TCDS TC 169

Type certificate data sheet · Wright Aeronautical Division Curtiss-Wright Corporation · Engine

Holder
Wright Aeronautical Division Curtiss-Wright Corporation
Revision
0
Status
Current
Product
Engine
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
Cyclone GR-1820G-102 Series

Airworthiness directives · 0

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What the data sheet saysOCR

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MORELS: Wright Cyclone GR-18206-102 series and Military R-1820-57, -79, -81, -83, -85, -89 IS. NUMBER: T.C. 169 Model - cyclone GR-18206 - 102 • 10 2A - 102B Type - 16:11 and 3:2 reduction gears Rating: Maximum continuous, spa. in.Hg.. at: tated pressure altitude (ft.) 900-2200-35-6000 900-2300-35.4-6700 850-2300-34.5-7500 pressure altitude 900-2200-36.7-S.L. 900-2300-37.5-S.L. 850-2300-38 1/2 -S.L. (one minute), Fuel hp. (minimum octane in. Hg. 1100-2350-43 6 1100-2200-43 1100-2350-43-5 1100-2350-43 aviation gasoline) Pore and stroke, in. (CFR Motor Method fuel) 90 6-112 × 6-718 87 risflacement, cu. in. 1823 compression ratio 6.7:1 6.0:1 height (dry), Ibs. 1275 Fropeller shaft, SAE NO. 50 Supercharging (infeller gear ratio) 7:1 Carburetion Holley C.G. 1375 C, E HA OI stromberg Chandler-Evans 1375 DA-1, or PD-12H2 or 3 carburetor with .. Strombexg PD-12B5 or 7 ox 3-1/4 in. venturi Ignition, dual Scintilla SF9L1, SF9L2, SF9IN, SF9LN1, SF9L3, SF9L4 or Bosch SF9LU3 magnetos Ignition timing, NOTES Certification basis degrees BIC Right 20; left 15 Type Certificate No. 169 Type 1,2,3 1. 2 Froduction casis None. The manufacturer does not hold a production certificate for the production of engines under this type certificate, and therefore, each engine so produced is subject to a Jetailed inspection for workmanshif and conformity with the approved data ky a Civil Aeronautics Administration Agent. In addition, the engine must have a satisfactory run-in including 5 hours at rated power and speed. Ufon satisfactory completion of the above, the agent will tag the engine with Iag Form ACA 186. Maximum permissible cylinder head, barrel, and oil inlet temperatures 500 degrees F.. 325 degrees I.. and 222 degrees F., respectively. NOIE 2. Eligitle with torquemeter No. 413516 at weight increase of 12 lbs. NOTE 3. Military models R-1820-79, -81, -83, -85 and -89, identical to model GR-18206-102A, are eligikle for use in certificated aircraft; however, the engine nameplate should be revised to include the correspondirg ivil model designation and Type Certificate number. NOTE 4. Military model R-1820-57 may be corverted to the Cyclone GR-18200-102 Ly substituting supercharger impeller P/N 27145 and using either the 1375 DA-1 carburetor, setting number 69445N1, 2 or 4 as applicable or substituting the Holley 1375 F carturetor with setting number 6927N29B.