TCDS 1A9

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. No. 22 13 13 13 13 13 13 13 13 13 13 13 13 13 14 14 14 14 14 14 Rev 22 changed TC holder. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A9 Revision 23 Taylorcraft 2000, LLC 19 F19 F21 F21A F21B F22 F22A F22B F22C March 22, 2022 AIRCRAFT SPECIFICATION NO. 1A9 Type Certificate Holder Taylorcraft 2000, LLC Dba Aircraft Taylorcraft Co., LLC 815 N Minnesota Avenue Brownsville, TX 78521 Type Certificate Ownership Record Taylorcraft Corporation transferred ownership to Syncrom, Inc., on October 19, 1994. Syncrom, Inc. transferred ownership to Airborne Marketing, Inc. on January 8, 1997. Airborne Marketing transferred ownership to Lee F. Booth on April 26, 1999. Lee F. Booth, dba Taylorcraft Aerospace, transferred ownership to Harvey & Vera Patrick Foundation on May 10, 2000. Harvey & Vera Patrick Foundation transferred ownership to Taylorcraft 2000, LLC on August 8, 2000. Taylorcraft 2000 LLC transferred ownership to Taylorcraft Aviation LLC on March 5, 2003 Taylorcraft Aviation LLC, 2124 n. Central Ave., Brownsville, TX 78521 transferred ownership to Taylorcraft 2000 LLC on May 21, 2008 Taylorcraft 2000 LLC transferred to Taylorcraft 2000 LLC Dba Aircraft Taylorcraft Co., LLC on October 7, 2009. I - Model 19, 2 PCLM (Normal and Utility Categories), Approved June 20, 1951 Engine Continental C85-12, C85-12F Fuel 80 Octane minimum grade aviation gasoline Engine Limits For all operations, 2575 rpm (85 HP) Airspeed Limits VP (Maneuvering) (Normal) 87 mph (76 knots) (True Indicated) (Utility) 86 mph (75 knots) Vno (Maximum Structural (Normal) 108 mph (94 knots) Cruising) (Utility) 104 mph (90 knots) Vne (Never exceed) (Normal) 136 mph (118 knots) (Utility) 141 mph (123 knots) C.G. Range Normal: (+16.1) to (+20.0) at 1500 lb. (+14.2) to (+20.0) at 1280 lb. or less Utility: (+15.1) to (+20.0) at 1380 lb. (+14.2) to (+20.0) at 1280 lb. or less 1A9, Rev 22 Page 2 of 20 I - Model 19 (Cont’d) Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight Normal Category: 1500 lb. Utility Category: 1380 lb. No. of Seats 2 (+23) Maximum Baggage 72 lbs. (+57) Fuel Capacity 24 gals. (12 gal. tank in fuselage at -9 and 6 gal. tank in each wing at +24) Oil Capacity 4-1/2 qts. (+30) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 25” down Aileron 23” up 23” down Rudder 25” right 26” left Serial Nos. Eligible 12,000, 4-13000 and up, except 4-13100 and 4-13102 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1, 2, or 3; 201(a); 202; 203; and 401(a) II - Model F19, 2 PCLM (Normal and Utility Categories), Approved July 3, 1973 Engine Continental 0-200-A with CMC oil cap retainer assembly # 637130 Fuel 80/87 octane minimum grade aviation gasoline Oil Detergent oil meeting Continental Specification MHS-24 Page 3 of 20 1A9, Rev 21 II - Model F19 (Cont’d) Engine Limits See NOTE 3 For aircraft S/N F-001 to F-153 inclusive: For all operations: 2750 rpm (100 HP) For aircraft S/N F-154 and up: Maximum Normal Operating Power: 2500 rpm (73 HP) For all operations: 2750 rpm (100 HP) Airspeed Limits VP (Maneuvering) (Normal) 87 mph (76 knots) (True Indicated) (Utility) 86 mph (75 knots) Vno (Maximum Structural (Normal) 108 mph (94 knots) Cruising) (Utility) 104 mph (90 knots) Vne (Never Exceed) (Normal) 136 mph (118 knots) (Utility) 141 mph (123 knots) C.G. Range Normal: (+16.1) to (+20.0) at 1500 lb. (+14.2) to (+20.0) at 1280 lb. or less Utility: (+15.1) to (+20.0) at 1380 lb. (+14.2) to (+20.0) at 1280 