AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 2 of 44 FAA APPROVED
© Copyright 2019
Garmin Ltd. or its subsidiaries
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Garmin International, Inc.
1200 E. 151
st
Street
Olathe, KS 66062 USA
Telephone: 913-397-8200
www.garmin.com
190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
FAA APPROVED Page 3 of 44
Garmin International, Inc.
Log of Revisions
FAA Approved Airplane Flight Manual Supplement for
G1000 NXi Integrated Avionics System and GFC 700 AFCS In Citation Mustang
MODEL 510
REV
NO.
PAGE
NO(S)
DESCRIPTION
DATE OF
APPROVAL
FAA APPROVED
1 ALL Original Issue See Cover See Cover
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
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Table of Contents
Section I – General ...................................................................................................................................... 7
Section II – Operating Limitations ............................................................................................................. 12
Section III – Operating Procedures ........................................................................................................... 29
Section IV – Performance ......................................................................................................................... 37
Section V – Supplements .......................................................................................................................... 39
Section VI – Weight and Balance .............................................................................................................. 41
Section VII – Advisory Information ............................................................................................................ 43
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FAA APPROVED Page 7 of 44
Section I – 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 G1000
NXi avionics upgrade in accordance with Garmin International, Inc. approved data, STC SA01896WI.
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 the supplement for possibly superseding information and
placarding applicable to operation of the airplane.
The Garmin G1000 NXi system installed in the Cessna Citation Mustang MODEL 510 provides a fully
integrated Display, Communications, Navigation and Flight Control system. Functions provided by the
G1000 NXi system include: Primary Flight Information, Powerplant Monitoring, Navigation,
Communication, Traffic Surveillance, TAWS Class B, Weather Avoidance, and a three-axis automatic flight
control / flight director system.
Use of this supplement requires the installation of Garmin G1000 NXi hardware and system software
version 0413.41 or later in the aircraft. Pilots are advised to carefully review the contents of this revision
before operating the airplane.
The following table lists the Pilot’s Guide and Cockpit Reference Guide applicable to the respective system
software version.
System Software
V
ersion
Pilot’s Guide
Part Number
Cockpit Reference Guide
Part Number
0413.41 or later 190-02522-00
Revision A or later
190-02523-00
Revision A or later
Table 1 - Applicable Pilot's Guide and Cockpit Reference Guide
USE OF THE AFMS
The following definitions apply to WARNINGS, CAUTIONS and NOTES found throughout the AFMS:
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
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 8 of 44 FAA APPROVED
ELECTRONIC FLIGHT BAG
Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC 120-
76D as a Type B Electronic Flight Bag (EFB) for FliteCharts and ChartView. Additional requirements may
make a secondary source of aeronautical charts necessary on the aircraft and available to the pilot, such
as traditional paper charts or an additional portable electronic device. If the secondary source of
aeronautical charts is a Portable Electronic Device (PED), its use must be consistent with the guidance in
AC 120-76D.
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 airplane. If the source of aeronautical
information is in electronic format, operators must determine non-interference with the G1000 NXi system
and existing aircraft systems for all flight phases.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with RTCA/DO-200A
and AC 20-153B for database integrity, quality, and database management processes for many of its
aviation databases. LOA status and RTCA/DO-200A List of Applicable Avionics (190-01999-00) can be
viewed at FlyGarmin.com.
REDUCED VERTICAL SEPARATION MINIMUMS (RVSM)
This airplane is equipped for operations in Reduced Vertical Separation Minimum (RVSM) airspace when
the required equipment is maintained in accordance with the Airplane Maintenance Manual. This does not
constitute operational approval. Operational approval must be obtained in accordance with applicable
operating rules.
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FAA APPROVED Page 9 of 44
ABBREVIATIONS AND TERMINOLOGY
The following glossary is applicable within the airplane flight manual supplement
AC Advisory Circular
ADS-B Automatic Dependent Surveillance - Broadcast
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 710 AFCS
Mode Controller
AMC Acceptable Means of Compliance
AMMD Airport Moving Map Display
APCH Approach
Aux Auxiliary
B-RNAV Basic Area Navigation
BARO Barometric Setting
BC Back Course
CDI Course Deviation Indicator
DEST Destination
DUATS Direct User Access Terminal Service
EASA European Aviation Safety Agency
EFB Electronic Flight Bag
ELEV Elevation
ESA Enroute Safe Altitude
FDE Fault Detection/Exclusion
FIS-B Flight Information Service-Broadcast
FMS Flight Management System
FPL Flight Plan
FPM Feet Per Minute
FRT Fixed Radius Transitions
GDU Garmin Display Unit
GEO Geographic
GFC Garmin Flight Control
GIA Garmin Integrated Avionics Unit
GMA Garmin Audio Panel System
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 10 of 44 FAA APPROVED
GMC Garmin Mode Control Unit
GNSS Global Navigation Satellite System
GP GPS Glide Path
GPS Global Positioning System
GRS Garmin Reference System (AHRS)
GS Glide Slope
GTX Garmin Transponder
HSI Horizontal Situation Indicator
ICAO International Civil Aviation Organization
IFR Instrument Flight Rules
ILS Instrument Landing System
JAA Joint Aviation Authorities
LDA Localizer Type Directional Aid
LNAV Lateral Navigation
LNAV/VNAV Lateral Navigation / Vertical Navigation
LOA Letter of Acceptance
LOC Localizer
LP Localizer Performance
LPV Localizer Performance with Vertical Guidance
MDA Barometric Minimum Descent Altitude
MFD Multi Function Display
MLS Microwave Landing System
MPS Meters per Second
MSA Minimum Safe Altitude
MSL Mean Sea Level
MT Meters
NAV Navigation
ODA Organization Designation Authorization
P-RNAV Precision Area Navigation
PFD Primary Flight Display
QFE The altimeter setting which will cause the altimeter to read the height above
the airport or runway threshold elevation.
