29 Increase in length of hydraulic nose gear Hydraulic extend and retract lines. Hydraulic system No No HO A A Power operation not affected. DIFFERENCE AIRCRAFT: Learjet 45 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 31 CAS and CWP messages added for Cabin Indicating Altitude problem awareness. Recording L R ECS CAS messages added for bleed air No No HO A A Systems system failures. Note; These changes will be introduced to M45 (S/N 001 to 2000) aircraft also. 32 Longer emergency landing gear cable, no No No HO A A Landing Gear change in system operation. 34 EGPWS, TCAS 2000 and ELT are Navigation installation standards, no operational No No HO A A differences from optional (STC) installations. 35 6 dual masks drop (was 5) Oxygen Oxygen chart in AFM and No No HO A A Pilot’s manual changed. 52 Fuel quantity increase relocated gravity fuel No No HO A A Doors fill door, no operational impact. 53 Fuselage length increase requires no special No No HO A A Fuselage maintenance or operational restrictions. 56 Additional three windows require no special No No HO A A Windows maintenance or operational restrictions. DIFFERENCE AIRCRAFT: Learjet 45 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 PTS No Changes No No HO A A Maneuvers Annex F ODR Table: Learjet 40 to Learjet 75 – DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 40 COMPLIANCE METHOD APPROVED BY (POI)____________________________ TRAINING CHKG/CURR
29 Hydraulic Power Increase in length of hydraulic nose gear extend and retract lines. Hydraulic system operation not affected. No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 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 31 Indicating Recording Systems CAS and CWP messages added for Cabin Altitude problem awareness. L R ECS CAS messages added for bleed air system failures. Note; These changes will be introduced to M45 (S/N 001 to 2000) aircraft also. No No HO A A 32 Landing Gear Longer emergency landing gear cable, no change in system operation. No No HO A A 34 Navigation EGPWS, TCAS 2000 and ELT are installation standards, no operational differences from optional (STC) installations. 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 52 Doors Fuel quantity increase relocated gravity fuel fill door, no operational impact. No No HO A A 53 Fuselage Fuselage length increase requires no special maintenance or operational restrictions. No No HO A A 56 Windows Additional three windows require no special maintenance or operational restrictions. No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 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 PTS Maneuvers No Changes No No HO A A Annex F – ODR Table: Learjet 40 to Learjet 75 DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 40 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR