Aircraft Data File 46718

8/12/2019 Aircraft Data File 46718

1/18

C

AIRBUS 300 SHOWN

Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location

D

D

D

AA

D

BE

{1} Jack incorporates telescoping legs. Set jack in extended position for this application.

AIRBUS 300 / 310

AIRCRAFT / JACK DATA

MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA

{2} Specify with leg extensions.

{3} Lift provided by 65P10 or 65P10AR axle jack.

REVISED DATE: JUNE 23, 1998

AIRCRAFT DATA MALABAR JACK MODELS AND DATA

A

B

REF.

Main Wing:Gear Swing

Main Wing:Oleo Removal

Forward:Gear Swing

44.1(40.0)

14.1(12.8)

MAX.JACKLOAD

MLG:Routine

MLG:Flats

ENLG:Flats

C

5.5(5.0)

LOCATION &SERVICE

Forward:Oleo Removal

64.7

(58.7)

24.8(22.5)

NLG:Routine

D

Aft (A310):Gear Swing

5.5(5.0)

Aft (A300):Gear Swing

793 {1}

65P10AR

733

8487A {2}

8487A

65P10AR

65L4.5 {3}

220

(5588)

14.37(365)

16.97(431)

215.65(5478)

162.46(4126)

138.46(3517)91.30

(2319)

157.24

(3994)

191.65(4868)

DISTANCEBETWEEN

TIRES

MIN.HT.

MAX.HT.

192.00(4877)

20.47(520)

17.28(439)6.20

(157)6.54(166)

11.38(289)

8.66(220)

13.40(340)

8.77(223)

193.00(4902)

163.66(4157)

218.00(5537)

17.5(445)

0 22(559)

4.5(114)

65(59)

65(59.0)

10.25(260)

32(813)

160(4064)

72(1829)

87(2210)

12(305)

171(4343)

30(27.2)

16

(406)

100

(90.7)

132

(3353)

72

(1829)

4.75(121)

11(279)

5(4.5)

228(5791)

8(203)

188(4775)

CAP.MAX.HT.

SCR.EXT.

HYD.LIFT

MIN.HT.

26(660)

26(660)

4.75(121)

11(279)

10.25(260)

65(59)

32(813)

8(203)

200(5080)

5(4.5)

MODEL

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. All tires at normal inflation pressure.

Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).

Caution: Aircraft manufacturer's specifications and instructions must be followed. In the event ofcontradiction between aircraft manufacturer's specifications and Malabar's, aircraft manufacturer'sspecifications will prevail.

Notes:

FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART


2/18

MLG DOUBLE AXLE SHOWN

E E

C

D

D

F

B

A

D

A

D



AIRBUS 319 / 320 / 321




Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tire 49 x 19-R20. Nose gear tire 30 x 8.8. All tires at normal inflation pressure.

{2} For roll-under clearance, oleos may have to be extended.

{1} Clearance between drag link bolts.

{5} Lift provided by 65P10 or 65P10ARaxle jack.

{4} Jack capable of 22 tons(20 metric tons).


NLG:Flats

NLG:Routine

MLG SingleAxle: Routine

MLG DualAxle: Flats

MLG DualAxle: Routine

MLG SingleAxle: Flats





Forward:Gear Swing

LOCATION &SERVICE


Aft:Oleo Removal

Aft:Gear Swing

17.5(445)

4.5(114)

65(59)

0 22(559)

65L4.5 {5}8.58(218)

50P9AR

8732 {4}

714A

8721 {2}

MALABAR JACK MODELS AND DATA

MODEL

50P9AR

713A {3}

8722

8731

B64.96(1650)

7.6(6.9)

F

Notes:

E

C

D

A

REF.

9.50(241)

6.53(166)

13.8(12.5)

7.80(198)

12.83(326)

23(584)

9.75(248)

4.13(105)

50(45.4)

9.13(232)

5.51 {1}(140)

123.90(3147)

6.0(5.4)

151.03(3836)

14.96(380)

21.73(552)

16.10(409)

123.22(3130)

7.09(180)

20.9(19.0)

10.63(270)

13.70(348)42.4

(38.5)

175.08(4447)

173.23(4400)

32.0

(29.0)

145.67(3700)

95.67(2430)

113.78

(2890)

DISTANCEBETWEEN

TIRES

MIN.HT.

MAX.HT.

MAX.JACKLOAD

AIRCRAFT DATA

23(584)

50(45.4)

9.75(248)

4.13(105)

9.13(232)

120(3048)

10(254)

174(4420)

12(10.9)

44(1118)

6(5.4)

187(4750)

10(254)

120(3048)

57(1448)

20(18.1)

6(152)

8.5(216)

2.5(64)

17(432)

10(9.1)

138(3505)

10(254)

71(1803)

57(1448)

10(254)

114(2896)

12(10.9)

60(1524)

97

(2464)

181

(4597)

72

(1829)

12

(305)

33

(29.9)

44(1118)

CAP.MAX.HT.

