NOTICE
~
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be
compatib7e with all
orevious afterations to assure continued conformity with the aoDlicable airworthiness requirements.
8. Description of Work Accomplished
(ff more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.)
BELL 412EP S/N 36106 N82628 PAGE 2
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
(CONTINUED)
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: Requires no special instructions due to simple installations using accepted methods,
techniques, and practices,
I/Am section 8 of this FAA FORM 337, and must be performed by persons authorized by FAR 43,
paragraph 43.3, refer to item 5.
8. DIAGRAMS: NIA
9. SPECIAL
INSPECT!Q"!S REQUll~EME(\ITS: NIA
10. APPLICATION OF PROTECTIVE TREATMENTS: N/A
11. DATA: REF: 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.
-END-
_J
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