lb. or less Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight Normal Category: 1500 lb. Utility Category: 1380 lb. No. of Seats 2 (+23) Maximum Baggage 72 lb. (+57) Fuel Capacity 24 gal. total, 21 gal. usable (12 gal. tank in fuselage at -9 and 6 gal. tank in each wing at +24) See NOTE 1 for data on unusable fuel. Oil Capacity 6 qt. (-29.4) 1A9, Rev 22 Page 4 of 20 II - Model F19 (Cont’d) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Serial Nos. Eligible F-001 thru F-1000 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, 201(b), 202, 203, 401(b) III - Model F21, 2 PCLM (Normal or Utility Category), Approved July 2, 1980 The Model F21 is similar to the Model F19 except for the installation of a Lycoming 0-235-L2C engine, baffles, cowling, engine mount, and hydraulic brakes. Engine Lycoming 0-235-L2C with Marvel Schebler MA-3A, Part Number 10-3103-1, carburetor. The internally mounted Lycoming Thermostatic Oil Bypass and Pressure Relief Valve is not appropriate for this installation. See NOTE 4. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2600 rpm (112 HP) Takeoff (5 min.), 2800 rpm (118 HP) Airspeed Limits VP (Maneuvering) (Normal): 87 mph (76 knots) (True Indicated) (Utility): 86 mph (75 knots) Vno (Maximum Structural Cruising) (Normal): 108 mph (94 knots) (Utility): 86 mph (90 knots) Vne (Never Exceed) (Normal): 136 mph (118 knots) (Utility): 141 mph (123 knots) C.G. Range Normal: (+16.1) to (+20.0) at 1500 lb. (+14.2) to (+20.0) at 1280 lb. or less Utility: (+15.1) to (+20.0) at 1380 lb. (+14.2) to (+20.0) at 1280 lb. or less Straight line variation between points given. Page 5 of 20 1A9, Rev 21 III - Model F21 (Cont’d) Empty Weight C.G. Range None Maximum Weight Normal Category: 1500 lb. Utility Category: 1380 lb. No. of Seats 2 (+23) Maximum Baggage 72 lb. (+57) Fuel Capacity 6 qt. (-28.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Serial Nos. Eligible F-1001 thru F-1499 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 6, 103, 104, 105, 106, 202, 203, 204, 401(c) IV - Model F21A, 2 PCLM (Normal or Utility Category), Approved November 15, 1982 The Model F21A is similar to the Model F21 except for increasing the wing fuel to two 21-gallon tanks and the removal of the 12-gallon fuselage tank. Engine Lycoming 0-235-L2C with Marvel Schebler MA-3A, Part Number 10-3013-1, carburetor. The internally mounted Lycoming Thermostatic Oil Bypass and Pressure Relief Valve is not appropriate for this installation. See NOTE 4. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2600 rpm (112 HP) Takeoff (5 mins.), 2800 rpm (118 HP) Airspeed Limits VP (Maneuvering) (Normal): 87 mph (76 knots) (True Indicated) (Utility): 86 mph (75 knots) Vno (Maximum Structural Cruising) (Normal): 108 mph (94 knots) (Utility): 104 mph (90 knots) Vne (Never Exceed) (Normal): 136 mph (118 knots) (Utility): 141 mph (123 knots) C.G. Range Normal: (+16.1) to (+20.0) at 1500 lbs. (+14.2) to (+20.0) at 1280 lbs. or less Utility: (+15.1) to (+20.0) at 1380 lbs. (+14.2) to (+20.0) at 1280 lbs. or less 1A9, Rev 22 Page 6 of 20 IV - Model F21A (Cont’d) Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight Normal Category: 1500 lbs. Utility Category: 1380 lbs. No. of Seats 2 (+23) Maximum Baggage 72 lbs. (+57) Fuel Capacity 42 gals. total, 40 gals. usable (a 21 gal. tank in each wing at +24). See NOTE 1 for data on unusable fuel. Oil Capacity 6 qts. (-28.