Dimensions Overall Length Reduced 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 45 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 reduction requires new formulas for weight and balance. No No HO A A 9 Towing and Taxiing Fuselage length reduction results in smaller turning radius, no operational impact. No No HO A A 11 Placards Fuel Quantity placards (interior & exterior) change to reflect useable quantity reduction. No No HO A A 21 Air Conditioning Removal of 2 gaspers. Reduction in length of main cabin condition air ducting. Reduction 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 Reduced length control system cables. Control system operation not affected. No No HO A A 28 Fuel Fuel System difference limited to a reduction in Total Useable Quantity. No change to any other system aspect. No No HO A A 29 Hydraulic Power Reductions in length of hydraulic nose gear extend and retract lines. Hydraulic system operation not affected. No No HO A A 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 M45 (S/N 001 to 2000) aircraft. No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 45 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR SYSTEM REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR 32 Landing Gear Shorter emergency landing gear cable, no change in system operation. No No HO A A 33 Lights Interior lights are LED-based, no operational impact. No No HO A A 34 Navigation EGPWS, TCAS 2000 and ELT are installation standards, no operational No No HO A A
differences from optional (STC) installations. 35 Oxygen 5 dual masks drop (was 6). Oxygen chart in AFM and Pilot’s manual changed. No No HO A A 52 Doors Fuel quantity reduction relocated gravity fuel fill door, no operational impact. No No HO A A 53 Fuselage Fuselage length reduction requires no special maintenance or operational restrictions. No No HO A A 56 Windows Removal of three windows requires no special maintenance or operational restrictions. No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 45 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 C – ODR Table: Learjet 45 to Learjet 75 DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 45 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 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
34 Navigation PFD inset map available to display traffic and navigation map controlled by PFD softkeys. No Norm TCBI, SU A A 34 Navigation FMS… GPS navigation source only, no other GNSS constellations. No Norm HO A A 34 Navigation FMS…. WAAS/LPV standard equipment was optional on base aircraft. No EGNOS capability. No Norm HO A A 34 Navigation Reactive windshear No Norm TCBI, SU A A 34 Navigation MFD auto zoom No Norm HO A A 34 Navigation MFD joystick removed, functionally available at GTCs No Norm HO A A 34 Navigation Standard takeoff and landing (TOLD) database (future provision) No Norm TCBI, SU A A 34 Navigation Nav to Nav transfer available for VOR/ILS approaches No Norm CSS, PTT FTD 2-5 C B 34 Navigation TCAS II Resolution Advisory (RA) indications differ No No HO A A 34 Navigation Garmin’s TAWS versus Honeywell’s EGPWS No Norm HO A A 34 Navigation GPWS panel removed. Functionality and selection now at GTCs No Norm TCBI, SU A A 35 Oxygen Oxygen quantity indications differ. No No HO A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 45 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 OXYGEN panel moved from copilot switch panel to pedestal and relabeled PAX OXY/PRESS No No HO A A 45 Central Maintenance System Optional Wi-Fi Iridium out No No HO A A 46 Information Systems Electronic flight charts via subscription AOPA airport directory available. No Norm TCBI, SU A A 46 Information Systems Graphical maps including geopolitical boundary, land mass and airspace boundaries. No Norm HO A A 46 Information Systems XM weather available through subscription No Norm HO A A 46 Information Systems International weather available through subscription (future provision) No Norm HO A A 46 Information Systems SD card slots installed on each DU to facilitate loading of data bases No Norm HO A A 46 Information CPDLC available No Norm TCBI, SU A A
(POI)____________________________ 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 E – ODR Table: Learjet 40 to Learjet 45 DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 40 APPROVED BY (POI)____________________________ COMPLIANCE METHOD TRAINING CHKG/CURR DESIGN REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR Weights Max Ramp Weight increased to 21,750 lbs. Max Takeoff Weight increased to21,500 lbs. Maximum Zero Fuel Weight increased to 16,500 lbs. No No HO A A Dimensions Overall Length increased 23.55 inches No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 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 23 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
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
