- Holder
- Consolidated Vultee Aircraft Corporation Stinson Division
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 2
- Registered
- 9 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 |
|---|---|---|
| SR-2 | ||
| JR. SR |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 5
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01757WITo allow the use of UL91 or UL94 (minimum) grade aviation fuelSTC SA6070NMInstallation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown.STC SA00024NYInstallation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: Stinson JI. SP, and SP-2, 4 PCL-SM
I.C. NUMBER: ATC 510
Ergine Lycoming R-680 (See Item 315)
Flacard limits махіти, except take-off
-- in.Hg., 2000 rpm (215 hp)
Take-off
in. Hg.. 2000 rpm (215 hp)
Fuel 50 gallons (one 25 gallon tank in each wing)
Cil 4 gallons
No. passengers
Baggage 75 lts. (Seaplane includes anchor and rope 30 lbs.)
Standard weight Landplane - 3160 1bs.
Seaplane - 3469 Its. (with adj. metal propeller)
- 3500 lrs. (with contr. metal propeller)
Specification basis Approved Type Certificate No. 510
Serial numbers 8700 and up manufactured prior to 9/30/39 eligible.
Approval expired as of that date.
EQUIPMENT: (* Means net increase)
Class I:
Landplane:
Engine ring cowl 22 1bs.
Wheel fenders 13 lbs.
Starter (direct electric) 26 Ibs.
Battery 36 1bs.
Heater
Propeller - adj. metal
107. 8.50-10 wheels and tires
108. 8 inch streamline tail wheel
Seaplane: Items 101, 103, 104, 105 and 106 PLUS
151. Edo P-3300 floats
152- Auxiliary fin on bottom of fuselage
replacing tail wheel
Class III:
Landplane:
Fuel and oil capacities
74 gallons fuel (2 at 37 gals.)
and 5 gallons oil 21 1bs.*
72 gallons fuel (2 at 36 gallons)
gallons oil 14 Its.*
302. Larger engine ring cowl 8 lbs.*
303. Wing and stabilizer fairing 1bs.
304. lts.
305- 6 or 9 1bs.
306. Generator 18 1bs.
307. Fog light 3 1bs.
308. Flares - five one-minute 16 1bs.
309. Leather trim 9 1bs.
310. Ryan retractable landing lights 26 1ts.
311. Wheel streamlines 22 lbs.
312. Lear radio 25 1bs.
313. 25x11-4 tires with hydraulic brakes 11 1bs.*
314. Propeller - Lycoming-Smith p-221 with
Curtiss 350 Smith blades 49 1bs.*
315. Lycoming R-680-7 engine (Item 314 must
be installed - low pitch setting 11
degrees 15') (Minimum fuel may be
computed on basis of 215 hp)
Placard limits:
Maximum, except take-off, 2000 rpm
(215 hp) ;
Take-off (one minute) 2300 rpm (240 hp)
316. 10.5 in. streamline tail wheel
seaplane: Item 314 PLUS
351. Edo 38-3439 floats
NOTE 1. The following placard must be displayed in full view of the pilot:
"ALWAYS CHECK FUEL FLOW AT STRAINER DRAIN BEFORE TAKE-OFF. NEVER FLY ON
ONE TANK WHEN FUEL IS LOW.I
Serial No. 8910 is eligible as model SR-2 with the following:
(Same as model SR except horizontal tail surfaces and their controls,
equipment and standard weight.)
Engine Lycoming R-680
Placard limits Same as for R-680 above
Fuel 50 gallons
Oil 4 gallons
Baggage 50 1bs.
Standard weight 3233 1bs.
Engine ring cowl 30 1bs.; starter (direct electric) 26 1bs.; battery 35 lbs.;
heel streamlines 28 lbs.; five 1-minute flares 16 lbs.: bonding 5 lbs.: leather
lbs.; special instruments 10 lbs.; heater; 8.50-10 wheels; 5.00-4 tail