flint aero inc.

218 Pages·2016·6.46 MB·English

I
f.) Form Approved Electronic Tracking Number
OMB No. 2120-0020
MAJOR REPAIR AND ALTERATION 2/28/2011
US Department For FAA Use Only
of Transportation (Airframe, Powerplant, Propeller, or Appliance)
Federal Aviation
Administration
INSTRUCTIONS: Print or type all entries. See Title 14 CFR §43.9, Part 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for
instructions and disposition of this form. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for each
such violation. (49 U.S.C. §46301(a))
Nationality and Registration Mark Serial No.
N179DM T20609179
I
1. Aircraft
Make Model Series
Cessna T206H
Name (As shown on registration certificate) Address (As shown on registration certificate)
eo
Address BOX ZZ04
2. Owner City Wichita State KS
Cessna Aviation Company Zip 67277 Country USA
3. For FAA Use Only
4. Type 5. Unit Identification
Repair Alteration Unit Make Model Serial No.
D D AIRFRAME (As described in Item 1 above)
D D
POWERPLANl
D D
PROPELLER
Type
D D APPLIANCE
Manufacturer
6. Conformity Statement
A. Agency's Name and Address B. Kind of Agency
I
Name Ebilip Glasgow I U. S. Certificated Mechanic Manufacturer
Address 2533 Dallas Creek Court Foreign Certificated Mechanic C. Certificate No.
City Eoct Collios State Co Certificated Repair Station
Zip 80528 Country USA Certificated Maintenance Organization A&P 3292572 IA
D. I certify that the repair and/or alteration made to the unit(s) identified in item 5 above and described on the reverse or attachments hereto
have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information
furnished herein is true and correct to the best of my knowledge.
Extended range fuel Signature/Date of Authorized Individual
per 14 CFR Part 43 D ~
App. B Philip Glasgow 12/1 /15
.....
...........__
7. Approval for Return to ServiU ./
Pursuant to the authority given persons specified below, the unit identified in ~m 5 was inspected in the manner prescribed by the
Administrator of the Federal Aviation Administration and is []I Approved O Rejected
I
FAA Flt. Standards Manufacturer Maintenance Organization Persons Approved by Canadian
Inspector Department of Transport
BY
Other (Specify)
FAA Designee Repair Station ./ Inspection Authorization ""-...
"'
Certificate or Signature/Date of Authorized Individual
Designation No. v~~
Philip Glasgow 12/1 /15
A&P 3292572 IA
FAA Form 337 (10-06) I Y"
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 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.)
IN179DM I .__l12_-,-1-_~, 1_s
Nationality and Registration Mark Date
Installed Flint Aero Inc. tip tank kit IAW STC SA4366WE. Updated weight and balance records.
----------------------------------------------------------------------END---------------------------------------------------------------------------
[{] Additional Sheets Are Attached
FAA Form 337 (10-06)
~niteh .;Stutes @f ,.Americu
JJf
g)epttdment of '<!rnmsporitttion - ebernl J\&iation J\mninistration
.fiGn-i&p
SA4366WE
,g;w.,~,;,Ps; 4.cak. i.J.Jaer//£.L Flint Aero, Inc.
1942 Joe Crosson Drive
El Cajon, California 92020-1236
Ce.1"4/f~ da~ ~ r..,frz,,~ tr/, uf:e ,r/t.C rfrl.J{p;/'bf, P //k; .,ll,#.6en-£R? /7/<'0r&&d a,;:'/,/{; ufe &.i:IMiff.7..40/1,Jt,' Ult'£
con~ifio.rw- de,~- t'b.J. ¥,ect/'fea ,,ff !/'CO;'I,n u;et:J. //lb (7~/'(DO/'df,//.C,J,J,J "ep<«&M.OU'/lt~:J. ~ 3 * ey~ ~oeif
.Air-~tt?a&4iM,;. and Part 23* t"/de /!hrk,u;C'.Aoe°£r.~eo/1, ..n~&00/1.J. *Certification basis is set
forth in Type Certificate Data Sheet A4CE, Revision 3 7.
