24 Electrics 27 or 38 Amp-Hour NiCad or 28 Amp-Hour Abnorm lead acid batteries are available. No battery No HO A A Emer heater. 24 Electrics Emergency Bus load shedding/distribution Abnorm TCBI, No A A Emer SU 24 Electrics CAB PWR SW/IND located on Co-Pilot’s No No HO A A sidewall 24 Electrics Circuit breaker panel (CBP), CB location on No No HO A A panels reassigned. 24 Electrics Electrical synoptic page accessed via DU No Norm HO A A bezel keys and different format 25 Equipment Emergency Locator Transmitter (ELT) does and not have GPS. ELT switch panel and No No HO A A Furnishings indicator light located on separate panel on pedestal. 26 Fire Engine and APU switches and panels No No HO A A relocated on pedestal. 26 Fire Crew Warning Panel/RMU indications Norm TCBI, No A A installed Emer SU 26 Fire Fire test accomplished with SYS TCBI, No Norm A A TEST/RESET rotary knob on pedestal SU 27 Flight EICAS and Synoptic Indications of: aileron Controls trim; rudder trim; pitch trim; flaps; and, No Norm HO A A spoilers different 27 Flight SPLN RESET and FLAP RESET Controls functionality on rotary test knob located on No Abnorm HO A A SYS TEST/RESET panel on throttle quadrant. 27 Flight PIT TRIM BIAS switch moved to throttle No No HO A A Controls quadrant 27 Flight PITCH TRIM/RUDDER TRIM panel No No HO A A Controls relocated on pedestal 27 Flight RUD BOOST SW/IND relocated to throttle No No HO A A Controls quadrant 27 Flight and RUD PEDAL switches Pilot’s copilot’s Controls relocated on pilot and copilot switch panels No No HO A A and relabeled RUDDER PEDAL 27 Flight Flaps test accomplished with SYS TCBI, No Norm A A Controls TEST/RESET rotary knob on pedestal SU 30 Ice and ANTI-ICE panel moved from pedestal to No No HO A A Rain center switch panel. 30 Ice and Anti-Ice system test accomplished on SYS TCBI, No No A A Rain TEST/RESET rotary test knob on pedestal SU
24 Electrics 27 or 38 Amp-Hour NiCad or 28 Amp-Hour lead acid batteries are available. No battery heater. No Abnorm Emer HO A A 24 Electrics Emergency Bus load shedding/distribution No Abnorm Emer TCBI, SU A A 24 Electrics CAB PWR SW/IND located on Co-Pilot’s sidewall No No HO A A 24 Electrics Circuit breaker panel (CBP), CB location on panels reassigned. No No HO A A 24 Electrics Electrical synoptic page accessed via DU bezel keys and different format No Norm HO A A 25 Equipment and Furnishings Emergency Locator Transmitter (ELT) does not have GPS. ELT switch panel and indicator light located on separate panel on pedestal. No No HO A A 26 Fire Engine and APU switches and panels relocated on pedestal. No No HO A A 26 Fire Crew Warning Panel/RMU indications installed No Norm Emer TCBI, SU A A 26 Fire Fire test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 27 Flight Controls EICAS and Synoptic Indications of: aileron trim; rudder trim; pitch trim; flaps; and, spoilers different No Norm HO A A 27 Flight Controls SPLN RESET and FLAP RESET functionality on rotary test knob located on SYS TEST/RESET panel on throttle quadrant. No Abnorm HO A A 27 Flight Controls PIT TRIM BIAS switch moved to throttle quadrant No No HO A A 27 Flight Controls PITCH TRIM/RUDDER TRIM panel relocated on pedestal No No HO A A 27 Flight Controls RUD BOOST SW/IND relocated to throttle quadrant No No HO A A 27 Flight Controls Pilot’s and copilot’s RUD PEDAL switches relocated on pilot and copilot switch panels and relabeled RUDDER PEDAL No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 30 Ice and Rain ANTI-ICE panel moved from pedestal to center switch panel. No No HO A A 30 Ice and Rain Anti-Ice system test accomplished on SYS TEST/RESET rotary test knob on pedestal No No TCBI, SU A A