fJ FormApproved I ElectronicTra ckingNumber OMSjohnpropst.yolasite.com/resources/337FA...
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fJ FormApproved I Electronic TrackingNumber OMS No. 2120-0020 MAJOR REPAIR AND AL TERATION 212812011 USDepartment ForFAAUse Only ofTransportation (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 fonn. 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. 1. Aircraft N3129E 7AC-6726 Make Model I Series Aeronca 7AC-Conv Champion Name (As shown on registration certificate) Address (As shown on registration certificate) AddressR R 3 Box 24 A 2. Owner City Elizabeth StateWV Propst, John E and Barbara J Zip 26143-9319 Country USA 3. For FAA Use Only "The tedUliaU,datti. ideatmed bmm be IIam bmd to complywilh the applicable aifworthiMM requWli1Ctd8 ad is bImby approved for UIe 0DIy Qlft the above ooscribcd aircraft, wbjcld to eonformily inspection by II pencil! in ~3.7." . !tJ-/7'/~ ~m4:~6 Date Siil""looe of &:: itispeaor: ~00.07 4. Type 5. Unit Identification Repair Alteration Unit Make Model Serial No. D [ZJ AIRFRAME (As described in Item 1 above) 0 0 POWERPLANT D 0 PROPELLER Type D 0 APPLIANCE Manufacturer ! - 6. Conformity Statement A. Agency's Name and Address B. Kind of AgencY Name C William Pancake .JR .f u. S. Certificated Mechanic I Manufacturer AddressRR 4 Box 218 Foreign CertificatedMechanic C. Certificate No. City Keyser State WV Certificated Repair Station Zip 26726 Country USA Certificated MaintenanceOrganization iA&P 2228906 D. I certify Ihatthe 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 infonnation fumished herein is true and correct to the best of my knowledge. Extended range fuel Signature/Date of Authorized Individual per 14 CFR Part 43 U 12 Oct 2012 App. B t..'1./~ fJ~'(\A 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is ~ Approved o Rejected. FAA Fit. Standards Manufacturer Maintenance Organization I PersonsApproved by Canadian Inspector DepartrnentofTransport BY Other (Specify) FAA Designee Repair Station .f Inspection Authorization Certificate or Signature/Date of Authorized Individual Designation No. 1A2228906 o.·V~ p~, 12 Oct 2012 . . FAA Form 337 (10-(£)
Transcript of fJ FormApproved I ElectronicTra ckingNumber OMSjohnpropst.yolasite.com/resources/337FA...
fJ FormApproved IElectronicTrackingNumberOMS No.2120-0020
MAJOR REPAIR AND AL TERATION 212812011USDepartment ForFAAUse OnlyofTransportation (Airframe, Powerplant, Propeller, or Appliance)Federal AviationAdministration
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) forinstructions and disposition of this fonn. This report is required by law (49 U.S.C. §44701). Failure to report can result in a civil penalty for eachsuch violation. (49 U.S.C. §46301 (a»
Nationality and Registration Mark Serial No.
1. AircraftN3129E 7AC-6726Make Model I Series
Aeronca 7AC-Conv ChampionName (As shown on registration certificate) Address (As shown on registration certificate)
AddressR R 3 Box 24 A2. Owner City Elizabeth StateWV
Propst, John E and Barbara J Zip 26143-9319 CountryUSA3. For FAA Use Only
"The tedUliaU,datti.ideatmed bmm be IIam bmd to complywilhthe applicable aifworthiMM requWli1Ctd8 ad is bImby approved for UIe 0DIyQlft the above ooscribcd aircraft, wbjcld to eonformily inspectionby II pencil! in ~3.7." .
!tJ-/7'/~ ~m4:~6Date Siil""looe of &:: itispeaor: ~00.07
4. Type 5. Unit Identification
Repair Alteration Unit Make Model Serial No.
D [ZJ AIRFRAME (As described in Item 1above)
0 0 POWERPLANT
D 0 PROPELLER
Type
D 0 APPLIANCE Manufacturer
!- 6. Conformity StatementA. Agency's Name and Address B. Kind of AgencYName C William Pancake .JR .f u. S. CertificatedMechanic I ManufacturerAddressRR 4 Box 218 ForeignCertificatedMechanic C. Certificate No.City Keyser StateWV CertificatedRepairStation
Zip 26726 CountryUSA CertificatedMaintenanceOrganization iA&P 2228906D. I certify Ihatthe 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 infonnationfumished herein is true and correct to the best of my knowledge.
Extended range fuel Signature/Date of Authorized Individual
per 14 CFR Part 43 U 12 Oct 2012App. B t..'1./~ fJ~'(\A7. Approval for Return to Service
Pursuant to the authority given persons specified below, the unit identified in item 5 was inspected in the manner prescribed by theAdministrator of the Federal Aviation Administration and is ~ Approved o Rejected.