SCR.EXT.

HYD.LIFT

MIN.HT.


3/18

AIRBUS 340 SHOWN

E

D D

C

F


D

A

B

D

A


{1} Second stage oleo must be depressurized prior to jacking.



Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. All tires at normal inflation pressure.



AIRBUS 330 / 340


MLG:Routine

MLG:Flats

CLG:Routine

CLG:Flats



NLG:Routine

NLG:Flats

Aft:Gear Swing

Aft:Oleo Removal


LOCATION &SERVICE

Forward:Gear Swing



9.31(236)

25.03(636)

65L4.5 {3} 22(559)

065(59)

4.5(114)

17.5(445)

65P10AR

8761

65L4.5 {3}

65P10AR

65P10AR

793 {2}

8756

MODEL


8760

733B

18.3(16.6)

92.30(2344)

Notes:

F

E{1}

D

C

REF.

A

34.2(31.0) 15.75

(400)5.85(149)

10.70(272)

15.75(400)

11.40(290)

10.25(260)

65(59)

26(660)

4.75(121)

11(279)

222.40(5649)9.9

(9.0)

12.8(11.6)

18.93(481)

25.03(636)

14.30(363)

14.80(376)

23.07(586)58.9

(53.4) 5.74(146)

23.07(586)

27.20(691)

183.20(4653)

196.70(4996) 249.90

(6347)

228.00(5791)83.8

(76.0) 239.70(6088)

170.50

(4331)

155.60(3952)

AIRCRAFT DATA

MAX.JACKLOAD

MAX.HT.

MIN.HT.

DISTANCEBETWEEN

TIRES

78(1981)

10(9.1)

274(6960)

16(406)

180(4572)

17.5(445)

4.5(114)

65(59)

0 22(559)

10.25(260)

65(59)

26(660)

4.75(121)

11(279)

11(279)

4.75(121)

26(660)

65(59)

10.25(260)

104(2642)

91(2311)

12(305)

207(5258)

30(27.2)

87(2210)

160(4064)

132(3353)

100(90.7)

16(406)

72(1829)

220(5588)

264(6706)

92(2337)

12(305)

100(90.7)

72(1829)

30(27.2)

171(4343)

12(305)

MIN.HT.

HYD.LIFT

SCR.EXT.

MAX.HT.

CAP.


4/18

BOEING 707 SHOWN

AA

DD

B

FC


EEEE


BOEING 707 / 720



50(45.4)

20(18.1)

12(10.9)

CAP.

40(1016)

44(1118)

10(254)

MIN.HT.

60(1524)

54(1372)

120(3048)

174(4420)

MAX.HT.

SCR.EXT.

HYD.LIFT

44(1118)

16(406)

120(3048)

104(2642)

10(254)

9.13(232)

9.75(248)

4.13(105)

23(584)

174(4420)

10(254)

44(1118)

120(3048)

12(10.9)

23(584)

4.13(105)

9.75(248)

22(559)

9.13(232)

4.5(114)

50(45.4)

50(45.4)

65(59)

017.5(445)

76.00(1930)

9.5(8.6)

7.1(6.4)

42.0(38.1)

153.00(3886)

100.00(2540)

103.00(2616)

DISTANCEBETWEEN

TIRES

MAX.JACKLOAD

MIN.HT.

72.00(1829)

122.00(3099)

MAX.HT.

AIRCRAFT DATA

8.80(224)

6.0(5.4)

171.00(4343)

130.00(3302)

6.30(160)

11.20(284)39.3

(35.7)18.70(475)

16.60(422)

17.4(15.8)

6.10(155)11.70(297)

7.80(198)

18.00(457)

12.00(305)

A

B

C

REF.

Notes:

E

F

D

50P9AR

65L4.5 {2}

50P9AR

713A {1}

718A

713A {1}

759A

MODEL




Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). Main gear tires 40 x 14-24. Nose gear tires 34 x 9.9-12. All tires at normal inflation pressure.



NLG:Routine

NLG:Flats

Forward:Gear Swing

Aft:Gear Swing


LOCATION &SERVICE

MLG:Routine

MLG:Flats

Wing Tip:Gear Swing



5/18

B

D D

A

C

A

E


Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). Main gear tires 49 x 17-28. Nose gear tires 32 x 11.5-12.

All tires at normal inflation pressure.


BOEING 727



{1} Specify with 18" leg extensions.


