Supplemental Type Certificate for Cirrus SR22T G6
Cirrus SR22T G6 · Supplemental Type Certificate
Overview
This document serves as a Supplemental Type Certificate (STC) for the Cirrus SR22T G6. It provides detailed information regarding the modifications and approvals associated with this specific aircraft model. The STC outlines the compliance with safety regulations and standards, ensuring that the aircraft meets the necessary requirements for operation. It is intended for use by aircraft owners, operators, and maintenance personnel who are involved with the Cirrus SR22T G6. The document includes technical specifications, installation instructions, and operational guidelines relevant to the modifications covered under the STC.
- The document is a Supplemental Type Certificate for the Cirrus SR22T G6.
- It includes detailed modifications and compliance information for the aircraft.
- Installation instructions are provided for the approved modifications.
- Safety and regulatory compliance are emphasized throughout the document.
- Operational guidelines help pilots understand performance changes.
Document
Source
Originally published by www.aircraftspruce.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Pages
- 13
- File size
- 1.6 MB
- Publisher
- www.aircraftspruce.com
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In this document
Introduction
The introduction section outlines the purpose of the STC, which is to certify modifications made to the Cirrus SR22T G6. It emphasizes the importance of adhering to the guidelines provided to maintain airworthiness.
Modifications Covered
This section details the specific modifications that are approved under the STC for the Cirrus SR22T G6. It includes descriptions of the changes made to the aircraft systems, structures, and components.
Installation Instructions
Installation instructions provide step-by-step guidance on how to implement the approved modifications. This includes necessary tools, equipment, and safety precautions to ensure proper installation.
Compliance and Safety
The compliance and safety section discusses the regulatory requirements that the modifications must meet. It highlights the importance of following these guidelines to ensure the safety and airworthiness of the aircraft.
Operational Guidelines
Operational guidelines are provided to assist pilots and operators in understanding how the modifications affect aircraft performance and handling characteristics.
Safety notes
- Adhere to all installation instructions to maintain airworthiness.
- Follow regulatory compliance guidelines to ensure safety.
Full document text
United States of America Department of Transportation-Federal Aviation Administration Supplemental Type Certificate Duplicate Original to replace lost STC Number SA00068SE This certificate, issued to: Electronics International, Inc. 63296 Powell Butte Highway Bend, OR 97701 certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Regulations. Original Product—Type Certificate Number: *See attached FAA Approved Model List (AML) Make: Model: No. SA00068SE for a list of approved airplane models and applicable airworthiness regulations. Description of the Type Design Change: Electronics International fuel flow/pressure instrument manufactured and installed in accordance with the drawings and