I keep running into this sort of scenario on the boards, here may be a solution no one will like.
BACKGROUND Short Story
Let’s start back in the days when GA had the Piper Tomahawk which came into Australia around 1975. Pipers version of a two seat (specs below) trainer for GA against the Cessna 150.
Now what is so very interesting is that this beastie was a widow maker and spun at the drop of a hat.
Long story short - After killing a few people in USA and here -- “it was then a requirement that ALL students before they go solo got a spinning endorsement” in Australia.
That’s right teach them to do full spins and recover before solo, which was not hard at all in the traumahawk as it was known back in the day.
Full power stall was all it needed or a low speed turn with speed bleeding off and you could see the earth rotate in front of your face if you were high enough, if not you were dead.
What it did teach, ‘STUDENTS, Pilots and Instructors’ was a VERY, VERY, Extremely (get the point) healthy respect for height, angle of bank and speed which was magnified in the circuit area and during practice engine failures with all students and instructors knowing the cause and to recognize the feel of the aircraft, with quick and correct recovery procedure even before "it developed". Flying this beast all those years ago and still today no matter what aircraft I am in GA or RAA, I always have this healthy respect of speed and angle of bank at or below circuit height from flying this beast.
Learning how to spin in a GA aircraft teaches also - - ‘As a Secondary Effect’ - galvanizes the voice in the back of your head if you have an engine failure at take of -NOT TO TURN BACK – AND LOWER THE NOSE QUICKLY - AND FLY THE AIRCRAFT.
Here’s The Problem - some people are terrified OF STALLS AND SPINS and they may give up flying. Also in that case should people be allowed to hold a license – but that’s another can of worms for another day.
As it not you we may care for but your passager!
THE ANSWER for RAA - you will not like it - Get a GA spin endorsement or do some time in a GA spin endorsed aircraft with an instructor and learn all there is to know about stalls and spins. You will never forget it and then hopefully you will never be a number with CASA. (please don’t tell me it can’t happen to you in your RAA aircraft, saying it just won’t spin. It does not have to spin it only needs to stall at the wingtip and you are gone).
With some old and the new faster aircraft being built and flying around it may be worth you time to think about it!
So should RAA pilots and GA coming into RAA get spin endorsed? That is the real question?
Also
Some comments below from guys who flew the tomahawk back in the day!
The Tomahawk was changed structurally so much between it;s certification flight tests and production, that the Piper Engineers and Test Pilots said it is NOT THE AIRPLANE WHICH WAS CERTITIFED !. Piper had modified the wing after and made it more flexible.
2. Spin recovery is extremely difficult. In the context of a approach stall/spin recovery it IS impossible.
3. The accident record of the Tomahawk as a trainer was appalling, and the industry that buys them ran the other way screaming. Many airplanes today are placarded against spinning, including the Bellanca which has been used successfully in airshow routines. Nobody in his right mind would want to get anywhere the limits in the tomahawk .
Being proficient in a fair airplane beats being incompetent in the best one.
Specifications for Piper Tomahawk (could be a RAA aircraft if we get 750kg )
Crew: 2
Length: 23 ft 1¼ in (7.04 m)
Wingspan: 34 ft 0 in (10.36 m)
Height: 9 ft 0¾ in (2.76 m)
Wing area: 124.7 ft² (11.59 m²)
Airfoil: NASA GAW-1
Empty weight: 1,128 lb (512 kg)
Max. takeoff weight: 1,670 lb (757 kg)
Engine: Avco Lycoming O-235-L2C air-cooled flat-four piston engine, 112 hp (83.5 kW)
Performance
Never exceed speed: 159 mph (138 knots, 256 km/h)
Maximum speed: 126 mph (109 knots, 202 km/h) at sea level
Cruise speed: 115 mph (100 knots, 185 km/h) at 10,500 ft (3,200 m) (65% power)
Stall speed: 56.5 mph (49 knots, 91 km/h) (IAS), flaps down
Range: 539 miles (468 nmi, 867 km) at 10,500 ft (3,200 m), (65% power)
Service ceiling: 13,000 ft (4,000 m)
Rate of climb: 718 ft/min (3.65 m/s)