A4CE
Cessna
U206F, TU206F, U206G, TU206G, 206H, T206H
!WcJc.l'Vl.40/1,o /.~u;, ~J~" W~.r~e: Installation of 14.9 gallon usable fuel-containing wing tips in accordance
with FAA sealed Flint Aero, Inc. Master Drawing List MDL FA3330, no revision, dated June 18, 1981 or later
approved FAA revisions, or Flint Aero Master Drawing List Number FAOS0-11, Revision "B", dated September 4,
2007, or later FAA Approved Revision. Increase in the gross weight from 3,600 to 3,800 pounds for landplane,
floatplane, amphibian, and ski plane versions of models U206F, TU206F, U206G, TU206G as applicable per TCDS
A4CE and the Flight Manuals. Increase in the gross weight from 3,600 to 3,800 pounds for landplane versions of the
206H and T206H. Flint Aero, Inc. FAA Approved Supplemental Airplane Flight Manual, dated December 7, 1987 for
models U206F, TU206F, U206G, TU206G, or Flint Aero, Inc. FAA Approved Flight Manual Appendix Report, 050.06,
dated July 19, 2001 or Report 050.04, dated July 20, 2001 for models 206H and T206H, or later approved revisions, is
required as part of this installation.
5&:nti~n:&o/1.fJ.7. .nd°Won<'.UUoT/t.h,eJ ,l.i·m itations and conditions of Data Sheet A4CE apply, except as
outlined on page 3 of this STC. (Continued on Page 3)
,9?{,e;e,e. ,t'~ea/e ru.d do #~y?o,/1:r,p mda t0,,{ed ,;s.d o tfaJtJ ,/!,, '¥1/1'"'-"Z.t Malcn.n•am ,:,,.e #,e.tt1 .nt'd' .wv,u,th«t
.Jmy'itYWUd;w, ,,o,&d "" a /l'!;'W.Ut<th:0,n,d 'a/19 ,;>o /AV(DIJ8 e.,/a,{'t/Jed' tf?·I ',(.. .Amn,:r<t:J/ndo, o/ /Xo/ JT~d .Ao,(ru,a,,n,
.A@,uti.>rn£1for1·.
~al~/YJl;;Jae.rL- June 15, 1990, February 25, 2000
August 28, 1981
.!?tfa/19a nu'/116JrL-December 7, 1987, September 7,
2000, October 16, 2001, February 5, 2008
(Signature)
Manager, Airframe Branch
Los Angeles Aircraft Certification Office
(Title)
)lny aCterationo f tfiis certificate is pu11isfia6fe6 y a fine of not e;cr:eed'in$91 ,000, or imprisonment not e;tJ:eed'in39 years, or 6otfi.
FAA Form 8110-J (10-68) Page 1 of 5 'Tliisc ertificatem ay 6e transferred'ina ccord'aruw:ei tli 'F)ltJ{.21.47.
·:,. ., ....,.. .. \
INSTRUCTIONS:'T he'irnnsfer endorsement below may be used 16 notify !he appropriate [,'AA Regional Office of
the transfer of th is Suppl~mental type certificate.
The FAA ivill rdssu~· t~e certificate;i n the name of !he transfereea nd forward it to him.
. l. ,.
TRANSFER ENDORSEMENT
Transfer the ownership of the Supplemental Type Certificate Number -----------
to (:Nameo f transfare_e)_. _
· · (Jl.c{cfreosfs t ra11sfar)
. '('.Nu1116at,ru f st.reel)
'\
(City,S tate, aruf Zit' code)
· · {;!~dresos f grimt or)
Extent of Authority (if licensing agreement):
Date of Transfer: -------------
Signatur~ of grantor (In iu{;).-·-_- ----------------------
~nibb J&mics ®f J\tlU!ricn
JJr
~.epartment .of 'mransp.orhtti.on - .en.em!J \fiiatinn J\oministrnti.on
~uppl.em.ental 'il1Jp.0e1 .ertifirat.e
( <ll.ontinunti.on ~~eet)
./JGn~eP
SA4366WE
REISSUE: 6/15/90, 2/25/00
Limitations and Conditions: (Continued)
The installation should not be incorporated in any aircraft unless it is determined that the interrelationship
between this installation and any previously approved configuration will not introduce any adverse effect
upon the airworthiness of the aircraft.