(POI)____________________________ TRAINING CHKG/CURR SYSTEM REMARKS FLT CHAR PROC CHNG LVL A LVL B LVL C LVL D CHK CURR 34 Navigation Reactive windshear No Norm TCBI, SU A A 34 Navigation MFD auto zoom No Norm HO A A 34 Navigation MFD joystick removed, functionally available at GTCs No Norm HO A A 34 Navigation Standard takeoff and landing (TOLD) database (future provision) No Norm TCBI, SU A A 34 Navigation Nav to Nav transfer available for VOR/ILS approaches No Norm CSS, PTT FTD 2-5 C B 34 Navigation TCAS II Resolution Advisory (RA) indications differ No No HO A A 34 Navigation Garmin’s TAWS versus Honeywell’s EGPWS No Norm HO A A 34 Navigation GPWS panel removed. Functionality and selection now at GTCs No Norm TCBI, SU A A 35 Oxygen 6 dual masks drop (was 5) Oxygen chart in AFM and Pilot’s manual changed. No No HO A A 35 Oxygen Oxygen quantity indications differ. No No HO A A 35 Oxygen PAX OXYGEN panel moved from copilot switch panel to pedestal and relabeled PAX OXY/PRESS No No HO A A 45 Central Maintenance System Optional Wi-Fi Iridium out No No HO A A 46 Information Systems Electronic flight charts via subscription AOPA airport directory available. No Norm TCBI, SU A A 46 Information Systems Graphical maps including geopolitical boundary, land mass and airspace boundaries. No Norm HO A A 46 Information Systems XM weather available through subscription No Norm HO A A 46 Information Systems International weather available through subscription (future provision) No Norm HO A A 46 Information Systems SD card slots installed on each DU to facilitate loading of data bases No Norm HO A A 46 Information Systems CPDLC available (future provision) No Norm TCBI, SU A A DIFFERENCE AIRCRAFT: Learjet 75 BASE AIRCRAFT: Learjet 40 APPROVED BY COMPLIANCE METHOD
27 Flight Controls PIT TRIM BIAS switch moved to FLIGHT CONTROL panel on pedestal. No No HO A A 27 Flight Controls ELEV DISC handle relocated on pedestal No No HO A A 27 Flight Controls RUD BOOST SW/IND located to FLIGHT CONTROL panel on pedestal. No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 30 Ice and Rain ANTI-ICE panel moved from center switch panel to pedestal. No No HO A A 30 Ice and Rain ANTI-ICE test moved from rotary switch to GTC 1 and 2 No No TCBI, SU A A 31 Indicating/ Recording Three LCD Display Units installed with select key functionality on lower bezel surfaces No Norm Abnorm CSS, PTT FTD 2-5 B B 31 Indicating/ Recording Summary Page and all Synoptics differ in presentation No No HO A A 31 Indicating/ Recording Electronic Flight Information System (EFIS) differs in presentation and functionality. No Norm Abnorm HO A A 31 Indicating/ Recording Engine Indicating and Crew Alerting System (EICAS) differs in presentation and functionality No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Selectable Synthetic Vision System (SVS) on Pilot and copilot DUs No Norm TCBI, SU B A 31 Indicating/ Recording System synoptics changed in presentation No Norm Abnorm HO A A 31 Indicating/ Recording Optional flight data recorder differs. (future provision) --- --- 31 Indicating/ Recording Clock functions and indications differ. No Norm HO A A 31 Indicating/ Recording Advisory AOA indication selectable at PFD. No No HO A A 31 Indicating/ Recording Cockpit Voice Recorder (CVR) panel removed. No No HO A A 31 Indicating/ Recording Garmin Stall Warning indications differ No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Stall Warning test moved to GTC 1 and 2 and indications during test differ. No Norm TCBI, SU A A 31 Indicating/ Recording New green bar indication on airspeed indicator represents approach reference speed. No Norm HO A A
34 Navigation PFD’s Nav source, course and bearing pointers controlled by DU soft key selection. No Norm CSS, PTT FTD 2-5 C C 34 Navigation Pilot’s and copilot’s Display Control panels replaced by DU softkeys and GTCs. No Norm Abnorm TCBI, SU A A 34 Navigation Garmin integrated AHRS system replaces Honeywell equipment. No Norm Abnorm HO A A 34 Navigation Navigation radios controlled and displayed at GTCs No Norm TCBI, SU A A 34 Navigation Navigation active and standby frequencies displayed on PFDs No No HO A A 34 Navigation ADC test removed, now a BIT test. No Norm HO A A 34 Navigation Electronic Standby Instrument System installed (ESIS) Four standby indications: A/S; ALT; ATT; and HDG. ESIS capable of ILS guidance. No Norm Abnorm CSS, PTT FTD 2-5 B B 34 Navigation PFD’s Nav Source and bearing pointers selected via DU softkeys. Course controlled via Garmin Mode Controller (GMC) No Norm TCBI, SU A A DIFF DIFFERENCE AIRCRAFT: Learjet 70 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 34 Navigation Mode S transponder with Enhanced Surveillance and ADS-B-Out (Future Provision) selected and displayed at GTCs. No Norm HO A A 34 Navigation Transponder automatic - ground or altitude. No No HO A A 34 Navigation Lightning detection standard equipment and controlled by GTC 1 and 2 No Abnorm HO A A 34 Navigation New weather radar selected at GTCs. No separate control panel. No Norm TCBI, SU A A 34 Navigation FMS CDUs removed, functionality and control at GTC1 and 2 No Norm CSS, PTT FTD 2-5 C C 34 Navigation PFD inset map available to display traffic and navigation map controlled by PFD softkeys. No Norm TCBI, SU A A 34 Navigation FMS… GPS navigation source only, no other GNSS constellations. No Norm HO A A
Annex I – ODR Table: Learjet 75 to Learjet 45 DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 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 75 (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 Aircraft General Dimensions unchanged No No HO A A DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 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 22 AFCS No UP/DOWN wheel on FGC panel. No Norm TCBI, SU A A
