# TCDS ATC 604: Hawker Beechcraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Hawker Beechcraft Corporation - Revision: 2 - Revised: November 12, 2010 - Product: Aircraft, Small Airplane - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/8c/b5/8cb53ed9b3155282afd39d13e1b8739a0a084c3eaf60f5269439e28123341b35 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F8E9B4B601F410C8862577DC0054F3B3.0001 - Page: https://openairdocs.org/tcds/ATC%20604 ## Models (2) As the data sheet lists them. - C17R (Army UC-43E) - SC17R ## What the data sheet says Some pages are OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text Page No. 1 2 3 4 Rev. No. 2 1 1 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION ATC 604 Revision 2 Hawker Beechcraft C17R (Army UC-43E) SC17R November 12, 2010 AIRCRAFT SPECIFICATION NO. 604 Type Certificate Holder Hawker Beechcraft Corporation 9709 East Central Wichita, Kansas 67201 Type Certificate Holder Record: Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 604 2 Rev. 1 Landplane Engine ring cowl 28 1bs. Starter (Eclipse E-80) 20 1bs. Generator amp (Eclipse G-1) 15 lbs. Battery (Exide 6TS-13-1) (Under baggage compartment) 36 1bs. 105. Control column - Swing-over or "T" type (Inspector should report type installed) 106. Oil radiator (Harrison) 8 1bs. 107. Propeller - fixed pitch metal 108. 6.50-10 or 7.50-10 wheels (Hayes) (Wheels must be approved for at least 1950 1bs. per wheel and must be placarded for 7.50-10 6-ply tires) 75 1bs. 109. 10x3 tail wheel Seaplane - Items 101 thru 106, 203 and 210 PLUS 151- Edo 39-4000 float installation with water rudder 527 1bs. Class II: 200- Miscellaneous items as noted in approved weight and balance report. 201. Miscellaneous extra instruments 202- Propeller - Hamilton Standard adj. metal 203. Propeller - Hamilton Standard hub 2D30 with: Blades 6095A-12 to 6095A-17, inclusive, or blades 6101A-18 to 6101A-23, inclusive, or blades 6167A-12 to 6167A-17, inclusive. Diameter 102 in. maximum, 96 in. minimum. 204_ Special landing gear complying with Canadian requiremen: - for ski installation 205. Landing lights Under lower wing (Grimes) 3.5 1bs. each (+18) (D) In wheel well (Hall) 3.5 1bs. each (+37) (c) S & M Use actual weight 206. Flares (Drawing I-17004) 207- Radio, variable (location and actual weight of installation includes controls, if already installed etc., or name of manu- facturer and included in certificated weight empty should be noted on inspector's report.) (Drawing I-17002 shows approved locations.) 208. Shielding (a) Breeze 15 1bs. (b) Packard 10 1hs. 209. Extra door on right side 6 1bs.* 210- Extra 23 or 25 gallon fuel tanks in wings, upper (+45.5) and lower (+24) 20 1bs. each (Any combination of fuel tanks include removal of the fuselage tanks may be used subject to inspector's approval and provided weight and balance accounts for actual installation.) Rev. 1 3 604 Oil tanks (a) 7 gallons (-13) 9 gallons (-13) Generator - 25 amp (Eclipse) 10.3 gallons 20 1h5. (-13) Golf bag compartment (Drawing I-17006). In bay aft of, and opens into, baggage compartment. Maximum capacity 70 1bs. golf bag and clubs only. Parachutes or parachute type chairs. Seaplane corrosion protection 20 1bs. Pressure fire extinguisher (Drawing I-17001) (Container at +14) Metal tank cover (Drawing I-17003) Camera well (Draving I-17006) Ballast installation Maximum 25 1bs. (+210) Special tool compartment in tail, including tools 25 1bs. (+218) 221. Camera installation (Drawings B17E015, B17E016, and B17E902) : Camera and viewfinder 110 1bs. (+51) ; operator's stool 4 1bs. (+65) ; 25 gallon fuel tank in baggage compartment 15 lbs. (+86). Remove: plates for camera and viewfinder (+51) and rear fuselage fuel tank (+55) 222- Skis (a) Pollack P-4600 B. Seaplane: Items 205 thru 221 Class III: 301- 24 in. streamline wheels (Hayes) with 6-ply tires 75 lbs. (Wheels must be placarded for 6-ply tires) 302. Puncture proof tubes (a) 7.50-10 9 lbs.* (b) 24 in. streamline 5 1bs.