Garmin SA01456Wi_D- Manuals

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 6 of 124 FAA APPROVED This page intentionally left blank.

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 7 of 124 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 ...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 9 of 124 Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153 for database Integrity, quality, and database management practices for the Navigation database. Pilots and...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 10 of 124 FAA APPROVED ABBREVIATIONS AND TERMINOLOGY The following glossary is applicable within the airplane flight manual supplement AC Advisory Circular ADC Air Data Computer ADF Automatic Direction Finder AFCS Automatic F...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 17 of 124 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 Haw...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 19 of 124 G1000 GNSS (GPS/SBAS) NAVIGATION SYSTEM LIMITATIONS NOTE Limitations are in bolded text for this section only The pilot must confirm at system initialization that the Navigation database is current. Nav...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 21 of 124 AHRS AREAS OF OPERATION Flight operations with the G1000 Integrated Avionics installed are prohibited in the following regions due to unsuitability of the magnetic fields near the Earth’s poles: 1. Nort...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 22 of 124 FAA APPROVED SYNTHETIC VISION AND PATHWAYS LIMITS Use of the Synthetic Vision system display elements alone for aircraft control without reference to the G1000 primary flight instruments or the aircraft standby inst...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 23 of 124 DATA LINK WEATHER (XM WEATHER) Datalink weather information displayed by the G1000 system is limited to supplemental use only. XM weather data is not a source of official weather information. Use of the...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 24 of 124 FAA APPROVED KINDS OF OPERATION LIMITS The Hawker Beechcraft models C90A and C90GT are approved for the following types of operations when the required equipment, as shown in the airplane AFM/POH Kinds of Operations...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 29 of 124 Section 3 - Emergency Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 30 AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY ...........

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 30 of 124 FAA APPROVED 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 CO...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 31 of 124 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 .............................................

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 32 of 124 FAA APPROVED ROLL AXIS FAILURE (Red annunciator on PFD) • Indicates a failure of the roll axis of the autopilot. The autopilot will be inoperative. NOTE If the red annunciator illuminates without the autopilot engag...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 33 of 124 AUTOPILOT PRE-FLIGHT TEST FAIL (Red annunciator on PFD) • Indicates the AFCS system failed the automatic Pre-Flight test. The autopilot, ESP (if installed), and electric elevator trim are inoperative. F...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 34 of 124 FAA APPROVED ENGINE FAILURE (AUTOPILOT ENGAGED) 1. AP/YD DISC / TRIM INTRPT Button .......................................................... PRESS and RELEASE 2. Engine Failure Procedure in EMERGENCY PROCEDURES Sec...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 36 of 124 FAA APPROVED 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. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 37 of 124 WINDSHEAR ENCOUNTER For airplanes equipped with Electronic Stability and Protection (ESP): 1. AP/YD DISC / TRIM INTRPT Button .................................................... PRESS and HOLD (To prev...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 39 of 124 Section 3A - Abnormal Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 41 AILERON MIS-TRIM .....................................

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 41 of 124 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 ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 42 of 124 FAA APPROVED If still inoperative: • Pitch Trim ............................................................. MANUALLY TRIM AIRPLANE IN PITCH (Using Elevator Tab Wheel) NOTE Autopilot and yaw damper may also be inop...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 43 of 124 RUDDER MISTRIM (amber or annunciation on PFD) Indicates a mistrim of the rudder while the autopilot is engaged. The autopilot cannot trim the airplane in yaw. During large changes in airspeed, engine fa...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 44 of 124 FAA APPROVED 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...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 45 of 124 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...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 46 of 124 FAA APPROVED 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 altit...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 47 of 124 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...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 48 of 124 FAA APPROVED PITCH MISCOMPARE This message is displayed in the upper right corner of the PFD when the G1000 detects a difference between the pilot’s and copilot’s pitch attitude of more than 5 degrees. Refer to GARM...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 49 of 124 DISPLAY UNIT FAILURE PFD FAILURE PFD failure is indicated by a complete loss of image on a display. The pilot should use the cross side PFD and the standby flight instruments for information to fly the ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 50 of 124 FAA APPROVED MFD FAILURE MFD failure is indicated by a complete loss of image on the center display. 1. Pilot’s Audio Panel DISPLAY BACKUP Button ........................................................................

