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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
8/12/2019 Aircraft Data File 46718
2/18
MLG DOUBLE AXLE SHOWN
E E
C
D
D
F
B
A
D
A
D
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
AIRBUS 319 / 320 / 321
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
REVISED DATE: JUNE 23, 1998
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).
{3} Specify with leg extensions.
NLG:Flats
NLG:Routine
MLG SingleAxle: Routine
MLG DualAxle: Flats
MLG DualAxle: Routine
MLG SingleAxle: Flats
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.
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
Main Wing:Gear Swing
Main Wing:Oleo Removal
Forward:Gear Swing
LOCATION &SERVICE
Forward:Oleo Removal
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.
8/12/2019 Aircraft Data File 46718
3/18
AIRBUS 340 SHOWN
E
D D
C
F
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
D
A
B
D
A
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
{1} Second stage oleo must be depressurized prior to jacking.
{2} Jack incorporates telescoping legs. Set jack in extended position for this application.
{3} Lift provided by 65P10 or 65P10AR axle jack.
Tripod jack point heights are based on: Main & nose landing gear strut oleos fully deflated. All tires at normal inflation pressure.
REVISED DATE: JUNE 23, 1998
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
AIRBUS 330 / 340
AIRCRAFT / JACK DATA
MLG:Routine
MLG:Flats
CLG:Routine
CLG:Flats
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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.
NLG:Routine
NLG:Flats
Aft:Gear Swing
Aft:Oleo Removal
Forward:Oleo Removal
LOCATION &SERVICE
Forward:Gear Swing
Main Wing:Oleo Removal
Main Wing: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
MALABAR JACK MODELS AND DATA
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.
8/12/2019 Aircraft Data File 46718
4/18
BOEING 707 SHOWN
AA
DD
B
FC
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
EEEE
REVISED DATE: JUNE 23, 1998
BOEING 707 / 720
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
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
MALABAR JACK MODELS AND DATA
{2} Lift provided by 65P10 or 65P10AR axle jack.
{1} Specify with leg extensions.
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.
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
NLG:Routine
NLG:Flats
Forward:Gear Swing
Aft:Gear Swing
Main Wing:Gear Swing
LOCATION &SERVICE
MLG:Routine
MLG:Flats
Wing Tip:Gear Swing
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
8/12/2019 Aircraft Data File 46718
5/18
B
D D
A
C
A
E
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
REVISED DATE: JUNE 23, 1998
BOEING 727
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
{1} Specify with 18" leg extensions.
{2} Lift provided by 65P10 or 65P10AR axle jack.
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
Forward:Oleo Removal
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)
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
MLG:Routine
MLG:Flats
NLG:Flats
LOCATION &SERVICE
NLG:Routine
Main Wing:Gear Swing
Main Wing:Oleo Removal
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.
DISTANCEBETWEEN
TIRES
MIN.HT.
MAX.HT.
MAX.JACKLOAD
AIRCRAFT DATA
MODEL
759A
50P9AR
718A
50P9AR
65L4.5 {2}
MALABAR JACK MODELS AND DATA
B
Notes:
E
C
D
A
REF. MIN.
HT.CAP.
MAX.HT.
SCR.EXT.
HYD.LIFT
8/12/2019 Aircraft Data File 46718
6/18
B
C
A
D
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
All tires at normal inflation pressure.
{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).
REVISED DATE: JUNE 23, 1998
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
BOEING 737-100 THRU -500
AIRCRAFT / JACK DATA
{4} Jack capable of 38.5 tons (34.9 metric tons).
{3} Specify with leg extensions.
{5} Lift provided by 65P10 or 65P10AR axle jack.
65(59)
35(31.8)
10(9.1)
20(18.1)
12(10.9)
25
(22.7)
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.
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
MALABAR JACK MODELS AND DATA
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
Forward:Oleo Removal
Aft:Gear Swing
Aft:Oleo Removal
LOCATION &SERVICE
Main Wing:Gear Swing
Main Wing:Oleo Removal
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
8/12/2019 Aircraft Data File 46718
7/18
B
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
All tires at normal inflation pressure.
{3} Lift provided by 65P10 or 65P10AR axle jack.
{2} Specify with leg extensions.
{1} Oleo piston removal is accomplished by positioning gear at angle. Maximum height dimension appliesfor this procedure.
REVISED DATE: JUNE 23, 1998
BOEING 737-600 THRU -800
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
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
MALABAR JACK MODELS AND DATA
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:Oleo Removal
Forward:Gear Swing
NLG:Routine
MLG:Flats
MLG:Routine
Main Wing:Oleo Removal
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
NLG:Flats
Main Wing:Gear Swing
LOCATION &SERVICE
8/12/2019 Aircraft Data File 46718
8/18
E
B
FF
A
C
A
E
D
FF
FF
G
FF
D
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
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.
{2} Lift provided by 65P10 or 65P10AR axle jack.
REVISED DATE: JUNE 23, 1998
BOEING 747
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
{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
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.
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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
MALABAR JACK MODELS AND DATA
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)
8/12/2019 Aircraft Data File 46718
9/18
E
B
FF
FF
A
C
A
FF
E
D
F
G
D
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
{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
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
Forward:Gear Swing
Aft:Gear Swing
Body:Gear Swing
LOCATION &SERVICE
NLG:Routine
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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.
