Model in Service Crew & Engines Total Mil. Remarks

MODEL |IN SERVICE |CREW & |ENGINES |TOTAL |MIL. |REMARKS

|OR FIRST FLIGHT|PAX MAX | |BUILT |EQUIV|

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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 . .

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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 . .

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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 | . | .

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. 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

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60 . 13.06.1991 | 2+8 |2xPWC PW305 | 379 | . |= 55. 43 INCH |LONGER

. |FBW GROUND STEERING

...... 1992 . . . . REPLACED MODEL 55

...... 1997 . . 314 . .

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. 60SE ...... 1997 . . 39 . INCLUDED IN LJ60

SPECIAL EDITION

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. 60XR ...... 2005 2+7 2xPWC PW305A . . PROJECT LAUNCHED

03.04.2006 2+7 . . . FIRST FLIGHT

...... 2007 2+7 . . . FIRST IN SERVICE

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75 |2015

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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