31 DU REVERSION/DIM panel moved to pilot CSS, Abnorm Indicating/ switch panel and labeled REVERSION - PTT No Emer B A Recording includes ADC/AHRS/ICSG reversion FTD switches 2-5 31 DU2 and DU3 reversion controls on CSS, pilot’s Indicating/ and glareshield. PTT copilot’s No Abnorm B A Recording FTD 2-5 31 Low Speed Awareness and Overspeed cues Indicating/ on PFDs, color logic changed. No No HO A A Recording 31 Heading, speed, altitude select bugs and Indicating/ navigation source color logic changes. No No HO A A Recording 31 VSI indication changed from a tape to an arc. Indicating/ No No HO A A Recording 31 Electronic navigation chart display not Indicating/ available No No HO A A Recording 31 FPV now FPA (Flight Path Angle) and Norm TCBI, Indicating/ generated by the Universal FMS. Includes No A A Abnorm SU Recording speed carat indication 31 Database management accomplished through Indicating/ separate Data Transfer Unit No No HO A A Recording 32 Shorter emergency landing gear cable, no No No HO A A Landing Gear change in system operation. 32 GEAR/HYD panel moved from center switch Landing Gear panel to co-pilot switch panel. No No HO A A 32 Landing Gear handle moved from Co-Pilot’s No No HO A A Landing Gear switch panel to GEAR/HYD panel 32 Gear test accomplished with rotary test knob TCBI, Landing Gear on pedestal No Norm A A SU 32 Gear Caution/Warning indications differ in Landing Gear presentation. Logic is the same No No HO A A 32 No Synoptic presentation of AUX HYD or No No HO A A Landing Gear HYD XFLOW indications 33 Lights Exterior light control; no smoking/belts; and Emergency light switches moved from No Norm HO A A overhead light switch panel to center switch panel 33 Lights Lights test accomplished with rotary knob on TCBI, No Norm A A pedestal. Also runs audio test. SU 34 Navigation Some of the and CSS, pilot’s copilot’s Garmin’s DU softkeys and GTCs functions replaced by Norm PTT No B B Pilot/Co-Pilot’s PFD Display Controllers. Abnorm FTD 2-5 34 Navigation AHRS replaces Honeywell’s Garmin’s Norm No HO A A integrated AHRS system Abnorm
31 Indicating/ Recording DU REVERSION/DIM panel moved to pilot switch panel and labeled REVERSION - includes ADC/AHRS/ICSG reversion switches No Abnorm Emer CSS, PTT FTD 2-5 B A 31 Indicating/ Recording DU2 and DU3 reversion controls on pilot’s and copilot’s glareshield. No Abnorm CSS, PTT FTD 2-5 B A 31 Indicating/ Recording Low Speed Awareness and Overspeed cues on PFDs, color logic changed. No No HO A A 31 Indicating/ Recording Heading, speed, altitude select bugs and navigation source color logic changes. No No HO A A 31 Indicating/ Recording VSI indication changed from a tape to an arc. No No HO A A 31 Indicating/ Recording Electronic navigation chart display not available No No HO A A 31 Indicating/ Recording FPV now FPA (Flight Path Angle) and generated by the Universal FMS. Includes speed carat indication No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Database management accomplished through separate Data Transfer Unit No No HO A A 32 Landing Gear Shorter emergency landing gear cable, no change in system operation. No No HO A A 32 Landing Gear GEAR/HYD panel moved from center switch panel to co-pilot switch panel. No No HO A A 32 Landing Gear Landing Gear handle moved from Co-Pilot’s switch panel to GEAR/HYD panel No No HO A A 32 Landing Gear Gear test accomplished with rotary test knob on pedestal No Norm TCBI, SU A A 32 Landing Gear Gear Caution/Warning indications differ in presentation. Logic is the same No No HO A A 32 Landing Gear No Synoptic presentation of AUX HYD or HYD XFLOW indications No No HO A A 33 Lights Exterior light control; no smoking/belts; and Emergency light switches moved from overhead light switch panel to center switch panel No Norm HO A A 33 Lights Lights test accomplished with rotary knob on pedestal. Also runs audio test. No Norm TCBI, SU A A 34 Navigation Some of the pilot’s and copilot’s Garmin’s DU softkeys and GTCs functions replaced by Pilot/Co-Pilot’s PFD Display Controllers. No Norm Abnorm CSS, PTT FTD 2-5 B B 34 Navigation Honeywell’s AHRS replaces Garmin’s integrated AHRS system No Norm Abnorm HO A A