TCDS 1A21

Page No. 1 2 3 4 5 Rev. No. 11 - - - 11 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A21 Revision 11 AERO COMMANDER (Volaire) 10 (Volaire) 10A (Aero Commander)100 (Aero Commander)100A (Aero Commander)100-180 August 11, 1989 TYPE CERTIFICATE DATA SHEET NO. 1A21 This data sheet which is a part of Type Certificate No. 1A21 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations/Federal Aviation Regulations. Type Certificate Holder Dynac Aerospace Corporation (See Note X) 672 S Washington St. Afton, Wyoming 83110 I. Volaire Model 10, 3 PCLM (Normal Category), 2 PCLM (Utility Category), approved November 30, 1961. Aero Commander Model 100A, 3PCLM (Normal Category), 2 PCLM (Utility Category) Volaire Model 10 designations changed to Aero Commander Model 100A on September 30, 1965. Engine Lycoming O-290-D2C (Carburetor setting #10-3561-1) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2600 r.p.m. (135 hp) Propeller and Propeller Limits Sensenich (fixed pitch) Model M74DM 31.5 lb. (-62.3) Static r.p.m. at maximum permissible throttle setting: Not over 2240, not under 2190 No additional tolerance permitted. Diameter: Not over 74 in., not under 71.5 in. Airspeed Limits (CAS) Vne (never exceed) 155.0 m.p.h. (135.0 knots) Vno (max. structural cruising) 135.0 m.p.h. (117.0 knots) Vp (maneuvering) 99.5 m.p.h. ( 86.5 knots) (normal category) 108.0 m.p.h. ( 94.0 knots) (utility category) Vfe (flaps extended) 80.0 m.p.h. ( 69.0 knots) C.G. Range Normal (14.35) to (18.90) at 1900 lbs. (11.75) to (18.90) at 1560 lbs. Utility (12.45) to (15.20) at 1650 lbs. (11.75) to (15.20) at 1560 lbs. Straight line variation between points given. Empty Wt. C.G. Range None Maximum Weight Normal 1900 lbs. Utility 1650 lbs. No. of Seats 3 - (2 at +13.4, 1 at +48.4) 1A21 2 Maximum Baggage 188 lbs. maximum with rear seat removed. Fuel Capacity 32 gal. total, 31.2 gal. usable. (Two 16 gal. tanks in wing at +23.4) Oil Capacity 2 gal. (-43.6) Control Surface Movements Aileron Up 18° Down 17° Elevator tab Up 15° Down 30° Elevator Up 25° Down 32° Rudder Left 26° Right 26° Flap Up 0° Down 40° Serial Nos. Eligible Volaire Model 10: 10-012, 10-013, and 10-014 Aero Commander Model 100A: 010, 011, 015 through 025 Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: (a) FAA Approved Airplane Flight Manual dated November 30, 1961, revised February 7, 1962. (b) Pre-stall warning device, Model 164R manufactured by Safe Flight Instrument Corporation. Datum Leading edge of wing II. Volaire Model 10A, 4 PCLM (Normal Category), approved June 1, 1965. Aero Commander Model 100, 4 PCLM (Normal Category) Volaire Model 10A designation changed to Aero Commander Model 100 on September 30, 1965. Engine Lycoming O-320-A2B or O-320-A2C (carburetor setting 10-3678-32) Fuel 80/87 minimum grade aviation gasoline Engine Limits For all operations, 2700 rpm (150 hp) Propeller and Propeller Limits Sensenich (fixed pitch metal) M74DM Sensenich Spinner No. 2 (32 lb. (-61.6) Static rpm at maximum permissible throttle setting: Not over 2385, not under 2235 Diameter: Not over 74 in., not under 72.5 in. Airspeed Limits (CAS) Vne (never exceed) 170 m.p.h. (147.5 knots) Vno (max. structural cruising) 135 m.p.h. (117.0 knots) Vp (maneuvering) 111 m.p.h. ( 96.4 knots) Vfe (flaps extended) 105 m.p.h. ( 91.1 knots) C.G. Range (14.35) to (18.9) at 2250 lbs. (11.75) to (18.9) at 1700 lbs. Straight line variation between points given. Maximum Weight 2250 lbs. No. of Seats 4 - (2 at +13.4, 2 at +48.4) 3 1A21 Maximum Baggage 120 lbs. Fuel Capacity 44 gal. total, 40 gal. usable (two 22 gal. tanks in wing at +24.0) Oil Capacity 2 gal. (-40.4) Control Surface Movements Aileron Up 19° ± 2° Down 17° ± 2° Elevator tab Up 20° ± 2° Down 20° ± 2° Elevator Up 25° ± 2° Down 20° ± 2° Rudder Left 25° ± 2° Right 25° ± 2° Flap Up 0° Down 30° ± 2° Serial Nos. Eligible Volaire Model 10A: 10A-026, 10A-027, 10A-028, 10A-029 10A-030 and 10A-033 Aero Commander Model 100: 031, 032, 034-039, 041, 042, 044-067, 069 and up Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: (a) Pre-stall warning device, Model 164R, manufactured by Safe Flight Instrument Corporation. (b) FAA Approved Airplane Flight Manual dated July 8, 1965. (c) Sensenich Spinner No. 2 installed in accordance with Volaire Drawing No. A1-11-100. Datum Leading edge of wing III. Aero Commander Model 100-180, 4 PCLM (Normal Category), approved September 26, 1967. Engine Lycoming O-360-A2F, MA-4-5 (carburetor setting 10-3878) Fuel 100 minimum grade aviation gasoline Engine Limits For all operations, 2700 r.p.m. (180 hp) Propeller and Propeller Limits McCauley 1A170/CFA 35.0 lbs. (-47.0) Static rpm at maximum permissible