LEAR
JET HISTORY
For many people, the name Learjet is a generic term to cover any and all
business jets, largely due to the public relations skill of Bill Lear,
and James R. Greenwood, who successfully headed the company's public relations
department for many years.
The name comes
from Missouri native William Powell. Lear - a prolific inventor whose
achievements included the first successful car radio, the first eight-track
stereo tape system, navigational radio systems and direction finders for
civil and military aircraft.
Bill Lear formed
the Radio Wire and Coil Company in 1922, created Motorola Corporation
and founded Lear Inc., which later merged with the Siegler Corp in the
1950s. - Lear Inc. became known for its conversions of Lockheed Loadstars
to executive Learstar configuration.
In 1959, Bill
Lear embarked on his most famous development - the Learjet. He had sold
out his interest in Lear Siegler. for $ 12.5 million and "retired" to
Switzerland where he conceived the design of a small jet business aircraft
and set up the Swiss American Aircraft Corporation. Much of the SAAC-23
At the urgining of Bill Lear Jr, his son, the Learjet design was based
on the single-seat FFA P-16 (P-1604) fighter-bomber which had been flown
in prototype form by the Flug und Fahrzeugwerke A.G. in April 1955. (Five
P-16s were built before the project was discontinued.)
Model |
Number
Built |
Construction
Numbers From |
To |
Notes |
23 |
105 |
23-001 |
23-099 |
Also
c/n 015A, 028A, 045A, 050A, 065A, 082A. Some conv. to Model
24 |
24
& 24A |
81 |
24-100 |
24-180 |
Model
24 and 24A, mixed |
24B |
49 |
24B-181 |
24B-229 |
24D |
99 |
24D-230 |
24D-328 |
24E
& 24F |
29 |
24E-329 |
24F-357 |
Model
24E and 24F, mixed |
25 |
64 |
25-001 |
25-064 |
c/n
25-065 to 25-069 not built |
25B
& 25C |
136 |
25C-070 |
25B-205 |
Model
25B and 25C, mixed |
25D |
168 |
25D-206 |
25D-373 |
28 |
5 |
28-001 |
28-005 |
29 |
2 |
29-001 |
29-002 |
31 |
34 |
31-001 |
31-034 |
31A |
220+ |
31-035 |
31-099 |
Current
production |
35 |
66 |
35-001 |
35-066 |
35A |
609 |
35A-067 |
35A-676 |
36 |
17 |
36-001 |
36-017 |
36A |
43 |
36A-018 |
36A-060 |
45 |
145+ |
|
|
Current
production |
55 |
126 |
55-001 |
55-126 |
Includes
two Model 55ER |
55B |
8 |
55B-127 |
55B-134 |
55C |
13 |
55C-135 |
55C-147 |
60 |
220+ |
60-001 |
60-043 |
Current
production |
Lear
moved back to the United States in 1962 to set up development and production
of his Learjet and settled on Wichita, Kansas as the base for operations.
In October 1963, the prototype Learjet Model 23 made its first flight
Wichita's Mid-Continent Airport. This aircraft crashed during testing
in the following June but, nevertheless, the type certificate under FAR.
Part 23 was granted on July 31st 1964. Lear Jet Corporation quickly put
the Model 23 into production and, with a price lower than the competing
aircraft, it was an immediate success.
However, it did gain a reputation for being very demanding for the average
pilot and much of the later Learjet development concentrated on improvement
to the low-speed handling characteristics of the type following an initial
rash of accidents.
The Model 23
was replace by the Model 24 in 1966. This was a considerably modified
development to meet FAR. Part 25 certification requirements. It was soon
joined on the production line by the stretched Model 25 with a maximum
on ten seats - still powered by General Electric CJ610 engines.
Both were offered
in alternative long-range versions with reduced passenger capacity. Bill
Lear also designed the Model 40 Lear Liner seating 28 passengers and using
the same jet engines adopted by Grumman for the Gulfstream II, but this
project was discontinued as financial pressures increased.
In 1966, the
name of the company was changed to Lear Jet Industries and on April 10th
1967, the Gates Rubber Company brought a controlling interest. The Learjet
was undoubtedly successful, but enormous operating losses had built up.
The 1966 acquisition
of Brantly Helicopters and the subsequent development cost of the Gates
Twinjet Helicopter (an aircraft of Sikorsky S-76 size) only served to
fuel the financial crisis.
On April 2nd
1969, Bill Lear resigned as Chairman of the Board. He went on to develop
the LearAvia steam powered car, the Learstar 600 (later to become the
Canadair Challenger) and the revolutionary Learfan - before his death
on May 14th 1978.
Gates renamed
the company Gates Learjet Corporation and, in 1969, sold Brantly to Aeronautical
Research and Development Corporation.
Increasing
pressure from the environmentalist lobby and competition from the Cessna
Citation now prompted the company to refit the Learjet with turbofan engines.
