TCDS A22EU

Page No. 1 2 3 4 5 6 Rev No. 5 2 2 2 5 2 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A22EU Revision 5 De Havilland Support Limited Beagle B.121 Series 1, 2, 3 March 1, 2012 TYPE CERTIFICATE DATA SHEET No. A22EU This data sheet, which is a part of Type Certificate No. A22EU 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 De Havilland Support Limited Building 213 Duxford Airfield C a m b r i d g e s h i r e CB2 4QR Type Certificate Holder Record British Aerospace, Aircraft Group Scottish Division transferred TC A22EU to De Havilland Support Limited in October 2002 Type Certificate Ownership Record (1) This TC was considered not valid by the state of design on June 19, 2007, and has been replaced by European Aviation Safety Agency (EASA) Specific Airworthiness Specification (SAS) number EASA.SAS.A.082, issued June 19, 2007. Only standard airworthiness certificates issued prior to March 1, 2012 are valid. (2) Future unsafe conditions existing in the aircraft may result in the revocation of the airworthiness certificates of the aircraft if there is no entity to comply with 14 CFR § 21.99(a), “Required design changes.” (3) Replacement parts may not be available in the future. I - Model B.121 Series 1 2PCLM (Normal and Utility Category), Approved January 11, 1969. Engine Rolls-Royce/Continental O-200-A Fuel 80/87 minimum grade aviation gasoline Engine limits For all opera tions 2750 r.p.m. (100 h.p.) Propeller McCauley IA105/SCM7053 Diameter range 70" max. - 68.5" min. Static r.p.m. at maximum pe rmissible throttle setting (Cross wind): Not over 2400, not under 2300 No additional tolerance permitted. Airspeed Limits (IAS) Knots M.P.H. Vne (Never exceed) 150 173 Vno (Max. structural cruising) 120 138 Va (Maneuvering) 110 127 Vfe (Flaps extended 0° to 40° 100 115 A22EU Page 2 of 6 C.G. range Normal Category (+66.1) to (+71.2) at 1470 lb. or less (+67.5) to (+71.2) at 1600 lb. Utility Category (+66.1) to (+69.1) at 1470 lb. or less (+67.5) to (+69.1) at 1600 lb. Straight line variation between points given Empty weight C.G. range None Maximum weight 1600 lb. Number of seats 2 (+78) Maximum baggage 85 lb. (+100) Fuel capacity 29 U.S. gallons usable (+65. 1) (See Note 1 for data on unusable fuel). Oil capacity 1.0 U.S. gallons usable (+ 15) (See Note 1 for data on system oil). Control surface movements Wing flaps Up 0° Down 39.5° Aileron Up 28° Down 12° Elevator Up 30° Down 20° Elevator trim tab Up 13° Down 32° Rudder Left 25° Right 25° Equipment The basic required equipment as pr escribed in the applicable airworthiness regulations (see CERTIFICATION BASIS) must be installed in the aircraft for certification. Beagle Report TECH/B121/62 contains a list of all required equipment as well as optional equi pment installations approved by the A.R.B. In addition, the following item of equipment is required: a) Stall Warning Indicator (Safeflight 164) b) ARB Approved Flight Manual Do c. No.B.S.3/5 dated 6th September 1968. II - Model B.121 Series 2 4PCLM (Normal Category), 2PCLM (Utility Category), Approved January 11, 1969. (Same as Model B.121 Series 1, except for power plant installation). Engine Lycoming O-320-A2B Fuel 80-87 minimum grade aviation gasoline Engine limits For all opera tions 2700 r.p.m. (150 h.p.) Propeller Sensenich M74DMS-0-60 Diameter range 74" max. - 72" min. Static r.p.m. at maximum pe rmissible throttle setting (cross wind): Not over 2400, not under 2200 No additional tolerance permitted. Airspeed limits (IAS) Knots M.P.H. Vne (Never exceed) 150 173 Vno (Max. Structural cruising) 120 138 Va (Maneuvering) 110 127 Vfe (Flaps extended 0° to 40°) 100 115 A22EU Page 3 of 6 C.G. range Normal Category (+62.8) to (+71.6) at 1250 lb. or less (+63.5) to (+71.6) at 1600 lb. (+65.8) to (+71.6) at 1800 lb. (+67.6) to (+71.2) at 1925 lb. Utility Category (+62.8) to (+69.1) at 1250 lb. or less (+63.5) to (+69.1) at 1600 lb. (+65.2) to (+69.1) at 1750 lb. Straight line variation between points given Empty weight C.G. range None Maximum weight 1925 lb. Normal Category 1750 lb. Utility Category Number of seats 2 (+78) (See Note 4) Maximum baggage 120 lb. (+124) Fuel capacity 29 U.S. gallons usable (+65.1). Optional extra tankage 14 U.S. gallons usable (+65.1) (See Note 1 for data on unusable fuel). Oil capacity 1.5 U.S. gallons usable (+ 12) (See Note 1 for data on system oil). Control surface movements Wing flaps Up 0° Down 39.5° Aileron Up 28° Down 12° Elevator Up 30° Down 20° Elevator trim tab Up 13° Down 32° Rudder Left 25° Right 25° Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Cer tification Basis) must be installed in the aircraft for certification. Beagle Report TECH/B121/76 contains a list of all required equipmen t as well as optional equipment installations approved by the A.R.B. In addition, the following item of equipment is required: a) Stall Warning Indicator (Safe Flight 164) b) A.R.B. Approved Flight Manual Doc. No.B.S.3/6 dated 6th September 1968. III - Model B.121 Series 3 2PCLM (Normal) and Utility Category, Approved 19 January 1970. (Same as Model B.121 Series 1, except for power plant installation). Engine Lycoming O-320-D2C. Fuel 91/96 minimum grade aviation gasoline Engine limits For all opera tions 2700 r.p.m. (160 h.p.) Propeller 1. Sensenich M74DMS-0-62 Diameter range 74" max. - 72" min. Static r.p.m. at maximum pe rmissible throttle setting (cross wind): Not over 2400, not under 2200 No additional tolerance permitted. 