Garmin SA01535Wi_D- Manuals

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 5 of 137 Table of Contents Section 1 - General ........................................................................................................ 7 Section 2 - Limitations ..................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 7 of 137 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 modi...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 8 of 137 FAA APPROVED OPERATIONAL APPROVALS G1000 GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT APPROVALS The Garmin G1000 Integrated Avionics GNSS navigation system installed in this aircraft is a GPS system with a Satellite Based Augmentat...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 9 of 137 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 operators ca...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 10 of 137 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 Flight Control ...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 15 of 137 Section 2 - Limitations INTRODUCTION The G1000 Cockpit Reference Guide for Hawker Beechcraft King Air 300/B300 series, GARMIN part number 190-01344-00 Revision A or later, must be immediately available to the flight...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 16 of 137 FAA APPROVED POWER PLANT LIMITATIONS AND INDICATOR MARKINGS No changes were made to the airplane’s engine operating limits. The engine gauges are marked as shown in the following table. Refer to the latest Airplane Flight Manual ...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 17 of 137 MANEUVER LIMITS No changes have been made to the aircraft’s maneuver limits. The Hawker Beechcraft Super King Air 300 is a Normal Category airplane. Acrobatic maneuvers, including spins, are prohibited. OPERATIONS I...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 18 of 137 FAA APPROVED Do not use SafeTaxi or Chartview functions as the basis for ground maneuvering. SafeTaxi and Chartview functions do not comply with the requirements of AC 20-159 and are not qualified to be used as an airport moving ...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 19 of 137 RAIM shall be confirmed for the intended flight (route and time). In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight, the flight should be delayed, canc...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 21 of 137 AHRS AREAS OF OPERATION The GARMIN G1000 system is not designed for use as a polar navigator. Operation outside the approved operating area is prohibited. Refer to Figure 1. Flight operations with the G1000 Integrat...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 22 of 137 FAA APPROVED Figure 1, GRS 77 Geographic Limits Geographic Longitude Geographic Latitude 180 o W 120 o W 60 o W 0 o 60 o E 120 o E 180 o W 80 o S 40 o S 0 o 40 o N 80 o N

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 23 of 137 AUTOPILOT OPERATION LIMITS One pilot must remain seated at the controls, with seatbelt fastened, during all autopilot operations. Do not use autopilot or yaw damper during takeoff and landing. The GFC 700 AFCS prefl...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 24 of 137 FAA APPROVED TAWS, GPWS, AND TERRAIN SYSTEM LIMITS Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with TAWS or GPWS warnings. The TAWS databases have an area of coverage as det...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 25 of 137 OPTIONAL L3 COMMUNICATIONS AVIONICS SYSTEM WX-500 STORMSCOPE Stormscope lightning information displayed by the G1000 system is limited to supplemental use only. The use of the Stormscope lightning data on the MAP – ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 26 of 137 FAA APPROVED KINDS OF OPERATION LIMITS The Hawker Beechcraft King Air 300 is approved for the following types of operations when the required equipment, as shown in the airplane AFM/POH Kinds of Operations Equipment List, supplem...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 31 of 137 Section 3 - Emergency Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 32   AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY ......................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 32 of 137 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 CONTROL SYSTEM A...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 33 of 137 NOTE The maximum altitude lost during malfunction tests was: Cruise – 230 Feet Descent – 555 Feet Maneuvering – 170 Feet Glideslope/Glidepath Approach – 79 Feet Non-Precision Approach – 100 Feet UNSCHEDULED RUDDER B...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 34 of 137 FAA APPROVED MANUAL AUTOPILOT DISCONNECT If necessary, the autopilot may be manually disconnected using any one of the following methods. 1. AP/YD DISC / TRIM INTRPT Button ...........................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 35 of 137 AUTOPILOT FAILURE (Red annunciator on PFD, Red ‘AP’ flashing on PFD, Continuous high-low aural tone) 1. AP/YD DISC / TRIM INTRPT Button ..................................................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 37 of 137 PITCH TRIM FAILURE (Red annunciator on PFD) 1. Indicates a failure of the pitch trim servo of the autopilot. The autopilot will be inoperative. The yaw damper will remain operative. 2. Control Wheel ...................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 38 of 137 FAA APPROVED AUTOPILOT OVERSPEED RECOVERY (Amber annunciation on PFD) 1. Power Levers ..................................................................................................................... REDUCE When overspeed con...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 39 of 137 ENGINE FAILURE (AUTOPILOT ENGAGED) 1. AP/YD DISC / TRIM INTRPT Button .......................................................... PRESS and RELEASE 2. Engine Failure Procedure in EMERGENCY PROCEDURES Section of AFM ....