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
MALABAR JACK MODELS AND DATA
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
8/12/2019 Aircraft Data File 46718
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C
DAA
E
B
D
D
D
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
REVISED DATE: JUNE 23, 1998
BOEING 757
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
Aft:Oleo Removal
Aft:Gear Swing
Forward:Gear Swing
Forward:Oleo Removal
Main Wing:Oleo Removal
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
NLG:Flats
Main Wing:Gear Swing
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}
MALABAR JACK MODELS AND DATA
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)
8/12/2019 Aircraft Data File 46718
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B
F
A
DD
E
C
A
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
REVISED DATE: JUNE 23, 1998
BOEING 767
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
{2} Lift provided by 65P10 or 65P10AR axle jack.
{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}
MALABAR JACK MODELS AND DATA
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
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
Body:Gear Swing
Body:Oleo Removal
LOCATION &SERVICE
Aft:Gear Swing
Aft:Oleo Removal
Forward:Gear Swing
Forward:Oleo Removal
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.
NLG:Routine
NLG:Flats
Mid-Wing:Gear Swing
MLG:Flats
MLG:Routine
8/12/2019 Aircraft Data File 46718
12/18
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
Body:Gear Swing
Body:Oleo Removal
Aft:Gear Swing
Forward:Gear Swing
Wing Tip:Gear Swing
Mid-Wing:Gear Swing
Aft:Oleo Removal
Forward: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).
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
Notes:
G{1}
H
H
A
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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
REVISED DATE: JUNE 23, 1998
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
BOEING 777
AIRCRAFT / JACK DATA
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)
MALABAR JACK MODELS AND DATA
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.
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CC
C
B
C
A
D
A
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
REVISED DATE: JUNE 23, 1998
DOUGLAS DC8
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
{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.
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
NLG:Routine
NLG:Flats
MLG:Flats
MLG:Routine
Forward:Oleo Removal
Forward:Gear Swing
LOCATION &SERVICE
Main Wing:Gear Swing
Main Wing:Oleo Removal
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
50P9AR {1}
50P9AR
MALABAR JACK MODELS AND DATA
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)
8/12/2019 Aircraft Data File 46718
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B
AA
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
D
F
C
EE
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
{1} Dimensions apply without wheels and tires.
REVISED DATE: JUNE 23, 1998
DOUGLAS DC9
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
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
Forward:Oleo Removal
MLG:Routine
Aft w/o Stair:Gear Swing
Aft w/ Stair:Gear Swing
Aft w/ Stair:Oleo Removal
Aft w/o Stair:Oleo Removal
Main Wing:Gear Swing
Main Wing: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
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
MALABAR JACK MODELS AND DATA
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.
8/12/2019 Aircraft Data File 46718
15/18
B
AA
DD
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
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.
All tires at normal inflation pressure.
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
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
MALABAR JACK MODELS AND DATA
711
759A
MODEL
50P9AR
642S
7210-S1
06.60(168)
Aft:Oleo Removal
Aft:Gear Swing
Main Wing:Oleo Removal
Main Wing:Gear Swing
LOCATION &SERVICE
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).
NLG:Routine
NLG:Flats
MLG:Flats
MLG:Routine
Forward:Oleo Removal
Forward:Gear Swing
8/12/2019 Aircraft Data File 46718
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{5}
A A
D
C
C C
B
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
C
{2} Models are suitable provided aircraft weight does not exceed 465,000 lbs.
{4} Lift provided by 65P10 or 65P10AR axle jack.
{5} For CLG jacking on DC10-30/40 series, de-pressurize strut prior to jacking and use axle jack models65P10 or 65P10AR.
{3} Jack incorporates telescoping legs. Set jack in extended position for this application.
DOUGLAS DC10
AIRCRAFT / JACK DATA
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
REVISED DATE: JUNE 23, 1998
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).
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
Main Wing:Oleo Removal
Main Wing:Gear Swing
LOCATION &SERVICE
Forward:Gear Swing
Forward:Oleo Removal
MLG:Routine
MLG:Flats
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.
REF.
Notes:
65L4.5 {4}
733 {2}
793 {2,3}
MODEL
MALABAR JACK MODELS AND DATA
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.
8/12/2019 Aircraft Data File 46718
17/18
C
{5}
B
D
C
D
E
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
D D
A A
{1} Models are suitable provided aircraft weight does not exceed 465,000 lbs.
REVISED DATE: JUNE 23, 1998
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
DOUGLAS MD 11
AIRCRAFT / JACK DATA
{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.
{4} Lift provided by 65P10 or 65P10AR axle jack.
{2} Jack incorporates telescoping legs. Set jack in extended position for this application.
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}
MALABAR JACK MODELS AND DATA
MODEL
793 {1,2}
65P10AR
65P10AR
65L4.5 {4}
8487A {3}
Main Wing:Gear Swing
Main Wing:Oleo Removal
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
Forward:Oleo Removal
Forward:Gear Swing
LOCATION &SERVICE
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.
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
8/12/2019 Aircraft Data File 46718
18/18
D
B
C
A
C
C
C
A
Legend: Aircraft primary tripod jack locationAircraft auxiliary tripod jack locationAircraft axle jack location
MALABAR INTERNATIONALSIMI VALLEY, CALIFORNIA
REVISED DATE: JUNE 23, 1998
LOCKHEED L1011
AIRCRAFT / JACK DATA
MALABAR JACK MODELS AND DATA
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
Main Wing:Gear Swing
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
FOR ALTERNATE JACK SELECTIONS, REFER TO"RECOMMENDED MALABAR AIRCRAFT JACK MODELS" CHART
MAX.HT.
186.00(4724)
147.00(3734)
23.00(584)
16.00(406)
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.
{1} Jack incorporates telescoping legs. Set jack in extended position for this application.
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.
Capacities shown in tons and (metric tons). Dimensions shown in inches and (millimeters).