122(3099)

10(254)

72(1829)

40(1016)

17.5(445)

23(584)

4.13(105)

9.75(248)

9.13(232)

13.86(352)

10.51(267)

13.40(340)

718A {1}

0 22(559)

4.5(114)

65(59)

40(1016)

54(1372)

10(254)

104(2642)

20(18.1)

120

(3048)

16

(406)

50

(45.4)

60

(1524)

44

(1118)

50(45.4)

50(45.4)

9.13(232)

9.75(248)

4.13(105)

23(584)

20(18.1)

Forward:Gear Swing


Aft:Gear Swing

Aft:Oleo Removal

104.00(2642)

116.00(2946)

6.4(5.8)

75.00(1905)

104.00(2642)

115.00(2921)

18.0(16.3)

30.5

(27.7)

101.00(2565)76.00

(1930)

64.00(1626)

83.00(2108)

21.63(549)

9.3(8.4)

45.6(41.4)

17.86(454)

8.73(222)

16.88(429)

13.20(335)


MLG:Routine

MLG:Flats

NLG:Flats

LOCATION &SERVICE

NLG:Routine





DISTANCEBETWEEN

TIRES

MIN.HT.

MAX.HT.

MAX.JACKLOAD

AIRCRAFT DATA

MODEL

759A

50P9AR

718A

50P9AR

65L4.5 {2}


B

Notes:

E

C

D

A

REF. MIN.

HT.CAP.

MAX.HT.

SCR.EXT.

HYD.LIFT


6/18

B

C

A

D


D

A

E

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H40 x 14.5-15. Nose gear tires 27 x 7.75-15.


{2} Oleo piston removal is accomplished by positioning gear at angle. Maximum height dimension appliesfor this procedure.

{1} Maximum combined aircraft weight must not exceed 55.5 tons (50.3 metric tons).



BOEING 737-100 THRU -500


{4} Jack capable of 38.5 tons (34.9 metric tons).



65(59)

35(31.8)

10(9.1)

20(18.1)

12(10.9)

25

(22.7)





CAP.

4.70(119)

4.00(102)

NLG:Flats

7.70(196)

12.40(315)

7.30(185)

57.00(1448)

101.00(2565)

64.00

(1626)

AIRCRAFT DATA

MIN.HT.

Notes:

21.4

(19.4){1}

8.6(7.8)

35.3(32.0)

6.9(6.3)

7.9(7.2)

MAX.JACKLOAD

MLG:Routine

MLG:Flats

B

E

C

D

A

REF.

NLG:Routine

Forward:Gear Swing


Aft:Gear Swing

Aft:Oleo Removal

LOCATION &SERVICE



89.30 {2}(2268)

125.00 {2}(3175)

107.32 {2}(2726)

13.30(338)

18.90(480)

89.30(2268)

125.00(3175)

107.32(2726)

10.00(254)

12.80(325)

7.00(178)

725A

718A

MODEL

642S

714A {3}

832R {4}

65L4.5 {5}

DISTANCEBETWEEN

TIRES

MAX.HT.

22(559)

8.25(210)

3(76)

17.25(438)

104(2642)

10(254)

40(1016)

44(1118)

10(254)

150(3810)

110

(2794)

10

(254)

40

(1016)

4.5(114)

7(178)

6(152)

54(1372)

96(2438)

60

(1524)

017.5(445)

22(559)

12(305)

3(76)

MIN.HT.

MAX.HT.

SCR.EXT.

HYD.LIFT


7/18

B


C

A

D D

A

E

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H40 x 14.5-15. Nose gear tires 27 x 7.75-15.




{1} Oleo piston removal is accomplished by positioning gear at angle. Maximum height dimension appliesfor this procedure.


BOEING 737-600 THRU -800



44

(1118)

60

(1524)

16

(406)

120

(3048)

50

(45.4)

44(1118)

12(10.9)

60(1524)

10(254)

114(2896)

CAP. HYD.

LIFTSCR.EXT.

MAX.HT.

MIN.HT.

17.25(438)

3(76)

8.25(210)

23(584)

4.13(105)

9.75(248)

22(559)

10(9.1)

65(59)

17.5(445)

0

6(152)

9.13(232)

4.5(114)

50(45.4)

MIN.HT.

AIRCRAFT DATA

MAX.JACKLOAD

109.20 {1}(2774)

MAX.HT.

DISTANCEBETWEEN

TIRES

34.9

(31.7)

73.10

(1626)

134.00(3404)

100.40(2550)

142.80 {1}(3627)

9.6(8.7)

42.7(38.7)

8.7(7.9)

62.80(1595)

8.50(216)

12.60(320)

8.90(226)

96.00(2438)

18.95(481)

13.25(337)

7.20(183)

15.82(402)

14.60(371)

104.80 {1}(2662)

REF.

