Garmin G1000 - Beechcraft King Air 300/B300 Owner's manual

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Owner's manual

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Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 5
Page 2 of 173
© Copyright 2016
GARMIN Ltd. or its subsidiaries
All Rights Reserved
Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,
disseminated, downloaded or stored in any storage medium, for any purpose without the express prior
written consent of GARMIN. GARMIN hereby grants permission to download a single copy of this
manual and of any revision to this manual onto a hard drive or other electronic storage medium to be
viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or
printed copy of this manual or revision must contain the complete text of this copyright notice and
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
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
Page 3 of 173
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 King Air 300/300LW Aircraft
REV
NO.
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
1
ALL
Original Issue
05/11/2012
Robert G. Murray,
ODA STC Unit
Administrator
GARMIN International, Inc.
ODA-240087-CE
2
ALL
Incorporate system software
0985.06, revised AHRS areas of
operation, added a VNAV
limitation, revised system
temperature limitations, revised
TAWS database coverage areas,
miscellaneous editorial
corrections, repaginated
11/16/2012
Robert G. Murray,
ODA STC Unit
Administrator
GARMIN International, Inc.
ODA-240087-CE
3
ALL
Incorporate system software
0985.07, revised AHRS areas of
operation to account for GRS
7800 installations
2/28/2014
Robert G. Murray,
ODA STC Unit
Administrator
GARMIN International, Inc.
ODA-240087-CE
4
ALL
Revised GRS 7800 AHRS areas
of operation
10/24/2014
Robert G. Murray,
ODA STC Unit
Administrator
GARMIN International, Inc.
ODA-240087-CE
5
ALL
Incorporate system software
0985.08, revised MFD FAILURE
procedure, miscellaneous
editorial corrections
See Cover
See Cover
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 5
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190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 5 of 173
Table of Contents
Section 1 - General ........................................................................................................ 7
Section 2 - Limitations ................................................................................................ 22
Section 3 - Emergency Procedures ........................................................................... 41
Section 3A - Abnormal Procedures ........................................................................... 55
Section 4 - Normal Procedures .................................................................................. 85
Section 5 Performance .......................................................................................... 117
Section 6 - Weight and Balance ............................................................................... 119
Section 7 - Systems Description .............................................................................. 120
Section 8 Handling, Service, and Maintenance ................................................... 173
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
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190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 7 of 173
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 King Air 300 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 this supplement requires Garmin G1000 system software version 0985.07 or later to be installed in
the aircraft. Pilots are advised to carefully review the contents of this revision before operating the
airplane.
USE OF THE HANDBOOK
The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the handbook:
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.
WARNING
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 8 of 173 FAA APPROVED
G1000 GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT
APPROVALS
The Garmin G1000 Integrated Avionics GNSS long range navigation system installed in this airplane is a
GPS system with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145a Class 3
approved Garmin GIA 63Ws, two TSO-C146a Class 3 approved Garmin GDU 104X display units, one GDU
1500 display unit, GARMIN GA36 and GA37 antennas, and GPS software version 3.2 or later approved
version. The G1000 GNSS navigation system is installed in accordance with AC 20-138D. When all the
equipment is operative, the Garmin G1000 system has two independent GNSS long-range navigation
systems. Failure of any of the above equipment or the posting of ‘BOTH ON GPS1’ or ‘BOTH ON GPS2’
annunciators indicates only one operational GNSS system.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this airplane complies with
the requirements of AC 20-138D and is approved for navigation using GPS and GPS/SBAS (within the
coverage of a Satellite Based Augmentation System complying with ICAO Annex 10) for IFR en-route,
terminal area, non-precision approach, and approach procedures with vertical guidance operations.
The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this airplane complies with
the equipment, performance, and functional requirements to conduct RNAV and RNP operations in
accordance with the following table:
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
RNAV 10
RNP 10
Oceanic and
Remote
Areas of
Operation
(Class II
Navigation).
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is
34 minutes
1
.
Two GNSS systems
required to be
operational, (one
GNSS system for
those routes requiring
only one long range
navigation system)
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
FAA AC
20-138D,
FAA AC:
91-70A,
FAA Order
8400.12C
EASA AMC
20-12
R
A1
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote airspace without
reliance on other long-
range navigation systems,
when used in conjunction
with the G1000 WFDE
Prediction program, part
number 006-A0154-01
(010-G1000-00) or later
approved version.
1
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 9 of 173
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
B-RNAV /
RNAV 5
(Europe)
This does not
constitute an
operational approval.
FAA AC
90-96A
CHG 1,
EASA AMC
20-4A
R
B2
RNP 4
Oceanic and
Remote
Areas of
Operation
(Class II
Navigation).
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is
25 minutes.
