# TCDS A-815: De Havilland Aircraft of Canada Limited - Type: Type certificate data sheet - Status: Current - Holder: De Havilland Aircraft of Canada Limited - Revision: 7 - Revised: October 19, 2026 - Product: Aircraft, Small Airplane - Certification basis: CAR 3, CAR 10 - Registered aircraft: 76, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b2/eb/b2ebc0f578172e8775e386c3746190a0c56f6498285cc1066e2a40a732bcd210 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137592319120261019144508.0001 - Page: https://openairdocs.org/tcds/A-815 ## Models (1) As the data sheet lists them. - DHC-3 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-815 Type Certificate Holder De Havilland Aircraft of Canada Limited 4100 Westwinds Drive NE Calgary, Alberta Canada T3J 4L2 Type Certificate Holder Record Viking Air Limited 9574 Hampden Road Sidney, British Columbia Canada V8L 5V5 Bombardier Inc. Regional Aircraft 123 Garratt Boulevard Downsview, Ontario, Canada M3K 1Y5 de Havilland, Inc. 123 Garrett Boulevard Downsview, Ontario, Canada M3K 1Y5 I - Model DHC-3, 16 PCL-SM (Normal Category) (U.S. Military Model U-1A, see Note 4) Engine. P&W Wasp S3H1-G, S1H1-G, R-1340-59 or R-1340-61 Fuel. 80/87 Min. grade aviation gasoline - see Fluid Specification Part 1 DHC-3 Maintenance Manual Oil. See Fluid Specification Part 1 DHC-3 Maintenance Manual Engine limits. S3H1-G, R- 1340-59 HP RPM MP (IN. HG.) ALT. Takeoff (one minute) 600 2250 36.0 - Maximum continuous 550 2200 33.5 S.L. 550 2200 32.5 5000 ft. S1H1-G, R-1340-61 Takeoff (one minute) 600 2250 36.0 - Maximum continuous 550 2200 35.0 S.L. 550 2200 33.0 8000 ft. Propeller and Propeller - Hamilton Sta ndard, Counterweight, Hub Model 3D40 propeller limits. (c/w 4.5 CTWT) Blade Models - 6511A-9X, 6529A-9X or 6631A-9 Pitch Setting - Low 19 degrees, High 33 degrees Propeller - Hamilton Standard, Hydromatic Hub Model 23D40 Blade Models - 6511A-9, 6529A-9 or 7035A-9 Pitch Setting - Low 18.5 degrees, High 34.5 degrees Constant Speed Governor 1A2-G5 for Counterweight Propeller, and 4B2-1 for Hydromatic Propeller Airspeed limits (TIAS). Landplane & Skiplane (mph) (knot) Seaplane (mph) (knot) Never exceed 192 167 183 159 Maneuvering 126 110 126 110 Center of Gravity Flaps extended Landplane 94 82 94 82 (C.G.) range.(+131.9) to (+151.4) at 6600 lb. or less (In) (+135.8) to (+151.4) at 7600 lb. (+135.8) to (+149.8) at 8000 lb. Landplane with Mod. 3/746 (Item 104) (+131.9) to (+152.2) at 6600 lb. or less (+135.8) to (+152.2) at 7600 lb. (+135.8) to (+152.2) at 8000 lb. Page No. 1 2 3 4 Rev. No. 7 4 6 4 A-815 Revision 7 De Havilland (Otter) DHC-3 October 19, 2026 A-815 Page 2 of 4 Skiplane (+131.9) to (+151.4) at 6600 lb. or less (+135.8) to (+151.4) at 7600 lb. (+135.8) to (+149.8) at 8000 lb. Seaplane (+131.9) to (+148.3) at 6600 lb. or less (+135.8) to (+148.3) at 7600 lb. (+138.1) to (+148.3) at 8000 lb. (with items 104 and 105) Straight line variation between points given Datum 60 in. fwd. of firewall Leveling Means Cabin floor level laterally and longitudinally Maximum weight Landplane: 7600 lb. 8000 lb. (With items 102, 103, 201, 400; or items 104 and 105) Skiplane: 7600 lb. (With item 300(a), (b), (c), (d), or (e)) 8000 lb. (With item 300(a), (b), (c), or (e) and 102, 103, 201 and 400) Seaplane: 7200 lb. (With item 100) 7967 lb. (With items 100,101, 102 and 103) 8000 lb. (With items 104 and 105) Mean Aerodynamic Chord 78 inches Minimum Crew 1 pilot No. of seats 16 including pilot. (See approved load ing instructions in Flight Manual, Section 4.7, for various arrangements.) Baggage and Cargo See Approved Loading In structions, Flight Manual, Section 4.7 Fuel capacity 214 U.S. gal. (178 Im p. gal.) total (under cabin floor): Front tank 61 U.S. gal. (51 Imp. gal.) (+121 in.) Center tank 102 U.S. gal. (85 Imp. gal.) (+154 in.) Rear tank 50 U.S. gal. (42 Imp. gal.) (+184 in.) Oil capacity 10.8 U.S. gal. (9 Imp. gal.) (+100 in.) Control surface movements Post-Mod. 3/744 Tailplane Up 4 1/2° + 1/2° Down 3 1/2° + 1/2° Elevator Up 23°, +2°, -1° Down 15°, +2°, -1° (Tailplane neutral) Elevator trim tab Up 5° + 1° Down 5° + 1/2° Elevator servo tab Up 10° + 1° Down 23° + 1° Ailerons Up 26 1/2° + 1° Down 18 1/2° + 1° Flaps Inboard leading Down 35° + 2° Inboard trailing Down 60° + 2° Outboard leading Down 26° + 2° Rudder Right 25° + 1° Left 25° + 1° Rudder trim tab Right 19° + 1° Left 19° + 1° Serial Nos. eligible 1 and subsequent. The Canadian Certificate of Airworthiness for Export must be submitted for each individual aircraft for which application for certification is made. (Not required for those surplus military aircraft certificated in accordance with NOTE 4.) Certification Basis Type Certificate No. 815 issued under CAR 10. (ICAO Annex 8, 2nd Edition (Transport Category D), and CAR 3 as amended to November 1, 1949 Equipment Essential equipment, which may not be removed unless replaced by approved equivalent items, is listed in DH Canada Report AEROC 3.1.G.7 Issue 1. Removable items are listed in the Flight Manual and the Weight and Balance Report contained therein must be corrected to show any changes. Miscellaneous 100: Edo 55-7170A or Bristol Model 903 Float Installation to Edo Drawing 12700 101: Ventral Fin to Bombar dier Modification 3/337 102: Wing Stall Plates to Bo mbardier Modification 3/272 103: Wing Stall Bar to Bombardier 3/544 104: Dual Wing Stall to Bombardier Modification 3/746 105: DHC-3 Amphibious Gear Installati on to Bombardier Modification 3/700 200: 11.00 x 12 Main wheel tires and tubes 6.00 x 6 Tail wheel tire and tube A-815 Page 3 of 4 201: Tailwheel hydraulic shock absorb er to Bombardier Modification 3/475 202: Canoe Carrying Installations With items 100, 101, 102 and 103 (a) Bombardier Modification No. 3/456 Starboard Side (See Note 3) (b) Ontario Provincial Air Services Universal Carrier Drawing No. 1561-0 with method of attachment to Drawing 1561-0-1. Canoe not to exceed 17'-0" in length, 3'-6" beam, and 160 lb. The aircraft gross weight is limited to 7647 lb. with the Aft C.G. Limit at 145 inches aft of the datum. (c) Ontario Provincial Air Services Universal Carrier Drawing No. 1561-0 with method of attachment to Drawing No. 1561-0- 1. Boat not to exceed 14'0" in length, 5'0" beam and 300 lb. Boat position: C.G. of boat at station 130. The aircraft gross weight is limited to 7048 lb. with the Aft C.G. Limit at 145 inches aft of datum. The maximum flap angle is limited to the takeoff setting. With items 104 and 105 (c) Dehavilland Drawing C3-M-70, Starboard side. Canoe not to exceed 17'- 0" in length, 3'-6" beam and 160 lb. The aircraft gross weight is limited to 7680 lb. Centre of canoe to be located at Station 196. 203: Lumber and Freight Carrying Installation (a) Ontario Provincial Air Services Universal Carrier Drawing No. 1561-0 with method of attachment to Drawing No. 1561-0-2. Lumber or freight must not exceed 18'-0" in length; 12" in width, 2'-0" in height and 1600 lb. in weight. Lumber or freight must be symmetrically distributed by weight and dimensions on each side of the aircraft with the fore and aft distribution midway between the strut ar ms. The aircraft gross weight is limited to 7863 lb. with the aft C.G. limi t at 144.8 inches aft of the datum. The maximum flap angle is limited to the take-off setting. 204: Water Dropping Tank Installations With items 100, 101, 102 and 103 (a) Bombardier Modification SOO/3009 with drawings C3-M-153 and C3-M-154. (b) Ontario Provincial Air Services Drawing No. 2436. The aircraft gross weight is limited to 7967 lb. with the aft C.G. limit at 143.5 inches aft of datum. With items 104 and 105 (a) Bombardier Drawing C3-M-153 The aircraft gross weight is limited to 8000 lb. with the aft C.G. limit at 141.0 inches aft of datum. 