Garmin SA01535Wi-D FAA Approved Airplane Flight Manual Supplement
© Copyright 2012
GARMIN Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
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manual and of any revision to this manual onto a hard drive or other electronic storage medium to be
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provided further that any unauthorized commercial distribution of this manual or any revision hereto is
strictly prohibited.
GARMIN International, Inc.
1200 E. 151
st
Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev. 1
Page 2 of 141
GARMIN International, Inc
Log of Revisions
Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual
Supplement for
G1000 Integrated Avionics System and GFC 700 AFCS In
Hawker Beechcraft B300 and B300C King Air Aircraft
REV
NO.
1 ALL Original Issue See Cover
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
See Cover
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
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Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev. 1
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Table of Contents
Section 1 - General ........................................................................................................ 7
Section 2 - Limitations ................................................................................................ 15
Section 3 - Emergency Procedures ........................................................................... 31
Section 3A - Abnormal Procedures ........................................................................... 43
Section 4 - Normal Procedures .................................................................................. 71
Section 5 – Performance ............................................................................................ 98
Section 6 - Weight and Balance ............................................................................... 101
Section 7 - Systems Description .............................................................................. 103
Section 8 – Handling, Service, and Maintenance ................................................... 141
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
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Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 6 of 141 FAA APPROVED
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 installation of the GARMIN G1000 Integrated Avionics System and GFC 700 Digital
Automatic Flight Guidance System in accordance with GARMIN International, Inc. approved data.
The information in this supplement supersedes or adds to the basic POH/AFM only as set forth below.
Users of the manual are advised to always refer to the supplement for possibly superseding information
and placarding applicable to operation of the airplane.
The GARMIN G1000 system installed in the Hawker Beechcraft B300 and B300C King Air Aircraft
provides a fully integrated Display, Communications, Navigation and Flight Control system. Functions
provided by the G1000 system include: Primary Flight Information, Powerplant Monitoring, Navigation,
Communication, Traffic Surveillance, TAWS Class A or B, Weather Avoidance, and a three-axis
automatic flight control / flight director system with optional Electronic Stability & Protection.
USE OF THE HANDBOOK
The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the handbook:
WARNING
Operating procedures, techniques, etc., which could result in personal injury or loss of life if
not carefully followed.
CAUTION
Operating procedures, techniques, etc., which could result in damage to equipment if not
carefully followed.
NOTE
Operating procedures, techniques, etc., which is considered essential to emphasize.
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 7 of 141
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 Augmentation System (SBAS) comprised of two TSO-C145a Class 3 approved
Garmin GIA 63Ws, TSO-C146a Class 3 approved Garmin GDU 104X Display Units, GARMIN GA36 and
GA37 antennas, and GPS software version 3.2 or later approved version. The G1000 GNSS navigation
system in this aircraft is installed in accordance with AC 20-138A.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with
the requirements of AC 20-138A and is approved for navigation using GPS and SBAS (within the
coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR en route,
terminal area, and non-precision approach operations (including those approaches titled “GPS”, “or GPS”,
and “RNAV (GPS)” approaches). The G1000 Integrated Avionics GNSS navigation system installed in
this aircraft is approved for approach procedures with vertical guidance including “LPV” and
“LNAV/VNAV”, within the U.S. National Airspace System.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with
the equipment requirements of AC 90-105 and meets the equipment performance and functional
requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures
without RF (radius to fix) legs. Part 91 subpart K, 121, 125, 129, and 135 operators require a Letter of
Authorization for operational approval from the FAA
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with
the equipment requirements of AC 90-100A for RNAV 2 and RNAV 1 operations. In accordance with AC
90-100A, Part 91 operators (except subpart K) following the aircraft and training guidance in AC 90-100A
are authorized to fly RNAV 2 and RNAV 1 procedures. Part 91 subpart K, 121, 125, 129, and 135
operators require a Letter of Authorization for operational approval from the FAA.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft has been
found to comply with the requirements for primary means of Class II navigation in oceanic and remote
navigation (RNP-10) without time limitations in accordance with AC 20-138A and FAA Order 8400.12A.
The G1000 can be used without reliance on other long-range navigation systems. This does not
constitute an operational approval.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft has been
found to comply with the navigation requirements for primary means of Class II navigation in oceanic and
remote navigation (RNP-4) in accordance with AC 20-138A and FAA Order 8400.33. The G1000 can be
used without reliance on other long-range navigation systems. Additional equipment may be required to
obtain operational approval to utilize RNP-4 performance. This does not constitute an operational
approval.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with
the accuracy, integrity, and continuity of function, and contains the minimum system functions required for
PRNAV operations in accordance with JAA Administrative & Guidance Material Section One: General
Part 3: Temporary Guidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1). The GNSS navigation system
has two ETSO-145 / TSO-C145a Class 3 approved Garmin GIA 63Ws, and ETSO-146 / TSO-C146a
Class 3 approved Garmin GDU 104X Display Units. The G1000 Integrated Avionics GNSS navigation
system as installed in this aircraft complies with the equipment requirements for PRNAV and BRNAV
operations in accordance with AC 90-96A and JAA TGL-10 Rev 1. This does not constitute an
operational approval.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 8 of 141 FAA APPROVED
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 can view the LOA status at www.Garmin.com > Aviation Databases > Type 2 LOA Status.
