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A
31ER version followed giving additional fuel capacity increasing the range
to just over 1,500 nautical miles. |
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The
35 is a development of the 25, being stretched by 13inches plus a larger
wingspan and TFE731-2 turbofans. 64 aircraft were built as the basic
35, superseded by 35A. Seating eight passengers, early models have
five starboard windows and four port, whereas later ones have six starboard
plus five port. The 35 first flew on 22nd August 1973. It can carry
up to eight passengers.
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The
35A is an upgraded version of the 35 powered by two TFE731-2-2B engines
and has a range of 2,789 miles plus revised wing giving improved short
field and low speed performance. It first flew in 1976. Over 500
of both variants were built.
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Lear
35A's demonstrating the five starboard, four port window configuration... |
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...and
the six starboard, five port version |
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Built
in a new construction number sequence, the Lear 36 was externally similar
to the 35, but differed in having a larger fuselage fuel tank giving 500
miles longer range but reducing cabin space to six passengers.
<
There are actually five windows on this pictured Lear 36A. The other is
on the right and covered internally! |
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The
36A is an upgraded version with the wing revisions as on the 35A.
64 36's were built in total, including six designated U-36A and used by
the Japanese Self Defence Force as target tugs.
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Japanese
U-36A
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The
Learjet 40 is designed as a replacement for the Lear 31 and is a shortened
version of the Learjet 45, truncated by 25.1 inches. Seating 6 passengers,
there are three fewer windows and a reduced range of 1803nm.
It has been designed as competition to the Citation Encore and is slightly
faster. It first flew on 31st August 2002, the prototype having been converted
from the first Lear 45. First production aircraft flew on 5th September
2002 and certification of the $6.78 million aircraft was achieved in September
2003. . |
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The
Learjet 40XR is an uprated model 40 which was announced at the 2004 NBAA
show. With service entry in 2006, the XR features almost 1000nm
greater range with greater climb and speed over the basic 40. This
is achieved by the use of Honeywell TFE731-20-BR engines, the same as on
the 45XR. Both versions of the 40 remain in production although the
40 is upgradable to XR standard. |
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This
version of the Learjet first flew on 7th October 1996 and is designed to
fit in between the 31 and 60 models, seating up to eight passengers over
ranges of up to 2,200 nm. It is powered by Garrett 731-20AR turbofans.
Although certification took longer than anticipated, around 250 had
been built as of mid 2004. |
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The
Learjet 45XR is a development of the 45, featuring a 1000lb increase in
maximum take off weight, enhanced performance provided by upgraded TFE731-20BR
engines plus new avionics and interior design. Range is 2000nm and
service entry took place in late 2003. Eight passengers can be carried
with full fuel load. There is a subsequent increase in cost of $575,000
to $10.42 million. Existing Lear 45's may be updated to the new specifications. |
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146
of all 55 models were built, these being the basic 55, the B,C and ER (2).
The aircraft is larger in dimensions than the 35 and first flew on 19th
April 1979, carrying the supercritical wing of the Lear 28. The ER is an
extended range version. There are four square windows on each side
and power comes from two Garrett TFE731-3A turbofans. Range is around 2,492
miles and up to eleven passengers can be accommodated. 126 of the
basic 55 were produced. An LR variant gave extra fuel capaity with
a reduced passenger load of seven with the XLR reducing this to six with
even more fuel. Initially, three models were envisioned, the 54, 55 and
56. However, the 54 and 56 designations were later abandoned leaving
the 55 as the base model. |
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This
is an improved 55 featuring an electronic cockpit, new systems and autopilot
plus thrust reversers and an increased gross weight. Eight were built
of this variant. |
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Similar
to the 55, but with the two ventral fins that were to become standard on
the Lear 60. It is powered by two TFE731-3A turbofans and can carry
up to eight passengers over a greater distance than the basic 55
model. 14 were built in total. An ER version gave a range of 2,079nm
and an LR version gave 2,052nm. |
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In
1992 the Lear 55 was replaced by the 60 using a new c/n sequence.
Differences
include the two delta the fins on the lower rear fuselage and a 43
inche
stretch. The 60 first flew on 13th June 1991. Up to ten
passengers
can be carried in this Pratt & Whitney PW305 powered aircraft of
which 293 had been produced by the time it was seperseded by the 60XR. |
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Announced
at the NBAA show 2005, the Lear 60XR replaced the standard 60 in
production
in early 2007. The first airframe to be built as such was no 294.
Improvements include an upgraded interior and new
avionics plus P&WC PW305A engines giving a speed of M079 and a
range
of 2451nm. This version first flew on 3rd April 2006 with
certification achieved on 28 September 2006 and first delivery made in
August 2007, six months later than planned.. |
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Announced
in October 2007, the Learjet 85 is sized between the Lear 60 and
Challenger 300 and features seating for ten with a 3000nm range and
M.82 speed. Powered by Pratt and Whitney Canada PW307B engines giving 6,100lb of thrust, the aircraft will be built wholly of composite materials in conjunction with Grob Aerospace.
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Around
80 of the Lear 35A are operated by the United States Air Force as VIP transports,
designated the C-21A. Additionally, several are flown by the Brazilian
Air Force as the C-35A. |
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