Garmin G5000 for Beechjet Owner's manual

Type
Owner's manual
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
ii
© 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,
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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
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
iii
GARMIN International, Inc
FAA Approved Airplane Flight Manual Supplement for
G5000 Integrated Flight Deck and GFC 700 AFCS
Beechcraft Model 400A Beechjet
Log Of Revisions
REV
NO.
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
1 ALL Original Issue See Cover See Cover
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
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190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
v
Table of Contents
Section 1 - General ..................................................................................................... 1-1
Section 2 – Limitations .............................................................................................. 2-1
Section 3 – Emergency Procedures ......................................................................... 3-1
Section 3A – Abnormal Procedures ...................................................................... 3A-1
Section 4 – Normal Procedures ................................................................................ 4-1
Section 5 – Performance ........................................................................................... 5-1
Section 6 - Weight and Balance ................................................................................ 6-1
Appendix A: Systems Description ........................................................................... A-1
Appendix B – Handling, Service, and Maintenance ............................................... B-1
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
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Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-1
Section 1 - General
The information in this supplement is FAA-approved material and must be attached to the FAA Approved
Airplane Flight Manual (AFM) when the airplane has been modified by installation of the GARMIN G5000
Integrated Flight Deck and GFC 700 Digital Automatic Flight Guidance System in accordance with
GARMIN International, Inc. approved data, STC ST01821WI.
The information in this supplement supersedes or adds to the basic AFM only as set forth below. Users
of the manual are advised to always refer to this supplement for possible superseding information and
placarding applicable to operation of the airplane.
The GARMIN G5000 system installed in the Beechcraft Model 400A Beechjet provides a fully integrated
Display, Communications, Navigation and Flight Control system. Functions provided by the G5000
system include: Primary Flight Instrumentation, Powerplant Instrumentation, Navigation,
Communication, Traffic Surveillance, TAWS-B or TAWS-A, Weather Avoidance, and a three-axis
automatic flight control / flight director system.
USE OF THIS AFMS
The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the AFMS:
Operating procedures or techniques that may result in personal injury or loss of life if not
carefully followed.
Operating procedures or techniques that may result in damage to equipment if not carefully
followed.
NOTE
Supplemental information or highlights considered of sufficient significance to require
emphasizing.
CAUTION
WARNING
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-2
G5000 GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT
APPROVALS
The Garmin G5000 Integrated Avionics GNSS navigation system installed in this aircraft is a GPS system
with a Satellite Based Augmentation System (SBAS) comprised of two TSO-C145c Class 3 approved
Garmin GIA 63Ws, two TSO-C146c Class 3 approved Garmin GTC 570 Touchscreen Control Units,
Garmin GA36 and GA37 antennas, and GPS software version 5.0 or later approved version. The G5000
GNSS navigation system in this aircraft is installed in accordance with AC 20-138D. When all the
equipment is operative, the Garmin G5000 system has two independent GNSS long-range navigation
systems. Failure of any of the above equipment indicates only one operational GNSS system.
The Garmin G5000 Integrated Avionics GNSS navigation system as installed in this aircraft 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 G5000 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. This table is accurate at the time it was published. However, changes
to operational rules, FAA advisory circulars, flight plan formats, etc., are possible. The pilot is responsible
to ensure compliance with current operational requirements.
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
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
CHG 2,
FAA AC
90-105A,
FAA AC
91-70A,
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 Garmin
WFDE Prediction program,
part number 006-A0154-01
or later approved version.
1
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-3
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
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
CHG 2,
FAA AC
90-105A,
FAA AC
91-70A
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 Garmin
WFDE Prediction program,
part number 006-A0154-01
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
CHG 2,
FAA AC
90-100A
CHG 2
R
C2
Includes RNAV Q and T
routes.
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-4
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
(continued)
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
CHG 2,
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 exists.
P-RNAV utilizes RNAV 1
flight plan codes.
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-5
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP 1
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) legs.
In accordance with
AC 90-105A, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly
RNP 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A
R
O2
Includes RNP terminal
departure and arrival
procedures, including
procedures with
radius-to-fix (RF) legs.
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-6
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
RNP-2
(Oceanic /
Remote)
GNSS FDE
availability must be
verified prior to flight.
Maximum predicted
FDE unavailability is 5
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
CHG2,
FAA AC
90-105A
R
TBD
The GPS equipment as
installed complies with the
requirements for GPS
primary means of Class II
navigation in oceanic and
remote navigation without
reliance on other
long-range navigation
systems when used in
conjunction with the Garmin
WFDE Prediction program,
part number 006-A0154-01
or later approved version.
1
Additional equipment may
be required to obtain
operational approval to
utilize RNP-2 performance.
Item 18 PBN flight plan
code is still
to-be-determined at time of
publication of this AFMS.
RNP-2
(Domestic /
Offshore
En route)
In accordance with
AC 90-105A, Part 91
operators (except
subpart K) following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly
RNP-2 domestic and
offshore routes.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A