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 40 of 137 FAA APPROVED LOAD MANAGEMENT TABLE This table replaces the Load Management Table published in the AFM. Use of the following equipment will reduce battery duration by the approximate times listed below. Multiple usage of the follo...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 41 of 137 TAWS AND GPWS TAWS OR GPWS WARNING (Red on PFD and aural “PULL UP” or “[Whoop, Whoop], PULL UP” 1. AP/YD DISC / TRIM INTRPT Button ............................................. PRESS and RELEASE (To disconnect the a...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.1 Page 42 of 137 FAA APPROVED WINDSHEAR ENCOUNTER For airplanes equipped with Electronic Stability and Protection (ESP): 1. AP/YD DISC / TRIM INTRPT Button .................................................... PRESS and HOLD (To prevent automatic ...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 43 of 137 Section 3A - Abnormal Procedures Table of Contents AUTOMATIC FLIGHT CONTROL SYSTEM ................................................................ 45   AILERON MIS-TRIM ................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 45 of 137 AUTOMATIC FLIGHT CONTROL SYSTEM AILERON MIS-TRIM (amber or annunciation on PFD) Indicates a mis-trim of the ailerons while the autopilot is engaged. The autopilot cannot trim the airplane in roll. During large chang...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 46 of 137 FAA APPROVED ELECTRIC PITCH TRIM INOPERATIVE NOTE This condition may be accompanied by a red or annunciation on the PFDs. 1. Move both halves of pilot and copilot pitch trim switches to check for stuck switch. 2. AFCS SERVOS Cir...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 49 of 137 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 lo...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 50 of 137 FAA APPROVED YAW AXIS FAILURE (Amber annunciator on PFD) 1. Indicates a failure of the yaw axis of the autopilot. The yaw damper will disconnect. The autopilot may be engaged and disengaged normally, but the yaw damper and rudde...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 51 of 137 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 Co...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 52 of 137 FAA APPROVED If Copilot and Standby Altimeter Agree (Pilot Altimeter Differs): NOTE The standby altimeter must be corrected for position error using the Altimeter Correction – Standby System chart in the Performance section of t...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 53 of 137 If Able to Identify Accurate Altitude Source: 1. Autopilot ALT Mode .................................................................................................... DISENGAGED 2. Use SENSOR softkey to select mos...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 54 of 137 FAA APPROVED 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...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 55 of 137 If Pilot’s and Copilot’s Altitude Agree: 3. Airspeed 120 KIAS MINIMUM on slowest indicator. 4. Monitor all three airspeed indicators during changes in power or altitude to determine which indicators are inaccurate. ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 56 of 137 FAA APPROVED HEADING 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 heading information. Refer to the GARMIN G1000 Cockpit Referenc...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 57 of 137 If a loss of altitude error correction advisory is received: • Above 18,000 feet MSL: 1. Altitude ....................... MAINTAIN USING CROSS-SIDE ALTIMETER OR STANDBY ALTIMETER NOTE The standby altimeter must be c...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 58 of 137 FAA APPROVED MFD FAILURE MFD failure is indicated by a complete loss of image on the center display. A failed MFD will auto-revert to PFD 1 to display engine data on PFD 1. Engine data may be displayed on PFD 2 by pressing the C...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 59 of 137 If No Alternate Navigation Sources Are Available: DEAD RECKONING (DR) MODE - ACTIVE WHEN THE AIRPLANE IS GREATER THAN 30 NM FROM THE DESTINATION AIRPORT: 1. Navigation - Use the airplane symbol, magenta course line ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 60 of 137 FAA APPROVED 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 occurs most ofte...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 61 of 137 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. I...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 62 of 137 FAA APPROVED FAILED ATTITUDE AND/OR HEADING (ATTITUDE FAIL AND/OR RED "X" OVER HEADING DISPLAY ON PFD) This indicates a loss of pitch, roll, and/or heading information from AHRS. Refer to GARMIN G1000 Cockpit Reference G...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 63 of 137 NOTE • The autopilot will disconnect and will not re-engage. ESP (if installed) will be inoperative. • Reference the GPS track on MFD/PFD map to improve situational awareness. GPS will continue to display correct GP...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 64 of 137 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 GEA circuit breakers ................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 65 of 137 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 informat...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 66 of 137 FAA APPROVED USING ADC1 or ADC2 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 di...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 67 of 137 TAWS AND GPWS TAWS or GPWS CAUTION When a TAWS or GPWS 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 ana...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 68 of 137 FAA APPROVED GPWS INHIBIT (TAWS-A Only) For airplanes equipped with TAWS-A, some GPWS functions may be inhibited to stop alerting if desired. Refer to GARMIN G1000 Cockpit Reference Guide for additional information. To Inhibit G...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 69 of 137 GLIDESLOPE/GLIDEPATH DEVIATION INHIBIT (TAWS-A Only) or For airplanes equipped with TAWS-A, the glideslope or glidepath deviation alerting function may be inhibited to stop alerting if desired. Refer to GARMIN G1000...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 71 of 137 Section 4 - Normal Procedures Table of Contents COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES ........................... 73   PREFLIGHT INSPECTION ...................................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 73 of 137 COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES To obtain an ATC clearance before starting the engines: 1. BAT Switch (Master Switch) ...................................................................................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 74 of 137 FAA APPROVED 12 INCHES 12 INCHES 14 INCHES 10 INCHES FWD STATIC PORTS Figure 2, RVSM Critical Region

