- Holder
- Wright Aeronautical Division Curtiss-Wright Corporation
- Revision
- 0
- Status
- Current
- Product
- Engine
- Models
- 3
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 3
| Model | Also known as | Note |
|---|---|---|
| Cyclone GR-1820G-105A | ||
| 718C9GB1 | ||
| Cyclone GR-1820G-105 |
Airworthiness directives · 1
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Wright Cyclone GR-1820G-105, -105A and 718C9GB1
I.C. NUMBER: T.C. 192
Model - Cyclone GR-1820G - 105 - 105A
New designation 718C9GB 1
Type - 9RA 16:11 6 3:2 reduction gears 3: 2
Rating (with low
impeller gear ratio): 7.14:1
melated grabore de.
900-2200-35.-6000 900-2300-35.4-6700 900-1200-35.4-6700
Sea level
pressure altitude 900-2200-36.7-8.I. 900-2300-37.5-S.L. 900-2300-37.5-S.L.
Take-off (5 minutes) ,
hp. rpm, in.Hg. 1100-2200-43 1100-2350-43.5 1100-2350-43.5
1080-2200-43.4
Rating (with high
impeller gear ratio) 10:1
faximum continuous.
bp. rpm, in.Hg.. at:
Raced pressure
altitude (ft.) 750-2200-33.-17000 775-2300-33-6-17300 775-2300-33-6-17300
Low critical
Fressure altitude
(£t.) 750-2200-36-11000 775-2300-36.-1100 775-2300-36.-11000
Take-off (5 minutes).
850-2200-39.5-S.L.
take-off (5 minutes).
altitude in. Hg.,rpm, hp 850-2200-36-8-15200
Fuel (minimum octane
aviation gasoline - Low impeller ratio 90
CFR Motor Method fuel) High impeller ratio 95
Fore and stroke, in. 6.125 × 6.875
Lisplacement, cu. in. 1823
compression ratio 6.7:1 6.3:1
height (dry), 1bs. 1272
Fropeller shaft,
SAE NO. 50
Carturetion Holley C.G. 1375 C, E, R,
Sentes. 75-25, 8% 4ận. or Stromberg HA Or
FD-12E5, B7, H2,
1375DA-1 cartureto:
Ignition, dual Scintilla SF9L2, 3, 4, or
Bosch SF9LU-3 magnetos
Ignition timing,
degrees BTC Right 20
Left 15
• 2, 4 1,2,3,4
Certification rasis Type Certificate No. 192
S1000CC101 04S1S The manufacturer does not hold a production certificate for the production of
engines under this type certiticate and, theretore, each engine so produced is subject
to a detailed inspection for workmanship and conformity with the approved data ty a
Civil Aeronautics Administration Agent. In additio nupon satisfactory completion of the the engine must have a satisfactory
run-in including 5 hours at rated power and speed.
above, the agent will tag the engine with Tag Form ACA 186.
AT 220 degrees permispectivelyinder head, barrel and oil inlet temperatures, 500 degrees F., 325 cegrees F., and
NOIE 2. Incorforates standard 68354 or uniflox 69115 pistons.
SOTE GR- 1820E- 0-10. to beats me fear it system and otherwise similar to Mode.
NOTE 4. Eligible with torquemeter number 413516 at a weight increase of 12 1bs.