- Holder
- Ryan Aeronautical Company
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 1
- Registered
- 7 aircraft
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 |
|---|---|---|
| SCW-145 |
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 · 11
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 SA4503NMRemove original cloth covering and install Ceconite coveringSTC SA01831WITo allow the use of UL91 (minimum) grade aviation fuelSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA02283SE PAGE 2Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 2Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA1626NM PAGE 2Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series)STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
RYAN AFRCHAUTICAL COMPANY
MODELS: Ryan SCW-145, 3 PCIM
I.C. NOMBER: 658
Engine Warner Super Scarab Series 50 or 50A
Placard limits For all operations, 2050 rpm (145 hp)
Propeller Maximum permissible diameter 84 inches
Placard speeds Level flight or climb - 147 mph True Ind.
Glide or dive - 198 mph True Ind.
Fuel capacity ST galLone done tak in agine compartment f-78%. Flaps extended - 108 mph True Ind. gallons (one tank in fuselage) (one tank in engine compartment f-25)
oil capacity 3 gallons 1bs. (-36)
No. passengers 2 (+4. +31) (crew at +4)
Baggage 190 1bs. (single compartment in rear of cabin) (+31)
(See NOTE 2)
Maximum weight 2150 1bs.
C.G. limits (-4.7) and (+2.1) Level for weighing on longitudinals
at bottom of cabin door.
Specification basis Type Certificate No. 658 (Aero Bulletin 7A requirements)
Serial numbers 201 and up eligible per NOTE A
EQUIPMENT: (Datum is centerline of the wing spar) (* Means net increase)
Class I:
101- Engine cowl 21 1bs. (-45)
102. Manifold and preheater 18 1bs. (-52)
103. Propeller - wood 30 lbs. (-67)
104. Starter (Eclipse Y-150) 20 lbs. (-40)
105- Battery (Reading 6AR19) 29 lbs. (-38)
107- Cabin heater-ventilator
108- Wheel streamlines 10 1bs. (-11)
109. (a) 18x8-3 wheels (Goodyear
3IMBA or 3IMBM) 14 lbs. (-15)
(b) 18x8-3 tires (Goodyear 4-ply HD)
(wheels must be placarded for
21 1bs. (-15)
Shock struts (Aerol A0-2) 20 1bs. (-91
110- inch streamline tail wheel 3 lbs. (+189)
111- Left elevator trailing edge tab,
manually operated
112. Center section flap, manually operated
Drawing No. C-2090
Class II:
201. Generator
(a) Hodges H-12-V 1bs. (-24)
(b) Bosch LE70/12R5 11 1bs. (-45)
202- Parachute (rear passenger) 20 1bs. (+31)
204. Landing lights (Grimes ST-250) 8 1bs. (+15)
205. Flares (Inter. MEII Model 1-3) 13 1bs. (+35)
Class III:
Parachutes (pilot and front passenger) 40 1bs. (+4)
Center section flap, manually operated
(Drawing No. C-2090A) 20 1bs.*
303. Battery (Exide 6TS-7-1) with box - 36
Each aircraft manufactured after 11/20/40 must, prior to original
certification, satisfactorily pass:
An inspection for workmanship, materials and conformity before any
covering, metal priming or final finish is applied. All woodwork
may be varnished.
(D) A final inspection of the completed aircraft.
(c) A check of the flight characteristics.
Eligible for export as follows subject to inspection for equipmert
specified in Chapter XII of Inspection Handbook:
(a) Canada
- Landplane - eligible
- skiplane - not eligible.
(b) All other countries except Great Britain, Australia and New Zealand.
NOTE 2. Baggage in compartment rear of cabin must be limited to zero when
passenger occupies rear seat and it must be so placarded. Maximum baggage
must be determined by C.G. check, not to exceed 190 lbs. in any case.