Installation of the Outboard Double-Slotted Flap

TASK 27-54-62-400-002-A
Installation of the Outboard Double-Slotted Flap

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.

ZONE: 500
ZONE: 600

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

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 3M (10 FT)
No specific	AR	SAFETY BARRIER(S)
No specific	AR	TAPE - ADHESIVE
No specific	AR	WARNING NOTICE(S)
No specific	Torque wrench: range to between 27 and 24 m.N (19.91 and 17.70 lbf.ft )
No specific	Torque wrench: range to between 0.132 and 0.108 m.daN (11.68 and 9.56 lbf.in )
No specific	Torque wrench: range to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in )
No specific	Torque wrench: range to between 1.0 and 0.9 m.daN (88.50 and 79.65 lbf.in )
No specific	Torque wrench: range to between 2.7 and 1.4 m.daN (19.91 and 10.32 lbf.ft )
No specific	Torque wrench: range to between 2.2 and 1.95 m.daN (16.22 and 14.38 lbf.ft )
No specific	Torque wrench: range to between 2.4 and 2.2 m.daN (17.70 and 16.22 lbf.ft )
No specific	Torque wrench: range to between 3.0 and 2.6 m.daN (22.12 and 19.17 lbf.ft )
No specific	Torque wrench: range to between 3.6 and 3.1 m.daN (26.55 and 22.86 lbf.ft )
No specific	Torque wrench: range to between 3.8 and 3.3 m.daN (28.02 and 24.34 lbf.ft )
No specific	Torque wrench: range to between 7.6 and 6.6 m.daN (56.05 and 48.67 lbf.ft )
No specific	Torque wrench: range to between 7.8 and 6.8 m.daN (57.52 and 50.15 lbf.ft )
No specific	Torque wrench: range to between 20 and 15 m.daN (147.49 and 110.62 lbf.ft )
98D27504083000	1	EXTRACTOR - PIN TRACKS 2 AND 3
98D27504084000	1	EXTRACTOR - PIN, TRACK 4
98D27504115000	2	GAUGES-DISTANCE
98D27504118000	1	SPANNER - FLAP ADJUSTMENT
98D27504119000	1	SPANNER - FLAP ADJUSTMENT
98D27804001000	1	ADAPTOR-DRIVE, SLAT (AND FLAP)

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.06ABB1)	Polysulfide Sealant-Fuel Tank Fillet -
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.12ACC1)	Corrosion Preventive Compound-Heavy Duty Soft Film -
(Material No.14QFB1)	Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
500	LEFT WING
600	RIGHT WING
573CB, 575AB, 575BB, 673CB, 675AB, 675BB

D. Expendable Parts

FIG.ITEM	DESIGNATION	IPC-CSN
127	COTTER PIN	AIPC 27-54-05-32-090
127	COTTER PIN	AIPC 27-54-05-32-190
144	COTTER PIN	AIPC 27-54-46-24-010
142	CRUSHABLE WASHER	AIPC 27-54-46-24-030
41	COTTER PIN	AIPC 27-54-46-24-095
144	COTTER PIN	AIPC 27-54-46-26-010
142	CRUSHABLE WASHER	AIPC 27-54-46-26-030
78	COTTER PIN	AIPC 27-54-46-26-280
127	COTTER PIN	AIPC 27-54-85-35-210
127	COTTER PIN	AIPC 27-54-85-35-220
24	COTTER PIN	AIPC 57-52-23-03-270
18	COTTER PIN	AIPC 57-52-23-03-328
21	SPACER(S)	AIPC 57-52-23-03-360
107	COTTER PIN	AIPC 57-53-23-03-130
107	COTTER PIN	AIPC 57-53-23-04-130
46	COTTER PIN	AIPC 57-53-23-10-070
69	COTTER PIN	AIPC 57-53-23-11-070

