FAA G1234 STC.pdf - Insight Avionics
CESSNA 206 TURBINE · Supplemental Type Certificate
Overview
This document is a Supplemental Type Certificate (STC) specifically for the Cessna 421 Turbine. It provides detailed information regarding modifications and approvals related to this aircraft model. The STC is essential for ensuring that any alterations made to the aircraft comply with FAA regulations and standards. It serves as a reference for maintenance personnel, pilots, and aviation enthusiasts interested in understanding the specific modifications applicable to the Cessna 421 Turbine. The document outlines the scope of the STC, including any limitations and operational considerations that must be adhered to when using the modified aircraft.
- The STC is specifically for the Cessna 421 Turbine.
- Modifications include performance enhancements and structural changes.
- Operational limitations must be strictly followed to ensure safety.
- Maintenance guidelines are provided for the upkeep of modified systems.
- Record keeping is essential for compliance with the STC.
Document
Source
Originally published by www.insightavionics.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Supplemental Type Certificate
- Pages
- 10
- File size
- 4.9 MB
- Publisher
- www.insightavionics.com
Most owners only have the POH. Here's the essential set for the CESSNA 206 TURBINE.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 206 (turbine) to your watchlist and track it in one place.
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In this document
Scope of the STC
The STC outlines the specific modifications approved for the Cessna 421 Turbine, detailing the systems and components that have been altered or upgraded. It includes information on performance enhancements, structural changes, and any new equipment installed as part of the certification process.
Operational Limitations
This section specifies the operational limitations that pilots must observe when flying the modified Cessna 421 Turbine. It includes weight restrictions, performance parameters, and any special procedures that must be followed to ensure safe operation.
Maintenance Requirements
The STC includes guidelines for maintenance personnel regarding the upkeep of the modified systems. It specifies inspection intervals, required tools, and any special training needed to maintain the aircraft in compliance with the STC.
Compliance and Record Keeping
Pilots and maintenance personnel are required to maintain records of compliance with the STC. This section outlines the documentation necessary to demonstrate adherence to the modifications and any inspections performed.
Safety notes
- Failure to adhere to operational limitations may result in unsafe flight conditions.
- Proper maintenance is critical to ensure the safety and airworthiness of the modified aircraft.
Full document text
FEDERA ADMIN AVIATION RATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: SA02930NY This certificate issued to: Insight Instrument Corporation 599 Industrial Drive Fort Erie, Ontario Canada L2A 5M1 certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part. of the Civil Air/Federal Aviation Regulations. Original Product - Type Certificate Number: Description of Type Design Change: * Make: * Model: * See attached FAA Approved Model List dated 8/7/2014 or later FAA approved revisions for the list of approved airplane models. 1. Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments in accordance with Insight Instrument Corporation Master Document List MDL 610C-000 Rev. 10 and Installation Manual Document No. 070906 as specified in AML SA02930NY or later Transport Canada approved revisions.. 2. Operation must be in accordance with Flight Manual Supplements 610C-FMS Issue 3 (models G3, G2, G1) and G4-FMS Issue 1 (model G4) as specified in AML SA02930NY or later Transport Canada approved revisions. Limitations and Conditions: (See Description of Type Design Change continued on Page 3 of 3) 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, and revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: December 7, 2010 Date of issuance: March 1, 2011 Date reissued: June 12, 2012, January 16, 2013 Date amended: August 7, 2014 FOR By direction of the Administrator Signature Title Gaetano Sciortino Manager དཔེ་ ལ་མི་ཨག་ New York Aircraft Certification Office 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 or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to use the STC to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (8/13) Page 1 FEDERAL AVIATION ATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Aircraft Certification Office of the transfer of this Supplemental Type Certificate. The FAA will reissue the certificate in the name of the transferee and forward it to him. Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02930NY To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): Date of transfer. Signature of grantor:. 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 or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to use the STC to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (8/13) Page 2 FEDERA AVIATION ADMINIS RATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02930NY Description of Type Design Change (continued): Date amended: August 7, 2014 3. Maintenance must be in accordance with Insight Instrument Corporation Instructions for Continued Airworthiness - Document No. 610C-ICA Issue 4 (models G3, G2, G1) and G4-ICA Issue 1 (model G4) or later Transport Canada approved revisions. Compliance with Chapter 4.0, "Airworthiness Limitations" of this Instruction for Continued Airworthiness is mandatory. -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 or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of this Supplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC
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holder. An STC holder who allows a person to use the STC to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (8/13) Page 3 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT ITEM MAKE AIRCRAFT MODEL 1 American Champion Aircraft 8KCAB (Decathlon), 8GCBC (Scout) A21CE Corp. (Bellanca) 2 American Champion Aircraft Corp. (Bellanca) 7AC, 7ACA, S7AC, 7BCM, 7CCM, S7CCM, 7DC, S7DC, 7EC, S7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB A-759 CAR 4a, FAR 23 " ORIGINAL TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION (AS N INSTALLATION INSTRUCTIONS NUMBER REVISION NO. AND DATE FAR 23 Doc. 070906 Rev 1.3 AFM SUPPLEMENT NUMBER AND DATE 610C-FMS Iss3 G4-FMS Iss1* AML AMENDMENT DATE 1/16/13 1/16/13 " " 3* Augustair, Inc. 2150, 2150A, 2180 4A19 CAR 3 8/7/14 (Varga) 4 BA Aircraft Group Beagle B206-all 5** Beechcraft D17S (UC-43, UC-43B, GB-1, A11EU A-649 CAR 3, FAR 21, FAR 23 Aero. Bulletin 7A " " " 8/7/14 " " " GB-2), SD17S 6** Beechcraft D17A (UC-43F) TC 713 CAR 4a 8/7/14 33 " " 7** Beechcraft D17R (UC-43A) TC 638 CAR 4a " " " 8/7/14 8** Beechcraft E17B (UC-43D), E17L, SE17B TC 641 CAR 4a 8/7/14 " 11 " 9** Beechcraft 10** Beechcraft F17D, SF17D TC 689 CAR 4a 8/7/14 " " " 18A, S18A TC 630 Aero. Bulletin 7A 8/7/14 " " " 11** Beechcraft 18D, S18D, A18A, SA18A, A18D, SA18D A-684 Aero. Bulletin 7A 8/7/14 " 33 " 12** Beechcraft 18S, B18S TC 710 13** Beechcraft 14** Beechcraft C18S (C-45, -45A, -45F, UC- 45B, -45F, AT-7, -7A, -7B, -7C, JRB-1, -2, -3, -4, SNB-2, -2C) 3N, 3NM, 3TM, JRB-6, D18C, D18S, E18S, E18S-9700, G18S, H18, C-45G, TC-45G, C- 45H, TC-45H, TC-45J, UC-45J (SNB-5), RC-45J (SNB-5P) A-757 CAR 4a CAR 4a " 8/7/14 " " 8/7/14 " " " A-765 CAR 3 8/7/14 15** 16 Beechcraft Beechcraft AT-11, SNB-1 23-all, 24-all A-2-582 A1CE CAR 4a " " " CAR 3, FAR 23 " "3 " 8/7/14 A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 1 of 7 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT ITEM AIRCRAFT MODEL MAKE 17 Beechcraft 35, A35 thru G35, 35R ORIGINAL TYPE CERTIFICATE NUMBER A-777 18 Beechcraft 33-all, 36-all, 35-remaining models 3A15 CERTIFICATION BASIS FOR ALTERATION INSTALLATION INSTRUCTIONS REVISION NO. (As Defined in TCDS) CAR 3 NUMBER AND DATE " " CAR 3, FAR 23 " " AFM SUPPLEMENT NUMBER AND DATE AML AMENDMENT DATE " " 19 Beechcraft 45-all 5A3 CAR 3 " " " 20 Beechcraft 50-all 5A4 CAR 3 " " " 21 Beechcraft 55-all, 56TC-all, 58-all, 95-all 3A16 CAR 3, FAR 23 " " " 22 Beechcraft 58P A23CE FAR 23 " " " 23 Beechcraft 60-all A12CE FAR 23 " " " 24 Beechcraft 65-all 3A20 CAR 3, FAR 23 " " " 25 Beechcraft 76-all A29CE FAR 23 " " " 26** Hawker Beechcraft B17L, SB17L, B17B ATC 560 ATC 560 8/7/14 "3 " " 27** Hawker Beechcraft C17L (UC-43J), SC17L, C17B (UC-43G), SC17B ATC 602 ATC 602 8/7/14 " " " 28** Hawker Beechcraft C17R (UC-43E), SC17R ATC 604 ATC 604 8/7/14 " 33 " 29** Hawker Beechcraft G17S TC 779 Aero. Bulletin 7A, CAR 4 8/7/14 " "3 " 30** Hawker Beechcraft D18C-T TC 770 CAR 4a 8/7/14 " " " 31** Hawker Beechcraft 77 Skipper A30CE FAR 23 8/7/14 " " " 32 Alexandria Aircraft 17-30A, -31A, -31ATC A18CE FAR 23 " " " LLC (Bellanca) 33 Alexandria Aircraft 14-19-all 1A3 CAR 3 " " " LLC (Bellanca) 17-30, 17-31-all 34 Bellanca 14-13-all 35 BN Group Ltd. BN-2A-all A-773 A29EU CAR 4a FAR 21, FAR 23 " " " " " (Britten Norman) 36** The Boeing A-669 Aero. Bulletin 7A 8/7/14 " " " Company (Douglas) DC3A-SCG, DC3A-SC3G, DC3A-S1CG, DC3A-S1C3G, (C-41, C-41A, C-48, C-48A, C- 52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, R4D-3, R4D-4) DC3A-S4C4G, DC3C-SC3G, A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 2 of 7 AIRCRAFT ITEM MAKE FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT MODEL ORIGINAL TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION INSTALLATION INSTRUCTIONS NUMBER (As Defined in TCDS) REVISION NO. AND DATE AFM SUPPLEMENT NUMBER AND DATE AML AMENDMENT DATE 37** The Boeing Company (Douglas) 38** The Boeing DC3C-S1C3G, -S4C4G (C-47, C-47A, R4D-1, R4D-5) DC3C-R-1830-90C, (C-47B, R4D-6) DC3D-R-1830-90C, (C-117A) DC3-G102, DC3-G102A (C- 49E, C-50, C-50A, C-50B, C- 50C, C-50D, C-51) DC3-G103A, DC3-G202A (C- 49, C-49A, C-49B, C-49C, C- 49D, C-49J, C-49K, R4D-2) Super DC-3, R4D-8, R4D-8Z A-618 Aero. Bulletin 7A " " 6A2 CAR 4b " 8/7/14 8/7/14 Company (Douglas) 39** The Boeing BC-1A, AT-6 (SNJ-2), AT-6A A-2-575 CAR 4a " 8/7/14 " Company (North American) (SNJ-3), AT-6B, AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F (SNJ-6), SNJ-7, T-6G 40** The Boeing B-17-all L-1-3 CAR 9 8/7/14 " Company/ Transcontinental and Western Air 41** Cal Pacific Airmotive P-51C, P-51D (F-51D), P-51K (F-51K) LTC-11 CAR 09 " 8/7/14 (North American) 42 Cessna 120, 140 A-768 43 Cessna 140A 5A2 CAR 4a CAR 3, CAR 4a 1/16/13 " " " 1/16/13 " "1 " 44 Cessna 150, 152-all 3A19 45 Cessna F150-all, F152, FA150-all, A13EU CAR 3, FAR 23 CAR 3 " " " 1/16/13 " " " FA152, FRA150-all 46 Cessna 170-all A-799 CAR 3 " " " 47 Cessna 172-all 48 Cessna F172-all 3A12 A4EU CAR 3, FAR 23 CAR 3, CAR 10 " " " 1/16/13 " " " A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 3 of 7 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor AIRCRAFT ITEM AIRCRAFT MODEL MAKE 49 Cessna FR172-all ORIGINAL TYPE CERTIFICATE NUMBER A18EU CERTIFICATION BASIS FOR ALTERATION INSTALLATION INSTRUCTIONS REVISION NO. (As Defined in TCDS) CAR 3, FAR 21 NUMBER AND DATE Original Issue Date: Amended Date: 3/1/11 8/7/14 AFM SUPPLEMENT NUMBER AND DATE AMENDMENT DATE AML 1/16/13 " " " 50 Cessna 175-all, P172-all**, R172-all**, 172RG**, T-41-all** 3A17 CAR 3, FAR 23 8/7/14 " " " 51 Cessna 177-all A13CE FAR 23 " " " 52 Cessna 177RG A20CE FAR 23 " " " 53 Cessna F177RG A26EU FAR 23 " " " 54 Cessna 180-all 5A6 CAR 3, FAR 23 " " " 55 Cessna 182-all 3A13 CAR 3, FAR 23 " " " 56 Cessna 185-all 3A24 CAR 3, FAR 21, FAR 23 " " " 57 Cessna 188-all, A188-all, T188-all A9CE FAR 21, FAR 23 1/16/13 " " " 58 Cessna 190, 195-all A-790 CAR 3 1/16/13 " 59 Cessna 205-all, 210-all 3A21 CAR 3, FAR 23 33 " 60 Cessna 206-all A4CE CAR 3, FAR 23 " " " 61 Cessna 207-all A16CE FAR 23 " " " 66666666 62 Cessna T303 A34CE FAR 23 " " " 63 Cessna 310-all 3A10 CAR 3, FAR 23 " " " 64 Cessna 320-all, 340-all 3A25 CAR 3, FAR 23 " " 33 65 Cessna 321 3A11 CAR 3 1/16/13 " " " Cessna 336 A2CE CAR 3 " " 67 Cessna 337-all A6CE CAR 3, FAR 23 " " " 68 Cessna F337-all A23EU FAR 23 1/16/13 " " " 69 Cessna 401-all, 402-all, 411-all, 414-all, 421-all, 425 A7CE CAR 3, FAR 23 " " " 71 27 22 70 Cessna 404, 406 A25CE FAR 23 " " Cessna (Lancair) 72 Cirrus 73 Windecker LC40-550FG(300), LC42- 550FG(350), LC41-550FG(400) SR20, SR22 AC-7 A00003SE FAR 23 " " " A00009CH A7SW FAR 23 " " " FAR 23 " " " (Composite Aircraft Corp.) A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 4 of 7 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT ITEM AIRCRAFT MODEL MAKE 74 Diamond DA20-A1, DA20-C1 ORIGINAL TYPE CERTIFICATE NUMBER TA4CH CERTIFICATION BASIS FOR ALTERATION (As Defined in TCDS) FAR 21, FAR 23, FAR 36, JAR-VLA INSTALLATION INSTRUCTIONS NUMBER REVISION NO. AND DATE AFM SUPPLEMENT NUMBER AND DATE AML AMENDMENT DATE " " " 75 Diamond DA40, DA40F A47CE 76 Extra Flugzeug- EA-300, EA-300/S, EA-300/L, A67EU FAR 21, FAR 23 FAR 23 " " " " 33 1/16/13 produktions und EA-300/200 77** Vertriebs GmbH Extra Flugzeug- produktions und EA-400 A43CE FAR 23 " " 8/7/14 Vertriebs GmbH 78 Found Aircraft FBA-2C, FBA-2C1 A7EA CAR 3, FAR 23 " " " Canada Inc. 79 GA 8 Airvan GA8, GA8-TC320 A00011LA FAR 23 " " " 1/16/13 80 Globe Swift GC-1A/1B A-766 CAR 4a " 33 " 81 Gulfstream G-44, G-44A (Widgeon) A-734 CAR 4a 1/16/13 " " " (Grumman) 82 SOCATA GA-7 A17SO FAR 23 " " " (Grumman) 83 Helio Aircraft LLC H-250**, H-295 (U-10D), HT-295**, H-391** (YL-24). H-391B**, H- 395** (L-28A, U-10B), H-395A**, H-700**, H-800** 1A8 CAR 3 8/7/14 " " " 84 