# TCDS A-782: Sierra Hotel Aero Inc. - Type: Type certificate data sheet - Status: Current - Holder: Sierra Hotel Aero Inc. - Revision: 51 - Revised: March 18, 2003 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 864, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/d7/03/d703b4ca6889d97ef17898d9d81ac91b3fdbdc5105d34dfa004df8b5b1575531 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8D44F5F1A44C469A86256E8B004AAB96.0001 - Page: https://openairdocs.org/tcds/A-782 ## Models (8) As the data sheet lists them. - Navion B - Navion H - Navion (Army L-17A) - Navion F - Navion A (Army L-17B and L-17C) - Navion D - Navion E - Navion G ## 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 A-782 Revision 51 NAVION Navion (L-17A) Navion A (L-17B) (L-17C) Navion B Navion D Navion E Navion F Navion G Navion H March 18, 2003 AIRCRAFT SPECIFICATION NO. A-782 Type Certificate Holder Sierra Hotel Aero, Inc. 1690 Aeronca Ln, Fleming Field South St. Paul, MN 55075 Type Certificate Holder Record North American Aviation, Inc. to Ryan Aeronautical Company (TC last dated February 3, 1949) Ryan Aeronautical Company to Navion, Division of Tusco Corporation (TC last dated April 2, 1958) Navion, Division of Tusco Corporation to Base Industries, Incorporated (TC last dated May 5, 1961) Base Industries, Incorporated to Navion Aircraft Corporation on November 19, 1964 Navion Aircraft Corporation to Cedric R. Kotowicz on June 16, 1972 Cedric R. Kotowicz to Navion Rangemaster Corporation on October 14, 1972 Navion Rangemaster Corporation to Jimmie Thompson on February 14, 1979 Jimmie Thompson to Charles L. Klinger on January 13, 1982 Charles L. Klinger to Diamond Aero Enterprises, Inc. on June 17, 1982 Diamond Aero Enterprises, Inc. to Navion Holdings, Inc. on January 9, 1995 Navion Holdings, Inc. to Navion Aircraft Company, Ltd on January 22, 1998 Navion Aircraft Company, Ltd. to Navion Aircraft LLC on July 14, 2001 Navion Aircraft LLC to Sierra Hotel Aero, Inc. on March 18, 2003 Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 51 51 47 51 47 47 47 47 51 51 51 47 47 47 51 47 47 47 47 47 A-782 2 of 20 I - Model Navion (Army L-17A); 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved January 28, 1947 Engine Continental E-185-3 or -9 (See Item 139 for optional engine.) Fuel 80 min. octane aviation gasoline Engine limits For all operations, 2,300 r.p.m. (185 hp.) Airspeed limits Maneuvering 124 m.p.h. (108 K) True Ind. Maximum structural cruising 160 m.p.h. (139 K) True Ind. Never exceed 190 m.p.h. (165 K) True Ind. Flaps and gear extended 100 m.p.h. ( 87 K) True Ind. Propeller limits With Item 1(a)(1) installed: Diameter 84 in. max., 82.4 in. min. Static r.p.m. 2,000, operating pitch settings at 30 in. sta.; Low 14°, High 23°. C.G. range (gear down) (See NOTE 5 for C.G. range with altered horizontal stabilizer angle of incidence.) Utility - (+93.9) to (+104.9) Normal - (+98.1) to (+104.9) at 2,750 lb. (+93.9) to (+104.9) at 2,350 lb. or less Straight line variation between points given. Effect of retracted landing gear (+1,480 in. lb.) Empty weight C.G. range (+93.9 to (+95.3) rega rdless of category. Range is not valid for nonstandard arrangement except that it may be used when auxiliary fuel tank per Item 110(a) or (b) is installed but not when Item 110(e) is installed. When E.W.C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Maximum weight Normal - 2,750 lb. Utility - 2,350 lb. No. seats 4 (2 at +96 and 2 at +132) Maximum baggage 180 lb. (+159) Fuel capacity 39.5 gal. (+103). See Item 110 for auxiliary fuel tank installation Oil capacity 10 qt. (+39) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 45° Stabilizer Fixed Serial Nos. eligible NAV-4-2 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), 1(b), 102(a), 103(a), 104(a), 105, 106(a) or (b), 201, 202, 302, 401(a). II - Model Navion A (Army L-17B and L-17C); 4 PCLM (Normal Category), 2 PCLM (Utility Category), Approved February 3, 1949 (Same as Model Navion except for engine installation and revised fuel system) Model Navion airplanes may be converted to Model Navion A by installing the following: (1) Continental E-185-3 or -9 engine which is eligible for 205 hp. takeoff rating. (2) Fuel system in accordance with Ryan Dwg. 145-948021 or 154-948001 (Item 113). Airplanes serial numbers 1566 and 1628 and subsequent were equipped with these items when delivered. Engine Continental E-185-3 or -9 Only engines serial numbers 5122 and up are eligible for the one minute 2600 r.p.m. (205 hp.) takeoff rating, and these engines must have dampered crankshafts. (Suffix "D" to the engine serial number indicates dampered crankshafts.) (See Item 139 for optional engine.) Fuel 80 min. octane aviation gasoline Engine limits Takeoff (one min.), 2,600 r.p.m. (205 hp.) Maximum continuous, 2,300 r.p.m. (185 hp.) Airspeed limits Maneuvering 124 m.p.h. (108 K) True Ind. Maximum structural cruising 160 m.p.h. (139 K) True Ind. Never exceed 190 m.p.h. (165 K) True Ind. Flaps and gear extended 100 m.p.h. ( 87 K) True Ind. 3 of 20 A-782 Propeller limits With Item 1(a)(1) installed: Diameter 84 in. max., 82.4 in. min. Static r.p.m. 2,300, operating pitch settings at 30 in. sta.: Low 10.5°, High 23°. With Item 1(a)(2) installed: Diameter 84 in. max., 82.4 in. min. Static r.p.m. 2,325, operating pitch settings at 30 in. sta.: Low 12.5°, High 24.5° C.G. range (gear down) (See NOTE 5 for C.G. range with altered horizontal stabilizer angle of incidence.) Utility - (+93.9) to (+104.9) Normal - (+98.1) to (+104.9) at 2,750 lb. (+93.9) to (+104.9) at 2,350 lb. or less Straight line variation between points given. Effect of retracted landing gear (+1,480 in. lb.) Empty weight (+93.9 to (+95.3) regardless of category. Range is not valid for nonstandard arrangement except that it may be used when auxiliary fuel tank per Item 110(a) or (b) is installed but not when Item 119 is installed. When E.W.C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Maximum weight Normal - 2,750 lb. Utility - 2,350 lb. No. seats 2 (+96) and 2 (+132) Maximum baggage 180 lb. (+159) Maximum baggage permissible in Army L-17B and L-17C aircraft is 167 lb. at +159 due to the weight of radio equipment installed in these models. This is a structural limitation, and the full 180 lb. of baggage may be carried if the extra radio equipment is removed. Fuel capacity 39.5 gal. (+103). See Item 110 for auxiliary fuel tank installations. Army L-17B aircraft were equipped with Item 110(c) when delivered, increasing the fuel capacity for those aircraft to 59.9 gal. Oil capacity 10 qt. (+39) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 45° Stabilizer Fixed Serial Nos. eligible NAV-4-2 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1(a), 1(b), 102(a), 103(a), 104(a), 106(a) or (b), 113, 201, 202, 302, 401(b) or (c) depending on whether Item 409 is installed. III - Model Navion B; 4 PCLM (Normal Category), 1 PCLM (Utility Category), Approved March 13, 1950 Engine Lycoming GO-435-C2 (See Item 139 for optional engine) Fuel 91/98 min. octane grade aviation gasoline. 80/87 min. octane when equipped with modified M-4-5 Marvel-Schebler carburetors, Part No. 10-3391-1, and cowl flap extensions specified in Ryan Service Bulletin No. 20 dated March 17, 1953. Airplane Flight Manual revision, Item 401(1), required with 80/87 grade fuel. Engine limits Takeoff (2 minutes), 3,400 r.p.m. (260 hp.) Maximum continuous, 3,000 r.p.m. (240 hp.) Airspeed limits Maneuvering 124 m.p.h. (108 K) True Ind. Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 190 m.p.h. (165 K) True Ind. Flaps and gear extended 100 m.p.h. ( 87 K) True Ind. C.G. range (gear down) (See NOTE 4 for C.G. range with altered horizontal stabilizer angle of incidence.) Utility - (+93.9) to (+103.5) Normal - (+98.1) to (+103.5) at 2,850 lb. (+93.9) to (+103.5) at 2,350 lb. or less Straight line variation between points given. Effect of retracted landing gear (+1,480 in. lb.) A-782 4 of 20 Empty weight C.G. range None. Maximum weight Normal Category - 2,850 lb. Utility Category - 2,350 lb. No. seats 2 at (+96) and 2 at (+132) Maximum baggage 180 lb. (+159) Fuel capacity 39.5 gal. (+103). See Item 110 for auxiliary fuel tank installations. Item 110(b) is installed at the factory. Oil capacity 12 qt. (+29.5) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2B and up (Suffix "B" to the manufacturer's serial no. indicates eligibility as a Model Navion B.) Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 4 or 5, 102(b), 103(b), 104(b), 106(b) or (d), 127, 128, 201, 202, 302, 401(e) or (f). IV - Model Navion D; 4 PCLM (5th Place Optional), (Normal Category), Approved April 2, 1958 Engine Continental O-470-P Fuel 91/96 min. grade aviation gasoline. Engine limits Takeoff (5 minutes), 2,600 r.p.m. (240 hp.) Maximum continuous, 2,600 r.p.m. (240 hp.) Airspeed limits Maneuvering 132 m.p.h. (115 K) True Ind. Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 198 m.p.h. (172 K) True Ind. Flaps extended 105 m.p.h. ( 91 K) True Ind. Gear extended 100 m.p.h. ( 87 K) True Ind. C.G. range (gear down) (+98.0) to (+103.4) at 3,150 lb. (+93.4) to (+103.4) at 2,350 lb. Straight line variation between points given. Effect of retracted landing gear (+1,467 in. lb.) Empty weight C.G. range None. Maximum weight 3,150 lb. No. seats 2 (+96) and 2 (+132) or (3 (+132) optional) Maximum baggage 180 lb. (+159) Fuel capacity 39.5 gal. (+103), 68 gal. (+107) Oil capacity 12 qt. total, 9 qt. usable (+32) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 13, 101(e), 102(c) or (d), 103(c), 104(c), 106(b) or (d), 110(h), 113(c), 122(b), 129(b), 301(d), 302(b), 401(o) 5 of 20 A-782 V - Model Navion E; 4 or 5 PCLM, (Normal Category), Approved May 22, 1959 Engine Continental IO-470-C Fuel 91/96 min. grade aviation gasoline. Engine limits Takeoff (5 minutes), 2,600 r.p.m. (250 hp.) Maximum continuous, 2,600 r.p.m. (250 hp.) Airspeed limits Maneuvering 132 m.p.h. (115 K) True Ind. Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 198 m.p.h. (172 K) True Ind. Flaps extended 105 m.p.h. ( 91 K) True Ind. Gear extended 100 m.p.h. ( 87 K) True Ind. C.G. range (gear down) (+98.0) to (+103.4) at 3,150 lb. (+93.9) to (+103.4) at 2,350 lb. Straight line variation between points given. Empty weight C.G. range None. Maximum weight 3,150 lb. No. seats 4 or 5 (2 at +96 and 2 at +132) or (2 at +96 and 3 at +132) Maximum baggage 180 lb. (+159) Fuel capacity 39.5 gal. (+103), 68 gal. (+107) Oil capacity 12 qt. total, 9 qt. usable (+32) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2 and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 14, 101(f), 102(c) or (d), 103(c), 104(c), 106(b) or (d), 110(i), 122(b), 127(b), 129(b), 138, 301(d), 302(b), 401(p) VI - Model Navion F; 4 or 5 PCLM, (Normal Category), Approved September 23, 1959 Engine Continental IO-470-H (See NOTE 6 for required structural modification) Fuel 100/130 min. grade aviation gasoline. Engine limits Takeoff (5 minutes), 2,625 r.p.m. (260 hp.) Maximum continuous, 2,625 r.p.m. (260 hp.) Airspeed limits Maneuvering 132 m.p.h. (115 K) True Ind. Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 198 m.p.h. (172 K) True Ind. Flaps extended 105 m.p.h. ( 91 K) True Ind. Gear extended 100 m.p.h. ( 87 K) True Ind. C.G. range (gear down) (+98.0) to (+103.4) at 3,150 lb. (+93.9) to (+103.4) at 2,350 lb. Straight line variation between points given. Empty weight C.G. range None. Maximum weight 3,150 lb. No. seats 4 or 5 (2 at +96 and 2 at +132) or (2 at +96 and 3 at +132) Maximum baggage 180 lb. (+159) Fuel capacity 39.5 gal. (+103), 68 gal. (+107) Oil capacity 12 qt. total, 9 qt. usable (+32) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2 and up (See NOTE 6 for required structural modification.) Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 15, 101(f), 102(c) or (d), 103(c), 104(c), 106(b) or (d), 110(i), 122(b), 127(b), 129(b), 138, 301(d), 302(b), 401(q). A-782 6 of 20 VII - Model Navion G; 5 PCLM, (Normal Category), Approved May 5, 1961 Engine Continental IO-470-H Fuel 100/130 min. grade aviation gasoline Engine limits Takeoff (5 minutes), 2,625 r.p.m. (260 hp.) Maximum continuous, 2,625 r.p.m. (260 hp.) Airspeed limits Maneuvering 132 m.p.h. (115 K) True Ind. (See NOTE 7) Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 198 m.p.h. (172 K) True Ind. Flaps extended 105 m.p.h. ( 91 K) True Ind. Gear extended 130 m.p.h. (113 K) True Ind. C.G. range (gear down) (+99.0) to (+103.4) at 3,315 lb. (+93.9) to (+103.4) at 2,350 lb. Straight line variation between points given. Empty weight C.G. range None. Maximum weight Takeoff - 3,150 lb. (See NOTE 7) Landing - 3,150 lb. No. seats 5 (2 at +96 and 2 at +132, and 1 at +164) Maximum baggage 176 lb. (+164) See NOTE 2(i) Fuel capacity 39.5 gal. (+103), 68 gal. (+107) Oil capacity 12 qt. total, 9 qt. usable (+32) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2351G and up (For NAV 4-2351 through 2497 See NOTE 7) Required equipment In addition to the pertinent basic equipment specified in CAR 3, the following items of equipment must be installed: 15(a), (b), (c); 101(g); 102(c) or (d); 103(c); 104(c); 106(b), (d), or (e); 110(i); 122(b); 127(b); 129(b); 138; 301(d) or (e); 302(b), (c), or (d); 401(s) or (u). VIII - Model Navion H; 5 PCLM, (Normal Category), Approved June 5, 1967 Engine Continental IO-520-B, See Item 142 for optional engine. Fuel 100/130 min. grade aviation gasoline Engine limits Takeoff (5 minutes), 2,700 r.p.m. (285 hp.) Maximum continuous, 2,700 r.p.m. (285 hp.) Airspeed limits Maneuvering 135 m.p.h. (117 K) True Ind. Maximum structural cruising 169 m.p.h. (147 K) True Ind. Never exceed 203 m.p.h. (176 K) True Ind. Flaps extended 108 m.p.h. ( 94 K) True Ind. Gear extended 130 m.p.h. (113 K) True Ind. C.G. range (gear down) (+99.0) to (+103.4) at 3,315 lb. (+93.9) to (+103.4) at 2,350 lb. Straight line variation between points given. Empty weight C.G. range None. Maximum weight Takeoff - 3,315 lb. Landing - 3,150 lb. No. seats 5 (2 at +96 and 2 at +132, and 1 at +164) Maximum baggage 176 lb. (+164) See NOTE 2(i) Fuel capacity 39.5 gal. (+103), 68 gal. (+107) Oil capacity 12 qt. total, 9 qt. usable (+32) Control surface movements Elevator Up 30° Down 20° Elevator tab Up 25° Down 30° Rudder (measured from centerline of fin chord): Right 23° Left 17° Aileron Up 25° Down 17° Flaps Down 40° Stabilizer Fixed Serial Nos. eligible NAV-4-2500H, NAV 4-2500T, and up Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 16(a), (b), and (c) or 17(a), (b), and (c); 101(g); 102(c) or (d); 103(c); 104(c); 106(b), (d), or (e); 110(i); 122(b); 127(b); 129(b); 138(b); 301(d) or (e); 302(b), (c), or (d); 401(v). 7 of 20 A-782 Specifications Pertinent to All Models Datum Fuselage station 0, located 93.25 in. forward of the forward bolt centerline (jig point), wing lower surface bolting angle. Leveling means External lugs on right side of fuselage at stations 58 and 89.43. Certification basis Type Certificate No. 782 (CAR 3 effective November 13, 1945); Model D, E, and F wing, landing gear and flight test requirements (CAR 3 effective May 15, 1956); Model G and H, all except power plant (CAR 3 effective May 15, 1956). Applied for Type Certificate November 5, 1945. Production basis None. Prior to original certification, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the technical data and a check of the flight characteristics. Equipment: A plus (+) or minus (-) sign preceding the weight of an item 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. An item marked with an asterisk may not have been manufactured under an FAA monitored or approved quality control system. Conformity must be determined if the item is not identified by a Form FAA-186, PMA, or other evidence of an FAA production approval. Propellers and Propeller Accessories Eligible Model 1. (a) Propeller - Hartzell, variable pitch, hub Model Navion HC-12X20-1, -5, -7, 7B, or -7C and either: (For interchangeable blades, see NOTE 6 Navion of Propeller Spec. P-845) Navion A (1) Blade Model 8428, or 62 lb. (+7) as noted (2) Blade Model 8433 (to be used only with engines 65 lb. (+7) having dampered crankshafts. Suffix "D" to the engine serial number indicates dampered crankshafts.) Minimum clearance between the propeller hub spider and the propeller control piston Jack Plate should be 1/16 inch for the -1 and -5 propellers, and 1/8 inch for the -7 propellers. On the -7 propellers, this clearance must be determined by observation while the engine is running. Low pitch stop is on the control lever per Ryan Dwg. No. 145-44054 for the -1 and -5 propellers and on Ryan Dwg. No. 145-44060 for -7 propellers. The propeller counterweight length required with the above is as follows: Airplane Propeller Counterweight Model T.O. Hp. Item Length Navion 185 1(a)(1) 4 1/2 in.