DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL SYSTEM REMARKS CHK CURR CHAR CHNG A B C D 35 Oxygen PAX OXY/PRESS panel relocated on pedestal moved to copilot switch panel and No No HO A A relabeled PAX OXYGEN 45 No Wi-Fi Iridium out. Maintenance data Central accessed with laptop via port in lower No No HO A A Maintenance pedestal System 46 No capability to display electronic flight Information charts or AOPA airport directory. No No HO A A Systems 46 No graphical map capability Information No No HO A A Systems 46 Not capable of XM or international weather Information presentation No No HO A A Systems 70 Powerplant L and R Engine controls relocated on pedestal No No HO A A 70 Powerplant TFE 731-20 AR or BR engines decreased thrust from 3850 lbs. to 3500 lbs. or 3650 lbs. No No HO A A with APR active DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL MANEUVER REMARKS CHK CURR CHAR CHNG A B C D PTS No Changes No No HO A A Maneuvers Annex J ODR Table: Learjet 75 to Learjet 40 – DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL DESIGN REMARKS CHK CURR CHAR CHNG A B C D Aircraft Flight Deck panel layout differs from Learjet General 75 (Garmin) to accommodate Honeywell No No HO A A Primus 1000 suite.
DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR SYSTEM REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR 35 Oxygen PAX OXY/PRESS panel relocated on pedestal moved to copilot switch panel and relabeled PAX OXYGEN No No HO A A 45 Central Maintenance System No Wi-Fi Iridium out. Maintenance data accessed with laptop via port in lower pedestal No No HO A A 46 Information Systems No capability to display electronic flight charts or AOPA airport directory. No No HO A A 46 Information Systems No graphical map capability No No HO A A 46 Information Systems Not capable of XM or international weather presentation No No HO A A 70 Powerplant L and R Engine controls relocated on pedestal No No HO A A 70 Powerplant TFE 731-20 AR or BR engines decreased thrust from 3850 lbs. to 3500 lbs. or 3650 lbs. with APR active No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR MANEUVER REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR PTS Maneuvers No Changes No No HO A A Annex J – ODR Table: Learjet 75 to Learjet 40 DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR DESIGN REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR Aircraft General Flight Deck panel layout differs from Learjet 75 (Garmin) to accommodate Honeywell Primus 1000 suite. No No HO A A