CJ3 to CJ2+ Differences

Aircraft General Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Aircraft General - Dimensions Difference Wing – 3.75” shorter Wheel Base – 0.87” narrower Tail – 0.69” shorter 20.78’ (6.33M) 20.09’ (6.32M) Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 15.98’ (4.87M) 15.11’ (4.85M) 52.85’ (16.11M) 49.10’ (15.19M) CJ3 CJ2+ Systems

Aircraft General - Dimensions Difference Length – 4.06” shorter Height – 1.14” shorter 15.14’ (4.61M) 14.00’ (4.27M) Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 51.14’ (15.59M) 47.08’ (14.53M) CJ3 CJ2+ Systems

Aircraft General – Turning Radius Difference Wing Tip to Tip – 2.49” shorter Curb-to-Curb – 0.88” wider 69.2’ (21.1M) 32.0’ (9.8M) 66.71’ (20.33M) 32.88’ (10.49M) Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: CJ3 CJ2+ Systems

Aircraft General – Cabin 58” (1.45M) 58” (1.45M) Difference Length – 2.08’ shorter Height – same Width – same 57” (1.45M) 57” (1.45M) 15.66’ (4.77M) 13.58’ (4.15M) Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: Standard configuration CJ3 – 4 club seats with 2 forward facing aft seats - Option for additional seat behind copilot CJ4 – 4 club seats with 2 forward facing aft seats & a 7th seat across from entry door CJ3 CJ2+ Systems

Aircraft General – Limitations Weights 14,070 LBS MAX Ramp 12,625 LBS 13,870 LBS MAX Takeoff 12,500 LBS 12,750 LBS MAX Landing 11,525 LBS 10,510 LBS MAX Zero Fuel 9,700 LBS Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 400 Nose 600 Tail 400 Nose 600 Tail Baggage CJ3 CJ2+ Systems

Aircraft General – Limitations Speeds .737 Mach (Above 29,300’) .737 Mach (Above 29,123’) MMO 278 KIAS (8,000’ – 29,300’) 278 KIAS (8,000’ – 29,123’) VMO 260 KIAS (Below 8,000’) 260 KIAS (Below 8,000’) VMO 278 KIAS or .737 Mach 278 KIAS or .737 Mach Autopilot Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 180 KIAS Flight In Icing 160 KIAS CJ3 CJ2+ Systems

Aircraft General – Limitations Speeds 200 KIAS VFE (15°) 200 KIAS 161 KIAS VFE (35°) 161 KIAS 140 KIAS (55°) Ground Flaps 140 KIAS (60°) 200 KIAS VLE / VLO 200 KIAS Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 165 KIAS Tire Ground Speed 165 KIAS CJ3 CJ2+ Systems

Master Warning System Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Master Warning System– Annunciator Panel No BAGGAGE SMOKE No NO TAKEOFF Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: CABIN DOOR CJ3 – Triggered by 4 pins equipped with microswitches CJ4 – Triggered by any of the 8 pins BAGGAGE DOOR FWD - NOSE DOOR L/R CJ3 – Triggered by key lock CJ4 – Triggered by pin latch and paddle latches (any trigger message) BAGGAGE DOOR AFT – AFT BAGGAGE DOOR Same – Triggered by door lock microswitch EMERGENCY EXIT Same – Triggered by proximity switch on locking bracket CJ3 CJ2+ Systems

Master Warning System– Annunciator Panel No STBY P/S HTR OFF No WING O’HEAT Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: CABIN DOOR CJ3 – Triggered by 4 pins equipped with microswitches CJ4 – Triggered by any of the 8 pins BAGGAGE DOOR FWD - NOSE DOOR L/R CJ3 – Triggered by key lock CJ4 – Triggered by pin latch and paddle latches (any trigger message) BAGGAGE DOOR AFT – AFT BAGGAGE DOOR Same – Triggered by door lock microswitch EMERGENCY EXIT Same – Triggered by proximity switch on locking bracket CJ3 CJ2+ Systems

Avionics Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Avionics – Limitations Autopilot 350’ AGL MIN Engage Height 240’ AGL 180’ AGL MIN Use – Prec. 70’ AGL 350’ AGL MIN Use – Non-Prec. 240’ AGL Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting 1000’ AGL Instructor Information: Additional Limitations Same Operating in the composite mode is limited to training and display failure conditions. Category II approaches are not approved. VOR approaches must not be conducted in the NAV mode of the flight director. Use the APPR mode, or manually track the approach course using the HDG mode. This limit applies to both flight director only and autopilot coupled operation. Autopilot coupled operation is prohibited during any portion of a VOR approach in which the VOR is located behind the airplane by more than 15 miles, unless the HDG mode of the flight director is being used to manually track the approach course. It is prohibited to display the non-coupled side Flight Director unless the coupled side Flight Director is being displayed. Failure to adhere to this limit will result in incorrect Flight Director guidance. Use of the coupled side Flight Director by itself will operate correctly. CJ3 The pilot’s PFD, copilot’s PFD and MFD must be installed and operational in the normal mode for takeoff. The FCS-3000 system must be verified to be operational by a satisfactory automatic preflight test (no messages on power up) prior to each flight in which the autopilot is to be used. CJ4 Taxiing the airplane is prohibited until all AHRS ground alignment is completed. Do not override the autopilot in pitch during normal operation. Use of the autopilot is prohibited if primary elevator trim is inoperative. VOR approaches conducted without DME must be intercepted greater than 6 nautical miles from the VOR. When conducting an approach that utilizes a localizer (ILS, LOC, LOC-BC, LDA, SDF), the approach mode (APPR) must not be selected until the course deviation indicator (CDI) has clearly moved away from a full scale deflection and the aircraft is within the published service volume for the approach. Failure to observe this limit may result in capture of a false localizer lobe, resulting in incorrect lateral guidance. MIN Use - Cruise 1000’ AGL CJ3 CJ2+ Systems