installation instructions specified on the FAA AML of this STC, or later FAA approved revision. NOTE: The instrument approved by this STC is to be used as a secondary instrument only. This approval does not allow the removal of any original equipment instrumentation. See the continuation sheet for required placards Limitations and Conditions: Approval of this change in type design applies to the airplanes and factory installed or STC'd float combinations listed on the AML only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, Continuation Sheet, and AML must be maintained as part of the permanent records for the modified aircraft. 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. (See Continuation Sheet page 3.) This certificate and the supporting data which is the basis for approval shall remain in effect until sur- rendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date reissued: October 15, 2002 Date of application: November 1, 1993 Date amended: October 15, 2002 March 31, 1994 Date of issuance: By direction of the Administrator FEDERAL AVIATION * ADMINISTRATION (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with FAR 21.47. FAA FORM 8110-2(10-68) United States of America Department of Transportation-Federal Aviation Administration Supplemental Type Certificate Electronics International, Inc. Reissued: October 15, 2002 Amended: October 15, 2002 (Continuation Sheet) Limitations and Conditions: (cont'd) Number SA00068SE The following placards must be located on the instrument panel adjacent to the Electronics International fuel flow/pressure instrument approved by this STC: For all aircraft models: "DO NOT RELY ON FUEL FLOW INSTRUMENT TO DETERMINE FUEL LEVELS IN TANKS" For aircraft originally equipped with fuel flow and/or pressure instruments: "REFER TO ORIGNAL FUEL FLOW/PRESSURE INSTRUMENTATION FOR PRIMARY INFORMATION: - END - Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with FAR 21.47. FAA FORM 8110-2(10-68) Page 3 of 3 Pages FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL ISSUE DATE: March 31, 1994 INSTALLATION INSTRUCTIONS REVISION AML AMENDED DATE ORIGINAL CERTIFICATION FAA SEALED DRAWINGS ITEM AIRCRAFT MAKE AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION NUMBER REVISION NUMBER TD1130921 C 06-04-2002 or Later FAA Approved Revision II 0506931 1 07-02-2002 or Later FAA Approved Revision 1 AERO COMMANDER (Volaire) 2 AERONCA INC. 10, 10A, 100, 100A, 100-180 1A21 " " CAR 3 02-11-2003 (Also See American Champion) 50-L, 50-LA, 65-LA, 65-LB 15AC, S15AC A-702 " " CAR 4A " 02-11-2003 A-802 CAR 3 " " " 10-16-1997 C-3, PC-3 A-396 BUL 7A " 10-20-2010 3 AEROMOT 4 AEROSPATIALE 5 AG CAT Grumman) AMT-100, AMT-200, AMT-200S, AMT-300 TG00004AT See Socata CFR 21 " " 02-11-2003 None 6 AIR TRACTOR INC. G-164, G164A, G164B, G164C, G-164D G-164B-15T, G-164B-34T, G-164B-T AT-250, AT-300, -301, -302, -400, -400A AT-401, AT-401A, AT-401B, AT-402, AT- 402A, AT-402B, AT-501 1A16 1A16 CAR 8 CAR 8 02-11-2003 02-11-2003 A9SW " FAR 21 10-20-2010 A17SW " FAR 21 10-20-2010 AT-502, AT-502A, AT-502B, AT-503, AT- 503A, AT-504 A17SW FAR 21 10-20-2010 AT-802, AT-802A, AT-602 A19SW FAR 23 " 10-20-2010 7 ALLIANCE AIRCRAFT GROUP (Helio Enterprises) 8 ALON 9 AMERICAN BLIMP COMPANY 10 AMERICAN CHAMPION H-391B, H-395, H395A H-391 H-700, H-800 See Univair A-60, A-60+ A-1-50 H-250, H-295, HT-295 1A8 CAR 3 " " " 02-11-2003 1A8 CAR 3 " " " 10-17-1994 1A8 CAR 3 " " 02-11-2003 1A8 CAR 3 " " " 10-17-1994 02-11-2003 AS1NM FAR 21 " " 10-16-1997 S00002SE FAR 21 " 10-16-1997 7AC, 7BCM, 7DC, S7DC A-759 CAR 4A " " " 02-11-2003 (Aeronca, Bellanca, Trytek) 7ACA, S7AC, 7BCM (L-16A) A-759 " CAR 4A " 10-20-2010 7CCM, S7CCM A-759 CAR 4A " " 02-11-2003 7FC, 7JC, 7EC, S7EC, 7GC, 7HC, 7KC A-759 CAR 4A " 10-20-2010 7GCA, 7GCB, 7GCAA, 7KCAB, 7ECA, A-759 CAR 4A " 02-11-2003 7GCBC 7KCAB, L-16A, L-16B A-759 CAR 4A " 02-11-2003 7GCBA A-759 CAR 8 " 02-11-2003 8KCAB, 8GCBC A21CE FAR 23 " " 02-11-2003 11AC, 11BC, S11AC, S11BC " " A-761 CAR 4A 02-11-2003 11CC, S11CC A-796 CAR 3 02-11-2003 11 AMERICAN GENERAL AIRCRAFT 12 AUGUSTAIR INC. (Varga) See Gulfstream American 02-11-2003 2150, 2150A, 2180 4A19 CAR 3 " 02-11-2003 PAGE 1 Of 11 ITEM AIRCRAFT MAKE 13 AVIAT INC.
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(Pitts, Sky, Child F. Doyle) (Christen Industries) (White International) 14 BEECH AIRCRAFT CORP. FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL CERTIFICATION FAA SEALED DRAWINGS INSTALLATION INSTRUCTIONS AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION ORIGINAL ISSUE DATE: March 31, 1994 AML AMENDED NUMBER REVISION NUMBER REVISION DATE A-1, A-1A, A-1B A-1C-180, A-1C-200 A22NM A22NM " FAR 23 " 02-11-2003 " " " FAR 23 10-20-2010 S-1S, S-1T, S-2 " " " A8SO FAR 23 " 02-11-2003 S-2A, S-2S, S-2B, S-2C A8SO " " " " FAR 23 02-11-2003 18A, S18A 630 BUL 7A " " " 02-11-2003 18D, A181A, A18D, SA18A, SA18D A-684 BUL 7A " " 02-11-2003 19A, B19, M19A, 23, A23, A23A, A23-24, C23, B23 A1CE " CAR 3 None A24, A24R, B24R, C24R, A23-19 A1CE CAR 3 " " 02-11-2003 35, 35R, A35, B35, C35, D35, E35, F35, G35 A-777 CAR 3 H35, J35, K35, M35, N35, P35, S35, V35, 3A15 CAR 3 V35A, V35B, 35-33 35-A33, 35-B33, 35-C33, 35-C33A, E33, 3A15 CAR 3 E33A, E33C, F33, F33A F33C, G33, 36, A36, A36TC, B36TC 3A15 CAR 3 " 45 (YT-34), A45 (T-34A, B-45), D45 (T34B) 5A3 CAR 3 50, B50, C50, D50, D50A, D50B, D50C 5A4 CAR 3 None " 02-11-2003 " 02-11-2003 None 10-20-2010 02-11-2003 D50E, D50E-5990, E50, F50, G50, H50, J50 5A4 CAR 3 02-11-2003 A55, B55, B55B, C55, C55A, D55, D55A, E55, E55A 3A16 CAR 3 None 56TC, A56TC 3A16 CAR 3 " " 58, 58A 3A16 CAR 3 " " " None 02-11-2003 58P, 58PA, 58TC, 58TCA A23CE " " " " FAR 23 None 60, A60, B60 A12CE FAR 23 " " " None 65, 65-80, 65-A80, 65-88, 65-B80, A65, 3A20 CAR 3 02-11-2003 A65-8200, 70 65-90, 65-A80-8800, 65-A90 3A20 CAR 3 " 10-20-2010 65-A90-1 (JU-21A, RU-21A, RU-21D, RU- 3A20 " CAR 3 10-20-2010 21H, U-21A, U-21G) 65-A90-2 (RU-21B), 65-A90-3 (RU-21C) 3A20 CAR 3 10-20-2010 65-A90-4 (RU-21E, RU-21H), 65-B80, 70, 3A20 CAR 3 10-20-2010 A65, A-65-8200, B90 C90, C90A, C90GT, C90GTi, E90, H90 3A20 CAR 3 10-20-2010 (T-44A) 76 A29CE " FAR 23 None 77 A30CE FAR 23 None 95, B95, B95A, D95A, E95, 95-55, 95- A55, 95-B55 3A16 CAR 3 None 95-B55A, 95-B55B, 95-C55, 95-C55A 3A16 CAR 3 None PAGE 2 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL ISSUE DATE: March 31, 1994 ORIGINAL CERTIFICATION FAA SEALED DRAWINGS ITEM AIRCRAFT MAKE AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION NUMBER INSTALLATION INSTRUCTIONS REVISION NUMBER REVISION AML AMENDED DATE BELL HELICOPTER 15 47, 47B, 47D, 47D1, 47E, 47G, 47G-2, 47H-1 H1 CAR 6 " 02-11-2003 " 2H1, 47J, 47K, 47J-2, 47J-2A, B-2, B-2A, B-2B, 2H1 CAR 6 None 2H2 CAR 6 None BELL HELICOPTER (CONT.) 