# TCDS A-803: Mooney Mite Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Mooney Mite Aircraft Corporation - Revision: 19 - Revised: February 1, 1972 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 98, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/17/ca/17ca6e925af82bbdf9cece2291bb1d0f3b033511eb51402c6fa32e974fe7b0a9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2D37206BEF82BAF18525673C006045CA.0001 - Page: https://openairdocs.org/tcds/A-803 ## Models (4) As the data sheet lists them. - M-18L - M-18C - M-18C 55 - M-18LA ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 7 Rev. No. 19 - - - - - - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-803 Revision 19 MOONEY M-18C M-18C55 M-18L M-18LA February 1, 1972 AIRCRAFT SPECIFICATION NO. A-803 Manufacturer Mooney Mite Aircraft Corporation Box 3999 Charlottesville, Virginia 22903 I - Model M-18 - Deleted - April 28, 1950 II - Model M-18L, 1 PCLM (Normal and Utility Category), Approved March 15, 1949 Engine Lycoming O-145-B2 Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2550 r.p.m. (65 hp.) Airspeed limits Maneuvering 103 m.p.h. ( 90 knots) (Normal Category) (CAS) 109 m.p.h. ( 95 knots) (Utility Category) Maximum structural cruising 109 m.p.h. ( 95 knots) Never exceed 143 m.p.h. (124 knots) Flaps extended 84 m.p.h. ( 73 knots) Landing gear extended 109 m.p.h. ( 95 knots) Landing gear operation 109 m.p.h. ( 95 knots) C.G. range (With landing gear extended) Normal Category: (+32.1) to (+33.8) at 780 lb. (+31.7) to (+33.8) at 725 lb. or less Utility Category: (+31.8) to (+32.9) at 740 lb. (+31.7) to (+32.9) at 725 lb. or less Straight line variation of forward limits between specified weights. Effect of retracting landing gear +266 in.-lb. (Not eligible for Utility Category operation with Items 302, 303 and 304 installed). 31 3 2 3 3 34 70 0 72 0 74 0 76 0 78 0 IN C H E S P O U N D S N O R M A L C A T E G O R Y U T IL IT Y C A T E G O R Y Empty weight C.G. range (+29.9) to (+30.0). When the E.W.C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Normal Category: 780 lb. Utility Category: 740 lb. A-803 2 No. seats 1 (+34) or (+35) for flat bottom seat Maximum baggage Normal Category: 40 lb. (+51) Utiltiy Category: None Fuel capacity 12 gal. (11 gal. usable) (one tank in fuselage) (+56.7) See NOTE 1 for data on unusable fuel and Item 111 for auxiliary fuel tank. Oil capacity 4 qt. (-9.0) Control surface movements Wing flaps Up 0° Down 16.5° Ailerons Up 15.5° Down 7° Elevators Up 25° Down 13° (stabilizer neutral at 0°) Rudder Right 20° Left 18° Stabilizer (Leading Edge) Up 2.5° Down 3.5° Serial Nos. eligible 2 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 2, 101, 201(c), 202(b), 205(b), 206(b), 401(b), 402. (For night flying, instrument lights or equivalent to provide illumination of all placards and instruments and flasher type landing gear warning light or aural (Horn) warning are required in addition to equipment required by CAR 43). III - Model M-18C, 1 PCLM (Normal Cateory), Approved April 11, 1950 Engine Continental A65-12 or -8 Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2300 r.p.m. (65 hp.) Airspeed limits Maneuvering 107 m.p.h. ( 93 knots) (CAS) Maximum structural cruising 114 m.p.h. ( 99 knots) Never exceed 143 m.p.h. (124 knots) Flaps extended 85 m.p.h. ( 74 knots) Landing gear extended 109 m.p.h. ( 95 knots) Landing gear operation 109 m.p.h. ( 95 knots) C.G. range (With landing gear extended) (+31.1) to (+34.4) Effect of retracting landing gear +362 in.