24 Electrics 27 or 38 Amp-Hour NiCad or 28 Amp-Hour lead acid batteries are available. No battery heater. No Abnorm Emer HO A A 24 Electrics Emergency Bus load shedding/distribution No Abnorm Emer TCBI, SU A A 24 Electrics CAB PWR SW/IND located on Co-Pilot’s sidewall No No HO A A 24 Electrics Circuit breaker panel (CBP), CB location on panels reassigned. No No HO A A 24 Electrics Electrical synoptic page accessed via DU bezel keys and different format No Norm HO A A 25 Equipment and Furnishings Emergency Locator Transmitter (ELT) does not have GPS. ELT switch panel and indicator light located on separate panel on pedestal. No No HO A A 26 Fire Engine and APU switches and panels relocated on pedestal. No No HO A A 26 Fire Crew Warning Panel/RMU indications installed No Norm Emer TCBI, SU A A 26 Fire Fire test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 27 Flight Controls EICAS and Synoptic Indications of: aileron trim; rudder trim; pitch trim; flaps; and, spoilers different No Norm HO A A 27 Flight Controls SPLN RESET and FLAP RESET functionality on rotary test knob located on SYS TEST/RESET panel on throttle quadrant. No Abnorm HO A A 27 Flight Controls PIT TRIM BIAS switch moved to throttle quadrant No No HO A A 27 Flight Controls PITCH TRIM/RUDDER TRIM panel relocated on pedestal No No HO A A 27 Flight Controls RUD BOOST SW/IND relocated to throttle quadrant No No HO A A 27 Flight Controls Pilot’s and copilot’s RUD PEDAL switches relocated on pilot and copilot switch panels and relabeled RUDDER PEDAL No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 30 Ice and Rain ANTI-ICE panel moved from pedestal to center switch panel. No No HO A A 30 Ice and Rain Anti-Ice system test accomplished on SYS TEST/RESET rotary test knob on pedestal No No TCBI, SU A A
DIFFERENCE AIRCRAFT: Learjet 45 BASE AIRCRAFT: Learjet 75 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 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 45 BASE AIRCRAFT: Learjet 75 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 J – ODR Table: Learjet 75 to Learjet 40 DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 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 75 (Garmin) to accommodate Honeywell Primus 1000 suite. No No HO A A
23 Comm Transmit and receive selection moved from GTC to ACP No Norm TCBI, SU A A 23 Comm L/R Oxygen Mask/Mic selection moved from pilot and copilot switch panels to ACPs and relabeled PAX OXY/AUTO No Norm Abnorm Emer HO A A 23 Comm RADIO CTL HOT BUS SW/IND added. No Norm TCBI, SU A A 23 Comm Optional Satellite Phone Handset on pedestal No Norm HO A A 23 Comm No record and playback of clearances capability No No HO A A 23 Comm EMER COM switch functionality differs No Abnorm Emer TCBI, SU A A 24 Electrics ELECTRICAL panel moved from pedestal to Pilot Switch Panel. No No HO A A 24 Electrics EMER BATT switch for STBY INSTR changed to SW/IND No Norm Emer TCBI, SU A A 24 Electrics 27 or 38 Amp-Hour NiCad or 28 Amp-Hour lead acid batteries are available. No battery heater. No Abnorm Emer HO A A 24 Electrics Emergency Bus load shedding/distribution No Abnorm Emer TCBI, SU A A 24 Electrics CAB PWR SW/IND located on Co-Pilot’s sidewall No No HO A A 24 Electrics Circuit breaker panel (CBP), CB location on panels reassigned. No No HO A A 24 Electrics Electrical synoptic page accessed via DU bezel keys and different format No Norm HO A A 25 Equipment and Furnishings Emergency Locator Transmitter (ELT) does not have GPS. ELT switch panel and indicator light located on separate panel on pedestal. No No HO A A 26 Fire Engine and APU switches and panels relocated on pedestal. No No HO A A 26 Fire Crew Warning Panel/RMU indications installed No Norm Emer TCBI, SU A A 26 Fire Fire test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 27 Flight Controls EICAS and Synoptic Indications of: aileron trim; rudder trim; pitch trim; flaps; and, spoilers different No Norm HO A A 27 Flight Controls SPLN RESET and FLAP RESET functionality on rotary test knob located on SYS TEST/RESET panel on throttle quadrant. No Abnorm HO A A 27 Flight Controls PIT TRIM BIAS switch moved to throttle quadrant No No HO A A 27 Flight Controls PITCH TRIM/RUDDER TRIM panel relocated on pedestal No No HO A A
27 Flight Controls RUD BOOST SW/IND relocated to throttle quadrant No No HO A A 27 Flight Controls Pilot’s and copilot’s RUD PEDAL switches relocated on pilot and copilot switch panels and relabeled RUDDER PEDAL No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 30 Ice and Rain ANTI-ICE panel moved from pedestal to center switch panel. No No HO A A 30 Ice and Rain Anti-Ice system test accomplished on SYS TEST/RESET rotary test knob on pedestal No No TCBI, SU A A 31 Indicating/ Recording Four CRT displays select key functionality on lower bezel surfaces No Norm Abnorm TCBI, SU B A 31 Indicating/ Recording Summary Page and all Synoptics differ in presentation No No TCBI, SU A A 31 Indicating/ Recording Electronic Flight Information System (EFIS) differs in presentation and functionality. No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Engine Indicating and Crew Alerting System (EICAS) differs in presentation and functionality No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording No Synthetic Vision System (SVS) No No HO A A 31 Indicating/ Recording Chronometer/clock installed at both the pilot and copilot position. No Norm TCBI, SU A A 31 Indicating/ Recording Advisory AOA indications located on optional stand-alone AOA gauge on instrument panel No No HO A A 31 Indicating/ Recording Cockpit Voice Recorder (CVR) panel installed. No No HO A A 31 Indicating/ Recording Honeywell Stall Warning system (No vane change) PFD indications differ in presentation No Norm Abnorm Emer TCBI, SU A A 31 Indicating/ Recording Stall system test accomplished with SYS TEST/RESET rotary knob on pedestal. PFD test indications different No Norm TCBI, SU A A 31 Indicating/ Recording No Green Circle Ratio presented on airspeed indicator No Norm Abnorm HO A A 31 Indicating/ Recording Landing gear position indications moved from EICAS to GEAR/HYD panel No Norm Abnorm HO A A 31 Indicating/ Recording Optional Runway Awareness Alerting System (RAAS) available No No HO A A 31 Indicating/ Recording (Optional) Electronic Checklist selected for display on MFD with MFD bezel keys. No Norm HO A A
