TCDS A-790

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Rev. No. 37 35 35 35 33 33 33 33 33 33 33 33 36 37 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-790 Revision 37 Textron Aviation Inc. 190 (LC-126A,B,C) 195 195A 195B July 29, 2015 TYPE CERTIFICATE DATA SHEET NO. A-790 This data sheet which is part of Type Certificate No. A-790 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 I. Model 195 (LC-126A,B,C), 5 PCLM (Normal Category), Approved June 12, 1947; 2 PCLM (Utility Category), Approved November 21, 1947; 5 PCSM (Normal Category), Approved May 3, 1948. (The LC-126C version incorporates relocated battery, aileron control system, and large baggage door to facilitate dual stretchers, reference Items 302(b), 605(c) and 609. Eligible landplane, seaplane and skiplane). Engine Jacobs R755-A2 with magneto-battery combination ignition system (See items 106 and 109 for optional engines) Fuel 80 min. octane aviation gasoline Engine Limits For all operations, 2200 r.p.m. (300 hp.) Airspeed Limits Landplane: Maneuvering 125 m.p.h. (109 knots) True Ind.(Normal Category) 130 m.p.h. (113 knots) True Ind.(Utility Category) Max. structural cruising 178 m.p.h. (155 knots)True Ind. Never exceed 200 m.p.h. (174 knots)True Ind. Flaps extended 130 m.p.h. (113 knots)True Ind. (See Note 3 for item 610) Seaplane: Maneuvering 125 m.p.h. (109 knots)True Ind. Max. structural cruising 165 m.p.h. (144 knots)True Ind. Never exceed 200 m.p.h. (174 knots)True Ind. Flaps extended 130 m.p.h. (113 knots)True Ind. A-790 2 Rev. 37 I. Model 195 (cont’d) C.G. range Landplane: (See NOTE 3 for items 610 and 611) (Normal Category) (+44.5) to (+48.3) at 3350 lb. (+36.9) to (+48.3) at 2500 lb. or less Straight line variation between points given 36 38 40 42 44 46 48 2000 2500 3000 3500 INCHES LB. NORMAL CATEGORY FRONT LIMIT REAR LIMIT (Utility Category) (+39.1) to (+42.2) at 2950 lb. (+36.9) to (+42.2) at 2500 lb. or less Straight line variation between points given 36 38 40 42 44 46 48 2000 2500 3000 3500 INCHES LB. UTILITY CATEGORY FRONT LIMIT REAR LIMIT Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. (+38.2) to (+47.4) at 2850 lb. or less Straight line variation between points given 36 38 40 42 44 46 48 2000 2500 3000 3500 INCHES LB. NORMAL CATEGORY FRONT LIMIT REAR LIMIT Empty Wt. C.G. Range Not available Maximum Weight Landplane: (Normal Category) 3350 lb. (Utility Category) 2950 lb. Seaplane: (Normal Category) 3600 lb. No. of Seats 5 (two at +36, three at +69.5) Maximum Baggage 220 lb. (+92) (Model 195 Standard). No baggage for Utility Category. (See item 606 for other baggage arrangements) Rev. 37 3 A-790 I. Model 195 (cont’d) Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63). (38 gal. usable fuel in each tank). (See NOTE 1 for unusable fuel and item 108 for optional fuel tanks). Oil Capacity 5 gal. (+4.5) (See NOTE 1 for data on unusable oil) Control Surface Movements Wing flaps Down 45° Aileron tab Fixed Ailerons Up 25° Down 25° Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° Elevators Up 28° Down 17° Rudder Right 21° Left 21° Serial Nos. Eligible 7004 through 7999 16000 through 16183 Prior to civil certification of LC-126A,B and C aircraft, which have been operated by the Military Services, must be modified in accordance with Cessna Dwg. 0400115. This drawing and FAA approved airplane flight manual may be obtained thru Cessna's dealer organization. The dealer should also have a file of Cessna Service Letters which should be reviewed for applicability. Required Equipment Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(a) or (b). Skiplane: Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(a). Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302, 302(a), 303 (when used in night operation if flap position indicator not installed), 403(a) and 602. II. Model 190 (5 PCLM (Normal Category)), Approved July 1, 1947; 2 PCLM (Utility Category), Approved November 21, 1947; 5 PCSM (Normal Category), Approved May 3, 1948. (Same as Model 195 except for engine installation) Engine Continental W670-23. Eligible with either dual magnetos or magneto-battery combination engine ignition system. Fuel 80 min. octane aviation gasoline Engine Limits For all operations, 2200 r.p.m. (240 hp.) Airspeed Limits Landplane: Maneuvering 125 m.p.h.(109 knots) True Ind. (Normal Category) 130 m.p.h.(113 knots) True Ind. (Utility Category) Max.structural cruising 178 m.p.h.(155 knots) True Ind. Never exceed 200 m.p.h.(174 knots) True Ind. Flaps extended 130 m.p.h.(113 knots) True Ind. (See NOTE 3 for item 610) Seaplane: Maneuvering 125 m.p.h.(109 knots)True Ind. Max.structural cruising 165 m.p.h.(144 knots)True Ind. Never exceed 200 m.p.h.(174 knots)True Ind. Flaps extended 130 m.p.h.(113 knots)True Ind. A-790 4 Rev. 37 II. Model 190 (cont’d) C.G. Range All limits same as Model 195 - see figures under Section I Landplane: (See NOTE 3 for items 610 and 611) (Normal Category) (+44.5) to (+48.3) at 3350 lb. (+36.9) to (+48.3) at 2500 lb. or less (Utility Category) (+39.1) to (+42.2) at 2950 lb. (+36.9) to (+42.2) at 2500 lb. or less Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. (+38.2) to (+47.4) at 2850 lb. or less Straight line variation between points given. Empty Wt. C.G. Range Not available Maximum Weight Landplane: (Normal Category) 3350 lb. (Utility Category) 2950 lb. Seaplane (Normal Category) 3600 lb. No. of Seats 5 (two at +36, three at +69.5) Maximum Baggage 220 lb. (+92). No baggage for Utility Category. See Item 606 for auxiliary baggage compartment Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63). (Usable fuel in each tank: 38 gal. with item 102(b); 37.5 gal. with gravity fuel system). (See NOTE 1 for unusable fuel, NOTE 2 for placard with gravity fuel system, and Item 108 for optional fuel tanks). Oil Capacity 5 gal. (+4.5) See NOTE 1 for data on unusable oil. Control Surface Movements Wing flaps Down 45° Aileron tab Fixed Ailerons Up 25° Down 25° Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° Elevators Up 28° Down 17° Rudder Right 21° Left 21° Serial Nos. Eligible 7004 through 7999 16000 through 16183 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: Items 1(a) and (c), 102(b), 103, 201, 202, 204, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(a) or (b). Skiplane: Items 1(a) and (c), 102(b), 103, 204, 208, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), 403(a). Seaplane: Items 1(a) and (c), 102(b), 103, 209, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), 403(a) and 602. III. Model 195A; 5 PCLM (Normal Category), Approved January 6, 1950; 2 PCLM (Utility Category), Approved January 6, 1950; 5 PCSM (Normal Category), Approved August 18, 1950. (Same as Model 195 except for engine.) Engine Jacobs L-4MB (R-755-9) with magneto-battery combination ignition system. Fuel 73 min. octane aviation gasoline Engine Limits Maximum continuous, 2000 r.p.m. (225 hp.) Takeoff (one minute), 2200 r.p.m. (245 hp.) Rev. 37 5 A-790 III. Model 195A (cont’d) Airspeed Limits Landplane: Maneuvering 125 m.p.h.