-lb. Empty weight C.G. range (+28.1) to (+29.3). When the E.W.C.G. falls within this r ange, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Maximum weight 850 lb. No. seats 1 (+34) or (+35) for flat bottom seat Maximum baggage 40 lb. (+51) (with battery): 40 lb. (+51 and 35 lb. (+70) (Standard airplane). Fuel capacity 12 gal. (9.6 gal. usable) (One tank in fuselage) (+56.7) (See Item 112 for alternate fuselage tank) See NOTE 1 for data on unusable fuel and Item 111 for auxiliary fuel tank. Oil capacity 4 qt. (-4.5) Control surface movements Wing flaps Up 0° Down 16.5° Ailerons Up 15.5° Down 7° Elevators Up 25° Down 13° (stabilizer neutral at 0°) Rudder Right 23° Left 18° Stabilizer (Leading Edge) Up 1.5° Down 3.5° Serial Nos. eligible 201 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 5, 101, 201(c), 202(b), 205(b), 206(b), 401(e), 402. (For night flying, instrument lights or equivalent to provide illumination of all placards and instruments and flasher type landing gear warning light or aural (Horn) warning are required in addition to equipment required by CAR 43). 3 A-803 IV - Model M-18LA, 1 PCLM (Normal Cateory), Approved July 12, 1950 Engine Lycoming O-145-B2 Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2550 r.p.m. (65 hp.) Airspeed limits Maneuvering 107 m.p.h. ( 93 knots) (CAS) Maximum structural cruising 114 m.p.h. ( 99 knots) Never exceed 143 m.p.h. (124 knots) Flaps extended 85 m.p.h. ( 74 knots) Landing gear extended 109 m.p.h. ( 95 knots) Landing gear operation 109 m.p.h. ( 95 knots) C.G. range (With landing gear extended) (+31.1) to (+34.4) Effect of retracting landing gear +362 in.-lb. Empty weight C.G. range (+28.1) to (+29.3). When the E.W.C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Maximum weight 850 lb. No. seats 1 (+34) or (+35) for flat bottom seat Maximum baggage 40 lb. (+51) with battery): 40 lb. (+51) and 35 lb. (+70) (Standard airplane) Fuel capacity 12 gal. (11 gal. usable) (one tank in fuselage) (+56.7) (See item 112 for alternate fuselage tank) See NOTE 1 for data on unusable fuel and Item 111 for auxiliary fuel tank. Oil capacity 4 qt. (-9.0) Control surface movements Wing flaps Up 0° Down 16.5° Ailerons Up 15.5° Down 7° Elevators Up 25° Down 13° (stabilizer neutral at 0°) Rudder Right 23° Left 18° Stabilizer (Leading Edge) Up 1.5° Down 3.5° Serial Nos. eligible 100 to 200, inclusive. Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 2, 101, 201(c), 202(b), 205(b), 206(b), 401(f), 402. (For night flying, instrument lights or equivalent to provide illumination of all placards and instruments and flasher type landing gear warning light or aural (Horn) warning are required in addition to equipment required by CAR 43). V - Model M-18C 55, 1 PCLM (Normal Cateory), Approved April 2, 1955. Engine Continental A65-12 or -8 Fuel 80 minimum octane aviation gasoline Engine limits For all operations, 2300 r.p.m. (65 hp.) Airspeed limits Maneuvering 107 m.p.h. ( 93 knots) (CAS) Maximum structural cruising 114 m.p.h. ( 99 knots) Never exceed 143 m.p.h. (124 knots) Flaps extended 85 m.p.h. ( 74 knots) Landing gear extended 109 m.p.h. ( 95 knots) Landing gear operation 109 m.p.h. ( 95 knots) C.G. range (With landing gear extended) (+31.1) to (+34.4) Effect of retracting landing gear +362 in.-lb. Empty weight C.G. range (+28.1) to (+29.3). When the E.W.C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Maximum weight 850 lb. No. seats 1 (+37) Maximum baggage 40 lb. (+51) with battery); 40 lb. (+51) and 35 lb. (+70) (Standard airplane). Fuel capacity 13.5 gal. (one tank in fuselage) (+58.7) See NOTE 1 for data on unusable fuel and Item 111 for auxiliary fuel tank. Oil capacity 4 qt. (-4.5) A-803 4 Control surface movements Wing flaps Up 0° Down 16.5° Ailerons Up 15.5° Down 7° Elevators Up 25° Down 13° (stabilizer neutral at 0°) Rudder Right 23° Left 18° Stabilizer (Leading Edge) Up 1.5° Down 3.5° Serial Nos. eligible 323 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 2, 101, 201(c), 202(b), 205(b), 206(b), 401(k). (For night flying, instrument lights or equivalent to provide illumination of all placards and instruments and flasher type landing gear warning light or aural (Horn) warning are required in addition to equipment required by CAR 43). SPECIFICATIONS PERTINENT TO ALL MODELS Datum 25.19 in. forward of wing leading edge outboard of fillet. Leveling means Right hand engine bearer tube (M-18L and M-18LA); front face of front spar under seat is 90° to level (M-18L, M-18LA, M-18C and M-18C 55) Certification basis Type Certificate No. 803 (CAR 3) Production basis None. Prior to original certification of each aircraft a FAA Inspector must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data and a check of the flight characteristics. Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net change when that item is installed. " " indicates "Does not apply." 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. An item marked with an asterisk may not have been manufactured under a FAA monitored or approved quality control system. Propellers and Propeller Accessories M-18-L M-18L M-18LA M18C 55 1. Deleted - April 28, 1950 2. Propeller-Sensenich 66CB-52 or any other fixed 10 lb. (-21.5) ----- (-21.5) ----- pitch wood propeller which is eligible for t he engine power and speed and which meets the following limits: Static r.p.m. at maximum permissible throttle setting: Not over 2085, not under 1890. No additional tolerance permitted. Diameter: Not over 66 in., not under 64.5 in. 3. Propeller-Sensenich 60LY44 or 60MY49 or 11 lb. (-21.5) ----- (-21.5) ----- any other fixed pitch wood propeller which is eligible for the engine power and speed and which meets the following limits: Static r.p.m. at maximum permissible throttle setting: Not over 2350, not under 2100. No additional tolerance permitted. Diameter: Not over 60 in., not under 59 in. (Item 401(c) required) 4. Propeller-Flottorp 63L60 or 63L56 or any 8 lb. (-21.5) ----- (-21.5) ----- other fixed pitch wood propeller which is eligible for the engine power and speed and which meets the following limits: Static r.p.m. at maximum permissible throttle setting: Not over 2220, not under 1995. No additional tolerance permitted. Diameter: Not over 63 in., not under 62 in. (Item 401(d) required). 5. Propeller-Flottorp 65A60 to 66, Sensenich 9 lb. ----- (-23) ----- (-23) 65CK58 to 62, or any other fixed pitch wood propeller which is eligible for the engine power and speed and which meets the following limits: Static r.p.m. at maximum permissible throttle setting: Not over 2030, not under 1800. No additional tolerance permitted. Diameter: Not over 65 in., not under 63.5 in. 5 A-803 M-18-L M-18L M-18LA M18C 55 * 6. Propeller-Flottorp Controllable, R002-101 29 lb. ----- (-23) ----- (-23) or R003-100 hub with R003-237-65T blades. Static r.p.m. at maximum permissible throttle setting: Not over 2030, not under 1800. Pitch settings at 3/4 sta.: Low - 18.5°, high 25.5° Diameter: Not over 65 in., not under 63.5 in. When this item is installed, Airplane Flight Manual must be revised to list this item and include the statement "With this propeller installed, performance is equal to or better than that shown for the fixed pitch wood propeller." Engine and Engine Accessories - Fuel and Oil Systems 101. Carburetor air heater 1 lb. (-8.5) (-10) (-8.5) (-10) 102. to 107. Deleted - April 28, 1950 108. Cabin air heater 1 lb. (-1.5) ( -6) (-1.5) ( -6) 109. Nose cowl and baffle (Mooney Dwg. Nos. 811 No wt. change ---- No wt. change ---- and 812 respectively) Item No. 109 must be used when electrical system is installed (Mooney Dwg. No. 846). 