Garmin Cessna Caravan G1000 Caractéristiques techniques

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

ISSUED 11 - 2004 1of33

REVISION A 06--2005 FAA APPROVEDREVISION B 03--2006

MOONEY AIRPLANE COMPANY, INC.

LOUIS SCHREINER FIELD KERRVILLE, TEXAS 78028

FAA APPROVED

AIRPLANE FLIGHT MANUAL SUPPLEMENT

FOR

GARMIN G1000

INTEGRATED AVIONICS SYSTEM

INSTALLED IN MOONEY M20R

REG. NO. _____________________________________________

SERIAL NO. ____________________________________________

This Supplement must be attached to the FAA Approved Airplane Flight

Manual when the GARMIN G1000 Integrated Avionics System is

installed in accordance with Mooney Drawing Number 950300. The in-

formation contained herein supplements and / or replaces the informa-

tion of the basic Airplane Flight Manual. For Limitations, Procedures

and Performance information not contained in this Supplement, consult

the basic Airplane Flight Manual.

FAA APPROVED

Michele M. Owsley

Manager, Aircraft Certification Office

FEDERAL AVIATION ADMINISTRATION

2601 Meacham Boulevard

Fort Worth, Texas 76137-0150

SUPP0001B

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

2of33 ISSUED 11 - 2004

REVISION A 06--2005

FAA APPROVED REVISION B 03--2006

LOG OF REVISIONS

REV.

NUMBER

PAGE

NUMBER(S)

DESCRIPTION FAA

APPROVED

APR’VD

DATE

A7, 17, 29,

Add following components

from Garmin G1000 Cockpit

Reference Guide:

GDL 69A

DME

ADF

B17, 30 Add SKYWATCHt

Capability

THE REVISED PORTIONS OF AFFECTED PAGES ARE INDICATED BY VERTICAL

LINES IN THE MARGIN.

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

ISSUED 11 - 2004 3of33

REVISION A 06--2005 FAA APPROVEDREVISION B 03--2006

TABLE OF CONTENTS

SECTION PAGE

I GENERAL 5...........................................

II LIMITATIONS 7........................................

III EMERGENCY PROCEDURES 15.........................

IV NORMAL PROCEDURES 21.............................

V PERFORMANCE 27.....................................

VI WEIGHT AND BALANCE 27..............................

VII AIRPLANE AND SYSTEM DESCRIPTIONS 27..............

VIII HANDLING AND SERVICING 33..........................

IX SUPPLEMENTAL DATA 33...............................

X SAFETY TIPS 33........................................

MOONEY

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AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

4of33 ISSUED 11 - 2004

REVISION A 06--2005

FAA APPROVED REVISION B 03--2006

INTENTIONALLY LEFT BLANK

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

ISSUED 11 - 2004 5of33

REVISION A 06--2005 FAA APPROVEDREVISION B 03--2006

SECTION I -- GENERAL

1. The GARMIN G1000 Integrated Avionics System is a fully integrated

flight, engine, communication, navigation and surveillance instru-

mentation system. The system consists of a Primary Flight Display

(PFD), Multi--Function Display (MFD), audio panel (GMA), Air Data

Computer (ADC), Attitude and Heading Reference System (AHRS),

engine / airframe processing unit (GEA), and integrated avionics

(GIA) containing VHF communications, VHS navigation, and GPS

navigation.

2. The primary function of the PFD is to provide attitude, heading, air

data, navigation, and alerting information to the pilot. The PFD may

also be used for flight planning. The primary function of the MFD is to

provide engine information, mapping terrain information and for

flight planning. The audio panel is used for selection of radios for

transmitting and listening, intercom functions, and marker beacon

functions.

3. The primary function of the VHF Communication portion of the

G1000 is to enable external radio communication. The primary func-

tion of the VOR/ILS Receiver portion of the equipment is to receive

and demodulate VOR, localizer, and Glide Slope signals. The prima-

ry function of the GPS portion of the system is to acquire signals from

the GPS satellites, recover orbital data, make range and Doppler

measurements, and process this information in real time to obtain

the user’s position, velocity, and time.

