock the aileron in position.

Subtask 27-14-41-420-052-L

D. Installation of the Aileron

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

(1) Use the crane to put the aileron in position.
(2) For hinges No 1, 2 and 3, do the steps that follow:
(a) Install the 98D27104000001 GUIDE CONE-AILERON on the hinge pin (71).
(b) Install the hinge pin (71) with the head outboard.
(c) Remove the 98D27104000001 GUIDE CONE-AILERON.
(d) Make sure that the hinge pin (71) is correctly aligned, so that the locking plate (72) can be installed.
(e) Install the washer (79) and the nut (80) on the hinge pin (71).
(f) TORQUE the nut (80) to between 5.2 and 4.7 m.daN (38.35 and 34.66 lbf.ft )

.
(g) Install the locking cap (81) on the nut (80).
(h) Safety the locking cap (81) with the new AIPC 27-14-05-31-110 COTTER PIN (82) or AIPC 27-14-85-31-100 COTTER PIN (82).
(i) Install the locking plate (72), the bolt (73) and the nut (74).
(j) Install the bonding strap (77), the washers (76) and (83), the bolt (84) and the nut (75) (Ref. AMM TASK 20-28-00-912-802).
(3) For hinges No 4 and 5, do the steps that follow:
(a) Install the 98D27104000001 GUIDE CONE-AILERON on the hinge pin (92).
(b) Install the hinge pin (92) with the head outboard.
(c) Remove the 98D27104000001 GUIDE CONE-AILERON.
(d) Make sure that the head of the hinge pin (92) is correctly aligned, so that the locking plate (93) can be installed.
(e) Install the washer (101) and the nut (102) on the hinge pin (92).
(f) TORQUE the nut (102) to between 5.2 and 4.7 m.daN (38.35 and 34.66 lbf.ft )

.
(g) Install the locking cap (103) on the nut (102).
(h) Safety the locking cap (103) with the new AIPC 27-14-05-31-110 COTTER PIN (104) or AIPC 27-14-85-31-100 COTTER PIN (104).
(i) Install the locking plate (93) and the bolt (94).
(j) Install the bonding strap (90), the washers (96) and (108), the bolt (95) and the nut (107) (Ref. AMM TASK 20-28-00-912-802).
(4) For hinge No 5, install the bonding strap (99), the washers (98) and (105), the bolt (97) and the nut (106) (Ref. AMM TASK 20-28-00-912-802).
(5) Hold the aileron, loosen the adjuster assemblies and remove the 98D27104001000 FRAME-LIFTING ASSEMBLY,AILERON from the aileron.
(6) Install the flanged bush (66) in each actuator attachment bracket.
(7) Apply Synthetic Oil base Grease-General Purpose Clay Thickened - (Material No.03GBB1) or Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) to the threads of the pins (67).

NOTE: For the lubricant grease specification and lubrication requirements, refer to (Ref. AMM D/O 12-22-00-00).

(8) Make sure that you do not get Material No 15-007 on the servocontrol spherical bearings in the step that follows.
(9) Apply Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the eye-ends of the piston rods on the rounded side only.
(10) Align the eye-ends of actuators No 1 and No 2:

CAUTION: IF YOU CANNOT ALIGN THE ACTUATOR EYE-ENDS WITH THE HOLES OF THE ATTACHMENT BRACKETS, DO NOT PUSH THE AILERON TOO FAR INTO THE UPPER POSITION. IF YOU DO, YOU WILL CAUSE DAMAGE TO THE AILERON LEADING EDGE. MANUALLY RETRACT OR EXTEND THE ACTUATOR ROD TO ALIGN THE HOLES.

(a) Align the eye-ends of actuators No 1 and No 2 with the holes of the actuator attachment brackets.
(11) Install the pins (67) with the heads outboard.
(12) Make sure that the heads of the pins (67) are correctly aligned, so that the locking plates (68) can be installed.
(13) Install the washers (62) and the nuts (63) on the pins (67).
(14) TORQUE the nuts (63) to between to between 8.0 and 7.5 m.daN (59.00 and 55.31 lbf.ft )

.
(15) Install the locking caps (64) on the nuts (63).
(16) Safety the locking caps (64) with the new AIPC 27-14-05-20-080 COTTER PINS (65) or AIPC 27-14-85-21-050 COTTER PINS (65).
(17) Install the locking plates (68), the washers (60), the bolts (69) and the nuts (61).
(18) Make sure that you do not get Material No 15-007 on the servocontrol spherical bearings in the steps that follow.
(19) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:

The bolts (69)
The washers (60) and (62)
The nuts (61) and (63)
The locking caps (64)
The cotter pins (65)
The pins (67).

