Turn the engine off. Inspect the entire system to be certain there is no interference with controls. Also,
check for loose fittings, proper connections, clamps, probes, and inspect for leaks, chafing, obstructions,
heat damage and anything that may cause unsafe flight. Check that all fittings are tight.
Check that all fittings are tight.
Check that all fittings are tight.
Check that all fittings are tight.
Check that all fittings are tight.
Loose
fitting can cause engine and/or aircraft damage and possibly personal injury.
5.4 First Flight Checkout:
Prepare the aircraft for flight. Fly the aircraft in the pattern. Check for proper operation of each func-
tion displayed on the CGR. Land the aircraft and perform the following checks as soon as possible:
A. Check all fittings, hoses and transducers for leaks.
B. Check all fittings, hoses, wires, system components and hardware to be secure and not chaffing.
C. Check for interference to any controls.
D. Check for any unsafe condition.
Do not release the aircraft for normal operation until all steps in this document have been performed and
the aircraft is safe to fly.
5.5 Read the "Warranty/Agreement" and the "Important Notice":
Require the pilot to read the "Warranty/Agreement" and the "Important Notice" located in the front of
the "Operating Instructions" before releasing the aircraft for flight.
6.1 Instructions for Continued Airworthiness (ICA):
The Instructions for Continued Airworthiness (ICA) are located in the Electronics International document
06211301 "CGR-30P & CGR-30C Instructions for Continued Airworthiness". If you need an additional
copy of the CGR-30 ICA please visit: www.Buy-Ei.com or call (541) 318-6060.
6.2 Airworthiness Limitations:
The Airworthiness Limitations section is FAA approved and specifies maintenance required under CFR 43.16 and
91.403 of the Code of Federal Aviation Regulations unless an alternative program has been FAA approved.
Operational:
The conditions and tests required for TSO approval of the CGR-30 are minimum performance
standards. It is the responsibility of those installing this system either on or within a specific type
or class of aircraft to determine that the aircraft installation
conditions are within the TSO standards. TSO articles must have
separate approval for installation in an aircraft. The CGR-30 may
be installed only if performed under 14 CFR part 43 or the appli-
cable airworthiness requirements. There are no further specific
operating limitations of this system.
46
Crimp Cavity
Pin Ears face Down
End View
of
the D-sub Pin in the Crimp Tool