Navigation information is referenced to WGS-84 reference system.
ELECTRONIC FLIGHT BAG
The G1000 Integrated Avionics System as installed in this aircraft supports approval of AC 120-76A
Hardware Class 3, Software Type C Electronic Flight Bag (EFB) electronic aeronautical chart applications
when using current FliteChart or ChartView data. Additional operational approvals may be required.
For operations under 14 CFR Part 91, it is suggested that a secondary or backup source of aeronautical
information necessary for the flight be available to the pilot in the aircraft. The secondary or backup
information may be either traditional paper-based material or displayed electronically. If the source of
aeronautical information is in electronic format, operators must determine non-interference with the
G1000 system and existing aircraft systems for all flight phases.
REDUCED VERTICAL SEPARATION MINIMUMS (RVSM)
This aircraft has been evaluated in accordance with 14 CFR Part 91, Appendix G, “Operations in
Reduced Vertical Separation Minimum (RVSM) Airspace,” and FAA Advisory Circular 91-85,
“Authorization of Aircraft and Operators for Flight in Reduced Vertical Separation Minimums Airspace,”
and is qualified for RVSM operations as a group aircraft. This finding does not constitute approval to
conduct RVSM operations.
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 9 of 141
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 System
AFM Airplane Flight Manual
AFMS Airplane Flight Manual Supplement
AGL Above Ground Level
Ah Amp hour
AHRS Attitude and Heading Reference System
AIRAC Aeronautical Information Regulation And Control
ALT Altitude, or AFCS altitude hold mode, or ALT button on the GMC 710 AFCS
Mode Controller
ALTS AFCS altitude capture using the altitude in the altitude preselect window
ALTV AFCS altitude capture using the altitude from the VNAV profile vertical
constraint
AMMD Airport Moving Map Display
AP Autopilot
APR AFCS Approach mode, or APR button of GMC 710 AFCS mode controller
APTSIGNS Airport Signs (SVS softkey on the PFD)
APV Approach with Vertical Guidance
ATC Air Traffic Control
AUX Auxiliary
BANK Low-bank mode of the AFCS
BARO Barometric Setting
BAT Battery
BC Back Course
BRNAV Basic Area Navigation
BRT Bright
CB Circuit Breaker
CDI Course Deviation Indicator
CFR Code of Federal Regulations
CLR Clear
COM Communication radio
CRS Course
CWS Control Wheel Steering
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 10 of 141 FAA APPROVED
DA Decision Altitude
DC Direct Current
DL LTNG GFDS Data Link Lightning
DME Distance Measuring Equipment
DN Down
DR Dead Reckoning
EC Error Correction
EFB Electronic Flight Bag
EIS Engine Indication System
ELEC Electrical
ENT Enter
ESP Electronic Stability and Protection
FAF Final Approach Fix
FD Flight Director
FLC AFCS Flight Level Change mode, or FLC button on the GMC 710 AFCS
mode controller
FLTA Forward Looking Terrain Avoidance
FMS Flight Management System
FPM Flight Path Marker or Feet Per Minute
FSB Fasten Seat Belts
ft Feet
ft/min Feet/Minute
GA Go-around
GCU Garmin Control Unit
GDC Garmin Air Data Computer
GDU Garmin Display Unit
GEA Garmin Engine/Airframe Unit
GEN Generator
GEO Geographic
GFC Garmin Flight Control
GFDS Garmin Flight Data Services
GIA Garmin Integrated Avionics Unit
GMC Garmin Mode Control Unit
GP GPS Glide Path
GPS Global Positioning System
GPWS Ground Proximity Warning System
GRS Garmin Reference System (AHRS)
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 11 of 141
GS Glide Slope
GSA Garmin Servo Actuator
GSR Garmin Iridium Satellite Radio
HDG AFCS heading mode or the HDG button on the GMC 710 AFCS Mode
Controller
HITS Highway in the Sky
HPa Hectopascal
HSI Horizontal Situation Indicator
IAF Initial Approach Fix
IAP Instrument Approach Procedure
IAS Indicated Airspeed
ICAO International Civil Aviation Organization
IFR Instrument Flight Rules
ILS Instrument Landing System
in-Hg inches of mercury
INH Inhibit
ITT Interstage Turbine Temper ature
KIAS Knots Indicated Airspeed
LCD Liquid Crystal Display
LDA Localizer Type Directional Aid
LNAV Lateral Navigation
LNAV + V Lateral Navigation with Advisory Vertical Guidance
LNAV/VNAV Lateral Navigation / Vertical Navigation
LOA Letter of Acceptance
LOC Localizer
LOI Loss of Integrity (GPS)
LPV Localizer Performance with Vertical Guidance
LRU Line Replaceable Unit
LTNG Lightning (XM Weather Product)
M Mach
MAP Missed Approach Point