E. Referenced Information

REFERENCE	DESIGNATION
TASK 20-28-00-912-802-A	Electrical Bonding - General Maintenance Procedure
TASK 27-50-00-000-002-A	Removal of the Inboard and Outboard Flap Hoisting-Sling
TASK 27-50-00-400-002-A	Installation of the Inboard and Outboard Flap Hoisting-Sling
TASK 27-50-00-866-008-A	Extension of the Flaps on the Ground
TASK 27-50-00-866-008-A-01	Extension of the Flaps/Slats on the Ground
TASK 27-50-00-866-012-A	Manual Retraction of the Flaps
TASK 27-51-00-820-003-A	To do a Check of the Flap Rigged Position (with the Sharks Fin)
TASK 27-51-00-820-009-A	Adjustment (Rigging) of the Flaps with the Sharks Fin Tool (A321)
TASK 27-51-44-000-001-A	Removal of the Interconnecting Strut
TASK 27-51-44-400-001-A	Installation of the Interconnecting Strut
TASK 27-54-00-710-001-A	Operational Test of the Flap System
TASK 27-54-41-000-001-A	Removal of the Right Angle Gearbox
TASK 27-54-41-400-001-A	Installation of the Right Angle Gearbox
TASK 27-54-61-000-002-A	Removal of the Flap Kink-Seals and Cushion-Seals
TASK 27-54-61-400-006-A	Installation of the Flap Kink-Seals and Cushion-Seals
TASK 27-54-63-000-001-A	Removal of the Flap Guide-Roller Assembly
TASK 27-54-63-400-001-A	Installation of the Flap Guide-Roller Assembly
TASK 27-60-00-866-002-A	Extension-Retraction of the Spoilers for Maintenance
TASK 27-64-00-710-001-A	Operational Test of the Spoiler Hydraulic Actuation
TASK 27-64-00-820-001-D	Adjustment of the Spoilers
TASK 57-55-11-010-002-A	To Lower the Flap Track No. 3 & No. 4 Movable Fairings for Access
TASK 57-55-11-410-002-A	To Lift the Flap Track No. 3 & No. 4 Movable Fairings after Access
TASK 12-22-00-00	LUBRICATION - DESCRIPTION AND OPERATION
Flap to Rotary Actuator Drive-Levers ** ON A/C NOT FOR ALL
Flap to Rotary Actuator Drive-Levers ** ON A/C NOT FOR ALL
Flap to Flap Carriage Connection
Distance Gages - Location and Detail
Details of the Z-Coupling
Details of the Tab Drive Control-Rod (Track 3)
Details of the Tab Drive Control-Rod (Track 4)
Details of the Blade Seal
Alignment of the Inboard Cruise Roller
Flap Removal and Installation Tools
Clearance of the Flap Drive-Arm Bolt at the Track 3 Position
Outboard Flap Forward-Eccentrics - Location and Detail
Slave Pins and Rigging Pin - Location and Detail
Alignment of the Outer Roller of the Outboard Flap
Interconnecting Strut - Location and Detail

3. Job Set-up
Subtask 27-54-62-941-061-A ** ON A/C NOT FOR ALL

A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the WARNING NOTICE(S) is in position on panel 400VU to tell persons not to operate the landing gear.
(3) Make sure that the WARNING NOTICE(S) is in position on panel 114VU to tell persons not to operate the flight controls.

Subtask 27-54-62-865-055-A ** ON A/C NOT FOR ALL

B. 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/FLP/CTL AND MONG/SYS1	6CV	B07
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1	6CV	B02
** ON A/C NOT FOR ALL
121VU	FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2	8CV	Q21

Subtask 27-54-62-860-061-A ** ON A/C NOT FOR ALL

C. 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 ACCESS PLATFORM 3M (10 FT) is in position below the applicable outboard flap.
(2) Make sure that the applicable access panels are removed:

for the left wing, panels 573CB, 575AB and 575BB
for the right wing, panels 673CB, 675AB and 675BB.

(3) Make sure that the applicable torque shaft has been disconnected from the right angle gearbox (Ref. AMM TASK 27-54-41-000-001).
(4) Make sure that the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) is installed on the right angle gearbox.
(5) Make sure that the applicable spoilers 2, 3, 4 and 5 are fully extended and locked.
(6) Make sure that a 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER is installed on each of the servo controls.
(7) Make sure that the flap track No. 3 and No. 4 movable fairings have been lowered (Ref. AMM TASK 57-55-11-010-002).
(8) Make sure that the flap kink seals have been removed (Ref. AMM TASK 27-54-61-000-002).

