STC SA800EA

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA800EA

FAA Form 8110-2 (5/14) Page 1 of 13 This certificate issued to:

Whelen Aerospace Technologies 51 Winthrop Road Chester, Connecticut 06412-0684 Part 3, 6, 23, and 27 of the Civil Air / Federal; Aviation Regulations.

Original Product - Type Certificate Number: See attached Eligibility List dated May 2, 2018.

Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, Part Numbers 01-0770019-( ), 01-0770024-( ), 01-0770030-( ), 01-0770031-( ), 01-0770032-( ), 01- 0770053-( ), 01-0770054-( ), 01-0770058-( ), 01-0771011-( ), 01-0771110-( ), 01-0790725-(), 01- 0790701-(), 01-0771554-(), 01-0771774-(), 01-0771900( ), and applicable associated power supplies, in accordance with Whelen Anti-Collision Light Systems Installation and Service Manual, Document No. 05131, Rev E, dated May 2019, or later FAA-approved revision.

Limitations and Conditions: See Page 3

Date of Application: May 2, 1969 Date of Issuance: November 14, 1969 Date reissued: June 12, 2026 Date amended: June 19, 2019 By direction of the Administrator Signature Michael Linegang Manager, East Certification Branch Title

FAA Form 8110-2 (5/14) Page 2 of 13

To (Name and address of transferee) Name:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Name:

Address (Number and Street, City, State, and ZIP Code):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8110-2 (5/14) Page 3 of 13 Limitations and Conditions:

1. The Anti-Co llision Lights Part Numbers 01-0770019-( ), 01-0770024-( ), 01-0770030-( ), 01- 0770031-( ), 01-0770032-( ), 01-0770053-( ), 01-0770054-( ), 01-0770058-( ), 01-0771011-( ), 01-0771110-( ) meet the requirements of FAR 23 and the similarly numbered sections of FAR 27 as follows:

a. 23.1397(c), 23.1401(c), (d), (e), effective August 11, 1971

b. 23.1401(f) in effect on August 10, 1971

c. Part numbers 01-0770019-19 and 01-0770019-22 with power supplies approved under STC SA615EA meet FAR 23.1401(f) effective August 11, 1971

d. Part numbers 01-0770054-00 through 01-0770054-07, 01-0770058-03, and 01- 0770058-13 with power supplies producing a minimum of 20 joules per flash meet FAR 23.1401(f) effective August 11, 1971

2. The Anti-Collision/Position Lights Part Numbers 01-0790725-(), 01-0790701-(), 01- 0771554-(), 01-0771774-(), 01-0771900( ) meet the following 14 CFR Part 23 and 14 CFR Part 27 requirements at the amendment indicated:

a. 23.25(a) [Amdt. 23-50], 23.853(a)(d)(3)(iv) [Amdt. 23-62], 23.867(a) [Amdt. 23-49],

23.1301 [Amdt. 23-62], 23.1309(a)(c) [Amdt. 23-62], 23.1351(a) [Amdt. 23-49],

23.1357(a) [Amdt. 23-43], 23.1365(a) [Amdt. 23-49], 23.1367(a) [Amdt. 23-0],

23.1385 [Amdt. 23-43], 23.1387 [Amdt. 23-43], 23.1389 [Amdt. 23-43], 23.1391 [Amdt. 23-43], 23.1393 [Amdt. 23-43], 23.1395 [Amdt. 23-43], 23.1397 [Amdt. 23- 11], 23.1401 [Amdt. 23-49], 23.1529 [Amdt. 23-26]

b. 27.25(a) [Amdt. 27-44], 27.853(a) [Amdt. 27-37], 27.1301 [Amdt. 27-0], 27.1309 [Amdt. 27-46], 27.1351(a) [Amdt. 27-13], 27.1357(a) [Amdt. 27-13], 27.1365(a) [Amdt. 27-35], 27.1367(a) [Amdt. 27-0], 27.1385 [Amdt. 27-0], 27.1387 [Amdt. 27-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8 110-2 (5/14) Page 4 of 13 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 TUR

NED OFF DURING ALL NIGHT TAKEOFFS AND LANDINGS.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12 , 2026

FAA Form 8110 -2 (5/14) Page 5 of 13

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 Manua l”, 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.

