- Holder
- Consolidated Vultee Aircraft Corporation Stinson Division
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 7
- Registered
- 14 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 7
| Model | Also known as | Note |
|---|---|---|
| SR-10J3 | ||
| SR-10C (Army UC-81K) | ||
| SR-10H | ||
| SR-10B | ||
| SR-10J | ||
| SR-10G3 | ||
| SR-10G (Army UC-81A) |
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 · 8
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 SA01831WITo allow the use of UL91 (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 SA00478CHInstallation of Cooper Superflite 102 Fabric.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA00068LAInstallation of tail wheel adapter ring.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Stinson SR-10B, -10C (Army UC-81K), -10G (Army UC-81A), -10G3, -10H, -10J,
- 10J3
1.C. NUMBER: 678
I - SPECIFICATIONS PERTINENT TO ALL MODELS
Propeller (See item 102)
Airspeed limits Level flight or climb - 155 mph True Ind.
Glide or dive - 209 mph True Ind.
Flaps extended - 121 mph True Ind.
No. passengers 4 (one front (+13.5), three rear (+53.5))
Baggage 150 1bs. (50 lts. under rear seat (+54) and 100 1bs.
aft of rear seat (+85)) (See NOTE 2)
Certification basis Type Certificate No. 678
Serial numbers 5801 and up manufactured prior to 2/28-41 and all
AAF numbers eligibie. Approval expired as of
2/28/41. (See NOTE 4)
EQUIPMENT:
(Datum is wing leading edge (outboard of curved portion)) (* Means net
increase)
5800 SERIES 5900 SERIES
SR-10B, C, G, SR-TOB, C,
G-3e Fe Je J=3 G-3e-He Le J-3 SR-10G
class I:
A• Landplane:
101. Engine cowl 50 1bs. 43 1bs. 43 lts.
102. Propeller
(a) Lycoming-Smith
P-220 with
Curtiss 32080
blades 117 1bs. (-64) (Item 302b) (Item 302b)
(b) Hamilton Standard
2B20 hub with
6135A-6 OI 6135A-
7 blades. Diameter
8'6-1/8" maximum,
8'3-7/8" minimum. (Item 302a) 104 1bs. (-65) 104 1bs. (-65)
103. Starter (Eclipse
E-80) 20 lts. 18 1bs. 18 1bs.
104. Battery and box
(Ł) (a) Exide 6TS-7-1 Exide 6TS-13-1 38 1bs. (+94) (Item 322' 30 lbs. (+33) 40 1bs. (+33)
105. 7.50-10 wheels with
8.50-10 4-ply tires
(wheels must be
placarded for these
tires) (See Sections
V and VII re tires) 76 1bs. 76 1bs. (+4) 76 Ibs. (+4)
106. 10 inch smooth
contour tail wheel
and tire 21 1bs. 21 1bs. 21 1bs.
107. Cabin heater 8 1bs. 6 1bs. 6 1bs.
108. Shielding - Packard
B.G. plugs 9 1bs. 9 1bs. 9 1bs.
109. Carburetor air
heater
110. (Now Class III
equipment)
111. Generator (Eclipse AI-15 amp.
or G) (Item 301b) (Item 301b) 25 1bs. (-31)
B• 111 PLUS! seaplane (SR-10C, SR-10G-3 and SR-10H (Items 101 thru 104, 107 thru 109,
151. Edo 39-4000 float
installation with
water rudder and
auxiliary fin 306 1bs.*(+25) 313 1bs.* (+29)
Class II:
200. Miscellaneous items
as noted in approved
weight and balance
report
201. Battery and box
(a) Exide 6XT-13-1 66 1bs. 74 1bs. +3= 74 1bs.
(C) Exide 6TX-19-1 80 lbs. 80 lbs. 1+33 80 1bs.
202. Fuel tanks - two
25 gallon main
(wing) 28 1bs. each (+34) 28 1bs. each (+34)
203. Adams mail pick-up
and delivery device
(Kirkham Eng. Corp.)
