NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration mu<>t be "'
compatible with all previous alterations to assure continued conformity with the applicable 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.)
1. Installed Aeronautical Accessories, Inc. External hoist kit PIN 412-150-100 in accordance
with Aeronautical Accessories, Inc. STC SH3189SO and structural 8110-3 by Richard T.
Morgenweck, S0-790, dated November 17, 1995.
Aeronautical Accessories,
Inc. FAA approved rotorcraft flight manual supplement dated
,,.-..,~·.~·:,: -~-.:.~··-Nov,emb'er.'f!'2J;:J]-~~ or later FAA approved·revision is required to be on board with this
r---r~:ti-·-_"·:·-rnst~~tf6ii:J.-t~ - .
,,,.,,,,:.,,.K-_ ...... ,., · .... t .... 4,
"-··t:~J ~; .· .,_ ,.:. ,:: . ,~-~ .
~~'
.
i-c~\ :;:::·-:P11taJle?~..:~11m~Qfter dual flight director (3-axis) PIN 412-706-024 in accordance with
r-+:i~L:..~~l~~~~t~~E~ app~ov~ drawing 41~-706-024. _
Pct·· -_-1re1r);re~~~approved rotorcraft flight manual supplement, BHT-412-FMS-37.4,
~
~cfoctober 18, 1994 or later FAA approved revision is required to be on board with
this installation.
3. Installed Bell Helicopter No. 1 radar altimeter kit PIN 412-706-025 in accordance with
Bell Helicopter FAA/DER approved drawing 412-706-025.
4. Installed Bell Helicopter DME adapter kit
PIN 412-706-046 in accordance with Bell
Helicopter FAA/DER approved drawing 412-706-046.
5.
· Installed Bell Helicopter external cargo suspension and mirror kit PIN 212-706-103-101 in
accordance with Bell Helicopter FAA/DER approved Service Instruction No. 412-17.
Bell Helicopter FAA approved rotorcraft flight manual supplement, BHT-412-FMS-9.3
and 9.4, dated September 15, 1995 or later FAA approved revision is required to be
on
board with this installation.
Weight, balance and equipment list revised.
------~-----~------------~----------------~----~~--------------------------------------------------
O Additional Sheets Are Attached
*U.S.GP0:1994-568-012/00019
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