SINGLE-ENGINE PISTON
Victa Airtourer 100
One model from CASA certificate of type approval data sheet 34-1. Every figure below is quoted from the sheet. Open any “Source” to see the words it comes from.
THE DATA SHEET
- Authority
- Civil Aviation Safety Authority (Australia)
- Sheet
- Certificate of Type Approval Data Sheet 34-1
- Revision
- 2
- Date
- 23 April 2007
- Holder
- Airtourer Cooperative Ltd.
- Licence
- CC BY 4.0 (opens in a new tab) (CASA website licence)
Scanned sheet. This sheet is a scanned image, and the text we store was read by OCR. We use only values whose label and figure sit together on a clean line. Check the PDF before relying on any value.
Performance figures (stall speeds, take-off and landing distances, climb, cruise and fuel burn) are in the aircraft's flight manual (POH/AFM), which we cannot reproduce. Always use the flight manual for the aircraft you fly.
Attribution: Civil Aviation Safety Authority, Certificate of Type Approval Data Sheet 34-1, Revision 2, licensed under CC BY 4.0. We changed the material: we selected values, set them out in our own layout, and quote from our stored text copy described below.
How we copied the sheet. Quotes are from our stored text copy of the scanned sheet, read by OCR. We converted maths markup to symbols, removed repeated table labels and marked table cells with |. Check the original PDF before relying on any figure.
Models not shown. The sheet covers one model, and it is included.
SPEC SHEET
Victa Airtourer 100: AT-100
Air Tourer
The sheet's heading for this modelAir Tourer AT-100 (Normal and Acrobatic Categories)
Source for the model heading
Model Air Tourer AT-100 (Normal and Acrobatic Categories) Approved 4 July 1962
Engine
- Engine
- Teledyne Continental Motors O-200-A
Source for Engine
Engine Teledyne Continental Motors O-200-A
- Rated power
Not in the type certificate data sheet
- Engine speed limit
- 2,750 rpmTake-off. The sheet gives the same maximum continuous figure.
Source for Engine speed limit
Engine limits Maximum, takeoff: 2750 rpm
- Propeller
- McCauley 1A105/SCM 6950
Source for Propeller
Propeller Type: McCauley 1A105/SCM 6950
Fuel and oil
- Fuel capacity
- 29 Imp gal≈ 132 L (converted)
Source for Fuel capacity
Fuel Capacity 29.0 Imp. Gal. (28.7 Imp. Gal. useable)
- Usable fuel
- 28.7 Imp gal≈ 130 L (converted)
Source for Usable fuel
Fuel Capacity 29.0 Imp. Gal. (28.7 Imp. Gal. useable)
- Oil capacity
- 1.25 Imp gal≈ 5.7 L (converted)
Source for Oil capacity
Oil capacity 1.25 Imp. Gal.
Weights and loading
- Maximum weight
- Normal category1,650 lb≈ 748 kg (converted)
Source for Maximum weight, Normal category
Maximum weight Normal Category: 1650 lb, Acrobatic Category: 1550 lb
Acrobatic category1,550 lb≈ 703 kg (converted)Source for Maximum weight, Acrobatic category
Maximum weight Normal Category: 1650 lb, Acrobatic Category: 1550 lb
- Seats
- 2
Source for Seats
Number of seats 2
- Baggage limit
- 100 lbnot during aerobatics≈ 45.4 kg (converted)Note 1: baggage must not be carried when performing aerobatics.
Source for Baggage limit
Maximum baggage 100 lb. See Note 1
- C.G. range
Left out. The scan cuts the aft limit lines, so the range is not complete.
Airspeed limits
- Never exceed speed (Vne)
- 175 kt IAS
Source for Never exceed speed (Vne)
(Knots IAS) Never exceed 175
- Maximum structural cruising speed (Vno)
- 122 kt IAS
Source for Maximum structural cruising speed (Vno)
Max. structural cruising 122
- Manoeuvring speed (Va)
- at 1650 lb107 kt IAS
Source for Manoeuvring speed (Va), at 1650 lb
Manoeuvring at 1650 lb 107
- Maximum flap extended speed (Vfe)
- 100 kt IAS
Source for Maximum flap extended speed (Vfe)
Flaps extended 100
Reference
- Datum
- 50.0 inches forward of front face of engine bulkhead
Source for Datum
Datum: 50.0 inches forward of front face of engine bulkhead
- Certification basis
- Commonwealth of Australia Department of Civil Aviation Air Navigation Orders Section 101.1 current at October 1960
Source for Certification basis
Commonwealth of Australia Department of Civil Aviation Air Navigation Orders Section 101.1 current at October 1960.
COCKPIT
The AT-100 limits on an airspeed indicator
Where the sheet gives them in knots, the dial shows Vne as a red line, the caution range from Vno to Vne as a yellow arc, a green tick at Vno and white ticks at the flap limit speeds (Vfe). The sheet gives flap limits, not instrument markings, and the stall speeds where the green and white arcs start are not in it.
- Airspeed indicator
- Attitude indicator
- Altimeter
- Turn coordinator
- Heading indicator
- Vertical speed indicator
- Tachometer
- Oil temperature
- Oil pressure
- Fuel quantity
- Suction gauge
What the dial shows
- Red line: never exceed speed (Vne)175 kt IAS
Source for the red line
(Knots IAS) Never exceed 175
- Yellow arc: caution rangeFrom Vno to Vne, 122 kt IAS to 175 kt IAS
- Green tick: Vno, top of the green arc122 kt IAS
Source for the green tick
Max. structural cruising 122
- White tick: Vfe, a flap limit speed100 kt IAS
Source for the white tick
Flaps extended 100
- Marks are drawn at the sheet's speeds in knots IAS.
- White tick marks the flap limit speed (Vfe) the sheet gives. The sheet gives flap limits, not instrument markings, so the flight manual says where this aircraft's white arc ends.
- The low ends of the white and green arcs are stall speeds. They come from the flight manual, so we have left them unmarked.
The other instruments are drawn at rest and are not linked to this aircraft. Learn what each instrument shows in the cockpit explorer.
For learning only. Not for flight planning or use in flight. Figures are certification limits from Civil Aviation Safety Authority, Certificate of Type Approval Data Sheet 34-1, Revision 2, retrieved 31 October 2026. Conversions marked “converted” are our own arithmetic. No manufacturer images are used. The instruments are drawn by us. Back to all aircraft.