Electrical Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

No Interior Master Switch* Electrical – Controls Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: Similar locations and functions No Interior Master Switch* (possible upgrade) CJ3 CJ2+ Systems

Fuel Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Fuel - Refueling Capacity: 4710 lbs. Capacity: 3960 lbs. Fuel Low Level 190 +/- 20 lbs Fuel Low Level 220 +/- 40 lbs Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: The CJ4 SPR system utilizes a single adapter to pressure refuel and defuel the left and right wing fuel tanks. An SPR access panel, just forward of the right wing on the fairing below the fuselage, provides access to the refuel/defuel adapter. Prior to refueling, a test of the automatic high level shutoff system must be performed using a precheck system. Perform the precheck procedure by: Raising (opening) the precheck lever of the wing(s) to be refueled. Provide refuel pressure (10-55 psi) to the system to precheck the auto-shutoff function. The fuel flow should stop. Place the lever back down (closed) and allow the wing(s) to refuel watching for evidence of any overboard spillage at the wing tank vent scoop or wing pressure tank relief valve. Shut down refuel flow after automatic shutdown or upon evidence of overboard spillage. CJ3 CJ2+ Systems

Powerplant Aircraft General Warnings Avionics Electrical Fuel Pneumatics Ice & Rain Lighting Systems

Powerplant FJ44-3A FJ44-3A-24 2,780 lbs 2416 lbs CJ3 CJ2+ Type Thrust Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: 2,780 lbs Thrust 2416 lbs CJ3 CJ2+ Systems

Pneumatics Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Pneumatics – Crew Alerting System Automatic Emergency Press On when cabin above 14,500’ +/- 400’ Must manually select EMER Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: PRESS SOURCE NOT NORM (amber) Indicates the PRESSURIZATION SOURCE Selector is not in the NORM position and the airplane is on the ground. PRESS SOURCE NOT NORM (cyan) Indicates the PRESSURIZATION SOURCE selector is out of the NORM position and the airplane is in the air. Supplemental Pressurization is only available in the NORM and L positions. PYLON BLEED LEAK L-R Indicates bleed air sensors have detected a leak around the environmental air supply or wing anti-ice air supply systems in the pylons. The associated environmental system control module will automatically close both valves on the affected side. If both L and R messages are displayed, complete the procedure for the L message first, and then repeat the procedure for the R message. TAILCONE BLEED LEAK L-R Indicates high air temperature in tailcone. WING BLEED LEAK L-R Indicates high temperature air near the wing anti-ice air supply lines in the tailcone or wing fairing. Both wing anti-ice valves close automatically. BLEED AIR MONITOR FAIL L-R Indicates loss of bleed air temperature monitoring capability. All bleed air systems (ECS and Anti-Ice) continue to function. Undertemperature or overtemperature conditions for the bleed air systems (ECS and Anti-Ice) and tail deice system failures on the affected side will not be displayed. Failure of both sides will result in loss of cabin altitude indications, however CABIN ALTITUDE warning will still function normally. CJ3 CJ2+ Systems

Ice & Rain Protection Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Ice & Rain - Limitations Min N2 required 80% N2 Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: CJ3 CJ2+ Systems

Lighting Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Systems

Lighting – Controls CJ3 CJ2+ Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Instructor Information: CJ3 – Lighting is located on the pilot lower instrument panel CJ4 – All lighting (except Emer lights) are located below the CDUs on the center pedastal CJ3 CJ2+ Systems

Lighting – Emergency Lights No Emergency Lighting Switch 5-G switch Loss of Main DC Power PASS SAFETY switch ON Door ENTRY LIGHT switch ON 5-G inertia switch PASS SAFETY switch ON Door ENTRY LIGHT switch ON Activation in ARMED Aircraft General Warnings Avionics Electrical Fuel Powerplant Pneumatics Ice & Rain Lighting Emergency Exit Signs Fwd Entry Light Fwd/Aft No-Smoking Signs Left Aisle Lights Escape Hatch/Two Wing Lights Instructor Information: EMERGENCY LIGHTS NOT ARMED Indicates the emergency lights are not in the armed position. This message may appear momentarily if an engine is restarted in flight. Emergency Exit Signs Fwd Entry Light Fwd/Aft No-Smoking Signs Left Aisle Lights Escape Hatch/Two Wing Lights Emergency Lights CJ3 CJ2+ Systems