on

.1-1

3_i

BEECH 90

Accessories Required For Smokejuinping

Primary Floor Anchor MEDC-617- Anchor cable for Beech 90 99 100200 Nomad N24A Series Aircraft

STC Strength 2000 poundsSTC 5A566NW

Other Accessories MEDC-643- Handrail Wind Deflector for Beech

90 99 100 200 Series AircraftMEDC-64L1 Floor Panels for Beechcraft 90 99

100 200 Series Aircraft

Jump Step Attachment Jump step not used on Beech 90

Note There is no secondary anchor design for the Beech 90

BEECH 99A

Accessories Required For Smokejumping

Primary Floor Anchor MEDC-617- Anchor cable for Beech 90 99 100200 Nomad N211A Series Aircraft

STC Strength 2000 poundsSTC 5A566NW

Secondary Anchor MTDC-809- Horizontal Anchor Track for Beech

99ASTC Strength 750 poundsSTC // SA4O47NM

Other Accessories MEDC-643- Handrail Wind Deflector for Beech

90 99 100 200 Series AircraftMEDC-644 Floor Panels for Beechcraft 90 99

100 200 Series Aircraft

Jump Step Attachment MEDC-759- Stepbasket universal SmokejumperAircraft

MEDC-794- Universal Step Strut

MEDC-785 Jump Step Attachment Points Beech

99

Note The Beech 99 requires door brace

between the aft air stair door and the

forward jump door Contact MTDC for

information about this accessory

KING AIR 200

Accessories Required For Smokejumping

Primary Floor Anchor MEDC-617-- Anchor cable for Beech 90 99 100200 Nomad N24A Series Aircraft

STC Strength 2000 poundsSTC SA566NW

Secondary Anchor Pending

Other Accessories MEDC-6k3- Handrail Wind Deflector for Beech

90 99 100 200 Series AircraftMEDC-644 Floor Panels for Beechcraft 90 99

100 200 Series Aircraft

Jump Step Attachment MEDC-759- Stepbasket universal SmokejumperAircraft

MEDC-79k- Universal Step Strut

Note Contact MTDC for information about

step attachment configuration for the KingAir 200

Uffltcd rrs ol 2lmnica

Bcpartmcnt of transportation fdcral Uiation quministration

upptcnicntat fl.jpc rdfiQtc

SA566NW

Forest Service

/A/ 4e cLyein /L /y/ ..c/J /e.r /L//Z11..7/i ÆIX1v11z1-

eL /4 nwv.r41.t 4..ry1non4nL i/./ /4

See attached Master Eligibility List MELrjn1nn/.5t.A4e/__5e r//n/ fn/ No SAS66NW for list of approved aircraft

models and applicable airworthiness regulations

/.iy///Ly /ny Installation of Parachute Deployment Static LineAttachment System in accordance with U.S Forest Service Specification and Installation Instructions and Drawing MEDC617 Sheets and

NOTE The static line andanchors are attached to the Beech Aeroquip R.H Seattrack

.hnaI1uzna The approval of this change in type design applies basicallyto the above model aircraft only This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporatedunless it is determined that the interrelationship between this change and any ofthose other previously approved modifications will introduce no adverse effect uponthe airworthiness of that aircraft copy of this Certificate Addendum No SAS66NWand MEL No 5A566NW shall be maintained as part of the permanent records for themodified aircraft

4n//iA1/ie-.-hey xZnt .a4a/aa./q/z4v-eta/4Aani.ze1c/.ztnh/2ar-

et4i Ja/te.ne44te.eei-r nn ah.nea44.tie4onc.ce.cJ/ad/JA-e.dJy

/Ae ./acs/ni/...r/

4e

4iiee/y0%az.n January 25 1978 9n/e sjan/

Ss11/a41n1o March 27 1978 July 14 1982

.4xLC/e..n 4//L p4Mark Baldwin SiAti1ur ChiefDenverAircraft Certification Field OfficeNorthwest Mountain Region Aurora CoJnrado

il/c

.4 ny alteration of/his certificate is punishable /i line of riot exceeding SI .000 or iniprisoniiient riot exceeding rears oi both