1
Two operational
long-range nav
systems required, (or
one navigation
system and one
GNSS sensor for
those routes requiring
only one long-range
navigation sensor).
No time limit using
GNSS as the primary
navigation sensor.
Part 91, Part 91
subpart K, 121, 125,
and 135 operators
require operational
approval.
FAA AC
20-138D,
FAA AC:
91-70A,
FAA Order
8400.33
R
L1
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote airspace without
reliance on other long-
range navigation systems,
when used in conjunction
with the G1000 WFDE
Prediction program, part
number 006-A0154-01
(010-G1000-00) or later
approved version.
1
Additional equipment may
be required to obtain
operational approval to
utilize RNP-4 performance.
RNAV 2
The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
In accordance with
AC 90-100A, CHG 2,
Part 91 operators
(except subpart K)
(continued)
FAA AC
20-138D,
FAA AC
90-100A
CHG 2
R
C2
Includes RNAV Q and T
routes.
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 10 of 173 FAA APPROVED
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
following the aircraft
and training guidance
in AC 90-100A are
authorized to fly
RNAV 2 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNAV 1
The GNSS RNAV
system is installed
and meets the
performance and
functional
requirements of AC
90-100A.
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 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D,
FAA AC
90-100A
CHG 2
R
D2
Includes RNAV terminal
departure and arrival
procedures.
P-RNAV
(Europe)
This does not
constitute an
operational approval.
FAA AC
90-96A
CHG 1,
JAA TGL
10 Rev 1
R
D2
ICAO flight plan code for
P-RNAV no longer exist.
P-RNAV utilizes RNAV 1
flight plan codes.
RNP 1
When flying a RNP
procedure containing
an RF leg, the AFCS
must be operational.
(continued)
FAA AC
90-105
R
O2
Includes RNP terminal
departure and arrival
procedures. For airplanes
that have system software
(continued)
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 11 of 173
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
At a minimum, the
flight director must be
displayed and utilized
when conducting
procedures containing
Radius-to-Fix (RF)
legs.
In accordance with
AC 90-105, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105 are
authorized to fly
RNP 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
0985.07 or later installed,
this includes procedures
with RF (radius to fix) legs.
RNP APCH
LNAV minima
When flying a RNP
procedure with a
Radius-to-Fix (RF)
leg, the AFCS must
be operational. At a
minimum, the flight
director must be
displayed and utilized
when conducting
procedures containing
RF legs.
In accordance with
AC 90-105, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105 are
authorized to fly RNP
APCH LNAV minima
procedures.
(continued)
FAA AC
20-138D
FAA AC
90-105,
EASA AMC
20-27
R
S1
Includes non-precision
approaches based on
conventional navigation
aids with “or GPS” in the
title and area navigation
approaches titled “GPS”,
“RNAV (GPS)”, and
“RNAV (GNSS)”. For
airplanes with system
software 0985.07 or later
installed, this includes
procedures with RF (radius
to fix) legs.
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 12 of 173 FAA APPROVED
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNP APCH
LNAV/VNAV
minima
When flying a RNP
procedure with a
Radius-to-Fix (RF)
leg, the AFCS must
be operational. At a
minimum, the flight
director must be
displayed and utilized
when conducting
procedures containing
RF legs.
In accordance with
AC 90-105, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105 are
authorized to fly RNP
APCH LNAV minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
FAA AC
90-105
EASA AMC
20-27 with
CM-AS-002
R
S2
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS).” For
airplanes with system
software 0985.07 or later
installed, this includes
procedures with RF (radius
to fix) legs.
Vertical guidance is based
on GPS/SBAS when within
SBAS coverage and by
baro VNAV (system
software 0985.07 or later)
when outside SBAS
coverage, or when SBAS
has been pilot disabled for
approaches with ‘WAAS
VNAV NA’.
The aircraft complies with
the criteria of AMC 20-27
for RNP approaches to
LNAV/VNAV minima, with
the exception that VNAV is
based on SBAS/GNSS
geometric altitude when
SBAS/GNSS is available
and authorized.
RNP APCH
LP minima
When flying a RNP
procedure with a
Radius-to-Fix (RF)
leg, the AFCS must
be operational. At a
minimum, the flight
director must be
(continued)
FAA AC
90-107
N/A
N/A
For airplanes with system
software 0985.07 or later
installed, this includes area
navigation approaches
titled “RNAV (GPS)” and
“RNAV (GNSS)” including
procedures with RF legs.
(continued)
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 13 of 173
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
displayed and utilized
when conducting
procedures containing
RF legs.
In accordance with
AC 90-105, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105 are
authorized to fly RNP
APCH LNAV/VNAV
minima procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
LP minima are available
only when within SBAS
coverage.
