FLT PROC LVL LVL LVL LVL DESIGN REMARKS CHK CURR CHAR CHNG A B C D Aircraft Flight Deck panel layout modified to integrate General new Garmin 5000 avionics suite and to No No HO A A enhance aesthetics. Aircraft Relocated flight deck control panels. No No HO A A General Aircraft Larger winglets No No HO A A General Aircraft Passenger cabin updated No No HO A A General Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to 21,500 lbs. No No HO A A Maximum Zero Fuel Weight 16,000 lbs. Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 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. 21 ECS PRESSURIZATION panel resized and reconfigured. L & R BLEED, PACK, HI FLOW and Norm EMERG PRESS switches moved to new No Abnorm HO A A PAX/OXY PRESS panel on pedestal. Emer APU BLEED switch move to APU panel on pedestal. DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 40 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL MANEUVER REMARKS CHK CURR CHAR CHNG A B C D 21 ECS ENVIRONMENTAL CONTROL SYSTEM No No HO A A (ECS) synoptic page controlled via GTCs
DESIGN REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR Aircraft General Flight Deck panel layout modified to integrate new Garmin 5000 avionics suite and to enhance aesthetics. No No HO A A Aircraft General Relocated flight deck control panels. No No HO A A Aircraft General Larger winglets No No HO A A Aircraft General Passenger cabin updated No No HO A A Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to 21,500 lbs. Maximum Zero Fuel Weight 16,000 lbs. No No HO A A Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 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 21 ECS PRESSURIZATION panel resized and reconfigured. L & R BLEED, PACK, HI FLOW and EMERG PRESS switches moved to new PAX/OXY PRESS panel on pedestal. APU BLEED switch move to APU panel on pedestal. No Norm Abnorm Emer HO A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 40 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR MANEUVER REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR 21 ECS ENVIRONMENTAL CONTROL SYSTEM (ECS) synoptic page controlled via GTCs No No HO A A