(109 knots)True Ind. (Normal Category) 130 m.p.h.(113 knots)True Ind. (Utility Category) Max. structural cruising 178 m.p.h.(155 knots)True Ind. Never exceed 200 m.p.h.(174 knots)True Ind. Flaps extended 130 m.p.h.(113 knots)True Ind. (See Note 3 for item 610.) Seaplane: Maneuvering 125 m.p.h.(109 knots)True Ind. Max. structural cruising 165 m.p.h.(144 knots)True Ind. Never exceed 200 m.p.h.(174 knots)True Ind. Flaps extended 130 m.p.h.(113 knots)True Ind. C.G. Range All limits same as Model 195 - See figures under Section I. Landplane: (See NOTE 3 for items 610 and 611) (Normal Category) (+44.5) to (+48.3) at 3350 lb. (+36.9) to (+48.3) at 2500 lb. or less (Utility Category) (+39.1) to (+42.2) at 2950 lb. (+36.9) to (+42.2) at 2500 lb. or less Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. (+38.2) to (+47.4) at 2850 lb. or less Straight line variation between points given Empty Wt. C.G. Range Not available Maximum Weight Landplane: (Normal Category) 3350 lb. (Utility Category) 2950 lb. Seaplane: (Normal Category) 3600 lb. No. of Seats 5 (two at +36, three at +69.5) Maximum Baggage 220 lb. (+92). No baggage for Utility Category. See item 606 for auxiliary baggage compartment. Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at (+63) (38 gal. usable fuel in each tank) (See NOTE 1 for unusable fuel) Oil Capacity 5 gal. (+4.5) (See NOTE 1 for data on unusable fuel) Control Surface Movements Wing flaps Down 45° Aileron tab Fixed Ailerons Up 25° Down 25° Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° Elevators Up 28° Down 17° Rudder Right 21° Left 21° Serial Nos. Eligible 7004 through 7999 16000 through 16183 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(e). Skiplane: Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(a). Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), 403(f) and 602. A-790 6 Rev. 37 IV. Model 195B, 5 PCLM (Normal Category), Approved March 31, 1952; 2 PCLM (Utility Category), March 31, 1952; 5 PCSM (Normal Category), Approved March 31, 1952. (Same as Model 195 except for engine.) Engine Jacobs R-755B2 with magneto-battery combination ignition system Fuel 80 minimum octane aviation gasoline Engine Limits For all operations, 2200 r.p.m. (275 hp.) Airspeed Limits Landplane: Maneuvering 125 m.p.h.(109 knots) True Ind. (Normal Category) 130 m.p.h.(113 knots) True Ind. (Utility Category) Max. structural cruising 178 m.p.h.(155 knots) True Ind. Never exceed 200 m.p.h.(174 knots) True Ind. Flaps extended 130 m.p.h.(113 knots) True Ind. (See Note 3 for item 610) Seaplane: Maneuvering 125 m.p.h.(109 knots) True Ind. Max. structural cruising 165 m.p.h.(144 knots) True Ind. Never exceed 200 m.p.h.(174 knots) True Ind. Flaps extended 130 m.p.h.(113 knots) True Ind. C.G. Range All limits same as Model 195 - See figures under Section I. Landplane: (See NOTE 3 for items 610 and 611) (Normal Category) (+44.5) to (+48.3) at 3350 lb. (+36.9) to (+48.3) at 2500 lb. or less (Utility Category) (+39.1) to (+42.2) at 2950 lb. (+36.9) to (+42.2) at 2500 lb. or less Seaplane: (Normal Category) (+44.5) to (+47.4) at 3600 lb. (+38.2) to (+47.4) at 2850 lb. or less Straight line variation between points given Empty Wt. C.G. Range Not available Maximum Weight Landplane: (Normal Category) 3350 lb. (Utility Category) 2950 lb. Seaplane: (Normal Category) 3600 lb. No. of Seats 5 (two at +36, three at +69.5) Maximum Baggage 220 lb. (+92). No baggage for Utility Category. See item 606 for auxiliary baggage compartment. Fuel Capacity 81 