Installation of the Forward Crossover Beam (Inboard Fan and T/R Cowls not Removed) [IAE]
TASK 78-30-10-400-010-A-01
Installation of the Forward Crossover Beam (Inboard Fan and T/R Cowls not Removed)
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Expendable Parts
C. Referenced Information
3. Job Set-up
Subtask 78-30-10-860-053-A ** ON A/C NOT FOR ALL
Subtask 78-30-10-420-058-A ** ON A/C NOT FOR ALL
Subtask 78-30-10-410-054-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 03:27:22 UTC
Installation of the Forward Crossover Beam (Inboard Fan and T/R Cowls not Removed)
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 2M (6 FT) |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 190 and 160 lbf.in (2.15 and 1.81 m.daN ) ![]() | |
| No specific | Torque wrench: range to between 690 and 480 lbf.in (7.80 and 5.42 m.daN ) ![]() | |
| No specific | Torque wrench: range to between 0.8 and 0.7 m.daN (70.80 and 61.95 lbf.in ) ![]() | |
| IAE1N20002 | 1 | SLING-FAN THRUST REVERSER |
| S889BH0 | 1 | BRACE - HOLD OPEN COWLS |
| TMHBS13-00-00 | 1 | BRACE-HOLD OPEN COWLS |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 1 | COTTER PIN | AIPC 54-57-17-02-260 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 54-56-00-400-002-A | Installation of the Lower Fairing |
| TASK 70-23-11-911-013-A | General Torque Tightening Techniques |
| TASK 71-00-20-400-040-A | Installation of the Power Plant |
| TASK 71-00-20-400-040-A-01 | Installation of the Power Plant with the Engine Positioner TWW 75E (MIAG) |
| TASK 71-13-00-410-010-A | Closing of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-11-400-010-A | Installation of the Left Fan Cowl |
| TASK 71-13-16-400-010-B | Installation of the Right Fan Cowl (438AR, 448AR) |
| TASK 78-32-00-410-010-A | Closing of the Thrust Reverser Halves |
| TASK 78-32-01-400-010-A | Installation of the Left Thrust Reverser Half - Eng No. 1 |
| TASK 78-32-04-400-010-A | Installation of the Right Reverser Half - Eng. No. 2 |
Subtask 78-30-10-860-053-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) On the center pedestal, on the ENG panel 115VU, make sure that a 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 a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position.
4. Procedure(1) On the center pedestal, on the ENG panel 115VU, make sure that a 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 a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
(3) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position.
Subtask 78-30-10-420-058-A ** ON A/C NOT FOR ALL
A. Install the forward crossover beam.
(1) Install the spacer (5), the bolt (4), the washer (3) and the nut (2).
(2) TORQUE the nut (2) to between 0.8 and 0.7 m.daN (70.80 and 61.95 lbf.in )
.
(3) Install the AIPC 54-57-17-02-260 COTTER PIN (1).
Subtask 78-30-10-420-059-B ** ON A/C NOT FOR ALL (1) Install the spacer (5), the bolt (4), the washer (3) and the nut (2).
(2) TORQUE the nut (2) to between 0.8 and 0.7 m.daN (70.80 and 61.95 lbf.in )
. (3) Install the AIPC 54-57-17-02-260 COTTER PIN (1).
B. Install the parts removed for access to the Crossover Beam.
(1) Configuration 1 : Outboard T/R half not removed.
(a) At the position No.1 of the T/R half hinge:
1 Install the bolt (1) and the washer (11).
2 Install the nut (10) to the bolt (1). Do not tighten the nut at this step.
(b) At the position No.4 of the T/R half hinge:
1 TORQUE the nut (6) to between 690 and 480 lbf.in (7.80 and 5.42 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
(c) At the positions No.2 and No.3 of the T/R half hinge:
1 TORQUE the nuts (8) to between 190 and 160 lbf.in (2.15 and 1.81 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
(d) At the position No.1 of the T/R half hinge:
1 TORQUE the nut (10) to between 190 and 160 lbf.in (2.15 and 1.81 m.daN )
(Ref. AMM TASK 70-23-11-911-013).
(2) Configuration 2 : Outboard T/R half removed.