MAXSPD Maximum Speed, AFCS Overspeed Protection mode
MDA Barometric minimum descent altitude
MEL Minimum Equipment List
MFD Multi Function Display
MLS Microwave Landing System
M
Maximum operation limit speed in Mach
MO
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 12 of 141 FAA APPROVED
MNPS Minimum Navigational Performance Spe cifications
MSL Mean Sea Level
NAT North Atlantic Track
NAV Navigation, or AFCS navigation mode, or NAV button on the GMC710 AFCS
Mode Controller
NEXRAD Next Generation Radar (XM Weather Product)
NM Nautical Mile
NPA Non-precision Approaches
OAT Outside Air Temperature
OBS Omni Bearing Selector
OVR Override
P/N Part Number
PDA Premature Descent Alert
PFD Primary Flight Display
PFT Pre-Flight Test
PIT AFCS pitch mode
POH Pilot’s Operating Handbook
PRNAV Precision Area Navigation
PROC Procedure button on the GDU or GCU 477
PSI Pounds per Square Inch
PTCH Pitch
RA Radar Altimeter, or Radar Altitude, or traffic Resolution Advisory
RNAV Area Navigation
RNP Required Navigation Performance
ROL AFCS roll mode
RPM Revolutions per Minute
RVSM Reduced Vert ical Separation Minimums
SBAS Satellite Based Augmentation System
SDF Simplified Directional Facility
SID Standard Instrument Departure
SPD Speed button on the GMC 710 AFCS Mode Controller. Toggles the FLC
speed between Mach and IAS references.
STAR Standard Terminal Arrival Route
STBY Standby
STC Supplemental Type Certificate
STD Standard
SUSP Suspend
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 13 of 141
SVS Synthetic Vision System
SYN TERR Synthetic Terrain softkey
SYN VIS Synthetic Vision softkey
TA Traffic Advisory
TAWS Terrain Awareness and Warning System
TCAS Traffic Alert and Collision Avoidance System
TEMP Temperature
TIS Traffic Information System
TMR Timer
TO Take off
TOD Top of Descent
TSO Technical Standard Order
VAPP AFCS VOR Approach Mode
VCO Voice Call Out
Vdc Volts DC
VDP Visual Descent Point
VFR Visual Flight Rules
VHF Very High Frequency
VMC Visual Meteorological Conditions
V
MO
Maximum operation limit speed in knots
VNAV Vertical Navigation
VNV Vertical Navigation button on the GMC 710 AFCS Mode Controller
VOR VHF Omni-directional Range
VPTH Vertical path
VS Vertical Speed
WAAS Wide Area Augmentation System
WFDE WAAS Fault Detection/Exclusion
WGS-84 World Geodetic System – 1984
WSHLD Windshield
XFR Transfer button on the GMC 710 AFCS Mode Control l er
XM XM satellite system
XPDR Transponder
YD Yaw Damper
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 14 of 141 FAA APPROVED
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 crew during all
phases of flight.
AIRSPEED LIMITATIONS AND INDICATOR MARKINGS
No changes were made to the airplane’s airspeed limitations. The airspeed indicators on the Primary
Flight Displays (PFDs) and the standby airspeed indicator are marked in accordance with the airplane’s
POH/AFM.
A red low speed awareness band is marked on the PFDs in red from 20 – 81 KIAS. The low-speed
awareness band is suppressed while the airplane is on the ground. The low-speed awareness band
appears in flight two seconds after main gear liftoff.
The standby airspeed indicator is marked in accordance with the airspeed markings called out in the
airplane’s AFM/POH. The standby airspeed indicator is not marked with a low speed awareness band.
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 15 of 141
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 or appropriate Airplane Flight
Manual Supplement for engine and propeller limitations.
NOTE
The gauge indicator pointer and digital display will flash inverse red/white video for 5
seconds, then remain steady red, if the indicated engine parameter exceeds its
established limit. The gauge indicator digital display will change to yellow for “caution”
conditions.
OPERATING
PARAMETER
Torquemeter (%) -- 0 to 100 (a) -- 100 (b)(c)
ITT (ºC) -- 400 to 820 (d) -- 820 (e)(f)
Prop N2 (RPM) -- 1050 to 1700 (g) -- 1700 (h)(i)
Gas Generator N1 (%) -- 62 to 104 -- 104
Oil Temperature. (ºC) (k) -- 0 to 99 -- 99
Oil Pressure (psi) (j) 60 90 to 135 60 to 90 135
Red Arc/Radial
(Minimum Limit)
PT6A-60A ENGINES COLOR MARKINGS & RANGES
Green Arc
(Normal)
Yellow Arc
(Caution)
Red Arc/Radial
(Maximum Limit)
Footnotes:
(a) Torque limit applies within range of 1000 - 1700 propeller RPM (N
). Below 1000 RPM, torque is
2
limited to 62%
(b) Torque indications between 100% and 156% are time limited to 20 seconds.