FAA Fov.Bi 021068his ccc li/calr mar tracts/cr red ii dance au/i b.l .47i ortic

DEPARTMENT OF TRANSPORTATIONFEDERAL AVIATION ADMINISTRATION

NORTHWEST MOUNTAIN REGIONDenver Aircraft Certification Field Office

10455 East 25th Avenue Suite 301

Aurora Colorado 80010

303 340-5302 or 5569

July 14 1982

USDA Forest Service

Equipment Development Center

Building Fort Missoula

Missoula Montana 59801

Gentlemen

Project No A687RM-S

We have satisfactorily completed our evaluation of the amendment to Supplemental Type Certificate SIC SA566NW The STC has been amended to increase

the maximum allowable load on the static line anchor cable to 2420 poundsAlso Item II on the Master Eligibility Listing MEL was amended to include

the Beech Model Series lO0aircraft The specification and installation instructions have also been amended to increase the load to 2420 pounds and

include statement concerning the slack in the cable assembly

copy of the amended certificate MEL and installation instructions are

enclosed Please return your previously issued SIC to this office for

cancell ation

As recipient of this approval except as provided in Federal Aviation Regulations FAR Part 21.3d you are required to report any failure malfunc

tion or defect in any product or part manufactured 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 telephoneand subsequently in writing to the Chief Denver Aircraft Certification

Field Office ANM-170D at the telephone number and address indicated aboveThis first contact shall take place within 24 hours after it has been determined that the failure required to be reported has occurred Federal Aviation Administration Form 8330-2 Malfunction or Defect Report or any other

appropriate format is acceptable in transmitting the required details

If you plan to manufacture or sell parts for installation on type certifica

ted aircraft please review FAR Part 21.303 which is applicable to replacement and modification parts Applications for Parts Manufacturer Approval

may be made in letter form listing the following information partname part number SIC number model or type certificated producton which the part will be installed and statement certifying that

fabrication inspection system has been established in accordance with FAR Part

21.303h This application should be mailed to the address indicated above

Sincerely

_1 OJLAi2 AjMark Baldwin

Chief Denver Aircraft

Certification Field Office

Enclosures

initrd Starts of gmca

cpartmcnt of transportationf cdcral Uiadon dministradon

upplcintat Ctjpe rtiatcQtontinuation hcct July 14 1982

SAS66NW

SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO SA566NW

The conditions and limitation of Type Certificate Data Sheet Nos 3A20 A14CE

and A24CE apply except where superseded by the following

This Supplemental Type Certificate Data Sheet which is part of STC SAS66NWprescribes the conditions and limitations under which the product for which the

STC was issued meets the airworthiness requirements of the Federal Aviation

Regulations

SUPPLEMENTAL TYPE CERTIFICATE HOLDER United States Forest Service

BEECH MODEL SERIES 90 99100 AND 200 AS MODIFIED BY STC SA566NW

Airframe No change

Engines No change

Performance No change

Limitations No change

Placards The following PLACARDS must be located near the Cargo Door that

reads

THE MAXIMUM ALLOWABLE LOAD ON THE STATIC LINE ATTACH CABLE

15 2420 POUNDS IN TYPICAL PARACHUTE DEPLOYMENT CONFIGURATI ON

THE CABLE STOP MUST BE ADJUSTED ALONG THE LENGTH OF THE

CABLE SO THAT THE PARACHUTE DEPLOYMENT BAG CANNOT TRAIL AFT

OF THE HORIZONTAL STABILIZER

NOTE determination was made that Supplemental Type Certificate SAS66NW does

not effect aircraft performance therefore no Airplane Flight Manual

Supplement change was deemed necessary

END

Any alteration of thiscertijicate

is punishable by fine of not exceeding $1000 or inprisonnient not exceeding years in bath