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Serial Nos. Eligible F-1500 thru F-1506 Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 6, 103, 104, 105, 106, 202, 203, 204, 401(d) Page 7 of 20 1A9, Rev 21 V - Model F21B, 2 PCLM (Normal or Utility Category), Approved September 6, 1985 The Model F21B is similar to the Model F21A except for increase in maximum allowable gross weight to 1750 lbs., baggage are capacity increased to 200 lbs., battery relocated to engine firewall, and improved visibility with an optional skylight, lower door window, and corresponding changes in regular windows, doors and interior upholstery. Engine Lycoming 0-235-L2C with Marvel Schebler MA-#A, Part Number 10-3103-1, carburetor. The internally mounted Lycoming Thermostatic Oil Bypass and Pressure Relief Valve is not appropriate for this installation. See NOTE 4. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2600 rpm (112 HP) Takeoff (5 mins.), 2800 rpm (118 HP) Airspeed Limits VP (Maneuvering) (Normal): 93 mph (81 knots) (True Indicated) (Utility): 86 mph (75 knots) Vno (Maximum Structural Cruising) (Normal): 117 mph (102 knots) (Utility): 104 mph (90 knots) Vne (Never Exceed) (Normal): 148 mph (128 knots) (Utility): 141 mph (123 knots) C.G. Range Normal: (+17.2) to (+20.0) at 1750 lbs. (+14.2) to (+20.0) at 1280 lbs. or less Utility: (+14.9) to (+20.0) at 1380 lbs. (+14.2) to (+20.0) at 1280 lbs. or less Straight line variation between points given. 1A9, Rev 22 Page 8 of 20 V - Model F21B (Cont’d) Empty Weight C.G. Range None Maximum Weight Normal Category: 1750 lb. Utility Cateogry: 1380 lb. No. of Seats 2 (+23) Maximum Baggage 200 lb. (+57) Fuel Capacity 42 gal. total, 40 gal. usable (a 21 gal. tank in each wing at +24). See NOTE 1 for data on unusable fuel. Oil Capacity 6 qt. (-28.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Serial Nos. Eligible F-1507 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 6, 103, 104, 105, 107, 202, 203, 204, 401(e), 501. VI - Model F22, 2 PCLM (Normal or Utility Category), Approved August 1, 1988 The Model F22 is basically a Model F21B with the addition of wing flaps, wider doors, top-hinged windows, and fore and aft adjustable individual seats. Engine Lycoming 0-235-L2C with Marvel Schebler MA-3A, Part Number 10-3103-1, carburetor. The internally mounted Lycoming Thermostatic Oil Bypass and Pressure Relief Valve is not appropriate for this installation. See NOTE 4. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum Continuous, 2600 rpm (112 HP) Takeoff (5 min.), 2800 rpm (118 HP) Airspeed Limits VP (Maneuvering) (Normal): 93 mph (81 knots) (Calbrated Airspeed (CAS)) (Utility): 86 mph (75 knots) Vno (Maximum Structural Cruising) (Normal): 117 mph (102 knots) (Utility): 104 mph (90 knots) Vne (Never Exceed) (Normal): 148 mph (128 knots) (Utility): 141 mph (122 knots) Vfe (Maximum Speed, Flaps Extended: 76 mph (66 knots) C.G. Range Normal: (+17.2) to (+20.0) at 1750 lb. (+14.2) to (+20.0) at 1280 lb. or less Utility: (+14.9) to (+20.0) at 1380 lb. (+14.2) to (+20.0) at 1280 lb. or less Page 9 of 20 1A9, Rev 21 VI - Model F22 (Cont’d) Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight Normal Category: 1750 lb. Utility Category: 1380 lb. No. of Seats 2 (+23) Maximum Baggage 200 lb. (+57) Fuel Capacity 42 gal. total, 40 gal. usable (a 21 gal. tank in each wing at +24). See Note 1 for data on unusable fuel. Oil Capacity 6 qt. (-28.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Flaps 0” up 30” down Serial Nos. Eligible F2202 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 6, 103, 104, 105, 106, 202, 203, 204, 401(f), 501. 