HONDA HA-420 Checklist

Verify Aft Baggage Door is closed and locked ☐ OK ☐ NG Verify Fuel Vent is clear ☐ OK ☐ NG Check Wheel, Tire and Strut condition (left and right strut should not be more that 1.5” different) ☐ OK ☐ NG Check Brake wear pins ☐ OK ☐ NG LEFT NACELLE Fan Air Outlet is clear ☐ OK ☐ NG Pylon NACA Scoop is clear ☐ OK ☐ NG Generator exhaust is clear ☐ OK ☐ NG Inboard Nacelle Access Door is closed ☐ OK ☐ NG Engine Exhaust is clear ☐ OK ☐ NG Engine drains are clear ☐ OK ☐ NG Oil Servicing Cap and Door secure ☐ OK ☐ NG Verify Anti-ice Exhaust Vent is clear ☐ OK ☐ NG LEFT WING Drain Wing Tank Aft Fuel Drain ☐ OK ☐ NG Check Aileron, Trim Tab and Flap condition ☐ OK ☐ NG Check static wicks are installed (3) ☐ OK ☐ NG Verify Anti-ice Exhaust Vent is clear ☐ OK ☐ NG Check winglet condition ☐ OK ☐ NG Check Wingtip Light Assembly ☐ OK ☐ NG Check Lower Surface Condition ☐ OK ☐ NG Check Wingtip Fence ☐ OK ☐ NG Check Wing Bump ☐ OK ☐ NG Check Upper Surface and Leading Edge condition ☐ OK ☐ NG Check Engine Inlet condition ☐ OK ☐ NG Check T1 probe condition ☐ OK ☐ NG Check Engine Duct and Fan condition ☐ OK ☐ NG Check stall strip condition ☐ OK ☐ NG Verify Anti-ice Exhaust Holes are clear ☐ OK ☐ NG Drain Wing Tank Fwd Fuel Drain ☐ OK ☐ NG Check Gear Door condition ☐ OK ☐ NG Check Wheel, Tire and Strut condition ☐ OK ☐ NG Check Ice Light ☐ OK ☐ NG Check External Power door ☐ OK ☐ NG Check Landing Light condition ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 5 CABIN DOOR Operate Verify: Pressurization door seal and cables Visual indicator flags Ease of operation ☐ OK ☐ NG EMERGENCY EXIT Operate Verify ease of operation (internal) ☐ OK ☐ NG Cockpit Seats and Restraints Operate Verify: Seat secured on track and stops Seatbelts Seat adjustments Latching Armrests ☐ OK ☐ NG CIRCUIT BREAKERS Visually Check Verify: All breakers marked clearly, set, not damaged Access door operation and fit ☐ OK ☐ NG PRIMARY FLIGHT CONTROLS Operate Verify: Smooth operation stop-to-stop Proper direction of travel Rudder pedals both sides, both positions Rudder pedal adjustment ☐ OK ☐ NG THRUST LEVERS Operate Verify while moving through full range: Smoot consistent operation Positive detent feel Cut-off triggers Set to CUT-OFF ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 6 COCKPIT KNOBS Operate Verify while moving through full range: Smooth consistent operation Positive detent feel Lubber line aligns with marking ☐ ☐ OK ☐ NG PLACARDS Verify installation of: AFM required placards ☐ Radio Call-sign placard ☐ OK ☐ NG BATTERY VOLTAGE BATTERY: ON Verify Voltage is ≥ 23.5 V and < 27.0 V ☐ OK ☐ NG EXTERNAL POWER VOLTAGE EXTERNAL POWER: CONNECTED Verify Voltage is > 27.0 V ☐ OK ☐ NG PILOT INITIATED TESTS Select: Preflight on CDU to initiate automatic tests Verify: FIRE indications / aural “Fire warning” Stall protection Shaker (Shakes 2x) Cockpit panel switch illumination Graphical Weight and Balance Basic Empty Weight set TOLD data matches current AFM