SUPPLEMENTAL TYPE CERTIFICATE 10051939
CESSNA 172C · Supplemental Type Certificate
Overview
This document is a Supplemental Type Certificate (STC) issued by the European Aviation Safety Agency (EASA) for the installation of the J.P. Instruments Primary Engine Data Management System in various models of the Cessna 172 series. The STC certifies that the design change meets the applicable Type Certification Basis and environmental protection requirements. The document outlines the limitations and conditions for the installation, ensuring that the airworthiness of the aircraft is maintained. It is intended for aircraft owners, maintenance personnel, and operators who are considering or planning to install the specified engine data management system in their Cessna 172 aircraft.
- The STC is for the installation of the J.P. Instruments EDM 900/930 in Cessna 172 models.
- The certification is valid as of January 19, 2015.
- Installation must comply with the JPI Installation Manual dated September 9, 2004.
- Prior to installation, assess compatibility with existing modifications to ensure airworthiness.
- The STC does not change the original environmental protection requirements.
Document
Source
Originally published by www.jpinstruments.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Year
- 2015
- Pages
- 11
- File size
- 1.8 MB
- Publisher
- www.jpinstruments.com
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172C.
CESSNA 172C for sale now
Free — save the 172C to your watchlist and track it in one place.
More CESSNA 172Cmanuals & documents
See all 29 →- Approved Model List For ETX900-TSO Battery InstallationType Certificate
- Service Bulletin SB-12Service Bulletins
- Special Inspection Policy ManualTraining Manual
- CRIMINAL OFFENDER RECORD INFORMATION (C.O.R.I.)Other Documents
- FAA Approved Airplane Flight Manual Supplement for Aerocet Model 2200 Seaplane Float Installation on Cessna Model 172 to 172P and F172D to F172P with Tricycle GearFlight Manual
- Aircraft Weight and Balance ControlPilot's Operating Handbook
- APPROVED MODEL LIST (AML) SA02594SE FOR INSTALLATION OF THE SKYVIEW HDX INSTRUMENTATION AND AUTOPILOT SYSTEMFlight Manual
- SUPPLEMENTAL TYPE CERTIFICATE - 10059692 REV. 1Supplemental Type Certificate
- HAWAII ARMY NATIONAL GUARD (HIARNG) BUILDING 621 RENOVATION AND LATRINE IMPROVEMENTSSpecifications
- Best Glide Speed and DistanceOther Documents
- Single Engine Service Bulletin SEB07-5 Revision 6, Pilot and Copilot Secondary Seat Stop InstallationService Bulletins
- 172 Preflight ChecklistChecklist
If you fly the CESSNA 172C, you may also be researching these.
In this document
Description of Design Change
The STC covers the installation of the J.P. Instruments (JPI) Primary Engine Data Management System, specifically the EDM 900 and EDM 930 models. This installation is intended to enhance the monitoring and management of engine data for improved operational efficiency.
EASA Certification Basis
The certification basis for the original Cessna 172 product remains applicable to this STC approval. The environmental protection requirements, including certified noise and emissions levels, are unchanged and must be adhered to during operation.
Limitations and Conditions
Before installing the design change, it is necessary to assess the interrelationship between this change and any previously installed modifications or repairs. This assessment is crucial to ensure that no adverse effects on the airworthiness of the aircraft are introduced.
Associated Technical Documentation
Installation must be performed in accordance with the JPI Installation Manual for the EDM 900/930, dated September 9, 2004, and operation must follow the JPI Flight Manual Supplement for the EDM-900 and EDM-930, dated December 10, 2004.
Safety notes
- Ensure that the installation does not adversely affect the airworthiness of the aircraft.