1A9, Rev 22 Page 10 of 20 VII - Model F22A, 2 PCLM (Normal Category), Approved February 20, 1991 The Model F22A is basically a Model F22 with a tricycle landing gear installed. Engine Lycoming 0-235-L2C with Marvel Schebler MA-3A, Part Number 10-3103-1, carburetor. The internally mounted Lycoming Thermostatic Oil Bypass and Pressure Relief Valve is not appropriate for this installation. See NOTE 4. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2600 rpm (112 HP) Takeoff (5 min.), 2800 rpm (118 HP) Airspeed Limits VP (Maneuvering) (Normal): 93 mph (81 knots) (Calbrated Airspeed (CAS)) Vno (Maximum Structural Cruising) (Normal): 117 mph (102 knots) Vne (Never Exceed) (Normal): 148 mph (128 knots) Vfe (Maximum Speed, Flaps Extended: 76 mph (66 knots)) C.G. Range Normal: (+17.2) to (+20.0) at 1750 lb. (+14.2) to (+20.0) at 1280 lb. or less Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight Normal Category: 1750 lb. No. of Seats 2 (+23) Maximum Baggage 200 lb. (+57) Page 11 of 20 1A9, Rev 21 VII - Model F22A (Cont’d) Fuel Capacity 42 gal. Total, 40 gal. usable (a 21 gal. tank in each wing at (+24). See NOTE 1 for data on unusable fuel. Oil Capacity 6 qt. (-28.5) Control Surface Movements Elevators 27o up 25o down Elevator tab 25o up 30o down Aileron 23o up 23o down Rudder 26o up 26o left Flaps 0o up 30o down Serial Nos. Eligible F2205 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 6, 102, 103, 104, 105, 106, 202, 204, 206, 207, 401(g), 501. VIII - Model F22B, 2 PCLM (Normal Category) Approved July 14, 1992 The Model F22B is basically a Model F22 except it has a Textron Lycoming 0-360-A4M engine installation with matching propeller, battery relocated from firewall to aft fuselage and fuel line sizes increased from 3/8” to 1/2” diameter. Engine Textron Lycoming 0-360-A4M with carburetor. Since an oil cooler is installed, the internally mounted thermostatic oil by-pass and pressure relief valve can be used for this installation. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2700 rpm (180 HP) Airspeed Limits VP (Maneuvering): 93 mph (81 knots) (Calbrated Airspeed (CAS)) Vno (Maximum Structural Cruising): 117 mph (90 knots) Vne (Never Exceed): 148 mph (128 knots) Vfe (Maximum Speed, Flaps extended): 76 mph (66 knots) C.G. Range (+17.2) to (+20.0) at 1750 lb. (+14.2) to (+20.0) at 1280 lb. or less 1A9, Rev 22 Page 12 of 20 VIII - Model F22B (Cont’d) Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight 1750 lb. No. of Seats 2 (+23) Maximum Baggage 200 lb. (+57) Fuel Capacity 42 gal. total, 40 gal. usable (a 21 gal. tank in each wing at +24). See NOTE 1 for data on unusable fuel. Oil Capacity 8 qt. (-27.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Flaps 0” up 30” down Serial Nos. Eligible F2213 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 7, 106, 108, 109, 110, 111, 112, 202, 203, 204, 401(h), 501. Page 13 of 20 1A9, Rev 21 IX - Model F22C, 2 PCLM (Normal Category) Approved February 20, 1992 The Model F22C is basically a Model F22A except is has a Textron Lycoming 0-360-AFM engine installation with matching propeller, battery relocated from firewall to aft fuselage and fuel line sizes increased from 3/8” to 1/2” diameter. Engine Textron Lycoming 0-360-A4M with carburetor. Since an oil cooler is installed, the internally mounted thermostatic oil by-pass and pressure relief valve can be used for this installation. Fuel 100/130 or 100 LL minimum