(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 E ODR Table: Learjet 40 to Learjet 45 – DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 40 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL DESIGN REMARKS CHK CURR CHAR CHNG A B C D Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to21,500 lbs. No No HO A A Maximum Zero Fuel Weight increased to 16,500 lbs. Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 40 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL SYSTEM REMARKS CHK CURR CHAR CHNG A B C D 6 Fuselage length increased requires new Dimensions formulas for weight and balance. No No HO A A and Areas 9 Fuselage length increase results in bigger Towing and turning radius, no operational impact. No No HO A A Taxiing 11 Fuel Quantity placards (interior & exterior) No No HO A A Placards change to reflect useable quantity increase. 21 Addition of 2 gaspers. Air Increase in length of main cabin condition air Conditioning ducting. No No HO A A Increase in length vacuum line (pressurization, outflow valve control). System operation not affected. 23 Antenna relocation results in no change to system operation. No No HO A A 27 Increased length control system cables. Flight Control system operation not affected. No No HO A A Controls 28 Fuel System difference limited to an increase Fuel in Total Useable Quantity. No change to any No No HO A A other system aspect.
(POI)____________________________ 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 E – ODR Table: Learjet 40 to Learjet 45 DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 40 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR DESIGN REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to21,500 lbs. Maximum Zero Fuel Weight increased to 16,500 lbs. No No HO A A Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 40 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR SYSTEM REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR 6 Dimensions and Areas Fuselage length increased requires new formulas for weight and balance. No No HO A A 9 Towing and Taxiing Fuselage length increase results in bigger turning radius, no operational impact. No No HO A A 11 Placards Fuel Quantity placards (interior & exterior) change to reflect useable quantity increase. No No HO A A 21 Air Conditioning Addition of 2 gaspers. Increase in length of main cabin condition air ducting. Increase in length vacuum line (pressurization, outflow valve control). System operation not affected. No No HO A A 23 Antenna relocation results in no change to system operation. No No HO A A 27 Flight Controls Increased length control system cables. Control system operation not affected. No No HO A A 28 Fuel Fuel System difference limited to an increase in Total Useable Quantity. No change to any other system aspect. No No HO A A