MODEL |IN SERVICE |CREW & |ENGINES |TOTAL |MIL. |REMARKS
|OR FIRST FLIGHT|PAX MAX | |BUILT |EQUIV|
------|------|------|------|------|-----|------
21.12.2015 4 PAGES
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ANDRE DILLIEN
RUE DES CYCLAMENS, 6
BE-1170 BRUXELLES
TEL/FAX 02 673 3632
MISE A JOUR MENSUELLE SUR HTTP://WWW.BAMFBAMRS.BE/DILLIEN
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LEARJET
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PROPRIETAIRES:
1 ...... 1922 RADIO WIRE AND COIL COMPANY
2 ...... 1930 LEAR INC
3 ...... 1950 MERGED WITH SIEGLER CORPORATION
LEAR INC. CONVERSION OF LOCKHEED LODESTAR TO LEARSTAR
4 ...... 1960 SWISS AMERICAN AVIATION CORPORATION
5 ...... 1962 LEARJET CORPORATION, WICHITA
6 ...... 1966 LEAR JET INDUSTRIES
7 10.04.1967 GATES RUBBER COMPANY CONTROLLING INTEREST
8 ...... 1969 GATES LEARJET CORPORATION
...... 1986 SE DEBARRASSE DE PIAGGIO (AVANTI 180)
9 29.06.1990 LEARJET INC., DIVISION OF BOMBARDIER INC. CANADA
10 ...... 2000 BOMBARDIER LEARJET
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23 ...... 1960 - . . . PROJECT DERIVED FROM
SWISS FFA P-16,
LATER NAMED SAAC23
16.09.1963 ROLLED OFF
07.10.1963 2+7 1° 2xCJ610-1 1 . FIRST FLIGHT
12500 LB TOGW
. 04.06.1964 2+7 2° 2xCJ610-4 . PROTOTYPE W/O
. 105 . .
------
24 ...... 1966 2+6 2xCJ610-4 11 . NEW WINDSHIELD
. & TIP TANKS
. 13000 LB TOGW
. EX MODEL 23
. 24A ...... 19.. 2+6 2xCJ610-6 81 . = 24
. 12499 LB TOGW
. 24B ...... 19.. 2+6 2xCJ610-6 49 . 13500 LB TOGW
. REVISED SYSTEMS
. REVISED INTERIOR
. 24BA ...... 19.. 2+6 2xCJ610-6 69 . 12500 LB TOGW
. 24C ...... 19.. 2+6 2xCJ610-6 . . = 24B ECONOMY MODEL
. REDUCED RANGE
. NO FUSELAGE TANK
. 3 WINDOWS LEFT RIGHT
. 12500 LB TOGW
. 19.07.1969 2+6 COMBINED WITH 24C
LAST BUILT IN 1970
. 24D ...... 1974 2+6 2xCJ610-6 325 . = 24C. 13500 LB TOGW
. 24E ...... 1975 2+6 2xCJ610-6 {29 . = 24C. FOR AIR TAXI
. 24F ...... 19.. 2+6 2xCJ610-6 { . = 24D. & ADDITIONAL
FUSELAGE TANKS
. 24XR ...... 2+6 2x 207 . .
------
25 ...... 1965 2+4 . . . PROTOTYPE
. . 12.08.1966 2+8 2xCJ610-6 64 . STRETCHED MODEL 24
. 25A NIL . . . . PROJECT NOT BUILT
. 25B ...... 1969 2+8 2xCJ610-6 {136 . = LJ25 4 WINDOWS L/R . { 910 US GALLONS
. 25C ...... 1973 2+8 2xCJ610-6 { . = 25B. SHORTER CABIN
. 1103 US GALLONS
. 25D ...... 1973-1979 2+8 2xCJ610-8A {319 . = 25B. NEW WING
. 15000 LB TOGW.
. 25E NIL . . . . PROJECT NOT BUILT
. 25F ...... 1973 2+8 2xCJ610-8A . . = 25D.