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 75 of 137 BEFORE ENGINE STARTING These procedures should be conducted during the airplane’s AFM BEFORE ENGINE STARTING checklist items, after the battery has been turned on and both AHRS have aligned. NOTE Autopilot preflight...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 76 of 137 FAA APPROVED BEFORE TAXI These procedures should be conducted after completing the airplane’s AFM BEFORE TAXI checklist items before brake release. 1. Standby Attitude Indicator .....................................................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 78 of 137 FAA APPROVED • With Elevator Tab Wheel in Motion, AP/YD DISC / TRIM INTRPT Button ....................................................... PRESS AND HOLD (verify elevator tab wheel motion stops) • Pilot’s Trim Override .............

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 79 of 137 WARNING CLIMB, CRUISE, AND DESCENT Disengage autopilot and yaw damper and re-trim the airplane in roll and/or yaw, if slight dutch roll activity is observed. Re-engage the autopilot and yaw damper after trimming the...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 80 of 137 FAA APPROVED VERTICAL MODES VERTICAL SPEED (VS) MODE 1. Altitude Preselect ....................................................................................SET to Desired Altitude 2. Press VS Button .............................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 81 of 137 VERTICAL NAVIGATION (VNAV) VNAV Descent Vertical navigation will only function when the navigation source is GPS navigation. VNAV will not function if the navigation source is VOR, Localizer, or ADF. The airplane’s ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 82 of 137 FAA APPROVED LATERAL MODES HEADING MODE (HDG) 1. HDG Knob ....................................................... PUSH to synch heading bug to current heading 2. HDG BUTTON ..........................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 83 of 137 NAVIGATION (GPS OBS Mode) 1. Navigation Source ................................................ SELECT GPS using the CDI softkey on PFD 2. Select Waypoint .................................................. PRESS the...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 84 of 137 FAA APPROVED c. HSI CDI ......................................................... VERIFY CDI automatically changes to LOC Course pointer slews to the front course d. Pathways ........................................................

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 89 of 137 6. At the FAF ........................................................................ Descend via GP if LNAV+V approach Use desired vertical mode to fly the approach’s vertical profile if LNAV approach Use Altitude...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 91 of 137 BACK COURSE (BC) 1. Load the approach into the Active Flight Plan .................................... VERIFY the G1000 tunes the proper LOC frequency 2. Approach Minimums ..............................................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 92 of 137 FAA APPROVED 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 will result in...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 93 of 137 NOTE 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 sequences to the first published misse...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 94 of 137 FAA APPROVED AUTOPILOT COUPLED GO AROUND (GA) (ESP Equipped Airplanes Only) 1. Control Wheel ................................................................................................... GRASP FIRMLY 2. GO AROUND button (l...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 95 of 137 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 following sections ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 96 of 137 FAA APPROVED 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 displayed along the...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 99 of 137 A L T IM E T E R CO RRE CT IO N - NO RM A L S Y S T EM FLA P S U P N O T E Ab o ve 1 8 ,0 0 0 f t, C o rr e c te d Al ti tu d e = I n d ic a te d Al ti tu d e -1 5 0 -1 4 0 -1 3 0 -1 2 0 -1 1 0 -1 0 0 -9 0 -8 0 -7 0...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW FAA APPROVED Page 101 of 137 Section 6 - Weight and Balance No Change. Refer to basic Aircraft Flight Manual or appropriate supplement.

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 103 of 137 Section 7 - Systems Description Table of Contents GENERAL ................................................................................................................... 104   G1000 INTEGRATED AVIONICS ........................

