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Learn To Fly Small Planes - Sport Pilot
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| What's All This
About Sport Pilot/Light-Sport Aircraft? |
In 2001, the FAA
confirmed that it would soon propose a major addition to regulations
relating to recreational flying. Called sport pilot/light-sport
aircraft (LSA), the proposal is among the most complex,
far-reaching changes ever to the FARs, and the objective is
to simplify the requirements and reduce the cost for people
who want to engage in aviation as a recreational activity.
Why would the FAA spend great amounts of time
and money on recreational flying? The answer is related to a
declining active pilot population in the U.S. over recent decades.
That is worrisome because unlike in the past, when airlines
and other commercial aviation activity drew most of its pilots
from the military and from pilots trained under the GI
Bill, advancement of pilots into business aviation
today is more often from general aviation sources with students
paying their own way.
The current high cost of training-even for the private pilot
license-and the cost of remaining proficient once licensed is
a major factor in the decline of general aviation flight hours
compared with the 1970s and '80s. |
| Sport Pilot/LSA Origins
Sport pilot/LSA began
in the early 1990s when the ultralight community petitioned
the FAA to liberalize the regulations to allow heavier, faster
and more capable aircraft…and to allow ultralight pilots
to carry a passenger. Instead of taking this route, the FAA
decided to retain the ultralight rule, FAR Part 103, but to
generate an entirely new category of pilot's license and a
new category of aircraft they could fly.
In February 2002, the FAA
released its sport pilot/light-sport aircraft notice of proposed
rulemaking (NPRM) and asked for public comment during a 90-day
period. On May 6, 2002, the public comment period closed with
more than 4000 comments and suggestions logged. After the
final rule is announced-expected by late 2003 or early in
'04-the FAA and the light-aircraft industry expect a major
increase in recreational flight resulting from thousands of
new pilots and new aircraft.
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LSA was defined in the
NPRM as:
"A simple single-seat or two-seat
aircraft with a maximum gross weight of 1320 pounds, a maximum
level speed of 115 knots, a maximum stall speed of 39 knots,
a maximum of one engine, and no complex systems such as in-flight
variable-pitch propellers or retractable gear".
Any aircraft that meets
the definition of a light-sport aircraft as called out in
FAR Part 1.1 is eligible to be operated by a sport pilot.
These aircraft can be certificated in any category, such as
standard, experimental amateur-built, experimental exhibition,
experimental light-sport aircraft (E-LSA), or special light-sport
aircraft (S-LSA).
New categories of aircraft
never before regulated by the FAA would be included. The types
would include airplanes, gliders, weight-shift (powered trikes),
lighter than air (balloons and blimps), gyroplanes and powered
parachutes. Pilots would obtain a logbook signoff from an
instructor for each type of aircraft to be flown.
Light-sport aircraft would
come from four sources:
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Existing certified,
manufactured aircraft that meet the definition. For example,
Piper J-3 Cubs and Aeronca 7AC Champions would qualify
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Amateur-built,
Experimental-category homebuilts that meet the LSA definition.
There are many.
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Light-sport
Special, a new category of factory-built, ready-to-fly
aircraft certified under a new concept termed consensus
standards that would be adopted by the aviation community.
These aircraft could be used in flight training and could
be rented
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Light-sport Experimental,
which would be produced as kits by factories for assembly
by customers. Unlike the amateur-built Experimental category,
however, these kits could be nearly complete by the factory.
They would conform to the consensus standards, but they
could not be used for hire (rental).Consensus Standards?
A key to the success of the proposal is adoption of the required
consensus standards by the manufacturing community and the
FAA before the final rule becomes effective, now expected
sometime in 2004, although details of the final rule may be
announced at any time. The consensus standards requirement
is a major departure (mandated by congressional legislation
in 1996) from the FAA's standard mode of operation, and it
is a huge task for the recreational aircraft industry.
The requirement is for
industry-wide standards for design, manufacturing, testing,
quality assurance, documentation and follow-up support. In
early 2002, EAA proposed engaging ASTM International, an independent,
nonprofit, 100+-year-old test standards organization for administering
the entire consensus standards activity. ASTM does not charge
for its administration and has a long track record of helping
industries develop their own standards. ASTM was elected to
assist, and the process of developing LSA standards began
immediately. The work is conducted primarily by volunteers
using e-mail.
Make/Model
The sport pilot/light sport aircraft NPRM encourages manufacturers
to group together aircraft with similar handling characteristics.
This will enable sport pilots to self-endorse rather than
obtaining an instructor's endorsement for each make and model
of aircraft. Maneuvers specified by the manufacturer in the
pilot's operating handbook must be followed by the sport pilot
to self-endorse prior to carrying a passenger. The Make/Model
Task Group will be meeting at the Marriott Waterside on 19
Nov 2003.
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FAA Definition
of a Light Sport Aircraft
Light-sport aircraft means an aircraft, other than a helicopter
or powered-lift that, since its original certification,
has continued to meet the following:
- A maximum takeoff weight of not more than
- 660 pounds (300 kilograms) for lighter-than-air
aircraft;
- 1,320 pounds (600 kilograms) for aircraft not
intended for operation on water; or
- 1,430 pounds (650 kilograms) for an aircraft
intended for operation on water.
- A maximum airspeed in level flight with maximum
continuous power (VH) of not more than 120 knots CAS
under standard atmospheric conditions at sea level.
- A maximum never-exceed speed (VNE) of not more
than 120 knots CAS for a glider.
- A maximum stalling speed or minimum steady flight
speed without the use of lift-enhancing devices (VS1)
of not more than 45 knots CAS at the aircraft's maximum
certificated takeoff weight and most critical center
of gravity.
- A maximum seating capacity of no more than two
persons, including the pilot.
- A single, reciprocating engine, if powered.
- A fixed or ground-adjustable propeller if a powered
aircraft other than a powered glider.
- A fixed or autofeathering propeller system if a
powered glider.
- A fixed-pitch, semi-rigid, teetering, two-blade
rotor system, if a gyroplane.
- A non pressurized cabin, if equipped with a cabin.
- Fixed landing gear, except for an aircraft intended
for operation on water or a glider.
- Fixed or repositionable landing gear, or a hull,
for an aircraft intended for operation on water.
- Fixed or retractable landing gear for a glider.
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Click here for PDF
file of FAA List of Airplane Sets
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