31 Indicating/ Recording DU REVERSION/DIM panel moved to pilot switch panel and labeled REVERSION - includes ADC/AHRS/ICSG reversion switches No Abnorm Emer CSS, PTT FTD 2-5 B A 31 Indicating/ Recording DU2 and DU3 reversion controls on pilot’s and copilot’s glareshield. No Abnorm CSS, PTT FTD 2-5 B A 31 Indicating/ Recording Low Speed Awareness and Overspeed cues on PFDs, color logic changed. No No HO A A 31 Indicating/ Recording Heading, speed, altitude select bugs and navigation source color logic changes. No No HO A A 31 Indicating/ Recording VSI indication changed from a tape to an arc. No No HO A A 31 Indicating/ Recording Electronic navigation chart display not available No No HO A A 31 Indicating/ Recording FPV now FPA (Flight Path Angle) and generated by the Universal FMS. Includes speed carat indication No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Database management accomplished through separate Data Transfer Unit No No HO A A 32 Landing Gear Shorter emergency landing gear cable, no change in system operation. No No HO A A 32 Landing Gear GEAR/HYD panel moved from center switch panel to co-pilot switch panel. No No HO A A 32 Landing Gear Landing Gear handle moved from Co-Pilot’s switch panel to GEAR/HYD panel No No HO A A 32 Landing Gear Gear test accomplished with rotary test knob on pedestal No Norm TCBI, SU A A 32 Landing Gear Gear Caution/Warning indications differ in presentation. Logic is the same No No HO A A 32 Landing Gear No Synoptic presentation of AUX HYD or HYD XFLOW indications No No HO A A 33 Lights Exterior light control; no smoking/belts; and Emergency light switches moved from overhead light switch panel to center switch panel No Norm HO A A 33 Lights Lights test accomplished with rotary knob on pedestal. Also runs audio test. No Norm TCBI, SU A A 34 Navigation Some of the pilot’s and copilot’s Garmin’s DU softkeys and GTCs functions replaced by Pilot/Co-Pilot’s PFD Display Controllers. No Norm Abnorm CSS, PTT FTD 2-5 B B 34 Navigation Honeywell’s AHRS replaces Garmin’s integrated AHRS system No Norm Abnorm HO A A
34 Navigation Pilot’s and copilot’s PFD display options controlled by PFD Display Controllers. No Norm Abnorm TCBI, SU A A 34 Navigation Tuning of Navigation radios via RMUs. Audio portion of Nav radios controlled via Audio control panels located on pilot and copilot instrument panels. No Norm Abnorm CSS, PTT FTD 2-5 B A 34 Navigation No automatic reversion of ADCs during malfunctions. No Norm Abnorm TCBI, SU A A 34 Navigation ADC test added, not a BIT test. Test completed with rotary test switch located on pedestal. No Norm TCBI, SU A A 34 Navigation Traditional round gauges replace Integrated Electronic Standby (IESI) for Airspeed, Attitude and Altitude. Standby navigation accomplished on RMU. No Abnorm Emer TCBI, SU B B 34 Navigation PFD’s Nav Source, Course and bearing pointers controlled via Pilot/Co-Pilot PFD display Controllers located on glareshield No Norm TCBI, SU A A 34 Navigation Mode S transponder without Enhanced Surveillance and ADS-B-Out No Norm Abnorm Emer HO A A 34 Navigation Transponder, no auto select function for ground and airborne ops. No Norm Abnorm HO A A 34 Navigation Different weather radar with panel located on pedestal. No lightning or turbulence detection. No Norm TCBI, SU A A 34 Navigation Universal FMS CDUs located on pedestal. Operation and functionality different No Norm CSS, PTT FTD 2-5 C C 34 Navigation No PFD insert map to display traffic or navigation. No No HO A A 34 Navigation Universal FMS uses GPS, VOR and DME/DME capability. (Garmin uses GPS and SBAS WAAS only) No Norm Abnorm HO A A 34 Navigation WAAS/LPV optional equipment on Universal FMS. Operation and functionality different No Norm Abnorm HO A A 34 Navigation No reactive wind shear detection and guidance. No No HO A A 34 Navigation No MFD Auto-Zoom No No HO A A DIFFERENCE AIRCRAFT: Learjet 40 BASE AIRCRAFT: Learjet 75 APPROVED BY (POI)____________________________ COMPLIANCE METHOD 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
24 Electrics CAB PWR SW/IND located on Co-Pilot’s sidewall No No HO A A 24 Electrics Circuit breaker panel (CBP), CB location on panels reassigned. No No HO A A 24 Electrics Electrical synoptic page accessed via DU bezel keys and different format No Norm HO A A 25 Equipment and Furnishings Emergency Locator Transmitter (ELT) does not have GPS. ELT switch panel and indicator light located on separate panel on pedestal. No No HO A A 26 Fire Engine and APU switches and panels relocated on pedestal. No No HO A A 26 Fire Crew Warning Panel/RMU indications installed No Norm Emer TCBI, SU A A 26 Fire Fire test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 27 Flight Controls Increased length control system cables. Control system operation not affected. No No HO A A 27 Flight Controls EICAS and Synoptic Indications of: aileron trim; rudder trim; pitch trim; flaps; and, spoilers different No Norm HO A A 27 Flight Controls SPLN RESET and FLAP RESET functionality on rotary test knob located on SYS TEST/RESET panel on throttle quadrant. No Abnorm HO A A 27 Flight Controls PIT TRIM BIAS switch moved to throttle quadrant No No HO A A 27 Flight Controls PITCH TRIM/RUDDER TRIM panel relocated on pedestal No No HO A A 27 Flight Controls RUD BOOST SW/IND relocated to throttle quadrant No No HO A A 27 Flight Controls Pilot’s and copilot’s RUD PEDAL switches relocated on pilot and copilot switch panels and relabeled RUDDER PEDAL No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 28 Fuel Fuel System difference limited to an increase in Total Usable 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 30 Ice and Rain ANTI-ICE panel moved from pedestal to center switch panel. No No HO A A 30 Ice and Rain Anti-Ice system test accomplished on SYS TEST/RESET rotary test knob on pedestal No No TCBI, SU A A 31 Indicating/ Recording Four CRT displays select key functionality on lower bezel surfaces No Norm Abnorm TCBI, SU B A
