TCDS TC 750

Type certificate data sheet · Timm Aircraft Corporation · Aircraft · Small Airplane

Holder
Timm Aircraft Corporation
Revision
0
Status
Current
Product
Aircraft · Small Airplane
Certification basis
CAR 4a
Models
1

The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.

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Models · 1

ModelAlso known asNote
PT-220-C

Airworthiness directives · 1

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Registered aircraft

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STCs approved under this data sheet · 3

What the data sheet saysOCR

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MCDEIS: Iimm PT-220-C, 2 POLM I.C. NUMBER_: 750 (Approved 4/28/42) Engine continer.tal W-670-6A or W-670-6N Fuel 65 minimum octane aviation gasoline Engine limits For all operations, 2075 pm (220 hp) Airspeed limits Level flight or climb - 160 mph True Ind. Glide or dive - 205 mph True Ind. extended - 108 mph True Ind. (Front face of Airspeed Calibration ring on pitot tube must be 4-5/8 inches aft of nose of pitot Propeller limits Static rpm at maximum permissible throttle setting (with Item 101) - not more than 2870 No additional tolerance permitted. - not more than 98 inches - not less than 96 inches C.G. range (+4902) to (+5202) Catum leveling means Lugs inside baggage compartment Maximum weight 2 (one at +43.5 and one at +96.5) Maximum baggage 20 Ibs. (+126.5) Fuel capacity cil capacity 3-3/4 gallons (-4) control surface Elevators - Up 24 degrees; down 30 degrees Rudder - right and left 16 degrees from centerline Ailerons - Up 17 degrees; down 13 degrees Serial numbers eligible 111, 114 and up (See NOTE A) Required equipment Items 101, 102, 103 and 104 SPECIFICATIONS PERTINENT TO ALL MODELS: Certification basis Type Certificate No. 750 (CAR 4a) Production basis None (See NOTE A) Export eligibility Eligible for export as follows, subject to provisions of MOP 2-4: - Landplane - eligible. - Skiplane - not eligible. (b) All other countries except Australia, Great Britain and New Zealand. EQUIPMENT: Propellers and Propeller Accessories Propeller - fixed pitch wood Index propeller in 90 degree position (blades at right angles to crankthrow) (-37) 202. Propeller - Fahlin Model D-760-68 (94) Index propeller in 90 degree position (blades at right angles to crankthrow) (Propeller limits under Part I, above, do not apply to this propeller.) 27 1bs. (-37) Engines and Engine Accessories - Fuel and Oil System 104. Carburetor air heater (Timm 2-34019) 4 1bs. (-10.5) 201. Starter - hand inertia (Bendix series 6) 19 1bs. (-10) Landing Gear 102. 7.00-8 wheels and brakes (Shinn 8C1YFB) with tires and tubes 66 1bs. (+33) 103. Steerable tail wheel (Shinn B0200) with tires and tube (+213) NOTE 1. Placard airplane: "Intentional spins prohibited with flaps extended." NOTE A. Each aircraft manufactured after 1/5/44 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 may be varnished. (b) A final inspection of the completed aircraft. A check of flight characteristics: