Annex M Learjet 70 to Learjet 40 – DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 70 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 70 (Garmin) to accommodate Honeywell No No HO A A Primus 1000 suite. Aircraft Relocated flight deck panels No No HO A A General Aircraft Smaller Winglets No No HO A A General Aircraft Passenger cabin differs No No HO A A General Weights Max Ramp Weight increased to 21,750 lbs. No No HO A A Max Takeoff Weight increased to 21,500 lbs. Dimensions Dimensions unchanged No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 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 21 ECS ENVIRONMENTAL CONTROL panel No No HO A A resized and reconfigured. 21 ECS PRESSURIZATION panel configuration. PAX/OXY PRESS panel relocated. APU BLEED switch located on Pressurization panel No No HO A A L/R BLEED, EMER PRESS, PACK, HIFLOW switches located on lower instrument panel 21 ECS ENVIRONMENTAL CONTROL SYSTEM (ECS) synoptic page accessed with DU bezel No Norm HO A A keys and format different 22 AFCS Garmin Mode Controller (GMC) replaced by CSS, Flight Guidance Controller Panel (FGC) PTT No Norm C C FTD 2-5 22 AFCS Flight Director Modes same as G5000 except CSS, Speed versus FLC. No Takeoff Mode (TO) PTT No Norm B B FTD 2-5 22 AFCS Autopilot servos, yaw damper and rudder boost (Manufacturer differs, operation the No No HO A A same) 22 AFCS FD button only disengages flight director. It TCBI, No Norm A A does not engage the flight director. SU
Annex M – Learjet 70 to Learjet 40 DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 70 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 70 (Garmin) to accommodate Honeywell Primus 1000 suite. No No HO A A Aircraft General Relocated flight deck panels No No HO A A Aircraft General Smaller Winglets No No HO A A Aircraft General Passenger cabin differs No No HO A A Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to 21,500 lbs. No No HO A A Dimensions Dimensions unchanged No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 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 21 ECS ENVIRONMENTAL CONTROL panel resized and reconfigured. No No HO A A 21 ECS PRESSURIZATION panel configuration. PAX/OXY PRESS panel relocated. APU BLEED switch located on Pressurization panel L/R BLEED, EMER PRESS, PACK, HIFLOW switches located on lower instrument panel No No HO A A 21 ECS ENVIRONMENTAL CONTROL SYSTEM (ECS) synoptic page accessed with DU bezel keys and format different No Norm HO A A 22 AFCS Garmin Mode Controller (GMC) replaced by Flight Guidance Controller Panel (FGC) No Norm CSS, PTT FTD 2-5 C C 22 AFCS Flight Director Modes same as G5000 except Speed versus FLC. No Takeoff Mode (TO) No Norm CSS, PTT FTD 2-5 B B 22 AFCS Autopilot servos, yaw damper and rudder boost (Manufacturer differs, operation the same) No No HO A A 22 AFCS FD button only disengages flight director. It does not engage the flight director. No Norm TCBI, SU A A