Garmin Cessna Caravan G1000 Technical specifications

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
CopyrightE2006 All Rights Reserved Mooney Airplane Company -- Louis Schreiner Field Kerrville, Texas 78028
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,
30
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
M20R
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
8of33 ISSUED 11 - 2004
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.
(c) Use of the G1000 VOR/ILS receiver to fly approaches not ap-
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
(c) MAP DATUM….WGS 84 (sets map datum to WGS--84, [see
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.