(20) For hinges No 1, 2 and 3, apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:

The hinge pin (71)
The bolt (73)
The nuts (74) and (80)
The washer (79)
The locking cap (81)
The cotter pin (82).

(21) For hinges No 4 and 5, apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to:

The hinge pin (92)
The bolt (94)
The washer (101)
The nut (102)
The locking cap (103)
The cotter pin (104).

(22) Remove the 98D27104002000 SUPPORT-AILERON ACTUATOR.
(23) Move the aileron through its travel range and examine for:

Free movement
The correct installation of the applicable bonding straps (77), (90) and (99).

(24) For hinges No 1, 2 and 3, seal the bonded items that follow (Ref. AMM TASK 20-28-00-912-802):

The bolt (84)
The nut (75)
The washers (76) and (83)
The bonding strap (77).

(25) For hinges No 4 and 5, seal the bonded items that follow (Ref. AMM TASK 20-28-00-912-802):

The bolt (95)
The nut (107)
The washers (96) and (108)
The bonding strap (90).

(26) For hinge No 5, seal the bonded items that follow (Ref. AMM TASK 20-28-00-912-802):

The bolt (97)
The nut (106)
The washers (98) and (105)
The bonding strap (99).

(27) Install the static dischargers (Ref. AMM TASK 23-61-41-400-001).

Subtask 27-14-41-410-050-A

E. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panels (Ref. AMM TASK 57-51-37-400-007), (Ref. AMM TASK 57-51-37-400-005):
(a) For the left wing, install 575AT 575MB 575KB 575LB 590AB 590BB.
(b) For the right wing, install 675AT 675MB 675KB 675LB 690AB 690BB.

Subtask 27-14-41-820-051-A

F. Adjustment of the Aileron Upper and Lower Seals

Aileron - Location and Detail

Aileron - Upper and Lower Seals

(1) Manually align the aileron with the trailing edge structure (to its neutral position).
(2) Make sure that dimensions W and Z are between 0.0 mm (0.00 in.) and 0.5 mm (0.02 in.). If necessary, adjust the seals (2), (4) and (6) then tighten the screws (1) and (5).
(3) Loosen the screws (3) on applicable panels 575AT ( 675AT), 575KB ( 675KB), 575LB ( 675LB) or 575MB ( 675MB) to let you move the seals (4).
(4) Position the seals (4) until dimension Y is 18 mm (0.71 in.) + 0 mm (0.00 in.) - 2 mm (0.08 in.). Make sure that dimension X is between 0.0 mm (0.00 in.) and 0.5 mm (0.02 in.). If necessary, adjust the seals (4) to get the two dimensions, then TORQUE the screws (3) to between 0.13 and 0.11 m.daN (11.50 and 9.73 lbf.in )

NOTE: Make sure that the seals are not above a level between the upper surface of the access panels and the aileron.

(5) Manually push the aileron up as far as possible. Make sure that the lower panel seals do not go below the leading edge of the aileron hinge/actuator points.
(6) Slowly move the aileron to its neutral position and monitor the seals. Make sure that they do not catch the leading edge of the aileron hinge/actuator points.
(7) Manually push the aileron down as far as possible. Make sure that the upper panel seal 575AT(675AT) and the fixed panel seal do not catch the aileron upper surface.
(8) Move the aileron to its neutral position and monitor the upper seals. Make sure that they do not catch the aileron hinge/actuator points.
(9) If the seals catch the aileron, loosen the applicable screws (3). Adjust the seal(s) at the point where they catch and TORQUE the screws (3) to between 0.13 and 0.11 m.daN (11.50 and 9.73 lbf.in )

.
(10) Do the steps (3) thru (8) again.

Subtask 27-14-41-863-050-A

G. Pressurize the Hydraulic Systems

WARNING: MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN CAUSE SERIOUS INJURY AND/OR DAMAGE.

(1) Pressurize the Green hydraulic system
(Ref. AMM TASK 29-10-00-863-001) or (Ref. AMM TASK 29-23-00-863-001).
(2) Pressurize the Blue hydraulic system
(Ref. AMM TASK 29-10-00-863-003).
(3) Remove the access platform(s).

Subtask 27-14-41-865-052-A

H. 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
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B11
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
** ON A/C ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20

Subtask 27-14-41-710-050-A

I. Test

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

(1) Do the adjustment of the ailerons (Ref. AMM TASK 27-14-00-820-001).
(2) Do an operational test on the ailerons (Ref. AMM TASK 27-14-00-710-001). During the operational test, make sure that the ailerons move correctly.

5. Close-up
Subtask 27-14-41-942-050-A

A. Removal of Equipment
(1) Remove the SAFETY BARRIER(S).
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.01 06:47:14 UTC