* Navion 185 1(a)(2) 4 1/8 in. Navion A 205 1(a)(1) 4 5/16 in. Navion A 205 1(a)(2) 4 1/8 in. *On Model Navion airplanes equipped with propeller Item 1(a)(1), and having Continental E-185-3 engines, serial nos. 4389-D through 5110-D, or engines which have been equipped with Tri-metal front main bearing inserts and bronze thrust washers at overhaul, the counterweight length must be adjusted in accordance with Ryan Field Service Bulletin No. 5 unless the rework outlined in Continental Motors Corp. Service Bulletin No. M48-30 has been accomplished. (b) Propeller control - Manual control for hydraulic 2 lb. (+56) unit on Hartzell Propellers, Ryan Dwg. No. 145-43020 (for Hartzell HC-12X20-1 and -5 propellers.) A-782 8 of 20 2. (a) Propeller - Koppers Aeromatic, variable pitch, hub 53 lb. (+7) Navion model 220 or 220-1, blade model O-85 Navion A Limits: as noted Model Navion: Diameter 85 in. max., 83.3 in. min. Static r.p.m. 2,200, operating pitch settings at 30 in. sta: Low 13.3°, high 27° Model Navion A: Diameter 85 in. max., 83.3 in. min. Static r.p.m. 2,500, operating pitch settings at 30 in. sta: Low 10.2°, high 27° Minimum allowable clearance between the propeller thrust plate and the thrust bracket screws is 0.094 in. when propeller blades are held in the full low pitch position and the control is in the full forward position. (See Koppers' approved "installation Procedure and Operating Limitations" No. 23.) (b) Altitude compensator - Koppers Aeromatic Model 11 lb. (+14) 4349-C, Ryan Dwg. 145-89100. When this item is installed on Model Navion aircraft, approved operating instructions covering operation with this item must be included in the Approved Operating Limitations (Airplane Flight Manual). (The Flight Manual page contained in Koppers' approved "Installation Procedure and Operating Limitations" No. 23 covers these instructions.) 3. Propeller - Hartzell, two-position automatic, hub model 64 lb. (+6) Navion HC-52X20-1, blades m odel 8433-0. as noted Eligible on model Navion with E- 185-3 engine having serial no. 5122D Eligible Model and above only. Low pitch blade angle meas ured at 30 in. sta. 17.7°. Pitch range 6° equivalent to 3/16 in. gap between adjusting screws and high pitch stop. Count erweight length 3 5/8 in. Low to high pitch trip r.p.m. 2,450, high to low pitch latch r.p.m. not less than 1,700. Item 401(d), Operating Limitations Supplement, must be added to 401(a) when this propeller is installed. 4. Propeller - Koppers Strato-Cruise, va riable pitch, hub model 220H, Navion B blades model O-93, with No. 4390 pitch control assy. Diameter 93 in. Static r.p.m. at maximum permissible throttle setting: Not over 3,300, not under 3,200. No additional tolerance permitted. Operating pitch settings at 30 in. sta: Low 14° to 14.5°, control 16°, high 29.7°. Koppers' "Adjustment Instructions and Operating Limitations No. 60" pertains to the use of this propeller on Navion B airplanes. 5. Propeller, Hartzell, variable pitch, hub mode l HC-12X20-8C, blades 76 lb. (+7) Navion B model 9333C, including control. Reference Ryan Dwg. 146-44002. Diameter 93 in. max., 91.2 in. min. Static r.p.m. at maximum permissible throttle setting: Not over 3,250, not under 3,150. No additional tolerance permitted. Operating pitch settings at 30 in. sta: Low 16.5°, high 31.5°. Propeller counterweight length is 4.25 in. See Hartzell Installation Instructions for this propeller. Minimum clearance between the propeller hub spider and the propeller control piston Jack Plate should be 1/ 16 in. This clearance must be determined by observation while the engine is running. Low pitch stop is shown on Ryan Dwg. No. 146- 44002. Placard required: "Avoid Continuous Ground Operation Betw een 1,675 and 2,150 Engine R.P.M." 6. Propeller spinner, Hartzell Model D-164. Eligible on Hartzell HC-12X20 3 lb. (+7) Noted propeller. Hartzell "Installation and Service Instructions" dated January 6, 1951, pertains to the us e of this spinner on Navion B aircraft. 9 of 20 A-782 7. Propeller - Hartzell, constant speed, hub model HC-12X20-7 Navion or -8 series, and either: Navion A (a) Blade model 8433 eligible on model Navion (185 hp. 65 lb. (+7) as noted for T.O.) and model Navion A (205 hp. for T.O.) Limits: Model Navion: Diameter 84 in. max., 82.4 in. min. Pitch settings at 30 in. sta: Low 12.5° (governor inoperative - static 2,360 r.p.m.), high 24.5° Model Navion A: Diameter 84 in. max., 82.4 in. min. Pitch settings at 30 in. sta: Low 10.5° (governor inoperative - static 2,480 r.p.m.), high 24.5° (b) Blade model 8428 eligible on model Navion (185 hp. 62 lb. (+7) for T.O.) and Navion A (205 hp. for T.O.) Limits: Model Navion and Navion A: Diameter 84 in. max., 82.4 in. min. Pitch settings at 30 in. sta: Low 10.5° (governor inoperative - static 2,360 r.p.m.), High 23°. Restrictions of Item 1(a) regarding counterweight lengths, dampered crankshafts, and thrust bearings, are applicable to same hub-blade combinations. Minimum clearance between the propeller hub spider and the propeller control piston Jack Plate should be 1/8 in. for the -7 propellers and 1/16 in. for the -8 propellers. This clearance must be determined by observation while the engine is running. Low pitch stop for -7 propellers is shown on Ryan Dwg. No. 145-44060 and on Ryan Dwg. No. 146-44002 for -8 propellers. (c) Constant speed governor, controls, and adapter 7 lb. (+44) installed in accordance with Hartzell Dwg. No. Eligible Model B-161 and Hartzell Installation Instructions No. 1 dated October 25, 1950. Includes Hartzell "T" Drive Adapter No. C-137 and Hartzell Governor model A-1. 8. Propeller - Hartzell, variable pitch, hub model 65 lb. (+7) Navion HC-12X20-7B, blade model 8433-0. Eligible only on Navion as noted aircraft equipped with Continental E-225-4 engines, Engine Item 131. Limits: Diameter 84 in. max., 82.4 in. min. Static r.p.m. 2,250 to 2,390, operating pitch settings at 30 in. sta: Low 14°, high 24°. Propeller counterweight length is 4 1/8 in. Minimum clearance between the propeller hub spider and the propeller control piston Jack Plate should be 1/8 in. for the -7 or -7C propeller. This clearance must be determined by observation while the engine is running. 9. Deleted. 10. Deleted. 11. Deleted. * 12. Propeller - Hartzell, controllable pitch, hub model HC-13X20-8D, blade Navion B model 8433-0. Eligible only on Navion B aircraft equipped with Symons as noted downdraft engine cooling system, Symons Dwg. No. 111-2. Limits: Diameter 84 in. max., 84 in. min. Pitch settings at 30 in. sta: Low 16.5°, high 32°. 13. (a) Propeller - McCauley constant speed, hub model 62 lb. (+7) Noted 2A36C18, blade model 90M-4. Eligible only on Navion aircraft equipped with Continental O-470-P engine. Limits: Diameter 86 in. max., 84.25 in. min. (No further reduction permitted.) Pitch settings at 36 in. sta: Low 11°, high 27.0°. (b) Governor, Woodward 210380 or 210105-2 4.5 lb. (+16) (c) Spinner assembly, McCauley 2A36 4 lb. (+ 7) A-782 10 of 20 14. (a) Propeller - McCauley, constant speed, hub model 60 lb. (+ 7) Noted C2A36C32, blade model 90M-4. Eligible only on Navion aircraft equipped with Continental IO-470-C engine. Limits: Diameter 86 in. max., 84.25 in. min. (No further reduction permitted.) Pitch settings at 36 in . sta: Low 11°, high 27.0°. (b) Governor, Woodward 210380 or 210105-2 4.5 lb. (+16) (c) Spinner assembly, McCauley 2A36 4 lb. (+7) 15. (a) Propeller - McCauley, constant speed, hub model 62 lb. (+ 7) Noted B2A36C31 or D2A3633, blade model 90M-4, or D2A34C49, blade model 90A-4. Eligible only on Navion aircraft equipped with Continental IO-470-H engine. Limits: Diameter 86 in. max., 84.25 in. min. (No further reduction permitted.) Pitch settings at 36 in . sta: Low 9.5°, high 27.5°. (b) Governor, Woodward 210380 or 210105-2 4 lb. (+16) (c) Spinner assembly, McCauley 2A36 4 lb. (+7) 16. (a) Propeller - McCauley, constant speed, hub model 62 lb. (+7) Noted D3A32C90, blade model 82NC-2. Eligible only on