4. Provided the GARMIN G1000 GPS receivers are receiving ade-

quate and usable GPS and/or VHF navigation signals, it has been

demonstrated capable of and meets the accuracy specifications for

the following types of flight operations:

VFR/IFR en--route, oceanic, and terminal operations as well as non-

precision instrument approach (GPS, Loran--C, VOR, VOR--DME,

TACAN, NDB, NDB--DME, RNAV) operation within the U.S. National

Airspace System in accordance with AC20--138A.

Navigation in the North Atlantic Minimum Navigation Performance

Specification (MNPS) Airspace in accordance with AC91--49 and AC

120--33.

The GARMIN G1000 system meets RNP5 airspace (BRNAV) re-

quirements of AC 90--96 and in accordance with AC 20--138A, JAA

AMJ 20X2 Leaflet 2 Revision 1, and FAA Order 8110.60 for oceanic

and remote

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

6of33 ISSUED 11 - 2004

REVISION A 06--2005

FAA APPROVED REVISION B 03--2006

airspace operations, provided it is receiving usable navigation infor-

mation from the GPS receiver. (A separate software application for

prediction of GPS navigation availability may be required for oceanic

and remote operations. Refer to appropriate limitations for the air-

space you are operating in to determine if this GPS prediction soft-

ware is required.)

Navigation is accomplished using the WGS--84 (NAD--83) coordinate

reference datum. GPS navigation data is based upon use of only the

Global Positioning System (GPS) operated by the United States of

America.

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

ISSUED 11 - 2004 7of33

REVISION A 06--2005 FAA APPROVEDREVISION B 03--2006

SECTION II -- LIMITATIONS

GENERAL

G1000 System:

1. The GARMIN G1000 Cockpit Reference Guide for the M20R Series

aircraft, P/N 190--00450--01, Revision A or later approved revision

must be immediately available to the flight crew.

2. The GARMIN G1000 must utilize the following or later FAA approved

software versions:

SUB--SYSTEM SOFTWARE VERSION

PFD 4.06

MFD 4.06

GMA 2.08

AHRS 2.03

ADC 2.05

GIA 2.08

GEA 2.04

GPS 3.01

The database version is displayed on the MFD power--up page immedi-

ately after system power--up and must be acknowledged. The remain-

ing system software versions can be verified on the AUX group sub--

page 5, “AUX – SYSTEM STATUS”.

3. IFR enroute, oceanic and terminal navigation predicated upon the

G1000 GPS Receiver is prohibited unless the pilot verifies the cur-

rency of the database or verifies each selected waypoint for accura-

cy by reference to current approved data.

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

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REVISION A 06--2005

FAA APPROVED REVISION B 03--2006

4. Instrument approach navigation predicated upon the G1000 GPS

Receiver must be accomplished in accordance with approved in-

strument approach procedures that are retrieved from the GPS

equipment database. The GPS equipment database must incorpo-

rate the current update cycle.

(a) Instrument approaches utilizing the GPS receiver must be

conducted in the approach mode and Receiver Autonomous

Integrity Monitoring (RAIM) must be available at the Final Ap-

proach Fix.

(b) Accomplishment of ILS, LOC, LOC--BC, LDA, SDF, MLS or

any other type of approach not approved for GPS overlay with

the G1000 GPS receiver is not authorized.

proved for GPS require VOR/ILS navigation data to be valid

on the PFD display.

(d) When an alternate airport is required by the applicable operat-

ing rules, it must be served by an approach based on other

than GPS navigation, the aircraft must have the operational

equipment capable of using that navigation aid, and the re-

quired navigation aid must be operational.

(e) VNAV information may be utilized for advisory information

only. Use of VNAV information for Instrument Approach Pro-

cedures does not guarantee step--down fix altitude protec-

tion, or arrival at approach minimums in a normal position to

land. VNAV also does not guarantee compliance with inter-

mediate altitude constraints between the top of descent and

the waypoint where the VNAV path terminates in terminal or

enroute operations.