The approval of this modification applies to the above noted airplane model series only. If the holder agrees
to permit another person to use this certificate to alter the product, the holder shall give the other person
written evidence of that permission. A copy of this STC must be included in the permanent records of each
airplane modified in accordance with this STC.
Fuel Capacity: Noted in Type Certificate A4CE for specific model plus two 15 U.S. gallon (14.9
gallon usable) auxiliary wing tip tanks at (F.S.+53).
Placards: The following placards are required in locations noted:
On instrument panel in clear view of the pilot: "Total wing tip fuel 30 U.S. gallons
(29.8 gallon usable). Transfer fuel during level flight. Transfer fuel when main
tank contains not less than 5.0 gallons and is at least 15.0 gallons below full. Wing
tip fuel switch must be off during takeoff, landing, refueling, and when empty.
Monitor main fuel tank gauge while transferring wing tip fuel to prevent over
filling"
Adjacent to the airspeed indicator: "Reduce V e5M PH per 1,000 above 18,000
0
Feet." (Turbocharged models only).
Forward of each wing tip tank filler: "15.0 U.S. Gallons (14.9 gallon usable)
lOOLL or 100/130 min. grade aviation gasoline."
Adjacent to wing tip fuel tank pump switches: "Wing tip fuel tank pumps must be ·
off during takeoff, landing, refueling and when empty. Monitor main fuel tank
gauge while transferring wing tip fuel to prevent over filling."
At wing tip fuel tank pump switches: "Left (right) wing tip fuel. 15.0 U.S.
gallons. 14.9 gallons usable. On. Off."
Adjacent to each wing tip fuel tank leak detection drain (3 per side): "Fuel or vapor
from drain requires immediate repairs."
}fny a{terationo f tliis certificatei s punisfza6(e6 y a fine of not e,;feedi11$91 ,000, or imprisonmentn ot a;s.eedi1139 y ears, or 6otfi.
FAA Form 8110-2(10-68) Page J of 5 'ITiisc ertificatem ay6 e transferreri!n accortfancwei tfi 'F}f.'1{.21.47.
~nilcll J&tatcs ®£ J'.mcrica
JJ!'
~£pttdnumt of W:rnnsporht±imt - £.O£rttlJ \.&httion J\ominisirnfion
~upp1£m£ntal fil£rtificat£
'{i[~p£
( illontinua:tion ~4eet)
JV~
SA4366WE
REISSUE: 6/15/90, 2/25/00
Limitations and Conditions: (Continued)
Adjacent to appropriate wing tip tank pump circuit breakers or fuses: "Tip
tank L (R) pump."
Gross Weight: 3,800 pounds or 3,600 pounds; see Limitation of Applicability.
Center of Center of gravity range, inches aft of datum.
Gravity:
Forward: 33.0 inches aft of datum at 2,500 lbs. or less, with straight line
variation to 44.4 inches aft of datum at 3,800 lbs. or 42.5 inches aft of datum at
3,600 lbs.
Aft: 49.7 inches aft of datum at all weights.
Reference datum: Front face of firewall at all weights.
Limitation of The approval of this change in type design applies to the basic Cessna 206 series
Applicability: airplanes of the models shown above. Flint Aero, Inc. FAA Approved
Supplemental Flight Manual, dated December 7, 1987, or later approved revisions,
is required as part of this installation on Models U206F, TU206F, U206G, and
TU206G.