data. ☐ OK ☐ NG PARKING/EMER BRAKE PARKING BRAKE: SET Verify: Handle operates and sets/releases easily Handle stows properly and brake pressure <100psi Proper indications ☐ OK ☐ NG FLAP HANDLE Operate Verify: Smooth operation Proper Indications ☐ OK ☐ NG ICE PROTECTION Operate knobs and switches TAIL DEICE: ON Verify smooth operation Verify aural Tail De-ice is heard ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 7 EXTERIOR LIGHTING Operate each exterior light from CDU  TAXI  LANDING  RECOGNITION (steady)  RECOGNITION (pulse)  ICE INSPECTION – left, right (if installed)  STROBES (ANTI-COLLISION)  LOGO (if installed)  BEACON (GROUND)  RECOGNITION  NAVIGATION ☐ OK ☐ NG PITCH TRIM PITCH MODE: NORM STBY PITCH TRIM: ON STBY PITCH TRIM: NORM Verify: Pilot/Copilot pitch trim (tab up for nose down trim) Pilot/Copilot AFCS/TRIM MASTER interrupts trim Travel full nose up / full nose down Verify: Normal pitch trim inoperative Half of STBY PITCH TRIM switch does not move trim Move STBY PITCH TRIM from full nose up to full nose down ☐ OK ☐ NG ROLL TRIM ROLL TRIM: NORM ROLL TRIM: OFF ROLL TRIM: NORM Verify: Pilot/Copilot roll trim (left tab up right tab down) for RWD trim Pilot/Copilot AFCS/TRIM MASTER interrupts trim Run roll trim full LWD and full RWD Verify roll TRIM Inoperative ☐ OK ☐ NG YAW TRIM YAW TRIM: NORM YAW TRIM: OFF YAW TRIM: NORM Operate yaw trim (tab right for nose-left trim) Pilot/Copilot AFCS/TRIM MASTER interrupts trim Run yaw trim full left and full right Verify YAW TRIM Inoperative ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 8 AUTOPILOT PRIMARY PITCH TRIM: STBY PRIMARY PITCH TRIM: NORM AP: ENGAGE AP: DISENGAGE USING THE FOLLOWING:  AFCS Controller AP  AP DISC/ACK (Pilot & Copilot)  Pitch Trim (Pilot & Copilot)  Roll Trim (Pilot & Copilot)  TO/GA (FD bars)  PITCH SERVO POWER  ROLL SERVO POWER  PITCH TRIM MODE STBY AFCS/TRIM MASTERS: PRESS AP: ENGAGE AFCS YAW SERVO POWER: OFF Verify AP will not engage Hold control column Verify green AP/YD indications Verify AP disengages and YD remains, AP disc tone sounds (cancelable) Verify AP/YD disengage, tone sounds & cancels Verify YD disengages ☐ OK ☐ NG DISPLAY REVERSION Pilot Reversion: REV Copilot Reversion: REV REVERSION: OFF (DARK) Verify pilot PFD/MFD transition Verify copilot PFD transitions Both SI’s dark, normal format ☐ OK ☐ NG BARO/ALTITUDE BARO: SET PILOT BARO: CHANGE ≥ 200 ft. Verify match ±100ft Verify amber altitude preselect and altitude alerter sounds ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 9 PREFLIGHT STATUS STATUS PAGE: DISPLAY EXTERNAL DOORS: OPEN/CLOSE  Forward Baggage Door  Electrical service doors (left and right)  Aft baggage door  Main entry door  Emergency exit door  External power door Verify: Solid State Relays NORMAL Fire bottle indications NORMAL Engine Oil Quantity NORMAL Verify proper indications (STATUS page / CAS message) ☐ OK ☐ NG FLUID QUANTITIES STATUS PAGE: DISPLAY FUEL SYNOPTIC PAGE: DISPLAY Verify HYD QTY 75%-100% Verify