(c) To account for power setting accuracy and steady state fluctuations, inadvertent torque excursions up
to 102% is time limited to 7 minutes.
(d) Maximum ITT during idle is 750ºC. High ITT at ground idle may be corrected by reducing accessory
load and/or increasing N
RPM.
1
(e) ITT indication between 820ºC and 850ºC is time limited to 20 seconds.
(f) ITT starting limit at 1000ºC (red triangle) is time limited to 5 seconds.
(g) Maximum reverse propeller operation is limited to 1650 RPM N
(h) Propeller (N
) speeds between 1735 RPM and 1870 RPM are time limited to 20 seconds.
2
speed.
2
(i) To account for power setting accuracy and steady state fluctuations, inadverte nt propeller RPM
excursions up to 1735 RPM are time limited to 7 minutes.
(j) Normal oil pressure is 90 to 135 psi at gas generator speeds above 72%. With engine torque below
62%, minimum oil pressure is 60 psi at normal oil temperature (60 degrees to 70 degrees C).
Oil pressures under 90 psi are undesirable. Under emergency conditions, to complete a flight, a
lower oil pressure limit of 60 psi is permissible at a reduced power, not to exceed 62% torque. Oil
pressures below 60 psi are unsafe and require that either the engine be shut down o r a landing be
made at the nearest suitable airport, using the minimum power required to sustain flight.
Fluctuations of plus or minus 10 psi are acceptable.
During extremely cold starts, oil pressure may reach 200 psi (red triangle). In flight, oil pressures
above 135 psi but not exceeding 200 psi are permitted only for the duration of the flight.
(k) Oil temperature limits are -40ºC an d +110 ºC. However, temperatures between 99ºC and 110 ºC
are limited to a maximum of 10 minutes.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 16 of 141 FAA APPROVED
MANEUVER LIMITS
No changes have been made to the aircraft’s maneuver limits. The Hawker Beechcraft Super King Air
B300 and B300C are Commuter Category airplanes. Acrobatic maneuvers, including spins, are
prohibited.
OPERATIONS IN RVSM AIRSPACE
The airplane is not permitted to operate in RVSM airspace if the static ports are damaged, or if damage or
surface irregularities are found within the RVSM critical region.
The pilot and copilot PFDs must display the on-side ADC information for operations in RVSM airspace.
G1000 INTEGRATED AVIONICS SYSTEM
The GARMIN G1000 Cockpit Reference Guide P/N 190-01344-00, Rev A, or later FAA accepted revision,
must be immediately available to the flight crew during all phases of flight.
Tuning of the COM and NAV radios using the GCU477 controller must be done from the left seat pilot’s
station and only referencing the pilot’s PFD.
Required flight crewmembers must wear and use headsets when the overhead cockpit speaker audio is
selected OFF.
Do not take off unless all display units are installed and operational.
Do not take off with any display in reversionary mode.
Do not take off with any of the following messages displayed in the ALERTS window:
GPS1 FAIL and GPS2 FAIL simultaneously PFD1 SERVICE
GPS NAV LOST PFD2 SERVICE
GIA1 SERVICE GMA1 SERVICE
GIA2 SERVICE GMA2 SERVICE
MFD SERVICE GEO LIMITS
Operation of the G1000 system is prohibited if the PFD1 FAN FAIL, PFD2 FAN FAIL or MFD FAN FAIL is
displayed in the ALERTS window AND the Outside Air Temperature is greater than 41°C (106°F) AND
cabin air conditioning is inoperative.
Do not takeoff if GIA1 FAN FAIL or GIA2 FAN FAIL is displayed in the ALERTS window AND the Outside
Air Temperature is greater than 42°C (107°F).
Ground operation of the G1000 system is not allowed when the Outside Air Temperature is greater than
47°C (116°F) AND cabin air conditioning is inoperative.
The G1000 system must be turned on and operated for at least 30 minutes before takeoff if ground
outside air temperature is -40°C (-40°F) or below.
Use of VNAV is prohibited during the intermediate segment of an approach that includes a teardrop
course reversal. VNAV will become ‘Unavailable’ at the beginning of the teardrop segment of the course
reversal.
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 17 of 141
The fuel quantity, fuel required, fuel remaining, and gross weight estimate functions of the G1000 are
supplemental information only and must be verified by the flight crew.
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 map display (AMMD). SafeTaxi and Chartview are to be used by the flight crew to
orient themselves on the airport surface to improve pilot situational awareness during gro und operations.
The use of the colors red and amber within the checklist function has not been evaluated or approved by
this STC. Use of the colors red and/or amber within user created checklists may require separate
evaluation and approval by the FAA.
