Garmin C90A/GT- Manuals

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 7 of 95 Section 1 - General The information in this supplement is FAA-approved material and must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual (POH/AFM) when the airplane has been modified by i...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 8 of 95 North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace per AC 91-49 and AC 120-33. Both GPS/SBAS receivers are required to be operating and receiving usable signals except for routes requiring on...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air FAA APPROVED Page 9 of 95 Section 2 - Limitations INTRODUCTION The G1000 Cockpit Reference Guide for Hawker Beechcraft C90A/GT (CRG) must be immediately available to the flight crew. Use the G1000 Cockpit Reference Guide for Hawker Beechc...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 10 of 95 FAA APPROVED GIA1 SERVICE GMA1 SERVICE GIA2 SERVICE GMA2 SERVICE MFD SERVICE GEO LIMITS Do not take off if MFD FAN FAIL is displayed in the ALERTS window AND the Outside Air Temperature is greater than 33 O C (91 O F). Do no...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air FAA APPROVED Page 11 of 95 crew must ensure that the planned approach is in the database. RNP operations are not authorized except as noted in the Operational Approvals section. When an approach being flown requires a course reversal and ...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 12 of 95 FAA APPROVED AHRS AREAS OF OPERATION Flight operations with the G1000 Integrated Avionics installed are prohibited north of 70° North latitude or south of 70° South Latitude due to unsuitability of the magnetic fields near t...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 14 of 95 FAA APPROVED PLACARDS On some aircraft, placards “On Instrument Panel Adjacent to Each Gyroscopic Instrument (Except for Flight Director)” were installed to identify the power source for the instrument (ref. AFM limitations ...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 18 of 95 FAA APPROVED This page intentionally left blank.

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 19 of 95 Section 3 - Emergency Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 20 AUTOPILOT MALFUNCTION / ELEVATOR TRIM RUNAWAY ..............................

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 20 of 95 Bolded checklist steps in the EMERGENCY PROCEDURES section indicate pilot memory action items. The pilot shall perform these items without reference to the checklist in this section. AUTOMATIC FLIGHT CONTROL SYSTEM AUTOPILOT...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 21 of 95 MANUAL AUTOPILOT DISCONNECT If necessary, the autopilot can be manually disconnected using any one of the following methods. 1. AP/YD DISC / TRIM INTRPT Button ............................................................ PRE...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 22 of 95 ROLL AXIS FAILURE (Red annunciator on PFD) • Indicates a failure of the roll axis of the autopilot. The autopilot will be inoperative. YAW AXIS FAILURE (Red annunciator on PFD) • Indicates a failure of the yaw axis of the au...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 23 of 95 AUTOPILOT OVERSPEED RECOVERY (Yellow MAXSPD on PFD) 1. Throttle ............................................................................................................................... REDUCE When overspeed condition ...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 24 of 95 If Neither Generator Will Reset: 7. Avoid IFR conditions if possible and LAND AT THE NEAREST SUITABLE AIRPORT. 8. Standby Battery Switch ............................................................................... INDICAT...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 25 of 95 TAWS TAWS WARNING (Red on PFD and aural “PULL UP”) 1. AP/YD DISC / TRIM INTRPT Button ............................................. PRESS and RELEASE (To disconnect the autopilot) 2. Aircraft Attitude ..........................

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 27 of 95 Section 3A - Abnormal Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 29 AILERON MISTRIM ............................................................

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 29 of 95 AUTOMATIC FLIGHT CONTROL SYSTEM AILERON MISTRIM (amber or annunciation on PFD) Indicates a mistrim of the ailerons while the autopilot is engaged. The autopilot cannot trim the airplane in roll. During large changes in airsp...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 30 of 95 IF STILL INOPERATIVE • Pitch Trim ............................................................. MANUALLY TRIM AIRPLANE IN PITCH (Using Elevator Tab Wheel) NOTE Autopilot and yaw damper may also be inoperative. IF OPERATIVE •...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 31 of 95 RUDDER MISTRIM (amber or annunciation on PFD) Indicates a mistrim of the rudder while the autopilot is engaged. During large changes in airspeed, engine failure, or single engine operation, illumination of this message may o...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 32 of 95 FLASHING AMBER MODE ANNUNCIATION NOTE Abnormal mode transitions (those not initiated by the pilot or by normal sequencing of the AFCS) will be annunciated by flashing the disengaged mode in amber on the PFD. Upon loss of a s...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 33 of 95 G1000 INTEGRATED AVIONICS SYSTEM ALTITUDE MISCOMPARE This message is displayed when the G1000 detects a difference of 200 feet or greater between the pilot’s and copilot’s altitude information. Refer to the G1000 Cockpit Ref...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 34 of 95 NOTE When comparing indicated altitude to GPS altitude, deviations from standard temperature or pressure can cause indicated altitude to deviate from GPS altitude. These errors are largest at high altitude. Below 10,000 feet...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 35 of 95 AIRSPEED MISCOMPARE This message is displayed when the G1000 detects a difference of 7 KIAS or greater between the pilot’s and copilot’s airspeed indicators (10 KIAS difference during takeoff or landing roll). Refer to the G...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 36 of 95 Reference Guide for additional information. 1. Refer to STANDBY ATTITUDE indicator to determine which AHRS is providing the most accurate data. 2. Use SENSOR softkey to select the most accurate AHRS on the affected PFD. ROLL...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 37 of 95 side PFD and the standby flight instruments for information to fly the airplane. If only individual elements of the display are failed, refer to appropriate procedures for the individual failures. To display a composite disp...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 39 of 95 • The airplane symbol is removed from all maps. The map will remain centered at the last known position. “NO GPS POSITION” will be annunciated in the center of the map. GPS APPROACH ALARM LIMITS EXCEEDED During a GPS LPV, LN...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 40 of 95 FAILED AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED (RED "X" ON PFD AIRSPEED, ALTITUDE, AND/OR VERTICAL SPEED INDICATORS) This indicates a loss of valid air data computer information to the respective system. ¾ IF BOTH ...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 42 of 95 ENGINE INDICATION SYSTEM (EIS) FAILURE (RED 'X' ON ENGINE DISPLAY) ¾ IF ALL ENGINE GAUGES ON ONE ENGINE RED ‘X’: Indicates failure of the GEA for that engine 1. Check ENG INST circuit breaker ...................................

