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3.2.3.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 5.
3.2.3.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.2.4 E3-3 Stanchion to P61 Panel Wiring
3.2.4.1 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.
3.2.4.2 Access the avionics compartment at the AE0303 disconnect bracket and Flight Deck P61
sidewall panel.
3.2.4.3 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.
3.2.4.4 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.
3.2.4.5 Install and terminate the E3-3 to P61 Equipment Interface loose wire, 56-0074-504-107
and associated parts at the printer per drawing 756-0074-304, sheet 5.
3.2.4.6 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 5.
3.2.4.7 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.2.5 Rework of P8 Panel wiring
3.2.5.1 Obtain installation sub kit 756-0074-304-109, P8 Equipment Interface Wire Installation, or
materials listed in drawing 756-0074-304 for the .109 configuration.
RMD-CERT/R- CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO. 756-0074-106 REV. A SHEET 8
3.2.5.2 Access the Flight Deck P8 panel.
3.2.5.3 Modify existing wiring, install and terminate the P8 Equipment Interface loose wire,
756-0074-504-109 and associated parts per drawing 756-0074-304, sheet 6.
3.2.5.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
For Training Purpose Only Printed:May 2005
B757-200 Aircraft Recurrent Training Manual - 85 -
sheet 6.
3.2.5.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.3 Group II aircraft
Obtain engineering installation kit 756-0074-300-103.
3.3.1 Rework of the E4-3 Shelf Wiring
3.3.1.1 Obtain installation sub kit 756-0074-304-101, ACARS E3-4 Equipment Interface Wire
Installation, or materials listed in drawing 756-0074-304 for the .101 configuration.
3.3.1.2 Access the avionics compartment and remove the E4-3 shelf, if required.
3.3.1.3 Modify existing wiring, install and terminate the ACARS E4-3 Equipment Interface loose
wire, 756-0074-504-101 and associated parts per drawing 756-0074-304, sheet 2.
3.3.1.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 2.
3.3.1.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note
3 as required.
3.3.2 Rework of the E3-3 Shelf Wiring
3.3.2.1 Obtain installation sub kit 756-0074-304-103, FDAMS E3-3 Equipment Interface Wire
Installation, or materials listed in drawing 756-0074-304 for the .103 configuration.
3.3.2.2 Access the avionics compartment and remove the E3-3 shelf, if required.
3.3.2.3 Modify existing wiring, install and terminate the FDAMS E3-3 Equipment Interface loose
wire, 756-0074-504-103 and associated parts per drawing 756-0074-304, sheet 3.
3.3.2.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 3.
3.3.2.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.3.3 Rework of the E3-3 to E4-3 Stanchion Wiring
3.3.3.1 Obtain installation sub kit 756-0074-304-105, E3-3 to E4-3 Stanchion Wire Installation, or
materials listed in drawing 756-0074-304 for the .105 configuration.
RMD-CERT/R- CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO. 756-0074-106 REV. A SHEET 9
3.3.3.2 Access the avionics compartment at the AE0303 and AE0403 disconnect brackets, as
required.
3.3.3.3 Modify existing wiring, install and terminate the E3-3 to E4-3 Stanchion Interface loose
wire, 756-0074-504-105 and associated parts per drawing 756-0074-304, sheet 5.
3.3.3.4 Perform continuity and isolation checks on installed wiring per drawing 756-0074-304,
sheet 5.
3.3.3.5 Secure new wiring with existing wire bundles as required. Reference section 3.0, Note 3 as
required.
3.3.4 E3-3 Stanchion to P61 Panel Wiring
For Training Purpose Only Printed:May 2005
B757-200 Aircraft Recurrent Training Manual - 86 -
3.3.4.1 Obtain installation sub kit 756-0074-304-107, E3-3 Stanchion to P61 Wire Installation, or
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