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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 confonnity 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 PAGE 1 of 1
Installed Aero Dynamix, Inc. Alternate Lighting System IAW STC SR09365RC.
Note: Reference FAA Forms 8110-3; ADl-07-16, dated 07/13/2007 DERT-750020-SW (Structural) and CDW 07040, dated 07/11/2007,
DERT-710263-SW (Systems and Equipment) along with Aero Dynamix, Inc. MDL 1845-01, Rev. R, dated 07/06/2007 (Master Drawing
List 8412) for detailed information concerning the alteration. Instructions for Continued Airworthiness to be performed in
accordance with Aero Dynamix, Inc. Document Number ICA 412EP-02, Rev. H, dated 10/20/2005 along with Appendix E, Rev. J
which was provided to the owner I operator. RFMS for Bell 412EP (412-327) with Alternate Lighting System, Rev. A, dated
05/13/2004 was provided to the owner I operator describing the operating procedures for the Aero Dynamix Alternate Lighting
System.
Installed Precise Flight, Inc. Pulselight Control System, P/N 1220/2410-2 IAW STC SH3319NM.
Note: Reference Precise Flight, Inc. Installation Instructions No. PPRl-2000 or No. I 071384 I 86-1, (latest revision) for detailed
information concerning the alteration. Instructions for Continued Airworthiness to be performed in accordance with Precise Flight,
Inc. Installation Instructions No. PPRl-2000 or No./ 071384 / 86-1, (latest revision) which was provided to the owner I operator.
Installed Bell Helicopter Textron Increased Generator Capacity Kit, PIN 412-706-026-101 IAW Bell Helicopter
Textron Service
Instruction for Increased Generator Capacity Auxiliary Equipment Kit, BHT-412-Sl-34, Revision 1, dated June 1, 2005.
The aircraft was weighed and a new weight and balance was computed. The aircraft's flight manual equipment list was revised.
Pertinent specific details of the alterations are on file at this agency. Aircraft log book entry was made.
!Reference: WIO
C07268EA/2.
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O Additional Sheets are Attached