RAIM Receiver Autonomous Integrity Monitoring
REF Reference
RF Radius-to-Fix
RNAV Area Navigation
RNP Required Navigation Performance
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FAA APPROVED Page 11 of 44
RVSM Reduced Vertical Separation Minimums
SAPT Service Availability Prediction Tool
SBAS Satellite Based Augmentation System
SDF Simplified Directional Facility
STC Supplemental Type Certificate
STD Standard
TAWS Terrain Awareness and Warning System
TGL Temporary Guidance Leaflet
TIS Traffic Information System
TOAC Time Of Arrival Control
TSO Technical Standard Order
TWY Taxiway
VFR Visual Flight Rules
VNAV Vertical Navigation
VNV Vertical Navigation, or Vertical Navigation Button on the GMC 710 AFCS
Mode Controller
VOR Very High Frequency Omni-directional Range
VS Vertical Speed
VSD Vertical Situation Display
WAAS Wide Area Augmentation System
WFDE WAAS Fault Detection/Exclusion
WGS-84 World Geodetic System – 1984
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 12 of 44 FAA APPROVED
Section II – OPERATING LIMITATIONS
TABLE OF CONTENTS
EICAS and Instrument Markings ............................................................................................................... 13
GARMIN G1000 NXi Avionics System ...................................................................................................... 13
G1000 NXi GNSS (GPS/SBAS) Navigation System Operational Approvals ............................................ 15
G1000 NXi GNSS (GPS/SBAS) Navigation System Limitations .............................................................. 23
AHRS AREAS OF OPERATION ............................................................................................................... 26
Traffic Avoidance System Limits ............................................................................................................... 26
Data Link Weather (XM, CONNEXT, or FIS-B Weather) .......................................................................... 27
Kinds of Operations Equipment List .......................................................................................................... 27
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FAA APPROVED Page 13 of 44
OPERATING LIMITATIONS
EICAS AND INSTRUMENT MARKINGS
No changes were made to the airplane’s power plant limitations and indicator markings. The power plant
limitations and indicator markings on the Multi Function Display (MFD) and the Primary Flight Displays
(PFDs) while in reversionary mode are marked in accordance with the airplane’s AFM.
No changes were made to the airplane’s airspeed limitations and indicator markings. The airspeed
indicators on the Primary Flight Displays (PFDs) and the standby airspeed indicator are marked in
accordance with the airplane’s AFM.
GARMIN G1000 NXI AVIONICS SYSTEM
1. The current Garmin G1000 Cockpit Reference Guide (CRG) Part Number and System Software
Version that must be available to the pilot during flight are displayed on the MFD Aux group, System
Status page.
2. Category II approaches are prohibited.
3. Takeoff is prohibited following a flight where either PFD/MFD COOLING or GIA1-2 COOLING
Garmin System Message was displayed, until the condition is identified and corrected.
4. Takeoff is prohibited with a PFD/MFD SERVICE, GIA 1-2 SERVICE, or GMA1-2 SERVICE Garmin
System Message displayed, until the condition is identified and corrected.
5. All display units must be installed and operational.
6. Takeoff with a display in reversionary mode is prohibited.
7. Autopilot:
a. One pilot must remain seated, with the seatbelt fastened, during all autopilot operations.
b. Autopilot operation is prohibited if either PFD is in AHRS reversion.
c. Autopilot Minimum-Use-Height:
1) Takeoff and Climb ............................................................................................ 700 feet AGL
2) Enroute and Descent ..................................................................................... 1000 feet AGL
3) Approach (GP or GPS Mode) .......................................................................... 200 feet AGL
4) Approach (FLC, VS, PIT, or ALT Mode) ............ Higher of 400 feet AGL or Approach MDA
8. [This limitation has been removed.]