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G- 38-1 2H3 CAR 6 None 47G-4, 47G-4A, 47G5, 47G-3B-2, 47G- 5A, 47G-3B-2A 2H3 CAR 6 " " None 16 BELLANCA AIRCRAFT CORPORATION (See American Champion) 17-30A, 17-31A A18CE " FAR 23 None 17-31ATC A18CE " " " FAR 23 None DW-1 A4NW FAR 21 " " 02-11-2003 14-13, 14-13-2, 14-13-3, 14-13-3W A-773 CAR 4A " 02-11-2003 14-19, 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC 1A3 CAR 3 02-11-2003 17 BOEING AIRCRAFT 18 BRANTLY 75 thru E75, A75J1, A75L300, A75N1 thru E75N1, IB75A A-743 CAR 4A 02-11-2003 " B-2, B-2A, B-2B 2H2 CAR 6 02-11-2003 47, 47B, 47D, 47D1, 47E, H1 CAR 6 02-11-2003 47G, 47G-2, 47H-1 H1 CAR 6 " " " 02-11-2003 47G-2A, 47G-2A-1, 2H3 " " CAR 6 02-11-2003 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 2H3 CAR 6 02-11-2003 47G-3B-2A 47G-4, 47G-4A, 2H3 CAR 6 " " " " 02-11-2003 47G-5, 47G-5A 2H3 CAR 6 " " " 02-11-2003 19 CESSNA AIRCRAFT CORP. 120, 140 A-768 CAR 4A " " " 02-11-2003 C-145, C-165 A-701 CAR 4A " " " 02-11-2003 150 thru 150M, A150K, A150L, A150M, 3A19 CAR 3 10-20-2010 152, A152 " 170 thru 170B A-799 CAR 3 02-11-2003 172 thru 172Q 3A12 CAR 3 " 02-11-2003 172R, 172S 3A12 " FAR 23 02-11-2003 172RG 3A17 " CAR 3 02-11-2003 P172D 3A17 CAR 3 " 10-20-2010 " R172E thru R172K 3A17 CAR 3 02-11-2003 " 175 thru 175C 3A17 CAR 3 10-16-1997 " 177 thru 177B A13CE FAR 23 02-11-2003 " 177RG A20CE FAR 23 02-11-2003 " 180 thru 180K 5A6 CAR 3 02-11-2003 " 182 thru 182S, 182T 3A13 CAR 3 10-20-2010 " R182, T182, T182T, TR182 3A13 CAR 3 10-20-2010 PAGE 3 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL ISSUE DATE: March 31, 1994 ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIGINAL CERTIFICATION FAA SEALED DRAWINGS TC BASIS FOR NUMBER ALTERATION INSTALLATION INSTRUCTIONS NUMBER REVISION NUMBER REVISION AML AMENDED DATE CESSNA AIRCRAFT CORP. (CONT.) 185, 185A, 185B 3A24 CAR 3 " " " 02-11-2003 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 " " " None 188, 188A, 188B A9CE " FAR 23 " " " 02-11-2003 A188, A188A, A188B, T188C A9CE FAR 23 " " " " 10-20-2010 190, 195, 195A, 195B A-790 CAR 3 " " " " 10-20-2010 206, 206H, P206 thru P206E, T206H A4CE CAR 3 " " " " 02-11-2003 TP206A thru TP206E A4CE CAR 3 " " " 02-11-2003 U206 thru U206G, TU206A thru TU206G A4CE CAR 3 " " " " None 207, 207A, T207, T207A A16CE FAR 23 " " " 02-11-2003 210, 210A, 210B, 210C, 210D, 210E, 3A21 CAR 3 " " " 10-20-2010 210F, 210K, 210R 210-5 (205), 210-5A (205A) 3A21 CAR 3 " " " 02-11-2003 T210F, 210G, T210G, 210H, 210J 3A21 CAR 3 " " T210H, T210J, T210K, 210M, 210K, 210L 3A21 CAR 3 " " " T210L, T210F, T210M, 210N, P210N, 3A21 CAR 3 " " P210R, T210R T210N 3A21 CAR 3 " T303 A34CE " FAR 23 " None 10-20-2010 10-20-2010 None 02-11-2003 305A, 305C, 305D, 305F 5A5 CAR 3 305B, 305E 3A14 CAR 3 310, 310A, 310B, 310C, 310D, 310E, 3A10 CAR 3 310F, 310H, E310H 3101, 310J, E310J, 310K, 310L 3A10 CAR 3 " 310N, 310P, 310R, T310P, T310R 3A10 CAR 3 " T310Q 3A10 CAR 3 " 310Q 3A10 CAR 3 320, 320A, 320B, 320C 3A25 CAR 3 320D, 320E, 320F 3A25 CAR 3 321 3A11 CAR 3 " 336 A2CE CAR 3 " 337, 337A, 337B A6CE CAR 3 337E, 337C A6CE CAR 3 " T337B, T337E, T337C A6CE CAR 3 " " " 337D, P337B, F337F A6CE CAR 3 " M337B, 337H A6CE CAR 3 " " T337D, T337H A6CE CAR 3 " " 340, 340A 3A25 CAR 3 " 401, 401A, 401B A7CE CAR 3 " " " " 02-11-2003 " 02-11-2003 02-11-2003 02-11-2003 02-11-2003 None None None 02-11-2003 02-11-2003 02-11-2003 " " 02-11-2003 02-11-2003 02-11-2003 " 02-11-2003 02-11-2003 02-11-2003 02-11-2003 " 02-11-2003 PAGE 4 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL CERTIFICATION FAA SEALED DRAWINGS ITEM AIRCRAFT MAKE AIRCRAFT MODEL INSTALLATION INSTRUCTIONS TC NUMBER BASIS FOR ORIGINAL ISSUE DATE: March 31, 1994 AML AMENDED ALTERATION NUMBER REVISION NUMBER REVISION DATE CESSNA AIRCRAFT CORP. (CONT.) 402, 402A, 402B 402C A7CE A7CE CAR 3 " " " 02-11-2003 CAR 3 " " " 02-11-2003 404 A25CE FAR 23 " " " " 02-11-2003 406 A25CE FAR 23 " " " " 02-11-2003 411, 411A A7CE CAR 3 " " 02-11-2003 414, 414A A7CE CAR 3 " " " 02-11-2003 421, 421A, 421B A7CE " " CAR 3 " 02-11-2003 421C, 425 A7CE CAR 3 " " None S-4A (Seibel) 5H2 CAR 6 " 02-11-2003 20 CHILD, DOYLE F. 21 CHRISTEN INDUSTRIES 22 CIRRUS DESIGN CORPORATION 23 CLARK 24 COMMANDER AIRCRAFT See Aviat 02-11-2003 See Aviat 02-11-2003 SR20, SR22 & SR22T 1000 12 A00009CH 2A6 2A12 FAR 23 CAR 8 " 10-20-2010 " 02-11-2003 CAR 8 " " " 02-11-2003 112, 112TC, 112B, 112TCA A12S0 FAR 23 " " " " 04-20-1994 114, 114A A12SO FAR 23 " 04-20-1994 500, 500-A, 500-B, 500-S, 500-U, 520, 6A1 CAR 3 " 10-20-2010 560, 560-A, 560-E 560-F, 680, 680-E, 680-F, 680FL, 680T, 2A4 CAR 3 " " 02-11-2003 680V, 680W, 681, 685 690A thru 690D, 695, 695A, 695B 2A4 CAR 3 " " " 10-16-1997 700 A12SW FAR 23 " " " 02-11-2003 COMMANDER AIRCRAFT (CONT. 720 2A4 CAR 3 " " 02-11-2003 114B, 114TC A12SO FAR 23 " 10-20-2010 25 DE HAVILLAND AIRCRAFT COMPANY, LTD. DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III A-806 CAR 10 " 10-20-2010 DHC-3 A-815 CAR 10 " " 10-16-1997 DHC-1B-2-S3, DHC-1B-2-S5 A26NM CAR 10 " " " 02-11-2003 DH82A A5PC FAR 21 " 02-11-2003 DH82A A8EU " FAR 21 02-11-2003 DE HAVILLAND AIRCRAFT COMPANY, LTD. (CONT.) DH.C1, 21, 22, 22A A44EU FAR 21 02-11-2003 L-20A AR-33 CAR 8 " 02-11-2003 26 DIAMOND AIRCRAFT INDUSTRIES DA 20-A1, DA 20-C1 TA4CH FAR 21 " " 02-11-2003 DA 40, DA 40F A47CE FAR 21 " " 10-20-2010 27 DORNIER-WERKE DO 27 Q-6 A8IN CAR 10 " " 02-11-2003 DO 28 A-1, DO 28 B-1 7A13 CAR 10 " " 02-11-2003 DO 28 D, DO 28 D-1 A16EU FAR 23 " " 02-11-2003 PAGE 5 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIGINAL CERTIFICATION FAA SEALED DRAWINGS TC BASIS FOR NUMBER ALTERATION ORIGINAL ISSUE DATE: March 31, 1994 INSTALLATION INSTRUCTIONS NUMBER REVISION NUMBER REVISION AML AMENDED DATE DORNIER-WERKE (CONT.) 228-100, 228-101, 228-200, 228-201, 228-202, 228-212 A16EU FAR 23 " " 02-11-2003 28 ENSTROM 29 ERCO F-28, F-28A, F-28C, F-28F " " H1CE CAR 6 02-11-2003 280, 280C, TH-28, 480, 280F, F-28FX See Univair H1CE CAR 6 " " 02-11-2003 02-11-2003 30 EXTRA FLUGZEUGBAU FAIRCHILD 31 EA-300, EA-300S, EA 300/200, 300L 24R9, 24R9S, 24R40, 24R40S, 24R46, 24R46A, 24R46S A67EU FAR 23 02-11-2003 A-706 CAR 4A 02-11-2003 24W-9, 24W-9S, 24W-40, 24W-40S, 24W- 41, 24W-41A A-707 CAR 4A 02-11-2003 24W-41AS, 24W-41S, 24W-46, 24W-46S A-707 CAR 4A 02-11-2003 M62A, M62A-3, M62A-4, M62B, M62C, M- 628 A-724 CAR 4A " 02-11-2003 24 C8C, 24 C8CS A-535 " BUL 7A 02-11-2003 M-84-C A-2-599 CAR 4A 02-11-2003 32 FORNEY 33 FUJI 34 GLOBE (Swift) 35 GOODYEAR See Univair 02-11-2003 FA-200-160, 180, 180AO A4PC CAR 10 02-11-2003 GC-1A, GC-1B A-766 CAR 4A " 02-11-2003 GA-22A 