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 51 of 124 DUAL GPS/SBAS FAILURE (AMBER “DR” OR “LOI” ON HSI) LOSS OF GPS/SBAS NAVIGATION DATA When both GPS/SBAS receivers are inoperative or GPS navigation information is not available or invalid, the G1000 syst...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 52 of 124 FAA APPROVED LOSS OF INTEGRITY (LOI) MODE - ACTIVE WHEN THE AIRPLANE IS WITHIN 30NM OF THE DESTINATION OR DEPARTURE AIRPORT (AS CALCULATED FROM THE PREVIOUS GPS OR DR POSITION). 1. Navigation - Fly towards known vis...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 53 of 124 ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH In some rare instances, the actual course and/or frequency for an ILS localizer may not match the course or frequency stored in the G1000 database. This occ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 54 of 124 FAA APPROVED 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 respect...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 56 of 124 FAA APPROVED ENGINE INDICATION SYSTEM (EIS) FAILURE (RED 'X' ON ENGINE DISPLAY) 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. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 57 of 124 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 A...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 58 of 124 FAA APPROVED USING ADC1 or ADC2 or 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...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 59 of 124 If G1000 operation in display backup mode is required: Select display backup mode on the G1000 system. When display backup mode is selected, the MFD will initially present a non-SVS (blue sky over solid...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 61 of 124 Section 4 - Normal Procedures Table of Contents COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES ........................... 63 BEFORE STARTING .............................................................

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 63 of 124 COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES To obtain an ATC clearance before starting the engines: 1. BAT Switch (Master Switch) ......................................................................

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 64 of 124 FAA APPROVED c. White PFT Annunciator .................................................................. ILLUMINATED (~ 5 Seconds) d. White PFT Annunciator ........................................ EXTINGUISHES when ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 66 of 124 FAA APPROVED WARNING • Pilot’s Trim Override .................................................................................................... CHECK Activate the copilot’s Pitch Trim Switches nose down. Verify el...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 67 of 124 SHUTDOWN AND SECURING These procedures should be conducted after the Battery and Generator Switches have been turned OFF in the AFM SHUTDOWN AND SECURING checklist, and before the flight crew vacates th...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 68 of 124 FAA APPROVED FLIGHT LEVEL CHANGE (FLC) MODE: 1. Altitude Preselect ....................................................................................SET to Desired Altitude 2. Press FLC Button .......................

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 69 of 124 NOTE If the VNV button is pressed more than 5 minutes before the TOD or the altitude preselect is not reset to a lower altitude, VPTH will begin to flash inverse video, white/black, when the aural alert...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 71 of 124 APPROACHES The G1000 is capable of performing many tasks for the pilot to reduce pilot workload during the approach and landing phases of flight. The G1000 system references the Flight Plan to predict t...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 76 of 124 FAA APPROVED NOTE Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized approach. These approaches are NOT considered Approaches with Vertical Guidance (APV). Approaches that a...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 79 of 124 NOTE If the Course Deviation Indicator (CDI) is greater than one dot from center, the autopilot will arm the BC mode and indicate BC in white on the PFD. The pilot must ensure that the current heading w...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 80 of 124 FAA APPROVED approach procedure and turn directly towards the first waypoint in the new approach. Do not attempt to load or activate a new approach while flying the missed approach procedure until ready to fly the n...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 81 of 124 NOTE In ESP equipped airplanes, when the GA button is pressed the Flight Director command bars will command 8 ° nose up and wings level, the HSI nav source automatically switches to GPS, the flight plan...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 82 of 124 FAA APPROVED SYNTHETIC VISION Use of Pathways If Synthetic Terrain is displayed on the PFD, the Pathways may be used to assist the pilot’s awareness of the programmed lateral and vertical navigation path. The follow...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air FAA APPROVED Page 83 of 124 Climb NOT displayed by Pathway VPTH displayed by Pathway TOD Leg 1 Leg 2 Leg 3 Enroute Pathway Altitude Display Approach During an approach transition with the GPS CDI active, the Pathway will be displa...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 85 of 124 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. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 87 of 124 Section 7 - Systems Description Table of contents GENERAL ..................................................................................................................... 88 G1000 INTEGRATED AVIONICS .............