This resulted in the Models 35 and 36 - both based on the Model 25 with
a small fuselage stretch and a pair of Garrett TFE731 engines.
Following the
previous formula, the Model 35 was a short-range aircraft and the Model
36 was its long-range sister. In practice, the Model 35 outsold the Model
36 by two-to-one because the five-hour endurance of the long-range model
was more than most customers required.
| A
detailed list of models built by Learjet is as follows:
|
Model |
Notes |
| 23 |
Original
Learjet to FAR.23 with 12,500 lb. TOGW, powered initially by two
CJ610-1 turbojets the, from c/n 23-028, by CJ610-4. 8-place max.
seating. Prot. N801L (c/n 23-001) FF.7 Oct.1963. w/o 4 Jun.1964. |
| 24 |
Model 23
certified to FAR.24. Redesigned windshield and tip tanks, new
engine fire control system and 13,000 lb. TOGW. CJ610-4 engines.
11 aircraft converted from Model 23 to Model 24 or 24A. |
| 24A |
Model 24
with optional 12,499 lb. TOGW at lower fuel load. 24B Model 24
with 13,500 lb. TOGW and revised systems and interior. Powered
by CJ610-6 engines. Model 24B-A has 12,500 lb. TOGW. |
| 24C |
Economy
Model 24B with no fuselage tank and reduced range and performance.
Three rectangular windows each side, no tail "bullet" fairing,
12,499 lb. TOGW. |
| 24D |
Model 24C
with 13,500 lb. TOGW and increased range. |
| 24E |
24C with
minor changes for air taxi work. |
| 24F |
24D with
additional fuselage fuel tank. |
| 25 |
Stretched
Model 24 with CJ610-6 engines and 52-inch fuselage plug to give
10-place interior. Prot. N463LJ (c/n 25-001) FF.12 Aug, 1966. |
| 25B |
Model 25
without tail "bullet" fairing and four rectangular cabin windows
each side. 910 U.S. gal. fuel capacity. |
| 25C |
Long-range
Model 25B with shorter passenger cabin and additional fuselage
fuel tank to give max 1,103 U.S. gal. fuel capacity. |
| 25D |
Model 25B
with CJ610-8A engines, and new wing to improve short field and
low speed performance. FAR.36 noise standard approved. 15,000
lb. TOGW. |
| 25E |
Not built.
"E" suffix not used due to "Economy" implication. |
| 25F |
Model 25D
with eight-place seating and increased fuel/range. |
| 25G |
Model 25D
with 16,300 lb. TOGW, higher range and wing modifications. |
| 26 |
Proposed
Model 23 with TFE731 engines. Not built. |
| 28
|
Model 25D
with supercritical wing, no tip tanks and Whitcomb winglets. 10-place
seating. Operating ceiling raised to 51,000 ft. Prot. N9RS (c/n
28-001). FF. 21 Aug, 1978. |
| 29 |
Long-range
version of Model 28. |
| 30 |
Model 35
with Model 55 wings incorporating winglets (but without tip tanks)
and rear fuselage delta fins. Powered by two TFE731-2 turbofans.
Five Port and six starboard cabin windows. Max range 1,202 naut.
miles. Prot. N311DF (c/n 31-001) FF. 11 May, 1987. |
| 31A |
Model 31
with new EFIS cockpit and avionics, FBW ground steering, increased
(Mach 0.81) speed. Replaced Model 31 in mid 1991. |
| 31ER |
Model 31
with additional fuel to give 1,526 NM range. |
| 35 |
Model 25
with 13-inch fuselage stretch, increased wingspan and two Garrett
TFE731-2 turbofans. 17,000 lb. TOGW. eight-seat cabin with various
window arrangements (max. six starboard, five port windows). |
| 35A |
Model 35
with redesigned wing resulting in better short field and low speed
handling. |
| 36 |
Long-range
Model 35 with six-seat cabin, increased fuel, 18,000 lb. TOGW. |
| 36A |
Model 36
with same wing modifications as Model 35A |
| 40 |
Lear Liner
project. Not built. |
| 45 |
New mid-sized
Learjet with redesigned wing, 8-10 passenger seating, eight windows
each side, 19,500 lb. TOGW and two 3,500 lb.s.t TFE731-20 turbofans. |
| 54 |
Enlarged
Learjet with 10-passenger cabin using 28/29 wing married to new
fuselage and powered by two TFE731-3-100B engines. Short-range
version of '50 series with 866 U.S. gal fuel. |
| 55 |
Main production
'50 series. Similar to Model 54 with 1,001 U.S. gal fuel capacity.