FAA FORM 8110-2-1 1069 Tb crLjicae may be znnLIcrrei Ifl 12Cc ii dance ck 2/U

PAGE OF PAGES

FAA AC 72-28.51

SPECIFICATION AND INSTALLATION INSTRUCTION

FOR SMOKEJUMPER STATIC LINE ANCHOR CABLE FOR

BEECHCRAFT MODELS 90 99 100 AND 200 SERIES AIRCRAFT

Part Load

Static Line Anchor Cable 242O

ll Load applied in typical parachute deployment

configuration with static line routed throughthe carabiner on the rear anchor

Parts are fabricated as illustrated in drawing MEDC-617 sheets and All

welding is by the arc process Assembled anchor units are installed in theaircraft right hand seat track with the one using Part 24 side brace placed

opposite the door used for jumper deployment Cable length between anchors

shall be of adequate length to allow all jumpers to attach their deploymentstatic line without having to move aft in the cabin This will facilitate

emergency evacuation The cable assembly shall be installed with inches of

slack measured in extreme spread Part 18 the cable stop must be adjusted

along the length of the cable so the parachute deployment bag cannot trail aft

of the horizontal stabilizer

All assemblies fabricated from steel are to be painted with zinc chromate P-27

or equivalent corrosion protecting prior to intallation in the aircraft

Amended July 14 1982

FA PPROVED

MASTER ELIGIBILITY LISTING NUMBER SA566NW

FOR

PARACHUTE DEPLOYMENT STATIC LINE ATTACHMENT SYSTEM

U.S FOREST SERVICE

DATE March 2/ 1978

65-90 65-A9O65-A90-165-A90-2

65-A90-365-A90-4

890 C90 E9O

99 99A A99

A99A 899 100

A100 A100AA100C 8100

200 A200OOT

H18 E18SC-45G C-45H

CAR eff May 15 1956

w/Amendments

See T.C 3A2O page 24

for details

Part 23 dated 2/11/65w/Amendments

See T.C A14CE page 15

for details

Part 23 dated 2/1/65

w/Amendments

See T.C A24CE Pagefor details

CAR 03 111345CAR 11-149 as

amended by 3-14

U.S Forest Service

Dwg No MEDC-617

Sheets

U.S Forest Service

Dwg No MEDC-617Sheets and

TM AIRCRAFTMAKE

AIRCRAFT

MODEL

ORIGINAL

TYPECERTIFICATE

NUMBER

CERTIFICATION

BASIS

FORALTERATION

FM SEALED

DRAWING/DRAWING LIST

AFM

SUPPLEMENT

NUMBER/DATE

MEL

AMENDMENT

DATE

NUMBER REV

Beech

Beech

Beech

Beech

3A 20

Rev.32

A14CE

A24CE

A-765

July 14 1982

April 12 1979

July 29 1982

DEPARTMENT OF TRANSPORTATIONFEDERAL AVIATION ADMINISTRATION

NORTHWEST MOUNTAIN REGIONDenver Aircraft Certification Field Office

10455 East 25th Avenue Suite 307

Aurora Colorado 80010

303 340-5302 or 5569

USDA Forest Service

Equipment Development Center

Building Fort Missoula

Missoula Montana 59801

Gentlemen

Project No A68JRM-S

We have satisfactorily completed our review of your drawing MEDC-617 revision sheets and

Sheet has been revised since the issuance of the amendment to Supplemental

Type Certificate STC 5A566NW dated July 14 This revision added the

length of the anchor cable and changed Note to increase the cable assemblyslack from to inches This change on the drawing necessitates an amendment to the Specification and Installation Instruction

Enclosed is Federal Aviation Administration approved copy of the Specification and Installation Instruction dated July 29 1982 and drawingMEDC617 Please return your previously issued STC to this office for cancellation

Sincerely

iT

J%I1fl9 1OQi%JIJ

MEOC

Woodford Boyce

Acting Manager Denver Aircraft

Certification Field Office

Enclosures

SPECIFICATION AND INSTALLATION INSTRUCTION

FOR SMOKEJUMPER STATIC LINE ANCHOR CABLE FOR

BEECHCRAFT MODELS 90 99 100 AND 200 SERIES AIRCRAFT

Part Load

Static Line Anchor Cable 2420 1/

1/ Load applied in typical parachute deploymentconfiguration with static line routed throughthe carabiner on the rear anchor