110. Starter Delco Remy (CMC 50309) 16 lb. ----- (+2.5) ----- (+2.5) Requires No. 2 gauge cable to battery 111. 6 gal. aux. fuel tank (Installed in 5 lb. (+49.5) (+49.5) (+49.5) (+49.5) accordance with Mooney Dwg. 1049). Arm of fuel is (+51). When this item is installed in M-18L or M-18LA no baggage is permitted and when installed in M-18C or M-18C 55, baggage in rear compt. only is permitted. See NOTE 1 for data on unusable fuel. (Item 401(g), (h), (i) or (k) required when this item is installed). 112. 15.5 gal alternate main fuel tank (may be +2 lb. ----- ----- (+59) ----- installed in lieu of the standard 12 gal. fuselage tank). See NOTE 1 for data on unusable fuel. Landing Gear 201. Two main gear assemblies, Type III (a) Goodyear model 15HBM, 5.00-5 11 lb. (+51) ----- ----- ----- Wheel assembly #9520265 Brake assembly #9520264 (c) Mooney model W-1, 4.00-4 11 lb. (+50) (+48) (+48) (+48) Wheel-Brake assembly #W-617 202. (a) Two main wheel 4-ply tires, 5.00-5, 12 lb. (+51) ----- ----- ----- Type III, with regular tubes (b) Two main wheel 6-ply industrial tires, 10 lb. (+50) (+48) (+48) (+48) 4.00-4, Type III, with regular tubes (c) Two main wheel 4-ply industrial tires, 8 lb. (+50) (+48) (+48) (+48) 4.00-4, Type III, with regular tubes 205. One nose wheel, Type III (a) Firestone model 5C2M-1, 5.00-5 3 lb. ( 0 ) ----- ----- ----- (b) Mooney model W-2 wheel assembly 3 lb. (+1.5) ( -1) ( -1) ( -1) W-619, 4.00-4 206. (a) One nose wheel 4-ply tire, 5.00-4, 5 lb. ( 0 ) ----- ----- ----- with regular tube (b) One nose wheel 6-ply industrial tire, 5 lb. (+1.5) ( -1) ( -1) ( -1) 4.00-4, Type III, with regular tube 207. Two main gear doors 4 lb. (+48) (+48) (+48) (+48) A-803 6 Electrical Equipment M-18L M-18C M-18LA M-18C 55 302. Battery and box, Willard SYW-7-3, 9 lb. (+119) ----- (+119) ----- 6 Volt, 10 Amp. (5 hr. rate) 302. Generators, Pearson models (a) W-78B, (E-68), 6 volt, 8 amp. 7 lb. (-15.5) ----- (-15.5) ----- (b) W-148B, 12 volt, 8 amp. 8 lb. (-15.5) ----- (-15.5) ----- (c) W-612B, 6 volt, 12 amp. 11 lb. (-14) ----- (-14) ----- (d) W-1210B, 12 volt, 10 amp. 11 lb. (-14) ----- (-14) ----- (e) W-1515B, 12 volt, 15 amp. 12 lb. (-13.5) ----- (-13.5) ----- (f) W-1520B, 12 volt, 20 amp. 12 lb. (-13.5) ----- (-13.5) ----- 304. Landing light, General Electric, 4538 1 lb. (-18.5) ----- (-18.5) ----- 305. Battery and box, Reading Models (a) S-24, 12 volt, 24 amp. hr. 23 lb. (+75) (+75) (+75) (+75) (b) 333L, 6 volt, 33 amp. hr. 15 lb. (+75) ----- (+75) ----- (c) 324L, 6 volt, 24 amp. hr. 12 lb. (+75) ----- (+75) ----- (d) S-12, 12 volt, 12 amp. hr. 16 lb. (+75) (+75) (+75) (+75) NOTE: only eligible when starter not installed. 306. Generator, Delco Remy (CMC 40435) 10 lb. ----- (+2.5) ----- (+2.5) 307. Landing light, G.E. 4537 1 lb. ----- (-18.5) ----- ----- Interior Equipment 401. CAA Approved Airplane Flight Manual (b) Airplane Flight Manual dated 8/12/49 Elig. ----- ----- ----- (c) Airplane Flight Manual Supplement dated Elig. ----- ----- ----- October 31, 1949 (Req uired with Propeller Item 3) (d) Airplane Flight Manual Supplement dated Elig. ----- ----- ----- January 25, 1950 (Required with Propeller Item 4) (e) Airplane Flight Manual dated April 10, 1950 ----- Elig. ----- ----- (f) Airplane Flight Manual dated July 12, 1950, ----- ----- Elig. ----- or Revision No. 1, dated May 14, 1952 (g) Airplane Flight Manual Supplement dated --- Elig. ----- Elig. June 6, 1950 (Pertinent to 6 gal. aux. fuel tank, Item 111) (h) Airplane Flight Manual Supplement dated Elig. ----- ----- ----- June 6, 1950 (Pertinent to 6 gal. aux. fuel tank, Item 111) (i) Airplane Flight