Navion aircraft equipped with Continental IO-520-B engine. Limits: Diameter 80 in. max., 78.4 in. min. (No further reduction permitted.) Pitch settings at 36 in . sta: Low 13.2°, high 30°. (b) Governor, Woodward 210452 or D210680 4 lb. (+16) (c) Spinner assembly, McCauley D3669 4 lb. (+7) 17. (a) Propeller - McCauley, constant speed, hub model 52 lb. (+7) Noted D2A34C58, blade model 90AT-4. Eligible only on Navion aircraft equipped with Continental IO-520-B engine. Limits: Diameter 86 in. max., 84.25 in. min. (No further reduction permitted.) Pitch settings at 36 in . sta: Low 10°, high 25.4°. (b) Governor, Woodward 210452 or D210680 4.0 lb. (+16) Eligible Model (c) Spinner assembly, McCauley D2771 4 lb. (+ 7) Engine and Engine Accessories - Fuel and Oil System 101. (a) Starter, Delco Remy 1109658 (Eligible with Continental 15 lb. (+47) Noted E-185-3 engines only) (b) Starter, Delco Remy 1109660 (Eligible with Continental 21 lb. (+47) Noted E-185-3 engines only) * (c) Starter, Precision Machine Works, Wichita , Kansas, 19 lb. (+47) Noted E-80-1001; or Eclipse E-80 modified in accordance with Continental Motors Dwg. 530983. (Eligible with Continental E-185-9 engines only. Cannot be used on airplanes equipped with Item 105.) (d) Starter, Eclipse 397, Model 50, St yle B 18 lb. (+48) Navion B (e) Delco Remy, 1109471 13 lb. (+44.5) Navion D (f) Delco Remy, 1109678 13 lb. (+44.5) Navion E,F (g) Delco Remy, 1109684/110914 starter 13 lb. (+44.5) Navion G,H (Eligible with Continental IO-470-H engine) (h) STARTER: Prestolite Model MCL6501 TCM, P/N 634592 with 18.6 lb (+44.5) Navion G, H Continental IO-520-BA engine 102. (a) Carburetor air filter, Farr Company N.A.A. 1 lb. (+22) Navion Dwg. No. 145-42103 Navion A (b) Carburetor air filter, Farr Company, Ryan Dwg. 146-42103 1 lb. (+22) Navion B (c) Carburetor air filter, American Air Filte r Corp 56C-1377 1 lb. (+15) Navion D, E , F , G , H (d) Carburetor air filter, Air Maze P/N 120737 or P/N 123664 1 lb (+15.5) Navion D, E , F , G , H 11 of 20 A-782 103. (a) Carburetor air intake system (less filter) N.A.A. 4 lb. (+26) Navion A Dwg. No. 145-42201 (b) Carburetor air intake system (less filter) Ryan 4 lb. (+24) Navion B Dwg. No. 146-42206 (c) Carburetor air intake system Navion Dwg. No. 147-30009 1.5 lb. (+19.5) Navion D E, F, G, H 104. (a) Oil cooler with pressure control valve, Harrison 12 lb. (+43) Navion AV-79C, AV-86C, or AV-87C. Navion A (b) Oil cooler with thermostatic control valve VAP type 12 lb. (+43) Navion B DV- 5, Harrison AV-79C, AV-86C, or AV-87C. (c) Oil cooler, Harrison Radiator Div. AP10AU08-02 or -04 5 lb. (+17) Navion D, E, F, G, H 105. Fuel pump installation - either: (Eligible in lieu of Navion Item 113 or 116 on Model Navion only) (a) Two Carter engine-driven fuel pumps, Models 624-S 5 lb. (+42) and 625-S (Continental P/N 50375) (b) Two Carter engine-driven fuel pumps, Models M687-S 5 lb. (+42) and M688-S (Continental P/N 530509) (c) One Adel electric fuel booster pump (connected in 4 lb. (+59) series with one Carter engine-driven fuel pump) (Ryan Dwg. No. 145-948020) * (d) Two Carter engine-driven fuel pumps, series connected, 7 lb. (+63.5) with modified Auto-pulse electric booster pump in accordance with Instructions and Installation Kit No. CJKM 115, Neo Air, Inc., Torrence Municipal Airport, Lomita, California 106. (a) Hydraulic pump assembly, engine-driven, Ryan Dwg. 2 lb. (+46) Navion No. 145-58010 Navion A (b) Hydraulic pump, engine-driven, New York Airbrake Model 2 lb. (+46) Navion No. 67A025 Navion A, D,E,F,G,H 2 lb. (+45) Navion B * (c) Hydraulic pump, Paul T. Arnold Dwg. No. 102, 6 lb. (+46) Navion Paul T. Arnold, Culver City, California Navion A (d) Hydraulic pump, engine-driven, Pesco P/N 1P677 1.5 lb. (+46) Navion D, E, F, G (e) Hydraulic pump, engine-driven, Eastern Industries, 2.3 lb. (+46) Navion D, Inc., Model No. 102-HBG-Type 219A E, F, G, H (f) Hydraulic pump, engine-driven, Eastern Industries, 2.2 lb. (+46) Navion Inc., Model 1235-HBG-Type 263 Navion A Eligible Model Navion H (g) Hydraulic pump, engine-driven, Eastern Industries, Inc., Model 1213-HBG-310 with Continental IO-520-BA engine. 107. (a) Vacuum system, Ryan Dwg. No. 145-89008 6 lb. (+46) Navion Navion A Navion B (b) Pesco engine-driven pump 3P-194-FA or 3P-194-F 4 lb. (+46) Navion D, E, F, G, H (c) Airborne Mechanism dry vacuum pump model 10-113 4 lb. (+46) Navion D, (Eligible as alternate to 107(b), system changes E, F, G, H required combined moment change 2 lb. (+51.5)) (d) Airborne Mechanism dry vacuum pump model 200 CW or 1.8 lb (+46) Navion H 212 CW with Continental 10-520-BA engine 108. See Item 105(d). *109. Engine fire extinguishing system, Walter Kidde 5 lb. CO2 17 lb. (+51) fixed system in accordance with drawings by Van's Air Service St. Cloud, Minnesota. A-782 12 of 20 110. Auxiliary fuel tank installation (when installed, approved Noted operating instructions covering operation with this item should be included in the Approved Operating Limitations (Airplane Flight Manual.)) * (a) 20 gal. installation in accordance with dwgs . 1, 2, 3, 10 lb. (+159) Navion 4, 5, and 34 and approved installation instructions Navion A prepared by Toth Aircraft and Accessories Co., Kansas City, Mo., Substitute following for baggage placard: "Maximum baggage compt. load: Aux. fuel tank empty, 170 lb. Aux. fuel tank full, 50 lb. Add following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only." (b) 20 gal. installation per Ryan Dwgs. 145-48201A 19 lb. (+151) Navion and 145-48225A Navion A Substitute following for baggage placard: "Maximum baggage compt. load: Aux. fuel tank empty, 161 lb. Aux. fuel tank full, 41 lb. Add following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only." (c) 20.4 gal. installation in accordance with Ryan Dwg. 20 lb. (+130) Navion No. 145-89067 Navion A Add following placard in front and in clear view of the pilot: "Aux. fuel tank not to be used for takeoff or landing." * (d) 20 gal. installation in accordance with Dwg. and 14 lb. (+132) Navion Installation Kit No. CJKM 3100, Neo Air, Inc., Navion A Metropolitan Airport, Van Nuys, California. Add the following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only." * (e) 20 gal. installation in accordance with Dwgs. 503A, 12 lb. (+132) Navion 503B, 503C, and "Instructions for Installing Long Navion A Beach Aeromotive Auxiliary Fuel Tank Kits in North American Navion," Long Beach Aeromotive, Long Beach, CA. Add the following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only." * (f) 20 gal. installation in accordance with Symons 10 lb. (+130) Navion Engineering Dwg. No. SY-102, and installation Navion A instructions. Add the following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only." * (g) Two 20 gal. wing tip tank installation per Brittain 35 lb. (+100.5) Noted Aircraft Enterprises Installation Manual TT1-2, Dwgs. 607A and 608A. When installed, approved operating instructions covering operation with this item should be Eligible Model included in the approved Operating Limitations (Airplane Flight Manual). Add the following placard in front and in clear view of the pilot: "Aux. fuel tank to be used in level flight only. To preclude possibility of unsymmetrical fuel flow when operating from both tanks (cross feed se lector switch 'on'), select each tank individually for approximately one minute prior to opening cross feed valve." 13 of 20 A-782 Eligible on the following models: Navion and Navion A: Maximum weight and C.G. range (Normal Category only); Tip Tanks Empty: Same as original model except if airplane is modified in accordance with NOTE 5. If so, C.G. limits in NOTE 5 apply. Tip Tanks Full: Same as Tip Tanks Empty except that rear C.G. limited to (+102.0). NOTE: Maximum weight of 2,850 lb. allowed for Navion A if landing gear meets requirements outlined in Brittain Aircraft Enterprises Installation Manual TT1-2. In such case, C.G. range same as above except that rear C.G. in tip tanks empty condition limited to (+104.0) at 2,850 lb. gross weight, straight line variation to (+104.9) at 2,750 lb. Navion B: Maximum weight and C.G.range (Normal Category only); Tip Tanks Empty: Same as original model except if airplane is modified in accordance with NOTE 4. If so, C.G. limits in NOTE 4 apply. Tip Tanks Full: Same as Tip Tanks Empty except that rear C.G. limited to (+102.0). NOTE: The 34:1 fuel to oil ratio for this installation is approved. (h) Two 34 gal. wing tip tanks manufactured by Fletcher 47 lb. (+107) Navion D Aircraft Company. Installation in accordance with Navion Dwgs. 147-30003 and 147-30012. Placards forward of fuel selector on floor between pilot's and copilot's chairs: "Tip Tanks (to be used in) Level Flight Only" "Do Not Use Tips with More Than 20 Gal. in Main" (i) Two 34 gal. wing tip tanks manufactured by Fletcher 47 lb. (+107) Navion E Aircraft Company. Installation in accordance with F, G, H Navion Dwgs. 147-30003 and 147-30012. Placards forward of fuel selector on floor between pilot's and copilot's chairs: "Tip Tanks (to be used in) Level Flight Only" "Do Not Use Tips with More Than 10 Gal. in Main" *111. Peterson-Jones oil cooler shutter model B2 installed in neglect weight Navion accordance with Peterson-Jones Dwg. 1A. Navion A Navion B *112. Southern Ohio Aviation controllable oil shutter in neglect weight Navion accordance with Dwgs. SOAC-361-1, -2, -3, -4. Navion A Navion B 113. One Adel electric fuel booster pump, connected in series 4 lb. (+66) Navion with one of the following engine-driven pumps: (Eligible Navion A in lieu of Item 105 on Model Navion and required on Model Navion A) B, D (a) Romec Model 7750-1 or 7790, Ryan Dwg. No. 145-948021 3 lb. (+42) (Reference: Ryan Kit Dwg. No. 145-89068 and Ryan Special Instruction No. 37). (b) Thompson model TFB-1100, Ryan Dwg. Nos. 145-948021 1 lb. (+42) or 154-948001 (c) One Lear engine-driven pump RG-15980, Navion Dwg. 1 lb. (+45) Navion D No. 147-30005 114. See Item 113(a). *115. Modified exhaust system, Long Beach Aeromotive Dwg. and 2 lb. (+42) Navion installation Instructions No. LB504 Navion A Navion B 116. Fuel pump installation (Eligible in lieu of Items 105 and Noted 113 on Model Navion only.) * (a) One engine-driven fuel pump, Long Beach Aeromotive Dwg. 4 lb. (+42) No. LB510 (Installation to be made in accordance with Long Beach Aeromotive "Installation Instructions for LB510 Fuel Pump"), Long Beach Aeromotive, Long Beach, California; and Eligible Model * (b) One fuel booster pump, Long Beach Aeromotive Dwg. 8 lb. (+73) Nos. 502A, 502B, and 502C (Installation to be made in accordance with Long Beach Aeromotive "Instructions for Installation - Booster Fuel Pump No. 502"), Long Beach Aeromotive, Long Beach, California. A-782 14 of 20 117. See Item 116(a). *118. Cowl flaps - Long Beach Aeromotive Dwg. and In stallation 5 lb. (+50) Navion Instructions No. 509 Navion A Navion B 119. See Item 110(e). 120. Controllable oil shutter, Ryan Dwg. No. 154-47001 neglect weight Navion 122. * (a) Modified exhaust system and cabin h eater, Symons no wt. change Navion Engineering Installation Instru ctions and Dwg. SY-103 Navion A Navion B (b) Hanlon and Wilson Co. Dwgs. 492-1 and 492-7 In stallation 6 lb. (+47) Navion D in accordance with Navion Dwg. 147-30001 E, F, G (c) Hanlon and Wilson Co. Dwgs. 492-23 and 492-55 Installation 6 lb. (+47) Navion H in accordance with Navion Dwg. 147-30001 *123. Oil cooler shutter, Long Beach Aeromotive Dwg. and neglect weight Navion Installation Instructions No. 508A Navion A Navion B *124. Manually controllable oil cooler shutter, Neo Air, Inc., neglect weight Navion Dwg. No. CJKM-4900 Navion A Navion B *125. Fram F30-W oil filter, installed in accordance with Fram 10 lb. (+55) Noted Instructions No. 62336-1 and Fram Dwg. No. 62337. (Eligible only on Continental E-185-3 or -9 engines, equipped with No. 530696 large capacity oil pump. Engine serial no. 6003 and above were so equipped at the factory.) *126. Davis Model 190-CN exhaust silencer installed in accordance 5 lb. (+37) Navion with Davis Silencer Co. No. 320. Navion A Navion B 127. (a) Cowl flaps installed in accordance with Ryan Dwg. 5 lb. (+53) Navion 146-31510 through 146-31515 and 145-89071 Navion A (b) Cowl flaps installed in accordance with Ryan Dwg. 5 lb. (+53) Navion B 146-31510 through 146-31515 and 146-51006 D,E,F,G,H 128. Navion B fuel system in accordance with Ryan Dwg. No. 146-48001 Noted and incorporating the following fuel pumps connected in series: (a) Adel Model 23067 electric fuel pump 4 lb. (+59) (b) Romec Model RD7790-A2N engine-driven fuel pump 3 lb. (+45) 129. * (a) Downdraft engine cooling system, manuf actured and No wt. change Noted installed in accordance with Symons Engineering Dwgs. SY-107 and -107A, B, C, D, E, F, G, H, and I. This installation requires cowl fl aps. Items 118, 127, or Symons Dwg. 103 called for in Item 122. (Eligible on Navion, Navion A, and on Navions e quipped with Engine Item 131.) (b) Downdraft engine cooling syst em. Installed in Navion D accordance with Navion Dwg. No. 147-30011. E, F, G, H *130. Fletcher Aviation Corp. engine cooling system. (Downdraft Noted type with exhaust augmenters.) Reference Fletcher Part Nos. SK6601 through SK6674, installed in accordance with Fletcher Aviation Corp. instructions. (Eligible on Navion, Navion A, and on Navions equipped with Engine Item 131.) 131. Continental E-225-4 engine (Interchangeable with No wt. change Noted Continental E-185-3 and -9) Limits: For all operations, 2,600 r.p.m., F.T., 224 hp. NOTE: Although the engine rati ng is 225 hp. at 2,650 r.p.m., the tachometer must be redlined at 2,600 r.p.m. because of propeller vibration limitations. Aircraft must also be placarded "Do Not Exceed 2,600 R.P.M." This engine approved only in accordance with either of the following: *(a) Symons installation with the following required: Engine cooling system, Item 129; cowl flaps in accordance with Items 118, 127 or cowl flaps specified in Item 122; cylinder head temperature gauge; propelle r, Item 8; and fuel system Item 113(a); Airplane Fli ght Manual Supplement Item 401(h). 15 of 20 A-782 Eligible Model *(b) Fletcher Aviation Corp. installation with the following required: Engine cooling system, Item 130; propeller, Item 8; fuel system 113(a); Airplane Flight Manual Supplement Item 401(i). *(c) Neo Air, Inc., installation with the following required: Engine cooling system, Item 136; propeller, Item 8; fuel system 113(a); Airplane Flight Manual Supplement Item 401(k). 132. Deleted. 133. Deleted. 134. Deleted. 135. Deleted. *136. Neo Air, Inc., Torsion cooling system (Downdraft type); No wt. change Noted installed in accordance with Neo Air Dwgs. CJKM-6002 and CJKM-6003, installation instructions. (Eligible on Navion, Navion A, and on Navions equipped with engine Item 131.) 137. Deleted. 138. (a) Weldon electric fuel pump P/N 4020-A2A or 3 lb. (+66) Navion E P/N 4020-A4A, connected in series with Continental F, G fuel injection pump, Navion Dwg. 147-30001, Sheet 4 of 4. (b) Dukes Astronautics electric fuel boost pump 2.5 lb. (+66) Noted P/N 4140-00-17N connected in series with Continental engine IO-520-B or IO-520-BA injection fuel pump, Navion Dwg. 161-30001, sheet 2 of 4. 139. Continental IO-470-H engine installed per Navion Report Navion Nav-TU-113. Navion A, B Fuel 100/130 octane aviation gasoline Engine limits: All operations 2,625 r.p.m. (260 hp.) The following items of equipment are required in lieu of their respective components as shown for the model receiving the installation: Items 15; 102(c) or (d); 103(c); 104(c); 106(b) or (d); 122(b); 127(b); 129(b); 138; 302(b); 401(c), or (f) and (r). 140. Continental O-470-P engine installed in accordance with Dwg. 147-30001. Navion A Fuel 91/96 octane aviation gasoline Engine limits: All operations 2,600 r.p.m. (240 hp.) Required equipment items: Items 13(a), (b), and (c); 102(c) or (d); 103(c); 104(c); 106(b) or (d); 122(b); 127(b); 129(b); 138; 302(b); 401(x). 141. Continental IO-520-B engine installed in accordance with Navion A Dwg. 161-30001. B,D,E,F,G Fuel 100/130 octane aviation gasoline. Engine limits: All operations 2,700 r.p.m. (285 hp.) Additional required equipment: Items 16(a), (b), and (c) or 17(a), (b) and (); 401(w). 