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 104 of 137 GENERAL This section supplements the Systems Description chapter in the aircraft’s original Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. This section will follow the format and layout of the chapter in th...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 105 of 137 AL T 29 92 1 000 30 0 60 10 0 15 0 200 25 0 40 80 1013 Figure 3, Instrument Panel

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 107 of 137 Figure 5, Copilot's Control Wheel With Trim Switches

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 108 of 137 Figure 6, Copilot's Control Wheel Without Trim Switches

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 109 of 137 ST AN DBY INS TRUMEN T LIGHTS WI ND S H IE LD W IP E R OFF PAR K SL O W FAS T PILO T PFD BRT OFF DO NO T OP E R A TE O N DR Y GL AS S MFD CL OCK S COPILO T PFD MA STE R PANE L LIG H TS ON OFF BR T OF F BR T OF F BR T BR T BR T ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 110 of 137 25 1 1 5 2 5 1 15 25 5 5 25 5 5 5 5 PRIMARY P O W E R A VION IC S MAST ER AVION IC S RC D R VOIC E AU DI O CAB IN WARN AU RA L AUX BA T ST B Y MFD FA N TP L F ED BU S FM S CTL CO M M NO 2 N O 2 CO M M NO 1 AU DI O NO 1 XP D R N...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 111 of 137 Figure 9, Pedestal Configuration

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 112 of 137 Figure 10, GFC 700 System Interface GDU 1040A PFD2 No. 2 GIA 63W AFCS Mode Logic Flight Director Servo Mgt GDU 1500 Multi-Function Display GSA 80 Roll Servo No. 1 GIA 63W AFCS Mode Logic Flight Director Servo Mgt GMC 710 AFCS M...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 113 of 137 FLIGHT CONTROLS AFCS, AUTOPILOT, FLIGHT DIRECTOR AND RUDDER BOOST 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 auto...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 115 of 137 The following tables list the available AFCS vertical and lateral modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 116 of 137 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 Select HDG Key H...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 117 of 137 The Flight Director is not designed to perform unusual attitude recoveries from attitudes outside the following range: Pitch 50° nose up to 50° nose down Roll ±75° If the above pitch or roll limits are exceeded with the flight ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 120 of 137 Once ESP becomes active in roll, the engagement limit indication that was crossed (either left or right) will move to the lower disengagement limit indication over a period of 1 second. The opposite roll limit remains at the en...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 121 of 137 The ESP roll limit indications are not de-cluttered when the aircraft is in an extreme attitude. ESP roll limit indications are not shown when ESP is not configured for a given installation, ESP is not available as determined b...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 122 of 137 FLIGHT INSTRUMENTS G1000 FLIGHT INSTRUMENTS Flight instruments are an integrated part of the G1000 system. For system descriptions, operating instructions, and abnormal failure indication refer to the Cockpit Reference and Pilo...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 123 of 137 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 rep...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 124 of 137 PROPELLER SYNCHROPHASER A push button ON/OFF switch is located on the instrument panel below the pilot ’ s PFD that turns the propeller synchrophaser ON and OFF. To turn the propeller synchrophaser ON, push the PROP SYNC switch...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 126 of 137 TRIPLE FED BUS Bus Tie Power, TPL FED Cabin Audio Cabin Lights Cabin Pressurization Control Cabin Temperature Control COM 1 Eng Anti-Ice, L & R Main Fan – PFD/GIA, L & R Fire Detection L & R Firewall Valve L & R...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 127 of 137 TRIPLE FED BUS Surface Deice Torquemeter, L & R Voice Recorder Windshield Wiper

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 128 of 137 STANDBY BATTERY POWER SUPPLY The G1000 installation incorporates a 24 vdc, 5 Ah L-3 Avionics model PS-835 Standby Battery that provides electrical power for the standby attitude gyro, standby altimeter vibrator, and internal li...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 129 of 137 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. The MASTER PA...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 130 of 137 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 is connected to the copilot ’ s Air Data Computer (ADC2) and the standby i...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 131 of 137 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 the SVS system ...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 132 of 137 The Terrain/Obstacle/Airport databases have an area of coverage as detailed below: • The Terrain Database has an area of coverage from North 75° Latitude to South 60° Latitude in all longitudes. • The Airport Terrain Database h...

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 134 of 137 Because the horizon heading is only displayed in 30 degree increments, it should only be used for general heading awareness and not be used to establish the aircraft heading. Airport Signs and runway highlight If APTSIGNS is se...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 135 of 137 TAWS AND GPWS Refer to the GARMIN Pilot’s Guide and Cockpit Reference Guide, P/N 190-01343-001 and 190-01344-00 Rev. A or later FAA accepted revision for complete detailed descriptions of the GARMIN G1000 TAWS and GPWS system f...

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 137 of 137 Section 8 – Handling, Service, and Maintenance Refer to the G1000/GFC 700 System Maintenance Manual (contains Instructions for Continued Airworthiness) P/N 190-00716-01 Rev. 1 or later FAA approved revision for maintenance requ...