# TCDS ATC 602: Hawker Beechcraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Hawker Beechcraft Corporation - Revision: 1 - Revised: September 1, 2010 - Product: Aircraft, Small Airplane - Registered aircraft: 10, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/e9/6b/e96b1f12d1c48bfe881f8abef84c92e980e91f8a359a8220ad197322b8dc6d0b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8E7EB2CB9F80370C862577BC006B3313.0001 - Page: https://openairdocs.org/tcds/ATC%20602 ## Models (4) As the data sheet lists them. - SC17L - C17L (Army UC-43J) - C17B (Army UC-43G) - SC17B ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION ATC 602 Revision 1 Hawker Beechcraft C17L, C17B SC17L, SC17B September 1, 2010 AIRCRAFT SPECIFICATION NO. 602 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 MODELS: Beechcraft C17L (Army UC-43J), SC17L, C17B (Army UC-43G), SC17B T.C. NUMBER: ATC 602 I - SPECIFICATIONS PERTINENT TO ALL MODELS LISTED BELOW: Placard speeds Landplane - Level flight or climb - 183 mph True Ind. Glide or dive - 225 mph True Ind. Flaps extended - 100 mph True Ind. Seaplane - Level flight or climb - 150 mph True Ind. Glide or dive - 223 mph True Ind. Flaps extended - 100 mph True Ind. Amphibian - Level flight or climb - 160 mph True Ind. Glide or dive - 223 mph True Ind. Flaps extended - 100 mph True Ind. Fuel 74 gallons (Three tanks: one 23 gallon tank in each upper wing (+46.5) and one 28 gallon tank in fuselage (+31.5) Oil 5 gallons (-19) No. passengers 4 (front +19, rear +60.5) (See NOTE 4) Baggage 126 lbs. maximum (+79.5) (See NOTE 4) Standard weight Landplane 3165 1bs. Seaplane 3525 1bs. Amphibian 3525 1bs. C.G. limits Landplane (+16.6) and (+29.4) Seaplane (+19.4) and (+29.7) Amphibian (+20.0) and (+27.0) spec. basis 6PProded Tram Certificate No. 602 Serial Nos. and up manufactured prior to 9/30/39 and all AAF Nos. eligible. Approval expired 9/30/39. EQUIPMENT: (Datum is leading edge of lower wing) (* Means net increase) (See NOTE 1) Page No. 1 2 3 4 Rev. No. 1 602 2 Rev. 1 Class I: Landplane 101. Engine ring cowl 30 lbs. Starter (electric) 20 1bs. 103- Generator (a) 10 amp (Bosch) for Jacobs I-4 10 1bs. (b) 15 amp (Eclipse) for Jacobs L-5 15 1bs. 104- Battery (Exide 6TS-13-1) (under floor in front of rear seat) 36 1bs. 105. Control column (a) Swing-over or (b) "T" type (Inspector shoudl report type installed.) 106- Cil radiator (Harrison) 9 1bs. 107. Propeller - fixed pitch metal (Curtiss 55501) 56 1bs. 108. 6.50-10 or 7.50-10 wheels (Hayes) with 7.50-10 tires 109. 10x3 tail wheel Seaplane: Items 101 thru 107 PLUS 150- Edo 38-3430 floats with 10 1bs. water rudder installation 490 1bs. iżs. Amphibian: Items 101 thru 107 PLUS Edo 49-3875 amphibian floats (ATC 73) with 7.50-10 wheels (Hayes 750A) and 7.50-10 6-ply tires 624 1bs. 176. Auxiliary fin 6 1bs. Rev. 1 3 602 Class II: 201. Propeller - wood (fixed pitch) (C17L and SC171 only) 203- Propeller - Lycoming P-220 hub and Pittsburgh B300SO blades (Models C171 and SC171 only) 127 1bs. 204- Special landing gear complying with Canadian requirements for ski installation 205. Landing lights (a) Under lower wing (Grimes) 3.5 1bs. each (+18) (b) In wheel well (Hall) 3.5 lbs. each (+37) (C) S & M Use actual weight 206- Flares (Drawing No. I-17004) 208- Shielding (a) Breeze 15 1bs. (b) Packard 10 Ibs. 209. Extra door on right side 6 1bs.* 210. Extra fuel tanks (any combination of tanks including removal of the fuselage tanks may be used subject to inspector's approval and provided weight and balance report accounts for actual installation) (a) 23 or 25 gallon tanks in wings, upper (+46_5) and lower (+24) 20 1bs. each (b) Fuselage, rear 42 gallons (+57.2) 211. Oil tanks (a) 6 gallons (-19) (b) 7.5 gallons (-19) (c) 8.5 gallons (-19) 212- Generator - 25 amp (Eclipse) 20 1bs. 213. Golf bag compartment (Drawing I-17006). in bay att of, and opens into, baggage compartment. Maximum capacity 70 1bs • golt bag and clubs only. 214. parachutes or parachute type chairs 215. Seaplane corrosion protection 20 1bs. 216. Pressure fire extinguisher (Drawing I-17001) (Container at +14) 217. Metal tank cover (Drawing I-17003) 218- Camera well (Drawing I-17005) 219. Ballast installation Maximum 25 1bs. (+210) 220- Special tool compartment in tail, including tools 25 1bs. (+218) 221. Battery (a) Under floor in front of rear seat 25 lbs. (b) In 1st bay aft of baggage compartment 36 1bs. 222. Engines (Use actual weight) (a) Jacobs I-4M, I-4MA or I-4MB (for models C17L and SC17L). Limits same as for I-4. (b) Jacobs I-5M or L-5MB (for models C17B and SC17B) . Limits same as for I-5. 