gal. total (two 40.5 gal. tanks in wings at +63) (38 gal. usable fuel in each tank) (See NOTE 1 for unusable fuel) Oil Capacity 5 gal. (+4.5) (See NOTE 1 for data on unusable oil) Control Surface Movements Wing flaps Down 45° Aileron tab Fixed Ailerons Up 25° Down 25° Elevator tab (See NOTE 3 for item 611) Up 12.5° Down 31° Elevators Up 28° Down 17° Rudder Right 21° Left 21° Serial Nos. Eligible 7004 through 7999 16000 through 16183 Rev. 37 7 A-790 IV. Model 195B (cont’d) Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: Landplane: Items 1(a) and (b), 102(a), 103, 104, 201, 202, 204, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(h). Skiplane: Items 1(a) and (b), 102(a), 103, 104, 204, 208, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), and 403(h). Seaplane: Items 1(a) and (b), 102(a), 103, 104, 209, 301, 302(a), 303 (when used in night operation if flap position indicator not installed), 403(i) and 602. Specifications Pertinent To All Models Datum Front face of firewall Leveling Means Top of fuselage immediately aft of wing trailing edge Certification Basis: CAR 3 dated December 15, 1946. Model 195B certificated under delegation option provisions of Part 410 of the Regulations of the Administrator. Type Certificate No. A-790 issued June 12, 1947. Production Basis: Production Certificate No. 4. Export Eligibility Landplane, seaplane and skiplane eligible for export to all countries subject to the provisions of FS P8130-1. 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 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, and therefore attention should be paid to workmanship and conformity with pertinent data called for in this specification. An item preceded by two asterisks (**) indicates approval under Federal Aviation Regulations Part 21. A-790 8 Rev. 37 Specifications Pertinent To All Models (cont’d) Propellers and Propeller Accessories (Excepting Deicing equipment) 195 190 195A 195B 1. Hamilton Standard constant speed (a) Hub 2B20, blades 6135-15 or 6135-16 104 lb. (-35) (-32) (-35) (-35) Pitch settings at 42 in. sta. ** Model 190, 195A & 195B: Low 9° - 12°, high 24° - 27° ** Model 195: Low 10.3° - 12°, high 25.3° - 27° (Propeller to be indexed with blades in line with crankthrow - 0° or 180° position) Diameter: (Not over 93 in.,not under 91-1/8 in. (b) Governor, Hamilton Standard - 1A4 8 lb. (-5) (-5) (-5) (c) Governor, Hamilton Standard - 1M12 or 4M12 8 lb. (-25) *(d) Montgomery spinner for Ham.Std.2B20 propeller 8 lb. (-35) (-32) (-35) (-35) (Special Ham.Std.bolts,P/N70234 required for inst. this item) **(e) Spinner (Cessna Dwg. 0352171) +4.5 lb. (-35) (-32) (-35) (-35) *(f) Spinner - Mfgr. Aircraft Access. Inc., 2630 8 lb. (-35) (-32) (-35) (-35) So.Wabash Ave.,Chicago,Ill.(Dwg. Nos. 77596-1,-1A, -2,-2A & -3). Special Ham. Std.bolts P/N 70234 required for inst. this item Engine and Engine Accessories - Fuel and Oil System 101 Starter (Eclipse 397-13) 20 lb. (-2) (-6) (-2) (-2) 102. Fuel pumps (a) Engine-driven(Romec RD-4140 or Pesco 2F-R400- 2 lb. (-5) (-5) (-5) BYLA remarked and reworked by Cessna dwg.0350284) (b) Engine-driven(Candler Hill Titan Model 200, 2 lb. (-4) H2E3-16) (not required with gravity fuel system) 103. Carburetor air filter X X X X 104. Oil radiator (UAP Model U-3140C) 9 lb. (-18) (-18) (-18) 105. Vacuum pumps (a) Engine-driven (Pesco 3P-194-E) 5 lb. (-5) (- 5) (- 5) (b) Engine-driven (Romec P-207)(Elig. with gravity fuel system) 4 lb. (- 4) *106. Jacobs L-4MB (R-755-9) Engines Use actual wt. Eligible on 