34 Navigation and PFD display options Pilot’s copilot’s Norm TCBI, No A A controlled by PFD Display Controllers. Abnorm SU 34 Navigation Tuning of Navigation radios via RMUs. CSS, Audio portion of Nav radios controlled via Norm PTT No B A Audio control panels located on pilot and Abnorm FTD copilot instrument panels. 2-5 34 Navigation No automatic reversion of ADCs during Norm TCBI, No A A malfunctions. Abnorm SU 34 Navigation ADC test added, not a BIT test. Test TCBI, completed with rotary test switch located on No Norm A A SU pedestal. 34 Navigation Traditional round gauges replace Integrated Electronic Standby (IESI) for Airspeed, Abnorm TCBI, No B B Attitude and Altitude. Standby navigation Emer SU accomplished on RMU. 34 Navigation Nav Source, Course and bearing PFD’s TCBI, pointers controlled via Pilot/Co-Pilot PFD No Norm A A SU display Controllers located on glareshield 34 Navigation Mode S transponder without Enhanced Norm Surveillance and ADS-B-Out No Abnorm HO A A Emer 34 Navigation Transponder, no auto select function for Norm No HO A A ground and airborne ops. Abnorm 34 Navigation Different weather radar with panel located on TCBI, pedestal. No lightning or turbulence No Norm A A SU detection. 34 Navigation Universal FMS CDUs located on pedestal. CSS, Operation and functionality different PTT No Norm C C FTD 2-5 34 Navigation No PFD insert map to display traffic or No No HO A A navigation. 34 Navigation Universal FMS uses GPS, VOR and Norm DME/DME capability. (Garmin uses GPS No HO A A Abnorm and SBAS WAAS only) 34 Navigation WAAS/LPV optional equipment on Universal Norm No HO A A FMS. Operation and functionality different Abnorm 34 Navigation No reactive wind shear detection and No No HO A A guidance. 34 Navigation No MFD Auto-Zoom No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR
34 Navigation Pilot’s and copilot’s PFD display options controlled by PFD Display Controllers. No Norm Abnorm TCBI, SU A A 34 Navigation Tuning of Navigation radios via RMUs. Audio portion of Nav radios controlled via Audio control panels located on pilot and copilot instrument panels. No Norm Abnorm CSS, PTT FTD 2-5 B A 34 Navigation No automatic reversion of ADCs during malfunctions. No Norm Abnorm TCBI, SU A A 34 Navigation ADC test added, not a BIT test. Test completed with rotary test switch located on pedestal. No Norm TCBI, SU A A 34 Navigation Traditional round gauges replace Integrated Electronic Standby (IESI) for Airspeed, Attitude and Altitude. Standby navigation accomplished on RMU. No Abnorm Emer TCBI, SU B B 34 Navigation PFD’s Nav Source, Course and bearing pointers controlled via Pilot/Co-Pilot PFD display Controllers located on glareshield No Norm TCBI, SU A A 34 Navigation Mode S transponder without Enhanced Surveillance and ADS-B-Out No Norm Abnorm Emer HO A A 34 Navigation Transponder, no auto select function for ground and airborne ops. No Norm Abnorm HO A A 34 Navigation Different weather radar with panel located on pedestal. No lightning or turbulence detection. No Norm TCBI, SU A A 34 Navigation Universal FMS CDUs located on pedestal. Operation and functionality different No Norm CSS, PTT FTD 2-5 C C 34 Navigation No PFD insert map to display traffic or navigation. No No HO A A 34 Navigation Universal FMS uses GPS, VOR and DME/DME capability. (Garmin uses GPS and SBAS WAAS only) No Norm Abnorm HO A A 34 Navigation WAAS/LPV optional equipment on Universal FMS. Operation and functionality different No Norm Abnorm HO A A 34 Navigation No reactive wind shear detection and guidance. No No HO A A 34 Navigation No MFD Auto-Zoom No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR