TCDS TC 661

MODELS: Rearwin 6000M, 2 PCLM I.C. NUMBER: 661 Engine Placard limits except take-off Hg.. 2175 pm (125 hp) Take-off (one minute) -- in. Hg-. 2175 pm (125 bp) Propeller Maximum permissible Placard speeds Level flight or climb - 141 mph True Ind. Glide or dive - 170 mph True Ind. Fuel capacity (two 17 gallon tanks in wing) (+19) Oil capacity NO. passengers 1 (rear seat +43) (crew at Baggage Standard weight C.G. limits (+10.5) and (+17.2) Spec. basis Type Certificate No. 661 (Aero. Bulletin 7A Serial Nos. 303 and up eligible (See NOTE A and NOTE 1) EQUIPMENT: (Datum is wing leading edge) (See NOTE 5) (* Means net increase) Class I: 18x8-3 wheels (Goodyear 3LMBM) with brakes and h.D. tires (wheels must be placarded for these tires) 102- 8 in. streamline tail wheel (Goodyear 80-A) (*189) 103. Propeller - wood (fixed pitch) 23 1bs. (-601 Miscellaneous items as noted in approved weight and balance report. 10 1bs. (+12) Instrument lights 1b. (-4) Starter (Eclipse Type 80) 22 1bs. (-17) Battery and box (Exide 3-TS-13-1 23 1bs. 1-32 Battery and box (Exide 6-AC-17-1) 22 1bs. 1-32 6.00-6 wheels placarded for these tires) 14 1bs.* (-5) Extra instruments 5 1bs. (-4) Wheel pants (Hill) 12 lbs. (-6) (-17) Fixed metal propeller (Curtiss Reed) (-60) (-38) 211. Steerable tail wheel mechanism 1 1b.* (+172) 212. Skiplane landing gear (Drawing 64-004) 2-3/4 gallon oil tank (Serial Nos. 303 and 304 only) Neglect weight change Each aircraft manufactured after 1/7/43, must, prior to original certification, satisfactorily pass: An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All woodwork A final inspection of the completed aircraft. Check of flight characteristics. NOTE 1. Airplane Serial No. 304 is limited to 1668 lbs. standard weight. 6000m landing gear is installed, standard weight may be increased to 1700 lbs. NOTE 2. Rudder travel must be limited to 17 degrees in either direction from neutral position. Elevator travel must be limited to not more than 19 degrees in the up position with the stabilizer parallel to the thrust line. NOTE 3. Placard airplane to be flown solo from front seat only. NOTE 4. Eligible for export to all countries except Great Britain, Canada, Australia and New Zealand. NOTE 5. Actual weight and balance report investigating the most forward C.G. condition with 170 1b. pilot and the most rearward C.G. condition with 120 1b. pilot and 220 1b. passenger must be submitted (through Mid-West Branch Office) with inspector's original report and all subsequent reports covering changes in equipment.