Full document text
EASAEuropean Aviation Safety Agency SUPPLEMENTAL TYPE CERTIFICATE 10051939 This Supplemental Type Certificate is issued by EASA, acting in accordance with Regulation (EC) No. 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to J.P. INSTRUMENTS, INC P.O.BOX. 7033 HUNTINGTON BEACH CA 92646 USA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and environmental protection requirements when operated within the conditions and limitations specified below: Original Type Certificate Number: SEE EASA APPROVED MODEL LIST Type Certificate Holder : SEE EASA APPROVED MODEL LIST Type Design - Model : SEE EASA APPROVED MODEL LIST Description of Design Change: Installation of J P Instruments (JPI) Primary Engine Data Management System. EASA Certification Basis: The Certification Basis (CB) for the original product remains applicable to this certificate! approval. The requirements for environmental protection and the associated certified noise and! or emissions levels of the original product are unchanged and remain applicable to this certificate! approval. See Continuation Sheet(s) For the European Aviation Safety Agency, Date of issue: 19 January 2015 Head of G neral Aviation and Remotely Piloted Aircraft Systems (RPAS) Note; The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 SUPPLEMENTAL TYPE CERTIFICATE - 10051939 - J.P. INSTRUMENTS, INC TE.STC.00091-003 - Copyright European Aviation Safety Agency. AN rights reserved. 1/2 EASAEuropean Aviation Safety Agency Associated Technical Documentation: Installation in accordance with JPI Installation Manual for the EDM 900/930, Report 908, dated September 9, 2004. Operation in accordance with JPI Flight Manual Supplement ref EDM-900 and EDM-930, Primary Engine Data Management System, dated December 10,2004, Document Numbers 900-0001 and 930-0001 Rev C respectively. or later revisions of the above listed documents approved by EASA in accordance with EASA ED Decision 2004/04/CF (or subsequent revisions of this decision)” and! or the Technical Implementation Procedures of EU! USA Bilateral Agreement. Limitations!Conditions: Prior to installation of this design change it must be determined that the interrelationship between this design change and any other previously installed design change and! or repair will introduce no adverse effect upon the airworthiness of the product. - end - Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 SUPPLEMENTAL TYPE CERTIFICATE - 10051939- J.P. INSTRUMENTS, INC TE.STC.00091-003 - Copyright European Aviation Safety Agency. All tights reserved. 2/2 --- I ji1iJJ11ITi Item AIRCRAFT MAKE A1%T MODEL . TYPE CRTIF)CAIIOF CERTIFICATE ASlS FOR ,u}sIglILft NUMBER CHANGE — 1. AERMACCHI SpA. 5.208, 5.208A EASA.A.587 FAR 21.29 2. AERMACCHI SpA. F.260, F.260B, F.260C, F.26U0. F.2i0E, :.2(;[)F EASA.A.586 CAR 3 FAR 23 3. (AERO COMMANDER) 100-180 (Aero Commander) 1A21 CAR 3 4. AIR TRACTOR AT-301 with STC SA01583CH A9SW FAR 21.25(a)(1) 5. Air Tractor AT-401, AT-401A, AT-401B, AI-402, AT-402A, AT-402B, with STCSAO1583CH A17SW FAR 21.25(a)(i) American Champion 7ECA, 7GCBC, 7GCAA A-759 CAR 4a 6. (Bellanca)(Champion)(Aeronca) 8GCBC, 8KCAB 7. American Champion (Bellanca)f Champion) A21CE FAR 23 Also 8GCBC with SIC 5A02990CH 8. AUGUSTAIR (Morrisey, Varga) 2150A 4A19 CAR 3 A-i, A-lA, A-lB. A-iC-isO, A-C-200. 