W&B 2-9

Figure 2-15. Sample excerpt from TCDS A00009CH (continued). Figure 2-15. Sample excerpt from TCDS A00009CH (continued). - 3- A 0 0 0 0 9 C H Minimum Crew One (1) Pilot Number of Seats 4 (2 at 143.5 inches aft of datum, 2 at 180 inches aft of datum) Maximum Baggage 130 Lbs. at 208 inches Fuel Capacity Total: S/N 1005 thru 1877, 1879 thru 1885 60.5 gal at 153.75 inches Usable: 56 gal (See Note 1) S/N 1878, 1886 and subsequent: 58.5 gal at 154.9 inches Usable: 56 gal (See Note 1) Oil Capacity 8 quarts at 76.2 inches Maximum Operating Altitude With a portable oxygen system, the aircraft is limited to 17,500 ft MSL. Oxygen must be provided as required by the operating rules. Only portable oxygen systems listed in the FAA Approved Airplane Flight Manual, document number 11934-002, or later FAA approved revisions, are allowed. Control Surface Movements Wing Flaps: Up 0°± 0.5° Down 50% 16°± 0.5° Down 100% 32°± 0.5° Aileron: Up 12.5° ± 1.0° Down 12.5° ±1.0° Elevator: Up 25.0° +0°/-1.0° Down 15° ± 1.0° Elevator Trim: Up 17.0° Minimum Down 10.5° ± 1.0° Rudder: Right 20.0° ± 1.0° Left 20.0° ± 1.0° Additional Limitations: Airframe life limit: 12,000 flight hours Design Data: The airplane shall be manufactured in accordance with the latest FAA approved revision of “Master Drawing List”, Document No. 13750, or other FAA approved data. NOTE: Document No. 12609 is the predecessor document to Document No. 13750. Serial Nos. Eligible 1005 and on II - Model SR22, Normal Category, Approved November 30, 2000 Engine Teledyne Continental IO-550-N, Type Certificate Data Sheet E3SO Engine Limits Maximum Take-off 2700 RPM (310 hp) Maximum Continuous Power 2700 RPM (310 hp) Propeller and Propeller limits 1. Hartzell Propeller Inc. P/N PHC-J3YF-1RF/F7694 or F7694B TCDS P36EA Hartzell Maximum Diameter: 78 inches Minimum Diameter: 76 inches Number of Blades: 3 Low Pitch: 14.1°+/-0.5° High Pitch: 35.0°+/-1.0° No operating limitations to 2700 RPM Spinner: Hartzell P/N A-2295-1(P) NOTE: Spinner may be painted or polished. 2. McCauley Propeller Systems P/N D3A34C443/78CYA-0 TCDS P47GL McCauley Maximum Diameter: 78 inches Minimum Diameter: 76 inches Number of Blades: 3 - 5- A 0 0 0 0 9 C H Minimum Crew One (1) Pilot Number of Seats 4 (2 at 143.5 inches aft of datum, 2 at 180 inches aft of datum) Maximum Baggage 130 Lbs. at 208 inches Fuel Capacity Total: S/N 0002 thru 2333, 2335 thru 2419, and 2421 thru 2437 84 gallon at 154.9 inches Usable: 81 gallon (See Note 1) S/N 2334, 2420, 2438 and subsequent 94.5 gallon at 154.9 inches Usable: 92.0 gallon (See Note 1) or 58.5 gal at 154.9 inches Usable: 56 gal (See Note 1) Oil Capacity 8 quarts at 77.1 inches Maximum Operating Altitude With a portable oxygen system, the aircraft is limited to 17,500 ft MSL. Oxygen must be provided as required by the operating rules. Only portable oxygen systems listed in the FAA Approved Airplane Flight Manual, document number 13772-001, or later FAA approved revisions, are allowed. Control Surface Movements Wing Flaps: Up 0°±0.5° Down 50% 16° ± 0.5° Down 100% 32° ±0.5° Aileron: Up 12.5° ± 1.0° Down 12.5° ± 1.0° Aileron Trim: Up 6 ± 1.0° Down 6 ± 1.0° Elevator: Up 25.0° +0°/-1.0° Down 15° ± 1.0° Elevator Trim: Up 17.0° Minimum Down 10.5° ± 1.0° Rudder: Right 20.0° ± 1.0° Left 20.0° ± 1.0° Additional Limitations: Airframe life limit: 12,000 flight hours Design Data: The airplane shall be manufactured in accordance with the latest FAA approved revision of “Master Drawing List”, Document No. 13750, or other FAA approved data. Serial Nos. Eligible 0001 and on. Data Pertinent to All Models Reference Datum 100 inches in front of the forward face of firewall bulkhead Leveling Means Door sill and leveling points as defined in AFM Certification Basis Model SR20: 14 CFR Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 23-47, except as follows: 14 CFR 23.573, 23.575, 23.611, 23.657, 23.673 through Amendment 23-48; 14 CFR 23.783, 23.785, 23.867, 23.1303, 23.1307, 23.1309, 23.1311, 23.1321, 23.1323, 23.1329, 23,1361, 23.1383, 23.1401, 23.1431, 23.1435 through Amendment 23-49; 14 CFR 23.3, 23.25, 23.143, 23.145, 23.155, 23.1325, 23.1521, 23.1543, 23.1555, 23.1559, 23.1567, 23.1583, 23.1585, 23.1589 through Amendment 23-50; 14 CFR 23.777, 23.779, 23.901, 23.907, 23.955, 23.959, 23.963, 23.965, 23.973, 23.975, 23.1041, 23.1091, 23.1093, 23.1107, 23.1121, 23.1141, 23.1143, 23.1181, 23.1191, 23.1337 through Amendment 23-51; 14 CFR 23.1305 through Amendment 23-52 Noise: 14 CFR Part 36 dated December 1, 1969 as amended by 36-1 through 36-21.