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 27-54-62-420-085-B ** ON A/C NOT FOR ALL

A. Preparation for Installation
(1) Remove the covers from the flaps.
(2) Clean the component interface and/or the adjacent area with a Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
(5) At the track 3 and the track 4 positions:

Flap to Rotary Actuator Drive-Levers ** ON A/C NOT FOR ALL

Flap to Flap Carriage Connection ** ON A/C NOT FOR ALL

Distance Gages - Location and Detail ** ON A/C NOT FOR ALL

(a) Make sure that the rotary actuator drive-levers (128) are in the fully extended position.
(b) Make sure that the carriage assemblies touch the end stops (149).
(c) Make sure that the 98D27504115000 GAUGES-DISTANCE (86) and (89) are installed.
(6) Make sure that the Z-coupling lever (17) on the outboard flap and the Z-coupling lever (27) on the inboard flap are held with TAPE - ADHESIVE.

Details of the Z-Coupling ** ON A/C NOT FOR ALL

(7) If necessary, remove the flap guide-roller assembly (Ref. AMM TASK 27-54-63-000-001).
(8) If necessary, remove the interconnecting strut from the inboard flap (Ref. AMM TASK 27-51-44-000-001).
(9) At the track 3 position, if installed, remove the tab drive control-rod (50) from the flap attachment bracket (44):

Details of the Tab Drive Control-Rod (Track 3) ** ON A/C NOT FOR ALL

(a) Remove and discard the cotter pin (46).
(b) Remove the nut (47), the washer (48), the bolt (43) and the loose bush (49).
(10) At the track 4 position, if installed, remove the tab drive control-rod (73) from the flap attachment bracket (67):

Details of the Tab Drive Control-Rod (Track 4) ** ON A/C NOT FOR ALL

(a) Remove and discard the cotter pin (69).
(b) Remove the nut (70), the washer (71), the bolt (66) and the loose bush (72).

Subtask 27-54-62-420-063-B ** ON A/C NOT FOR ALL

B. Installation of the Outboard Flap
(1) If necessary, install the hoisting sling (Ref. AMM TASK 27-50-00-400-002).
(2) Make sure that the blade seal (164) is in the fully retracted position.

Details of the Blade Seal ** ON A/C NOT FOR ALL

(3) Remove the cushion seal (175) and make sure that the cruise roller (180) (at the inboard end of the outboard flap) is aligned at the minimum position.

Alignment of the Inboard Cruise Roller ** ON A/C NOT FOR ALL

(4) Install the flap on the wing:

Flap to Flap Carriage Connection ** ON A/C NOT FOR ALL

CAUTION: MAKE SURE THAT THE FLAP DOES NOT HIT THE AIRCRAFT STRUCTURE.

(a) With the hoist and the hoisting sling, carefully lift the flap and put it in position above the wing.
(b) Lower the flap and engage the spherical bearings in the flap track 3 and the flap track 4 carriages.
(5) Make sure that the flap spherical bearing is set to its nominal position. At this position:

the painted (red) marks on the spherical bearing are aligned, and/or
the hole of the spherical bearing is at its maximum aft position.

(a) If necessary, repair the painted (red) marks.
(6) Apply a thin layer of 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 bolts (150).

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

(7) If necessary, install:

Flap Removal and Installation Tools ** ON A/C NOT FOR ALL

the 98D27504083000 EXTRACTOR - PIN TRACKS 2 AND 3 at the track 3 carriage to the bolt (150)
the 98D27504084000 EXTRACTOR - PIN, TRACK 4 at the track 4 carriage to the bolt (150).

NOTE: Make sure that you screw the extractor tools fully on to the threads. This will let the carriage bushes compress the retaining wire ring (151) when the bolts (150) are installed.

(8) Install the splined bushes (140):

CAUTION: MAKE SURE THAT THE SPLINED BUSH IS FULLY ENGAGED WITH THE SPHERICAL BEARING. THIS PREVENTS DAMAGE TO THE PARTS.