31 Indicating/ Recording Summary Page and all Synoptics differ in presentation No No TCBI, SU A A 31 Indicating/ Recording Electronic Flight Information System (EFIS) differs in presentation and functionality. No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Engine Indicating and Crew Alerting System (EICAS) differs in presentation and functionality No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording No Synthetic Vision System (SVS) No No HO A A 31 Indicating/ Recording Chronometer/clock installed at both the pilot and copilot position. No Norm TCBI, SU A A 31 Indicating/ Recording Advisory AOA indications located on optional stand-alone AOA gauge on instrument panel No No HO A A 31 Indicating/ Recording Cockpit Voice Recorder (CVR) panel installed. No No HO A A 31 Indicating/ Recording Honeywell Stall Warning system (No vane change) PFD indications differ in presentation No Norm Abnorm Emer TCBI, SU A A 31 Indicating/ Recording Stall system test accomplished with SYS TEST/RESET rotary knob on pedestal. PFD test indications different No Norm TCBI, SU A A 31 Indicating/ Recording No Green Circle Ratio presented on airspeed indicator No Norm Abnorm HO A A 31 Indicating/ Recording Landing gear position indications moved from EICAS to GEAR/HYD panel No Norm Abnorm HO A A 31 Indicating/ Recording Optional Runway Awareness Alerting System (RAAS) available No No HO A A 31 Indicating/ Recording (Optional) Electronic Checklist selected for display on MFD with MFD bezel keys. No Norm HO A A 31 Indicating/ Recording DU REVERSION/DIM panel moved to pilot switch panel and labeled REVERSION - includes ADC/AHRS/ICSG reversion switches No Abnorm Emer CSS, PTT FTD 2-5 B A 31 Indicating/ Recording DU2 and DU3 reversion controls on pilot’s and copilot’s glareshield. No Abnorm CSS, PTT FTD 2-5 B A 31 Indicating/ Recording Low Speed Awareness and Overspeed cues on PFDs, color logic changed. No No HO A A 31 Indicating/ Recording Heading, speed, altitude select bugs and navigation source color logic changes. No No HO A A 31 Indicating/ VSI indication changed from a tape to an arc. No No HO A A
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
24 Electrics EMER BATT switch for STBY INSTR changed to SW/IND No Norm Emer TCBI, SU A A 24 Electrics 27 or 38 Amp-Hour NiCad or 28 Amp-Hour lead acid batteries are available. No battery heater. No Abnorm Emer HO A A 24 Electrics Emergency Bus load shedding/distribution No Abnorm Emer TCBI, SU A A 24 Electrics CAB PWR SW/IND located on Co-Pilot’s sidewall No No HO A A 24 Electrics Circuit breaker panel (CBP), CB location on panels reassigned. No No HO A A 24 Electrics Electrical synoptic page accessed via DU bezel keys and different format No Norm HO A A 25 Equipment and Furnishings Emergency Locator Transmitter (ELT) does not have GPS. ELT switch panel and indicator light located on separate panel on pedestal. No No HO A A 26 Fire Engine and APU switches and panels relocated on pedestal. No No HO A A 26 Fire Crew Warning Panel/RMU indications installed No Norm Emer TCBI, SU A A 26 Fire Fire test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 27 Flight Controls EICAS and Synoptic Indications of: aileron trim; rudder trim; pitch trim; flaps; and, spoilers different No Norm HO A A 27 Flight Controls SPLN RESET and FLAP RESET functionality on rotary test knob located on SYS TEST/RESET panel on throttle quadrant. No Abnorm HO A A 27 Flight Controls PIT TRIM BIAS switch moved to throttle quadrant No No HO A A 27 Flight Controls PITCH TRIM/RUDDER TRIM panel relocated on pedestal No No HO A A 27 Flight Controls RUD BOOST SW/IND relocated to throttle quadrant No No HO A A 27 Flight Controls Pilot’s and copilot’s RUD PEDAL switches relocated on pilot and copilot switch panels and relabeled RUDDER PEDAL No No HO A A 27 Flight Controls Flaps test accomplished with SYS TEST/RESET rotary knob on pedestal No Norm TCBI, SU A A 30 Ice and Rain ANTI-ICE panel moved from pedestal to center switch panel. No No HO A A 30 Ice and Rain Anti-Ice system test accomplished on SYS TEST/RESET rotary test knob on pedestal No No TCBI, SU A A 31 Indicating/ Recording Four CRT displays select key functionality on lower bezel surfaces No Norm Abnorm TCBI, SU B A
31 Indicating/ Recording Summary Page and all Synoptics differ in presentation No No TCBI, SU A A 31 Indicating/ Recording Electronic Flight Information System (EFIS) differs in presentation and functionality. No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording Engine Indicating and Crew Alerting System (EICAS) differs in presentation and functionality No Norm Abnorm TCBI, SU A A 31 Indicating/ Recording No Synthetic Vision System (SVS) No No HO A A 31 Indicating/ Recording Chronometer/clock installed at both the pilot and copilot position. No Norm TCBI, SU A A 31 Indicating/ Recording Advisory AOA indications located on optional stand-alone AOA gauge on instrument panel No No HO A A 31 Indicating/ Recording Cockpit Voice Recorder (CVR) panel installed. No No HO A A 31 Indicating/ Recording Honeywell Stall Warning system (No vane change) PFD indications differ in presentation No Norm Abnorm Emer TCBI, SU A A 31 Indicating/ Recording Stall system test accomplished with SYS TEST/RESET rotary knob on pedestal. PFD test indications different No Norm TCBI, SU A A 31 