calibrated.
G.
System Checkout is performed.
2.1 Important Information and Initial Checkout:
A.
The installer and aircraft owner must read the Warranty/Agreement before startingThe installer and aircraft owner must read the Warranty/Agreement before starting
The installer and aircraft owner must read the Warranty/Agreement before startingThe installer and aircraft owner must read the Warranty/Agreement before starting
The installer and aircraft owner must read the Warranty/Agreement before starting
the installation.the installation.
the installation.the installation.
the installation. There is information in the Warranty/Agreement that may alter your decision
to install this instrument.
If you do not accept the terms of the Warranty/Agreement, doIf you do not accept the terms of the Warranty/Agreement, do
If you do not accept the terms of the Warranty/Agreement, doIf you do not accept the terms of the Warranty/Agreement, do
If you do not accept the terms of the Warranty/Agreement, do
not install this instrument.not install this instrument.
not install this instrument.not install this instrument.
not install this instrument.
B.
If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install- If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-
If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install- If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-
If you are not an FAA Certified Aircraft Mechanic familiar with the issues of install-
ing engine and aircraft instruments, ing engine and aircraft instruments,
ing engine and aircraft instruments, ing engine and aircraft instruments,
ing engine and aircraft instruments,
Do not attempt to install this instrument.Do not attempt to install this instrument.
Do not attempt to install this instrument.Do not attempt to install this instrument.
Do not attempt to install this instrument.
The The
The The
The
installer should use current aircraft standards and practices to install this instru-installer should use current aircraft standards and practices to install this instru-
installer should use current aircraft standards and practices to install this instru-installer should use current aircraft standards and practices to install this instru-
installer should use current aircraft standards and practices to install this instru-
ment (refer to AC 43.13).ment (refer to AC 43.13).
ment (refer to AC 43.13).ment (refer to AC 43.13).
ment (refer to AC 43.13).
C.
Check that any necessary FAA Approvals for installing this system are available forCheck that any necessary FAA Approvals for installing this system are available for
Check that any necessary FAA Approvals for installing this system are available forCheck that any necessary FAA Approvals for installing this system are available for
Check that any necessary FAA Approvals for installing this system are available for
your aircraft before starting the installation. The STC and AML are located at theyour aircraft before starting the installation. The STC and AML are located at the
your aircraft before starting the installation. The STC and AML are located at theyour aircraft before starting the installation. The STC and AML are located at the
your aircraft before starting the installation. The STC and AML are located at the
back of this manual.back of this manual.
back of this manual.back of this manual.
back of this manual. One CGR-30C should be installed per aircraft.
D. Check the red, yellow and green limits in the “CGR-30 Configuration” document (provided with
the kit) match the aircraft POH/AFM for each function monitored by the CGR-30. It is impor-
tant the CGR-30 is properly configured for the engine and aircraft it is to monitor.
E. Read the Installation Instructions entirely and resolve any issues you may have
beforebefore
beforebefore
before starting
the installation. This may eliminate any delays once the installation is started.
F. Inspect the contents of this package prior to installation.
If the CGR-30 system is to beIf the CGR-30 system is to be
If the CGR-30 system is to beIf the CGR-30 system is to be
If the CGR-30 system is to be
installed into a certified aircraft, check that the Model Number listed on the TSOinstalled into a certified aircraft, check that the Model Number listed on the TSO
installed into a certified aircraft, check that the Model Number listed on the TSOinstalled into a certified aircraft, check that the Model Number listed on the TSO
installed into a certified aircraft, check that the Model Number listed on the TSO
label incorporates the Aircraft ID for which it is to be installed. Each CGR-30Clabel incorporates the Aircraft ID for which it is to be installed. Each CGR-30C
label incorporates the Aircraft ID for which it is to be installed. Each CGR-30Clabel incorporates the Aircraft ID for which it is to be installed. Each CGR-30C
label incorporates the Aircraft ID for which it is to be installed. Each CGR-30C
display is configured for a specific aircraft and should only be installed in thatdisplay is configured for a specific aircraft and should only be installed in that
display is configured for a specific aircraft and should only be installed in thatdisplay is configured for a specific aircraft and should only be installed in that
display is configured for a specific aircraft and should only be installed in that
aircraft.aircraft.
aircraft.aircraft.
aircraft.
G.
Do not install a non-certified CGR in a certified aircraft.Do not install a non-certified CGR in a certified aircraft.
Do not install a non-certified CGR in a certified aircraft.Do not install a non-certified CGR in a certified aircraft.
Do not install a non-certified CGR in a certified aircraft. A certified CGR lists the
applicable TSO numbers at the bottom of the Model Label attached to the side of the CGR.
H.
Before starting the installation make sure the instrument will fit in the intendedBefore starting the installation make sure the instrument will fit in the intended
Before starting the installation make sure the instrument will fit in the intendedBefore starting the installation make sure the instrument will fit in the intended
Before starting the installation make sure the instrument will fit in the intended
installation location without obstructing the operation of any controls.installation location without obstructing the operation of any controls.
installation location without obstructing the operation of any controls.installation location without obstructing the operation of any controls.
installation location without obstructing the operation of any controls. CFR
23.1321(a) states, “Each flight, navigation, and powerplant instrument for use by any required pilot
during takeoff, initial climb, final approach, and landing must be located so that any pilot seated at
the controls can monitor the airplane’s flight path and these instruments with minimum head and eye
movement.” AC 23.1311 provides one method (but not the only method) of complying with this
CFR. AC 23.1311 recommends a powerplant instrument be installed within a distance of 21"
from the pilot’s visual centerline to the middle of the instrument. The pilot’s visual centerline is a
perpendicular line from the pilot’s eye to the instrument panel. In most aircraft, installing the
CGR-30C to the right of the Radio Stack would be acceptable. In some aircraft, the visual
centerline falls to the right of the Attitude Indicator.
If the powerplant instrument cannot be installed within 8" of the pilot’s visual centerline, AC
23.1311 recommends Master Caution and Warning Lights be installed. Installation of Master
Caution and Warning Lights is covered in this manual.
8
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