195 landplane with following limits: Fuel 73 min.octane aviation gasoline Engine limits Takeoff (one min.), 2200 r.p.m. (245 hp.) For all other operations, 2000 r.p.m. (225 hp.) When this engine is installed, revised engine baffles, relocated oil cooler, modified engine mount bolts, relocated engine breather and oil separator vent lines, remarked power plant instruments, and FAA Approved Airplane Flight Manual Supplement dated October 21, 1948, as approved for the Purdue Aeronautics Corp., Lafayette, Ind., must be incorporated. 195 190 195A 195B 107. Winterization equipment (Cessna dwg. 0350285 & 2 lb. (-30) (-27) (-30) (-30) 0350286 for Model 195; Cessna dwg. 0350285 & 0350302 for Model 190). Item 403(c) required when this equipment installed. 108. Two 50.5 gal. fuel tanks in wings installed +2 lb. (+63) (+63) (+63) per Cessna dwg. 0320001 (replaces two 40.5 gal. tanks). With this item installed, fuel capacity is 101 gal. total at (+63)(46 gal.) usable in each tank). Item 403(d) required when these tanks are installed. (See NOTE 1 for weight of unusable fuel) Rev. 37 9 A-790 Specifications Pertinent To All Models (cont’d) Engine and Engine Accessories - Fuel and Oil System (cont’d) *109. Jacobs L-6MB engine Use actual weight Eligible on 195 landplane with the following limits: Fuel 80 min.octane aviation gasoline Engine limits Takeoff (one min.) 330 hp. 2200 r.p.m. 26 in.Hg.M.P. Max. continuous 300 hp. 2100 r.p.m. 24.5 in.Hg M.P.at S.L. 200 hp. 2100 r.p.m. 23.5 in.Hg M.P. at 3700' With propeller (item 1),Ham.Std.2B20/6135A-15 Pitch settings at 42" sta.: Low -13°, high 28° Installation of this item to be accomplished in accordance with data approved for Scott Aero Services, Inc., 4100 Donald Douglas Drive, Long Beach, Calif. 90808. Item 403(g) required when this item installed. Landing Gear and Floats 201. Two main wheel-brake assemblies, Type III (a) Goodyear Model L610HBM (6.50-10) 29 lb. (+25) (+25) (+25) (+25) Wheel Assembly 530858-M Brake Assembly 511613-M (b) Goodyear Model CL8HBM (6.50-8 castering) 29 lb. (+25) (+25) (+25) (+25) Wheel assembly 9530505 L.H. 9530506 R.H. Brake assembly 9530503 L.H. 9530504 R.H. Installed in accordance with Cessna dwg. 0341150 202. (a) Two main wheel 4-ply rating tires, 6.50-10, 28 lb. (+25) (+25) (+25) (+25) Type III with regular tubes (b) Two main wheel 6-ply rating tires, 7.50-10, 38 lb. (+25) (+25) (+25) (+25) Type III with regular tubes (c) Two main wheel 6-ply rating tires, 7.00-8, 31 lb. (+25) (+25) (+25) (+25) Type III with regular tubes 204. Tail wheel assembly, General Model 204-A-702M with 8 lb. (+272) (+272) (+272) (+272) Type I tire 208. Two skis. Skiplane elig. only in normal category. 8 lb. (+272) (+272) (+272) (+272) (Either a Cessna Skiplane Flight Manual dated February 10, 1949 (190), November 14, 1947 (195) or the following required as supplement to the Airplane Flight Manual with any of these skis installed: "PERFORMANCE WITH SKIS INSTALLED Takeoff and Landing: Under the most favorable conditions of smooth packed snow at temperatures approximately 30°F. skiplane takeoff distance is approximately 10 percent greater than the distance shown for the landplane. In applying the performance data, caution should be exercised in that lower temperatures or other snow conditions will increase the ski friction and hence increase the takeoff run and either increase or decrease the landing run. Climb Performance: The skiplane rate of climb is approximately 50 feet per minute less than the landplane." (a) Federal