# TCDS 1A1: Piper Aircraft Inc. - Type: Type certificate data sheet - Status: Current - Holder: Piper Aircraft Inc. - Revision: 13 - Revised: August 7, 2006 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 276, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/5c/eb/5ceb0f65d29b044e3c1cf421aa4e2d706b47a961d9cb46d0ad2125d4e13569db - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6F02ECA7D3DE8A3D8625720900718F4D.0001 - Page: https://openairdocs.org/tcds/1A1 ## Models (2) As the data sheet lists them. - PA-16 (Clipper) - PA-16S ## 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 1A1 Revision 13 Piper Aircraft, Inc PA-16 PA-16S August 7, 2006 AIRCRAFT SPECIFICATION NO. 1A1 Type Certificate Holder Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 Type Certificate Holder Record The New Piper Aircraft, Inc transferred TC 1A1 to Piper Aircraft, Inc on August 7, 2006 I - Model PA-16; 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved October 18, 1948 Engine Ly coming O-235-C1 Fuel 80 minimum octane aviation gasoline Engine Limits Take-off (one minute), 2800 r.p.m. (115 hp) with Item 3 propeller only All other operations, 2600 r.p.m. (108 hp) Airspeed Limits Maneuvering (Normal Category) 105 mph (91 knots) (True Indicated) Maneuvering (Utility Category) 108 mph (94 knots) Max. Structural Cruising 117 mph (102 knots) Never exceed 140 mph (122 knots) C. G. Range Normal Category: (+11.5) to (+23.0) at 1650 lbs. (+10.0) to (+23.0) at 1175 lbs. or less Utility Category: (+10.7) to (+15.5) at 1400 lbs. (+10.0) to (+15.5) at 1175 lbs. or less Straight line variation between points given. 10 12 14 16 18 20 22 1000 1200 1400 LBS. INCHES 1400 1600 22 24 UTILITY CATEGORY NORMAL CATEGORY Gross Weight Empty Weight C. G. Range None Maximum Weight Normal Category: 1650 lbs. Page No. 1 2 3 4 5 Rev. No. 13 11 11 9 10 1A1 2 of 5 Utility Category: 1400 lbs. Number of Seats 4 (2 at +18 to +21 and 2 at +49) Rear seat not to be used when operating in Utility Category. Maximum Baggage 50 lbs. (+67) in Normal Category only. Fuel Capacity 30 gallons (12 gallons fuselage tank at (-8) and 18 gallons left wing tank at (+24)) Oil Capacity 1½ gallons (-29) Control Surface Stabilizer 1° Up 6½° Down . Movements Elevator 26° Up 10° Down Aileron 12° Up 12° Down Rudder 16° Right 16° Left Serial Numbers Eligible 16-1 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: Items 1, 201(a), 202(a), 204(a), and 401(a). Skiplane: Items 1, 205, 401(a) and (b). II - Model PA-16S; 3 PCSM (Normal Category Only); Approved July 20, 1949 Engine Ly coming O-235-C1 Fuel 80 minimum octane aviation gasoline Engine Limits For all operations, 2600 r.p.m. (108 hp) Airspeed Limits Maneuvering 105 mph (91 knots) (True Indicated) Max. Structural Cruising 117 mph (102 knots) Never Exceed 140 mph (122 knots) C. G. Range (+14.0) to (+20.0) at 1738 lbs. (+10.0) to (+20.0) at 1300 lbs. or less Straight line variation between points given. 8 101 21 41 6 182 0 1300 1500 1700 INCHES FRONT LIMIT REAR LIMIT Gross Weight (lbs.) Empty Weight C. G. Range None Maximum Weight 1738 lbs. Number of Seats 3 (2 at +18 to +21 and 1 at +49) Maximum Baggage 50 lbs. (+67) 3 of 5 1A1 Fuel Capacity 30 gallons (12 gallon fuselage tank at -8 and 18 gallon left wing tank at +24) Oil Capacity 1½ gallons (-29) Control Surface Stabilizer 1° Up 6½° Down Movements Elevator 26° Up 10° Down Aileron 12° Up 12° Down Rudder 16° Right 16° Left Serial Numbers Eligible 16-1 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Items 4, 105, 209, and 401(d). Specifications Pertinent to All Models Datum Wing leading edge Leveling Means Plumb from hole in upper channel of front door to center punch mark on front seat cross tube. Certification Basis Type Certificate No. 1A1 (CAR 3) Production Basis Approved for manufacture of spare parts only under Production Certificate No. 206. Export Eligibility Deleted as of - August 14, 1995. Equipment A plus (+) or minus (-) sign preceding the weight of an item of equipment indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. Propellers and Propeller Accessories 1. Propeller - Sensenich Model 74FM56, or any other fixed pitch wood propeller eligible for the engine power and speed and which meets the following limits: (Landplane and skiplane only): Static r.p.m. at max. permissible throttle setting: Not over 2400, not under 2050. No additional tolerance permitted. Diameter: Not over 74 inches, not under 70.5 inches. +11 lbs. (-50) *2. Propeller - fixed pitch metal, McCauley Model 1C90-LM-7254 or any other Model 1C90-LM propeller which meets the following limits: Landplane and skiplane only: Static r.p.m. at max. permissible throttle setting: Not over 2290, not under 2180. No additional tolerance permitted. Diameter: Not over 72 inches, not under 70.5 inches. Item 401(c) required. +23 lbs. (-50) *3. Propeller - Koppers Aeromatic (Landplane and skiplane only) (a) F200/00-73E; Parts List Assembly No. 4368 or 4368-1. Koppers Installation Procedure & Operating Limitations No. 34. +19 lbs. (-50) (b) F200/00-74E; Parts List Assembly No. 4292A or 4292A-1. Koppers Installation Procedure & Operating Limitations No. 16B. +32 lbs. (-50) (c) F200-H/00-73E; Parts List Assembly No. 4368H or 4368H-1. Adjustment Instructions & Operating Limitations No. 52A. +33 lbs. (-50) Altitude control Assembly No. 4382 +6 lbs. (-35) 1A1 4 of 5 Propellers and Propeller Accessories (cont.) (d) F200-H/00-74E; Parts List Assembly No. 4292AH-1 Instructions & Operating Limitation No. 52A. +34 lbs. (-50) Altitude Control Assembly No. 4382 +6 lbs. (-35) Diameter: (a), (c) Not over 73 inches, not under 71.5 inches (b), (d) Not over 74 inches, not under 72.5 inches Low pitch settings at 24 in. station: (a), (c) 10.4° (b), (d) 11.0° Static r.p.m. at max. permissible throttle setting (No additional tolerance permitted): (a), (b) Not over 2750, not under 2700 (c), (d) Not over 2800, not under 2750. The following note must be inserted in the Airplane Flight Manual: "Aeromatic Propeller Model - (a, b, c, or d as applicable) - Installation and operation must be accomplished in accordance with Koppers 'Installation Procedure (or Adjustment Instructions) and Operating Limitations No. ----' " (as applicable) (Items 103 and 401(c) also required). *4. Propeller - fixed pitch metal, Sensenich M76AM-2 or -3 with following diameter and static r.p.m. limits at max. permissible throttle setting (no additional tolerance permitted): (a) Landplane and skiplane (Item 401(c) required): Static r.p.m.: Not over 2500, not under 2150 Diameter: Not over 74 inches, not under 71.5 inches (b) Seaplane (Item 401(d) required): Static r.p.m.: Not over 2500, not under 2400 Diameter: Not over 74 inches, not under 72.5 inches +24 lbs. (-50) *5. Propeller - two-position controllable, Sensenich Hub CS-2FM6-1, with PC276A7-2 blades (Landplane and skiplane only). Diameter: Not over 74 inches, not under 72.5 inches Blade pitch settings at 3/4 radius (28.5 in. station): Low 11.8°, High 15.3° Prop. control installation required per Sensenich Dwg. D-3028. Items 104 and 401(c) required. +27 lbs. (-50) Engines and Engine Accessories - Fuel and Oil Systems 101. Starter - Delco-Remy 1109657 (with Bendix Unit) +17 lbs. (-42) 102. Starter and generator drive +6 lbs. (-42) *103. Oil sump baffle and blast tube, Koppers Company, Inc., Dwg. No. 3351 (required with Propeller Item 3) *104. Oil sump baffle, Sensenich Dwg. No. D-3028, Revision C, required with propeller Item 5. 105. Seaplane bottom engine cowl assembly, Piper P/N 11965-5 Neglect Wt. Change 106. Oil filter, Fram PB-5 Kit No. K-520, Fram Dwg. 62687, and Instructions No. 62686 (weight includes 1 quart oil). +4 lbs (-18.5) Landing Gear and Floats 201. Two main wheel-brake assemblies, 8.00-4 , Type III (a) Goodrich Model 841A Wheel Assembly D-3-13A-1 Brake Assembly D-2-113 +10 lbs. (0) 202. (a) Two main wheel 4-ply rating tires, 8.00-4, Type III with regular tubes +22 lbs. (0) 204. Tail wheel assembly (a) Scott Model 3-24B, Steerable +6 lbs. (+177) 205. Two skis (a) Federal A-1850, A-2000 or A-2000A per Federal Dwg. 11R262 *(b) Wesco per Western Aircraft Equipment Company Dwgs. Nos. 12 and 148: (1) A-20, (2) A-25, (3) AS-2A, (4) AS-2B. Use Actual Wt. Change *206. Consolidair Model 17 wheel fenders (Consolidair Dwg. 0045) +9 lbs. (0) 5 of 5 1A1 Landing Gear and Floats (cont.) 209. Two Edo 88-1650 floats with water rudder installed in accordance with Edo Dwg. No. 05525. Fuselage reinforcement, Piper P/N 12480; seaplane fin, Piper P/N 11030-3; and seaplane bottom engine cowl assembly (Item 105) must be installed in accordance with Piper Dwg. 12479. (Net weight increase is for installation of all above items.) +152 