A

D

C

E

Notes:

12(10.9)

96(2438)

150(3810)

10(254)

44(1118)

10.9(9.9)

112.20(2850)B


65L4.5 {3}

50P9AR

714A {2}

642S

MODEL

714A

759A

6.75(171)

6.50(165) 642S

6(152)

10(9.1)

8.25(210)

3(76)

17.25(438)

Aft:Oleo Removal

Aft:Gear Swing


Forward:Gear Swing

NLG:Routine

MLG:Flats

MLG:Routine





NLG:Flats


LOCATION &SERVICE


8/18

E

B

FF

A

C

A

E

D

FF

FF

G

FF

D



Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires 46 x 16-28. Nose gear tires 46 x 16-26. All tires at normal inflation pressure.



BOEING 747



{3} With 4" ship adapter. Lift providedby 65P10 or 65P10AR axle jack.

{1} Clearance between brake link bolts at 6.25" (159 mm) above ground (routine).

MODEL



NLG:Routine

LOCATION &SERVICE

Body:Gear Swing

Aft:Gear Swing

Forward:Gear Swing

Wing Tip:Gear Swing

Mid-Wing:Gear Swing

Aft: OleoSeal Change

MLG:Routine

MLG:Flats

Body: OleoSeal Change

Forward: OleoSeal Change

NLG:Flats

65L4.5 {2}

9.00(229){1}

5.50(140) 0

65(59)

4.5(114)

22(559)

17.5(445)

65P10AR

65L4.5 {3}

795

763

733

703

706

65P10AR


Notes:

G

B

A

E

D

F

C

REF.

13.50(343)

18.50(470)

10.50(267)

26.50(673)11.50

(292)

46.0(41.7)

10.25(260)

11(279)

4.75(121)

26(660)

65(59)

017.5(445)

26(660)

65(59)

8.5(114)

AIRCRAFT DATA

100.0

(90.7)

168.00(4267)

132.00(3353)

96.00(2438)

281.00(7137)

233.00(5918)

11.00(279)

196.00(4978)

156.00(3962)

15.0(13.6)

12.5(11.3)

19.7(17.9)

47.5(43.1)

MIN.HT.

MAX.HT.

DISTANCEBETWEEN

TIRES

MAX.JACKLOAD

302.00(7671)

169.00(4293)

136.00(3454)

269.00(6833)

100.00

(2540)

233.00(5918)

48.4(43.9)

20.50(521)

72(1829)

317(8052)

24(610)

24(610)

12(305)

249(6325)

290(7366)

77(1956)

88(2235)

60(54.4)

CAP.

25(22.7)

15(13.6)

65(59)

30(27.2)

MAX.HT.

SCR.EXT.

HYD.LIFT

26(660)

4.75(121)

11(279)

100

(90.7)

MIN.HT.

10.25(260)

87(2210)

97

(2464)

221(5613)

148(3759)

190(4826)

72(1829)

171(4343)

12(305)

24

(610)

72

(1829)

193

(4902)


9/18

E

B

FF

FF

A

C

A

FF

E

D

F

G

D



{1} Clearance between brake link bolts at 6.25" (159 mm) above ground (routine).

{4} With 4" ship adapter. Lift providedby 65P10 or 65P10AR axle jack.

{2} Jack incorporates telescoping legs. Set jack in retracted position for this application.

{3} Lift provided by 65P10 or 65P10ARaxle jack.

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires 46 x 16-28. Nose gear tires 46 x 16-26. All tires at normal inflation pressure.

BOEING 747SP

AIRCRAFT / JACK DATAREVISED DATE: JUNE 23, 1998


Forward:Gear Swing

Aft:Gear Swing

Body:Gear Swing

LOCATION &SERVICE

NLG:Routine



NLG:Flats

Forward: OleoSeal Change

Body: OleoSeal Change

MLG:Flats

MLG:Routine

Aft: OleoSeal Change

Mid-Wing:Gear Swing

Wing Tip:Gear Swing

22(559)

4.5(114)

65(59) 0

5.50(140)

9.00(229){1} 65L4.5 {3}

17.5(445)

65L4.5 {4}

65P10AR

706

703

733

761 {2}

795


65P10AR

G

Notes:

REF.

C

F

D

E

A

B

11.50(292)

26.50(673) 10.50

(267)

18.50(470)

13.50(343)46.0

(41.7)

65(59)

26(660)

4.75(121)

11(279)

10.25(260)

8.5(114)

65(59)

26(660)

17.5(445)

0

100.00

(2540)

77.5

(70.3)

163.00(4140)

197.00(5004)

240.00(6096)

282.00(7163)

233.00(5918)

197.00(5004)

266.00(6756)

MAX.HT.

MIN.HT.