FUEL QTY ☐ OK ☐ NG Temp°C Fuel(lbs) FUEL FUEL SYNOPTIC PAGE: DISPLAY L(R)FUEL PUMP: ON L(R)FUEL PUMP: OFF FUEL CROSSFEED: L AND R FUEL CROSSFEED: NORM Verify proper operation Verify proper operation ☐ OK ☐ NG FIREWALL SHUTOFF ENGINE FIRE SWITCHES: PUSH ENGINE FIRE SWITCHES: RESET (Caution: Do not push FIRE EXT PUSH) Verify: FIRE EXT PUSH switch illuminates FUEL SOV CLOSED CAS posts Verify: FUEL SOV CLOSED CAS clears ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 10 COCKPIT LIGHTING Check the following:  All instruments, controls, and panels adequately illuminated  Text legible with uniform color and balance  Verify no light bleeds on illuminated panels  Balance displays backlight levels  Cycle Master / Individual Panel dimmers through full range  Day / Night switch  MAP light and Dome Light  FOOTWELL, NO SMOKING, FASTEN SEATBEALTS ☐ OK ☐ NG ENGINE STARTS/GROUND CHECKS RIGHT ENGINE START EXTERNAL POWER: CONNECT ELECTRICAL PAGE: DISPLAY RH ENGINE: START PER AFM Verify bus voltage is >27 volts Verify proper power distribution ☐ OK ☐ NG Peak ITT (≦556℃) ℃ LEFT ENGINE START LH ENGINE: START PER AFM EXTERNAL POWER: DISCONNECT Verify proper power distribution ☐ OK ☐ NG Peak ITT (≦556℃) ℃ HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 11 PNEUMATIC AND ENVIROMENTAL SYSTEMS ENVIROMENTAL PAGE: DISPLAY INFLOWS: OFF 1 AT A TIME INFLOWS: ON BLEEDS: OFF 1 AT A TIME BLEEDS: ON COCKPIT/CABIN TEMP MODE: NORMAL COCKPIT/CABIN TEMP: MAX COCKPIT/CABIN TEMP: MIN COCKPIT/CABIN TEMP MODE: MANUAL COCKPIT/CABIN DUCT TEMP MODE: WARMER COCKPIT/CABIN DUCT TEMP MODE: COOLER COCKPIT/CABIN TEMP MODE: NORMAL COCKPIT CABIN FAN: MANUAL COCKPIT CABIN FAN: NORMAL Verify proper valve movement Verify proper valve movement Verify duct temperature increases Verify duct temperature decreases Verify duct temperature increases Verify duct temperature decreases Cycle through each fan speed in the cockpit and the cabin. ☐ OK ☐ NG ELECTRICAL SYSTEM ELECTRICAL PAGE: DISPLAY Verify data displayed is green ☐ OK ☐ NG FUEL SYSTEM FUEL PAGE: DISPLAY Verify correct fuel used ☐ OK ☐ NG HYDRAULIC SYSTEM HYDRAULIC PAGE: DISPLAY Verify no amber or red indications. (no CAS) ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 12 ICE PROTECTION WING A/I: ON ENGINE A/I: ON WING FLOW: NORM TAIL DE-ICE: ON WING FLOW: L THEN R WING FLOW: NORM WINDSHIELD HEAT: OFF WINDSHIELD HEAT: NORM Verify valve movement on ICE synoptic page, proper operation and indications. Verify proper valve movement. Verify zones white when OFF and CAS message. In NORM, green and no CAS ☐ OK ☐ NG ALTIMETRY LOCAL ALTIMETER SETTING: SET Verify altitudes ±50 ft of known altitude and each other ☐ OK ☐ NG LH ftΔ RH ftΔ STBY ftΔ ENGINE CHARACTERISTICS THRUST LEVERS: IDLE L(R)THRUST LEVER: 30 SECONDS TO TAKEOFF THRUST L(R) THRUST LEVER: 30 SECONDS TO IDLE L(R) THRUST LEVER: SLAM TO T.O. L(R) THRUST LEVER: SLAM TO IDLE Repeat for other thrust lever Verify Fuel Pressure ≥ 3 PSIG Stabilize 3 minutes Verify Fuel Pressure ≥ 9 PSIG @T.O. Verify no abnormal indications ☐ OK ☐ NG ☐ OK ☐ NG TAKEOFF CONFIG WARNING PARKBRAKE: RELEASE Select item below outside allowable takeoff setting, sequentially:  Pitch trim outside green band, cyan CAS  Flaps LDG, cyan CAS  Speedbrake EXT (if installed), cyan CAS THRUST LEVERS: ADVANCE TO T.O. ONE AT A TIME PARKBRAKE: SET Verify NO TAKEOFF CONFIG CAS and aural alert. ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 13 FLIGHT CONTROLS FLIGHT CONTROL CHECK SPEEDBRAKE: EXTEND LR THRUST LEVER: T.O. ONE AT A TIME Elevator, aileron, and rudder move smoothly through full range Cycle flaps, proper indications, set for takeoff Verify proper indications and speedbrake retracts a 80% N1 ☐ OK ☐ NG TAXI PARK BRAKE: RELEASE TAXI Verify: Taxi light “ON” when Parking Brake released Aircraft tracks straight NWS operation Normal brakes both sides Emergency brakes ☐ OK ☐ NG TAKEOFF AND CLIMB CHECKS COMPASS CHECK Position aircraft to T/O RWY Heading or any equivalent Verify heading ±4 deg. of known heading and each other ☐ OK ☐ NG LH °Δ RH °Δ STBY °Δ TAKEOFF CONDUCT A TAKEOFF PER THE AFM (All parameter must be Normal) Verify strobe and landing lights come ON and Pre-pressurization bump does not exceed 1100 fpm ☐ OK ☐ NG fpm INITIAL CLIMB Verify cabin rate is no more than +500 fpm or less than -300 fpm, landing gear retracts, YD engages automatically, landing gear de-clutters from the ASI after 30 seconds, landing lights extinguish and recognition lights illuminate ☐ OK ☐ NG FLIGHT DISPLAYS Observe Verify: Pilot, Copilot and STBY airspeed agree within 2 KIAS Pilot, Copilot and STBY altimeters agree within 50 ft Pilot, Copilot and STBY headings agree within 2 degrees ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 14 TRIM AND RIGGING AIRSPEED: 220 YD: OFF WING FUEL: BALANCED Verify: Yokes are within 2 degrees of level Roll and Yaw trim indications would be within the green band (the green band is only shown on the ASI on the ground) ☐ OK ☐ NG 270KT VIB. AND BUFFETT AIRSPEED: 270 KIAS Verify: No buffet, excessive vibration, or unusual sounds up to VMO ☐ OK ☐ NG 250KT SPEEDBRAKE AIRSPEED: 250 KIAS AP/YD: OFF THRUST LEVERS: BELOW AUTO RETRACT SPEED SPEED BRAKE: EXTEND CONTROL WHEEL: RELEASE AIRSPEED: DECELERATE TO 200 KIAS Verify: Bank angle is less than 10 degrees after 5 seconds No objectionable yaw Proper ASI indications (you may retake a hold of the control wheel) ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 15 200KT SPEEDBRAKE AIRSPEED: 200 KIAS CONTROL WHEEL: RELEASE SPEEDBRAKE: RETRACT Verify: Bank angle is less than 10 degrees after 5 seconds No objectionable yaw Proper ASI indications ☐ OK ☐ NG 195KT FLAP ROLL AP/YD: OFF FLAPS: TO/APP AIRSPEED: 195 KIAS CONTROL WHEEL: RELEASE Verify bank angle is less than 10 degrees after 5 seconds and proper indications on the ASI ☐ OK ☐ NG 155KT FLAP ROLL AP/YD: OFF FLAPS: LANDING AIRSPEED: 155 KIAS CONTROL WHEEL: RELEASE FLAPS: UP Verify bank angle is less than 10 degrees