(a) Install the splined bushes (140).
(9) Install the bolts (150):

CAUTION: DO NOT REMOVE THE RETAINING WIRE RING FROM THE CARRIAGE BOLT ASSEMBLY. IF YOU DO, YOU MUST INSTALL A NEW CARRIAGE BOLT ASSEMBLY TO KEEP THE FAIL SAFE FUNCTION.

(a) Install the bolts (150) to the track 3 and the track 4 carriages.
(b) Remove the 98D27504083000 EXTRACTOR - PIN TRACKS 2 AND 3 from the bolt (150) at the track 3 position.
(c) Remove the 98D27504084000 EXTRACTOR - PIN, TRACK 4 from the bolt (150) at the track 4 position.
(d) Make sure that you can see the retaining wire ring (151) and that it is free to turn.
(10) Temporarily install the locking plates (141), the washers (146) and the nuts (145) hand tight only.
(11) Make sure that the failsafe hook nuts (152) are hand tight only.

CAUTION: SUPPORT THE FLAP ALONG THE FULL LENGTH OF THE TRAILING EDGE. THIS WILL PREVENT DAMAGE TO THE FLAP.

(12) Remove the hoisting sling:

NOTE: The weight of the outboard flap is 205kgs (451lbs).

(a) Remove the hoisting sling (Ref. AMM TASK 27-50-00-000-002).

CAUTION: MAKE SURE THAT THE DISCONNECTED PARTS DO NOT TOUCH AND/OR CATCH THE ADJACENT STRUCTURE WHEN YOU MOVE THE FLAP. THIS WILL PREVENT DAMAGE TO THE WING.

(13) Manually push the flap forward and engage the flap drive-arms (124) with the rotary actuator drive-levers (128).
(14) Install the bolts (123), the washers (125) and the nuts (126). Do not torque the nuts at this stage.
(15) Remove the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER from the servo controls.
(16) Lower the spoilers 2, 3, 4 and 5 (Ref. AMM TASK 27-60-00-866-002).

Subtask 27-54-62-820-058-A ** ON A/C NOT FOR ALL

C. Check and Adjustment of the Outboard Flap Rigged Position

NOTE: Before you do the rigging procedure, make sure that:

the aircraft weight is on all three landing gears
the engines are installed
the fuel load is symmetrical or the wing tanks are empty
the flaps are fully retracted (Ref. AMM TASK 27-50-00-866-012).

(1) Install the sharks fin flap rigging kit and do a check of the outboard flap rigged position (Ref. AMM TASK 27-51-00-820-003).
(2) If necessary, adjust the outboard flap rigged position (Ref. AMM TASK 27-51-00-820-009).

Subtask 27-54-62-420-095-F ** ON A/C NOT FOR ALL

D. Complete the Installation of the Flap Drive Levers and the Rotary Actuator Drive-Levers

Flap to Rotary Actuator Drive-Levers ** ON A/C NOT FOR ALL

(1) At the track 4 position:
(a) TORQUE the nut (126) to between 2.2 and 1.95 m.daN (16.22 and 14.38 lbf.ft )

.
(b) Safety the nut (126) with the new AIPC 27-54-05-32-190 COTTER PIN (127) or AIPC 27-54-85-35-210 COTTER PIN (127).
(2) At the track 3 position:
(a) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to slowly extend the flaps to the position 2.
(b) Measure the dimension V between the flap track 3 beam assembly (225) and the end of the bolt (226). This must be 3 mm (0.1181 in.) or more.

Clearance of the Flap Drive-Arm Bolt at the Track 3 Position ** ON A/C NOT FOR ALL

(c) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to fully retract the flaps.
(d) TORQUE the nut (126) to between 7.6 and 6.6 m.daN (56.05 and 48.67 lbf.ft )

.
(e) Safety the nut (126) with the new AIPC 27-54-05-32-090 COTTER PIN (127) or AIPC 27-54-85-35-220 COTTER PIN (127).
(3) Attach the bonding strap (121) with the bolt (119), the washer (120) and the nut (122) (Ref. AMM TASK 20-28-00-912-802).