Indicating/ Recording No Green Circle Ratio presented on airspeed indicator No Norm Abnorm HO A A 31 Indicating/ Recording Landing gear position indications moved from EICAS to GEAR/HYD panel No Norm Abnorm HO A A 31 Indicating/ Recording (Optional) Runway Awareness Alerting System (RAAS) available No No HO A A 31 Indicating/ Recording (Optional) Electronic Checklist selected for display on MFD with MFD bezel keys. No Norm HO A A 31 Indicating/ Recording DU REVERSION/DIM panel moved to pilot switch panel and labeled REVERSION - includes ADC/AHRS/ICSG reversion switches No Abnorm Emer CSS, PTT FTD 2-5 B A 31 Indicating/ Recording DU2 and DU3 reversion controls on pilot’s and copilot’s glareshield. No Abnorm CSS, PTT FTD 2-5 B A 31 Indicating/ Recording Low Speed Awareness and Overspeed cues on PFDs, color logic changed. No No HO A A 31 Indicating/ Recording Heading, speed, altitude select bugs and navigation source color logic changes. 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 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
91. 9 (a) Compliance with Flight Manual, Markings, and Placard Markings Compliant An Airplane Flight Manual is provided and placards are installed Complies 91. 9 (b)(1) Availability of Current Airplane Flight Manual in Aircraft Compliant An Airplane Flight Manual is provided and placards are installed Complies 91. 9 (c) Identification of Aircraft in Accordance with FAR 45 Compliant Aircraft is identified painted on the aircraft Complies 91.103 (a) IFR Flight Planning and Fuel Requirements Compliant Aircraft performance information is provided in the AFM and in the Pilots guide Complies 91.103 (b)(1) Preflight Planning Runway Performance Data Compliant Aircraft performance takeoff and landing data is provided in the AFM Complies 91.126 (c) On or In The Vicinity of an Airport in Class G Airspace Minimum Certificated Landing Flap Setting Compliant Aircraft performance landing data for normal and abnormal flap settings are provided in the AFM Complies 91.180 (a)(1) Reduced Vertical Separation Minimums Compliant RVSM operational information and procedures are provided in the AFM Complies 91.189 Category II or III Operations Not Applicable Not approved for operation Not Applicable
91.217 (b) Same Source Compliant Derived from same source Complies 91.219 (a) Approved Altitude Alerting System Compliant An altitude alerting system is installed in the aircraft Complies 91.219 (b) Altitude alerting system or device. Compliant An altitude alerting system is installed in the aircraft Complies 91.221 (a)(b) Traffic Alert and Collision Avoidance System Equipment and Use Compliant A Traffic Collision Avoidance System, TCAS, with resolution advisory is installed in the aircraft Complies 91.223 (a) Terrain Awareness and Warning System Compliant Compliant Class A TAWS to C151B installed Complies 91.223 (b) Terrain Awareness and Warning System Not applicable Manufactured after Mar 29, 2002 Not Applicable 91.223 (c) Terrain Awareness and Warning System Compliant The AFM contains the procedures for the Terrain Awareness Warning System, TAWS Complies 91.223 (d) Terrain Awareness and Warning System Not applicable Not Applicable
91.413 ATC Transponder Tests and Inspections Operator Responsibility Agree - Operator Responsibility 91.503 (a)(1) Flying Equipment and Operating Information: Flashlights Operator Responsibility PIC responsibility Agree - Operator Responsibility 91.503 (a)(2) Cockpit Checklist Compliant Procedure provided in AFM & a checklist is provided with the aircraft Complies 91.503 (a)(3) (a)(4) Aeronautical Charts Operator Responsibility PIC responsibility Agree - Operator Responsibility 91.503 (a)(5) One Engine Inoperative Climb Performance Data Compliant Procedure provided in AFM & a checklist is provided with the aircraft Complies 91.503 (b)(c) Cockpit Checklist Contents Compliant Procedure provided in AFM & a checklist is provided with the aircraft Complies 91.503 (d) Use of Data by Crew Operator Responsibility PIC responsibility Agree - Operator Responsibility 91.505 Familiarity with Operating Limitations and Emergency Equipment Operator Responsibility PIC responsibility Agree - Operator Responsibility
91.507 Equipment Requirement: Over the Top, or Night VFR Operations Compliant Aircraft has necessary instruments and equipment and multiple landing lights Complies 91.509 (a) Survival Equipment for Overwater Operations (life preserver / flotation means) Compliant Aircraft has flotation devices for each seat Complies 91.509 (b) Survival Equipment for Overwater Operations (extended overwater equipment) Operator Responsibility PIC responsibility Agree - Operator Responsibility 91.509 (d)(e) Survival Equipment for Overwater Operations (extended overwater equipment) Operator Responsibility PIC responsibility Agree - Operator Responsibility 91.511 Radio Equipment for Overwater Operations Compliant The radio communication and navigation equipment installed meets the requirements Complies 91.513 Emergency Equipment Compliant All emergency equipment is installed Complies 91.517 Passenger information Compliant Passenger signs are installed Complies 91.519 Passenger Briefing Operator Responsibility Part of Cabin Management System (CMS) Agree - Operator Responsibility
91.521 Shoulder Harness Compliant Shoulder harnesses are installed Complies 91.525 Carriage of Cargo Operator Responsibility Agree - Operator Responsibility 91.527 Operating in Icing Conditions Compliant Anti-ice equipment is installed Complies 91.531 Second In Command Requirements Compliant Two pilots required Complies 91.533 Flight Attendant Requirements Not applicable Not Applicable 91.535 Stowage of Food, Beverages and Passenger Service Equipment. Operator Responsibility Agree - Operator Responsibility 91.603 Aural Speed Warning Device Compliant Aural Speed warning installed Complies 91.605 Transport Category Civil Airplane Weight Limitations Operator Responsibility Agree - Operator Responsibility
91.607 Emergency Exits for Airplanes Carrying Passengers for Hire Compliant Equipped with emergency exit Complies 91.609 (a) Operation with Inactive Flight Data Recorder or Cockpit Voice Recorder Operator Responsibility Agree - Operator Responsibility 91.609 (b) Operation by Other than Holder of Air Carrier or Commercial Certificate Operator Responsibility Agree - Operator Responsibility 91.609 (c) Requirements for Flight Data Recorder - 10+ passengers Not applicable Not Applicable 91.609 (d) FDR Operations Operator Responsibility Agree - Operator Responsibility 91.609 (e)(f) Requirement for Cockpit Voice Recorder Compliant CVR installed Complies 91.609 (g) Accident Reporting Operator Responsibility Agree - Operator Responsibility 91.609 (h) CVR specifications effective April 7, 2012 Compliant CVR meets requirements Complies
91.609 (i) Cockpit Voice Recorder Not Applicable Operator Responsibility 91.609 (j) Datalink Recording Not applicable Operator Responsibility 91.613 Materials for Compartment Interiors Compliant Interior materials meet requirements Complies 91.801 (a)(2) Part 36 Applicability Compliant Meets noise limits Complies 91.805 Operating Noise Limits for Subsonic Airplanes Compliant Meets noise limits Complies 91.853 Operating Noise Limits for Subsonic Airplanes Compliant Meets noise limits Complies 91.1023 & .1025 Program Operating Manual Requirements and Contents Operator Responsibility Agree - Operator Responsibility 91.1033 (a)(1) & (b) Cockpit Checklist Compliant Checklist provided with aircraft Complies
91.1033 (a)(2) & (c) Emergency Cockpit Checklist Compliant Checklist provided with aircraft Complies 91.1033 (a)(3) Aeronautical Charts Operator Responsibility Agree - Operator Responsibility 91.1033 (a)(4) IFR Navigation/Approach Charts Operator Responsibility Agree - Operator Responsibility 91.1035 (e) Automated Briefing Recording Optionally Compliant Integrated into the Cabin Management System (CMS) Agree - Operator Responsibility 91.1035 (f) Passenger Briefing Cards Compliant Cards come with aircraft Complies 91.1045 (b)(1) Cockpit Voice Recorder Compliant CVR installed Complies 91.1045 (b)(2) Flight Recorder Not applicable Not Applicable 91.1045 (b)(3) TAWS System Compliant TAWS installed Complies
91.1045 (b)(4) TCAS System Compliant TCAS installed Complies 91.1045 (b)(5) Airborne Weather Radar Equipment Compliant Weather radar installed Complies 91.1109 (b)(1) Manufacturer Aircraft Maintenance Inspection Program Operator Responsibility Agree - Operator Responsibility 91.1115 (a) Minimum Equipment List Operator Responsibility Agree - Operator Responsibility 91.1411 Continuous Airworthiness Maintenance Program Operator Responsibility Agree - Operator Responsibility 91.App A Category II Operations Not Applicable Not approved for operation Not Applicable 91.App C Operations in the North Atlantic (NAT) Minimum Navigation Performance Specifications (MNPS) Airspace Compliant Navigation tolerances qualify for NAT MNPS airspace Complies 91 App G Operations in Reduced Vertical Separation (RVSM) Airspace Compliant Navigation tolerances qualify for RVSM airspace Complies
135.123 Emergency and Emergency Evacuation Duties Operator Responsibility Agree - Operator Responsibility 135.127 Passenger Information Compliant Passenger signs installed Complies 135.128 Safety Belts and Child Restraint Systems Operator Responsibility Safety belts installed. Child restraint system provided by carrier or passenger Agree - Operator Responsibility 135.129 (d)(e) Exit Seating Passenger Information Cards Operator Responsibility Agree - Operator Responsibility 135.143 (b) Approved/Operable Instruments and Equipment Compliant Required instruments installed Complies 135.143 (c) ATC Transponder Compliant Required transponder installed Complies 135.145 (d)(1) Validation Testing Operator Responsibility Agree - Operator Responsibility 135.147 Dual Controls Required Compliant Two pilots required Complies
135.149 (a) Altimeter Adjustable for Barometric Pressure Compliant Two primary and standby altimeters installed Complies 135.149 (b) Heating or Deicing Equipment Not applicable Not Applicable 135.149 (c) Turbojet Additional equipment Compliant Standby ADI installed Complies 135.149 (e) Additional Equipment Administrator Requires Compliant As required by the Administrator Complies 135.150 (a) Public Address System Not applicable PA system installed Not Applicable 135.150 (b) Crew Interphone System Not applicable Interphone system installed Not Applicable 135.151 (a) Requirement and Installation of CVR Compliant CVR installed Complies 135.151 (b) Requirement and Installation of CVR Not applicable CVR installed Not Applicable
135.151 (d) Boom and Mask Microphone Compliant Boom and mask interphone installed Complies 135.151 (c)(e) CVR - Recorded Data Compliant CVR capable of keeping recorded data Complies 135.151 (f) Additional CVR Requirements Not applicable Operator Responsibility 135.151 (g) Additional CVR Requirements Compliant Required CVR installed Complies 135.151 (h) Recording Datalink messages Not applicable Operator Responsibility 135.152 (a) Requirement for FDR Not applicable Operator Responsibility 135.152 (b) Requirement for Flight Data Recorder Not applicable Not Applicable 135.152 (c) FDR Operations Not applicable Operator Responsibility