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 88 of 124 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 ch...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 89 of 124 Figure 1, Instrument Panel

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 91 of 124 Figure 3, Copilot's Control Wheel With Trim Switches

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 92 of 124 Figure 4, Copilot's Control Wheel Without Trim Switches

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 93 of 124 Figure 5, Overhead Light Control Panel

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 102 of 124 Figure 14, GFC 700 System Interface

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 103 of 124 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 autop...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 105 of 124 AFCS LATERAL MODES Lateral Mode Control Annunciation Maximum Roll Command Limit Roll Mode (default) ROL 25 ° Left Bank 25 ° Right Bank Level ** LVL 0° Roll Low Bank BANK Key * 15 ° Left Bank 15 ° Right Bank Heading...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 106 of 124 If the above pitch or roll limits are exceeded with the flight director displayed on either PFD or the MFD, the flight director will be removed (decluttered) from the display until the aircraft is within display li...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 108 of 124 displayed in order to reduce clutter on the roll indicator. See Figure 16 for an example of the ESP engagement limit indications. Figure 16 – Nominal Roll Attitude ESP Engagement Limit Indications Once ESP becomes ...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 109 of 124 If an attitude becomes extreme enough for the upper disengagement limit indication to be shown it will be drawn in a similar fashion to the engagement limit indication. See Figure 18 for an example of the ESP roll ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 110 of 124 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 R...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 111 of 124 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 ga...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 117 of 124 STANDBY BATTERY POWER SUPPLY The G1000 installation incorporates a 24 vdc, 5 Ah JET model PS-835 Standby Battery that provides electrical power for the standby attitude gyro, standby altimeter vibrator, and interna...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 118 of 124 LIGHTING SYSTEMS COCKPIT An overhead light control panel, accessible to both pilots, incorporates a functional arrangement of all lighting systems. Each light group has its own rheostat switch placarded BRT – OFF. ...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 119 of 124 PITOT AND STATIC SYSTEM PITOT The pitot heads are the sources of impact air for the operation of the flight instruments. A heated pitot mast is located on each side of the lower portion of the nose. Tubing from the...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 120 of 124 SYNTHETIC VISION General The SVS sub system is dependent upon terrain data provided by the underlying G1000 system. If, for some reason, the terrain data is not available from the G1000, all of the components of th...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 121 of 124 For airplanes that have system software 0636.02 or earlier installed, the terrain/obstacle/airport databases have an area of coverage as detailed below: • The terrain database has an area of coverage from North 75°...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 122 of 124 The FPM indicates the current path of the airplane but does not predict the future path. If aircraft attitude, power setting, airspeed, crosswind, etc. are changed, the FPM will move to indicate the new path result...

190-00682-02 Rev. F Hawker Beechcraft C90A, C90GT and C90GTi King Air Page 123 of 124 aircraft altitude. Terrain that is shown below the horizon line is below the aircraft altitude. Horizon Heading A heading scale may be displayed on the PFD horizon line, if selected by the pilot. The heading marks ...

Hawker Beechcraft C90A, C90GT and C90GTi King Air 190-00682-02 Rev. F Page 124 of 124 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 syste...