Learjet 23
1963
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Learjet 23

The Swiss FFA P-16 jet fighter, cancelled by the federal government in the late 1950s, caught the attention of Bill Lear Snr, who saw in it the basis for a twin-jet executive aircraft. He initiated preliminary design work at St Gallen, Switzerland, in November 1959 and sold his electronics company to the Siegler Corporation. Lear then formed the Swiss American Aviation Corporation to develop the aircraft, known originally as the SAAC Lear Jet 23. An important objective was to keep the aircraft's gross weight below 5670kg so that it would qualify for single-pilot operation under FAA CAR.3 regulations and for air taxi operations without requiring CAB approval.

In August 1962, after the design had been finalised and tooling was in progress, Lear transferred the project to Wichita, Kansas, and renamed the organisation the Lear Jet Corporation. In every way a stylish aircraft reflecting its fighter origins, the Learjet 23 marked a new era in 'bizjet' design, offering very high performance - if not much headroom.

The prototype made its first flight on 7 October 1963, the second and third aircraft being flown on 5 March and 15 May 1964 respectively. Following the receipt of certification on 31 July the first production Lear Jet 23 was delivered on 13 October 1964 to the Chemical and Industrial Corporation of Cincinnati, Ohio. Despite the fact that the Lear Jet was considerably smaller than the piston-engined aircraft that it was designed to replace, it more than made up for this in performance, and though intended for single-pilot operation the basic layout was for a crew of two and for five to seven passengers. The first 30 production aircraft to be completed were powered by 1293kg thrust General Electric CJ610-1 turbojets, but the remainder of the production run of a little over 100 Lear Jet 23s had CJ610-4s of similar thrust.

Learjet 23


Specification 
 ENGINE2 x General Electric CJ610-4 turbojets, 1293kg
 WEIGHTS
    Take-off weight5670 kg12500 lb
    Empty weight2790 kg6151 lb
 DIMENSIONS
    Wingspan10.85 m35 ft 7 in
    Length13.18 m43 ft 3 in
    Height3.84 m12 ft 7 in
    Wing area21.46 m2230.99 sq ft
 PERFORMANCE
    Max. speed903 km/h561 mph
    Cruise speed781 km/h485 mph
    Ceiling13715 m45000 ft
    Range2945 km1830 miles

Comments 
Fred Martin, fredf658(@)aol.com, 23.07.2008

The Lr23 gross wt. was 12,499lb. We first gave a letter of competency to pilots who passed the flight check in the aircraft. The letter could be used to add a type rating when the aircraft became a type rating aircraft. Myself, Ansil McAllister and Ed King were the first FAA Inspectors that started the Lear check outs. Our ground school was at the factory. Paul Donohoe from EJA in Coumbus, OH gave us our flight training. A great and enjoyable aircraft. Fred

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