TCDS A7NW

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A 7NW Boeing KC97G March 30, 1982 Type Certificate Data Sheet No. ANW This data sheet which is part of Type Certificate No. A7NW prescribes conditions and limitations under which the product for which the type certificate was Issued meets the airworthiness requirements of the Civil Air Regulations. Hawkins & Powers Aviation, Inc. Type Certificate Holder P. 0. Box 391 Greybull, Wyoming 82426 I - Model HP-KC-97G (Restricted Category) Approved April 17, 1981 Engines: 4 - P & W R-4360-59B Fuel: Aviation Gasoline 115/145 Grade For Alternate Fuels See T.O. 1C-976-1 Section V Engine Limita: Maximum Wet Power, Sea Level 3500 BHP @ 2700 RPM and 247 TPSI (Torque Pressure) Maximum Dry Power, Sea Level 3250 BHP @ 2700 RPM and 230 TPSI (Torque Pressure) See Airplane Flight Manual T.O. 10-97G-1 and Appendix I.O. 1C-97G-1-1 Part 2 for complete engine power and performance data. Propellers: 4 - Hamilton Standard 34G60, Blade No. R-C7021D-8 See T.O. 1C-97G-1 Section V for limitations Airspeed Limits: 'WE = 302 knots or Mach 0.62 whichever 18 less VA * 206 knots IAS Maneuvering = 155 knots IAS for 55% to 100% flaps = 190 knots IAS with flaps to 55% VLO = 200 knots IAS Landing Gear Extension Speed Maximum Cargo Doors Open and Aerial Delivery Speed V = 155 knots IAS Rev. No. Page No. 4 AZNW C.G. Range: Operating Range 18.5% to 30.5% MAC DATUM: 50 in. fud of nose (Distance from datum to nose jacking cone 228.6 in.) Leveling Means: Indicator below floor in forward lower compartment (Sta. 356) Maximum Grogs Weight - Take Off = 153,000 Itg. Landing Weight (10 FPS Sink Speed) = 130,000 1ba. (Note: Chart for Contact Sinking Speed between 130,000 and 153,000 lbs. provided in Flight Manual T.O. 1C-97G-1) (8.3 FPS Sink Speed) = 153,000 1bs. Maximum Zero Fuel Weight = 128,000 1bs. (See Flight Manual for Fuel Loading distribution and limitations) Minimum Crew: Pilot, Copilot, and Flight Engineer and the number of persons essential to perform the special purpose operation. Fuel Capacity: 7,790 gals. total - 2 outboard tanks 1,770 gal. each - 2 Inboard tanks 1,520 gal. each - 1 Center Wing tank 1,210 gal. 011 Capacity: 186 gals. total - 4 engine tanks 32.5 gal. each - 2 transfer tanks 56 gal. Cargo Capacity: See Flight Manual T.O. 1C-97G-1 Section V AYNW -3 Control Surface Movements: MOVEMENT FRON TRAILING ROGE CONTROL SURFACE POSITION EUTRAL POSITIOI * DEGREE MOYEMENT IN INCHES AILERONS UP 33 12 13 1283) bOrN AILERON TRIM TABS DOWN 5.] (3 }) 3(20) ELEYATORS UP 1243 (2-43) DOWN ELEYATOR TRIM TABS RIGHT UP 12(2 3) 135(2 431) DOWN LEFT - WING FLAPS UP, NEUTRAL POSITION OF TRIN TAB WITH ELEVATOR IN UF 1.5 (+ .57.25) 32 (1.111.05) NEUTRAL POSITION NING FLAPS DOWN UP 3 (8 112) 84 (8.11) IS DEGREES, ELEVATO IN NEUTRAL POSITION MEASURED FROM POSITION GIVEN ABOVE RUDDER (BY PEDAL WITH RUDDER PENT 309 2 1:12) 8OOST ON) BY TRIM KNOD WITH RUDDE RIGHT 133/0 12 13) 17:83 ( 112 1.69) TOOST DH LEFT RUDDER TAS RIGHT 285(8 15) LEFT WING FLAPS DOWN 45 19 2) Serial Numbers Eligible: USAF Serial Number 52-918 Certification Basia: FAR 21.25(a) (2) dated May 1974, Amendment 21-1 through 21-53 Restricted Type Certificate 1ssued Apr1l 17, 1981 Production Basis: None - Prior to original airvorthinese certification of each aircraft, an FAA representative must perform inspection for workmanship, materials and conformity with the approved technicel data, and witness a flight check. Equipment: The basic required equipment as prescribed in the applicable Airworthiness Regulations (See Certifica- tion Basis), must be installed in the aircraft for certification. In addition, an FAA approved Air- plane Flight Manual Supplement is required in addition to the operating limitations specified in Section V of T.O. 10-976-1. - 4- AZNA NOTE 1. Current weight and balance report and loading instructions for Model HP-1C-97G aircraft must agree with Section V of ₫.0. 1C-97G01 Manual. NOTE 2. A. This approval applies to USAF (Boeing) KC97G aircraft with modifications as described in data per Hawkins & Powers April 9, 1981, or later FAA approved revision thereto. Aviation, Inc. FAA approved drawing list HPA-97-DL1 dated B. Airplane certified for the special purpose of mineral explora- tion, agriculture, forest and wildlife conservation, and carriage of cargo. (1) Operation over densely populated areas is probabited. (2) In addition to the operating limitations in this data sheet, area, economic, passenger and other appropriate operating limitations in accordance with FAR 21.25 shall be shown on placards or listing accessible to the pilot. (3) Carriage of hazardous materials is prohibited unless compliance is shown with applicable regulations in Code of Federal Regulations 49, Part 175. (4) The following placard must be displayed in front of and in clear view of the pilot: "This airplane must be operated as a restricted category airplane in compliance with the operating limitations stated in the form of placards, markings, and manuals." NOTE 3. The aircraft must be serviced and maintained in accordance with USAF I.O. 1C-97 (K)E(C)-2-1. NOTE 4. USAF Serial Numbers: 52-918, 53-317, 52-2698, 53-350 - END -