lbs. (+19) *210. Tandem Gear Model GW-100, installed in accordance with A. W. Whitaker, 5001 N.E. Union Avenue, Portland, Oregon, Dwg. T-10 and Installation Instructions dated June 8, 1949. +46 lbs. (0) Electrical Equipment 301. Battery - Reading S24-12V +25 lbs. (+21) 302. Generator - Delco-Remy 1101878 +10 lbs. (-42) 303. Regulator - Delco-Remy 1118259 +2 lbs. (-16) 304. Landing lights in wing leading edge per Piper Dwg. 12534 +4 lbs. (+5) Interior Equipment 401. (a) CAA (FAA) Approved Airplane Flight Manual, dated October 18, 1948 (b) Skiplane Supplement. When skis are installed the following supplemented information shall be appended to the Airplane Flight Manual: "Performance Information with Ski Installation: Climb: Skiplane climb performance is essentially equal to that of the landplane. Take-off and landing: Under the most favorable conditions of smooth packed snow temperature approximating 30°F, skiplane take-off distance approximately 20% greater than the landplane distance. In applying the performance data, caution should be exercised in that lower temperatures or other snow conditions will increase the ski friction and hence increase the take-off and decrease the landing run." (c) When Item 2, 3, 4(a) or 5 propeller is installed, the Airplane Flight Manual shall be revised to reflect this installation under 'Limitations' section and the following statement added under 'Performance' section following Item 4: "5. Performance with the Model _______ propeller has been demonstrated to equal or exceed that presented herein over the altitude and temperature range shown." (d) CAA (FAA) approved Airplane Flight Manual - Seaplane, dated July 18, 1949 *402. Javelin A-2 single axis automatic pilot installed in accordance with Javelin Dwg. 721 and Instructions dated June 15, 1954. (Landplane only). +18 lbs. (+94) NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. The following placards must be displayed. (a) On the instrument panel in full view of the pilot: (1) "Operate in Normal Category in compliance with Approved Flight Manual. Airplane marked for Normal Category. Acrobatics (including spins) prohibited in Normal Category." (2) "No Smoking." (b) On the baggage compartment: (1) "Maximum Baggage - 50 lbs. See Loading Schedule." (c) Adjacent to fuel valve: (1) "Fuselage tank must be full until wing tank is empty." ....END.... ``` ## ADs (15, in force first) - [AD 2025-02-11](https://openairdocs.org/ad/2025-02-11): Rudder Structure · FS 2001 J5A (Army L-4F), J5A-80, J5B (Army L-4G) and 67 more. Effective Mar 20, 2025 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2015-08-04](https://openairdocs.org/ad/2015-08-04): Wings · FS 2000 L-14, AE-1, HE-1 and 77 more. Effective Jun 3, 2015 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996 - [AD 85-06-04](https://openairdocs.org/ad/85-06-04): Fuel Tank · FS 2001 AE-1, HE-1, J5A-80 and 60 more. Effective May 4, 1985 - [AD 78-10-03](https://openairdocs.org/ad/78-10-03): Fuel Venting · FS 2001 AE-1, HE-1, J5A-80 and 66 more. Effective May 23, 1978 - [AD 74-17-04](https://openairdocs.org/ad/74-17-04): Fabric Reinforcement · FS 2002 PA-14, PA-12, PA-12S and 18 more. Effective Apr 11, 1977 - [AD 68-05-01](https://openairdocs.org/ad/68-05-01): Exhaust Mufflers · FS 2001 J5A-80, J5A (Army L-4F), J5B (Army L-4G) and 67 more. Effective Mar 31, 1968 - [AD 57-22-01](https://openairdocs.org/ad/57-22-01): Fire Prevention Rework · Piper PA-16, PA-16S, PA-20 and 12 more - [AD 58-12-02](https://openairdocs.org/ad/58-12-02): Aileron Hinge Brackets · Piper J-3, J3C-40, J3C-50 and 20 more - [AD 51-23-03](https://openairdocs.org/ad/51-23-03): Battery Box Insulation · Piper PA-16, PA-20 and PA-22 - [AD 99-01-05 R1](https://openairdocs.org/ad/99-01-05-R1) (historical): Wings · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Jan 14, 2014 - [AD 99-01-05](https://openairdocs.org/ad/99-01-05) (historical): Wing Lift Struts or Forks · FS 2000 L-14, AE-1, HE-1 and 73 more. Effective Feb 8, 1999 - [AD 93-10-06](https://openairdocs.org/ad/93-10-06) (historical): Corroded Wing Lift Struts or Cracked Forks · Piper Aircraft, Inc., The New J-2, J-3, J4 and 28 more. Effective Jul 9, 1993 ## Registered aircraft by registry model (OpenAirDocs) - [Piper PA-16](https://openairdocs.org/model/piper-pa-16): 276 aircraft (registry code 7101602) - [Piper