. INCREASED FUEL RANGE
. 25G . 2+8 2xCJ610-8A . . = 25D. 16300 TOGW
. NEW WING
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26 . NIL . . . . PROJECT NOT BUILT
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27 . NIL . . . . PROJECT NOT BUILT
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28 . 24.08.1977 2+4 2xCJ610-8A . . PROTOTYPE
1340 KGP/13 KN
. . 21.08.1978 2+8 2xCJ610-8A 5 . = 25D NO TIP TANKS
. SUPER CRITICAL WING
. WHITCOMB WINGLETS
. CEILING 51000 FT
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29 . 1978 2+8 2xCJ610-8A 4 . = 28 LONG RANGE
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30 . 11.05.1987 2+8 2xTFE731-2 . . = 35. MODEL 55 WINGS
. WINGLETS
. NO TIP TANKS
. REAR FUSELAGE DELTA
. FINS. 5 PORT WINDOWS
. 6 STARBOARD WINDOWS
. MAXIMUM 1202 NM
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31 . 09.1987 . . 34 . PROJECT NOT BUILT
. 31A ...06.1991 2+8 . 319 . = 31. EFIS COCKPIT
...... FBW GROUND STEERING
...... SPEED 0.81 MACH
2xTFE731-2-2B 1588
KGP
...... 2003 . . . . OUT OF PRODUCTION
. 31ER ...... 1991 2+8 . . . = 31. 1526 NM RANGE
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35 ...... 1991 2+6 2xTFE731-2 66 . = 25. TURBOFANS
. 13 INCH LONGER
. 17000 LB TOGW
. LONG RANGE 5 HOURS
. 35A ...... 1980-1991 2+6 2xTFE731-2 609 C21A = 35. NEW WING
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36 ...... 2+6 2xTFE731-2 17 . = 35. 18000 LB TOGW
. LONG RANGE
. 36A ...... 1985 2+4 2xTFE731-2 43 . = 36.
. WING OF 35A
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40 . NIL . . . . PROJECT NOT BUILT
. LEAR LINER 28 PAX
2xROLLS ROYCE SPEY JUNIOR 5170 KGP
. 40XR ...01.2004 2+4 2xHONEYWELL TFE731-20BR XR = EXTENDED RANGE
------|------|------|------|------|-----|------45 . | 07.10.1992 | 6-10 |2xTFE731-20 | 404 |. |NEW WING. 8 WINDOWS
. | 07.10.1975-FF | |19500 LB TOGW
. . | ...... 1996 | . . . . |COMMERCIAL
DELIVERIES
. 45XR| ...06.2004 | . . . . XR = EXTENDED RANGE ------|------|------|------|------|-----|------
50 . NIL . . . . PROJECT 50 NOT BUILT
------|------|------|------|------|-----|------54 . | NTU | 2+8 |2xTFE731-3- |ZERO | . | = 50. WINGS OF
. | 100B | |MODELS 28 & 29
. |866 US GALLONS
------|------|------|------|------|-----|------55 ...... 1977 | 2+5 |2xTFE731-3 | . | . PROJECT
FF 19.04.1979 | 2+8 |2xTFE731-3A |126 | . = 50
-> 1982 | = 54
|1001 US GAL.
...... 1991 . . |147 | . | .
------|------|------|------|------|-----|------
. 55B . 2+8 2xTFE731-3A |8 . = 55. EFIS
. NEW AUTOPILOT
. THRUST REVERSERS
------|------|------|------|------|-----|------. 55C | . | 2+8 | 2x | . | . | .
------|------|------|------|------|-----|------. 55LR ...... 1982 2+5 2xTFE731-3A . . = 55. 1141 US GAL.
. 55XLR . 2+4 2xTFE731-3A . . = 55. 1231 US GAL.
. 55C ...... 1988 2+8 2xTFE731-3A-2B 11 . = 55B. DELTA FINS
. NEW ENGINE PYLONS
. 55CER ...... 1983 2+8 2xTFE731-3A 2 . = 55B. 2079 NM
. 55CLR ...... 2+8 2xTFE731-3A . . = 55B. 2052 NM
. DISCONTINUED 1991
------|------|------|------|------|-----|------
60 . 13.06.1991 | 2+8 |2xPWC PW305 | 379 | . |= 55. 43 INCH |LONGER
. |FBW GROUND STEERING
...... 1992 . . . . REPLACED MODEL 55
...... 1997 . . 314 . .
------|------|------|------|------|-----|------
. 60SE ...... 1997 . . 39 . INCLUDED IN LJ60
SPECIAL EDITION
------|------|------|------|------|-----|------
. 60XR ...... 2005 2+7 2xPWC PW305A . . PROJECT LAUNCHED
03.04.2006 2+7 . . . FIRST FLIGHT
...... 2007 2+7 . . . FIRST IN SERVICE
------|------|------|------|------|-----|------
75 |2015
------|------|------|------|------|-----|------
85 . |...... 2008 |2+6 |2xPWC-PW307B . . PROJECT ALL
COMPOSITE
BOMBARDIER-GROB
|...... 2013 | EXPECTED IN SERVICE
|...... 2015 | TOTAL 1 – PROJET ABANDONNÉ
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600 ...... 19...... LEARSTAR
PROJECT FROM WILLIAM
P. LEAR , SR
...04.1976 . . . . RIGHTS ACQUIRED BY
CANADAIR
08.11.1978 . . . . RENAMED CL600
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2100 ...... LEARFAN
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CONVERSIONS:
DEE HOWARD XR . . . . SWEPT WING CENTER
SECTION.
LONGER RANGE
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18-12-15 Page 4 of 4 Dossier: AVION-LEARJET