47.5(43.1)

19.7(17.9)

12.5(11.3)

15.0(13.6)

11.00(279)

96.00(2438) 132.00

(3353)

168.00(4267)

AIRCRAFT DATA

48.4(43.9)

136.00(3454)

169.00(4293)

MAX.JACKLOAD

DISTANCEBETWEEN

TIRES

20.50(521)

30(27.2)

65(59)

15(13.6)

25(22.7)

CAP.

60(54.4)

88(2235)

77(1956)

290(7366)

249(6325)

12(305)

24(610)

24(610)

282(7163)

72(1829)

193

(4902)

72

(1829)

24

(610)

12(305)

171(4343)

72(1829)

190(4826)

148(3759)

186(4724)

97

(2464)

87(2210)

10.25(260)

MIN.HT.

100

(90.7)

11(279)

4.75(121)

26(660)

HYD.LIFT

SCR.EXT.

MAX.HT.

MODEL


10/18

C

DAA

E

B

D

D

D


Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H40 x 14.5-19. Nose gear tires H31 x 13-12.

All tires at normal inflation pressure.{1} Jack point "C" (aft) is a stabilization point and is not to be used while raising or lowering the airplane.

Point "C" should be engaged only after primary jacks are secured in final position.

{5} Model 8704 includes a 2.25 ton (2.0 metric ton) by-pass valve setting.

{4} For shoring aft jack point during oleo piston removal, specify 30" extension kit p/n 870450.

{3} Specify with 3/4" female spherical radius ship adapter.

{2} Brake rod pins installed with nut out-board on brake side.


BOEING 757



Aft:Oleo Removal

Aft:Gear Swing

Forward:Gear Swing






NLG:Flats


LOCATION &SERVICE

NLG:Routine

MLG:Flats

MLG:Routine

3.50(89)

6.50(165)

8685

8685

743

795 {3}

749

733

MODEL

8704 {4,5}


B13.5

(12.2)106.00(2692)

Notes:

C{1}

D

E

REF.

A

8.00 {2}(203)

2.0(1.8)

123.00(3124)

10.00(254)

16.0(406)

15.40(391)

154.00(3912)

176.00(4470)

10.30(262)

11.00(279)

6.90(175)

16.6(15.1)

29.0(26.3)

164.00(4166)

142.00(3607)

184.00(4674)

162.00(4115)46.5

(42.2)

130.00

(3302)

MIN.HT.

AIRCRAFT DATA

MAX.JACKLOAD

MAX.HT.

DISTANCEBETWEEN

TIRES

35(31.8)

6.5(165)

10.5(267)

2.5(64)

35(31.8)

19.5(495)

2.5(64)

10.5(267)

6.5(165)

5(4.5)

118(2997)

32(813)

8(203)

158(4013)

87(2210)

12(305)

171(4343)

30(27.2)

72(1829)

20(18.1)

47.5(1207)

160(4064)

10.5(267)

102(2591)

40(1016)

116(2946)

60(54.4)

16(406)

172(4369)

193(4902)

97(2464)

72(1829)

24(610)

100(90.7)

CAP. HYD.

LIFTSCR.EXT.

MAX.HT.

MIN.HT.

19.5(495)


11/18

B

F

A

DD

E

C

A


E

E E

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated.

Main gear tire H45 x 17-20. Nose gear tire H37 x 14-15. All tires at normal inflation pressure.


BOEING 767




{1} For roll-under clearance, oleos may have to be extended.

SCR.EXT.

HYD.LIFT

MIN.HT.

97

(2464)

193

(4902)

72

(1829)

24

(610)

100

(90.7)

CAP. MAX.

HT.

40(36.3)

140(3556)

10(254)

214(5436)

64(1626)

30(27.2)

20(18.1)

25(22.7)

77(1956)

249(6326)

24(610)

148(3760)

102(2591)

72(1829)

87(2210)

171(4343)

10.5(267)

160(4064)

47.5(1207)

065(59)

65(59)

17.5(445)

4.5(114)

26(660)

4.75(121)

11(279)

10.25(260)

22(559)

12(305)

DISTANCEBETWEEN

TIRES

MIN.HT.

MAX.HT.

MAX.JACKLOAD

161.80(4110)

10.5(9.5)

14.0(12.7)

52.5

(47.6)

75.0

(68.0)

33.5(30.4) 206.30

(5240)

165.20(4196)

105.00(2667)

6.50(165)

11.90(302)

205.70(5225)

149.40(3795)

171.40(4354)

10.00

(254)

17.90

(455)

98.50

(2502)

148.60(3774)

184.30(4681)

139.80(3551)

7.10(180)

5.35(136)

B

C

A

REF.