(See NOTE 3)
(a) Pick-up unit
(replaces rear
hammock seat 22
Ibs. (+59) and rear
seat supports 8
1bs. (+163)) 54 1bs. (+95) (+54) 54 (+54) 54 Its. (+54)
(K) Delivery unit 5 1bs. ibs (+95) 5 lbs. (+95)
(c) Cable and hook
(pick-up) 20 1bs. (+80) 20 1bs. (+80) 20 1bs. (+80)
(Q) Rope and basket (delivery)
14 1bs. (+95) 14 1bs. (+95) 14 Ibs. (+95)
(e) Forward mail com-
partment (200 1b.
capacity) (replaces
copilot chair 24
Ibs. (+12) and
controls 4 1bs.
(-13)) 5 1bs. (+6) 5 1bs. (+6) 5 1bs. (+6)
(f) Center mail com-
partment (150 1b.
capacity) 5 lbs. (+27) 5 1bs. (+27) 5 lbs. (+27)
(g) Rear mail compart-
ment (150 1b.
8 lbs. (+115)
Well in floor Ibs. (+85)
Long cabin type trim 2 1bs. (+85)
cations per Stinson
Drawing 2-3325 25 lts. (+80) 25 lbs. (+80)
Metal skin on belly 15 lts. (+123)
6 1bs. (+41) 6 1bs. (+41)
204. (a) Generator - 25
(Eclipse D) (Item 301a)
generator control
(Item 301c)
205. Vacuum pump and
accessories (Item 305) 10 1bs. (-21) (Item 305)
206. Extra set of
controls (rear) 55 1bs.* (+36)
207. All American Type
AAS-3 mail pick-up
and delivery device
(All American Avia-
tion, Inc.) in-
stalled on model
SR-10C only (See
NOTE 6)
(a) Pick-up unit 39 Ibs. (+47) 39 lts. (+47) _ -
(Ł) Hydraulic system
compiete (AI] Amer-
ican Aviation, Inc.
Drawing S-1) 20 ibs. (-14) 20 ibs. (-94)
(c) Pole knee 8 lbs. (+38) lbs. (+38)
(d) Pole yoke 11 Ibs. (+167) 11 1bs. (+167)
(e) Pole 7 1bs. (+86) 7 1bs. (+86)
(İ) Pick-up rope and
hook 3 1bs. (+40) 3 1bs. (+40) - -
(9) Structural modifi-
cations per Stinson
Drawings 2-2838,
Revision D. Z-4032,
Revision B and
supplementary draw-
ings (including
metal belly cowl,
special fittings,
reinforced floor,
structure, less rear revised cabin special
hatch and
seat) 35 1bs. (+80) 35 1bs. (+80)
(h) Swiveling co-
pilot's chair 4 Its.* (+13) 4 1bs.* (+13) - -
208. All American Type
AAS-4 mail pick-up
and delivery device
(All American Avia-
tion, Inc.) installed
on Model SR-10C only
(See NOTE 8)
(a) Pick-up unit 38 1bs. (*55) 38 1bs. (+55)
(k) Electric control
switch 11 10. (+50) 1 1b. (+50)
(c) Electric drive unit Ibs. (+58) ibs. (+58)
(₫) Arm yoke and lever 14 lbs. (+71) 14 1bs. (+71)
(e) Arm (including
track and hook
retainer) 10 1bs. (+140) 10 1bs. (+140)
(f) Pick-up line and
hook 1bs. (+55 4 1bs. (+55)
(g) Release unit 3 1bs.
(b) Auxiliary seat 6 1bs. (+47) 6 lbs. (+47)
(i) Well to floor 7 1bs. (+79) (+79)
Metal skin on belly 20 1bs. (*135) 20 1bs. (+135)
Baggage shelf (two)
(15 lb. capacity
each) 5 1bs. (+90) 5 1bs. (+90)
(1) Structural modifi-
cations per Stinson
Drawing 2-5081 and
supplementary
drawings)
209. Alternate pneumatic
operated contact arm
yoke installation
tor use with item
207 or 208; as
described in All
American Aviatior,
Inc. Report AM-107-S
(Model SR-10C only).