Subtask 78-30-10-420-060-B ** ON A/C NOT FOR ALL (1) Configuration 1 : Outboard T/R half not removed.
(a) At the position No.1 of the T/R half hinge:
1 Install the bolt (1) and the washer (11).
2 Install the nut (10) to the bolt (1). Do not tighten the nut at this step.
(b) At the position No.4 of the T/R half hinge:
1 TORQUE the nut (6) to between 690 and 480 lbf.in (7.80 and 5.42 m.daN )
(Ref. AMM TASK 70-23-11-911-013). (c) At the positions No.2 and No.3 of the T/R half hinge:
1 TORQUE the nuts (8) to between 190 and 160 lbf.in (2.15 and 1.81 m.daN )
(Ref. AMM TASK 70-23-11-911-013). (d) At the position No.1 of the T/R half hinge:
1 TORQUE the nut (10) to between 190 and 160 lbf.in (2.15 and 1.81 m.daN )
(Ref. AMM TASK 70-23-11-911-013). (2) Configuration 2 : Outboard T/R half removed.
- For ENG 1 (Ref. AMM TASK 78-32-01-400-010)
- For ENG 2 (Ref. AMM TASK 78-32-04-400-010)
C. Install the Outboard Fan Cowl (Ref. AMM TASK 71-13-11-400-010) or (Ref. AMM TASK 71-13-16-400-010).
Subtask 78-30-10-420-061-A ** ON A/C NOT FOR ALL D. Install the Brace of the Outboard Fan Cowl and Thrust Reverser Halves.
(1) Install the S889BH0 BRACE - HOLD OPEN COWLS or TMHBS13-00-00 BRACE-HOLD OPEN COWLS to support the fan and thrust reverser cowl doors.
(2) Put the adjustable struts in position.
(3) Adjust the length of the struts so that they hold the weight of the thrust reverser halves.
(4) Put the thrust reverser half-open rods in their storage positions (Ref. AMM TASK 78-32-00-410-010).
(5) Install the support arms so that they hold the weight of the fan cowl doors.
Subtask 78-30-10-080-050-A ** ON A/C NOT FOR ALL (1) Install the S889BH0 BRACE - HOLD OPEN COWLS or TMHBS13-00-00 BRACE-HOLD OPEN COWLS to support the fan and thrust reverser cowl doors.
(2) Put the adjustable struts in position.
(3) Adjust the length of the struts so that they hold the weight of the thrust reverser halves.
(4) Put the thrust reverser half-open rods in their storage positions (Ref. AMM TASK 78-32-00-410-010).
(5) Install the support arms so that they hold the weight of the fan cowl doors.
NOTE: The support arms must be installed so that the brackets are on the second latch from the front of the thrust reverser halves.
(6) Put the fan cowl hold-open rods in their storage positions (Ref. AMM TASK 71-13-00-410-010). E. Remove the thrust reverser sling and the slat protection mat
-For ENG 1
-For ENG 2
(1) Remove the IAE1N20002 SLING-FAN THRUST REVERSER (1) from the thrust reverser half (3).
(2) install the threaded fasteners in the hoist point nut plates.
(3) Remove the slat protection mats from the slats.
(4) Position the hinge access panel (2) on the thrust reverser half.
(5) Attach the hinge access panel with the 11 screws (4).
(6) Install the thrust reverser pylon fairing (Ref. AMM TASK 54-56-00-400-002).
Subtask 78-30-10-420-062-A ** ON A/C NOT FOR ALL 5. Close-up-For ENG 1
-For ENG 2
(1) Remove the IAE1N20002 SLING-FAN THRUST REVERSER (1) from the thrust reverser half (3).
(2) install the threaded fasteners in the hoist point nut plates.
(3) Remove the slat protection mats from the slats.
(4) Position the hinge access panel (2) on the thrust reverser half.
(5) Attach the hinge access panel with the 11 screws (4).
(6) Install the thrust reverser pylon fairing (Ref. AMM TASK 54-56-00-400-002).
Subtask 78-30-10-410-054-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) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the WARNING NOTICE(S).
(3) Remove the access platform(s).
Forward Crossover Beam