Supplemental Type Certificate for the CESSNA C-165

[Amdı. 27-35], 27.1367(a) [Amdt. 27-0], 27.1385 [Amdt. 27-0], 27.1387 [Amdt, 27- 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 (5/14) Page 3 of 13 FEDER VIATION ADMIN ETRATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA June 19, 2019 7], 27.1389 [Amdt. 27-0], 27.1391 [Amdt. 27-0], 27.1393 [Amdt. 27-0], 27.1395 [Amdt. 27-0], 27.1397 [Amdt. 27-6], 27.1401 [Amdt. 27-10], 27.1529 [Amdt. 27-18] 3. To complete the approval of these lights as anti-collision light systems, the installations on individual aircraft must be checked to show compliance with 14 CFR 23.1401(b) or 14 CFR 27.1401(b), as appropriate, for field of coverage unless the "Anti-Collision Light Systems Installation and Service Manual", Document 05131, Rev E or later FAA approved revision, specifically indicates that a particular installation has been checked for compliance with the aforementioned sub-sections. NOTE: The aforementioned Installation and Service Manual contains an acceptable method for checking the adequacy of coverage when using two lights (wing tips) or three lights (wing tips and tail lights). For some other acceptable methods, see Advisory Circular AC 43.13-2, Chapter 4, Paragraph 46b(2). Installations made in accordance with STC SA800EA Amendments prior to 9/14/71 need only be checked for obstructed visibility to meet anti-collision light requirements. 4. Install the following placard, Whelen Part No. A421-1, or other FAA approved equivalent, in view of the pilot: WARNING TURN OFF STROBE LIGHTS WHEN TAXING IN VICINITY OF OTHER AIRCRAFT OR DURING FLIGHT THROUGH CLOUDS, FOG OR HAZE. STANDARD POSITION LIGHTS TO BE ON FOR ALL NIGHT OPERATIONS. 5. On all helicopter installations, install the following placard in view of the pilot: THE WHITE STROBE LIGHT MUST BE TURNED OFF DURING ALL NIGHT TAKEOFFS AND LANDINGS. 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 (5/14) Page 4 of 13 FEDER AVIATION ADMINIST United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA June 19, 2019 6. The modifications approved by this STC can be installed in conjunction with those approved by STC SA615EA or STC SA738EA as delineated in the "Anti-Collision Light Systems Installation and Service Manual", Document 05131, Rev C, or later FAA approved revision. 7. On Mitsubishi MU-2B, MU-2B-10, -20, -15, -30 aircraft: Whelen's Mitsubishi MU-2B, -10, -20, -15, -30 Wing Tip and Tail Strobe Light Installation Procedure", dated 19 February 1971, is required in addition to the “Anti-Collision Light Systems Installation and Service Manual", Document 05131, Rev E, or later FAA approved revision. 8. This approval should not be incorporated in any aircraft for these specific models on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft. This determination should include a night flight check as specified in AC 43.13-2, Chapter 4, Paragraph 42A. NOTE: Aircraft whose application for type certification was made before April 1, 1957, may but need not, comply with the field of coverage requirements of FAR 23(27).1401(b). Compliance with FAR 91.33(c) may be shown provided the light installation is in accordance with data approved prior to August 11, 1971, and applicable criteria of Advisory Circular 43.13-2 are met. 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 (5/14) Page 5 of 13 FED ADMINIS NATION TRATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA June 19, 2019 AMENDMENT HISTORY: This STC has been previously amended on the following dates: 11/20/69; 4/23/70, 12/10/70; 5/26/71, 9/14/71; 5/18/72, 9/22/72, 11/7/72; 7/21/76, 7/30/76; 12/30/77; 2/21/78, 10/4/78; 5/17/79; 3/26/81, 8/5/81, 8/25/81; 5/21/82; 7/16/91; 11/22/93; 6/7/99; 6/18/99; 9/8/99, 6/17/05, 5/5/10, 12/5/14 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 (5/14) Page 6 of 13 FEDERAL VIATION ADMINISTRATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer (Continuation Sheet) Number SA800EA June 19, 2019 Eligibility List May 2, 2018 Aero Commander American Aviation Model *100, 100-180 111 112 500, 500-A, 500-B, 500-5, 500-U, 520, 560, 560A, 560E Type Certificate 1A21 A1150 A12SO 6A1 560F, 680, 680E, -F, 720, 680FL, 680FL(P), 680T, V, W, 681, 690, 685 2A4 *AA-1, *AA-1A A11EA AA-5 A16EA Beech 23, A23, A23A, A23-19, -24, -19A, B19, M19A, B23, C23, A24, A24R A1CE 35, A35, B35, C35, D35, E35, F35, G35, 35R A-777 H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35- B33, 35-C33, 35-C33A, 36, A36, A36TC, B36TC, G36, E33, E33A, E33C, F33, F33A, F33C 3A15 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 (5/14) Page 7 of 13 FEDERA AVIATION ADMINISTRATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer Beech (continued) (Continuation Sheet) Number SA800EA June 19, 2019 Model 50(L-23A), B50(L-23B), C50, D50(L- 23E), D50A, D50B, D50C, D50E, E50(L- 23D, RL-23D), F50, G50, H50, J50 Type Certificate 5A4 95-55, 95-A55, 95-B55, 95-B55B{T- 42A), 95-B55D, 95C55, 95, B95, B95A, D95A, E95, D55, D55A, E55, E55A, 56TC, A56TC, 58 3A16 65(L23F), A65, A65-8200, 65-80, 65- A80, 65-A80-8800, 65-B80, 65-88, B90, C90, 65-90, 65-A90, 65-A90-1, (U-21A, RU-21A, RU-21D), 65-A90-2, (RU-21B), 65-A90-3 (RU-21C), 70 60, A60 99, 99A, 100 3A20 A12CE A14CE 1A3 Bellanca 14-19-3A, 17-30 17-30A, 17-31A, 17-31ATC A18CE 7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, A-759 7KCAB Bell 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 407 H2SW 47B, B3, D, D1, E, G, G-2, H-1 H-1 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 (5/14) Page 8 of 13 FEDERAL ADMINIS VIATION RATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer Bell (continued) (Continuation Sheet) Number SA800EA June 19, 2019 Model 47G-2A, -2A-1, -3, -3B, -3B-1, -3B-27, Type Certificate 2H3 4, -4A, -5, -5A 471, K, J-2, J-2A 2H1 Britten Norman BN-2, -2A, -2A-2, -2A-6, -2A-8 A17EU BN-2A, MK.JII A29EU Cessna 120, 140 A-768 140A 5A2 150, 150A, B, C, D, E, F, G, H, J, K, L, M, 3A19 A150K, A150L, A150M, 152, A152 170, 170A, 170B A-799 172, 172A, B, C, D, E, F, G, H, I, K, L, M, 3A12 N, P 175, 175A, B, C, P172D, 172RG 3A17 177, 177A, B 177RG A13CE A20CE 180, 180A, B, C, D, E, F, G, H, J, K 5A6 182, 182A, B, C, D, E, F, G, H, J, K, L, M, N, P, Q, R, T182, R182, TR182 3A13 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 (5/14) Page 9 of 13 FEDERA ADMINI VIATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA June 19, 2019 Model Aircraft Manufacturer Type Certificate Cessna (continued) 185, 185A, B, C, D, E, A185E, A185F 3A24 188, 188A, B, A188, A188A, A188B, A9CE T188C 190, 195, 195A, B A-790 206, P206, P206A, B, C, D, E, TU206A, A4CE B, C, D, E, F, G, TP206A, B, C, D, E, U206, U206A, B, C, D, E, F, G 207, 207A, T207, T207A A16CE 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, 210-5(205), 210-5A(205A), T201K, 210L, T210L, T210M, T210N, 210N, P210N 3A21 310, 310A, B, C, D, E, F, G, H, I, J, 310J- 1, E310J, 310K, L, N, P, T310P, 310Q, 3A10 T310Q *320, A, B, C, D, E, F, 320-1, 340, 340A 3A25 *336 A2CE 337, 337A, B, C, D, E, F, T337D, E, F, G A6CE *401, 401A, B, 402, 402A, B, 411, 411A, 421, 421A, 414, 421B A7CE 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 (5/14) Page 10 of 13 FEDERAL ADMINIS AVIATION TRATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer (Continuation Sheet) Number SA800EA June 19, 2019 Model Type Certificate DeHavilland of Canada DHC-2, MK. I, MK. II, MK. III A-806 DHC-3 A-815 DHC-6, Models 1, 100, 110, 200, 210, A9EA 300 Fairchild Hiller FH-1100 H2WE Grumman G-164, G-164A, G-164B 1A16 Helio H-250, H-295, H-391, H-3918, H-395, H-395A 1A8 Hughes 269A, 269A-1, 269B, 269C 4H12 369D, 369E, 369F, 369FF, 500N, 600N H3WE Piper **PA-11 A-691 **PA-12 A-780 **PA-14 A-797 **PA-15 A-800 **PA-16, PA-165 1A1 **PA-17 A-805 **PA-18 Series, PA-19, PA-19S 1A2 **PA-20 Series 1A4 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 (5/14) Page 11 of 13 VIATION ADMINTON United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer Piper (continued) (Continuation Sheet) Number SA800EA June 19, 2019 Model **PA-22 Series Type Certificate 1A6 **PA-25 Series 2A8 PA-23, PA-23-160, *PA-23-235, *PA- 23-250, *PA-E23-250 1A10 PA-24, -24-250, -24-260, -24-400 1A15 PA-28-140, -28-150, -28-151, -28-160, -28-161, -28-180, -28-235, -285-160, 2A13 -28R-180, -285-180, -28-181, -28R- 200, -28R-201, -28R-201T, -28RT-201, -28RT-201T, -28-201T, -28-236 PA-30, PA-39 A1EA PA-31P A8EA PA-31, PA-31-300, 325, 350 A20SO PA-32-260, -300, -325-300 A3SO Mooney Mitsubishi Univair (Stinson) M20B, C, D, E, F, G 2A3 MU-2B, MU-2B-10, -15, -20, -30 A2PC 108, 108-1, -2, -3, -5 A-767 Viking Air Limited DHC-2 MK I, DHC-2 Mk II, DHC-2 Mk III A806 DHC-3 A815 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 (5/14) Page 12 of 13 FEDERA ADMINIST VIATION RATION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Aircraft Manufacturer (Continuation Sheet) Number SA800EA June 19, 2019 Model Type Certificate Viking Air Limited (continued) DHC-6-1, DHC-6-100, DHC-6-200, DHC-6-300 A9EA NOTES TO ELIGIBILITY LIST: *1. Aircraft as marked require specific attention to proper balancing of the rudder. Refer to the Manufacturer's Service Manual for balancing instructions. **2. Installations on these aircraft require prior or concurrent installation of STC SA4-977. 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 Fom 8110-2 (5/14) Page 13 of 13