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.
Navigation database is expected to be current for the duration of the flight. If the AIRAC cycle will
change during flight, the pilot must ensure the accuracy of navigation data, including suitability of
navigation facilities used to define the routes and procedures for flight. If an amended chart
affecting navigation data is published for the procedure, the database must not be used to
conduct the procedure.
GPS/SBAS based IFR enroute, oceanic, and terminal navigation is prohibited unless the pilot
verifies and uses a valid, compatible, and current Navigation database or verifies each waypoint
for accuracy by reference to current approved data.
Discrepancies that invalidate a procedure should be reported to Garmin International. The affected
procedure is prohibited from being flown using data from the Navigation database until a new
Navigation database is installed in the aircraft and verified that the discrepancy has been
corrected. Contact information to report Navigation database discrepancies can be found at
www.Garmin.com>Support>Contact Garmin Support>Aviation. Pilots and operators can view navigation
data base alerts at www.Garmin.com > In the Air> NavData Alerts.
For flight planning purposes, in areas where SBAS coverage is not available, the pilot must check
RAIM availability. Within the United States, RAIM availability can be determined using the G1000
WFDE Prediction program, part number 006-A0154-01 (010-G1000-00) or later approved version with
GARMIN GA36 and GA37 antennas selected, or the FAA’s en route and terminal RAIM prediction
website: www.raimprediction.net, or by contacting a Flight Service Station. Within Europe, RAIM
availability can be determined using the G1000 WFDE Prediction program or Europe’s AUGER GPS
RAIM Prediction Tool at http://augur.ecacnav.com/augur/app/home. For other areas, use the G1000
WFDE Prediction program. This requirement is not necessary if SBAS coverage is confirmed to be
available along the entire route of flight. The route planning and WFDE prediction program may be
downloaded from the GARMIN G1000 website on the internet. For information on using the WFDE
Prediction Program, refer to GARMIN WAAS FDE Prediction Program, part number 190-00643-01,
‘WFDE Prediction Program Instructions’.
For flight planning purposes, operations within the U.S. National Airspace System on RNP and
RNAV procedures when SBAS signals are not available, the availability of GPS integrity RAIM
shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of
RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed,
canceled, or re-routed on a track where RAIM requirements can be met.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 18 of 141 FAA APPROVED
For flight planning purposes for operations within European B-RNAV and P-RNAV airspace, if
more than one satellite is scheduled to be out of service, then the availability of GPS integrity
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, canceled, or re-routed on a track where RAIM requirements can be met.
For flight planning purposes, operations where the route requires Class II navigation the aircraft’s
operator or flight crew must use the Garmin WFDE Prediction program to demonstrate that there
are no outages on the specified route that would prevent the G1000 from providing primary means
of Class II navigation in oceanic and remote areas of operation that requires (RNP-10 or RNP-4)
capability. If the Garmin WFDE Prediction program indicates fault exclusion (FDE) is unavailable for
more than 34 minutes in accordance with FAA Order 8400.12B for RNP-10 requirements, or 25 minutes
in accordance with FAA Order 8400.33 for RNP-4 requirements, then the operation must be rescheduled
when FDE is available.
Both GIA 63Ws GPS navigation receivers must be operating and providing GPS navigation
guidance to their respective PFD for operations requiring RNP-4 performance.
North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace operations per
AC 91-49 and AC 120-33 require both GPS/SBAS receivers to be operating and receiving usable signals
except for routes requiring only one Long Range Navigation sensor. Each display computes an
independent navigation solution based on the on-side GPS sensor. However, either display will
automatically revert to the cross-side sensor if the on-side sensor fails or if the cross-side sensor is
determined to be more accurate. A “BOTH ON GPS1” or “BOTH ON GPS2” message does not
necessarily mean that one GPS has failed. Refer to the MFD AUX-GPS STATUS page to determine the
state of the unused GPS.
Whenever possible, RNP and RNAV routes including Standard Instrument Departures (SIDs) and
Obstacle Departure Procedures (ODPs), Standard Terminal Arrival (STAR), and enroute RNAV “Q” and
RNAV “T” routes should be loaded into the flight plan from the database in their entirety, rather than
loading route waypoints from the database into the flight plan individually. Selecting and inserting
individual named fixes from the database is permitted, provided all fixes along the published route to be
flown are inserted. Manual entry of waypoints using latitude/longitude or place/bearing is
prohibited.
“GPS”, “or GPS”, and “RNAV (GPS)” instrument approaches using the G1000 System are
prohibited unless the pilot verifies and uses the current Navigation database. GPS based
instrument approaches must be flown in accordance with an approved instrument approach
procedure that is loaded from the Navigation database.
Not all published Instrument Approach Procedures (IAP) are in the Navigation database. Pilots
planning on flying an RNAV instrument approach must ensure that the Navigation database
contains the planned RNAV Instrument Approach Procedure and that approach procedure must
be loaded from the Navigation database into the FMS flight plan by its name.