5. If not previously defined, the following default settings must be made

in the “SYSTEM SETUP” menu of the G1000 prior to operation (refer

to Pilot’s Guide for procedure, if necessary.

(a) DIS, SPD…..nmkt(sets navigation units to “nautical miles”

and “knots”)

(b) ALT, VS……..ftfpm (sets altitude units to “feet” and “feet per

minute”)

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

ISSUED 11 - 2004 9of33

REVISION A 06--2005 FAA APPROVEDREVISION B 03--2006

note below])

(d) POSITION……..deg--min (sets navigation grid units to deci-

mal minutes)

example: dd.mm.ss: 45_30’ 30” in decimal minutes are: 45_

30.5’

NOTE:

In some areas outside the United States, datums other than

WGS--84 or NAD--83 may be used. If the G1000 is authorized

for use by the appropriate Airworthiness authority, the re-

quired geodetic datum must be set in the G1000 prior to its

use for navigation.

6. Operation is prohibited north of 70oN and south of 70oS latitudes. In

addition, operation is prohibited in the following two regions: 1) north

of 65o N between 75oW and 120oW longitude and 2) south of 55oS

between 120oE and 165oE longitude.

7. CAUTION: CDI automatic source switching to the ILS on Nav 1 or 2

must be set to manual for instrument approaches conducted with the

autopilot coupled. If the CDI navigation source is changed when au-

topilot is engaged in GPSS mode, the S--Tec 55x autopilot lateral

mode will revert to wings level mode and indicate GPSS FAIL. NAV

mode must be manually reselected by the pilot in order to track the

ILS or Localizer.

8. Display of autopilot operational mode on the PFD is supplemental to

the data which is presented on the display of the S--Tec 55X autopilot

control unit.

2.1 AIRSPEED MARKINGS – M20R

Marking IAS Significance

Red band 20 KIAS – 59 KIAS Low speed awareness -- stall is

imminent

White band 59 KIAS – 110 KIAS Operating range with flaps fully ex-

tended

Green band 66 KIAS – 174 KIAS Normal operating range

Yellow band 174 KIAS -- 195 KIAS Caution range -- smooth air only

Red band 195 KIAS and greater Lower limit of 195 KIAS is the maxi-

mum speed for all operations

The airspeed indicator is marked in IAS values.

MOONEY

M20R

AFM SUPPLEMENT

GARMIN G1000 INTEGRATED AVIONICS SYSTEM

10 of 33 ISSUED 11 - 2004

REVISION A 06--2005

FAA APPROVED REVISION B 03--2006

2.2 POWER PLANT INSTRUMENT MARKINGS

Power plant instrument markings and their color code significance are

shown in the table below.

NOTE:

When an indication lies in the caution range, the legend for

that display will change to the color of the caution range.

When an indication lies in the upper or lower prohibited

range, the legend for that display will change to the color of

the prohibited range and will begin flashing as well.

MOONEY M20R

Indication Red

arc / bar

Lower

prohibited

range

Yellow

arc / bar

Caution

range

Green

arc / bar

Normal

operating

range

Yellow

arc / bar

Caution

range

Red

arc / bar

Upper

prohibited

range

Engine RPM -- -- -- -- 2200 – 2500 -- -- 2500 – 2600*

Manifold

Press. In. Hg

-- -- -- -- 10 – 35** -- -- -- --

Oil Temp oF-- -- -- -- 75 – 240 -- -- >240

Oil Press PSI 0–10 10–30 30 – 100 -- -- >100

Cyl. Head

Temp oF

-- -- -- -- 250 – 460 -- -- >460

Fuel Flow

gal/hr

-- -- -- -- 0--30 -- -- -- --

* To prevent nuisance alerts during normal takeoffs: the “RPM” and

“MAP” data will not turn red or flash until the RPM exceeds 2540.

** No color scale is depicted, and manifold pressure should be within

this range.

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