TCDS TC 2-584

JAMIESON CORPORATION MODELS: Jamieson J-1 (Remodeled Culver Army PQ-SA, Navy IDC-2), 2 PCIM T.C. NUMBER: 2-584 (Approved 5/23/46) (Remodeled by C.M. Jamieson, 1039 South Topeka Avenue, Wichita 11, KS) Engine Lycoming 0-290-B Fuel 73 minimum octane aviation gasoline Engine limits For all operations 2600 rpm (125 hp) Propeller limit Static rpm at maximum throttle setting: Not more than 1790 rpm; not less than 17?0 Ipm Diameter: Not more than 72 in./ not less than 70 in. Airspeed limits Level flight or climb - 130 mph True Ind. Glide of dive - 175 mph True INd. C.G. range (+10.6) to (+15.1) Datum Leading edge of wing at fuselage (18 in. forward of wing attachment fitting) Leveling means Plumb bob line from upper rear engine mount attaching bolt to reference mark 5-11/16 in. aft of lower rear engine mount attaching bolt. Maximum weight 1535 1bs. No. seats 2o'1hl. (and passenger) (+27) Maximum baggage Ibs. Fuel capacity 24 gallons (one fuselage tank) (-3) oil capacity 2 gallons (-28) Control surface Elevator Up 14 degrees Down 28 degrees movements Elevator tab Up • 12 degrees Down 22 degrees (Maximum tolerance Aileron Up 14 degrees Down 14 degrees plus or minus 1 Aileron tab Fixed degree on all Rudder Right 16 degrees Left 17 degrees surfaces except Rudder tab Fized ailerons plus 2 Stabilizer Pixed degrees only.) Serial Nos. eligible Required equipment nirvorthiness certificate only (CAR 04.031 of Certification basis Export eligibility Bligible for export as follows subject to inspection for equipment specified in Chapter III of Hanual of Procedure: - Landplane - eligible - Skiplane - not eligible (b) All other countries except Australia, Great Britain and New Zealand. Items included in required list may not be removed unless replaced by approred equivalent items. The effect upon balance of all eguipment changes must be computed and the aircraft operation record rerised accordingly Values in inches shown in parenthesis after each item represent horizontal arms to the C.G. of the item measured minus (-) ahead and plus (+) A plus (*) or minus (-) sign preceding the weight of an optional item indicates the net veight change between that item and the equivalent reguired item. Propellers and Propeller Accessories Propeller - Sensenich 12BC-66 or any other fixed pitch wood propeller which is eligible for the engine pover and speed and which meets the diameter and static Ipm limits given abore. Engine and Engine Accessories - Fuel and Oil Systems Carburetor air heater 2 1bs. (-29) Carburetor air scoop with filter - 5 1bs. (-34) Engine-driven fuel pump - Pesco 2P-227-CA or DA or DD 2 1bs. (-19) Hand fuel pump (AC No. 1523197) 2 1bs. (- 13) Starter - Eclipse Model 635 17 1bs. (-17) Engine-driven fuel pump - Romec RB-4360-4C-A 2 1bs. (-19) Landing Gear 6.00-6 main wheels (Goodyear 16H/MBS) with 1/8# single disc brakes and 4-ply and tubes 35 1bs. (+29) 5.00-4 nose wheel (Hayes 451M less brake) with 6-ply tire and tube 10 1bs. (-30) Nose wheel mud scraper 1 1b. (-26) Electrical Eguipment Battery - 12 volt - 24 Amp Hr. Min. Maximum weight 40 1bs. (+4d) Generator Leece - Neville E-7A, 50 Amp. 24 1bs. (-15) Eclipse Type 790 model 3-D, 50 Amp. 24 1bs. (-15) Eclipse Type 790 model 3-A, 25 Amp. 24 1bs. (-15) 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 change in equipment. be weighed to determine its weight and balance prior to original certification. All Army and Navy serial numbers corresponding to Culver Serial Numbers L304AR to 1703AR, inclusive, are eligible for certification when converted in accordance with the approved Jamieson data. NOTE 3. The following permanent placard shall be installed on the instrument panel in full view of the pilot: "Intentional Spinning Prohibited."