Flint Aero, Inc. FAA Approved Flight Manual Appendix, Report Number 050.04 or
050.06, or later FAA Approved revisions, are required as part of this installation
on Model 206H and T206H. The appropriate Airplane Flight Manual selected and
Maximum Takeoff Gross Weight (MTOGW) allowable is dependent upon the
airplane serial number and the status of incorporation of Cessna Aircraft Company
Accomplishment Instruction AI 206-57-01 as shown in the table below.
)111ya [teraticmo f tliis certificate is pu11islia6f6ey a fine of not IJ)(;eed'i11JJg, 000, or imprisonmentn ot e;cr:eecfi3,l (yJe ars, or 6otfi.
PAA Form 8110-2 (10-68) Page 4 of 5 'ITiisc ertificatem ay 6e transferredi1 1a ccortfa11wciet li 'F)ll]t21.47.
~nitd, Ji,t11te1®1 f J\merirn
Jlf'
g).epa:r±numt of 'rn:ra:m,poria:tion - .eb-.eraJl \nintion J\bministrntion
~uppl£nt£ntal tTiyp£fi l£rtifirat£
( aiontinua:tion ~4ed)
./JGni,&P
SA4366WE
REISSUE: 6/15/90, 2/25/00
Limitations and Conditions: (Continued)
Applicability Table
206BJT206H SIN AI 206-57-01 AFM Appendix MTOGW
("T" prefixes included) Incorporated?
20608001-20608059 Not Required FA050.04 3,800 lb.
20608060-20608091 No FA 050.06 3,600 lb.
20608060-20608091 Yes FA050.04 3,800 lb.
20208092-20608100 Not Required FA050.04 3,800 lb.
20608101-20608158 No FA 050.06 3,600 lb.
20608101-20608158 Yes FA050.04 3,800 lb.
20608159 and subs Not Required FAOS0.04 3,800 lb.
-END-
Jln)I afteratit111 of tfris certifaate is puni.rfin6fo 6y a fine ,f nnt •:g:o,dino $1,000, or in,pn"sonrnant not •-'(f•o£n9 3 year., o~ 6otfi.
FAA Form 8110-2 (10-68) Page S of 5 'lTiis certificate may 6e tra11sferreai1a1c confance-witli' FJl.'1{.21.47.
---,w-
A. E R. C> • N C
PERMISSION STATEMENT
This is a Flint Aero Inc. memo and is not part of the STC.
This permission statement is in accordance with Public Law 104-264, Federal Aviation
Reauthorization Action of 1996, which requires Flint Aero to issue a "permission
statement" to whomever we permit the use of the STC.
Permission is hereby granted to: Cessna Aircraft Company
Address of Registered Owner: PO Box 7704, Dept. 095
Wichita, KS 67277
by Flint Aero Inc. to install Flint Aero auxiliary fuel kit Serial Number: 15H-1571C
on Cessna Model: T206H
aircraft serial number: T20609179
in accordance with STC No: SA4366WE
~d--C::::
Signed: -Date: _q...___-._..).J.__..qS __
President, Flint Aero, Inc
Note:
The second page of the STC is intended to transfer ownership of the STC to a new manufacturer. This has
caused some confusion. Your purchase ofour fuel kit includes a copy of the STC but does not transfer
ownership of the STC. To clarify this situation, we have stamped "VOID" across the second page of the copy
of the STC which is provided with the kit you have purchased.
Flint Aero recommends that the installation manual be kept in the aircraft for continued air worthiness
instructions and to aid in troubleshooting. Copies of the installation manual may be purchased from Flint
Aero.
Flint Aero Inc.
1942 Joe Crosson Drive, El Cajon, CA 92020 USA
Voice: [phone] I Fax: [phone] I Website: www.flintaero.com
Listo f effectiveP ages Reada ll instructions
~ before beginning
~
~ -~~
<~; ~"' ~ ...~..~.. ~"' installation.