1A12 CAR 3 " " " " 02-11-2003 GA-2, GA-2B A-784 CAR 4A " " 02-11-2003 G-115, 115A, 115B, 115C, 115C2, 115D, 335 GROB 36 A-57EU FAR 21 02-11-2003 115D2 37 GULFSTREAM AMERICAN CORP. (American General) (Grumman Aircraft) (Tiger Aircraft) 38 HELICOPTER TECHNIK 39 HELITECH CORP. 40 HELIO Aircraft 41 HILLER HILLER (CONT.) UH-12D G-159 1A17 CAR 4B " None G-1159 A12EA CAR 4B " None AA-1, AA-1A, AA-1B A11EA FAR 23 None AA-1C A11EA FAR 23 " None AA-5, AA-5A, AA-5B, AG-5B A16EA " FAR 23 " 02-11-2003 FJ Sky-Trac H5EU FAR 27 " " 02-11-2003 H-S-1N H12WE " " FAR 21 02-11-2003 15A, 20 3A3 CAR 4A " " 10-16-1997 UH-12, UH-12A " 6H1 CAR 6 " " 02-11-2003 UH-12B, UH-12C 6H2 CAR 6 " " 02-11-2003 4H10 CAR 6 " " 02-11-2003 UH-12E, UH-12E-L 4H11 CAR 6 " " 02-11-2003 UH-12L H1WE CAR 6 " " 02-11-2003 42 HOWARD DGA-8 (Army UC-70C) " " 612 BUL 7A 10-20-2010 DGA-9 (Army UC-70D), DGA-12 (Army 645 BUL 7A 10-20-2010 UC-70A) DGA-11 672 " BUL 7A 10-20-2010 PAGE 6 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ITEM AIRCRAFT MAKE HOWARD (CONT.) ORIGINAL CERTIFICATION FAA SEALED DRAWINGS AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION NUMBER REVISION NUMBER DGA-15P (Army UC-70, Navy GH-1, GH- 2, GH-3, NH-1) A-717 CAR 4A DGA-15J (Army UC-70B), DGA-15W A-717 CAR 4A DGA-18, DGA-18K 739 CAR 4A ORIGINAL ISSUE DATE: March 31, 1994 INSTALLATION INSTRUCTIONS AML AMENDED REVISION DATE " 10-20-2010 10-20-2010 10-20-2010 43 INTERCEPTOR JODEL See Prop-Jets D-140-B 02-11-2003 A3IN CAR 10 " " 02-11-2003 DR-1050 A4IN CAR 10 " 02-11-2003 D-1190 A10IN CAR 10 " " " 02-11-2003 150 A14IN CAR 10 " " 02-11-2003 44 LAKE (Revo) C-1, C-2, LA-4, LA-4A, LA-4P, LA-4-200, 250 1A13 CAR 3 " " " 02-11-2003 45 LUSCOMBE 46 MARCHETTI (See SIAI) 8A thru 8F, T-8F A-694 CAR 4A " 10-16-1997 S205-18/F, -18/R A9EU FAR 21 " 02-11-2003 S205-20/F, -20/R S205-22/R A9EU FAR 21 " " 02-11-2003 A9EU FAR 21 " " " 02-11-2003 S208, S208A A9EU FAR 21 " " " 02-11-2003 F260, F260B-F A10EU CAR 3 " 02-11-2003 S211A A86EU " FAR 23 02-11-2003 47 MAULE M-4, M-4C, M-4S, M-4T, M-4-180C, M-4- 180S, M-4-180T 3A23 CAR 3 02-11-2003 M-4-210, M-4-210C, M-4-210S, M-4-210T M-4-220, M-4-220C, M-4-220S, M-4-220T 3A23 CAR 3 02-11-2003 3A23 CAR 3 " " 02-11-2003 M-5-180C, M-5-200, M-5-210C, M-5- 3A23 CAR 3 None 210TC M-5-220C, M-5-235C 3A23 CAR 3 " None M-6-180, M-6-235 3A23 " CAR 3 10-17-1994 MX-7-160, MX-7-160C, MXT-7-160 3A23 CAR 3 " 02-11-2003 M-7-180, MX-7-180A thru MX-7-180C, 3A23 CAR 3 " 02-11-2003 MX-7-180AC MXT-7-180, MXT-7-180A 3A23 CAR 3 02-11-2003 M-7-235, M-7-235A thru M-7-235C, MT-7- 3A23 CAR 3 " 02-11-2003 235, MX-7-235 M-7-260, M-7-260C, MT-7-260 3A23 CAR 3 02-11-2003 MAULE (CONT.) 48 MESSERSCHMITT M-7-420AC, MX-7-420, MXT-7-420, M-8- 3A23 CAR 3 " 02-11-2003 235 BO-209-150 FV &RV A27EU FAR 21 " 02-11-2003 BO-209-160 FV & RV A27EU FAR 21 " 02-11-2003 BO 209-150 FF A27EU FAR 21 02-11-2003 49 MEYERS See Interceptor 02-11-2003 PAGE 7 of 11 ITEM AIRCRAFT MAKE 50 MOONEY AIRCRAFT 51 MORAVAN FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL ISSUE DATE: March 31, 1994 INSTALLATION ORIGINAL CERTIFICATION FAA SEALED DRAWINGS INSTRUCTIONS AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION AML AMENDED NUMBER REVISION NUMBER REVISION DATE M-18C, M-18C55, M-18L, M-18LA A-803 CAR 3 " " " " 02-11-2003 M20, M20A thru M20M " 2A3 CAR 3 " " " M20R, M20S, M20TN 2A3 CAR 3 " " " " None 10-20-2010 M22 Zlin 526L " " A6SW CAR 3 " " None A30EU FAR 21 " " A76EU FAR 21 02-11-2003 02-11-2003 None Zlin Z 242L, 143L NAVION 52 See Thompson 53 PARTENAVIA P-68, P-68B, P-68C, P-68TC P-68C-TC A31EU FAR 21 " 02-11-2003 54 PIAGGIO P-166, P-166B, P-166C, 7A4 CAR 10 " 02-11-2003 P-136-L, P-136-L1, P-136-L2 A-813 CAR 10 " " 02-11-2003 55 PILATUS PC-6, PC-6-H1, PC-6-H2, 7A15 CAR 10 " " 02-11-2003 PC-6/350, PC-6/350-H1, PC-6/350-H2 7A15 CAR 3, 10 " " 02-11-2003 PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B- 7A15 CAR 3, 10 " 10-20-2010 H2, PC-6/B1-H2 PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1-H2 7A15 CAR 3, 10 " 10-20-2010 PC-7 A50EU FAR 23 " 10-20-2010 PC-12, PC-12/45, PC-12/47, PC-12/47E A78EU FAR 23 " 10-20-2010 PA-11, PA-11S, J3C-40, J3C-50, J3C- PIPER AIRCRAFT CO. A-691 CAR 4A " " 02-11-2003 56 50S, J3C-65, J3C-65S PA-12, PA-12S A-780 CAR 3 " " " 02-11-2003 PA-14 A-797 CAR 3 " " " " 02-11-2003 PA-15 A-800 CAR 3 " " " " 02-11-2003 PA-16, PA-16S 1A1 CAR 3 " " " " 02-11-2003 PA-17 A-805 CAR 3 " " " " 02-11-2003 PA-18, PA-18A, PA-18AS, PA-18S, PA- 1A2 19, PA-19S CAR 3 " 02-11-2003 PA-20, PA-20S 1A4 CAR 3 " " " " PA-22, PA-22S 1A6 CAR 3 " " " " None 02-11-2003 PA-23, PA-23-160, PA-23-235, PA-23-250 1A10 CAR 3 " " " None PA-24, PA-24-250, PA-24-260, PA-24-400 1A15 CAR 3 " " " 02-11-2003 PA-25, PA-25-235, PA-25-260 2A8 CAR 3 " " " 02-11-2003 PA-28-140, PA-28-150, PA-28-151, PA- 28-160, PA-28S-160 2A13 CAR 3 " None PA-28-161, PA-28-180, PA-28R-180, PA- 2A13 CAR 3 None 28-181, PA-28R-200 PA-28R-201, PA-28-201T, PA-28R-201T, 2A13 CAR 3 None PA-28-235, PA-28-236 PAGE 8 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL CERTIFICATION FAA SEALED DRAWINGS ITEM AIRCRAFT MAKE ORIGINAL ISSUE DATE: March 31, 1994 INSTALLATION INSTRUCTIONS AIRCRAFT MODEL TC NUMBER BASIS FOR ALTERATION NUMBER REVISION NUMBER REVISION AML AMENDED DATE PIPER AIRCRAFT CO. (CONT.) PA-28RT-201, PA-28RT-201T, PA-28S- 2A13 CAR 3 02-11-2003 180 PA-30 A1EA CAR 3 " " 02-11-2003 PA-31, PA-31-300, PA-31-325, PA-31-350 PA-31P, PA-31T, PA-31T1, PA-31T2, PA- 31T3, PA-31P-350 A20S0 " " " " CAR 3 02-11-2003 A8EA CAR 3 " 02-11-2003 PA-32-260, PA-32-300, PA-32R-300, PA- A3SO CAR 3 " " " None 32RT-300T, PA-32-301 PA-32-301T, PA-32R-301, PA-32R-301T A3SO CAR 3 " " " None PA-34-200, PA-34-200T, PA-34-220T A7SO FAR 23 " " " " None PA-36-285, PA-36-300, PA-36-375 A9SO FAR 23 " " " " None PA-38-112 A18SO FAR 23 " " " " None PA-39, PA-40 A1EA " " CAR 3 " " 02-11-2003 PA-44-180, PA-44-180T A19SO FAR 23 " " " None PA-46-310P, PA-46-350P, PA-46-350T A25SO FAR 23 " " 10-20-2010 PA-60-600 (Aerostar 600), PA-60-601 A17WE FAR 23 " 10-20-2010 (Aerostar 601) PA-60-601P (Aerostar 601P), PA-60-602P A17WE FAR 23 10-20-2010 (Aerostar 602P) PA-60-700P (Aerostar 700P) A17WE FAR 23 " 10-20-2010 57 PITTS 58 PROP-JETS (Interceptor) See Aviat 02-11-2003 200, 200A, 200B, 200C, 200D, 400 3A18 CAR 3 10-16-1997 (Aero Commander & Meyers) 59 QUEST Kodiak 100 A00007SE FAR 23 10-20-2010 60 REVO 61 ROCKWELL 62 SIAI MARCHETTI See Lake 02-11-2003 See Commander Aircraft 02-11-2003 S205-18/F, -18/R A9EU " " FAR 21 " 02-11-2003 S205-20/F, -20/R A9EU " " FAR 21 02-11-2003 S205-22/R S208, S208A F260, F260B-F S211A A9EU FAR 21 " " " 02-11-2003 " " " A9EU FAR 21 02-11-2003 A10EU CAR 3 " 02-11-2003 A86EU " " " " FAR 23 