- Holder
- Rans Inc.
- Revision
- 0
- Revised
- September 14, 2001
- Status
- Current
- Product
- Aircraft · Small Airplane
- Certification basis
- Part 21, Part 36
- 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 |
|---|---|---|
| S-7C |
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
STCs approved under this data sheet · 1
What the data sheet says
From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.
P a g e N o .123
R e v . N o .---
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
TYPE CERTIFICATE DATA SHEET NO. A00011WI
This Data Sheet, which is part of Type Certificate No. A00011WI prescribes conditions and limitations
under which the product for which the Type Certificate was issued meets the airworthiness requirements of
the Federal Aviation Regulations.
Type Certificate Holder: Rans Inc.
4600 Highway 183 Alternate
Hays, Kansas 67601
MODEL S-7C (PRIMARY CATEGORY) - APPROVED SEPTEMBER 14, 2001.
ENGINE: Rotax 912 ULS
FUEL:
Unleaded automotive (ASTM D 4814) gasoline with minimum AKI (Anti Knock Index)
of 91(R+M)/2 – no alcohol permitted.
Or Avgas 100 LL Grade Aviation Fuel
For other fuel see Rotax Operators Manual supplied with engine.
OIL:
SAE- Motorcycle oil of registered brand with gear additives.
Use only oil with API classification “SF” or “SG”.
Minimum recommended viscosity SAE 10W-40.
For additional information refer to Rotax Operators – and Maintenance Manual.
COOLANT:
50%/50% glycol antifreez / water (ASTM D4985) with additives against corrosion. For additional
information refer to Rotax Operators Handbook.
ENGINE LIMITS:
Maximum Takeoff (max. for 5 minutes): 98.5 HP at 5800 RPM
Maximum Continuous: 92.5 HP at 5500 RPM
(Power tolerance + 5%)
PROPELLER AND PROPELLER LIMITS:
Sensenich W72RR
Diameter: not over 72” in., not under 70 in.
A00011WI
Original
Rans Inc.
Model S-7C
September 14, 2001
A00011WI 2 of 3
AIRSPEED LIMITS (MPH CAS):
Never exceed: 130 mph
Maneuvering: 97 mph
Flaps extended: 69mph
CG RANGE:
(+46.1) in to (+50.25) in at 950 lb. or less
(+48.4) in to (+50.25) in at 1200 lb.
Straight line variation between points given.
EMPTY WEIGHT CG RANGE:
None
MAXIMUM WEIGHT:
Maximum Ramp: 1200 lb.
Maximum Take off: 1200 lb.
Maximum Landing: 1200 lb.
MINIMUM CREW:
One (1) Pilot
NO. OF SEATS AND LOADING:
Pilot (+37.4) in
Passenger (+65.4) in
MAXIMUM BAGGAGE:
50 lb. at (+92.5) in
FUEL CAPACITY:
18 gal total (16.75 gal usable, two 9 gal tanks in wings at +52.2)
OIL CAPACITY:
6.4 liq pt, min. 4.2 liq pt)
MAXIMUM OPERATING ALTITUDE:
12500 ft
CONTROL SURFACE MOVEMENTS:
Rudder: Right 28º Left 28º
Elevators: Up 28º Down 20º
Elevator trim tab: Right 30º Left 20º
Ailerons: Up 28º Down 20º
Wing Flaps: Half 17º Full 34º
DATUM:
Front of firewall.
LEVELING MEANS:
Top of upper cabin longeron (below door).
CERTIFICATION BASIS:
Primary Category FAR Part 21 Certification using Canadian TP10141E and FAR Part 36.
Equivalent Safety Findings have been granted as follows:
JAR- VLA Paragraph 145(a) was used in lieu of Transport Canada TP10141E
Paragraph 145 as an Equivalent Level of Safety per FAA letter dated September 13, 2001.
A00011WI 3 of 3
Application for Type Certificate was dated January 27, 1994. The Model S-7C Type
Certificate was obtained by RANS under authority of FAR Part 21, Subpart J.
PRODUCTION BASIS:
None
EQUIPMENT:
N/A
NOTE 1. Current weight and balance data, loading information and a list of equipment included in
empty weight must be provided for each airplane at the time of original certification.
(a) Basic empty weight includes unusable fuel of 7.5 lb (1.25 gall) at (+52.2) in.
NOTE 2. All Placards required in the FAA Approved Flight Manual P/N CPAC0103 must be
installed in the appropriate location.
NOTE 3. The type design of the RANS S-7C is defined by RANS Corporation Master Drawing
CVAC0001, Revision None, dated August 10, 2001.
….END….