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Page A-4 GTX 330 Installation Manual
Revision G 190-00207-02
5. Maintenance Instructions
Maintenance of the GTX 330 is ‘on condition’ only. Periodic maintenance is not required. Refer
to the GTX 330 Maintenance Manual.
6. Troubleshooting Information
Refer to the GTX 330 Maintenance Manual.
7. Removal and Replacement Information
Refer to Section 2 of this manual. If the unit is removed and reinstalled, a functional check of the
equipment should be conducted in accordance with Section 5 of this manual.
8. Diagrams
Refer to Section 3 and Section 4 of this manual.
9. Special Inspection Requirements
N/A
10. Application of Protective Treatments
N/A
11. Data: Relative to Structural Fasteners
Antenna installation, removal and replacement should be in accordance with applicable provisions
of
AC 43.13-1B and AC 43.13-2A. Also, refer to Section 2 of this manual.
12. Special Tools
N/A
13. This Section is for Commuter Category Aircraft Only
A. Electrical loads: Refer to Section 1.3 of this manual.
B. Methods of balancing flight controls: N/A.
C. Identification of primary and secondary structures: N/A.
D. Special repair methods applicable to the airplane: Antenna installation, removal, and
replacement should be in accordance with applicable provisions of AC 43.13-1B and AC 43.13-2A.
14. Overhaul Period
No additional overhaul time limitations.
15. Airworthiness Limitation Section
N/A.
16. Revision
To revise this ICA, a letter must be submitted to the local FSDO with a copy of the revised FAA
Form 337, and revised ICA. The FAA inspector accepts the change by signing Block 3 and
including the following statement:
“The attached revised/new Instructions for Continued Airworthiness (date ______) for the above
aircraft or component major alteration have been accepted by the FAA, superseding the Instructions
for Continued Airworthiness (date ______).”