9. Aviat Aircraft, Inc. EASA.IM.A.294 FAR 23 Also A-i, A-lA, A-lB with STC SAO2O23CH or SA014465E. Also A-lB with STC SA1O463SC. Also A4, A-lA, A-1B, A-1C-180, A-1C-200 with STC SAO287OCH 10. Aviat Aircraft, Inc. S-2B A850 FAR 23 11. Beechcraft 19A, Bl9, A23-19, M9A, C23, A24R, B24R, C24R A1CE CAR 3 EA;tl i.ppro’r!U Mod& List (AML) .tIi! 1939 ].P. STF.JI1ENTS, INC ¶1 Note: The following numbers are listed on the certifi:te: EASA current Project Number: 0010033200-001 STC API’ROVAL —10051939 —J.P. INSTRUMENIS, INC — EASA Approved Model List .‘li L 1/9 EASA Approved Model List (AML) 10051939 i.P. INSTRUMENTS, INC Note: The following numbers are Iiste1 on the certificate: EASA current Project Number: 0010033200-001 SIC APPROVAL — 10051939 —J.P. INSTRUMENTS, INC — ESA Approved Model List (AML) 2/9 N \ \ \ \ \ \ \ \ N ¶1 ;r i1fti1tll.fflIllffli1 TYPE CERTIFICATION Item AIRCRAFT MAKE 1fliH1ttTH{Iftll AIRCRAFT MODEL 4JI i bh4tTt1H9 CERTIFICATE BASIS FOR fjPfflllH l11ii UIP!IJW )1UMBER CHANGE 35-33, 35-A33, 35-B33, 35-C33, E33 F33, E33A, E33C, 35-C33A, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, \i3!A ‘j3!EI, i(, t\36, G36, A36TC, B36TC Also 35-33, 35-A33, 35-333, 35-C33, E33, F33 with STC 5A09603SC. Also G33 with SIC 5A686CE. Also 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, S G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V358, 36, A36 STC 5A22005W. Also A36, 535, V35, V35A, V35B, E33A, E33C, 35-C33A, F33A, F33C with STC 5A1835S0. Also 36, 12. Beechcraft A36 with STC SA2682NM. Also E33A, E33C, 35-C33A, 535, V35, V35A, V35B, F33A, F33C, 36, 3A15 CAR 3 A36 with SIC SAIO145SC. Also 35-C33A, 36, A36, E33A, F33A, G33, S35, V35, V35A, V3SB, A36TC, B36TC with STC 5A5223NM. Also 36, A36, with STC SA2682NM or 5A493CH. Also F33A, A36, 36, S35, V.15, V3SA, V35B with STC SA86765W. Also 35, V35, V35A, V35B, 35C33A,
Show full textShow less
E33A, E33C, F33A, F33C with STC SA2556WE. Also 36, A36, S35, V35, V35A, V3SB, F33A, F33C with STC SA 762N W. Also 535, V35, V35A, V35B with STC SA1O3SWE. Also 535, V35, V35A, V35B, 35-C33A, E33A, E33C, F33C, G33, 36, and A36 with STC SA096195C. Also 35-33, 35-A33, 35-333, 35-C33, E33 and F33 with SIC 5A5527SW. 150, 150A, 1503, 150C, 150D, 150E, 150F, 150G, TSOH, 150], 150K, A1SOK, 150L, A15OL, 150M, A1SOM, 152, A152 13. CESSNA 3A19 CAR 3 Also 150, 150A, 1503, 150C, ThUD, 150E, 150F, 1SOG, 150H, 150], 150K, A15OK, 150L, A15OL, 150M, A5OM, 152, A152 with SIC SA47955 W or 5A3788NM 14. CESSNA F15OF,F1SOG,F15OH, F1501, F5OK, F150L, F15OM, F152, FA152, FA15OK, FA5OL, FA15OM, A13EU CAR 3 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 EASA Appraved ModEi List (AMI) 1OO51339 J.P. INSTRUMENTS, INC SIC APPROVAL — 10051939 — J.P. INSTRUMENTS, INC — EASA Approved Model List (AM) ¶1 — l I11 iIf TYPE CERTIFICATrON Item AIRCRAFT MAKE ${ AIRCRAFT MODE11j I cJ 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 1721, 172K, 172L, 172M, 172N, 12P. 1720. Also 172B, 172C, 172D, 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N, 172P, 172R 15 CESSNA with SIC 5A44285W. Also 172, 172A; 172B, 172C, 172D, 172E, 172F, 172G. 172H with SIC 3A12 CAR 3 . 