300: Ski Installations (a) Bombardier Drawing No. C3-US-1 Use (b) Bombardier Retractable Ski to Drawing No. Actual C3-US-100, Issue 1 Weight (c) Federal AWB-8000 wheel-skis to Federal and Aircraft Works' Drawing No. 11R 1010 change "C" Balance (d) Ontario Provincial Air Services Drawing 1872 Change (e) Ontario Provincial Air Services Drawing 1861-1 400: Rework Bulkhead at sta. 444.38 to Bombardier Modification No. 3/396 NOTE 1. Refer to Approved Flight Manual for specific information. The Flight Manual shall include an approved Weight and Balance Report and shall be carried in the aircraft at all times. NOTE 2. The following placards must be displayed as noted: (a) Instruments shall be placarded to show all normal operating ranges and limitations. (b) All doors shall be placarded on the inside: "Exit - Turn to Release". (c) In front and in clear view of pilot: "THIS AEROPLANE MUST BE OPERATED IN COMPLIANCE WITH THE OPERATING LIMITATIONS SPECIFIED IN THE APPROVED DEHAVILLAND DHC-3 FLIGHT MANUAL." A-815 Page 4 of 4 NOTE 3. Canoe Carrying Installation on starboard side of aircraft to Bombardier Modification No. 3/456. Canoe not to exceed 16'6" length, 3'6" beam and 100 lb. NOTE 4. Those surplus military Bombardier Model U-1A aircraft, identified by civil and military serial numbers in Bombardier Report QA/DHC-3/G13, are eligible for a U.S. Standard Airworthiness Certificate without requiring a Canadian Certificate of Airworthiness for Export when all of the following conditions have been satisfied: (a) Aircraft records must indicate, or a determination must be made, that the aircraft has been subjected to FAA initial screening inspection. The screening inspection record must show that the aircraft has a reasonable potential for standard certification. (Those aircraft dispositioned as havi ng no reasonable potential for standard certification are not certifiable. These aircraft are sold by U.S. Department of Defense only for the purpose of "Recovery of Parts or Reduction to Scrap".) (b) The aircraft must be converted to Bombardier Model DHC-3 in accordance with Bombardier Modification SOO- 3028, Issue 6, and Bombardier Service Bulletin 3/21, Original Issue. (c) The applicant shows and the FAA finds that the aircraft conforms to the type design and is in a condition for safe operation. (d) A satisfactory "100 hour" type inspection has been accomplished and recorded. (e) Any deviations to the type design must be appropriately approved by an FAA Supplemental Type Certificate or other methods acceptable to the FAA. Upon satisfying all the foregoing conditions, and when all other pertinent U.S. regulatory requirements have been met, a U.S. Standard Airworthiness Certificate may be issued. (Certification basis is FAR 21.183(c) since these are import aircraft.) Technical data needed for conversion purposes are available to the applicant through Bombardier of Canada Limited. Inquiries for this data should be submitted to The Product Support Department, Bombardier of Canada, Limited, Downsview, Ontario, Canada. -END- ``` ## ADs (32, in force first) - [AD 2025-17-08](https://openairdocs.org/ad/2025-17-08): Elevator Structure · Viking Air DHC-3. Effective Sep 29, 2025 - [AD 2023-22-17](https://openairdocs.org/ad/2023-22-17): Engine Mount Section · Viking Air DHC-3. Effective Jan 19, 2024 - [AD 2023-18-03](https://openairdocs.org/ad/2023-18-03): Flight Control System · Viking Air DHC-3. Effective Oct 24, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2022-21-51](https://openairdocs.org/ad/2022-21-51): Elevator Structure · Viking Air DHC-3. Effective Dec 1, 2022 - [AD 2022-05-11](https://openairdocs.org/ad/2022-05-11): Wing Structure · Viking Air DHC-3. Effective Apr 13, 2022 - [AD 2021-24-18](https://openairdocs.org/ad/2021-24-18): Wing Structure · Viking Air DHC-3. Effective Jan 24, 2022 - [AD 2018-21-02](https://openairdocs.org/ad/2018-21-02): Wings · Viking Air DHC-3. Effective Nov 28, 2018 - [AD 