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VOLPAR
Accessories Required For Smokejumping
Primary Vertical Anchor
Floor Platform MEDC-747- Primary Vertical Static-line Anchor
STC Strength 2000 poundsSTC SA1599NM
Secondary Horizontal Anchor MEDC-758- Volpar Horizontal Anchor Track
STC Strength 750 poundsSTC SA274ONM
Jump Step Attachment MEDC-799- Volpar Step
MEDC-79k- Universal Step Strut
iLjnirzd tara of mnica
Department of transportation jSeral oiation dmini.stration
uppfrmentat gpc ZertIficate
SA1S99NM
United States Forest Service
MEDC BuildingMissoula Montana 59801
cer/ea /XaI/Xe eAanJJzeJyatnfr V/winy/iaa
4aa/eee4a/Aenwnteeh g7 Ci vii
4/lZId_.4fr V4/knhr 765
%zAe Beech
..Za/ 1118 as modified by Volpar BE8I conversion
Installation of staticline anchorcable in accordance with Federal AviationAdministration FM sealed Drawing Number DC741 dated August 1984 FAA approvedJanuary 1985 or subsequent approved revisions
This approval limited to Volpar BE8T conversions This approval should not beextended to other aircraft of this model on which other previously approvedmodifications are incorporated unless it is determined that the interrelationshipbetween this change and any other previously approved modification will introduce no
adverse effect upon the airworthiness of the aircraft
avtA 6oJa n-ea/4Aa/fnwzain e/4bn/di4tb
nnai2aenanotoienz nn w/ n ha.e/Aeneicni/a//aALidAp .c 6a/mZ
June 19 1984
/Ja4.ja4aancc January 1985
..//C .c/sea/w/e-r
Denver Aircraft Certification Office
Northwest Mountain Region Aurora ColoradoTitle
Any alteration of this certificate is punishable by fine of not exceeding $1000 or imprisonment not exceeding 3years or both
This certifiane may be transjned in accordance with FAR 2/ 47
fAAfoog 811021068
USDeParImenINORTHWEST MOUNTAIN REGION
ohranspoctction.j Denver Aircraft Certification Office
L0455 East 25th Avenue Suite 307Federal Aviation
SI
Administration nurOra ora
303 3305575 or 5578
JAN j9
Mr Lee Northcutt Director
Missoula Equipment Development Center USFS
Building Fort Missoula
Missoula Montana 59801
Dear Mr Northcutt
Project No A1O93NMD-S
We have received and reviewed your revised data received by us on December 281984
With these data the conformity inspection and test results of September 261984 performed in Anchorage Alaska you have demonstrated compliance with the
applicable certification regulations Accordingly we have enclosed Supplemental Type Certificate STC SA1S99NM installing staticline vertical anchor
cable in the Volpar BE8T conversion of the Beech H18 series aircraft and
Federal Aviation Administration FM sealed copy of your Top Drawing MEDC
747
This STC is official FAA approval of your installation and may be used to
authorize identical installations on other aircraft of the same model subject
to the limitations noted on the certificate It may be transferred or otherwise made available to another party by means of licensee arrangement in
accordance with Federal Aviation Regulations FAR 21.47 You are requested to
advise this office within 30 days after the transfer when you transfer or grantlicensee rights to the STC in order that we may take the necessary recording or
reissuance action
As recipient of this approval except as provided in FAR 21.3d you are
required to report any failure malfunction or defect in any product or partmanufactured by you that you have determined has resulted or could result in
any of the occurrences listed in FAR Part 21.3c The report should be conununicated initially by telephone to the Manager Denver Aircraft Certification
Office telephone number 303 3405575 within 24 hours after It has been
determined that the failure has occurred In addition written notification to
the Manager ANM170D at the above address is required FM Form 8330-2
Malfunction or Defect Report or any other appropriate format is acceptable in
transmitting the required details
Edward Warren First American Atoll
If you plan to manufacture replacement or modification parts for sale in
conformance with approved data listed on the Certificate you are required to
comply with FAR 21.303 Parts Manufacturer Approval PMA may be issued
under the provisions of FAR 21.303d when you submit statement certifyingthat you have established fabrication inspection system as required by FAR
21.303h The identification requirements for parts produced under PMA are
in FAR 45.15 Your statement may be in letter form with reference to the
STC number and should be addressed to Federal Aviation AdministrationDenver Aircraft Certification Office 10455 25th Avenue Suite 307 AuroraColorado 80012
Sincerely