5A004615E. Also 1721, 172K, 172L, 172M with STC 5A1225CE. Also, 172M, 172N, 172P FAR 23 with STCSA7O3GL. Also172D, 172E, 172F, 172G. 172H, 1721, 172K, 172L,172LM, 172N, 172P with STC SA2196CE. Also 1721, 172K, 172L, 172M with SIC 5A23755W-D. Also 172, 172A, 172 B, 172C, 172D, 172E, 172F(USAF T-41A), 172G. 172H (USAF T-41A), 1721, 172K, 172L, 172M, 172N with SIC SA8O7CE. Also 172, 172A with SIC 5A02282AK 16. CESSNA 172R, 1725. Also 172R with STCSA4428SW EASA.IM.A.051 CAR3 17 CESSNA CESSNA F172D, CESSNA F172E, CESSNA F172F, CESSNA F172G, CESSNA F172H, CESSNA CAR 10 . F172K, CESSNA F172L, CESSNA F172M, CESSNA F172N, CESSNA F172P, CESSNA FP172D CAR 3 18. CESSNA Cessna FR172E, Cessna FR172F, Cessna FR172G, Cessna FR172H, Cessna FR172i A18EU FAR 21 29 175, 175A, 175B, 175C, P172D, 172RG, R172E, R172F, R172G, R172H, R172K 19. CESSNA Also 175, 175A, 175B, 175C with SIC 5A02282AK or 5A02343AK. Also R172K with SIC 3A17 CAR 3 5A1437CE. Also 175, 175A, 175B, 175C, P172D, R172E with SIC SA777CE 177, 177A, 177B 20. CESSNA A13CE FAR 23 Also 177 with SIC SA9O6CE 177RG 21. CESSNA A2OCE FAR 23 Also 177RG with STC SA838NE or 5A4081NM or SA109445C 22. CESSNA CESSNA F177RG A26EU FAR 23 3/9 CERTIFICATIONIm BASS FOR CUANGE 1> CAR 3 \ .\ EASA Approved Model List (AML) 10051939 J.P. INSTRUMENTS, INC 4)J)Jl ‘ .. s . .,, . . Item AIRCRAFT MARE thU{tJf{1{ T ML CEJRE 180, 180A, 1808, 180C, 18CC 80E, 180F, 1806, 180H, 180J, 180K Also 180, 180A, 1808, 180C, 18OD, 1$0E, 180F, 1806, 180H, 180J, 180K 23. CESSNA with STCSAOO468WI orSAOO785ATorSAOO53I WI orSAO9132SC or SAO9O55SC or 5A6 SAO9O18SC or 5A89505 W or SA8842S W or 5A01345AT or 5A02278AK or 5A00562NY. Also 180, 180A, 1808, 1$OC, 180D, 180E, 180F, 1806, 180H, 180K with STC 5A02294CH or 5A095305C 182, 182A, 1828, 182C, 182D, 182E, 182F, 1826, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 1820, 182R, T182, R182, TR182 Also 182, 182A, 1828. 1820.. 1820, 182E, 182, 1826, 182H, 182i, 182K, 182L, 182M, 182N, 182P, 1820., 182R with STC 5A09133SC or 5A90565C or SA090265C or 5A89515W or SA8842SWorSAO2278AKorSAOO562NYorSAO953OSC. Also 182H, 182], 182K, 182L, 24 CESSNA 182M, 1$2N, 182P, 1820., 182R with STCSAOO1S2WI (10-550 or 0-520-0 engine). Also 3A13 CAR 3 182E, 182F, 1826, 182H, 182J, 182K, 182L, 182M, 1$2N, 182P, 1820. 1$2R FAR 23 with STC SA38255W. Also 182H, 182J, 182K, 1821., 1$2M, 182N, 182P with STCSA5664NM. Also 1820, 182R with STCSAO33O2ATorSA5966NM. Also 182, 182A, 1828, 182C, 182D, 182E, 182F, 1826 with SIC SAO2O92SE. Also 182, 182A, 182B, 182C, 1820, 1.82E, 182F, 1826, 182H, 182], 182K, 182L, 1$2M, 182N, 182P, 1820, 182R with STC SA02294CH. Also R182withSTCSAOO86IWIorSAIO8I1SC. Also 182E, 182F, 1826, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 1820., 182R with SIC SA1O232SC A 1825, 182T, T182T. Also 1825, 182T with STC SAO23IINY. Also 1825, 182T and T182T with A IM A 52 CAR 3 25. CESSN STC SA1143SC. Also 1825, 1821 with SIC SA03323CH E SA. . 