(a) Pick-up arm and
(10) vacuum cylinder, 17 1bs. (+13) (413)
brackets and rod 16 1bs. (-23) (-23)
Class III:
110. Wheel streamlines 24 lbs. (+ 3) 21 1bs. (+3) 21 lbs. (+3)
301. Generators
(a) 25 amp. (Eclipse D) 30 1bs. (-40) (Item 204a) 30 1bs. (-31)
(k) 15 amp. (Eclipse
AL-1-G) 25 1bs. (-40) 25 lbs. (-31) (Item 111)
(c) Quick detachable
type control box 2 1bs. (-22) (Item 204b) 2 1bs. (-22)
302. Propellers
(a) Hamilton Standard
2B20 hub with
6135A-6 or 6135A-7
blades. Diameter
8'6-1/8" maximum,
8'3-7/8" minimum. 104 1bs. (-63) (Item 102b) (Item 102b)
(k) Lycoming-Smith
P220 with Curtiss
32050 blades (Item 102a) 117 1bs. (-64) 117 1bs. (-64)
(c) Pitch change
accessories
(Lycoming-Smith) 6 1ks. (-59)
(d) Constant speed
accessories
(Hamilton Standard) 9 1bs. (-36) 9 1bs. (-36)
(e) Lycoming-Smith P220
with Lycoming
S0200806 blades 111 Ibs. 111 Ibs. 111 Its.
(1) Lycoming-Smith
P-220 with Lycoming
S0220806 blades 111 1bs. 111 Ibs. 111 Ibs.
303. Fuel analyzer -
Cambridge 7 1bs. (-14) 7 1bs. (-14) 7 1bs. (-14)
304. Lights
(a) Landing (Grimes
ST-1000 12 Ibs. (+13)
(%) Ianding (Grimes
ST-250) 9 lbs. (+16) 9 1bs. (+16) 9 1bs. (+16)
(c) Fog 3 1bs. (+2) 3 lbs. (+2) 3 1bs. (+2)
(d) Moonbeam 1 1b. (+10) 1 1b. (+10) 1 1b. (+10
305. Vacuum pump and
accessories 8 1bs. (-25) (Item 205) 10 1bs. (-21)
306. (a) Flares (three
1-1/2 minute) 14 Ibs. (+116) 15 Ibs. (+116) 15 Its. (*116)
(k) Flare wiring
(three flares) 2 1bs. (+33) 3 1bs. (+33) 3 1bs. (+33)
(c) Flares (four
1-1/2 minute) 20 1hs. (+116)
(d) Flare wiring
(four flares) 4 1ks. (+33)
307. Two pilot parachute
chairs 30 1bs.* (+17) 24 1bs.* (+17) 24 1bs. * (+17)
308. TWO rear seat
parachutes 0 1bs. (+54 40 1bs. (+57) 40 1bs. (+57)
309. (a) Special paint 5 1bs. (+48 15 1bs. (+48) 15 1bs. (+48)
(k) Special Folish
(14-16 coats) 10 1bs. (+36) 10 1bs. (+36)
(c) Special polish
(10-12 coats) 7 1bs. (+36) 7 1bs. (+36)
310. Radio equipment
(a) Miscellaneous (maximum) 60 1bs. between (+16.3) 8 (+54) 66 1bs. (+16.3) between 8 (+43) 66 1bs. (+16.3) between (+43)
(k) Miscellaneous
(maximum in 37 1bs. between 37 1bs. between 37 1bs. between
addition to (a)) (+1603) 8 (+54) (+16.3) & (+45.6) (+16.3) and (+45.6)
(c) Radio equipment box 7 1bs. (+54) 9 1bs. (+54) 9 lbs. (+54)
(d) Antenna - tee type 2 lbs. 2 lbs. (+125) 2 1bs. (+125)
(e) Antenna - vee type 4 lbs. (+91) " lbs. (+91) 4 1bs. (+91)
(f) Antenna - maximum 9 1bs. between 9 lbs. between 9 1bs. between
reel allowance (+15) & (+115) (+15) (+115) (+15) & (+115)
(g) Antenna trailing 1bs. (*219) 3 1bs. (+219) 3 Its. (+219)
