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materials listed in drawing 756-0074-304 for the .107 configuration.
3.3.4.2 Access the avionics compartment at the AE0303 disconnect bracket and Flight Deck
P61sidewall panel.
3.3.4.3 Install and terminate the E3-3 to P61 Equipment Interface loose wire, 756-0074-504-107
and associated parts per drawing 756-0074-304, sheet 5.
3.3.4.4 Route the E3-3 to P61 Equipment Interface loose wire, 756-0074-504-107 right along E3-3
and E4-3, aft along right side of P36 panel up at station 520 and fwd along the right side
ceiling in the wire raceway up through and along flight deck floor wire raceway to the P61
panel per drawing 756-0074-304, sheet 7.
3.3.4.5 Install and terminate the E3-3 to P61 Equipment Interface loose wire, 756-0074-504-107
and associated parts at the printer per drawing 756-0074-304, sheet 5.
3.3.4.6 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 5.
3.3.4.7 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.3.5 Rework of P8 Panel wiring
3.3.5.1 Obtain installation sub kit 756-0074-304-113, P8 Equipment Interface Wire
Installation,
or materials listed in drawing 756-0074-304 for the .113 configuration.
3.3.5.2 Access the Flight Deck P8 panel.
3.3.5.3 Modify existing wiring, install and terminate the P8 Equipment Interface loose wire,
756-0074-504-113 and associated parts per drawing 756-0074-304, sheet 6.
3.3.5.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 6.
RMD-CERT/R- CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO. 756-0074-106 REV. A SHEET 10
3.3.5.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.4 Group III aircraft
Obtain engineering installation kit 756-0074-300-105.
3.4.1 Rework of the E3-3 Shelf Wiring
3.4.1.1 Obtain installation sub kit 756-0074-304-111, FDAMS E3-3 Equipment Interface Wire
Installation, or materials listed in drawing 756-0074-304 for the .111 configuration.
3.4.1.2 Access the avionics compartment and remove the E3-3 shelf, if required.
3.4.1.3 Modify existing wiring, install and terminate the FDAMS E3-3 Equipment Interface loose
wire, 756-0074-504-111 and associated parts per drawing 756-0074-304, sheet 4.
3.4.1.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 4.
3.4.1.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
For Training Purpose Only Printed:May 2005
B757-200 Aircraft Recurrent Training Manual - 87 -
required.
3.4.2 E3-3 Stanchion to P61 Panel Wiring
3.4.2.1 Obtain installation sub kit 756-0074-304-107, E3-3 Stanchion to P61 Wire Installation, or
materials listed in drawing 756-0074-304 for the .107 configuration.
3.4.2.2 Access the avionics compartment at the AE0303 disconnect bracket and Flight Deck P61
sidewall panel.
3.4.2.3 Install and terminate the E3-3 to P61 Equipment Interface loose wire,
756-0074-504-107and associated parts per drawing 756-0074-304, sheet 5.
3.4.2.4 Route the E3-3 to P61 Equipment Interface loose wire, 756-0074-504-107 right along E3-3
and E4-3, aft along right side of P36 panel up at station 520 and fwd along the right side
ceiling in the wire raceway up through and along flight deck floor wire raceway to the P61
panel per drawing 756-0074-304, sheet 7.
3.4.2.5 Install and terminate the E3-3 to P61 Equipment Interface loose wire, 756-0074-504-107
and associated parts at the printer per drawing 756-0074-304, sheet 5.
3.4.2.6 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 5.
3.4.2.7 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.5 Continuity and Isolation Checks
3.5.1 Access the avionics compartment, P8 and P61 panel as required.
RMD-CERT/R- CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO. 756-0074-106 REV. A SHEET 11
3.5.2 Reinstall the E3-3 and E4-3 shelves if removed for the modification.
3.5.3 Perform continuity and isolation checks on installed wiring in accordance with drawing
756-0074-601, Wiring Diagrams 23-22-13, 23-22-14, 31-31-02, 31-31-65 and 31-35-02 as
applicable.
4.0 Close Up
NOTE: If additional modifications are required in an area, final close-up may be suspended until
all work is completed in that area.
1. Reinstall all sidewall liners, thermal blankets and ceiling or floor panels, which have been
removed during this installation.
2. Secure all areas that were opened for access throughout the installation, close any previously
opened hatches used to gain access to the avionics compartment.
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飞机复训教材(43)