Manual Supplement dated ---- ----- Elig. ----- July 12, 1950 (Pertinent to 6 gal. aux. fuel tank, Item 111) (j) Airplane Flight Manual Supplement dated ----- ----- Elig. ----- July 12, 1950 (Pertinent to propellers, Item 3 & 4) (k) Airplane Flight Manual dated April 10, 1950 ----- ----- ----- Elig. and Supplements No. 5 and No. 6 dated April 11, 1955 402. Fixed Ballast (as required to balance) M-18L M-18C M-18LA M-18C 55 (a) Without electrical system installed) 0-8½ lb. (+155) 0-3½ lb. (+155) 0-3½ lb. (+155) ---- (b) With electrical system installed 0-2** lb. (+155) 0-3½ lb. (+155) 0-2 lb. (+155) ---- When other than standard tail cone (Mooney Dwg No. 66-1 1/2) is installed, the maximum a llowable fixed ballast must be reduced by the following amounts: Tail Cone Installed Reductions Mooney Dwg. No. 66-2 .5 lb. Mooney Dwg. No. 66-2 1/2 1.0 lb. Mooney Dwg. No. 66-3 1.5 lb. **No ballast allowed when air driven generator installed NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, 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). The certificated weight empty and corresponding center of gravity location must include unusable fuel as follows: MODEL M-18L: Unusable Fuel of 7 lb. at (+56.7) (Included in Fuel Capacity). MODEL M-18LA: Unusable Fuel of 7 lb. at (+56.7) for 12 gal. fuselage tank; or unusable fuel of 24.8 lb. at (+59) for 15.5 gal. fuselage tank (Included in Fuel Capacity). MODEL M-18C: Unusable Fuel of 16 lb. at (+56.7) for 12 gal. fuselage tank; or unusable fuel of 24.8 lb. at (+59) for 15.5 gal. fuselage tank (Included in Fuel Capacity). MODEL M-18C 55: No unusable fuel. 7 A-803 NOTE 2. The following placards must be displayed in front of and in clear view of the pilot: MODEL M-18L: "THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE IN COMPLIANCE WITH THE APPROVED FLIGHT MANUAL." All markings and placards on this airplane apply to its operation as a Normal Category Airplane. For Utility Category operations, refer to the Airplane Flight Manual. "NO ACROBATIC MANEUVERS (INCLUDING SPINS) ARE APPROVED FOR NORMAL CATEGORY OPERATIONS." MODEL M-18C: "THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COMPLIANCE M-18LA, WITH THE APPROVED FLIGHT MANUAL." and M-18C 55: "NO ACROBATIC MANEUVERS (INCLUDING SPINS) ARE APPROVED FOR NORMAL CATEGORY OPERATIONS." "NO SMOKING." (Required when ash tray not installed). .....END..... ``` ## ADs (9, in force first) - [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 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 79-11-05 R1](https://openairdocs.org/ad/79-11-05-R1): Wood Deterioration · Mooney Mite M-18C, M-18C 55, M-18L and 1 more. Effective Apr 1, 1981 - [AD 79-18-07](https://openairdocs.org/ad/79-18-07): Wood Deterioration · Mooney Mite M-18C, M-18C 55, M-18L and 1 more. Effective Sep 3, 1979 - [AD 50-01-01](https://openairdocs.org/ad/50-01-01): Engine Mount Reinforcement · Mooney Mite M-18L - [AD 51-03-01](https://openairdocs.org/ad/51-03-01): Fuel Line Rework · Mooney Mite M-18C, M-18C 55, M-18L and 1 more - [AD 53-17-01](https://openairdocs.org/ad/53-17-01): Control Stick Boot · Mooney Mite M-18C, M-18C 55, M-18L and 1 more - [AD 53-24-03](https://openairdocs.org/ad/53-24-03): Landing Gear Bellcrank · Mooney Mite M-18L - [AD 59-22-03](https://openairdocs.org/ad/59-22-03): Empennage · Mooney Mite M-18C, M-18C 55, M-18L and 1 more ## Registered aircraft by registry model (OpenAirDocs) - [Mooney M-18C](https://openairdocs.org/model/mooney-m-18c): 52 aircraft (registry code 5870102) - [Mooney M-18L](https://openairdocs.org/model/mooney-m-18l): 23 aircraft (registry code 5870106) - [Mooney M-18C 55](https://openairdocs.org/model/mooney-m-18c-55): 12 aircraft (registry code 5870104) - [Mooney M-18LA](https://openairdocs.org/model/mooney-m-18la): 11 aircraft (registry code 5870108) - [Mooney / Cox M18C MOONEY MITE](https://openairdocs.org/model/mooney-cox-m18c-mooney-mite): 0 aircraft (registry code 5870105) ## STCs approved under this data sheet (55, first 50) - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, 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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [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 SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [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 SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [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 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 SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.. Universal Corporation - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA01157LA](https://openairdocs.org/stc/SA01157LA): Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.. Electronics International Inc. - [STC SA00071SE](https://openairdocs.org/stc/SA00071SE): Cockpit sun visor installation.. Rosen Sunvisor Systems LLC - [STC SA01944CH](https://openairdocs.org/stc/SA01944CH): Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM Specification D-439 or D-4818 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc. - [STC SA866GL](https://openairdocs.org/stc/SA866GL): Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline, 87 mimimum antiknock index.. EAA Aviation Foundation - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA1008WE](https://openairdocs.org/stc/SA1008WE): Installation of Poly-Fiber covering material.. Poly-Fiber Inc. - [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc - [STC SA09470SC](https://openairdocs.org/stc/SA09470SC): Installation of Starter Indicator light system.. Texas Skyways Inc - [STC SA71GL](https://openairdocs.org/stc/SA71GL): Installation of air filters. Brackett Aero Filters Inc. - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA5755NM](https://openairdocs.org/stc/SA5755NM): Installation of a propeller anti theft device.. Davis Ray G - [STC SA4-302](https://openairdocs.org/stc/SA4-302): Installation of BN-1 propeller spinner.. ACS Products Co, Inc - [STC SA1351WE](https://openairdocs.org/stc/SA1351WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12). Ceconite Inc - [STC SA4289WE](https://openairdocs.org/stc/SA4289WE): Installation of Continental 0-200-A engine and McCauley 1A100 propeller. Edward L. Soncrant - [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc - [STC SA308EA](https://openairdocs.org/stc/SA308EA): Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental, Franklin, and Lycoming type engines equipped with Marvel-Schebler MA-2, MA-3, MA-4, MA-4-5, MA-6 and HA-6 series carburetors. (Normal,Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.). Alfred R Puccinelli - [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co - [STC SA1350WE](https://openairdocs.org/stc/SA1350WE): Replace existing fabric on wings, fuselage, empennage and/or control surfaces with fiberglass cloth.. Ceconite, Inc - [STC SA1-615](https://openairdocs.org/stc/SA1-615): Installation of Fram lube oil filter Model PB55-1.. Fram Aerospace - [STC SA1044WE](https://openairdocs.org/stc/SA1044WE): Continental A75-8 65 hp engine and McCauley 1B90-CM/6753 propeller.. Aero Spec - [STC SA2-1053](https://openairdocs.org/stc/SA2-1053): Wing, fin and stabilizer structure reinforcements accomplished in accordance with Poplawski Drawing No. 23. A.H. Frank Poplawski All 55: https://openairdocs.org/tcds/A-803/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.