TCDS ATC 560

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION ATC 560 Revision 1 Hawker Beechcraft B17L, SB17L, B17B September 1, 2010 AIRCRAFT SPECIFICATION NO.560 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 B17L, SB17L, B17B I.C.. NUMBFR: ATC 560 I - SPECIFICATIONS PERTINENT TO ALL MODELS: Placard speeds Landplane Level flight or climb - 170 mph Ind. Glide or dive - 225 mph Ind. Flaps extended - 115 mph Ind. Seaplane Level flight or climb - 150 mph Ind. Glide or dive - 223 mph Ina. Flaps extended - 100 mph Ind. Fuel 50 gallons (two tanks in upper wings at 25 gallons each) (+45.5) oil 5 gallons (-13) No. passengers 4 maximum (front +19, rear +60.5) (See NOTE 3) Standard weight Landplane 3165 1bs.; Seaplane 3525 1bs. Baggage 125 1bs. (See NOTE C.G. limits Landplane (for serial Nos. 3 thru 25) (*16.6) and (+30.3) (for serial nos. 26 and up) (+16.6) and (+29.4) Seaplane (+19.4) and (+29.7) Spec. basis Approved Type Certificate No. 560 Serial Nos. Landplane 3 and up manufactured prior to 9-30-39 eligible Seaplane 40, 43 and up manufactured prior to 9/30/39 eligible Approval of both expired as of 9/30/39. EQUIPMENT: (Datum is leading edge of lower wing) (* Means net increase) Page No. 1 2 3 4 Rev. No. 1 560 Rev 1 Class I: Landplane (B17L and B17B) 101. Engine ring cowl 30 1bs. 102- Battery (under floor in front of rear seat) 17 1bs. 103. Starter (Electric or Heywood) 25 1bs. 104- Generator 10 1bs. 105. Heater 3 lbs. 106. 24 in. streamline wheels (with 4 or 6 ly tires) 107- 10x3 tail Whee. 10 1bs. 108. Propeller (a) Pixed pitch wood (b) Fixed pitch metal Seaplane (SB17L) : Items 101, 103, 104, 106. 108 (a) PLUS 151. Edo 38-3430 float installation 452 1bs. 152. Battery funder floor in front of rear 36 1bs. Class II: 200- Miscellaneous items as noted in approved weight and balance report. 201. Golf bag compartment (Drawing I-17006) (In bay of, and opens into, baggage compartment) (Maximum capacity 70 lbs. golf bag and clubs only.) 202- Ballest installation maximum 25 1bs. (+210) 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) Rear seat 31 1bs. (+62) ; cover plates for camera and viewfinder (*51) and rear fuselage fuel tank (+55) Class III: 301. Radio, variable (location and actual weight of installation including controls, etc., or name of manufac- turer and model if already installed and included in empty weight should be noted on Inspector's report.) (Drawing I-17002 shows approved locations.) Manufacturer has substantiated 30 1bs. installed between limits of instrument board and baggage compartment so far as balance is concerned. Any additional must be substantiated Rev 1 3 560 by weight and balance. 302- Landing lights Under lower wing (Grimes) 3.5 1bs. each (+ 18) In wheel well (Hall) 3.5 1bs. each (+37) 303. Under floor in front of rear seat 25 lbs. or 36 lbs. In first bay aft of baggage compartment 36 1bs. 304. 6 1bs- 305- Flares - three 1-1/2 min. 18 1bs. (+79) 306- 307- Miscellaneous extra instruments 308. 6.50-10 or 7.50-10 wheels with 7.50-10 (4 or 6 ply tires) 309 - Propeller - fixed metal (Curtiss 55501) (large size elevator must be installed and so noted on inspector's report. Distance from hinge centerline to elevator trailing edge increased from 18 in. to 20 in.) 310- (Lycoming Smith P-220 hub and Pittsburg" 127 1bs- Propeller - controllable metal B300SO blades) (Large size elevator must be installed and so noted on inspector's report. Item 303 (b) must be installed also unless C.G. check is made.) 311. one or two extra 20, 23 or 25 gallon fuel tanks in lower one 20 gallon tank in fuselage (+50) 20 1bs. each The 25 gallon tanks in upper wings may be replaced with 20 or 23 gallon tanks with no change in weight. 312- 6, 7, 5 or 8.5 gallon oil capacity 313- Electric motor and installation for auxiliary to manually operated retracting gear 8 1bs. 314- Tail wheel steering device No change in weight 315. Parachute seats 316- "T" type or "throw-over" type controls 317. Pressure fire ext. (Drawing I-17001) (Container at *14) 318- Metal tank cover (Drawing I-17003) 319- Camera well (Drawing I-17005) NOTE. 1- Serial Nos. B17L-3 to B171-21, inclusive, may have aluminum firewalls at first fuselage bulkhead and must have original insulating material forward of this point removed. This material may be replaced by asbestos. Serial Nos. B-171-22 and up must have firewalls at first fuselage bulkhead conforming to Aero. Bulletin 7-A 10-1-34), and may have asbestos insulating material forward of this point. Eligible for export as follows. subject to inspection for equipment specified in Chapter XII of Inspection Handbook: (August 27, 1937) Canada - Landplane Skiplane - not eligible Seaplane - maximum standard weight 3430 1bs. (b) Australia - Landplane only (c) All other countries NOTE 3. Five place type must be placarded for 15 1bs. baggage when 3 passengers occupy rear seat unless more is substantiated by C.G. check. 560 4 Rev 1 II - MODEL B171, 5 PCLB: Engine Jacobs I-4 Placard limits Maximum, except take-off - in. Hg.. 2000 Ipm (225 hp) Take-off (one minute) - in. Hg.. 2000 Ipm (225 hp) III - MODEL SB171, 5 PCSB: Engine Jacobs L-4 Placard limits Maximum, except take-off - in. Hg., 2000 cpm (225 hp) Take-off (one minute) - in. Hg., 2000 rpm (225 hp) IV - MODEL B17B, 5 PCIB: Engine Jacobs I-5 Placard limits Maximum, except take-off 22.5 in. Hg., 1950 rpm (225 hp) Take-off (one minute) - in. Hg.. 2000 Ipm (285 hp) ** END **