Subtask 27-54-62-420-101-A ** ON A/C NOT FOR ALL

E. Safety the Forward Eccentrics

Outboard Flap Forward-Eccentrics - Location and Detail ** ON A/C NOT FOR ALL

(1) If the forward eccentrics have been adjusted, do the subsequent steps:
(a) At track 3 install the serrated plate (103) on the eccentric bolt (102).
(b) Install the bolt (104), the washer (105) and the nut (106).
(c) Tighten the nut (106) and safety the nut with a new AIPC 57-53-23-03-130 COTTER PIN (107).
(d) At track 4 install the serrated plate (103) on the eccentric bolt (102).
(e) Install the bolt (104), the washer (105) and the nut (106).
(f) Tighten the nut (106) and safety the nut with a new AIPC 57-53-23-04-130 COTTER PIN (107).
(2) Make sure that the outboard flap trailing edge is in the correct rigged position (Ref. AMM TASK 27-51-00-820-003)

Subtask 27-54-62-420-092-A ** ON A/C NOT FOR ALL

F. Complete the Installation of the Flap to Carriage Assemblies

Flap to Flap Carriage Connection ** ON A/C NOT FOR ALL

WARNING: USE PROTECTIVE 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.

(1) At the track 3 position:
(a) Make sure that the spherical bearing and the splined bush (140) are engaged correctly.
(b) Install the locking plate (141), the washer (146) and the nut (145).
(c) Install the new crushable washer (142) and the nut (143) as follows:
1 Put the new AIPC 27-54-46-24-030 CRUSHABLE WASHER (142) in position on the bolt (140).
2 Loosely install the nut (143) on the bolt (150) and turn it sufficiently to engage the threads correctly.
3 Put the crushable washer (142) in position on the flange of the nut (143) and hold it there.
4 Continue to turn the nut (143) until the crushable washer (142) touches the locking plate (141).
(d) Use the 98D27504118000 SPANNER - FLAP ADJUSTMENT to hold the head of the bolt (150) and TORQUE the nut (143) to between 20 and 15 m.daN (147.49 and 110.62 lbf.ft )

.
(e) Safety the nut (143) with the new AIPC 27-54-46-24-010 COTTER PIN (144).
(2) At the track 4 position:

Flap to Flap Carriage Connection ** ON A/C NOT FOR ALL

(a) Make sure that the spherical bearing and the splined bush (140) are engaged correctly.
(b) Install the locking plate (141), the washer (146) and the nut (145).
(c) Install the new crushable washer (142) and the nut (143) as follows:
1 Put the new AIPC 27-54-46-26-030 CRUSHABLE WASHER (142) in position on the bolt (150).
2 Loosely install the nut (143) on the bolt (150) and turn it sufficiently to engage the threads correctly.
3 Put the crushable washer (142) in position on the flange of the nut (143) and hold it there.
4 Continue to turn the nut (143) until the crushable washer (142) touches the locking plate (141).
(d) Use the 98D27504119000 SPANNER - FLAP ADJUSTMENT to hold the head of the bolt (150) and TORQUE the nut (143) to between 20 and 15 m.daN (147.49 and 110.62 lbf.ft )

.
(e) Safety the nut (143) with the new AIPC 27-54-46-26-010 COTTER PIN (144).
(f) Tighten the nuts (152) and TORQUE to between 0.132 and 0.108 m.daN (11.68 and 9.56 lbf.in )

.
(g) Saftey the nuts (152) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(3) Install the bonding straps (147) with the bolts (148) (Ref. AMM TASK 20-28-00-912-802).
(4) TORQUE the bolts (148) to between 0.45 and 0.4 m.daN (39.82 and 35.40 lbf.in )

.
(5) Safety the bolts (148) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.

Subtask 27-54-62-820-070-A ** ON A/C NOT FOR ALL

G. Completion of the Flap Rigging Procedure
(1) Complete the outboard flap rigging procedure and remove the sharks fin flap rigging kit (Ref. AMM TASK 27-51-00-820-009).