Parts are fabricated as illustrated in drawing MEDC-617 sheets and All

welding is by the arc process Assembled anchor units are installed in the

aircraft right hand seat track with the one using Part 24 side braceplaced opposite the door used for jumper deployment Cable length between

anchors shall be 76 1/2 inches The cable assembly shall be installed with

inches of slack measured in extreme spread Part 18 the cable stopmust be adjusted along the length of the cable so the parachute deployment

bag cannot trail aft of the horizontal stabilizer

All assemblies fabricated from steel are to be painted with zinc choromate

P27 or equivalent corrosion protection prior to installation in the aircraft

Amended July 14 1982

Amended July 29 1982

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Unitrd tatts of innta

3epartmcnt of rransportation JTcdcral 2Uiation dministradon

upptemcntal tijpc Zertulkatc

SA4O47NN

USDA Forest ServiceMissoula Technology and Development Center

./Aen/-i- 23 d/zZeFederal Aviation

CE

Beech

9A

.12

Installation of horizontal anchor track and tether system for cargospotter

This approval should not be extended to other aircraft of thismodel on which other previously approved modifications are incorporatedunless it is determined that the interrelationship between this changeand any other previously approved modification will introduce no adverseeffect upon the airworthiness of the aircraft

9%cahnvOctober 31 1988

Ja/ee/aja4zncc April 25 1989

c7P/rn JAocCI%nnthhw-h

MICHAEL BORF gaat SupervisorDenver Aircraft Certification Field OfficeNorthwst Mountain Pnginn Aiirnra nlorado

Tide

tiny alteration of/his cer4/icate is punishable by a/inc of not exceeding Sl000 or zznpnsonment not exceeding Syears Or both

This certificate may be transferred in accordance wit/i FAR 21.47FAA FoRM 81102 10 68

NORTHWEST MOUNTAIN REGIONUSoeportment Denver Aircraft Certification Pield OfficeoTransportotion 10455 East 25th Avenue Suite 307FederalAviation Aurora Colorado 20010Administration 3033705575

April 25 1989

USDA Forest ServiceMissoula Technology and Development Center

Building No Ft Missoula

Missoula Montana 59801

Project No ANM-lOOD--0l88

Gentlemen

We have completed our evaluation of your Supplemental TypeCertificate STC project and find that you have satisfactorilydemonstrated compliance with the applicable certification

regulations Accordingly we have enclosed STC No SA4O47NM datedApril 25 1989 for the installation of horizontal anchor trackand tether system for cargo spotter in Beech Model 99A

This STC is official FAA approval of your installation and may beused to authorize identical installations on other aircraft of thesame model subject to the limitations noted on the certificateIt may be transferred or otherwise made available fo another partyby means of licensee arrangement in accordance with FederalAviation Regulations FAR 21.47 You are requested to advise yourlocal office within 30 days after the transfer when you transferor grant licensee rights to the STC in order that we may take the

necessary recording or reissuance action

As recipient of this approval except as provided by FAR 21.3dyou are required to report any failure malfunction or defect in

any product or part manufactured by you that you have determinedhas resulted or could result in any of the occurrences listed inFAR 21.3c The report should be communicated initially bytelephone to the Supervisor Denver Aircraft Certification FieldOffice telephone number 303 3405575 within 24 hours after ithas been determined that the failure has occurred In additionwritten notification to the Supel-visor at the above address is

required FAA Form 8010-4 Malfuncticn or Defect Report or anyother appropriate format is acceptable in transmitting the requireddetails

If you plan to manufacture replacement or modification parts forsale in conformance with approved data listed on the Certificateyou are required to comply with FAR Part 21.303 PartsManufacturer Approval PMA may be issued under the provisions ofFAR 21.303d when you submit statement certifying that you haveestablished fabrication inspection system as required by FAR21.303h The identification requirements for parts producedunder PMA are in FAR 45.15 Your statement may be in letterform with reference to the STC number and should be mailed tothe address indicated above

Sincerely

Michael Bor itzSupervisor Denver Aircraft Certification

Field Office

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