135.152 (d)(e) FDR – Recorded Data Operator Responsibility Agree - Operator Responsibility 135.152 (f) Installation Requirements Not applicable Operator Responsibility 135.152 (g) Underwater Locator Device Not applicable Operator Responsibility 135.152 (h) Operational Parameters Required to be Recorded Not applicable Operator Responsibility 135.152 (i) FDR required parameters data ranges, accuracies, resolutions and intervals Not applicable Not Applicable 135.152 (j) FDR required parameters data ranges, accuracies, resolutions and intervals Not applicable Not Applicable 135.152 (m) FDR Requirements Not applicable Operator Responsibility 135.153 (a) Requirement for GPWS Compliant Installed GPWS compliant Complies
135.153 (c) Airplane Flight Manual Compliant AFM supplied with aircraft Complies 135.154 (a) Terrain Awareness and Warning System Compliant Installed TAWS compliant Complies 135.154 (c) AFM procedures for TAWS Compliant AFM supplied with aircraft Complies 135.155 (a) Fire Extinguishers: Type and Suitability of Agent Compliant Halon 1211 Complies 135.155 (b) Fire Extinguisher on Flight Deck Compliant Halon 1211 Complies 135.155 (c) Fire Extinguisher in Passenger Compartment Compliant Customer option Complies 135.156 Flight data Recorders: Filtered Data Not applicable Not Applicable 135.157 (a) Oxygen Equipment Requirements Unpressurized aircraft. Not applicable Not Applicable
135.157 (b) Oxygen Equipment Requirements Pressurized Aircraft. Compliant Installed O2 system compliant Complies 135.157 (c) Equipment requirement Compliant Installed O2 system compliant Complies 135.158 (a) Pitot Heat Indicating Systems Requirement and Operation Compliant Pitot Heat Indicating System installed Complies 135.159 (a) - (g) Equipment Requirements: Carrying Passengers under VFR at Night or under VFR Over The Top Conditions Compliant Required equipment installed Complies 135.161 Radio and Navigational Equipment: Aircraft Carrying Passengers Under VFR at Night or under VFR Over The Top Compliant Required equipment installed Complies 135.163 Equipment Requirements: Aircraft Carrying Passengers Under IFR Compliant Required equipment installed Complies 135.165 Radio and Navigational Equipment: Extended Overwater or IFR Operations Compliant Required equipment installed Complies 135.167 Emergency Equipment: Extended Overwater Operations Optionally Compliant Operator Responsibility
135.169 Additional Airworthiness Requirements Compliant Cargo bay compliant Complies 135.170 Materials for Compartment Interiors Compliant Interior materials compliant Complies 135.171 (a) Shoulder Harness Installation at Flight Crewmember Stations Not applicable Shoulder harness system installed Complies 135.173 (a) Airborne Thunderstorm Detection Equipment Not applicable Airborne weather radar installed Not Applicable 135.173 (f) Power Supply Not applicable Not Applicable 135.175 (a) Airborne Weather Radar Equipment Compliant Airborne weather radar installed Complies 135.175 (e) Power Supply Not applicable Not Applicable 135.177 Emergency Equipment Requirements for more than 19 Passengers Not applicable Not Applicable
135.178 Additional Emergency Equipment Not applicable Not Applicable 135.179 (a) Inoperable Instruments and Equipment Operator Responsibility Instruments installed and operating Agree - Operator Responsibility 135.179 (b) Instruments and Equipment NOT included in MEL Operator Responsibility Instruments installed and operating Agree - Operator Responsibility 135.180 (a) Requirement for an approved TCAS Not applicable TCAS installed Complies 135.180 (b) Flight Manual Requirements Not applicable TCAS instructions included in AFM Complies 135.181 (a)(1) Performance Requirements: Single Engine Aircraft Operated Over The Top or in IFR Conditions Not applicable Not Applicable 135.181 (a)(2) Performance Requirements: Multi Engine Aircraft Operated Over The Top or in IFR Conditions Compliant Aircraft compliant if limitations in AFM are not exceeded Complies 135.183 (a) Performance Requirements: Land Aircraft Operated Over Water Operator Responsibility Agree - Operator Responsibility
135.183 (c) Performance Requirements: Multi Engine Land Aircraft Operated Over Water Compliant Aircraft compliant if limitations in AFM are not exceeded Complies 135.185 (a) Empty Weight and Center of Gravity: Currency Requirement Not applicable Aircraft weight report supplied at delivery. Subsequent weighing is operator’s responsibility Operator Responsibility 135.185 (b) Aircraft Original Airworthiness Certificate Compliant Aircraft weight report supplied at delivery. Subsequent weighing is operator’s responsibility Complies 135.227 (a),(b) (c),(e), (f) Icing Conditions: Operating Limitations Compliant Anti-ice system installed Complies 135.363 (f) AFM Performance Data Compliant Performance data supplied with AFM Complies 135.364 Maximum Flying Time Outside the U.S. Operator Responsibility Agree - Operator Responsibility 135.397 Small Transport Category Airplane Performance Operating Limitations Operator Responsibility Performance data supplied with AFM Agree - Operator Responsibility 135.398 (a) (b) (c) (d) Commuter Category Airplanes Performance Operating Limitations Operator Responsibility Performance data supplied with AFM Agree - Operator Responsibility
135 App. B Not applicable Not Applicable 135 App. D Not applicable Not Applicable 135 App. F Not applicable Not Applicable 135 App. G Not applicable Not Applicable APPENDIX 4 Pilot Training Course Outlines Differences Course Learjet 40/45 to Learjet 70/75 ( 2 Pilots = Complete Crew) Day Theoretical Training Hours Practical Training Training Hours 1 Classroom Instruction 4.0 IPT / FTD 2.0 / 2.0 1 Classroom Instruction 4.0 IPT / FTD 2.0 / 2.0