(POI)____________________________ TRAINING CHKG/CURR FLT PROC LVL LVL LVL LVL DESIGN REMARKS CHK CURR CHAR CHNG A B C D Weights Maximum Zero Fuel Weight 16,500 No No HO A A lbs.(aircraft modified by SB 75-11-1) Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 70 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 No No HO A A Comm system operation. 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. 29 Increase in length of hydraulic nose gear Hydraulic extend and retract lines. Hydraulic system No No HO A A Power operation not affected. 32 Longer emergency landing gear cable, no No No HO A A Landing Gear change in system operation. 35 6 dual masks drop (was 5) Oxygen Oxygen chart in AFM and manual No No HO A A Pilot’s changed. DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 70 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR
(POI)____________________________ TRAINING CHKG/CURR DESIGN REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR Weights Maximum Zero Fuel Weight 16,500 lbs.(aircraft modified by SB 75-11-1) No No HO A A Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 70 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 Comm 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 29 Hydraulic Power Increase in length of hydraulic nose gear extend and retract lines. Hydraulic system operation not affected. No No HO A A 32 Landing Gear Longer emergency landing gear cable, no change in system operation. No No HO A A 35 Oxygen 6 dual masks drop (was 5) Oxygen chart in AFM and Pilot’s manual changed. No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 70 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR