- Holder
- Textron Lycoming AVCO 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.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| R-680-D5 | 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-D5
I.C. NUMPER: I.C. 172
Model R-680-D5
туре 9RA
kating:
Maximum continuous,
Df. Ipm. at S.L.
Fress. alt. 245-2100-S.L.
Take-off (one minute).
rEm, at full
throttle 260-2300
Fuel (minimum octane
aviation gasoline) 80
Fore and stroke, in. 4.625 × 4.5
Cisplacenent, cu. in. 680-4
Corfression ratio 6-5:1
weight (dry) . Ibs. 516
Fropeller shaft,
SAE NO.
Carturetion Stromberg NA-F7A carburetor with 2-1/16 in. venturi
Ignition, dual Scintilla SC-A2 magneto
Certification tasis Type Certificate No. 172 (See NOTE 3)
NOTE 1. Eligible with constant speed propeller drive with increase in weight of 2 Ibs-
NOTE 2. Maximum permissible cylinder head, barrel and oil inlet temperatures, 525 degrees F.. 300 legrees F.. ard
200 degrees F., respectively.
NOTE 3. Approval expired 11/2/50. No engines manufactured after 12/15/40 or with serial number above 1475 eligitle
for use in certificated aircraft.