2016-10-03](https://openairdocs.org/ad/2016-10-03): Leveling and Weighing · Viking Air DHC-3. Effective May 31, 2016 - [AD 2015-24-02](https://openairdocs.org/ad/2015-24-02): Wings · Viking Air DHC-3. Effective Jan 4, 2016 - [AD 2014-17-01](https://openairdocs.org/ad/2014-17-01): Stabilizers · Viking Air DHC-3. Effective Sep 16, 2014 - [AD 2011-18-11](https://openairdocs.org/ad/2011-18-11): Flight Controls · Viking Air DHC-3. Effective Oct 3, 2011 - [AD 2011-12-02](https://openairdocs.org/ad/2011-12-02): Placards and Markings · Viking Air DHC-3 with STC SA09866SC. Effective Jun 2, 2011 - [AD 2008-12-12](https://openairdocs.org/ad/2008-12-12): Ignition connector plug · Viking Air DHC-2 Mk.I, DHC-2 Mk.II and DHC-3. Effective Jul 23, 2008 - [AD 2005-25-08](https://openairdocs.org/ad/2005-25-08): Electronic Flight Information System (EFIS) · B-N Group BN-2A, 172, 180 and 22 more. Effective Jan 23, 2006 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-24-10](https://openairdocs.org/ad/2004-24-10): Heating blankets on P3 and PY pneumatic lines · Viking Air DHC-3. Effective Jan 6, 2005 - [AD 2004-24-01](https://openairdocs.org/ad/2004-24-01): Elevator servo tab assembly · Viking Air DHC-3. Effective Dec 28, 2004 - [AD 2004-05-01 R1](https://openairdocs.org/ad/2004-05-01-R1): Elevator servo-tab · Viking Air DHC-3. Effective May 25, 2004 - [AD 98-18-08](https://openairdocs.org/ad/98-18-08): Voltage Regulator, Voltage-Ammeter Gauge, and Auxiliary Bus Systems · Viking Air DHC-3 with STC SA3777NM. Effective Oct 10, 1998 - [AD 96-09-04](https://openairdocs.org/ad/96-09-04): Tailplane Main Rib Forward & Lower Flanges · Viking Air DHC-3. Effective May 17, 1996 - [AD 92-08-08](https://openairdocs.org/ad/92-08-08): Fuel Condition Lever Lock · Viking Air DHC-3. Effective May 18, 1992 - [AD 88-15-08](https://openairdocs.org/ad/88-15-08): Utility Seat Forward Leg · Viking Air DHC-3. Effective Aug 27, 1988 - [AD 86-16-12](https://openairdocs.org/ad/86-16-12): Elevator Pushrod Inspection · Viking Air DHC-3. Effective Aug 15, 1986 - [AD 83-04-05](https://openairdocs.org/ad/83-04-05): Control Column Lower Assembly · Viking Air DHC-3. Effective Mar 1, 1983 - [AD 83-02-01](https://openairdocs.org/ad/83-02-01): Wing Strut Tiebar · Viking Air DHC-3. Effective Feb 3, 1983 - [AD 76-08-05](https://openairdocs.org/ad/76-08-05): Various Modifications · Viking Air DHC-3. Effective Apr 29, 1976 - [AD 56-17-02](https://openairdocs.org/ad/56-17-02): Flap Control Restriction · Viking Air DHC-3 - [AD 2022-23-08](https://openairdocs.org/ad/2022-23-08) (historical): Elevator Structure · Viking Air DHC-3. Effective Nov 2, 2022 - [AD 2011-05-02](https://openairdocs.org/ad/2011-05-02) (historical): Flight Controls · Viking Air DHC-3 with STC SA01059SE. Effective Mar 31, 2011 - [AD 2004-21-06](https://openairdocs.org/ad/2004-21-06) (historical): Firewall Connector Plugs Lockwire Security · Viking Air DHC-3, DHC-2 Mk.I and DHC-2 Mk.II. Effective Dec 6, 2004 - [AD 2004-05-01](https://openairdocs.org/ad/2004-05-01) (historical): Elevator servo-tab · Viking Air DHC-3. Effective Apr 20, 2004 ## Registered aircraft by registry model (OpenAirDocs) - [Dehavilland DHC-3](https://openairdocs.org/model/dehavilland-dhc-3): 67 aircraft (registry codes 2802412, 2800202, 2802414) - [Dehavilland Canada DHC-3](https://openairdocs.org/model/dehavilland-canada-dhc-3): 8 aircraft (registry code 2821704) - [Dehavilland-Hansen DHC-3](https://openairdocs.org/model/dehavilland-hansen-dhc-3): 1 aircraft (registry code 2802411) ## STCs approved under this data sheet (149, first 50) - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA12291AK](https://openairdocs.org/stc/SA12291AK): Tail Wheel Fork Installation. Rust’s Flying Service - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA09857SC](https://openairdocs.org/stc/SA09857SC): Installation of GE Aviation Czech s.r.o. Turboprop Model M601E-11 or H75-200 engines. Stolairus Aviation Inc. - [STC SA02533NY](https://openairdocs.org/stc/SA02533NY): Installation of Harbour Air Ltd. PanaVue Windows. Harbour Air Ltd. - [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc. - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA02343NY](https://openairdocs.org/stc/SA02343NY): Installation of International Aeroproducts IntAero 8100-200 Floats using the 55-7170 attachment. Harbour Air Ltd. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA00139IB](https://openairdocs.org/stc/SA00139IB): Installation of Ski Shackles. Bartel Mechanical and Aerospace - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA02761SE](https://openairdocs.org/stc/SA02761SE): Installation of a new clamp nut and safety wire on the horizontal stabilizer trim actuator. Kenmore Air Harbor LLC - [STC SA02570AK](https://openairdocs.org/stc/SA02570AK): Installation of large tailwheel fork P/N YCAC3UT85-3 per YCAC3UT144 Large Tail Wheel Maintenance Manual Supplement. Hans Munich - [STC SA00082IB](https://openairdocs.org/stc/SA00082IB): Installation and fabrication of the Front Fuel Feeder Tank. Aerotech Industries Limited - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc. - [STC SA4-183](https://openairdocs.org/stc/SA4-183): Installation of VIP P/N 101-79 engine mount.. FTG, Inc. - [STC SA02561AK](https://openairdocs.org/stc/SA02561AK): Maximum Gross Weight Increase to 8367 lbs.. Rust's Flying Service Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA02489AK](https://openairdocs.org/stc/SA02489AK): Aft Center of Gravity Envelope Expansion. Rust's Flying Service Inc - [STC SA04701NY](https://openairdocs.org/stc/SA04701NY): Replacement of Fixed Wing Control Cables. Thunder Bay Aviation Ltd - [STC SA04658NY](https://openairdocs.org/stc/SA04658NY): Manufacturing and Installation of the Fuselage Attachment. Aerotech Industries - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02543AK](https://openairdocs.org/stc/SA02543AK): Installation of Harbour Air Ltd. cabin seats and seat track. Talkeetna Aero Svcs Inc - [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems - [STC SA04561NY](https://openairdocs.org/stc/SA04561NY): Install Part 1 - Harbour Air Ltd. Water Rudder Blade, Pulleys and Fairlead Assemblies. Harbour Air Ltd. - [STC SA04560NY](https://openairdocs.org/stc/SA04560NY): Manufacture of the Door Latch Modification. Harbour Air Ltd. - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA02547NY](https://openairdocs.org/stc/SA02547NY): Improved Strut Assembly - Float. Aerotech Industries - [STC SA5190NM](https://openairdocs.org/stc/SA5190NM): Installation of Gustin Aviation chip detector light system.. A & L Aircraft Parts Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA02653SE](https://openairdocs.org/stc/SA02653SE): Installation of a wing lift struts. Kenmore Air Harbor LLC - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.. Whelen Aerospace Technologies - [STC SA00104SE](https://openairdocs.org/stc/SA00104SE): Installation of automatic EPA fuel drain system.. Kenmore Air Harbor LLC - [STC SA00155SE](https://openairdocs.org/stc/SA00155SE): Installation of one-piece aluminum lever/fitting on elevator servo tab.. Kenmore Air Harbor LLC - [STC SA02250SE](https://openairdocs.org/stc/SA02250SE): Installation of a Cleveland Wheel and Brake Kit Number 199-92,. Kenmore Air Harbor LLC - [STC SA02542SE](https://openairdocs.org/stc/SA02542SE): Installation of a Lower Fuselage Tie Bar Assembly. Kenmore Air Harbor LLC - [STC SA02604SE](https://openairdocs.org/stc/SA02604SE): Fabrication of Kenmore Air Harbor, Inc. windshield posts. Kenmore Air Harbor LLC - [STC SA4345NM](https://openairdocs.org/stc/SA4345NM): Installation of a one to nine passenger configuration.. Kenmore Air Harbor LLC - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine All 149: https://openairdocs.org/tcds/A-815/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.