0 FAR 23 26. CESSNA Cessna F182P, Cessna F182Q, Cessna FR182 A42EU CAR 3 185, 185A, 185B, 185C, 185D, 185E, A185E. A185F Also A185E, A18SF with SIC 5A00344 WI. Also 185. 185A, 1858, 185C, 185D, 185E, A185E, 27. Cessna A185F with SiC SA2118NM orSAO996OSC. Also 185, 185A, 1858, 185C, 1850, 185E with 3A24 CAR 3 STCSA525NW. Also 185, 185A, 1858, 185C, 1850, 1$5E, A185E, A185F with STC 5A293350. Also A85E, A185F with SIC 5A1522GL or 5A02528CH-D. Also A185E, A185F with SIC 5AO2294H Also A185E, A185F with STC SAOO214DE Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 STC APPROVAL —10051939— hP. INSTRUMENTS, INC — EASA Approved Model Ust (AM L) 4/9 Note: The following numbers are listed on the certificate: EASA current Project Number: 0010033203-001 SIC APPROVAL 10051939 —J.P. INSTRUMENTS, INC — EASA Approvad Model List (AML) CAR3 CERTIFICATION BASIS FOR CI-fANGE CAR 3 EASA Approved Model List (AM 1) 10051939 J.P. INSTRUMENTS, INC item AIRCRAFTMAKE AIRCRAFT11ODaNIlli1ilii1liIjK CERTIFICATE 44flfl ‘itI1 NUMBER 210-5 (205), 210-5A (205A) 28. CESSNA 3A21 Also 210-5 (205) and 210-5A (205A) with STCSAO9467SC 206, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU2O6A, 1U206B, TU2O6C, TU2O6D, TU2O6E, TU2O6F, 1U206G, P206, P206A, P206B, P206C, P206D, P2O6E, TP206A, TP2O6B, TP2O6C, TP206D, TP2O6E Also U206A, U206B, U206C, U206D, U206E, U206F, and U206G with SIC 5A2123NM. Also P206A, P206B, P206C, P206D, P206E, U206B, U206C, U206D, U206E, U206F, U2066, TU2O6F, TU2O6G with STC 5A02507AT-D. Also 206, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, P206, P206A, P206B, P20C, P206D, P206E with SIC SA100IOSC. Also 206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, P206, P206A, P206B, 29. Cessna P206C, P206D, P206E, TU2O6G with STC SA02294CH. Also TP2O6A, 1P206B, TP2O6C, A4CE TP2O6D, 1P206E, TU206A, TU2068, 1U206C, TU2O6D, TU206E, 1U206F with STC SAO1300ATorSA2782S W. Also U206B, U206C, U206D, U206E, U206F, U206G with SIC SA14S2GL. Also U206B, U206C, U206D, tJ206E, U206F, U206G, with SIC 5A00332AT. Also 206, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G with STCSA283OSO. Also 206, U206, U206A, U206B, U206C, U206D, U206E, U206F, U2OGG, TU2O6A, TU2O6B, TU206C, TU2O6D, TU2O6E, 1U206F, 1U206G with STC 5A00428 WI. Also 206, P206, P2O6A, U206, U206A, U2068, U206C, U206D, U206E, U206F, U206G, TP2O6A, TU2O6A, TU2O6B, TU2O6C, TU2O6D, 1U206E, TU2O6F with SIC SAO2752cH-D 30. Cessna 2C)6H, T206H EASA.IM.A.053 CAR3 207, 207A, 1207, T207A 31. Cessna A16CE FAR 23 Also 207, 207A, with STC SAOO1SC. Also 207, 207A with STC 5A00173AT 5/9 SIC APPROVAL —10051939— J.P. INSTRUMENTS, INC — CASA Approved Model List (AML) EASA Approved Model List IAML) 10051939 J.P. INSTRUMENTS, INC lten. AlRAFTMKE ii AICRF1t0DEL , 210, 210A, 210B, 210C, 210D, 210E, 210F, 2106, 210H, 210J, 210K, 210C, 210M, 210N, 210R, P21ON, P210R, l2ioF, 12106, F2W:-l, 1210], T210K, T210L, T210M, T210N, T210R Also 210K, 