311. Two point thermo-
couples 3 1bs. (-11) 2 1bs. (-25) 2 1bs. (-25)
312. Double intensifier
tutes 8 1bs.* (-42)
313. (a) Camera door
(k) I.H. cabin door
(c) Releasable door and step 1 Ib.* (+15 - 30 • 1b. (+15) • Ib. (+15)
(d) Multi-purpose door
(Drawing F-3980)
314. Heated pitot tube 1 1b. (-8) 1 1b. (-8) 1 1b. (-8)
315. Corrosive proofing
(a) Salt water 25 1b5. (+55) 25 lbs. (+50)
(₺) Fresh water 15 1bs. (+50)
316. Puncture proof tubes
or inner liners 6 1bs. (+4) 6 1bs. (+4) 6 lks. (+4)
317. Fire extinguisher
(Lux No. 5) 8 ibs.* (-25) 20 lts. (+1)
318. Thermo-pete
(built-in) 2 1bs. (-34)
319. Special instruments
(a) 371bs. (-16) 20 1bs. (-16) 15 lbs. (-16)
(Ł) 2 1bs. (-12) 2 1bs. (-12)
320. Fuel tanks - one or
two auxiliary 24 22.5 1bs. 22.5 lbs. 23 lbs. (+17)
gallon (wing L.E.) each (+17) each (+17) (one only)
321. Oil tanks
(a) 6-1/2 gallon 2 1bs.*(-34) 2 1bs.* (-34)
(C) 7-3/4 gallon or
8 gallon 2 1k8.* (-34) 2 1bs.* (-34)
322. Battery and box
(Exide 6TS-13-1) (Item 104b) 40 1bs. +33 (Item 104b)
323. 8.50-10 6-ply tires 8 1bs.* (+4) 8 Ibs.* (+4
324. Lycoming R-680-E3A
engine (Models
SR-10J and - 10J3
only) 10 1bs.* 10 lbs.*
NOTE 1. Eligible for export as follows, subject to inspection for equipmert
specified in Chapter XII of Manual of Procedures:
- Landplane - eligible.
- Skiplane - not eligible. structure complies with Canadian
requirements for ski installation with maximum ski height 10-1/2 inches
and maximum tread 113 inches.
All other countries except Australia and New Lealand. - Seaplane - (SR-10C
NOTE 2. Rear baggage must be limited to 50 lbs. when three passengers are carried
or rear seat and compartment must be so placarded, unless substantiated by
weight and balance data.
The following speed and weight limitations must be observed during
pick-up and delivery when item 203 is installed.
Maximum airspeed during pick-up or delivery 100 mph.
Maximum pick-up load 50 lbs.
Maximum delivery load 84 1bs.
NOTE 4. Serial numbers 5901 and up same as 5800 series except vertical tail
surface, battery installation, fuel system, exhaust collector ring, ergine
cowl, control wheel, and pilot's chair.
NOTE 5. Model SR-10G, serial numbers 5943 and up eligible at 4000 lbs. with
6-ply tires, item 323, required equipment. Serial numbers 5901
to 5942, inclusive, eligible as follows:
Maximum weight 4150 1bs.
Airspeed limits Ievel flight or climb - 165 mph True Ind.
Glide or dive - 220 mph True Ind.
Flaps extended - 121 mph True Ind.
(8.50-10 6-ply tires, item 323, required equipment.)
