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 35 Oxygen PAX OXY/PRESS panel relocated on pedestal moved to copilot switch panel and No No HO A A relabeled PAX OXYGEN (Also in 21) 45 No Wi-Fi Iridium out. Maintenance data Central accessed with laptop via port in lower No No HO A A Maintenance pedestal System 46 No capability to display electronic flight Information charts or AOPA airport directory. No No HO A A Systems 46 No graphical map capability Information No No HO A A Systems 46 Not capable of XM or international weather Information presentation No No HO A A Systems 70 Powerplant L and R Engine controls relocated on pedestal No No HO A A 70 Powerplant TFE 731-20 AR or BR engines (Decreased thrust from 3850 lbs. to 3500 lbs. or 3650 lbs. No No HO A A with APR active DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 70 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 APPENDIX 3 AIRCRAFT REGULATORY COMPLIANCE CHECKLIST Compliance checklist supplied by Bombardier Learjet for LR-75 only, Original FSB report for LR-45 (05/10/1998) and LR-40 (03/03/2006) did not have compliance checklist. 14 CFR Requirement Compliance Remark FSB Finding Section
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 35 Oxygen PAX OXY/PRESS panel relocated on pedestal moved to copilot switch panel and relabeled PAX OXYGEN (Also in 21) No No HO A A 45 Central Maintenance System No Wi-Fi Iridium out. Maintenance data accessed with laptop via port in lower pedestal No No HO A A 46 Information Systems No capability to display electronic flight charts or AOPA airport directory. No No HO A A 46 Information Systems No graphical map capability No No HO A A 46 Information Systems Not capable of XM or international weather presentation No No HO A A 70 Powerplant L and R Engine controls relocated on pedestal No No HO A A 70 Powerplant TFE 731-20 AR or BR engines (Decreased thrust from 3850 lbs. to 3500 lbs. or 3650 lbs. with APR active No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 70 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 APPENDIX 3 AIRCRAFT REGULATORY COMPLIANCE CHECKLIST Compliance checklist supplied by Bombardier Learjet for LR-75 only, Original FSB report for LR-45 (05/10/1998) and LR-40 (03/03/2006) did not have compliance checklist. 14 CFR Section Requirement Compliance Remark FSB Finding