* 303. Tail wheel steering device No change in weight 304- Electric motor and installation for auxiliary to manually operated retracting gear (25 amp fuse required) 8 lbs.* NOTE 1. The following placards were required on serial No. 74 when originallY certificated- muSE MAIN FUSELAGE TANKS FOR TAKE-OFF AND At the fuel valve: USE FUEL OUT OF AUXILIARY LOWER WING TANKS BEFORE EMPTYING MAIN TANKS. (c) 1o Bagage Placarded to 75 1os. At rear fuselage fuel tank: "AS 4-PLACE 47 GAIS., AS 5-PLACE Similar instructions must be placed in subsequent airplanes when the actual weight and balance report is based on any but the most adverse (from balance standpoint) use of the fuel. Inspector's report and weight and balance report should specify restrictions applicable. 604 4 Rev. 1 Eligible for export as follows, subject to inspection for equipment specified in Chapter III of Inspection Handbook: - Landplane - Seaplane - maximum standard weight 4000 1bs. - Skiplane - not eligible. However, structure complies with Canadian requirements for ski installation when approved special landing gear (Item 204) is installed. All other countries except Australi NOTE 3. Five place type must be placarded for 75 lbs. when 3 passengers occupy rear seat unless more is substantiated in weight and balance report. Baggage includes anchor and rope 25 lbs. when carried. II - MODEL C17R (UC-43E), 5 PCLB: Wright R-975E-3 or R-975E-2 With fixed metal or adj. metal propeller Maximum, except take-off 33.0 in.Hg., 1800 or 31.5 in.Hg.. 1900 rpm or 29.5 in. Hg., 2000 rpm or 28.5 in.Hg.. 2100 Ipm Take-off (one minute) -- in. Hg., 1900 rpm or 35.0 in.Hg., 2200 rpm B. With controllable metal propeller except take-off ft.) 28.5 in.Hg.. 2200 rpm (330 hp) (4000 ft. and up) 27.0 in.Ag.. 2200 rpm (330 hp) (one minute) 35.0 in. Hg.. 2200 Ipm (420 hp) Placard speeds Level flight or climb - 206 mph True Ind. Glide or dive - 225 mph true Ind. Flaps extended - 100 mph True Ind. standard weight C.G. limits (+16.6) and (+29.0) III - MODEL SC17R, 5 PCSB: Engine Wright R-975E-3 or R-975E-2 Placard limits Maximum, except take-off 34.5 in.Hg., 2200 rpm (420 hp) Take-off (one minute) 35.0 in.Hg., 2200 rpm (420 hp) Propeller Controllable metal only (Item Placard speeds Level flight or climb - 178 mph True Ind. Glide or dive - 216 mph True Ind. Flaps extended - 100 mph True Ind. Standard weight 4105 1bs. C.G. limits (+17.5) and (+25.9) ** END ** ``` ## ADs (2, in force first) - [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 ## Registered aircraft by registry model (OpenAirDocs) - [Beech C17R](https://openairdocs.org/model/beech-c17r): 1 aircraft (registry code 1150524) - [Beech SC17R](https://openairdocs.org/model/beech-sc17r): 0 aircraft (registry code 1150528) ## STCs approved under this data sheet (15) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc. - [STC SA1512WE](https://openairdocs.org/stc/SA1512WE): Installation of exhaust gas temperature monitoring systems Model EGT-1.. K S Avionics Inc - [STC SA2557NM](https://openairdocs.org/stc/SA2557NM): Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.. K S Avionics Inc - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA2-952](https://openairdocs.org/stc/SA2-952): Installation of fiberglass covering.. Razorback Fabrics Inc - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA1455NM](https://openairdocs.org/stc/SA1455NM): Installation of a flame proof auxiliary heater-dryer, Model12-1600.. Thermal, Inc - [STC SA1461NM](https://openairdocs.org/stc/SA1461NM): Installation of fuselage structure assembly. Anything Antiques - [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc - [STC SA555NW](https://openairdocs.org/stc/SA555NW): Installation of front and rear landing gear truss assemblies.. Anything Antiques - [STC SA131GL](https://openairdocs.org/stc/SA131GL): Installation of Eastern Aircraft Corp. fuel quantity indicating system.. Eastern Aircraft Corporation --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.