- Holder
- Wright Aeronautical Division Curtiss-Wright Corporation
- Revision
- 0
- Status
- Current
- Product
- Engine
- Models
- 2
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 2
| Model | Also known as | Note |
|---|---|---|
| Cyclone R-1820G-2 | ||
| Cyclone GR-1820G-2 |
Airworthiness directives · 1
ADs whose products are models on this data sheet, matched by model and maker.
STCs approved under this data sheet · 1
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Wright Cyclone R and GR-18206-2, -2E and Military Models R-1820-49, -53, -55
I.C. NUMBER: T.C. 157
Model - Cyclone R-1820G-2 GP-1820G-2
Direct drive 16:11 reduction gearing
Rating:
hE. rEm, in. Hg., at:
Rated pressure
altitude (ft.) 850-2100-34-5-5800
Sea level pressure
altitude 820-2100-345-S.L.
Take-off (one minute),
in.Hg. 1000-2200-40.0
aviation gasoline) 87
Fore and stroke, in. 6.125 × 6.875
Displacement, cu. in. 1823
Comfression ratio 6-45:1
weight 1bs. 1103 1198
Fropeller shaft,
SAE NO. 50
Supercharging
(imfeller gear ratio)
Carturetion Stromberg NA-F7F Frolley C.G. J or K with
2-3/8 in.
1375 C, 2, *• H or Chandler-Evang
1375DA-1
Ignition, dual Scintilla SF9L1, Sf9L2, SF9LN,
SF9LN1, SF9IN2, SF9L3 OL
SF9L4 magnetos
Certification basis Type Certificate No. 157
Froduction basis None. The manufacturer does not hold a production certificate for the production of engires
inspection to demand contity in the poved data vile title. workmanshif and data by a Civil Aeronautics
an adaicion, cne engine must nave a satisractory run in incidaing
5 hours at power and speed. Upon satisfactory completion of the above, the agent
NOTES 1. 3,1 tag the engine with lag Form ACA 1,62, 3, 4, 5
linder head, barrel, and oil inlet temperatures, 500 degrees F., 300 degrees F.,
NOTE 2. 2A engines, numbers 25844 to 25850 inclusive, were subsequently modifief to model
Models R and GR-1820G-2E, imilar to corresponding models R and GR-18206-2, eligible at weights (dry) of
incorporate the G-100 series steel crankcase.
KOTE WO43. 24005, 2405, 2551, 24033, 20054, 24037, 24028 2e eleven 20110ing at 29: 24040, 24041, 24042.
1pm in. Hg.. at:
850-2100-35.5-5500
Sea level pressure altitude 820-2100-35.5-S.L.
Take-off (one minute), hp. rpm, in. Hg. 1000-2200-42.0
Eith the mary noturer instructiong to theorporate at leat the following new farts and setting settingccordar.ce
ModEl
R-1820-49 and -55 R-1820-53 The eat, an else me 6970, 516, 61975 one 108. ave 2 4 830 Supercharger impeller, P/N 27145; carburetor, Stromberg NAF7F2, settirg rumber 64551 or
(Remove all high ratio
drive parts.)