NOTE 6. The following speed and weight limitations must be observed during
pick-up and delivery when item 207 is installed:
(a) aximum airspeed during pick-up or delivery 100 mph.
(b) aximum pick-up load 50 1bs
Maximum delivery load 50 1bs.
NOTE 7. Maximum weight may be increased to 4150 1bs. for Model SR-10C when
Item 323 is installed.
NOTE 8. The following speed and weight limitations should be observed during
pick-up and delivery when Item 208 is installed.
Maximum Speed Maximum Load
150 60
140 70
130
120 90
II - MODEL SR-10B, DESIGNATION 5 PCLM
Engine Lycoming R-680-D6
Engine limits except take-off
-- in.Hg.. 2100 rpm (225 hp)
Take-off (one mir.ute)
-- in.Hg.. 2300 rpm (245 hp)
Fuel capacity 76 gallons (two 38 gallon tanks in wings) (+34)
Oil capacity 5 gallons (-34)
Maximum weight 5900 1bs.
c.G. limits 5900 series (+16-3) and (+26.7) 5800 series (+16.3)
III - MODEL SR-10C (UC-81K), DESIGNATION 5 PCL-SM
(Same as Model SR-10B except engine installation)
Engine
Engine limits 9, 210 re- (245 hp)
-- in. Ng., 2300 rpm (260 hp)
Fuel capacity (two 38 gallon tanks in wings) (+34)
oil capacity
Maximum weight Landplane 3900 1bs. (See NOTE 7)
Seaplane 4210 1ks.
C.G. limits
5800 geries (+16.3) and (+27.7
6900 series (*16.3) and (*26.7
5800 series (+17.0) and (+27.6)
5900 series (+17.0) and (+26.6)
IV - MODEL SR-10G (UC-81A), DESIGNATION 5 PCIM
(Same as Model SR-10D, I.C. 679, except engine installation)
Engine
Engine limits except take-off
2200 rpm (275 hp)
2300 pm (290 hp)
Fuel capacity
oil capacity
Maximum weight 3900 1bs. (See NOTE 5)
C.G. limits 5900 series (*16.3) and (*26.7)
V - MODEL 8R-10G3, DESIGNATION 5 PCIM
(Same as Model SR-10B except engine installation and standard weight, 8.50-10
5-ply tires, item 323, required equipment.)
Engine Lycoming R-680-E1
Engine limits Maximum, except take-off
2200 rpm (275 hp)
Fuel capacity -- in.Pgs' (two tanks at 38 gallons each in wings 2300 pm (290 hp)
Cil capacity 6-1/2 gallons (-34)
Maximum weight
c.G. limits 5900 series (*16.3) and (+26.7)
VI - MODEI SR-108, DESIGNATION 5 PCI-SM
(Same as Model SR-10B except engine installation)
Engine
Engine limits Maximum, except take-off
-- in. Hg., 2200 rpm (265 hp)
-- 1n.Hg.. 2300 Ipm (280 hp)
Fuel capacity (two 38 gallon tanks in wings) (+34)
cil capacity
Maximum weight Landplane 3900 1bs.
Seaplane 4210 1bs.
C.G. limite
5900 Series (+16.3) and (+26.7
800 series (+17.0) and (+</..
5900 series
VII - MODEL SR-10J Or SR-10J3, DESIGNATION 5 PCIM
(Same as Model SR-10B except engine irstallatior and standard weight, 8.50-10
6-fly tires, item 323, requires equipment)
Engine Lycoming R-680-E3 (see item 324)
Engine limits Maximum, except take-off
-- in. Hg.. 2200 rpm (285 hp)
Take-off (one minute)
-- in. Hg.. 2300 rpm (300 hp)
Fuel capacity (two 38 gallon tanks in wings) (+34)
Cil capacity 5 gallons (-34)
Maximum weight
c.G. limits 800 series (+16.3) and (+21.!
5900 series (+13.3)