210L, 210M, 210N with SIC SAO2O29AT-D. Also 210M, 210N with STC 5A00274AT. Also 210D, 210E, 210F, 2106, 210H, 210], 210K, 210L, 210M, 210N, 210R with STC 5A099525C. Also 1210M, T21ON with SIC 5A3203NM or 5A2598NM. Also 210K, 32. CESSNA 210L, 210M, 210N, T21OK, T21OL, T21OM, T21ON with STC 5A310450. Also 1210F, 12106, 3A21 CAR 3 1210H, T210i, T21OK, T21OL with STCSA2689SW. Also T21OL, T21OM, T21ON with SIC SAO2918CH. Also T21OK, 1210L, 1210M, T2ION with STC SAO21O7AT-D. Also 210F, 210G. 210H, 210], 210K, 210L, 210M, 210N, T21OF, T2IOG, T2OH, T210J, T21OK, 1210L with SIC 5A00773AT. Also P21ON with STC 5A2528NM or 5A3557NM or SA02918CH or SA2568NM or SA2528NM 33. CESSNA — LC40-550FG A00003SE FAR 23 34. CESSNA - LC42-550FG EASA.lM.A.516 FAR 23 SR2O, SR22 35. Cirrus Design Corporation EASA.lM.A.007 14 CFR 23 Also 5R22 with SIC 5A105885C 112, 112B, 112TC, 12TCA, 114, 114A, 114B, 114TC 36. COMMANDER Also 112, 112B with STC SA52O2NM. Also 114, 114A, 114B, 114TC with STCSAOO241BO. A1250 FAR 23 Also 114, 114A with STC SAOO356DE 37. DIAMOND DA2O-A1, DA2O-C1 EASA.IM.A.223 F R ?1 29 DA4O, DA4OF 38. DIAMOND EASA.A.022 14 CFR 21.29 Also DA 40 with STC SA02476CH-D 39. EXTRA EA-300, EA-300/S, EA-300/L, EA300/200 EASA.A.362 FAR 23 40. EXTRA EA-400 EASA.A.011 14 CFR 21.29 41. FFA AS 202/18A “BRAVO”, AS 202/18A4 “BRAVO” EASA.A.591 FAR 23 Note: The following numbers are listed on the certificate: EASA Current Project Number: 0010033200-001 6/9 1 N1{I:tTui Ili P’dlljilllllllluhtt ‘VjtD TYPE CERTIFICATION Item AWT MAKE jt ic {RAFT MODEL f 1flIIII 1 4 IP I littllth1 1111I1 I 11 CERTIFICATE BASIS FOR ‘u l1 1flc1U’k’t di t}31tq)1 H IdI in bni II111t1PI1 1 NUMBER 1IIIHANGE 42. GA 8 Airvan (Pty) Ltd. GA8-1C320 EASA.IM.A.042 FAR 23 43. GeneralAvia F22C A75EU FAR 23 44. LAVIA S.A. PA-25-235 AR AV-0004 CAR 3 45. LIBERTY XL-2 EASA.IM.A.343 FAR 23 M-4-220, M-4-220C, M-4-220S, M-4-220T, M-5-180C, M-5-200, M-5-210C, M-5-235C, 46. MAULE M-6-235, MI-7-235, M-7-235B, M-7-235C, M-7-260, MX-7-180A, MX-7-180B, MX-7-180C, EASA.lM.A.018 CAR 3 MX-7-8OAC, MXI-7-180A, M-7-260C, M-9-235 M2OA, M2OB, M20C, M2OD, M2OE, M2OF, M2OG, M20J, M2OK, M2OL, M2OS, M2OTN Also M2OA, M2OB, M2OC, M2OD, M2OE, M2OF, M2OG with SIC SA3ISCU. Also M2OC, M2OD, M2OE, M2OF, M2OG, M20J with SIC 5A4529NM-D. Also M2OK with SIC SA569INM orSA4566NM. Also M20i with SIC SA004725E. Also M2OE, M2OF, M2OJ with SIC CAR 3 47 Moone” A3 . SA09695AC. Also M2OK with STC SA310650. FAR 23 Also M20J with STC SA95CH. M2OA, M208, M2OC, M20D, M2OE, M2OF, M2OG, M20] with STCSAO244CH-D. Also M2OTN with STC SA02483CH. Also M2OC, M2OD, M2OE, M2OF, M2OG, M20J with STC SA4529NM-D. Also M2OR, M2OS with STC 5A02193CH. Also M2OE, M2OF, M20i with SIC 5A02461NY 4$. Mooney M2OM and M2OR EASA.IM.A.266 CAR3 4 Mooney_______________________ M22 A6SW CAR 3 PA-24, PA-24-250, PA-24-260, PA-24-400 50. Piper Aircraft, Inc 1A15 CAR 3 Also PA-24-250 with SIC SA3451 WE. Also PA-24 with STC SAOO631CH PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-2$-161, PA-28-180, PA-2$-181, PA-28R480, PA-28R-200, PA-28R-201, PA-28RT-201, PA-28-201T, PA-28R-201T, . PA-28RT-201T