IFR non-precision approach approval using the GPS/SBAS sensor is limited to published
approaches within the U.S. National Airspace System. Approaches to airports in other airspace
are not approved unless authorized by the appropriate governing authority.
When operating under instrument flight rules, flight plan selection of any required alternate airport must
not be based on an RNAV (GPS) LP/LPV or LNAV/VNAV approach. Alternate airport selection must be
based upon an LNAV approach or an available ground-based approach for which the aircraft is equipped
to fly.
The navigation equipment required to join and fly an instrument approach procedure is indicated by the
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 19 of 141
title of the procedure and notes on the IAP chart. Use of the GARMIN G1000 GPS/SBAS receivers to
provide navigation guidance during the final approach segment of an ILS, LOC, LOC-BC, LDA,
SDF, MLS or any other type of approach not approved for “or GPS” navigation is prohibited.
When using the G1000 VOR/LOC/GS receivers to fly the final approach segment, VOR/LOC/GS
navigation data is must be selected and presented on the CDI of the pilot flying.
Navigation information is referenced to WGS-84 reference system, and should only be used where the
Aeronautical Information Publication (including electronic data and aeronautical charts) conform to
WGS-84 or equivalent.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 20 of 141 FAA APPROVED
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 Integrated Avionics
installed are prohibited in the following regions due to unsuitability of the Earth’s magnetic fields:
1. IntheNorthernhemisphere,Northofthelinebeginningat:
N069°48'57.14"W180°00'00.00" to
N067°09'04.64"W180°00'00.00" to
N067°09'04.64"W151°00'00.00" to
N060°34'40.96"W123°00'00.00" to
N054°43'13.96"W123°00'00.00" to
N054°43'13.96"W094°30'00.00" to
N054°43'13.96"W065°30'00.00" to
N060°03'03.37"W065°30'00.00" to
N067°13'16.31"W038°00'00.00" to
N067°13'16.31"W007°00'00.00" to
N069°52'01.37"W007°00'00.00" to
N069°52'01.37"W007°00'00.00" to
N069°52'01.37"E026°30'00.00" to
N065°49'54.43"E026°30'00.00" to
N065°49'54.43"E057°00'00.00" to
N060°59'40.52"E057°00'00.00" to
N060°59'40.52"E086°30'00.00" to
N060°59'40.52"E118°00'00.00" to
N062°30'03.55"E118°00'00.00" to
N062°30'03.55"E147°00'00.00" to
N068°00'43.26"E147°00'00.00" to
N068°00'43.26"E180°00'00.00" to
N069°48'57.15"E180°00'00.00" topointofbeginning;
2. IntheSouthernhemisphere,Southofthelinebeginningat:
S070°00'00.00"W180°00'00.00" to
S070°00'00.00"E097°00'00.00" to
S047°00'00.00"E097°00'00.00" to
S047°00'00.00"E155°00'00.00" to
S053°00'00.00"E155°00'00.00" to
S053°00'00.00"E180°00'00.00" topointofbeginning
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 21 of 141
o
80
N
o
N
40
Geographic Latitude
o
0
o
40
S
o
80
S
180oW 120oW 60oW 0
Figure 1, GRS 77 Geographic Limits
o
Geographic Longitude
o
60
E 120
o
E 180oW
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 22 of 141 FAA APPROVED
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 preflight test must complete successfully prior to use of the autopilot, flight director or
manual electric trim.
The maximum fuel imbalance with the autopilot engaged is 300 pounds.
Minimum speed for autopilot operation is 100 KIAS.
Maximum speed limit for autopilot operation is unchanged from the airplane’s maximum airspeed limit
(V
MO/MMO
Autopilot coupled ILS, LOC, LPV, or LNAV/VNAV approaches with the yaw damper inoperative or not
engaged is prohibited.
Do not use autopilot below the following altitudes:
).
1. On takeoff, do not engage the autopilot below ....................................................... 400 feet AGL
2. Cruise .................................................................................................................... 1000 feet AGL
3. Approach (GP or GS mode) .................................................................................... 200 feet AGL
4. Approach (FLC, VS, PIT or ALT mode) .................... Higher of 400 feet AGL or Approach MDA
5. Steep Approaches (GP or GS mode) ..................................................................... 286 feet AGL
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 instruments is prohibited.
Use of the Synthetic Vision system alone for navigation, or obstacle or terrain avoidance is prohibited.
Use of the SVS traffic display alone to avoid other aircraft is prohibited.
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 23 of 141
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 detailed below:
1. The terrain database coverage area is from North 75° Latitude to South 60° Latitude in all
longitudes.
2. The Airport Terrain Database coverage area includes airports from North 75° Latitude to
South 60° Latitude in all longitudes.