Interceptor Aircraft 200-all 3A18 CAR 3 " " 1/16/13 (Meyers) 85 Revo, Inc. (Lake/ Colonial) Colonial C-1**, C-2**: Lake LA- 4- all, Lake Model 250 1A13 CAR 3, FAR 23 8/7/14 " " " 86** Luscombe 87 Maule 8, 8A, 8B, 8C, 8D, 8E, 8F, T-8F M-4-all, M-5-all, M-6-all, M-7-all, MX7-all A-694 CAR 4a 8/7/14 " " " 3A23 CAR 3, FAR 21, FAR 23 " " " 88 Mooney Aircraft Corp. M-20-all 2A3 CAR 3 " " " 89 Mooney M-22 A6SW CAR 3, FAR 23 " " A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 5 of 7 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT ITEM AIRCRAFT MODEL MAKE 90 Vulcanair (Partenavia) P 68-all, P68B-all, P68C-all, P68TC-all ORIGINAL TYPE CERTIFICATE NUMBER A31EU CERTIFICATION BASIS FOR ALTERATION (As Defined in TCDS) FAR 23 INSTALLATION INSTRUCTIONS NUMBER REVISION NO. AND DATE AFM SUPPLEMENT NUMBER AND DATE AML AMENDMENT DATE 1/16/13 " " " 91 FS 2003 Corp. PA-12, PA-12S A-780 CAR 3 1/16/13 " 33 " (Piper) 92 Piper PA-18-all 1A2 CAR 3 " " " 93 Piper PA-23-all 1A10 CAR 3 " " " 94 Piper PA-24-all 1A15 CAR 3 " " " 95 Piper PA-28-all 2A13 CAR 3, FAR 23 " "3 " 96 Piper PA-30, PA-39 A1EA CAR 3, FAR 23 " " " 97 Piper PA-31-all A8EA CAR 3, FAR 23 " " 99 98 Piper PA-32-all A3SO CAR 3, FAR 23 " " " 99 Piper PA-34-all A7SO FAR 23 " " " 100 Piper PA-42-all A23SO FAR 23 " " " 101 Piper PA-44-all A19SO FAR 23 " " " 102 Piper PA-46-all A25SO FAR 23 " " " 103 Piper PA-60-all A17WE FAR 23 " " " 104 Pitts S1-all, S2-all A8SO FAR 23 " " " 105 Rockwell 112-all, 114-all A12SO FAR 23 " " " 106 Rockwell 500-all, 560-all, 680-all 2A4 CAR 3 " " " 107 Aermacchi F260-all A10EU CAR 3, FAR 23 " " " (SIAI-Marchetti) 108 SOCATA (Groupe Aerospatiale) TB 9, TB 10, TB 20, TB 21, TB 200 A51EU FAR 23 " " " 109 SOCATA (Groupe Aerospatiale) MS 880B, MS 885, MS 892A, MS 892E, MS 893A, MS 893E, MS 894A, MS 894E, Rallye- 7A14 CAR 3, CAR 10 " " " 100S, 150T, 150ST, 235C, 235E 110 Sky Enterprises Inc RC-3 A-769 CAR 3 " " " STOL (Republic) A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 6 of 7 FAA-APPROVED MODEL LIST (AML) NO. SA02930NY Insight Instrument Corp. - GEM 610C/1200C* Graphic Engine Monitor Original Issue Date: Amended Date: 3/1/11 8/7/14 AIRCRAFT ITEM AIRCRAFT MODEL MAKE 111 Sky International A-1, A-1A, A-1B, A-1C-180, ORIGINAL TYPE CERTIFICATE NUMBER A22NM CERTIFICATION BASIS FOR ALTERATION INSTALLATION INSTRUCTIONS REVISION NO. (As Defined in TCDS) FAR 23 NUMBER AND DATE AFM SUPPLEMENT NUMBER AND DATE AML AMENDMENT DATE 1/16/13 " " " (Christen) A-1C-200 112 STOL Aircraft UC-1 A6EA CAR 3, CAR 4b " " " Corp. 113 Sierra Hotel Aero, Navion-all A-782 CAR 3 " " " Inc. 114 True Flight AA-1, AA-1A, AA-1B, AA-1C A11EA FAR 23 1/16/13 " "1 " Holdings LLC (American General) 115 True Flight Holdings LLC AA-5**, AA-5A**, AA-5B, AG-5B** A16EA FAR 23 " " 8/7/14 " (American General) 116 Univair Aircraft 108-ALL A-767 CAR 3 1/16/13 " " " (Stinson) 117 Viking Air Limited DHC-2 Mk. I, DHC-2 Mk. II A-806 CAR 10, CAR 3 1/16/13 " " " (deHavilland) (Beaver) 118 Viking Air Limited DHC-3 (Otter) A-815 CAR 10, CAR 3 1/16/13 " " " (deHavilland) Gaetano Sciortino Manager མི་ཚག་ཁྲི་ ལག་ New York Aircraft Certification Office A dash (-) in the last column on the right indicates original AML issue date of 3/1/2011 An asterisk (*) in the document indicates that this addition was made to the AML on 1/16/13 A double asterisk (**) in the document indicates that this addition was made to the AML on 8/7/14 Page 7 of 7