Powered by two TFE731-3A turbofans. Prot. N551GL (c/n 55-001)
FF. 19 Apr, 1979. |
| 55B |
Model 55
with electronic flight instrumentation, new autopilot, increased
gross weight, systems changes and thrust reversers. |
| 55LR |
Model 55
with seven-passenger cabin and 1,141 U.S. gal. fuel capacity. |
| 55XLR |
Model 55
with six-passenger cabin and 1,231 U.S. gal. fuel capacity. |
| 55C |
Model 55B
with delta fins similar to those on the Model 31 and redesigned
engine pylons. Also Model 55C/ER with 2,079 naut. mile range and
55C/LR with 2,052 NM range. Discontinued, 1991 and replace by
Model 60. |
| 60 |
10-passenger
development of Model 55 with 43-inch fuselage stretch, two 4,600
lb.s.t Pratt & Whitney Canada PW305 turbofans, electronic
FBW ground steering etc. Prot. N60XL (c/n 55-001) FF. 13 June,
1991. Replaced Model 55 in 1992. |
The
next major development for the Learjet was the introduction of the "longhorn"
wing - first tested on a Model 25, N266GL (c/n 25-064) and a model 24,
N682LJ (c/n 24B-218). The NASA-designed supercritical wing was fitted
with winglets and the tips - and as a consequence all fuel had to internally
housed due to the deletion of the wingtip tanks.
First production aircraft to be fitted with the winglets were the Models
28 and 29 - respectively short and long range variants. Very few were
built - largely because they were still powered by the CJ610 turbojet
engine, a power plant soon to be phased out.
The Longhorn wing was mainly intended for the new, larger, Model 54/55/56
series of Learjets. With the same wing attach points as the Model 20 and
30 series, these aircraft were designed to meet customer requirements
for a larger Learjet cabin. They were scaled up versions of the previous
types with a stand-up cabin capable of carrying up to ten passengers in
addition to two crew.
Most orders were for the mid-range Model 55 - and the Model 54 and 56
designations were later abandoned. The final version was the Model 55C
introduced in 1988 with "delta fins" mounted on the lower rear fuselage
to improve low-speed handling but this model has now been replaced in
production by the Model 60.
Also introduced at the same time was the Model 31 which is a Model 35
with delta fins and the Longhorn wing, aimed at users stepping up into
jet aircraft for the first time. Learjets latest aircraft is the completely
new Model 45, which was announced in September 1992, falling between the
Model 31 and the Model 60, and features a new wing and a larger fuselage
than the Model 31.
The Model 45 made its first flight on October 7th 1995 exactly 32 years
after the first Learjet took to the skies.
Learjets have been delivered to a number of governmental operators and
have been used for target towing, high altitude mapping and photography.
Foreign air forces that have bought Learjets, include Bolivia, Ecuador,
Argentina, Mexico, Peru and Yugoslavia. The U.S. Air Force has acquired
Learjet 35As, designated C-21A, for personnel transport, communications,
medical evacuation and high priority cargo duties, replacing obsolescent
T-39A Sabreliners.
International records achieved by Learjets include the first round-the-world
flight by a business jet (which included this writer as part of the four
man crew), a standard production Model 24 traveled 22,993 miles in 50
hours 20 minutes flying time, with a total elapsed time of 65 hours, 4
minutes. The crew included Hank Beaird, John Lear (Bill's son), John Zimmerman
and Rick King.
Zimmerman's role was to take care of all required paperwork activity and
all photos at each of the 18 stops. The Model 24 Learjet was the first
unit in the series (N427LJ) and made the flight May 23-26, 1966.
A number of special conversions have been carried out on Learjets, particularly
the Dee Howard XR modification which includes a new swept wing center
section, wing leading edge, and engine pylons so as to improve high speed
performance, increase useful load and give longer range.
In 1976, Gates Learjet relocated a significant part of its production
in Tucson while continuing with some completion, service and marketing
functions in Wichita. With the slow-down in the business jet market, Learjet
sales fell and Gates came under pressure over the financial position.
In August 1987 Gates announced that it would sell its 64.8% interest in
Gates Learjet to Integrated Acquisitions Inc., a wholly owned subsidiary
of Integrated Resources Inc., of New York. This led to the moving of most
production from Tucson back to Wichita.
In mid-1989 a financial crisis in its property business forced Integrated
Resources to seek buyers for Learjet once again. On June 29th 1990, it
was acquired by the Canadian company, Bombardier Inc. and the name was
changed to Learjet Inc., a division of Bombardier.
According
to the records of AvDataInc, Wichita, KS the world Learjet operational
fleet at beginning of July 2001 was:
| Learjet
23 |
32 |
| Learjet
24 |
210 |
| Learjet
25 |
311 |
| Learjet
28 |
5 |
| Learjet
29 |
4 |
| Learjet
31 |
221 |
| Learjet
35 |
632 |
| Learjet
36 |
55 |
| Learjet
45 |
138 |
| Learjet
55 |
140 |
| Learjet
60 |
209 |
| TOTAL |
1,957 |
|