Subtask 27-54-62-420-086-A ** ON A/C NOT FOR ALL

H. Installation of the Tab Drive Control-Rod at the Track 3 Position

Details of the Tab Drive Control-Rod (Track 3) ** ON A/C NOT FOR ALL

(1) Install the loose bushes (39) and (49).
(2) Install the tab drive control-rod (50) to the tab attachment bracket (44) with the bolt (43). Do not install the washer (48) and the nut (47) at this time.
(3) If necessary, adjust the tab drive control-rod (50) to let you connect it to the carriage assembly (38):
(a) Remove the bolt (43) and remove the tab drive control-rod (50).
(b) Remove and discard the lockwire from the nuts (45) and (51).
(c) Loosen the nuts (45) and (51).
(d) Install the tab drive control-rod (50) to the tab attachment bracket (44) with the bolt (43).
(e) Adjust the length of the tab drive control-rod (50) until you can install the bolt (52).
(4) When the tab drive control-rod (50) is at its correct length:
(a) Tighten the nut (51) and tighten the nut (45) by hand as much as possible.
(b) Remove the bolts (43) and (52) and remove the tab drive control-rod (50).
(c) Make sure that the threads of the eye-ends of the tab drive control-rod (50) are in safety.
(d) TORQUE the nut (51) to between 3.8 and 3.3 m.daN (28.02 and 24.34 lbf.ft )

.
(e) TORQUE the nut (45) to between 2.4 and 2.2 m.daN (17.70 and 16.22 lbf.ft )

.
(f) Safety the nuts (51) and (45) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(g) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the nuts (51) and (45).
(h) Install the correctly adjusted tab drive control-rod (50) with the bolts (43) and (52).
(i) Install the washer (40) and the nut (42).
(j) TORQUE the nut (42) to between 2.7 and 1.4 m.daN (19.91 and 10.32 lbf.ft )

.
(k) Safety the nut (42) with the new AIPC 27-54-46-24-095 COTTER PIN (41).
(l) Install the washer (48) and the nut (47).
(m) TORQUE the nut (47) to between 7.8 and 6.8 m.daN (57.52 and 50.15 lbf.ft )

.
(n) Safety the nut (47) with the new AIPC 57-53-23-10-070 COTTER PIN (46).

Subtask 27-54-62-420-094-A ** ON A/C NOT FOR ALL

I. Installation of the Tab Drive Control-Rod at the Track 4 Position

Details of the Tab Drive Control-Rod (Track 4) ** ON A/C NOT FOR ALL

(1) Install the loose bushes (75) and (72).
(2) Install the tab drive control-rod (73) to the tab attachment bracket (67) with the bolt (66). Do not install the washer (71) and the nut (70) at this time.
(3) If necessary, adjust the tab drive control-rod (73) to let you connect it to the carriage assembly (63):
(a) Remove the bolt (66) and remove the tab drive control-rod (73).
(b) Remove and discard the lockwire from the nuts (68) and (74).
(c) Loosen the nuts (68) and (74).
(d) Install the tab drive control-rod (73) to the tab attachment bracket (67) with the bolt (66).
(e) Adjust the length of the tab drive control-rod (73) until you can install the hinge pin (65).
(4) When the tab drive control-rod (73) is at its correct length:
(a) Tighten the nut (74) and tighten the nut (68) by hand as much as possible.
(b) Remove the hinge pin (65) sufficiently to let you remove the tab drive control-rod (73). Do not fully remove the hinge pin (65).

NOTE: If you fully remove the hinge pin (65) from the carriage (63), the roller bearing block (64) will fall out of alignment.

(c) Remove the bolt (66) and remove the tab drive control-rod (73).
(d) Make sure that the threads of the eye-ends of the tab drive control-rod (73) are in safety.
(e) TORQUE the nut (74) to between 3.8 and 3.3 m.daN (28.02 and 24.34 lbf.ft )

.
(f) TORQUE the nut (68) to between 2.4 and 2.2 m.daN (17.70 and 16.22 lbf.ft )

.
(g) Safety the nuts (74) and (68) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
(h) Apply a layer of Corrosion Preventive Compound-Heavy Duty Soft Film - (Material No.12ACC1) to the nuts (74) and (68).
(i) Install the correctly adjusted tab drive control-rod (73) with the bolt (66) and the hinge pin (65).
(j) Install the washer (76) and the nut (77).
(k) TORQUE the nut (77) to between 2.7 and 1.4 m.daN (19.91 and 10.32 lbf.ft )

.
(l) Safety the nut (77) with the new AIPC 27-54-46-26-280 COTTER PIN (78).
(m) Install the washer (71) and the nut (70).
(n) TORQUE the nut (70) to between 3.0 and 2.6 m.daN (22.12 and 19.17 lbf.ft )

.
(o) Safety the nut (70) with the new AIPC 57-53-23-11-070 COTTER PIN (69).

