,1,' ,.)
NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be
comoatible with all orevious 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
PAGE 3 of 3
5. MAINTENANCE INSTRUCTIONS: This modification shall be inspected at BHT Scheduled Inspections, Part A or Part B as
applicable, (reference:
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-01 (latest revision), Chap. 5 -
lm;pections; (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 manufacturer's publications are
proprietary to the manufacturer and it's approved facilities). Inspections, maintenance and/or repairs are limited to
authorized persons with the approved current publications, and training.
(d) Within the preceding 24 calendar months, or following any installation or maintenance of the transponder or altimeter
encoder, the integrated ATC transponder system must be tested, and inspected
1/A/W FAR 91.413, & FAR 43, Appendix E,
Paragraph (c).
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. If no wiring problems are found, refer to item 5.
7. REMOVAL AND REPLACEMENT: Applicable installation/maintenance manuals listed in section
8 of this FAA Form 337 should be
referenced, but the removal and replacement of all equipment listed will require no special instructions due to simple installations
using accepted methods, techniques, and practices, as listed
1/A/W section 8 of this field approved FAA Form 337. Removal and
replacement must be performed by authorized persons with the approved current publications, and training.
8. DIAGRAMS: NIA
9. SPECIAL INSPECTIONS REQUIREMENTS: N/A
10. APPLICATION OF PROTECTIVE TREATMENTS: N/A
11. DATA: Reference: Advisory Circular AC 43.13-18 Chapter 7.
12. LIST OF SPECIAL TOOLS: N/A
13. COMMUTER CATEGORY AIRCRAFT: N/A
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 accepted by the FAA, via FAA Form 337 Field Approval Process.
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D Additional Sheets are Attached
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