grade aviation gasoline Engine Limits Maximum continuous, 2700 rpm (180 HP) Airspeed Limits VP (Maneuvering): 93 mph (81 knots) Vno (Maximum Structural Cruising): 117 mph (90 knots) Vne (Never Exceed): 148 mph (128 knots) Vfe (Maximum Speed, Flaps Extended): 76 mph (66 knots) C.G. Range (+17.2) to (+20.0) at 1750 lb. (+14.2) to (+20.0) at 1280 lb. or less Straight line variation between points given. Empty Weight C.G. Range None Maximum Weight 1750 lb. No. of Seats 2 (+23) Maximum Baggage 200 lb. (+57) Fuel Capacity 42 gal. total, 40 gal. usable (a 21 gal. tank in each wing at +24). See NOTE 1 for data on unusable fuel. 1A9, Rev 22 Page 14 of 20 IX - Model F22C (Cont’d) Oil Capacity 8 qt. (-27.5) Control Surface Movements Elevators 27” up 25” down Elevator tab 25” up 30” down Aileron 23” up 23” down Rudder 26” right 26” left Serial Nos. Eligible F2212 and up Required Equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 7, 105, 108, 109, 110, 111, 112, 202, 204 , 206, 207, 401(1), 501. Specifications pertinent to all Models Datum Wing leading edge Leveling Means Upper surface of horizontal stabilizer immediately adjacent to the vertical fin. Production basis Type certificate only. Prior to original certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, materials, conformity with the approved technical data, and a check of the flight characteristics. Export eligibility Eligible for export to all countries subject to the provisions of Federal Aviation Regulations Part 21.329. 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 for 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 manufacturer under an FAA monitored or approved quality control system, and therefore, conformity must be determined if the item is not identified by Parts Manufacturer Approval or other evidence of FAA production approval. Specifications pertinent to Models 19, F19, F21, F21A, F21B, F22 and F22A Aircraft Certification basis Part 3 of the Civil Air Regulations effective November 1, 1949, and Part 3.84a, 3.85a, 3.87, 3.112, 3.120 and 3.124 of Amendment 3-4 dated January 15, 1951. In addition, FAR 23.1555(d), 23.1557(c)(1) and 23.221(c) effective August 11, 1971, in lieu of CAR 3.767(a) and 3.124(c) for Model F19, F21, F21A, F21B, F22 and F22A aircraft. FAR 36 effective January 15, 1979, for Model F19 (S/N F-154 and up), F21, F21A, F21B, F22 and F22A aircraft. Dates of applications for Model 19, not available; for Model F19, September 10, 1971; for Model F21, March 1, 1978; for Model F21A, September 1, 1981; for Model F21B, April 27, 1983; for Model F22, August 1, 1988; for Model F22A, April 17, 1990. Specifications pertinent to Models F22B and F22C Certification basis Part 3 of the Civil Air Regulations, effective November 1, 1949 and 3.84a, 3.85a, 3.87, 3.112, 3.120 and 3.124 of Amendment 3-4, dated January 15, 1951. In addition, FAR 23.1555(d) and 23.1557(c)(1) effective August 11, 1971, in lieu of CAR 3.767(a). FAR 36, Appendix G, Amendments 1 through 18. Date of application for F22B and F22C, April 17, 1990. Page 15 of 20 1A9, Rev 21 Propellers and Propeller Accessories 1. Propeller (with Continental C85-12 or C85-12F engine) - Sensenich 72CK46 or 72CK48 or any other fixed pitch wood propeller which meets the following limits: Diameter - not over 74 ins., not under 70.5 ins. Static rpm at maximum permissible throttle setting, not over 2350, not under 2350. No additional tolerance permitted. 