Garmin G1000 NXi - Cessna Citation Mustang Owner's manual

AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1

Page 2 of 44 FAA APPROVED

Garmin Ltd. or its subsidiaries

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

190-02450-02 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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190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510

FAA APPROVED Page 5 of 44

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

AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510 190-02450-02 Rev. 1

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190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510

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.

190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510

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

190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510

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

190-02450-02 Rev. 1 AFMS, G1000 IAS and GFC 700 AFCS in Citation Mustang Model 510

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

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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