E

D

Notes:

F

795 {1}


MODEL

749

733

65L4.5 {2}

65P10AR

748A

703

65P10AR25.0

(22.7)17.25(438)

12.20(310)

10.80(274)

65(59)

10.25(260)

11(279)

4.75(121)

26(660)

AIRCRAFT DATA


Body:Gear Swing

Body:Oleo Removal

LOCATION &SERVICE

Aft:Gear Swing

Aft:Oleo Removal

Forward:Gear Swing




NLG:Routine

NLG:Flats

Mid-Wing:Gear Swing

MLG:Flats

MLG:Routine


12/18


Body:Gear Swing

Body:Oleo Removal

Aft:Gear Swing

Forward:Gear Swing

Wing Tip:Gear Swing

Mid-Wing:Gear Swing

Aft:Oleo Removal


MLG Aft:Routine

MLG Forward:Routine

MLG Forward:Flats

MLG Aft(Aux.): Flats

LOCATION &SERVICE

NLG:Routine

NLG:Flats

B

Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H49 x 19-22. Nose gear tires 42 x 17R18. All tires at normal inflation pressure.

Caution: Aircraft manufacturer's specifications and instructions must be followed. In the eventof contradiction between aircraft manufacturer's specifications and Malabar's, aircraftmanufacturer's specifications will prevail.

{5} Jack incorporates telescoping legs. Set jack in retracted position for this application.{4} Tripod jacking height may be reduced by 8" (203 mm) if wheels and tires are removed.

{3} 184.70" (4691 mm) with nose landing gear inflated & main landing gear deflated.

{1} The simultaneous use of two axle jacks are required to remove the center wheels and tires.

{2} Load shown for 634,500 lbs gross weight "B" market aircraft. For 537,000 lbs gross weight"A" market, load is 67.7 tons (61.4 metric tons).


Notes:

G{1}

H

H

A


A

F

E

D

G

C

B

F{1}

C

E

D

F

G

D

E

REF.

A

78.7(71.4)

{2}85

(77.1)5.0

(127)18.25(464)

23.25(591)085L5.0 {6}

5.27(134)

85P10AR

85L5.0 {6}

85P10AR



BOEING 777


74.2(67.3)

{2}

8.12(206)

22.08(561)

6.70(170)

10.46(266)

16.00(406)

38.8(35.2)

19.37(492)

11.07(281)

18.10(460)

7.07(180)

13.02(331)

{6} Lift provided by 85P10AR axle jack.

023.25(591)

18.25(464)

5.0(127)

85(77.1)

26(660)

26(660)

4.62(117)

10.88(276)

10.5(267)

85(77.1)

4.62(117)

10.88(276)

10.5(267)

85(77.1)


MODEL

761 {5}

8811

8810

8802

8803

85P10AR

194.20(4933)

{3}

49.5(44.9) 255.00 {4}

(6477)

212.00 {4}(5385)

119.80(3043)

16.00(406)

20.30(516)

13.26(337)

290.00(7366)

254.00(6452)

184.00(4674)

11.0(10.0)

8.6(7.8)

233.80(5939)

204.40(5192)

22.5(20.4)

AIRCRAFT DATA

202.00 {4}(5130)

122.20

(3104)

104.0

(94.3)

MAX.HT.

MIN.HT.

MAX.JACKLOAD

DISTANCEBETWEEN

TIRES

227.00(5766)

174.00(4420)

72(1829)

60(54.4)

281(7137)

24(610)

185(4699)

98(2489)

25(22.7)

208(5283)

26(660)

26(660)

88(2235)

88(2235)

15(13.6)

25(22.7)

294(7468)

260(6604)

190(4826)

16(406)

16(406)

156(3962)

85(77.1)

10.5(267)

10.88(276)

4.62(117)

84(2134)

MAX.HT.

SCR.EXT.

HYD.LIFT

MIN.HT.

105

(95.3)

26

(660)

74

(1880)

98

(2489)

198

(5029)

CAP.


13/18

CC

C

B

C

A

D

A



DOUGLAS DC8



{1} Use Douglas adapter p/n 5706789.

Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). Main gear tires 44 x 16-28. Nose gear tires 34 x 11-18. All tires at normal inflation pressure.



NLG:Routine

NLG:Flats

MLG:Flats

MLG:Routine


Forward:Gear Swing

LOCATION &SERVICE




50P9AR {1}

50P9AR


MODEL

759A

718AB59.38(1508)

12.0(10.9)

40(1016)

54(1372)

10(254)

104(2642)

20(18.1)

C

D

Notes:

A

REF.

15.00(381)

18.50(470)

40.0(36.3)

13.50(343)

1.00(25)

7.25(184)

7.00(178)

12.50(318)

11.00(279)

12.00(305)

7.00(178)

20.0(18.1)

82.00(2083)

114.80(2916)

78.00(1981)

118.00(2997)

93.30

(2370)

50.0

(45.4)

DISTANCEBETWEEN

TIRES

MIN.HT.