Woodford Boyce
Manager
Enclosures
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oodfordr BoycejSignaturigerDenver Aircraft Certification Office
Northwest Mountain Region Aurora Colorado
Title
Any alteration of this certjficate is punishable by fine of not exceeding $1000 or imprisonment not exceeding 3years or both
This cer4ficate may be transferred in accordance wa//a FAR 21.47
FAA FoRM 811021068
Thitrd totrs of mnko
Fepartmcnt of Eransportation JednaI 2thation dminiztration
upptrniental ttpr rrtiatc
SA274ONM
United States Forest Service
MEDC Building Fort Missoula
Missoula Montana 59801
a/A.e Civil Al
4zSd-as/knh 765
Lute Beech
1118 as modified by Volpar BE8T conversion
Installation of overhead cargodropper tether anchor in accordance with
Federal Aviation Administration FAA sealed Drawing Number MEDC758 dated
September 1985 FAA approved March 20 1986 or subsequent approved revsions
This approval should not be extended to other aircraft of this model on
which other previously approved modifications are incorporated unless it is
determined that the interrelationship between this change and any other
previously approved modification will introduce no adverse effect upon the
airworthiness of the aircraft
P2LqfAy4%cahoQv November 25 1984
March 20 1986
INSTRUCTIONS The transfer endorsement below may be used to notify the appropriate FAA Regional Office of
the transfer of this Supplemental Type Certificate
The FAA will reissue the cenificate in the name of the transferee and forward it to him
TRANSFER ENDORSEMENT
Transfer the ownership of Supplemental Type Certificate Number
to Name of transferee
Address of transfereeNumber and Street
City Stale and ZIP cade
from Name of granto Print or type
I.
Address of grantorNumber and street
City Stale and ZIP csde
Extent of Authority if licensing agreement
Date of Transfer __________________
Signature of grantor In ink
NORTHWEST MOUNTAIN REGION
u.spartment Denver Aircraft Certification Office
oflransportation 10455 East 25th AvenueSuite 307
FederalAviatlon Aurora Colorado 80010
Administration 303 340-5575 or 5578
MAR 1986
U.S Forest Service
MEDC Building Fort Missoula
Missoula Montana 59801
Gentlemen
Project No A1197NMD-S
We have completed our evaluation of your supplemental type certificate STCproject and find that you have satisfactorily demonstrated compliance with
the applicable certification regulations Accordingly we have enclosed
STC No SA274ONM for the installation of overhead cargodropper tether anchor
in Beech H18 as modified by Volpar BE8T conversion
This STC is official FAA approval of your installation and may be used to
authorize identical installations on other aircraft of the same modelsubject to the limitations noted on the certificate It may be transferred
or otherwise made available to another party by means of licensee
arrangement in accordance with Federal Aviation Regulations FAR 21.47 You
are requested to advise your local office within 30 days after the transfer
when you transfer or grant licensee rights to the STC in order that we maytake the necessary recording or reissuance action
As recipient of this approval except as provided in FAR 21.3d you are
required to report any failure malfunction or defect in any product or partmanufactured by you that you have determined has resulted or could result in
any of the occurrences listed in FAR Part 21.3c The report should be
communicated initially by telephone to the Manager Denver Aircraft Certification Office telephone number 303 340-5575 within 24 hours after it has
been determined that the failure has occurred In addition written notification to the Manager ANM-100D at the above address is required FAA Form
8330-2 Malfunction or Defect Report or any other appropriate format is
acceptable in transmitting the required details
1936
_____ -5O Years of Air Traffic Control Excellence
Standard for the World
If you plan to manufacture replacement or modification parts for sale in
conformance with approved data listed on the Certificate you are required to
comply with FAR Part 21.303 Parts Manufacturer Approval PMA may be
issued under the provisions of FAR 21.303d when you submit statement
certifying that you have established fabrication inspection system as
required by FAR 21.303h The identification requirements for parts
produced under PMA are in FAR 45.15 Your statement may be in letter formwith reference to the STC number and should be mailed to the address
indicated above
Sincerely
Ioodford Boyce
Manager Denver Aircraft
Certification Office
Enclosure
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