3. The Obstacle Database coverage area includes the United States and Europe.
Use of the TAWS or GPWS for navigation or terrain and/or obstacle avoidance is prohibited.
NOTE
The TAWS page and terrain display is intended to serve as a situational awareness tool only. It
may not provide the accuracy, fidelity, or both, on which to solely base decisions and plan
maneuvers to avoid terrain or obstacles.
To avoid unwanted alerts, TAWS and/or GPWS should be inhibited when landing at an airport that is not
included in the airport database.
TRAFFIC AVOIDANCE SYSTEM LIMITS
Use of the MAP - TRAFFIC MAP to maneuver the airplane for traffic avoidance without outside visual
reference is prohibited. The Traffic Information System (TIS) or optional Skywatch HP, Skywatch TAS,
Honeywell KTA-870 TAS, Garmin GTS 820/850 TAS, or Collins TCAS-94 or TCAS-4000 Systems are
intended as an aid for the pilot to visually locate traffic. It is the responsibility of the pilot to see and
manually maneuver the airplane to avoid other traffic. Maneuvers based solely on a traffic advisory (TA)
or on information displayed on a traffic display are not authorized.
DATALINK WEATHER (XM OR GFDS WEATHER)
Datalink weather information displayed by the G1000 system is limited to supplemental use only. XM or
Garmin Flight Data Service (GFDS) weather data is not a source of official weather information. Use of
the NEXRAD, PRECIP, XM LTNG and DL LTNG (Datalink Lightning) data on the MAP – NAVIGATION
MAP, MAP – XM WEATHER DATA LINK or MAP – GFDS WEATHER DATA LINK pages for hazardous
weather, e.g., thunderstorm, penetration is prohibited.
NEXRAD, PRECIP, XM LTNG and DL LTNG information on the MAP – NAVIGATION, MAP – XM
WEATHER DATA LINK, or MAP – GFDS WEATHER DATA LINK pages is intended only as an aid to
enhance situational awareness of hazardous weather, not penetration. It is the pilot’s responsibility to
avoid hazardous weather using official weather data sources and the airplane’s in-flight weather rada r.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 24 of 141 FAA APPROVED
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 – NAVIGATION MAP and/or MAP –
STORMSCOPE page for hazardous weather (thunderstorm) penetration is prohibited. Stormscope
lightning data on the MAP - NAVIGATION or MAP – STORMSCOPE page is intended only as an aid to
enhance situational awareness of hazardous weather, not penetration. It is the pilot’s responsibility to
avoid hazardous weather using official weather data sources and the airplane’s weath er radar.
PLACARDS
On Instrument Panel above the Standby Attitude Indicator:
STANDBY ALT/AS
ALTITUDE – FEET V
S.L TO 21,000 263
21,000 TO 25,000 242
25,000 TO 30,000 217
ABOVE 30,000 194
-KIAS
MO
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 25 of 141
KINDS OF OPERATION LIMITS
The Hawker Beechcraft B300/B300C is approved for the following types of operations when the required
equipment, as shown in the airplane AFM/POH Kinds of Operations Equipment List, supplemented by the
Kinds of Operations Equipment List from other applicable Airplane Flight Manual Supplements, and the
Kinds of Operations Equipment List contained in this Airplane Flight Manual Supplement, is installed and
operable.
1. VFR Day
2. VFR Night
3. IFR Day
4. IFR Night
5. Icing Conditions
KINDS OF OPERATIONS EQUIPMENT LIST
This airplane may be operated in day or night VFR, day or night IFR, and icing conditions when the
required systems and equipment are installed and operable.
The following equipment list identifies the systems and equipment upon which type certification for each
kind of operation was predicated. The system and equipment listed must be installed and operable for
the particular kind of operation indicated unless:
The airplane is approved to be operated in accordance with a current Minimum Equipment List (MEL)
issued by the FAA.
Or:
An alternate procedure is provided in the Pilots Operating Handbook and FAA Approved Flight Manual for
the inoperative state of the listed system or equipment and all limitations are complied with.