PA-16S](https://openairdocs.org/model/piper-pa-16s): 0 aircraft (registry code 7101604) ## STCs approved under this data sheet (155, first 50) - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [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 SA02525LA](https://openairdocs.org/stc/SA02525LA): Installation of Wheel and Brake Assemblies. Game Aerospace LLC - [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc. - [STC SA01704LA](https://openairdocs.org/stc/SA01704LA): Installation of the Grove Disk Brake System. Grove Aircraft Landing Gear Systems Inc. - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA24EA](https://openairdocs.org/stc/SA24EA): Conversion of aircraft for parachute jumping and aerial photography.. Steve Pierce - [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC - [STC SA11854CH](https://openairdocs.org/stc/SA11854CH): Installation of modified exhaust system in lieu of original components. Dakota Cub Aircraft Inc. - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [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 SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd - [STC SA01343WI](https://openairdocs.org/stc/SA01343WI): Installation of B&C Specialty Products BC400 alternator. B & C Specialty Products Inc. - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [STC SA8438SW](https://openairdocs.org/stc/SA8438SW): Installation of dual toe brakes including rudder pedals, linkages and torque tubes.. Peter C. Morrison - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc. - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC - [STC SA04474CH](https://openairdocs.org/stc/SA04474CH): Installation of Rubbert Exhaust Assembly RR-1210, RR-1210-HR, RR-1212 and RR-1212-HR on Piper Aircraft models PA-12, PA- 14, PA-16, PA-18, PA-19, PA-20 and PA-22, in accordance with Installation Instructions, document number RR-120, revision Org., dated 04/24/2020 and Instruct 1201, revision Org., dated July 27, 2020 or later FAA approved revision.. Rubbert Aircraft Services - [STC SA01843SE](https://openairdocs.org/stc/SA01843SE): Installation of Lycoming engine and modified fuel system. Dan Stewart - [STC SA01863SE](https://openairdocs.org/stc/SA01863SE): Installation of Niagara Oil Cooler in the above model aircraft. Steve Pierce - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA02846CH](https://openairdocs.org/stc/SA02846CH): Installation of MT Propeller model MTV-15-B/210-58 on Piper Aircraft models PA-20 and PA-22,. Svenn's Aviation LLC - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): 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 SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC. - [STC SA02264AK](https://openairdocs.org/stc/SA02264AK): Fabrication and Installation of a Right Hand Seaplane Door.. Trimmer Marvin E/Trimmer Aviation LLC - [STC SA02263AK](https://openairdocs.org/stc/SA02263AK): Fabrication and Installation of a Left Hand Seaplane Door.. Trimmer Marvin E/Trimmer Aviation LLC - [STC SA02241AK](https://openairdocs.org/stc/SA02241AK): Installation of a Maule Fuel Selector Valve and Associated Fuel System Upgrade in accordance with the Descriptive Data listed in Trimmer Aviation, LLC, Master Data List, MDL-001, dated March 22, 2005, or later FAA approved revision.. Trimmer Marvin E/Trimmer Aviation LLC - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA3606NM](https://openairdocs.org/stc/SA3606NM): Installation of landing gear fueling step.. F. Atlee Dodge Aircraft Services, LLC - [STC SA02484AK](https://openairdocs.org/stc/SA02484AK): Installation of Sensenich W80CM8 wood propeller. Trimmer, Marvin E. - [STC SA02483AK](https://openairdocs.org/stc/SA02483AK): Installation of : (1) Cleveland 199-62 or 199-62A wheel and brake kit or ABI LLC AB-199-62 or ABI-199-62A wheel and brake kit on aircraft with 1.5" axles, OR (2) Cleveland wheel and brake kit 199-71 or ABI LLC ABI-199-71 kit on aircraft with 1.25" axles.. Trimmer Marvin E/Trimmer Aviation LLC - [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA02734CH](https://openairdocs.org/stc/SA02734CH): Installation of Lightweight Battery and Circuit Breaker Master Switch in lieu of original components. Svenn s Aviation LLC - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. All 155: https://openairdocs.org/tcds/1A1/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.