142. Continental IO-520-BA engine installed in accordance with Navion H Dwg. 161-30001 Fuel 100/130 octane aviation gasoline Engine limits: All operations 2,700 r.p.m. (285 hp.) Additional required equipment: Items 16(a), (b), and (c); 101(h); 106(g); 107(d); 301(f); 304(d); 401(y). Landing Gear and Floats 201. Main Landing Gear - 7.00-8 4-ply rating tires and Type III Noted 7.00-8 wheel brake assemblies, either: (Eligible on Navion, Navion, A, B, D, E, F, and Navion G at 3,150 lb.) Main Landing Gear tires - 6.50-8 6-ply sidewall inflated 20.5 lbs. (+114) Navion G, H tubeless required on Navion G and H with gross weight on 3,315 lbs. (a) Goodrich Model 6057MD 50 lb. (+114) (b) Firestone Model DFA234 50 lb. (+114) (c) Goodrich Model G-14-720-MD-1 50 lb. (+114) (d) Goodyear 9532135 wheel assy. 17.5 lb. (+114) Navion G, H (e) Goodyear 9541868 brake assy. 16.0 lb. (+114) Navion G, H A-782 16 of 20 202. Nose Wheel - 6.00-6 4-ply rating tire and Type III All Models 6.00-6 wheel, either: (a) Firestone Model 6C-5 14 lb. (+46) (b) Goodrich Model D-3-609-MD-1 14 lb. (+46) (c) Goodyear 9532112 nose wheel assy. (+46) All Models Eligible Models *203. Tennes-Navion landing gear-wheel fairing kit. Landing 8 lb. (+114) All Models gear fairing fabricated and installed in accordance with Dwg. Nos. T-100 and T-101, a nd wheel fairing fabricated and installed in accordance with Dwg. No. T-200-FI for Firestone wheels, or wheel fa iring fabricated in accordance with Dwg. Nos. C-T-200-G and T-200-GI for Goodrich (Hayes) wheels. *204. Nose gear enclosure 6 lb. (+60) All Models Main wheel enclosures, both wheels 5 lb. (+114) Installed per Long Beach Aeromotive Dwgs. LB505A and LB505B 205. Landing gear fairing installation, Ryan Dwg. No. 145-33301 (a) Nose gear fairing 6 lb. (+114) All Models (b) Main gear fairing 5 lb. (+114) *206. Landing gear fairing installation, Symons Engineering All Models installation Dwg. Nos. SY-105-A and -B; Symons Engineering, Box 2262, El Segundo, California (a) Nose gear fairings 3 lb. (+50) (b) Main gear fairings 4 lb. (+114) 207. Toe brake master cylinders 2.0 lb. (+65) Navion G, H Paramount Machine Co. P/N V1-15-750-4 Electrical Equipment 301. Generator or DC alternator (a) Delco Remy 25 amp. 15 lb. (+47) Navion Navion A (b) Ryan Dwg. No. 146-40100 22 lb. (+49) Navion B * (c) 50 amp., Lear Dwg. A43977 15 lb. (+47) Navion Navion A (d) Delco Remy, 12 volt, 50 amp., 1101909 or 1101912 16 lb. (+44.5) Navion D E , F , G (e) Delco Remy, 12 volt, 70 amp., alternator 1100715 Navion G, H (Eligible on Navion G and H models with IO-520-B Continental engine) (f) Prestolite 12 volt, 70 amp. alternator ALX-9405 TCM, 11.4 lb. (+47) Navion H P/N 634785 with Continental IO-520-BA engine 302. (a) Battery (Exide 6-TAS-9B) and battery case, NAA 37 lb. (+151) Navion Dwg. 145-54020 Navion A, B (b) Battery, re-bat type R-33 30 lb. (+151) Navion D 30 lb. (+52) E, F, G, H (c) Battery, Exide AC 66 26 lb. (+51) Navion G, H (d) Battery, Exide AC 78 27 lb. (+51) Navion G, H 303. Landing light (G.E. 4509) and bracket, NAA Dwg. 145-54007 3 lb. (+114) All Models 304. Voltage regulator (a) Delco Remy 1118340 neglect weight Navion Navion A (b) Leece-Neville 3038-R6 neglect weight Navion B (c) Leece-Neville 3038-RB-6 3 lb. (+53) Navion D (d) Prestolite VSF72035 or 7204 0.8 lb. (+53) Navion H 17 of 20 A-782 Interior Equipment 401. CAA or FAA Approved Airplane Flight Manual (Approved Noted O perating Limitations) (a) Issue dated 6-3-47. Required for Model Navion airplanes. (b) Issue dated 2-3-49. Required for Model Navion A airplanes if item 409 is installed. (c) Issue dated 7-26-49. Required for Model Navion A airplanes if Item 409 is not installed. (d) Supplement to Item 401(a), dated 4-20-49. Required w ith Item 3. (e) Issue dated 3-13-50. For Model Navion B airplanes equipped with propeller Item 4. (f) Issue dated 7-17-50. For Model Navion B airplanes equipped with propeller Item 4 or 5. * (g) Supplement to Airplane Flight Manual dated 10-24-51. Required for airplanes with automatic pilot. Item 412(a). Revision 9-2-52 (Lear No. 96122) required when altitude controller installed; revision dated 12-1-54 permitted with 974R attitude gyro installed. Revision dated 6-18-54 required with approach coupler. * (h) Supplement to Airplane Flight Manual dated 8-21-52. Required for airplanes equipped with engine Item 131(a) (Symons Installation). * (i) Supplement to Airplane Flight Manual dated 6-26-52. Required for airplanes equipped with engine Item 131(b) (Fletcher A irplane Installation). * (j) Deleted. * (k) Supplement to Airplane Flight Manual dated 4-14-53. Required for airplanes equipped with engine Item 131(c) (N eo Air Installation). (l) Revision No. 2 dated 3/27/53 to Item 401(f) Airplane Flight Manual. Required with 80/87 octane fuel on Model Navion B. (m) Deleted. (n) Deleted. (o) Issue dated 4-2-58. Required for Model Navion D airplanes. (p) Issue dated 5-1-59. Required for Model Navion E airplanes. (q) Issue dated 9-23-59. Required for Model Navion F airplanes. (r) Supplement to Airplane Flight Manual dated 10/25/62. Required for aircraft equipped with Item 139. (s) Issue dated 5-5-61. Required for Model Navion G airplanes S/N 2351 through 2400. Required for S/N 2401 through 2497 if NOTE 7 has not been complied with and maximum gross weight is 3,150 pounds. (t) Airplane Flight Manual Supplement dated 11-1-62. Required when Item 412(f) ARC512A or B automatic pilot is installed. (u) Issue dated 10-25-62. Required for Model Navion G airplanes S/N 2498 and up and S/N 2401 through 2497 with a maximum gross weight of 3,315 pounds. (v) Issue dated 6-5-67 required for Model Navion H airplanes. (w) Supplement to AFM dated 8/3/66, required for Model Navion G (3,315 pounds) airplanes equipped with Item 141. Supplement dated 8-23-66 required for Models Navion A, B, D, E, or F airplanes equipped with Item 141. (x) Supplement to AFM dated 11/14/67. Required for aircraft equipped with Item 140. (y) Issue dated 6-5-67, revised 12-27-74, required when Item 142 is installed. 404. Flare installation (a) 3 International MK-1 parachute flares and Kilgore 16 lb. (+188) All Models Mfg Co. Model R3M-1 switch panel. (b) Mounting bracket, NAA Dwg. 145-89002 All Models 407. Heater Installation, NAA Dwg. 145-89006 12 lb. (+47) Navion Navion A Navion B A-782 18 of 20 408. Venturi tube accessory Kit installation, Ryan Dwg. 145-89066. 4 lb. (+60) All Models 409. Intermediate flap setting provisions (Valve Assembly, Neglect Weight All Models Flap indicator line, flap indicator light installation) in accordance with Ryan Dwg Nos. 145-58012-J, 154-00010-E, 145-540001-K, and 145-54076. (Item 401(b) may be used only in those airplanes in which item 409 is installed.) 410. Deleted 6/13/61. 411. Safe Flight indicator installation in accordance with 1 lb. (+78) All Models Ryan Dwg. No. 145-89111. 412. Automatic pilot installations * (a) Lear Model L-2B according to Lear Dwgs. 82984 and 43654 33 lb. (+160) Navion and Model 1404 or 2203 altitude controller (opt. equip.) Navion A according to Lear Dwg. 82894. 1.5 lb. (+222) B, D, E, F Model 1350A-2 approach coupler (opt. equip.) acco rding to 7.5 lb. (+151) Lear Dwg. 82984. Model 937A controller (replaces 1049A). 2.5 lb. (+77) Eligible Model Items 301(c), 304(a), and 401( g) or 301(b), 304(b), and 401(g) or 301(d), 304(c), a nd 401(g) are also required. Servo stall torque measured at the servo on the ground: Aileron 40 in. lb., elevator 40 in. lb., rudder 55 in. lb. The following placard shall be installed near the autopilot controller: "(1) When Using Autopilo t in Cruise Configurations, Minimum Terrain Clearance is 500 feet. "(2) When Using Autopilot in Approach, Minimum Terrain Clearance is 300 feet. (Minimum Altitudes Do Not Override any Higher Operational Altitudes.) (3) Do Not Override Autopilot to Increase Angle of Bank." (b) Deleted. * (c) Javelin A-2 or A-3 Single Axis autopilot according to 18 lb. (+192) Navion Javelin Dwg. 724, Revision B1, and instructions Navion A dated 5/10/55. Navion B * (d) Lear Arcon rudder control per L ear Dwg. No. 703767 15 lb. (+160) Navion Navion A Navion B * (e) Mitchell Industries, Inc., Model AK045 automatic pilot 10 lb. (+55) Navion in accordance with Mitchell Bulletin No. 109 and Navion A supplement dated 1-19-56 (weight doe s not include gyros). B, D, E, F (f) Aircraft Radio Corporation Model ARC512A or B installed 12 lb. (+97.35) Navion G in accordance with Navion Dwg. 161-70002, Revision "C." Servo actuator assembly No. 29720 torque adjustment is 4 5 ±3 in. lb. Item 401(t) required. NOTE 1. Current weight and balance report, incl uding 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 a pproved weight control system). NOTE 2. The following placards must be displayed: (a) In front and in clear view of the pilot: "This airplane must be operated in comp liance with FAA Approved Operating Limitations." (b) In front and in clear view of the pilot: (1) For Navion airplanes. "Normal Category Only (G.W. 2,750 lb.). No acrobatic maneuvers, including spins, approved." (2) For Navion A airplanes. "Normal Category Only (G.W. 2,750 lb.). No acrobatic maneuvers, including spins, approved." When incorporating wing tip fuel tanks and with landing gear meeting the requirements outlined in Brittain Aircraft Enterprises' Installation Ma nual TTI-2, placard should specify G.W. 2,850 lb. (3) For Navion B airplanes. "Normal Category Only (G.W. 2,850 lb.). No acrobatic maneuvers, including spins, approved." (4) Deleted. 