NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be
compatible with all previous alterations to assure continued conformity with the aoolicable airworthiness requirements.
8. Description of Work Accomplished
(If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.)
BELL 412EP SIN 36106 N412SV
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
CONTINUED
PAGE2 of 2
3. CONTROL, OPERATION INFORMATION: Reference the "FAA Approved Rotorcraft Flight Manual Supplement for Garmin GNS
530 VHF COM Transceiver I VOR I ILS Receiver I GPS Receiver", listed in section 8 of this FAA Form 337 along with Garmin
International Inc. GNS 530 Pilot's Guide, PIN 190-00181-00, Rev. C, dated April 2003 or later appropriate revision for detailed
operating instructions.
4. SERVICING INFORMATION: Reference the applicable manufacturer's installation instructions along with the EA drawing listed
above.
5. MAINTENANCE INSTRUCTIONS: This modification shall be inspected at BHT Scheduled Inspections Part A or Part B as
applicable (ref: BHT-412-MM below) and Annually
1/A/W:
(a) The scope and detail contained in FAR 43 Appendix D, as applicable to the particular line item(s).
(b) Bell Helicopter Textron Model 412 Maintenance Manual BHT-412-MM-1, Rev. 10, dated 30 June 2005, or later revision,
Chapter 5 - Inspections; (Note: Aircraft maintenance manuals are available to each aircraft owner from Bell Helicopter
Textron).
(c) Manufacturer's publications, as referenced in Section 8 of this FAA Form 337; (Note: Many manufacturers' publications are
proprietary to the manufacturer and it's approved facilities). Inspections, maintenance and I or repairs are limited to
authorized persons with the approved current publications, and training.
6. TROUBLE SHOOTING: If a failure or malfunction is noted, the wiring in the aircraft may be checked for proper connections per
installation print, as referenced in Section 8 of this FAA Form 337 by authorized persons with the approved current publications, and
training. If no wiring problems are found, refer to item 5.
7. REMOVAL AND REPLACEMENT: In accordance with the Bendix/King Installation Manual PIN 006-15533-0000, Rev. 5, January
1999 or later approved revision using accepted methods, techniques, and practices as addressed in this FAA Form 337. Removal
and replacement must be performed by authorized persons with the approved current publications and training.
8. DIAGRAMS: As referenced in Section 8 of this FAA Form 337.
9. SPECIAL INSPECTIONS REQUIREMENTS: NIA
10. APPLICATION OF PROTECTIVE TREATMENTS: NIA
11. DATA: Reference: Advisory Circular AC 43.13-18, Chapter 7.
12. LIST OF SPECIAL TOOLS: NIA
13. COMMUTER CATEGORY AIRCRAFT: NIA
14. RECOMMENDED OVERHAUL PERIODS: No additional overhaul time limitations.
15. AIRWORTHINESS LIMITATION SECTION: No additional airworthiness limitations.
16. REVISIONS: Any revisions or alterations of this ICA must be approved via FAA Form 337 Field Approval Process.
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D Additional Sheets are Attached
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