PA-28-235, PA- 28-236 51. Piper Aircraft, Inc 2A13 CAR 3 Also PA-2$RI-201T with STC SAOO95CH. Also PA-28R-180, PA-28R-200, PA-28R-201, PA 28RT-201 with STC SAI29CH. Also PA-28R-201T, PA-28RT-201I with SIC SAO1O24H Note: The following numbers are l!sted on the certificate: EASA current Project Number: 0010033200-001 STC APPROVAL 10051939 1?. INSTRUMENTS, NC — EASA Approved Modal List (AML) EASA Approved Mdl List (AML) 1OO139 J.P. INSTRUMENTS, INC ¶1 7/9 STC APPROVAL —10051939 —i.P. INSTRUMENTS, INC — EASA Approved Model List (AML) EASA Aøprovec Model lAst (AM I) 10051939 ].P. INSTRUMENTS, INC $ YPE . CERTIFICATION Item AIRCRAFT MAKE AIRCRAFT MODEL CERTIFICATE BASLFOR 4 , , rI1H%II’tW1W NUMBER CIANGE . . PA-32-260, PA-32-300, PA-32R-300, PA-32S-300, PA-32-301, PA-32R-301 tSP) PA-32-301T, 52. Piper Aircraft, Inc PA-32RT-300, PA-32RT-3001, PA-32R-33lY — — A350 CAR 3 53. Piper Aircraft, Inc PA-32R-301 (Saratoga II HP), PA-32R-301T fSaratcnga II TC) EASA.IM.A.239 . PA-36-285, PA-36-375, PA-36-300 FAR 23 54. Piper Aircraft, Inc A9SO A1OSO FAR 21 Also PA-36-2$5, PA-36-300 with STC SA3452WE —_______________________________ PA-38-112 55. Piper Aircraft, Inc A18SO FAR 23 Also PA-38-112 with STC :SA4135NM PA-46-3 lOP, PA-46-350P, PA-46R-350T 56. Piper EASA.IM.A.077 FAR 23 Also PA-46-310P with SIC SAOO38OATor SAO177OCH Lake Model 250, Lake LA-4-200 CAR 03 57. Revo, Inc. 1A13 14 CFP 23 Also Lake Model 250 with SIC SA469NE 14 CFR 21.29 58. RUSCHMEYER R90-230RG Germany 1082 14 CFR 21.83 14 CFR_23 14 CFR 21.29 59. SOCATA TB 9, TB 10, TB 20, TB 21, TB 200 EASA.A.37$ 14 CFR 23 14CFR36 60. SOCATA MORANE SAULNIER fRallye) Series RalIye 235E, MS 893A, MS 893E, MS 894A EASA.A.379 CAR 3 CAR 10 61. SYMPHONY AIRCRAFT INDUSTRIES, INC. SA 160 EASA.IM.A.031 14C 36 62. True Flight Holdings LLC (American AA-1, M-1A, AA-1B, AA-1C A11EA FAR 23 General) AA-5, AA-5A, AA-5B, AG-58 63. True Flight Holdings LLC A16EA FAR 23 Also AA-5A with SIC SA1186NW. Also AA-5B with SIC 5A01658NY Note: The following numbers are listed on the certificste: EASA current Project Number: 0010033200-001 8/9 For the European Aviation Safety Agency, Date of Issue; 19 January 2015 Note; The following numbers are listed on the certificate: EASA current Project Number: 0010033200-001 SIC APPROVAL —10051939— i.P. INSTRUMENTS, INC — EASA Approved Model List (AML) YvrMORIER Head of eneraI Aviation Remotely Piloted Aircraft system (RPAS) I> I> Item MAKE EASA Approved Model List (AMI) 10051939 J.P. INSTRUMENTS, INC AIRCRAFT MODEL F-5, F5C Aero Bulletin 64. WACO EASA.IM.A.055 7A Also F-5, F5C with STC SA1000GL E CERTIFICATE NUMBER CERTIFICATION BASIS FOR CHANGE 65. WACO Classic Aircraft Corporation 2T-1A-1, 2T-1A-2 A12EA FAR 23 66. Zenair CH2000 TA5CH FAR 21.29 67. ZLIN AIRCRAFT a.s. Z 143L EASA.A.028 FAR 23 68. ZLIN AIRCRAFT a.s. Z 242L —- EASA.A.027 FAR 23 9/9 5’ \ 5’ 5” ‘S ‘\ \ \ \ \\ \ 5. S5•
What's in the CESSNA 172C TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
43 CESSNA 172C parts for sale
See all →
Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.