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data to the ELACs and SECs for flight envelope
protection computation.
TMUFCLG02-T07 LEVEL 3
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EFCS CONTROL INTERFACE - ADIRS
TMUFCLG02-P07 LEVEL 3
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EFCS CONTROL INTERFACE
LANDING GEAR CONTROL AND INTERFACE UNIT
The Landing Gear Control Interface Units (LGCIUs)
transmit landing gear position information to the ELACs
and SECs.
TMUFCLG02-T08 LEVEL 3
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EFCS CONTROL INTERFACE
SLAT AND FLAP CONTROL COMPUTER
The Slat Flap Control Computers (SFCCs) transmit slat
flap surface position to the ELACs and SECs for law
computation.
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TMUFCLG02-P09 LEVEL 3
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EFCS CONTROL INTERFACE
RADIO ALTIMETER
The Radio Altimeter (RA) transmits the altitude
information to the ELACs for flare law activation.
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TMUFCLG02-P10 LEVEL 3
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EFCS CONTROL INTERFACE
BRAKING/STEERING CONTROL UNIT
The Braking Steering Control Unit (BSCU) receives
information from the ELACs for the nose wheel steering
system and from the SECs for the auto brake function.
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TMUFCLG02-P11 LEVEL 3
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EFCS CONTROL INTERFACE
WHEEL TACHOMETER
Each main landing gear wheel speed is transmitted by
wheel tachometers to the SECs for ground spoiler
extension.
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TMUFCLG02-P12 LEVEL 3
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EFCS CONTROL INTERFACE
ACCELEROMETER
The vertical accelerometers, installed in the FWD cargo
compartment, transmit the vertical acceleration of the
aircraft to the ELACs and SECs.
The vertical accelerometers are also used for the
computation of Pitch Trim function and Load Factor
function.
TMUFCLG02-T13 LEVEL 3
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TMUFCLG02-P13 LEVEL 3
EFFECTIVITY 27-90-00 Page 27
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