Subtask 27-54-62-820-059-A ** ON A/C NOT FOR ALL

J. Adjustment of the Blade Seal
(1) Remove the 98D27504115000 GAUGES-DISTANCE.

Distance Gages - Location and Detail ** ON A/C NOT FOR ALL

(a) At the track 3 position, release the pins (87) and (88) and remove the distance gage (86).
(b) At the track 4 position, release the pin (90) and remove the distance gage (89).
(2) Install the 98D27504006000 PIN-RIGGING, FLAPS (193) at the track 1 position only.

Slave Pins and Rigging Pin - Location and Detail ** ON A/C NOT FOR ALL

(3) Adjust the flap outboard-end blade seal.

Details of the Blade Seal ** ON A/C NOT FOR ALL

(a) Make sure that the dimension G is 33.4 mm (1.31 in.) +/- 6 mm (0.24 in.).
(b) Loosen the screws (163).
(c) Adjust the blade seal (164) until the dimension H is 8 mm (0.31 in.).
(d) Tighten the screws (163) so that the seal is compressed but not out of shape.
(e) Apply a bead of the Polysulfide Sealant-Fuel Tank Fillet - (Material No.06ABB1) between the cap strip (162) and the outboard flap structure.

Subtask 27-54-62-820-071-C ** ON A/C NOT FOR ALL

K. Alignment and Adjustment of the Cruise Rollers

Alignment of the Inboard Cruise Roller ** ON A/C NOT FOR ALL

(1) Align the inboard cruise roller of the outboard flap:
(a) Measure dimension K.
1 If dimension K is less than, or equal to 3 mm (0.12 in.):

Adjust the position of the cruise roller (180) until dimension J is 3 mm (0.12 in.).

2 If dimension K is more than 3 mm (0.12 in.):

Adjust the position of the cruise roller (180) until dimension J is 0 mm (0.00 in.).

(2) To adjust the cruise roller (180):
(a) If necessary, remove the cushion seal (175).
(b) Remove the nut (178), the collar (177) and the serrated plate (179).
(c) Turn the eccentric (176) until dimension J is correct.
(d) Install the serrated plate (179) to lock the eccentric (176).
(e) Install the collar (177) and the nut (178). Tighten the nut (178) with your hand.
(f) Do a check of dimensions K and J again.
(g) TORQUE the nut (178) to between 27 and 24 m.N (19.91 and 17.70 lbf.ft )

.
(3) If the flap guide-roller assembly was removed, install it (Ref. AMM TASK 27-54-63-400-001). Make sure that the correct size guide-roller is installed.
(4) Measure and adjust the outer-roller:

Alignment of the Outer Roller of the Outboard Flap ** ON A/C NOT FOR ALL

(a) Use a straight-edge to measure the alignment between the outboard flap top-surface and the outer fixed-shroud top-surface.
(b) If the dimension is less than 0.5 mm (0.02 in.), the position of the outer roller (240) is correct.
(c) If the dimension is more than 0.5 mm (0.02 in.), adjust the outer roller (240) as follows:
1 Remove and discard the lockwire from the bolts (239).
2 Remove the bolts (239), the washers (238) and the locking plate (237).
3 Turn the spindle (241) until the outer roller (240) moves the flap in the specified limits.
4 Install the locking plate (237), the washers (238) and the bolts (239).
5 Safety the bolts (239) with 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.

Subtask 27-54-62-220-058-A ** ON A/C NOT FOR ALL

L. Clearance Checks
(1) Do a check of the clearance (between the trailing edge of the spoilers 2, 3, 4 and 5) and the top surface of the flap (Ref. AMM TASK 27-64-00-820-001).