A-3500 according to Cessna dwg. 0340001 Use actual wt. change or Federal Inst. dwg. 11R178 (b) Federal A-3500A Federal Inst. dwg. 11R178 Use actual wt. change (c) Federal AWB-3500 Main and AWT-3500 Tail Use actual wt. change Wheel Skis, in accordance with Federal Aircraft Works dwg. 11R692 and 11R874 The following placard is required with this installation: "Do Not Extend or Retract Skis while in motion on the Ground." A-790 10 Rev. 37 Specifications Pertinent To All Models (cont’d) Landing Gear and Floats (cont’d) 195 190 195A 195B 209. Float installation, two Edo 38-3430 per Cessna +272 lb. (+43) (+43) (+43) (+43) dwg. 0341102 210. Two wheel streamlines per Cessna dwg. 0341143 10 lb. (+25) (+25) (+25) (+25) 211. Tail ski, Federal AT-3500 per Cessna dwg. 0342102 8 lb. (+272) (+272) (+272) (+272) 212. Two 3/4 in. tapered spring type landing gear per -25 lb. (+25) (+25) (+25) (+25) Cessna dwg. 0341109 *213. Two "no drag" wheel fenders per Liquid Tool Co., 8 lb. (+26) (+26) (+26) (+26) Box 299, Morrow, Ohio, dwg. 105 Electrical Equipment 301. Generator (Eclipse 308-1A or Eclipse 309-8A) 22 lb. (- 2) (- 2) (- 2) (- 2) 302. Battery - 12 v. 24 a. hr. (a) Installation in accordance with Cessna dwg. 0310005 36 lb. (+108) (+108) (+108) (+108) (b) Installation in accordance with Cessna dwg. 0311063 36 lb. (+ 86) (+ 86) (+ 86) (+86) 303. Landing lights (Grimes G-3800) 5 lb.ea.(+56) (+ 56) (+56) (+56) *304. Generator (Eclipse 309A-8A, 50 a. 22 lb. ( -2) ( -2) ( -2) ( -2) *305. Voltage regulator (a) Delco-Remy 1118340 Neglect wt. (b) Delco-Remy 1118713 with shock mounting kit 1910966 *306. Generator (Eclipse 30E01-1) 50 a. 24 lb. ( -2) *307. Voltage regulator, Eclipse 1337-17 Neglect wt. *308. Generator (Eclipse 790-1-B modified per Duryee 22 lb. ( -2) ( -2) ( -2) Aero. Ser. dwg. DAS 47) 50 a. (Item 305 required) *309. Voltage regulator, Delco Remy 1118884 Neglect wt. *310. Generator (Eclipse 790-1-B modified per Garwin 22 lb. ( -2) ( -2) ( -2) dwg. G50A and installed according to Garwin instructions dated July 25, 1955), 50 a. (Item 305 or 309 required). Interior Equipment 401. Cabin heater (Exhaust manifold muff type) 3 lb. (0) (0) (0) (0) 402. Omitted 403. (a) FAA Approved Airplane Flight Manual and pertinent revisions applicable to the particular model and serial number (b) FAA Approved Airplane Flight Manual dated September 14, 1949 (pertinent to decrease in landing distance) (c) FAA Approved Supplement No. 1 to Airplane Flight Manual (pertinent to winterization equipment, Item 107) (d) FAA Approved Supplement No. 2 to Airplane Flight Manual (pertinent to 50.5 gal. fuel tanks, item 108) (e) FAA Approved Airplane Flight Manual dated December 27, 1949 (Model 195A Landplane) (f) FAA Approved Airplane Flight Manual dated August 18, 1950 (Model 195A Seaplane) *(g) FAA Approved Airplane Flight Manual dated March 15, 1951 (Model 195 Landplane with item 109 installed) **(h) DOA Approved Airplane Flight Manual dated March 31, 1952 (Model 195B Landplane and Skiplane) **(I) DOA Approved Airplane Flight Manual dated March 31, 1952 (Model 195B Seaplane only) **(j) DOA Approved Airplane Flight Manual dated April 22, 1953 (Model 190 Landplane and Skiplane with items 610 and 611 installed) **(k) DOA Approved Flight Manual dated April 22, 1953 (Model 195 Landplane and Skiplane with items 610 and 611 installed) **(l) DOA Approved Flight Manual dated April 22, 1953 (Model 195A Landplane and Skiplane with items 610 and 611 installed) **(m) DOA Approved Flight Manual dated April 22, 1953