throttle setting: Not over 2410, not under 2310 Diameter: 76 in. Airspeed Limits (CAS) Vne (never exceed) 176 m.p.h. (154 knots) Vno (max. structural cruising) 140 m.p.h. (121 knots) Vp (maneuvering) 116 m.p.h. (100 knots) Vfe (flaps extended) 105 m.p.h. ( 91.1 knots) C.G. Range Serial Nos. 068 and 5001 through 5100 (36.15) at 2100 lbs., varying linearly to (40.55) at 2450 lbs. (46.25) at 2450 lbs., aft limit at maximum allowable weight Serial No. 5101 and above (36.15) at 2100 lbs., varying linearly to (40.95) at 2475 lbs. (46.25) at 2475 lbs., aft limit at maximum allowable weight 1A21 4 Maximum Weight Serial Nos. 068 and 5001 through 5100 2450 lbs. Serial No. 5101 and above 2475 lbs. No. of Seats 4 - (2 at +39.2, 2 at +74.2) Maximum Baggage 120 lbs. (+152.4) Fuel Capacity 44 gal. total, 40 gal. usable (two 22 gal. tanks in wing at +49.8) Oil Capacity 2 gal. (-21.0) Control Surface Movements Aileron Up 19° ± 2° Down 17° ± 2° Elevator tab Up 20° ± 2° Down 20° ± 2° Elevator Up 25° ± 2° Down 20° ± 2° Rudder Left 25° ± 2° Right 25° ± 2° Flap Up 0° Down 30° ± 2° Serial Nos. Eligible Aero Commander Model 100-180 068, 5001 and up. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: (a) Pre-stall warning device, Dialco 82-1312-0111-201. (b) FAA Approved Airplane Flight Manual dated September 25, 1967. Datum Front face of engine firewall. Specifications Pertinent to all Models Leveling Means Top of fuselage immediately aft of cabin. Certification Basis CAR 3 dated May 15, 1956, including Amendments 3-1 to 3-4 inclusive. Type Certificate No. 1A21 issued November 30, 1961. Date of application for Type Certificate January 26, 1959. Production Basis None NOTE 1. Current weight and balance report including list of equipment incl uded in the certificated empty weight and loading instructions when necessary, must be provided for each aircraft at the time of original certification. (a) For the Volaire Model 10 and Aero Commander Model 100A, the certificated empty weight and corresponding center of gravity location must include unusable fuel of 6 lb. at (+23.4) and unusable oil of 7.5 at (-43.6). (b) For the Volaire Model 10A and the Aero Commander Model 100, the certificated empty weight and corresponding center of gravity must include unusable fuel of 24 lbs. at (+24.0) and unusable oil of 6 lbs. at (-40.4). (c) For the Aero Commander Model 100-180, the certificated empty weight and corresponding center of gravity must include unusable fuel of 24 lbs. at (+50.6) and unusable oil of 6 lbs. at (-21.0). 5 1A21 NOTE 2. The following placards must be displayed: (a) Volaire Model 10 and Aero Commander Model 100A (1) On the instrument panel in full view of the pilot: "THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE IN COMPLIANCE WITH THE APPROVED AIRPLANE FLIGHT MANUAL." "NO ACROBATIC MANEUVERS (INCLUDING SPINS) ARE APPROVED FOR NORMAL CATEGORY OPERATIONS." "RETRACT FLAPS IMMEDIATELY IF SPIN IS INADVERTENTLY ENTERED." (2) On the center of the rear deck panel fairing, facing forward: "BAGGAGE CAPACITY = 50 LBS. WITH MAXIMUM LOAD AT REAR SEAT NOT EXCEEDING 138 LBS." (b) Volaire Model 10A and Aero Commander Model 100 (1) On the instrument panel in full view of the pilot: "ALL INTENTIONAL ACROBATIC MANEUVERS INCLUDING SPINS PROHIBITED. RETRACT FLAPS IMMEDIATELY IF SPIN IS INADVERTENTLY ENTERED. OPERATE IN NORMAL CATEGORY IN COMPLIANCE WITH APPROVED FLIGHT MANUAL." (2) On the center of the rear deck panel fairing, facing forward: "BAGGAGE CAPACITY 120 LBS." (c) Aero Commander Model 100-180 (1) On the instrument panel in full view of the pilot: "ALL INTENTIONAL ACROBATIC MANEUVERS INCLUDING SPINS PROHIBITED. RETRACT FLAPS IMMEDIATELY IF SPIN IS INADVERTENTLY ENTERED. OPERATE IN NORMAL CATEGORY IN COMPLIANCE WITH APPROVED FLIGHT MANUAL." (2) On inboard side of baggage door: "MAXIMUM WEIGHT IN BAGGAGE COMPARTMENT NOT TO EXCEED 120 LBS. SEE WEIGHT AND BALANCE INFORMATION FOR ALLOWABLE LOADING." NOTE 3. The Aero Commander Model 100 aircraft prior to S/N 153 are approved for day VFR operations only. This restriction removed upon approved installation of Aero Commander Kit No. SBK 1007. NOTE 4. The Volaire Model 10A and Aero Commander Model 100 may be operated with the right door removed in accordance with the FAA approved Airplane Flight Manual revised June 1967. NOTE 5. All operations are approved with or without the propeller spinner for the Model 100-180. NOTE 6. Christen Industries, Inc., P.O. Box 547, Afton, Wyoming 83110, is licensed by Dynac Aerospace Corporation to manufacture and obtain airworthiness certificates for Models 100, 100A, and 100-180 airplanes listed in this ty pe certificate data sheet. ....END....