after 5 seconds and proper indications on the ASI ☐ OK ☐ NG UNDERSPEED PROTECTION (If installed) AP/YD or FD: ENGAGED AIRCRAFT: DECELERATE Verify aural airspeed alert, amber MIN SPD alert on top of airspeed tape, a pitch limit indication (feathers), aircraft pitches down and wings level, vertical and lateral modes are white on FMA ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 16 STALL WARNING ADC: BOTH ON 1(2) AC WEIGHT: 8,800-9,800 LBS FUEL IMBALANCE <100 LBS ALTITUDE: 12,000 TO 17,500 FLAPS: UP GEAR: UP YD: ON ESP: OFF TRIM SPEED: 130 KIAS THRUST LEVERS: IDLE AND DECELERATE AT 1 KT/SEC REPEAT WITH: FLAPS: TO/APPR GEAR: UP FLAPS: DN GEAR : DN An amber STALL PUSHER FAIL CAS message will post when both on the same ADC Recover at stick shaker activation. Verify stick shaker values are within 2 knots of each other and within the allowable values in the table ☐ OK ☐ NG WT(lbs) Shaker (KIAS) ADC1 KIAS ADC2 KIAS ADC1 KIAS ADC2 KIAS ADC1 KIAS ADC2 KIAS Stick Shaker Onset Speed (KIAS) Wt (lbs) UP / UP TO/APPR / UP LDG / DN 8800 103-107 94-98 91-95 9000 104-108 95-99 92-96 9200 105-109 96-100 93-97 9400 107-111 97-101 94-98 9600 108-112 98-102 95-99 9800 109-113 100-104 96-100 HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 17 CRUISE CHECKS ALTITUDE: 12,000 TO 17,500 WING AI: NORM TAIL AI: NORM ENGINE AI: OFF BLEEDS: NORM Verify: P/CP KIAS within 2 knots P/CP Mach within 0.005 M P/CP SAT within 1 degree C P/CP ISA within 1 degree C L/R ITT <810 degrees C L/R ITT within 20 degrees N2 within 1.5% P/L CP/R KIAS Mach SAT ISA ITT N2 No amber or red on synoptic pages ☐ OK ☐ NG WING ANTI ICE WING A/I: ON ENGINE A/I: ON WING FLOW: NORM TAIL DE-ICE: ON WING FLOW: L THEN R WING FLOW: NORM WINDSHIELD HEAT: OFF WINDSHIELD HEAT: NORM STALL WARING ICE ADVANCE: RESET Verify valve movement on ICE synoptic page, proper operation and indications. Verify proper valve movement. Verify zones white when OFF and CAS message. In NORM, green and no CAS. ☐ OK ☐ NG COMMUNICATION Verify that all VHF communications systems work in the air ☐ OK ☐ NG ADS-B IN TRAFFIC PAGE: DISPLAY Verify: ADS-B targets display and can be interrogated ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 18 PRESSURIZATION PRESSURIZATION CONTROL MODE: HOLD PRESSURIZATION CONTROL MODE: NORM Climb to 15,000 – 16,500 ft ENGINE BLEED: OFF (one at a time) ENGINE BLEED: NORM OXYGEN MASKS: DON CABIN DUMP: DUMP CABIN INFLOWS: OFF CABIN DUMP: NORM CABIN INFLOWS: NORM CABIN INFLOWS: OFF CABIN INFLOWS: NORM OXGEN MASKS: STOW Verify after 2000 ft of climb that the cabin altitude remains constant Verify cabin remains pressurized Verify: DUMP is displayed on MFD Cabin climbs to 13,500 ± 500 ft Verify: Oxygen masks drop 14,500 ± 500 ft CABIN OXYGEN ON CAS posts Descent cabin below 10,000ft Verify: CABIN ALT HIGH CAS posts 10,000 ft -0/+500 ft CABIN ALTITUDE aural interval is approximately 30 sec Verify: CABIN ALT HIGH CAS clears when cabin altitude is <10,000 ft ☐ OK ☐ NG ft ft ft ft HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 19 APPROACH AND LANDING APPROACH REFERENCE CUE LANDING GEAR: DN FLAPS: LDG AIRSPEED: VREF Verify approach reference cue matches Vref ±3 knots ☐ OK ☐ NG LANDING GEAR WARNING LANDING GEAR: UP FLAPS: LDG Verify LANDING GEAR aural activates and cannot be cancelled ☐ OK ☐ NG BARO MINIMUMS BARO MINS: ENTER Verify MINMUMS aural sounds at DA ☐ OK ☐ NG PRESSURIZATION During Landing Verify no objectionable pressure bump on landing ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 20 HIGH ALTITUDE CHECKS (> 18,000 FT) AVIONICS OPTIONS Flight Charts Jepp View Synthetic vision Cockpit Iridium Enhanced Checklists IFR/VFR Charts Flight Stream 510 XM radio Verify installed options function properly ☐ OK ☐ NG CABIN OXYGEN SYSTEM ALTITUDE: FL350-FL430 CABIN OXYGEN: DROP MASKS CABIN OXYGEN: OFF Verify: Masks drop Cyan CABIN OXYGEN ON CAS posts ☐ OK ☐ NG ENGINE HANDLING ALTITUDE: FL410-FL430 THRUST LEVERS: MCT AI: NORM OR OFF ENGINE BLEEDS: NORM L(R) THRUST LEVER: RETARD RAPIDLY TO IDLE L(R): THURST LEVER @92% N1 SELECT MCT RAPIDLY Repeat for other engine Verify: No compressor stalls or abnormal engine indications. ☐ OK ☐ NG ☐ OK ☐ NG PRESSURIZATION ALTITUDE: FL410-FL430 L(R) ENGINE BLEED: OFF Repeat for other bleed Verify: Cabin altitude is <8100 ft Cabin delta P is between 8.4 and 8.9 Verify: Cabin altitude and delta P still fall within the parameters listed above ☐ OK ☐ NG ft psi ☐ OK ☐ NG ft psi ALTIMETERS ALTITUDE: FL410-FL430 AIRSPEED: ≥0.55M Verify: P/CP altitude is ±100 ft Standby altitude is ±175 ft ☐ OK ☐ NG ft ft ft HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 21 MMO DESCENT AIRSPEED: MMO Verify aircraft is free from buffet, excessive vibration, unusual sounds and excessive air noise ☐ OK ☐ NG SPEED BRAKE (IF INSTALLED) AIRSPEED: MMO AP: OFF YD: ON THRUST LEVERS: BELOW AUTO RETRACT SPEED SPEED BRAKE: EXTEND CONTROL WHEEL: RELEASE SPEEDBRAKE: RETRACT Verify: Bank angle is less than 10 degrees after 5 seconds No objectionable yaw Proper ASI indications ☐ OK ☐ NG TRIM AND RIGGING ALTITUDE: FL330-FL350 AIRSPEED: MH (<MMO) AP: OFF YD: ON WING FUEL: BALANCED Verify: Yokes are within 2 degrees of level Roll and Yaw trim indications should be within the green band (the green band is only shown on the ASI on the ground) ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 22 ENGINE HANDLING ALTITUDE: FL330-FL350 THRUST LEVERS: MCT AI: NORM OR OFF ENGINE BLEEDS: NORM L(R) THRUST LEVER: RETARD RAPIDLY TO IDLE L(R) THURST LEVER @92% N1 SELECT MCT RAPIDLY Repeat for other engine Verify: No compressor stalls or abnormal engine indications. ☐ OK ☐ NG ☐ OK ☐ NG ENGINE SYNC THRUST LEVERS: MCT THRUST LEVERS: RETARD Verify: SYNC posts on ASI when thrust is < MCT and N1’s match ±0.2% ☐ OK ☐ NG HA-420 ELITE JCAB Flight Test Procedures Rev 3 ACTION CHECK POINT RESULT HA-420 ELITE Flight Test Procedure Rev 3 12/21/2020 23 EMI Throughout flight verify no EMI/RFI noted during aircraft operations ☐ OK ☐ NG