19 of 20 A-782 (5) Navion, Navion A, and Navion B airplanes (except Navions incorporating wing tip fuel tanks). "Utility Category (G.W. 2,350 lb.). No acrobatic maneuvers, including spins, approved except those listed below: Maneuver Entry Speed Steep turns (up to 60° only) 110-150 m.p.h. TIAS Chandelles 150-160 m.p.h. TIAS Lazy 8's 130-150 m.p.h. TIAS Stalls (except whip stalls) straight flight, power off, Gear and flaps up 69 m.p.h. TIAS (64 IAS) Gear and flaps down 55 m.p.h. TIAS (50 IAS)" (6) On Navion D airplanes. "G.W. 3,150 lb.). No acrobatic maneuvers, including spins, approved." (c) On Navion, Navion A, and Navion B: "Do not enter or leave airplane while engine is running." (d) On all models with a canopy, on the left hand canopy rack, 7 1/2 inches from windshield and in clear view of occupants: "Do not open enclosures beyond this point while in flight except for emergency." (e) In front and in clear view of the pilot: (1) With items 110(a), 110(b), 110(d), 110(e), and 110(f): "Aux. fuel tank to be used in level flight only." (2) With item 110(c): "Aux. fuel tank not to be used for takeoff and landing." Eligible Model (3) With item 110(g): "Aux. fuel tanks to be used in level flight only." "To preclude the possibility of unsymmetrical fuel flow when operating from both tanks (cross feed selector switch 'on'), select each tank individually for approximately one minute prior to opening cross feed valve." (f) On Navion B airplanes only, in front and in clear view of the pilot: "When one or more seats are unoccupied, ballast is required. See Approved Flight Manual." (g) On Navion B airplanes equipped with propeller item 5 only, in front and in clear view of the pilot: "Avoid Continuous Ground Operation Between 1,675 and 2,150 Engine R.P.M." (h) On Navion D airplanes, the placards specified in the Airplane Flight Manual, item 401(o), must be displayed in front and in clear view of the pilot: (i) On Navion G and H airplanes on left side of bulkhead closure at Sta. 179: "Max. capacity 176 lb. passenger or cargo with seat installed; 190 lb. when seat removed." (j) For aircraft incorporating tip tank, the following placard is to be located forward of the fuel selector valve on the floor between the pilot and copilot's seats: "Tip tanks to be used in level flight only. Do not use tip tanks with more than 10 gal. in mains." This is required to provide space in main tanks for fuel and vapor return. NOTE 3. Deleted. Information pertinent to twin-engine Navions now covered in Aircraft Specification 2A1. *NOTE 4. The horizontal stabilizer angle of incidence may be altered on all Navion B model airplanes when accomplished in accordance with Palo Alto Airport, Inc., "Instructions for Modifying Navion Tail Assemblies." The following C.G. range will apply: Utility - (+94.8) to (+103) Normal - (+98.1) to (+103) at 2,850 lb. (+94.8) to (+103) at 2,350 lb. or less Straight line variation between points given. Effect of retracted landing gear (+1,480) in. lb. *NOTE 5. The horizontal stabilizer angle of incidence may be altered on all Navion A model airplanes when accomplished with the following: (a) Palo Alto Airport, Inc., "Instructions for Modifying Navion Tail Assemblies" or (b) Symons Engineering Dwg. SY-108 "Installation Instructions for Navion Stabilizer Change. The following C.G. range applies for both (a) and (b): Utility - (+94.8) to (+104.9) Normal - (+98.1) to (+104.9) at 2,750 lb. (+94.8) to (+104.9) at 2,350 lb. or less Straight line variation between points given. Effect of retracted landing gear (+1,480) in. lb. NOTE 6. Fuselage structural reinforcing in accordance with Navion Dwg. 143-31001-700 required with installation of Continental IO-470-H engine on all models through Navion F. A-782 20 of 20 NOTE 7. Airplane S/N 2351 through S/N 2400 maximum weight is 3,150 lb. takeoff and landing. Takeoff weight may be increased to 3,315 lb. on S/N 2401 through S/N 2497 with modifications per Navion Dwg. No. 161-00002-3. S/N 2498 and up, takeoff weight is 3, 315 lb. Airspeed limits at 3,315 lb. are as follows: Maneuvering 135 m.p.h. (117 knots) True Ind. Maximum structural cruising 169 m.p.h. (147 knots) True Ind. Never exceed 203 m.p.h. (176 knots) True Ind. Flaps extended 108 m.p.h. ( 94 knots) True Ind. Gear extended 130 m.p.h. (113 knots) True Ind. ...END... ``` ## ADs (43, in force first) - [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 2008-05-14](https://openairdocs.org/ad/2008-05-14): Fuel system · Sierra Hotel Aero Navion A (Army L-17B and L-17C), Navion B, Navion D and 5 more. Effective Apr 16, 2008 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 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 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 75-05-02](https://openairdocs.org/ad/75-05-02): Engine Oil · Beryl D Shannon Aviation Specialties Engine Crankcase… (D'Shannon Products STC SA2653WE). Effective Feb 21, 1975 - [AD 68-20-06](https://openairdocs.org/ad/68-20-06): Rudder Horn Inspection · Sierra Hotel Aero Navion A (Army L-17B and L-17C), Navion B, Navion D and 5 more. Effective Oct 3, 1968 - [AD 62-03-03](https://openairdocs.org/ad/62-03-03): Landing Gear Selector Valve Fitting · Sierra Hotel Aero Navion A (Army L-17B and L-17C), Navion B, Navion D and 4 more. Effective Mar 6, 1962 - [AD 47-11-01](https://openairdocs.org/ad/47-11-01): Rudder-Nose Gear Steering Bellcrank · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-11-02](https://openairdocs.org/ad/47-11-02): Hartzell Propeller Blade Rework · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-04](https://openairdocs.org/ad/47-21-04): Fuel Scupper Drain Line · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-05](https://openairdocs.org/ad/47-21-05): Propeller Control Friction Lock · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-07](https://openairdocs.org/ad/47-21-07): Carburetor Air Intake Scoop Filler Strip · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-08](https://openairdocs.org/ad/47-21-08): Generator Terminal Stud Insulator · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-09](https://openairdocs.org/ad/47-21-09): Hydraulic System Modifications · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-21-10](https://openairdocs.org/ad/47-21-10): Propeller Guide Pin Dowel · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-31-01](https://openairdocs.org/ad/47-31-01): Nose Gear Hydraulic Actuating Cylinder Lines · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-31-02](https://openairdocs.org/ad/47-31-02): Carburetor Vapor Return Line · Sierra Hotel Aero Navion (Army L-17A) - [AD 47-31-03](https://openairdocs.org/ad/47-31-03): Fuel Drain Cock · Sierra Hotel Aero Navion (Army L-17A) - [AD 48-06-03](https://openairdocs.org/ad/48-06-03): Hartzell Propeller Blade Inspection · Sierra Hotel Aero Navion (Army L-17A) - [AD 48-08-03](https://openairdocs.org/ad/48-08-03): Fuel Valve Control Support Clip · Sierra Hotel Aero Navion (Army L-17A) - [AD 48-29-01](https://openairdocs.org/ad/48-29-01): Fuel Pump Drain · Sierra Hotel Aero Navion (Army L-17A) - [AD 49-05-03](https://openairdocs.org/ad/49-05-03): Continental Engines Bearing Inserts · Sierra Hotel Aero Navion (Army L-17A) and Navion A (Army L-17B and L-17C) - [AD 49-09-02](https://openairdocs.org/ad/49-09-02): Booster Pump Rework · Sierra Hotel Aero Navion (Army L-17A) and Navion A (Army L-17B and L-17C) - [AD 49-11-01](https://openairdocs.org/ad/49-11-01): Carter Fuel Pump Rework · Sierra Hotel Aero Navion (Army L-17A) and Navion A (Army L-17B and L-17C) - [AD 49-12-02](https://openairdocs.org/ad/49-12-02): Fuel Pumps · Sierra Hotel Aero Navion (Army L-17A) and Navion A (Army L-17B and L-17C) - [AD 49-28-01](https://openairdocs.org/ad/49-28-01): Unsatisfactory Spinner · Sierra Hotel Aero Navion (Army L-17A) and Navion A (Army L-17B and L-17C) - [AD 50-05-02](https://openairdocs.org/ad/50-05-02): Push-Pull Controls · Textron 35, A35, Push-Pull Controls and 1 more - [AD 50-10-02](https://openairdocs.org/ad/50-10-02): Air Intake Hose · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 51-07-01](https://openairdocs.org/ad/51-07-01): Throttle Housing · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 52-08-02](https://openairdocs.org/ad/52-08-02): Carburetor Ducting · Sierra Hotel Aero Navion B - [AD 52-24-01](https://openairdocs.org/ad/52-24-01): Aileron Control Chain Guard · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 52-26-01](https://openairdocs.org/ad/52-26-01): Stabilizer Spar Web · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 53-03-01](https://openairdocs.org/ad/53-03-01): Hartzell Propeller Vibration · Sierra Hotel Aero Navion B - [AD 53-08-01](https://openairdocs.org/ad/53-08-01): Horizontal Stabilizer Fitting · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 54-18-01](https://openairdocs.org/ad/54-18-01): Wing-to-Fuselage Attachment · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 55-01-01](https://openairdocs.org/ad/55-01-01): Fuselage Frame Cracks · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 56-03-03](https://openairdocs.org/ad/56-03-03): Wing Rear Spar Fitting Inspection · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C) and Navion B - [AD 56-27-04](https://openairdocs.org/ad/56-27-04): Engine Cooling Kit Removal · Sierra Hotel Aero Navion B - [AD 59-06-04](https://openairdocs.org/ad/59-06-04): Hydraulic Actuating Cylinders · Sierra Hotel Aero Navion (Army L-17A), Navion A (Army L-17B and L-17C), Navion B and 1 more - [AD 63-21-05](https://openairdocs.org/ad/63-21-05): Main and Nose Retraction Links · American Navion Society D-16, D-16A, 480 and 8 more - [AD 64-04-05](https://openairdocs.org/ad/64-04-05): Outer Wing Panel · Sierra Hotel Aero Navion D, Navion E, Navion F and 1 more ## Registered aircraft by registry model (OpenAirDocs) - [North American NAVION](https://openairdocs.org/model/north-american-navion): 203 aircraft (registry codes 6150130, 6150137) - [Ryan NAVION](https://openairdocs.org/model/ryan-navion): 170 aircraft (registry code 6150160) - [Ryan NAVION A](https://openairdocs.org/model/ryan-navion-a): 115 aircraft (registry code 6150162) - [Navion NAVION A](https://openairdocs.org/model/navion-navion-a): 99 aircraft (registry code 6150104) - [Ryan NAVION B](https://openairdocs.org/model/ryan-navion-b): 68 aircraft (registry code 6150170) - [Navion NAVION G](https://openairdocs.org/model/navion-navion-g): 61 aircraft (registry code 6150120) - [North American NAVION A](https://openairdocs.org/model/north-american-navion-a): 46 aircraft (registry code 6150132) - [Navion NAVION B](https://openairdocs.org/model/navion-navion-b): 42 aircraft (registry codes 6150112, 6150012) - [Navion NAVION H](https://openairdocs.org/model/navion-navion-h): 36 aircraft (registry code 6150122) - [Navion NAVION F](https://openairdocs.org/model/navion-navion-f): 6 aircraft (registry code 6150118) - [Navion NAVION D](https://openairdocs.org/model/navion-navion-d): 5 aircraft (registry code 6150114) - [North American NAVION B](https://openairdocs.org/model/north-american-navion-b): 3 aircraft (registry code 6150140) - [Ryan NAVION G](https://openairdocs.org/model/ryan-navion-g): 3 aircraft (registry code 6150178) - [North American NAVION F](https://openairdocs.org/model/north-american-navion-f): 2 aircraft (registry code 6150146) - [Ryan NAVION D](https://openairdocs.org/model/ryan-navion-d): 2 aircraft (registry code 6150172) - [North American NAVION D](https://openairdocs.org/model/north-american-navion-d): 1 aircraft (registry code 6150142) - [North American NAVION G](https://openairdocs.org/model/north-american-navion-g): 1 aircraft (registry code 6150148) - [Ryan NAVION E](https://openairdocs.org/model/ryan-navion-e): 1 aircraft (registry code 6150174) - [Navion NAVION E](https://openairdocs.org/model/navion-navion-e): 0 aircraft (registry code 6150116) - [North American NAVION E](https://openairdocs.org/model/north-american-navion-e): 0 aircraft (registry code 6150144) - [Ryan NAVION F](https://openairdocs.org/model/ryan-navion-f): 0 aircraft (registry code 6150176) ## STCs approved under this data sheet (271, 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 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 SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [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 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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA543SW](https://openairdocs.org/stc/SA543SW): Installation of Alcor turbocharger on aircraft modified to Continental IO-470-H engines.. Alcor LLC - [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC - [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 SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine - [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc - [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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA46GL](https://openairdocs.org/stc/SA46GL): Install Cleveland Aircraft Products wheel and brake conversion kit, P/N 199-52A.. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA36GL](https://openairdocs.org/stc/SA36GL): Install Cleveland Aircraft Products wheel and brake conversion kit, P/N 199-52.. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA4882NM](https://openairdocs.org/stc/SA4882NM): Installation of Moonshadow full view canopy.. Russell Herrington - [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 SA7088NM](https://openairdocs.org/stc/SA7088NM): Installation of a Teledyne Continental Motors IO-550B engine; McCauley D3A32C409C/82NDB-2 propeller; tubular engine mount; cowling; baffles; air induction system; and cowl flap mechanism. Navion Customs LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King) - [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 SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA2372CE](https://openairdocs.org/stc/SA2372CE): Installation of Teledyne Continental IO-520-K engine and McCauley D3A34C401/90DFA-12 propeller. Kevin Lewis Martinez - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA1190CE](https://openairdocs.org/stc/SA1190CE): Installation of King KFC 200 flight control system (2 axis).. Honeywell International Inc - [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. Honeywell International Inc - [STC SA4-1007](https://openairdocs.org/stc/SA4-1007): Installation of balance weights(Brittain Aircraft P/N 3010) on leading edge of Navion ailerons.. General Aviation Modifications Inc. - [STC SA4-1121](https://openairdocs.org/stc/SA4-1121): Increase in allowable gross weight from 2850 to 3100 pounds per STC SA4-915 when equipped with 20 gallon wing-tip tanks (Brittain Aircraft P/N 1000) installed.. General Aviation Modifications Inc. - [STC SA4-915](https://openairdocs.org/stc/SA4-915): Installation of Brittain Mark II20-gallon wing tip tanks(P/N 2009).. General Aviation Modifications Inc. - [STC SA758WE](https://openairdocs.org/stc/SA758WE): Installation of modified Navion main landing gear wheel and axle. Eligible only on the Navion aircraft models which have Goodrich (Hayes expander tube brakes) wheels Models 6057MD or G-14-720-NO-1.. General Aviation Modifications 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00950NY](https://openairdocs.org/stc/SA00950NY): Modification of forward cockpit seats and provisions for installation of upper torso restraint system.. Timothy Mulhall - [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 271: https://openairdocs.org/tcds/A-782/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.