Subtask 27-54-62-420-087-A ** ON A/C NOT FOR ALL

M. Installation of the Z-coupling

Details of the Z-Coupling ** ON A/C NOT FOR ALL

(1) Remove the Z-coupling lever (27) from the inboard flap attachment-bracket (23):
(a) Remove the nut (25), the washer (26), the bolt (22) and the lever (27).
(b) Remove the nut (19), the washer (20) and the spacer(s) (21).
(2) Put the lever (27) in position on the lever (17) and at the inboard flap attachment-bracket (23).
(3) Temporarily install the bolt (22).
(4) Measure and write down the minimum value of the dimension E that can be measured between the levers (17) and (27):
(a) Subtract 2 mm (0.08 in.) from dimension E and use sufficient 57522303-360SPACER(S)21 to get the remaining thickness.
(b) If dimension E is less than 2 mm (0.08 in.), put the spacer(s) (21) between the lever (17) and the washer (20).
(c) If there is no gap (between the levers (17) and (27)), apply a load to the outboard end of the inner flap to get a gap of 0.1 mm (0.004 in.). The load must be applied vertically in line with the lever (27) and must not be more than 20 daN (45 lbf).
(5) If necessary, remove the bolt (22) and the lever (27).
(6) Install the lever (27) with the correct thickness of spacer(s) (21) between the levers (17) and (27).
(7) Install the bolt (22).
(8) Remove the 98D27504006000 PIN-RIGGING, FLAPS (193) at the track 1 position.

Slave Pins and Rigging Pin - Location and Detail ** ON A/C NOT FOR ALL

(9) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to extend the flaps to position 1.
(10) Install the washer (26) and the nut (25) on the bolt (22).
(11) TORQUE the nut (25) to between 1.0 and 0.9 m.daN (88.50 and 79.65 lbf.in )

.
(12) Safety the nut (25) with a new AIPC 57-52-23-03-270 COTTER PIN (24).
(13) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to retract the flaps to the 0 position.
(14) Install the remaining spacer(s) (21) above the washer (20) and the nut (19).
(15) TORQUE the nut (19) to between 3.6 and 3.1 m.daN (26.55 and 22.86 lbf.ft )

.
(16) Safety the nut (19) with a new AIPC 57-52-23-03-328 COTTER PIN (18).
(17) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to extend the flaps to position 1.
(18) Install the interconnecting strut to the outboard flap (Ref. AMM TASK 27-51-44-400-001).
(19) Use the pneumatic wrench and the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) to retract the flaps to the 0 position.
(20) Install the 98D27504006000 PIN-RIGGING, FLAPS (193) at the track 1 position.
(21) Remove the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP).
(22) Connect the right angle gearbox (Ref. AMM TASK 27-54-41-400-001).
(23) Remove the 98D27504006000 PIN-RIGGING, FLAPS (193) at the track 1 position.
(24) Extend the flaps to position 1 (Ref. AMM TASK 27-50-00-866-008).
(25) Install the flap kink seals (Ref. AMM TASK 27-54-61-400-006).
(26) Remove the access platform(s).

Subtask 27-54-62-865-069-A ** ON A/C NOT FOR ALL

N. 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/FLP/CTL AND MONG/SYS1	6CV	B07
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1	6CV	B02
** ON A/C NOT FOR ALL
121VU	FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2	8CV	Q21

Subtask 27-54-62-710-052-A ** ON A/C NOT FOR ALL

O. Test
(1) Do an operational test of the flap system (Ref. AMM TASK 27-54-00-710-001).
(2) Do an operational test of the spoiler system (Ref. AMM TASK 27-64-00-710-001).

5. Close-up
Subtask 27-54-62-410-054-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) Lift the flap track No. 3 and No. 4 movable fairings and adjust if necessary (Ref. AMM TASK 57-55-11-410-002).
(3) Install the access panels:

Interconnecting Strut - Location and Detail ** ON A/C NOT FOR ALL

for the left wing, panels 575AB 575BB 573CB
for the right wing, panels 675AB 675BB 673CB.

Subtask 27-54-62-942-053-A ** ON A/C NOT FOR ALL

B. Removal of Equipment
(1) Remove the safety barriers.
(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] 2026.03.31 23:54:56 UTC