In accordance with
AC 90-107, Part 91
operators (except
subpart K), following the
operational considerations
and training guidance in AC
90-107 are authorized to fly
RNP APCH LP minima
procedures.
RNP APCH
LPV minima
When flying a RNP
procedure containing
an RF leg, the AFCS
must be operational.
At a minimum, the
flight director must be
displayed and utilized
when conducting
procedures containing
Radius-to-Fix (RF)
segments.
In accordance with
AC 90-107, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-107 are
authorized to fly RNP
APCH LPV minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
90-107,
EASA
AMC 20-28
B
N/A
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS).” For
airplanes with system
software 0985.07 or later
installed, this includes
procedures with RF (radius
to fix) legs. LPV minima
are available only when
within SBAS coverage.
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 14 of 173 FAA APPROVED
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
Notes
Item 10a
Code
Item 18
PBN/
Advanced
RNP
See Notes for
specific
Advanced
RNP
functions.
This does not
constitute an
operational approval.
FAA AC
20-138D
N/A
N/A
RNAV Holding:
Supported.
RF Legs: Supported
in airplanes with
system software
0985.07 or later
installed.
Parallel Offsets: RNP-
4 parallel offsets as
defined by AC 20-138D
Chapter 10 are
supported. However,
Advanced RNP parallel
offsets as defined by
AC 20-138D Appendix
3 are not supported.
Higher Continuity:
Supported when both
GIA 63W GPS/SBAS
receivers are operating
and providing GPS
navigation guidance to
their respective PFD.
Scalable RNP:
Not supported.
Fixed Radius
Transitions (FRT):
Not supported.
Time of Arrival Control
(TOAC):
Not supported.
_________________________________
1. FDE/RAIM availability worldwide can be determined via the following:
Using G1000 WFDE Prediction program, part number 006-A0154-01 (010-G1000-00) or later
approved version with GARMIN GA36 and GA37 antennas selected.
Also, within the United States:
Via the FAA’s RAIM Service Availability Prediction Tool (SAPT) website: http://sapt.faa.gov.
Contacting a Flight Service Station (not DUATS) to obtain non-precision approach RAIM.
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 15 of 173
Within Europe,
Using the G1000 WFDE Prediction program,
Europe’s AUGER GPS RAIM Prediction Tool at http://augur.ecacnav.com/augur/app/home.
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’.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153A for
database integrity, quality, and database management practices for the Navigation database. Flight crews
and operators can view the LOA status at FlyGarmin.com then select” Type 2 LOA Status”.
Navigation information is referenced to the 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 B Electronic Flight Bag (EFB) electronic aeronautical chart applications
when using current FliteChart or ChartView data. Additional operational approvals may be required.
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 FliteChart database. Flight crews
and operators can view the LOA status by selecting the Type 2 LOA status quick link at
www.FlyGarmin.com.
For operations under 14 CFR Part 91, it is suggested that a secondary or back up 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.
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 16 of 173 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 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
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 17 of 173
DA Decision Altitude
DC Direct Current
DG Directional Gyro
DH Decision Height
DL LTNG Connext 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 Awareness
FMS Flight Management System
FPM Flight Path Marker or Feet Per Minute
FSB Fasten Seat Belts
FSD Full Scale Deflection
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
GIA Garmin Integrated Avionics Unit
GMC Garmin Mode Control Unit
GP GPS Glide Path
GPS Global Positioning System
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 18 of 173 FAA APPROVED
GPWS Ground Proximity Warning System
GRS Garmin Reference System (AHRS)
GS Glide Slope
GSA Garmin Servo Actuator
GSR Garmin Iridium Satellite Radio
GTS Garmin Traffic System
GWX Garmin Weather Radar
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 Temperature
KIAS Knots Indicated Air Speed
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)
LP Localizer Performance
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
190-00716-02 Rev. 5 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 19 of 173
MDA barometric minimum descent altitude
MEL Minimum Equipment List
MFD Multi Function Display
MLS Microwave Landing System
M
MO
Maximum operation limit speed in mach
MNPS Minimum Navigational Performance Specifications
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 TCAS II Resolution Advisory
RF Radius-to-Fix
RNAV Area Navigation
RNP Required Navigation Performance
ROL AFCS roll mode
RPM Revolutions per Minute
RVSM Reduced Vertical 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
Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev.5
Page 20 of 173 FAA APPROVED
speed between Mach and IAS references.
STAR Standard Terminal Arrival Route
STBY Standby
STC Supplemental Type Certificate
STD Standard
SUSP Suspend
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 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
VDI Vertical Deviation Indicator
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 Controller
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Garmin G1000 - Beechcraft King Air 300/B300 Owner's manual

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Owner's manual
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