02-11-2003 63 SEABEE See Sky Enterprises 02-11-2003 64 SIKORSKY 65 SKY ENTERPRISES (SeaBee) 66 SKY INTERNATIONAL S-43, S-43B, S43W A-593 BUL 7A " " 02-11-2003 RC-3 A-769 CAR 3 02-11-2003 See Aviat 02-11-2003 67 SOCATA GROUP (Aerospatiale) TB 9, TB 10, TB 20, TB 21 A51EU CAR 3 " None TB 200 A51EU CAR 3 " GA-7 A17SO " FAR 23 02-11-2003 02-11-2003 PAGE 9 of 11 FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS ORIGINAL ISSUE DATE: March 31, 1994 ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIGINAL CERTIFICATION FAA SEALED DRAWINGS TC BASIS FOR NUMBER ALTERATION INSTALLATION INSTRUCTIONS NUMBER REVISION NUMBER REVISION AML AMENDED DATE SOCATA GROUP (Aerospatiale) (CONT.) MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A 7A14 CAR 10 10-20-2010 MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150ST 7A14 CAR 10 10-20-2010 68 STINSON Rallye 150T, Rallye 235C, Rallye 235E See Univair 7A14 CAR 10 10-20-2010 None 69 SWIFT (Globe) GC-1A, GC-1B A-766 CAR 4A 10-16-1997 TAYLORCRAFT 70 19, F19, F21, F21A, F21B, F22, F22A, F22B, F22C 1A9 " CAR 3 " 02-11-2003 A A-643 BC, BCS, BC-65, BCS-65, A-696 BUL 7A CAR 4 " " " 02-11-2003 " " " 02-11-2003 BC12-65, BCS12-65, BC12-D, BCS12-D, A-696 CAR 4 " " 02-11-2003 BC12-D1, BCS12-D1 BC12D-85, BCS12D-85, BC12D-4-85, A-696 CAR 4 02-11-2003 BCS12D-4-85 TAYLORCRAFT (CONT.) BF, BFS, BF-60, BFS-60, BF-65, BFS-65, A-699 CAR 4 02-11-2003 BF 12-65 BL, BLS, BL-65, BLS-65, BL12-65, BLS12-65 A-700 CAR 4A 02-11-2003 DC-65, DF-65, DL-65, DCO-65 A-746 CAR 4A " " 02-11-2003 71 THOMPSON Navion, Navion A, B, C, D, E, F, G, H A-782 CAR 3 " " " 10-20-2010 (Navion, North American) L-17A, L-17B, L-17C A-782 CAR 3 " " " " None THRUSH AIRCRAFT, INC. 600 S2D, S-2R, S2R-T34, S2R-T15, S2R- A4SW CAR 8 " " 10-20-2010 72 R3S, S2R-T11, S2R-T65 S2RHG-T65, S2R-R1340, S2R-R1820, (Ayres Corp) A4SW CAR 8 10-20-2010 S2R-T45, S2R-G6, S2R-G10 (Rockwell Commander) S2R-G5, S2RHG-T34, S2R-G1, S2R- A4SW CAR 8 10-20-2010 T660 600 S-2D, S2R, S2R-T34, S2R-T15, S2R- T11, S2R-R3S, S2R-R1340 A3SW CAR 3 10-20-2010 S2A 2A9 CAR 8.10(a)(1) 10-20-2010 S-2B, S-2C, 600-S2C 2A7 CAR 8.10(a)(1) " 10-20-2010 73 TIGER AIRCRAFT See Gulfstream American 02-11-2003 74 TRYTEK See American Champion 02-11-2003 75 UNIVAIR AIRCART 108, 108-1, 108-2, 108-3, 108-5 A-767 CAR 3 " " 10-16-1997 (Alon, Erco, Forney, Mooney) V-77 A-774 " CAR 4A 02-11-2003 (Stinson) L-5, L-5B, L-5C, L5-D, L5-E, L5-E-1, L5-G 10A, 10B A-764 CAR 4A " " " " 02-11-2003 " " A-738 CAR 4A " 02-11-2003 415-C, 415-CD A-718 " " CAR 4A " 02-11-2003 415-D, E, G, F-1, F-1A, A-2, A2-A, M-10 A-787 " " " CAR 3 02-11-2003 HW-75 A-709 CAR 4A " " " 02-11-2003 PAGE 10 of 11 ITEM AIRCRAFT MAKE FAA APPROVED MODEL LIST (AML) SA00068SE FOR ELECTRONICS INTERNATIONAL, INC. FUEL FLOW/PRESSURE INSTRUMENTS AIRCRAFT MODEL TC NUMBER ORIGINAL CERTIFICATION FAA SEALED DRAWINGS BASIS FOR ALTERATION NUMBER 76 VARGA See Augustair Inc. 77 WSK-"PZL-MIELIEC" OBR 78 ZENAIR PZL M20 03 CH2000 END of LIST A68EU TA5CH FAR 21 FAR 21 INSTALLATION INSTRUCTIONS ORIGINAL ISSUE DATE: March 31, 1994 AML AMENDED REVISION NUMBER REVISION DATE 02-11-2003 " 02-11-2003 10-16-1997 FAA APPROVED: AMENDED: Acting Manager, Seattle Aircraft Certification Office April 20, 1994; October 17, 1994; October 16, 1997; July 19, 2002; February 11, 2003; October 20, 2010 REISSUED: PAGE 11 Of 11