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 43 of 95 BOTH ON ADC1, BOTH ON ADC2 This message is displayed on both PFDs and indicates that both pilot and copilot PFDs are displaying data from the same Air Data Computer. Normally the pilot’s side displays ADC 1 information and t...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 44 of 95 XSIDE ADC This message is displayed on both PFDs and indicates that both PFDs are displaying data from the opposite side Air Data Computer. Normally the pilot’s side displays ADC 1 and the copilot’s side displays ADC 2. Refe...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 45 of 95 TAWS ABNORMAL PROCEDURES TAWS CAUTION When a TAWS CAUTION occurs, take positive corrective action until the alert ceases. Stop descending or initiate either a climb or a turn, or both, as necessary, based on analysis of all ...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 47 of 95 Section 4 - Normal Procedures Table of Contents COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES........................... 49 BEFORE STARTING ....................................................................................

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 52 of 95 • Pilot’s Trim Override.................................................................................................... CHECK Activate the copilot’s Pitch Trim Switches nose down. Verify elevator tab wheel is moving nose...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 53 of 95 AUTOPILOT OPERATION Autopilot/Flight Director mode annunciations on the PFDs displayed in green indicate active autopilot/flight director modes. Annunciations displayed in white indicate armed autopilot/flight director modes...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 54 of 95 Altitude Hold (ALT) Mode, Manual Capture: 1. At the desired altitude ................................................... PRESS ALT Button on Mode Controller 2. Green ‘ALT’........................................................

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 55 of 95 Vertical DIRECT TO To descend from the present position to a waypoint: 1. Altitude Preselect............................................................................................................. RESET 2. VNV Button .....

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 57 of 95 ILS 1. Load the approach into the Active Flight Plan .................................... VERIFY the G1000 tunes the proper ILS frequency 2. Approach Minimums ....................................................................

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 62 of 95 7. Level airplane in ALT mode at MDA.............................. PRESS NAV button 200 ft above MDA If airplane is descending via GP, GP will extinguish and PIT mode will be active and airplane will capture MDA. 8. AFTER LE...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 65 of 95 GO AROUND (GA) 1. Control Wheel ................................................................................................... GRASP FIRMLY 2. GO AROUND button (left throttle) .......................................... ...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 67 of 95 Section 5 - Performance No Change. Refer to basic Aircraft Flight Manual or appropriate supplement. Section 6 - Weight and Balance No Change. Refer to basic Aircraft Flight Manual or appropriate supplement

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 69 of 95 Section 7 - Systems Description Table of contents GENERAL..................................................................................................................... 70 G1000 INTEGRATED AVIONICS .......................

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 70 of 95 GENERAL This section supplements the Systems Description chapter in the airplanes original Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. This section will follow the format and layout of the chapter in ...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 71 of 95 Figure 1, Instrument Panel

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 73 of 95 Figure 3, Copilot's Control Wheel With Trim Switches

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 74 of 95 Figure 4, Copilot's Control Wheel Without Trim Switches

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 75 of 95 Figure 5, Overhead Light Control Panel

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 76 of 95 Figure 6, Left Side Circuit Breaker Panel

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 80 of 95 Figure 10, GFC 700 System Interface

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 81 of 95 FLIGHT CONTROLS AFCS, AUTOPILOT AND FLIGHT DIRECTOR The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G1000 System avionics architecture. The GFC 700 is a three axis autopilot and f...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 83 of 95 AFCS LATERAL MODES Lateral Mode Control Annunciation Maximum Roll Command Limit Roll Mode (default) ROL 25 O Left Bank 25 O Right Bank Low Bank BANK Key * 15 O Left Bank 15 O Right Bank Heading Select HDG Key HDG 25 O Left B...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 84 of 95 ELECTRIC ELEVATOR TRIM The electric elevator trim is standard with the G1000 system installation. The electric elevator trim can be operated manually by the pilot using the pitch trim switches on the control wheel, or, autom...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 85 of 95 FLIGHT INSTRUMENTS G1000 FLIGHT INSTRUMENTS The flight instruments are an integrated part of the G1000 system. For system descriptions, operating instructions, and abnormal failure indication refer to the Cockpit Reference G...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 86 of 95 ENGINE INSTRUMENTATION Engine instruments, located in a window on the left side of the MFD, are grouped according to their function. The G1000 engine gauges are constructed and arranged to emulate the mechanical gauges they ...

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C Page 92 of 95 During normal operations, the standby battery is kept in a fully charged state by its own trickle charger powered from the triple-fed bus through the STBY AUX BAT circuit breaker located on the right side circuit breaker pan...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 93 of 95 STATIC The normal static system has two separate sources of static air, one source is connected to the pilot ’ s Air Data Computer (ADC1), and the other source is connected to the copilot ’ s Air Data Computer (ADC2) and the...

190-00682-02 Rev. C Hawker Beechcraft C90A and C90GT King Air Page 95 of 95 Section 8 – Handling, Service, and Maintenance Refer to Garmin G1000 Instructions For Continued Airworthiness, P/N 190-00682-01 Rev. A or later FAA approved revision for maintenance requirements for the G1000 system and comp...