2. Sensenich 74DM655-0-62 Diameter range 74" max. - 72" min. Static r.p.m. at maximum pe rmissible throttle setting (cross wind): A22EU Page 4 of 6 Not over 2400, not under 2200 No additional tolerance permitted. Airspeed limits (IAS) Knots M.P.H. Vne (Never exceed) 150 173 Vno (Max. Structural cruising) 120 138 Va (Maneuvering) 110 127 Vfe (Flaps extended 0° to 40°) 100 115 C.G. range Normal Category (+62.8) to (+71.6) at 1250 lb. or less (+63.5) to (+71.6) at 1600 lb. (+66.2) to (+71.6) at 1825 lb. (+67.6) to (+71.2) at 1950 lb. Utility Category (+62.8) to (+69.1) at 1250 lb. or less (+63.5) to (+69.1) at 1600 lb. (+65.2) to (+69.1) at 1750 lb. Straight line variation between points given Empty weight C.G. range None Maximum weight 1950 lb. Normal Category 1750 lb. Utility Category Number of seats 2 (+78) (See Note 4) Maximum baggage 120 lb. (+124) Fuel capacity 42 U.S. gallons usable (+65.1) (See Note 1 for data on unusable fuel). Oil capacity 1.5 U.S. gallons usable (+15) (See Note 1 for data on system oil). Control surface movements Wing flaps Up 0° Down 39.5° Aileron Up 28° Down 12° Elevator Up 27° Down 25° Elevator trim tab Up 13° Down 35° Rudder Left 25° Right 25° Equipment The basic required equipment as pr escribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for type certification. Beagle Report TECH/B121/89 contains a list of all required equipment as well as optional equi pment installations approved by the A.R.B. In addition, the following item of equipment is required: a) Stall Warning Indicator (Safe Flight 164) b) A.R.B. Approved Flight Manual Doc. No.B.S.3/8 dated 16 October, 1969. A22EU Page 5 of 6 SPECIFICATIONS PERTINENT TO ALL MODELS Datum Fuselage station zero which is situ ated 73.0 ins. forward of the weighing reference station which is marked on a plate on the fuselage. Leveling means Holes for datum pins on which straight edge is placed are located at Stns. 104 and 128.5 on left side of fuselage for longitudinal levelling and on each side of door frame at Stn. 100 for lateral levelling. Serial Nos. eligible Only those ai rcraft serials holding a standard airworthiness certificate issued prior to March 1, 2012 are eligible. The United Kingdom Certificate of Airworthiness for Export endorsed as noted under "Import Requirements" must be submitted for each individual aircraft for which a pplication for certification is made. Import Requirements None elig ible after March 1, 2012. Previous to this date: A United States Airworthiness Certificate may be issued on the basis of a U.K. Certificate of Airworthiness for Export signed by a representative of the Board of Trade containing the following statement: "The aircraft covered by this Certificate has been examined and found to comply with U.S. Federal Aviation Regulation FAR 23 effective February 1, 1965, including amendm ents 23-1 through 23-6 and conforms to Type Certificate A22EU". Certification basis FAR 21.29, FAR 23, effective February 1, 1965, including amendments 23-1 through 23-6. Type Certificate No. A22EU issued January 11, 1969. Date of application for type certificate, January 12, 1966. NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding cen tre of gravity location must include unusable fuel of 7 lb. (+65.1), (Series 1, 2 and 3) and system oil of 4 lb. (+15 Series 1) (+12 Series 2 and 3). NOTE 2. The following placards must be displayed in full view of the pilot: THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE IN COMPLIANCE WITH THE APPR OVED AIRPLANE FLIGHT MANUAL. ALL MARKINGS AND PLACARDS ON THIS AIRPLANE APPLY TO ITS OPERATIONS AS A UTILITY CATEGORY AIRPLANE. FOR NORMAL CATEGOR Y OPERATIONS REFER TO THE AIRPLANE FLIGHT MANUAL. NO ACROBATIC MANOEUVR ES, INCLUDING SPINS, ARE APPROVED FOR NORMAL CATEGORY OPERATIONS. FOOTNOTE : All placards required in the approved airplane Fli ght Manual must be installed in the appropriate locations. NOTE 3. Each individual airplane will be supplied with a placard that specifies the kind of operation, such as V.F.R., I.F.R., day or night, to which the ope ration of the airplane is limited by the equipment installed. NOTE 4. One or two additional rear seats (+110) may be installed in B.121 Series 2 and 3 airplanes to A.R.B. approved Beagle modificati ons Nos. BE.23 or BE.22 respectively. A22EU Page 6 of 6 ---END---