- Holder
- Textron Lycoming AVCO Corporation
- Revision
- 0
- Status
- Current
- Product
- Engine
- Models
- 2
- Registered
- 2 aircraft
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 |
|---|---|---|
| R-680-4 | Formerly Avco Corporation, Lycoming Division | |
| R-680-B4 Series | Formerly Avco Corporation, Lycoming Division |
Airworthiness directives · 5
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.
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: Avco Lycoming R-680-B4 series, R-680-4 and Military R-680-5, -7, -8, -11, -17
I.S. NUMBER: I.C. 108
Kodel - Lyccming R-680-4 and B4 K-680-846
Jype ORA
Fating:
kaximum continuous,
np. xpm, at 5-1.
press. alt. 225-2100-5-1.
Jake-oti, ho, rEm,
at full throttle 225-2100
Fuel (rinimum octane
aviation gasoline) 65
bore and stroke, in. 4.625 × 4.5
Disflacement, cu. in. 680-4
Compression ratio 5.5:1
Leight (dry), ibe. 471 495
Fropeller shaft,
SAE NO.
Carturetion Stromkerg NA-RIA carburetor Stromberg NA-R7B carburetor
with 2.0625 in. venturi with 2.0625 in. venturi
ignition, dual Scintilla SC-A or SC-AZ magneto Scintilla DF or DFN magneto
Ignition tiring,
deg- BIC Front 30, Rear 30 Front 34, Fear 30
Certification basis Type Certificate No. 108 (See NOTE 4)
NCIES 1. 2, 4 1.3.4
NOTE 1. Maximum permissitle cylinder head, tarrel, and oil inlet temperatures, 525 degrees F., 300 degrees F..
and 200 degrees F.. respectively.
R-680-84 engines were formerly designated R-680-4. Serial Nos. 2-751 and 2-752 engines of these
mcdels are eligible at 215 hp at 2000 rpm for all operations. The R-680-4 or k-680-B4 may be corverted
to the R-680-B6 which makes it eligitle for use with a controllable pitch propeller.
NOTE 3. Military model R-680-5 is identical to model R-680-B4B. Models K-689-84C, R-680-B4D and R-680-84L are
similar to model R-680-B48, the differences being noted below. The corresponding military modeis are indicate:
in farenthesis.
Mcdel Difference
F-680-B4C (R-680-7) Includes automatic valve gear lubrication.
R-680-84D (R-680-8, -11) 490 lbs. (dry) weight includes automatic valve gear lubrication
R-680-B4E (R-680-17) a it. tape, aceight inciudes automatic valve gear lubrication,
AN type accessory drive, a redesigned crankshaft and steel link
the pertinent die model designation and eNo. the pertinent certificated aircraft, its rame-plate should te revised to include
NOTE #_ Approval expired 11/2/50. engines of these models manufactured after the dates showr. talow or with
above those indicated, are eligible for use in certification aircraft:
Model Serial No. Date
R-680-4 and
R-680-24 and
R-680-B42 8-1619 3/18/39
R-680-E4C 2552 7/15/41
R-680-B4C 3935 12/31/41
R-680-B4E I015483 3/30/44