Applicabmle odelsU: 206FT, U206F,
I cover rev K 9/4/07 U206GT, U206G,206H,T206H
2 installatioinn struclions version5 9/7/ 06
3 installatioinn structions 5 9/7/06 Note": INTr"e fers1 on onr ubber ContinuedA irworthiness
4a notes 4 6/11/04 celle quippeadi rcraft.
4b notes 3 8/4/05 Instructionms ay be foundo n
5 billo fm aterials 5 2/3/07
Thisk iti s configurefdo r·
6 billo f materials 4 2/3/07 sheet 29
tanks erialn umber:
7 billo f materials 4 10/19/04
8 billo fm nlerials 3 9/4/07
aircrafst erialn umber:
9a overalflu ell inep lacemenrte, 5 B/4/05 Noteto installer:
9b overalfl uell inep lacemeni!n, t 4 S/4/05 Anyd eviationosr changebs yi nstalledr uringin stallatiosnh albl e in
10 accessc overs 4 10/19/04 os follows: accordancwei thF AAm anuaAl C4 3.13- 18/2Ao r by FAAFS DOopproval.
II deleted
Mainta nks
12 deleted O bladder
13 sparw eb 4 6/14/04 0 "hard"t onks Thesed rawingssh ouldp hysicallbye kepti n thea ircraft.
14 air ductm odification I 3/18/04 FAAPo rt9 1-417re quiresth att he STCal sor emainw itht he aircraft.
15a fuelp umpin stallationl ,4 v int 4 6/15/04
Turbo
lSb fuelp umpin stallalion2,8 vr e 4 6/15/04 O yes Useo nlyth e typeo fw heelst,i resa ndb rakesth olt hea ircrafwt ~s
15c fuelp umpin stallation2,8 vi nt 4 6/15/04 D no originalleyq uippewd ithf romth e Cessnfaa ctory.
15d fuelp umpin stallationl ,4 v re 4 6/15/04
16 wingc orner/accesCso ver 4 10/19/04
Voltage
17 accessc overd, etail 4 10/19/04 D 14 Thesed rawingos ret he exclusivper oprietaryc,o pyrightepdr opertoyf
18 deleted D 2a FlinAt eroI nc.a ndm ayn otb e reproduceodr usedi na nyw ayo thert har.
19 fuell ines upport 4 6/15/04 expresslyp ermittedb yF linAt eroI nc.
20a electrica1l,4 v 6 9/4/07
Gougse1 yle
20b electrica2l,8 v 6 9/4/07 0 2 gauges II is suggestedth att he Flintta nksb e keptf ullw hent he airplineis on the
s
2la navl ightw ires 6/17/04 0 1d ualg auge groundT. hisw illr educec ondensatioann dp rolongth e lifeo ft hes ending
21b alternateli ghts 4 6/10/04 units.
22 ventl ineb racket 3 6/8/04
Octane
23 ventings ystem 3 6/15/04 D eo/s6
11942Jo e CrossoDn rive
24a plumbinjgu nctionr,e 3 6/15/04 O lOOLL FLINATE RION C.
ElC aionC, A9 2020·
24b plumbinjgu nctionin, t 3 6/15/04 D 100/130
25 fuelo utlet/ribm odification 3 6/8/04 CessnaA uxiliarFyu elS ystem dole:9 /4/07
26 lankm ounlinsgc rews 3 6/10/04 InstallationIn structions,
RevisionK:
27 lanka lignment 2 12/13/06 CoverP age
Installatioins compatiblwe ith
28 stallw arningad justment 2 3/18/04 landplanesa,m phibianfsl,o alplanes, drawnC: LG Ia pprovedD: LH
29 maintenance 3 6/15/04 skiplanesc,a rgop ods,a utopilot FA3330 IS heet1 of3 6
30 placards 4 10/19/04
systemsa ndS TOcLo nversions.
31 index 2 3/18/04 Alld imensionosr ei ni nches
·,
I .Drainfu elf romm aint anks.C AUTIOeNar:t hg rounda ircraftR. eada ll instructionths oroughlayn du nderstandb efores tartingC. heckp artsw ithp artsl ist.