R
TBD
Includes RNP-2 domestic
and offshore routes.
Item 18 PBN flight plan
code is still
to-be-determined at time of
publication of this AFMS.
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-7
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
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 90-105A, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A 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
CHG 2,
FAA AC
90-105A,
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)”. This
includes procedures with
radius-to-fix (RF) legs.
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-8
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
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 90-105A, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-105A are
authorized to fly RNP
APCH LNAV/VNAV
minima procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
FAA AC
20-138D
CHG 2,
FAA AC
90-105A,
EASA AMC
20-27 with
CM-AS-002
R
S2
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS).” This
includes procedures with
radius-to-fix (RF) legs.
Vertical guidance is based
on GPS/SBAS when within
SBAS coverage and on
baro VNAV when outside
SBAS coverage, when
SBAS has been disabled
by pilot selection, or 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
displayed and utilized
when conducting
procedures containing
RF legs
In accordance with
AC 90-107, Part 91
operators (except
subpart K), following
the aircraft and
training guidance in
AC 90-107 are
(continued)
FAA AC
20-138D
CHG 2,
FAA AC
90-107
N/A
N/A
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS)” including
procedures with
radius-to-fix (RF) legs.
LP minima are available
only when within SBAS
coverage.
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-9
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
(continued)
authorized to fly RNP
APCH LP minima
procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
RNP APCH
LPV 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 90-107, 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
20-138D
CHG 2,
FAA AC
90-107,
EASA
AMC 20-28
B
N/A
Includes area navigation
approaches titled
“RNAV (GPS)” and
“RNAV (GNSS)”, including
procedures with
radius-to-fix (RF) legs.
LPV minima are available
only when within SBAS
coverage.
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-10
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
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
CHG 2,
FAA AC
90-105A
N/A
N/A
RNAV Holding:
Supported.
RF Legs:
Supported.
Parallel Offsets:
RNP-4 parallel offsets
as defined by AC
20-138D Chapter 10
are supported.
Advanced RNP parallel
offsets as defined by
AC20-138D Appendix 3
are 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):
Supported
Time of Arrival Control
(TOAC):
Not supported.
________________________________
1. FDE/RAIM availability worldwide can be determined via the following:
Using Garmin WFDE Prediction program, part number 006-A0154-01 or later approved
version with GPS SW >= 3.0 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.
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-11
Within Europe,
Using the Garmin 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 Fly-Garmin
website on the internet (fly.garmin.com/fly-garmin/support/). 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 “Aviation Database Declarations”.
Navigation information is referenced to the WGS-84 reference system.
ELECTRONIC FLIGHT BAG
The G5000 Integrated Avionics System as installed in this aircraft supports approval of AC 120-76C
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 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
G5000 system and existing aircraft systems for all flight phases.
REDUCED VERTICAL SEPARATION MINIMUM (RVSM)
This aircraft is approved for operations in Reduced Vertical Separation Minimum (RVSM) airspace when
required equipment and markings are maintained in accordance with the Garmin G5000 / GFC 700
System Maintenance Manual Beechcraft Model 400A Beechjet.
This does not constitute operational approval. Operational approval must be obtained in accordance
with applicable operating rules.
TRANSPONDER
The ADS-B Out system has been shown to meet the equipment requirements of 14 CFR 91.227.
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-12
ABBREVIATIONS AND TERMINOLOGY
The following glossary is applicable within the airplane flight manual supplement
AC Advisory Circular or Alternating Current
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
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 7250 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 Approach
APPR Approach mode, or APPR button of GMC 7250 AFCS mode controller
APV Approach with Vertical Guidance
ATC Air Traffic Control
AUX Auxiliary
BANK Low-bank mode of the AFCS
BARO Barometric Setting
BC Back Course
BRNAV Basic Area Navigation
CDI Course Deviation Indicator
CFR Code of Federal Regulations
COM Communication radio
CRS Course
CWS Control Wheel Steering
DC Direct Current
DME Distance Measuring Equipment
DN Down
DR Dead Reckoning
Model 400A Section 1 - General
190-01508-03 Rev. 1 Beechcraft Model 400A Beechjet
1-13
EFB Electronic Flight Bag
EIS Engine Indication System
FAF Final Approach Fix
FD Flight Director
FDE Fault Detection and Exclusion
FLC AFCS Flight Level Change mode, or FLC button on the GMC 7250 AFCS
mode controller
FMS Flight Management System
FPM Flight Path Marker or Feet Per Minute
ft Feet
ft/min Feet/Minute
GA Go-around
GCU Garmin Control Unit
GDC Garmin Air Data Computer
GDL Garmin Data Link Radio
GEA Garmin Engine/Airframe Unit
GEN Generator
GEO Geographic
GFC Garmin Flight Control
GIA Garmin Integrated Avionics Unit
GMA Garmin Audio Processor System
GMC Garmin Mode Control Unit
GP GPS Glide Path
GPS Global Positioning System
GPWS Ground Proximity Warning System
GRS Garmin Reference System (AHRS)
GS Glide Slope
HDG AFCS heading mode or the HDG button on the GMC 7250 AFCS Mode
Controller
HSI Horizontal Situation Indicator
IAF Initial Approach Fix
IAS Indicated Airspeed
ICAO International Civil Aviation Organization
IFR Instrument Flight Rules
ILS Instrument Landing System
INH Inhibit
ITT Inter-Turbine Temperature
Model 400A Section 1 - General
Beechcraft Model 400A Beechjet 190-01508-03 Rev. 1
1-14
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
LOC Localizer
LOI Loss of Integrity (GPS)
LPV Localizer Performance with Vertical Guidance
LRU Line Replaceable Unit
M Mach
MAN Manual thrust mode of the Target N
1
Computer. Manual speed select mode
of FLC
MAP Missed Approach Point
MAXSPD Maximum Speed, AFCS Overspeed Protection mode
MCT Maximum Continuous Thrust
MCR Maximum Cruise Thrust
MDA Barometric minimum descent altitude
MFD Multi Function Display
MLS Microwave Landing System
MSL Mean Sea Level
NAV Navigation, or AFCS navigation mode, or NAV button on the GMC7250
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
PRNAV Precision Area Navigation
PROC Procedure button on the GDUs or GCU 475
PSI Pounds per Square Inch
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Garmin G5000 for Beechjet Owner's manual

Type
Owner's manual

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