224- Starter (Heywood) 25 1bs. 225- 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 1bs. (+86) - Remove: Rear seat 31 1bs. (+62) and cover plates for camera and viewfinder 3 1bs. (+51). 226- Propeller - Hamilton Standard 2B20 with 6135A-12 or -13 blades. Di amet er 81 1/8" - 7" 9-7/8". (Model C17B only) 602 4 Rev. 1 Class III: 24 in. streamline wheels (Hayes) with 6-ply tires (Wheels must be placarded these tires.) 75 1bs. 102- Puncture proof tubes 7.50-10 8 1bs.* 24 in. streamline 5 lbs.* 303. Tail wheel steering device No change in weight Electric motor and installation for auxiliary to manually operated retracting gear (25 amp fuse required) 8 1bs.* NOTE 1. Weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be submitted for each aircraft with original inspector's report and each subsequent report covering changes in Class I or Il equipment. NOTE 2. Eligible for export as follows, subject to inspection for equipment specified in Chapter III of Inspection Handbook: (9/30/39) - Landplane - Seaplane - maximum standard weight 3430 1bs. - Amphibian - not eligible Skiplane - not eligible. However, structure complies with Canadian requirements for ski installation when approved special landing gear (Item 204) is installed. (D) Australia - Landplane only (c) All other countries NOTE 3. On Model SC17B (Amphibian type only) rudder travel must be limited 19 degrees right and 22 degrees left of fin centerline. NOTE 4. Five place type must be placarded for 60 lbs. baggage when 3 passengers occupy rear seat unless more is substantiated in weight and balance report. Baggage includes anchor and rope 25 1bs. when carried. II - MODEL C171 (UC-43J), 5 PCLB: Engine Jacobs L-4 Placard limits Maximum, except take-off -- in. Hg., 2000 pm (225 hp) Take-off (one minute) -- in. Hg.. 2000 rpm (225 hp) III - MODEL SC17L, 5 PCSB: Engine Jacobs I-4 Placard limits Maximum, except take-off -- in. Ho.. 2000 pm (225 bp) Take-off (One minute) -- in.Hq., 2000 rpm (225 hp) IV - MODEL C17B (UC-43G), 5 PCLB: Engine Jacobs I-5 Placard limits Maximum, except take-off -- in. Hg., 2000 pm (285 hp) Take-off (one minute) -- in. Hg.. 2000 Ipm (285 hp) V - MODEL SC17B, 5 PCSB or 5 PCAmB (See NOTE 3) ; Engine Jacobs I-5 Placard limits Maximum, except take-off -- in.Hg.. 2000 pm (285 hp) Take-off (one minute) -- in-Hg-. 2000 Ipm (285 hp) ** 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 C17B](https://openairdocs.org/model/beech-c17b): 5 aircraft (registry code 1150512) - [Beech C17L](https://openairdocs.org/model/beech-c17l): 5 aircraft (registry code 1150518) - [Beech SC17B](https://openairdocs.org/model/beech-sc17b): 0 aircraft (registry code 1150516) - [Beech SC17L](https://openairdocs.org/model/beech-sc17l): 0 aircraft (registry code 1150522) ## STCs approved under this data sheet (21) - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA2691SO](https://openairdocs.org/stc/SA2691SO): Installation of Cleveland hydraulic brake conversion kit no. 199-167. Rare Aircraft Ltd - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [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 SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): 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 SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International - [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 - [STC SA4-319](https://openairdocs.org/stc/SA4-319): Eonite covering of complete airplane.. Lott William C - [STC SA4-449](https://openairdocs.org/stc/SA4-449): Laminate 514 applied to elevator and horizontal stabilizer.. Lott William C --- 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.