2.lnstalal dditionailn spectiopnl atesa s showo n sheets1 0,1 6a nd 17t o ease installatioonf fuell ines,f uelp umpsa ndw iringA. lle lectricawl iringtp be performedin
accordancwe ithF AAm anuaAl C431:3 -1o r as notedi nt hesed rawingsC. AUTIODNon : otm ounot r contacht ighv oltagew ireso f strobel ightsw ithf uelg auges endingu nit
wires.
3. deleted
4.lnstalfl uelp umpi n accordancwe ithF A333s0h eet 15.R outep umpw iresw ithf actoryn avl ightw ires.D rilnl umbe1r 0h ole( tod etectl eaks)b eneathth e fuelp umpa ndi nstall
F/N8 3.
5.lnstaltlh e fuell inesa ndf uell ineb racketsa ndg rommetsS. ees heets9 and 19.B es uret hat allf uell inesa re cleani nsidef roma nyc uttingos r filingsD. oublsep iralw rap
fuell inef roms tation2 3t o station5 3 on RCe quipedp lanesw ithv inylt ape( F/N8 8)t o preventc hafing.
6.lnstalfl uelg augesi n instrumenpta nel,p edestalo r overd oorsi n a locationsu cht hatt he pilots eateda t the controlcs anm onitotrh e airplane'sf lightp atha ndt he
instrumenwt ithm inimumhe ada nde ye movemenRt. outes endingu nitw iresw ithf actoryn avl ightw ires.I nstallo n/offs witcheasn df usesi n accordancwe iths heet2 0.l nstall
resistor,F /N6 5n eart he fuelg augeo n 24 voltm odels.
7.Removfea ctoryti psa ndn avigatiolni ghts.
(A)H ermeticalslyea lt he navb ulbsa ndt heir mountinbga ses.T hisi s to includea ll lights ocketsa, nyw iringa t connectionins the wingt ip area. UseC oastP roseaol r PRCF uel
TankS ealantC ompounCd.a refullfyo llowa ll manufacturedrsi rectionfso ru sings ealingc ompound.
(BJI nspecat ll wirec ables plicesa ndc onnectortso determinteh at theya re potted,h ermeticallsye aleda ndt hat theya re lockedC. AUTIOTNhe:s trobeh ighv oltagep ower
supplys plicesa ndc onnectorws hicha re deemed" explosionp roof"b utw hicha re opena ndn oth ermeticallsye aleda ndl ockedm ustb e locatedo utsideo ft he fuelt ankz one
preferablyin a dryb aya rea oft he fuselagef ree froma nyp ossiblev apors.
Routew iresf or switcheasn dg augesw ithC essnalo wv oltagew iresi nf actorym ountingisn accordancwe ithF AAre gulationsI.n stallq uickd isconnecfitt tingsa t the junctioonf
the tip tankw iresa ndt he factoryn avl ightw iresa nd sealp er paragraph"( A)"o nt hisp age.
((}D eterminteh at allh olesi n the wingt ip tankl ightm ountinsgu rfacew herew ireso r screwsp enetratet his surfacea re sealedw ithC oastP ros ealo r PRCF ueTl ankS ealant
CompounTda. kec aren ott o plugl eakd etectionh olei n bottomo f navl ightd ryb aya rea.U ses ealantc ompounedq uivalentot MIL-S-88c0l2as sB .( sees heet2 1)
Usea ll abovep recautionasn dp rocedurefso r mountinnga vigatiolnig hts.
8. Installs pard oubler(ss ees heet1 3).
9.Trimth e leadinge dget ip cornert o specificationosn sheet1 6a t station2 08.
I
FLINATE RION C. FA3330
CessnaA uxiliarFyu eSl ystem
Sequencoef i nstallatio(n1 of 2)
Sheet2 of 36 I
date:9 /7/06V ersio5n