MAX.HT.

MAX.JACKLOAD

AIRCRAFT DATA

9.13(232)

9.75(248)

4.13(105)

23(584)

23(584)

4.13(105)

9.75(248)

9.13(232)

50(45.4)

50(45.4)

MIN.HT.

CAP. MAX.

HT.SCR.EXT.

HYD.LIFT

120

(3048)

16

(406)

50

(45.4)

60

(1524)

44

(1118)


14/18

B

AA


D

F

C

EE


{1} Dimensions apply without wheels and tires.


DOUGLAS DC9



Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). Main gear tires 40 x 14. Nose gear tires 26 x 6.6. All tires at normal inflation pressure.

30(762)

8(203)

78(1981)

12(10.9)

MIN.HT.

HYD.LIFT

SCR.EXT.

MAX.HT.

CAP.

36

(914)

50

(1270)

25

(22.7)

10

(254)

96

(2438)

25(22.7)

96(2438)

10(254)

50(1270)

36(914)

9.13(232)

9.75(248)

4.13(105)

23(584)

10(9.1)

64(1626)

4(102)

24(610)

36(914)

50(45.4)

40(1016)

17.25(438)

3(76)

8.25(210)

6(152)

10(9.1)

91.00(2311)62.00

(1575)

57.00

(1448)

95.00(2413)

DISTANCEBETWEEN

TIRES

MAX.JACKLOAD

MIN.HT.

MAX.HT.

10.7(9.7)B

REF.

32.00(813)

51.00(1295)

9.50(241)

13.10(333) 19.40

(493)

7.0(6.4)

38.2(34.7)

10.7(9.7)

43.00(1092)

82.00(2083)

22.1

(20.0)

LOCATION &SERVICE

Forward:Gear Swing


MLG:Routine

Aft w/o Stair:Gear Swing

Aft w/ Stair:Gear Swing

Aft w/ Stair:Oleo Removal

Aft w/o Stair:Oleo Removal



D

E

C

A

AIRCRAFT DATA

97.00 {1}(2464)

92.00 {1}(2337)

84.00 {1}(2134)

59.00 {1}(1499)

6.00(152)

8.50(216)

NLG:Flats

F0

7.4(6.7) 6.60

(168)

11.60(295)

NLG:Routine

Notes:

08.00(203)

MLG:Flats

642S

50P9AR

7210-S1

7120A

7120A

7212-S8

MODEL





15/18

B

AA

DD


C

E

Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). Main gear tires 44.5 x 16.5-20. Nose gear tires 26 x 6.6.



DOUGLAS MD80 / MD90

AIRCRAFT / JACK DATAREVISED DATE: JUNE 23, 1998

{1} Do not lift aircraft at this jack point. For shoring aircraft only.

{2} Dimensions apply without wheel and tire.

60

(1524)

50

(45.4)

16

(406)

120

(3048)

HYD.LIFT

SCR.EXT.

MAX.HT.

CAP.

44

(1118)

MIN.HT.

23(584)

4.13(105)

9.75(248)

9.13(232)

50(45.4)

10(9.1)

6(152)

8.25(210)

3(76)

17.25(438)

4(102)

64(1626)

10(9.1)

36(914)

24(610)

AIRCRAFT DATA

MAX.JACKLOAD

MAX.HT.

MIN.HT.

DISTANCEBETWEEN

TIRES

81.00(2057)

67.00

(1702)

94.00(2388)29.1

(26.4) 97.00 {2}(2464)

84.00 {2}(2134)

6.20(157)

8.50(216) 11.60

(295)7.5

(6.8)

38.2(34.7)

19.40(493)

14.40(3658)

8.40(2134)

9.50(241)

0

53.00 {2}(1346)

7.0(6.4)

50.00(1270)34.00

(864)

REF.

A

D

E

C{1}

Notes:

15(13.6)

100(2540)

4(102)

54(1372)

42(1067)

61.00(1549)

14.5(13.2)B


711

759A

MODEL

50P9AR

642S

7210-S1

06.60(168)

Aft:Oleo Removal

Aft:Gear Swing



LOCATION &SERVICE




NLG:Routine

NLG:Flats

MLG:Flats

MLG:Routine


Forward:Gear Swing


16/18

{5}

A A

D

C

C C

B


C

{2} Models are suitable provided aircraft weight does not exceed 465,000 lbs.


{5} For CLG jacking on DC10-30/40 series, de-pressurize strut prior to jacking and use axle jack models65P10 or 65P10AR.


DOUGLAS DC10




Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H54 x 20-20. Nose gear tires 37 x 14-14. All tires at normal inflation pressure.