FAA Fit. Standards Manufacturer Maintenance Organization I PersonsApproved by CanadianInspector DepartrnentofTransport
BY Other (Specify)FAA Designee Repair Station .f Inspection Authorization
Certificate or Signature/Date of Authorized IndividualDesignation No.
1A2228906 o.·V~ p~, 12 Oct 2012. .FAA Form 337 (10-(£)
NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must becompatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements.
IN3129E 1112Oct 2012
Nationality and Registration Mark Date
Install J. P. Instruments model EDM 830-4c Engine Data Management system using STC SA2586NM as a reference.This installation is to enhance the aircraft safety, reliability, and performance by providing an additional means formonitoring engine performance data, fuel consumption data, and prediction of fuel endurance. The data system willmonitor EGT, CHT, MAP, Oil Temp, Oil Pressure, Voltage, OAT, Carb Temp, RPM, and %HP in addition to fuelconsumption data.(Note that primary panel mounted oil temperature and oil pressure gauges and tachometer remainoperationaL) This instrument, which includes a fuel flow management system as part of the overall engine datamanagement system, is replacing an existing JPI FS-450 Fuel Flow system that was previously installed on a fieldapproval dated 22 July, 2010. The eXistiQgairY,[9ft fu,~I.sys!~91J!a,~.taD~m~unted~elgauges visible through windowsfrom the cabin to the wing butt ritl,"O.eneActf!,~;iJnQn~j;di5un1tG~b':daiA'~.'.,.:il1$!i~%fi\'~rl.·.EiHgEfld~8CurateIYsee the fuel
- ~~~'.••. ,";f;' ~._~~~.~ '-:".fZ'~;'~).~(.r:.~,_~"':.-.{ts'tl"< c~-·,:._--!~~..•:'h;:..t~~-·-!>·i r2~~,t~1·~->·1i}.i.~.(;'''';;'; ~. I~ 'f,.t~,-.k": Si~1gauges and it is also difficult to accurately de.tet.Jt\iQ.E;}[email protected]\)'Vpjl~;!£f.Vi.Qht,Jhf~fUeJ.ijqwsystem will supplementthe pilot's awareness of fuel used and fuel remaining. Using the $TC asa referefice,:,i~~:t~~Gflow system will beinterfaced with the existing aircraft portable, panel rn~ul'lt~~ qps s~~tem ~o.pr~videadditi~nal trip related fuelconsumption and reserve. In addition to fuel m:at{agemenftliiis;;j@sti'Um:efltw.nr;aIsoenl'fa'fi~lJ,ilot awareness of engineperformance and reliability. It will also monitor and alarm a multitude of engine operating parameters. This installationis a deviation from the STC because this Aeronca 7AC make and model aircraft is not specifically identified in the STCApproved Model List. However, American Champion Aircraft Corporation Models 7GCBC, 7ECA, 7GCBA, 7GCAA, and7KCAB are specifically approved. These approved aircraft are all manufactured under the same Type Certificate A-759as the model 7AC. These AML aircraft are all later versions of the Aeronca 7AC in which electrical systems wereinstalled. The Aeronca 7AC never originally had an electrical system. The Aeronca 7EC was the first Aeronca aircraftmodel to have an electrical system. N-3129E has an upgraded instrument panel already approved under a separatefield approval dated 25 May 2010. N-3129E also has a battery powered electrical system already approved under aseparate field approval dated 25 May 2010. The instructions and recomendations of the STC were all followed for the »
installation of the unit Fuel must be verified in each tank prior to takeoff and during flight.Instruction for continued airworthiness1. Introduction: Installation of engine data monitoring system in accordance with STC.2. Description: Installation of supplemental fuel flow system and engine data system in accordance with STC.3. Control: NfA4. Service Information: During annual/100 hr inspection,check all components, hoses, and wiring for functionality,
security, routing, chafing, and damage.5. Maintenance Instructions: Unit requires 110 ongoing routine adjustments.6. Troubleshooting Information: Troubleshoot in accordance with EDM-830 manual.7. Removal and placement Info: N/A8. Diagrams: Installation and operation in accordance with published STC diagrams.9. Special Inspection Requirements: N/A10. Application of Protective Treatment N/A11. Data: N/A1.2: List of Special Tools: N/A13. For Commuter Category Aircraft: N/A14_ Recommended Overhaul Period: N1A15. Airworthiness Limitation Section: N/A16. Revision: N/A
8. Description of Work Accomplished(If more space is reqotred, attach additional sheets. Identify With aiICraft nationality and registration mark and date work completed.)
END
oAdditional Sheets Are Attac~ed
FAA Form 337 (10-00)