FAA Form 8110-2 (5/14) Page 6 of 13 (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026 AMENDMENT HISTORY:

This STC has been previously amended on the following dates:

11/20/69; 4/23/70, 12/10/7 0; 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; 5/1 7/79; 3/26/81, 8/5/81, 8/25/81; 5/21/8 2; 7/16/91; 11/22/93; 6/7/99;

6/18/99; 9/8/99, 6/17/05, 5/5/10, 12/5/14

FAA Form 8110-2 (5/14) Page 7 of 13 Aircraft Manufacturer Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026 Eligibility List May 2, 2018 Model Type Certificate Aero Commander *100, 100‐180 1A21 111 A11SO 112 A12SO 500, 500‐A, 500‐B, 500‐S, 500‐U, 520, 560, 560A, 560E 6A1 560F, 680, 680E, ‐F, 720, 680FL, 680FL(P), 680T, V, W, 681, 690, 685 2A4 American Aviation *AA‐1, *AA‐1A A11EA AA‐5 A16EA Beec h 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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8110-2 (5/14) Page 8 of 13 Aircraft Manufacturer Model Type Certificate Beech (continued) 50(L‐23A), B50(L‐23B), C50, D50(L‐ 23E), D50A, D50B , D50C, D50E, E50(L‐ 23D, RL‐23D), F50, G50, H50, J50 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 3A20 60, A60 A12CE 99, 99A, 100 A14CE Bellanca 14‐19‐3A, 17‐30 1A3 17‐30A, 17‐31A, 17‐31ATC A18CE 7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KCAB A‐759 Bell 206A, 206B, 206L, 206L‐1, 206L‐ 3, 206L‐4, 407 H2SW 47B, B 3, D, D1, E, G, G‐2, H‐1 H‐1

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8 110-2 (5/14) Page 9 of 13 Aircraft Manufacturer Model Type Certificate Bell (continued) 47G‐2A, ‐2A‐1, ‐3, ‐3B, ‐3B‐1, ‐3B‐27, 4, ‐4A, ‐5, ‐5A 2H3 47J, K, J‐2, J‐2A 2H1 Britten Norman BN‐2, ‐2A, ‐2A‐2, ‐2A‐6, ‐2A‐8 A17EU BN‐2A, MK.III A29EU Cessna 120, 140 A‐768 140A 5A2 150, 150A, B, C, D, E, F, G, H, J, K, L, M, A150K, A150L, A150M, 152, A152 3A19 170, 170A, 170B A‐799 172, 172A, B, C, D, E, F, G, H, I, K, L, M, N, P 3A12 175, 175A, B, C, P172D, 172RG 3A17 177, 177A, B A13CE 177RG 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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 811 0-2 (5/14) Page 10 of 13 Aircraft Manufacturer Model Type Certificate Cessna (continued) 3A24 A9CE A‐790 A4CE A16CE 3A21 185, 185A, B, C, D, E, A185E, A185F 188, 188A, B, A188, A188A, A188B, T188C 190, 195, 195A, B 206, P206, P206A, B, C, D, E, TU206A, B, C, D, E, F, G, TP206A, B, C, D, E, U206, U206A, B, C, D, E, F, G 207, 207A, T207, T207A 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, 210‐5(205), 210‐5A(205A), T210K, 210L, T210L, T210M, T210N , 210N, P210N 310, 310A, B, C, D, E, F, G, H, I, J, 310J‐ 1, E310J, 310K, L, N, P, T310P, 310Q, T310Q 3A10 *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

FAA Form 8110-2 (5/14) Page 11 of 13 Aircraft Manufacturer (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026 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, 300 A9EA Fairchild Hiller FH‐1100 H2WE Grumman G‐164, G‐164A, G‐164B 1A16 Helio H‐250, H‐295, H‐391, H‐391B, 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‐16S 1A1 **PA‐17 A‐805 **PA‐18 Series, PA‐19, PA‐19S 1A2 **PA‐20 Series 1A4

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8110-2 (5/14) Page 12 of 13 Aircraft Manufacturer Model Type Certificate Piper (continued) **PA‐22 Series 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, ‐28S‐160, ‐28R‐180, ‐28S‐180, ‐28‐181, ‐28R‐ 200, ‐28R‐201, ‐28R‐201T, ‐28RT‐201, ‐28RT‐201T, ‐28‐201T, ‐28‐236 2A13 PA‐30, PA‐39 A1EA PA‐31P A8EA PA‐31, PA‐31‐300, 325, 350 A20SO PA‐32‐260, ‐300, ‐32S‐300 A3SO Mooney M20B, C, D, E, F, G 2A3 Mitsubishi MU‐2B, MU‐2B‐10, ‐15, ‐20, ‐30 A2PC Univair (Stinson) 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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA800EA Amended June 19, 2019 Reissued June 12, 2026

FAA Form 8 110-2 (5/14) Page 13 of 13 Aircraft Manufacturer 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 f or balancing instructions.

**2. Installations on these aircraft require prior or concurrent installation of STC SA4-977.