10 lb. (-50) 2. Propeller (with Continental C85-12 or C85-12F engine) - McCauley 1A90, fixed pitch metal, with the following limitations: Diameter - not over 71 ins., not under 69.5 ins. S tatic rpm at the maximum permissible throttle setting, not over 2400, not under 2300. No additional tolerance permitted. 26 lb. (-50) 3. Propeller (with Continental C85-12 or C85-12F engine) - Sensenich M74CK-2, fixed pitch metal, with the following limitations: Static rpm at the maximum permissible throttle setting, not over 2350, not under 2250. No additional tolerance permitted. Diameter - not over 72 ins., not under 70 ins. NOTE: The applicable Airplane Flight Manual shall be revised by the Modifier and approved by the FAA to reflect this installation change. 21 lb. (-50) 4. Propeller (with Continental O-200-A engine) - McCauley 1A105/SCM 6950, fixed pitch metal, with the following limitations: Diameter - not over 69 ins. Static rpm at the maximum permissible throttle setting, not over 2550, not under 2450. No additional tolerance permitted. 20 lb. (-50) 5. Propeller (with Continental O-200-A engine) - McCauley 1B90/CM7443, fixed pitch metal with the following limitations: Diameter - not over 74 ins., not under 71 ins. Static rpm at the maximum permissible throttle setting, not over 2400, not under 2300. No additional tolerance permitted. 20.9 lb. (-50) 6. (a) Propeller (with Lycoming O-235-L2C engine) - Sensenich 72CK-0-50, fixed pitch metal, with the following limitations: Diameter - not over 72 ins., not under 70 ins. Static rpm at the maximum permissible throttle setting, not over 2500, not under 240 0. No additional tolerance permitted. (b) Spinner - Taylorcraft P/N 2800-3 backing plate and 2800-4 spinner. 24.8 lb. (-50) 7. (a) Propeller (with Lycoming O-360-A4M engine) - Sensenich 76EM8S5-0-60, fixed pitch metal, with the following limitations: Diameter - not over 76 ins., not under 74 ins. Static RPM at the maximum permissible throttle setting, not over 2400, not under 2300. No additional tolerance permitted. (b) Spinner - Taylorcraft P/N 4315 backing plate and spinner installation. 39.9 lb. 5.0 lb. (-52.5) (-50.0) Engines and Engine Accessories - Fuel and Oil systems 19 F19 F21 & F21A F22 & F21B F22A F22B F22C 101. (a) Starter, Delco Remy 1109656 (b) Starter, Prestolite MZ4214 16 lb. 15.25 lb. 0.75 lb. (-24.00) - - - - - - (-24) (-17.4) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 102. Starter, Prestolite, P/N MZ4204 17 lb. - - - - (-33.75) (-33.75) (-33.75) - - - - 1A9, Rev 22 Page 16 of 20 Engines and Engine Accessories (Cont’d) 19 F19 F21 & F21A F22 & F21B F22A F22B F22C 104. Exhaust Stacks - Taylorcraft P/N/2835-1 (left), and 2840-1 (right) 10.5 lb. - - - - (-30) (-30) (-30) - - - - 105. Fuel Strainer - Taylorcraft P/N 2581 (Latour Gascolator Kit) .50 lb. (-17.4) (-17.4) (-17.4) (-17.4) (-17.4) (-17.4) (-17.4) 106. Carburetor Air Intake Housing Continental P/N A50256 or P/N 628122 or P/N 641534 1.44 lb. (-38) (-38) (-28) (-28) (-28) - - - - 107. Oil Cooler (optional) Stewart Warner P/N 8406R 2.8 lb. - - - - (-21.5) (-21.5) (-21.5) - - - - 108. Starter, Textron Lycoming, P/N 31A21210 11.3 lb. - - - - - - - - - - (-34) (-34) 109. Carburetor Air filter - Bracket Air Filter Assembly, P/N BA6110 1.0 lb. - - - - - - - - - - (-34) (-34) 110. Exhaust Stacks - Taylorcraft P/N 2835-12 (left), and 2840- 12 (right) 10.50 lb. - - - - - - - - - - (-30) (-30) 111. Fuel Strainer - Taylorcraft P/N 4313 .50 lb. - - - - - - - - - - (-17.4) (-17.4) 112. Carburetor Air Intake Hosing Taylorcraft P/N 4310