9. Use of the NAVIGATION MAP page for pilotage navigation is prohibited unless required by AFM
procedure. The NAVIGATION MAP page is intended only to enhance situational awareness.
Navigation is to be conducted using only current charts, data, and authorized navigation facilities.
10. Use of the TRAFFIC MAP to maneuver the airplane to avoid traffic is prohibited. The TRAFFIC
INFORMATION SYSTEM (TIS) and the optional GTX 345 ADS-B Traffic system are for advisory
use only. TIS and ADS-B are intended only to help the pilot to visually locate traffic. It is the
responsibility of the pilot to see and maneuver to avoid traffic.
11. Use of the TERRAIN information for primary terrain avoidance is prohibited. The TERRAIN
information is intended only to enhance situational awareness. It is the pilot’s responsibility to
provide terrain clearance at all times.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 14 of 44 FAA APPROVED
NOTE
For terrain database cycle 08T2 and earlier cycles, TERRAIN information is not available in locations
north of 75° North latitude or south of 60° South latitude due to the absence of terrain data in these
geographical areas.
12. Do not use data link weather information shown on any display for maneuvering in or near areas
of hazardous weather. The data link weather information is intended to assist in avoiding
hazardous weather. The actual age of the weather phenomena may be older than the indicated
age of the data link weather product.
13. 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.
14. Takeoff with a noticeably drifting heading indicator (1/2 degree per second or greater when the
airplane is stationary) is prohibited. AHRS failure may occur when the heading is drifting in this
manner. A constant heading offset is not an indication of a drifting heading.
15. [This limitation has been removed.]
16. Do not use SafeTaxi, FliteCharts, ChartView, or SurfaceWatch functions as the basis for ground
maneuvering. These 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). These functions are to be used
by the flight crew to orient themselves on the airport surface to improve pilot situational awareness
during ground operations.
17. 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.
190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
FAA APPROVED Page 15 of 44
G1000 NXI GNSS (GPS/SBAS) NAVIGATION SYSTEM OPERATIONAL
APPROVALS
The Garmin G1000 NXi 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 GIAs, TSO-C146d Class 3 approved Garmin GDU 1050A and GDU 1550 Display Units,
Garmin GA36 and GA37 antennas, and GPS software version 5.1 or later approved version. The G1000
GNSS navigation system in this airplane is installed in accordance with AC 20-138D. When all the
equipment is operative, the Garmin G1000 NXi 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 NXi 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 NXi Integrated Avionics GNSS navigation system as installed in this aircraft complies
with the equipment, performance, and functional requirements to conduct RNAV and RNP operations in
accordance with the applicable requirements of the reference documents listed in 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 an FDE prediction
tool that satisfies the
guidance of FAA AC 20-
138D and AC 90-105A (or
later revision).
1
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 16 of 44 FAA APPROVED
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 an FDE prediction
tool that satisfies the
guidance of FAA AC 20-
138D and AC 90-105A (or
later revision).
1
Additional equipment may
be required to obtain
operational approval to
utilize RNP-4
performance.
RNP-2
(Oceanic/
Remote)
GNSS FDE
availability must be
verified prior to
oceanic or remote
continental flight.
Maximum predicted
FDE unavailability is
5 minutes.
1
Two operational
long-range nav
(continued)
FAA AC
20-138D
CHG 2
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 airspace without
reliance on other long-
range navigation systems,
when used in conjunction
with an FDE prediction
tool that satisfies the
(continued)
190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
FAA APPROVED Page 17 of 44
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
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.
guidance of FAA AC 20-
138D and AC 90-105A (or
later revision).
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.
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)
followin
g
the aircraft
FAA AC
20-138D
CHG 2
FAA AC
90-100A
CHG 2
R
C2
Includes RNAV Q and T
routes.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 18 of 44 FAA APPROVED
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
Notes
Item 10a
Code
Item 18
PBN/
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 exist.
P-RNAV utilizes RNAV 1
flight plan codes.
RNP 1
When flying a RNP
procedure containing
a radius-to-fix (RF)
leg, the AFCS must
be operational.
(continued)
At a minimum, the
fli
g
ht director must be
FAA AC
20-138D
CHG 2
FAA AC
90-105A
R
O2
Includes RNP terminal
departure and arrival
procedures. This includes
procedures with radius-to-
fix (RF) legs.
190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510
FAA APPROVED Page 19 of 44
Navigation
Specification
Operational
Requirements/
Authorization
Reference
Documents
ICAO Flight
Plan Code
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 90-105A are
authorized to fly
RNP 1 procedures.
Part 91 subpart K,
121, 125, 129, and
135 operators require
operational approval.
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.
AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1
Page 20 of 44 FAA APPROVED
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 operational
(continued)
FAA AC
20-138D
CHG 2
FAA AC
90-107
N/A
N/A
This 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.
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