Numbers in the Kinds of Operations Equipment List refer to quantities required to be operative for the
specified condition. The list does not include all equipment that may be required by specific operating
rules. It also does not include components obviously required for the airplane to be airworthy such as
wings, empennage, engines, etc.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 26 of 141 FAA APPROVED
System and/or Equipment
Remarks and/or Exceptions
COMMUNICATIONS
No Changes - Refer to Aircraft Flight
Manual
ELECTRICAL POWER
Inverter 0 0 0 0 0 Removed by G1000 modification
INVERTER Annunciator 0 0 0 0 0 Removed by G1000 modification
Standby Battery 0 1 1 1 1
ENGINE INDICATIONS
No Changes - Refer to Aircraft Flight
Manual
ENGINE OIL
No Changes - Refer to Aircraft Flight
Manual
ENVIRONMENTAL
No Changes – Refer to Aircraft Flight
Manual
EQUIPMENT/FURNISHINGS
No Changes – Refer to Aircraft Flight
Manual
FIRE PROTECTION
No Changes – Refer to Aircraft Flight
Manual
FLIGHT CONTROLS
No Changes - Refer to Aircraft Flight
Manual
FUEL
No Changes - Refer to Aircraft Flight
Manual
ICE AND RAIN PROTECTION
No Changes - Refer to Aircraft Flight
Manual
LANDING GEAR
No Changes - Refer to Aircraft Flight
Manual
LIGHTS
No Changes - Refer to Aircraft Flight
Manual
MISCELLANEOUS EQUIPMENT
(Single Pilot Operation Only)
No Changes – Refer to Aircraft Flight
Manual
VFR
Day
VFR
Night
IFR
Day
IFR
Night
Icing
Conditions
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 27 of 141
System and/or Equipment
Remarks and/or Exceptions
NAVIGATION INSTRUMENTS
Magnetic Compass
Outside Air Temperature
G1000 Integrated Avionics
GARMIN G1000 Cockpit Reference
Guide
Autopilot 0 0 1 1 0
Electronic Stability & Protection
(ESP)
Yaw Damper/Rudder Boost 1 1 1 1 1
Control Wheel Autopilot
Disconnect/Trim Interrupt Switches
VHF Communications System 0 0 1 1 1
Audio Control Panel 1 1 1 1 1
Primary Flight Display 2 2 2 2 2
Multi Function Display 1 1 1 1 1
Air Data Computer 2 2 2 2 2
Attitude/Heading Reference System
(AHRS)
Standby Attitude Indicator
Standby Altimeter
Standby Airspeed Indicator
ATC Transponder 0 0 1 1 1
VHF Navigation Receiver 0 0 0 0 0
GPS/SBAS Receiver 1 1 2 2 2
Automatic Direction Finder (ADF) 0 0 0 0 0
Distance Measuring Equipment
(DME)
Radar (Radio) Altimeter 0 0 0 0 0
VFR
Day
VFR
Night
IFR
Day
1 1 1 1 1
1 1 1 1 1
1 1 1 1 1
0 0 0 0 0
1 1 1 1 1
2 2 2 2 2
0 0 1 1 1
1 1 1 1 1
1 1 1 1 1
0 0 0 0 0
IFR
Night
Icing
Conditions
Required only for operations in RVSM
airspace.
Yaw damper is required for flight
above a certain altitude. Refer to
Aircraft’s POH or AFMS for any
installed modifications that affect this
requirement. Rudder Boost is
required for all flights.
Left side is required. Both sides
required for two-crew operation.
Or as required by operating
regulation.
Pilot's audio panel required for single
pilot operation. Both sides required
for two-crew operation.
Required for RVSM operations, or as
required by operating regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 28 of 141 FAA APPROVED
System and/or Equipment
Remarks and/or Exceptions
Marker Beacon Receiver 0 0 0 0 0
Terrain Awareness and Warning
System (TAWS)
Ground Proximity Warning System
(GPWS)
Weather Radar 0 0 0 0 0
XM or GFDS Datalink Weather
GSR 56 Satellite Receiver
GDU Cooling Fans (3 total) 2 2 2 2 2
GIA Cooling Fans (2 total) 0 0 0 0 0
RNAV Operations Equipment and
Components
GPS/SBAS receiver with GPS Software
3.2 or later approved version **Note 1,
2
GDU 104X Display (PFD)
GDU 1500 Display (MFD)
GA36 antenna
GA37 antenna
OXYGEN
No Changes - Refer to Aircraft Flight
Manual
PROPELLER
No Changes VACUUM SYSTEM
Gyro Suction Gage
Instrument Air System
VFR
Day
VFR
Night
IFR
Day
0 0 0 0 0
0 0 0 0 0
0
0
1
2
1
1
1
0 0 0 0 1
0 0 0 0 1
0
0
1
2
1
1
1
0
0
2
2
1
1
1
IFR
Night
Icing
Conditions
Or as required by operating
regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
Or as required by operating
regulation.
0
0
2
2
1
1
1
0
0
All fans are required if OAT is above
41°C (106°F).
Both fans are required if OAT is above
42°C (107°F).
Equipment and components required
for RNAV 2, RNAV 1, B-RNAV,
P-RNAV, Class II navigation, RNP and
RNAV routes including Standard
2
Instrument Departures (SIDs) and
Obstacle Departure Procedures
(ODPs), Standard Terminal Arrival
2
Routes (STARs), and enroute RNAV
“q” and RNAV “T” routes, and “GPS”,
1
“or GPS”, and “RNAV (GPS)”
Instrument approach operations
1
NOTE 1: Some approaches require
1
two functioning GPS/SBAS receivers.
NOTE 2: If only one is required, and
only one is operative, it must be #1.
Refer to Aircraft’s POH or AFMS for
any installed modifications
190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 29 of 141
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Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.1
Page 30 of 141 FAA APPROVED
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