{1} DC10-30/40 maximum load shown. For DC10-10/15, maximum load is 90 tons (81.6 metric tons).




LOCATION &SERVICE

Forward:Gear Swing


MLG:Routine

MLG:Flats



REF.

Notes:

65L4.5 {4}

733 {2}

793 {2,3}

MODEL


65P10AR

65P10AR

DISTANCEBETWEEN

TIRES

B36.5

(33.1)90.30(2294)

30(27.2)

171(4343)

12(305)

87(2210)

72(1829)

D

C

A

6.30(160)

35.0(30.8)

22.50(572)

19.00(483)

60.1(54.5) 11.50

(292)

27.60(701)

8.90(226)

14.10(358)

7.50(191)

0

11.80(300)

140.30(3564)

NLG:Flats

NLG:Routine

118.1

(107.1){1} 206.50(5245)

123.90(3147)

145.30

(3691)

182.80(4643)

MAX.JACKLOAD

AIRCRAFT DATA

MAX.HT.

MIN.HT.

4.75(121)

11(279)

10.25(260)

65(59)

65(59)

4.5(114)

22(559)

017.5(445)

65(59)

10.25(260)

11(279)

4.75(121)

26(660)

26(660)

72

(1829)

132

(3353)

100

(90.7)

16

(406)

220

(5588)

HYD.LIFT

SCR.EXT.

MAX.HT.

CAP. MIN.

HT.


17/18

C

{5}

B

D

C

D

E


D D

A A

{1} Models are suitable provided aircraft weight does not exceed 465,000 lbs.



DOUGLAS MD 11


{5} For CLG jacking, de-pressurize strut prior to jacking and use axle jack models 65P10 or 65P10AR.

{3} Use Douglas adapter p/n DZZ7320. Adapter adds 12" (305 mm) to jack mininum height.



MIN.HT.

CAP. MAX.

HT.SCR.EXT.

HYD.LIFT

220

(5588)

16

(406)

100

(90.7)

132

(3353)

72

(1829)

26(660)

4.75(121)

11(279)

10.25(260)

65(59)65

(59)4.5

(114)22

(559)017.5

(445)

65(59)

10.25(260)

11(279)

4.75(121)

26(660)

32(813)

160(4064)

8(203)

200(5080)

5(4.5)

MAX.HT.

AIRCRAFT DATA

MAX.JACKLOAD

DISTANCEBETWEEN

TIRES

MIN.HT.

207.50(5271)

125.40(3185)

148.40

(3769)

184.30(4681)120.3

(109.1)

19.00

(483)

8.90(226)

0NLG:Flats

NLG:Routine

140.30(3564)

23.50(570)

30.5

(27.7) 7.10(180)

9.50(241)

16.00(406)

13.00(330)

27.10(688)11.00(279)

64.0(58.1)

178.00(4521)

4.0(3.6)

192.00(4877)

REF.

A

D

C

C

30(27.2)

72(1829)

87(2210)

12(305)

171(4343)

30.6(27.8)

93.30(2370)B

733 {1}


MODEL

793 {1,2}

65P10AR

65P10AR

65L4.5 {4}

8487A {3}





Forward:Gear Swing

LOCATION &SERVICE



Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. Main gear tires H54 x 21.0-24. Nose gear tires 40 x 15.5-16. All tires at normal inflation pressure.

Notes:

MLG:RoutineMLG:Flats

Wing Tip:Gear Swing


18/18

D

B

C

A

C

C

C

A




LOCKHEED L1011



MODELDISTANCEBETWEEN

TIRES

MIN.HT.

CAP. MAX.

HT.SCR.EXT.

HYD.LIFT

793 {1}72

(1829)132

(3353)100

(90.7)16

(406)220

(5588)

72(1829)

87(2210)

12(305)

171(4343)

30(27.2)

733

65P10AR

65P10AR

65(59.0)

10.25(260)

11(279)

4.75(121)

26(660)

26.00(660)

11.50(292)

9.00(229)

0

26(660)

4.75(121)

11(279)

10.25(260)

65(59.0)

LOCATION &SERVICE


REF. MIN.

HT.

MAX.JACKLOAD

AIRCRAFT DATA

80.0(72.6)

151.00(3835)

A

B 28.0(25.4)

112.00(2845)

Forward:Gear Swing

MLG:Routine

MLG:Flats

NLG:Flats

NLG:Routine 28.0

(25.4)

8.00(203)

11.00(279)

7.00(178)

14.00(356)55.0

(49.9)

Notes:

D

C


MAX.HT.

186.00(4724)

147.00(3734)

23.00(584)

16.00(406)



Tripod jack point heights are based on: Main & nose landing gear strut oleos at normal operating empty weight (OEW). All tires at normal inflation pressure.


Aircraft Data File 46718

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