REPORT MDC K0388 REVISION “E” ISSUED: 1996 MD-11 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING OCTOBER 1990

REPORT MDC K0388
REVISION “E”
ISSUED: ___ 1996

MD-11
AIRPLANE CHARACTERISTICS

FOR AIRPORT PLANNING

OCTOBER 1990

To Whom It May Concern:

This document is intended for airport planning purposes.
Specific aircraft performance and operational requirements are
established by the airline that will use the airport under consideration.

Questions concerning the use of this document should be
addressed to:

Airport Compatibility Group
McDonnell Douglas
3855 Lakewood Blvd.
M/C 801–23
Long Beach, CA 90846 USA

Tel. (310) 593–6497 FAX (310) 982–6713

DOUGLAS AIRCRAFT COMPANY

i

REVISIONS
MD-11 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING

REV. A REV. B REV. C REV. D REV. E
NOV. 12, 1990 FEB. 2, 1991 MAY 22, 1991 NOV. 30, 1993 JUN. 30, 1996

PAGE PAGE PAGE PAGE PAGE

2–2 2–2 5–7 2–2
2–3 2–3 2–3
2–14 2–5 7–7 2–4
2–15 2–25 2–5
3–1 2–27 4–3 2–16
3–2 4–4 2–18
3–3 4–5 2–23
3–4 4–8 2–24
3–5 5–12 2–25
3–6 7–4 2–27
3–7 7–5 Section 3
3–8 7–7 4–3
3–9 7–9 4–7
3–10 7–11 5–3
3–11 7–13 5–12
3–12 7–15 6–9
3–13 7–21 7–2
3–14 7–22 7–4
3–15 7–23 7–5
3–16 7–24 7–6
3–17 7–7

7–9
7–11
7–13
7–15
7–21
7–22
7–23
7–24

CONTENTS

Section Page

1.0 SCOPE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1
1.1 Purpose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-1
1.2 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1-2

2.0 AIRPLANE DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
2.1 General Airplane Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-1
2.2 General Airplane Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-4
2.3 Ground Clearances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
2.4 Interior Arrangements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6
2.5 Cabin Cross Section . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-12
2.6 Lower Compartment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-17
2.7 Door Clearances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-19

3.0 AIRPLANE PERFORMANCE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
3.1 General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-1
3.2 Payload-Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-2
3.3 FAR Takeoff Runway Length Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-10

3.4 FAR Landing Runway Length Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3-16

4.0 GROUND MANEUVERING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
4.1 General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-1
4.2 Turning Radii, No Slip Angle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-2
4.3 Minimum Turning Radaii . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-3
4.4 Visibility from Cockpit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-4
4.5 Runway and Taxiway Turn Paths . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-5
4.6 Runway Holding Bay (Apron) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-10

5.0 TERMINAL SERVICING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1
5.1 Airplane Servicing Arrangement (Typical) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-1
5.2 Terminal Operations, Turnaround . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-4
5.3 Terminal Operations, En Route Station . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-5
5.4 Ground Service Connections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-6
5.5 Engine Starting Pneumatic Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-8
5.6 Ground Pneumatic Power Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-10
5.7 Preconditioned Airflow Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-11
5.8 Ground Towing Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-12

6.0 OPERATING CONDITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1
6.1 Jet Engine Exhaust Velocities and Temperatures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-1
6.2 Airport and Community Noise . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-8

v

CONTENTS (CONTINUED)

Section Page

7.0 PAVEMENT DATA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1
7.1 General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-1
7.2 Footprint . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-4
7.3 Maximum Pavement Loads . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-5
7.4 Landing Gear Loading on Pavement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-6
7.5 Flexible Pavement Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-8
7.6 Flexible Pavement Requirements, LCN Conversion . . . . . . . . . . . . . . . . . . . . . . . . . . 7-10
7.7 Rigid Pavement Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-12
7.8 Rigid Pavement Requirements, LCN Conversion . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-14
7.9 ACN-PCN Reporting System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7-18

8.0 POSSIBLE MD-11 DERIVATIVE AIRPLANES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-1

9.0 MD-11 SCALE DRAWINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9-1

vi

1.0 SCOPE

1.1 Purpose
1.2 Introduction

1.0 SCOPE
1.1 Purpose
This document provides, in a standardized format, airplane characteristics data for general airport
planning. Since operational practices vary among airlines, specific data should be coordinated with the
using airlines prior to facility design. Douglas Aircraft Company should be contacted for any additional
information required.
Content of this document reflects the results of a coordinated effort by representatives of the following
organizations:

S Aerospace Industries Association
S Airports Council International
S Air Transport Association of America
S International Air Transport Association
The airport planner may also want to consider the information presented ine the “CTOL Transport
Aircraft: Characteristics, Trends, and Growth Projections,” available from the US AIA, 1250 Eye St.,
Washington DC 20005, for long range planning needs. This document is updated periodically and
represents the coordinated efforts of the folllowing organizations regarding future aircraft growth trends:
S International Coordinating Council of Aerospace Industries Association
S Airports Council International
S Air Transport Association of America
S International Air Transport Association

REV E
1–1

1.2 Introduction
This document conforms to NAS 3601. It provides Model MD-11 characteristics for airport operators,
airlines, and engineering consultant organizations. Since airplane changes and available options may alter
the information, the data presented herein must be regarded as subject to change. Similarly, for airplanes
not yet certified, changes can be expected to occur.
For further information, contact:

McDonnell Douglas
Attention: Airport Compatibility Group
M/C 801–23
3855 Lakewood Blvd.
Long Beach, California, 90846–0001 USA

or
Telex: 674357
FAX: (562) 982–6713

REV E
1–2

1.0 SCOPE
1.1 Purpose
This document provides, in a standardized format, airplane characteristics data for general airport
planning. Since operational practices vary among airlines, specific data should be coordinated with the
using airlines prior to facility design. Douglas Aircraft Company should be contacted for any additional
information required.
Content of this document reflects the results of a coordinated effort by representatives of the following
organizations:

S Aerospace Industries Association
S Airports Council International
S Air Transport Association of America
S International Air Transport Association
The airport planner may also want to consider the information presented ine the “CTOL Transport
Aircraft: Characteristics, Trends, and Growth Projections,” available from the US AIA, 1250 Eye St.,
Washington DC 20005, for long range planning needs. This document is updated periodically and
represents the coordinated efforts of the folllowing organizations regarding future aircraft growth trends:
S International Coordinating Council of Aerospace Industries Association
S Airports Council International
S Air Transport Association of America
S International Air Transport Association

REV E

1–1

1.2 Introduction
This document conforms to NAS 3601. It provides Model MD-11 characteristics for airport operators,
airlines, and engineering consultant organizations. Since airplane changes and available options may alter
the information, the data presented herein must be regarded as subject to change. Similarly, for airplanes
not yet certified, changes can be expected to occur.
For further information, contact:

McDonnell Douglas
Attention: Airport Compatibility Group
M/C 801–23
3855 Lakewood Blvd.
Long Beach, California, 90846–0001 USA

or
Telex: 674357
FAX: (562) 982–6713

REV E
1–2

2.0 AIRPLANE DESCRIPTION

2.1 General Airplane Characteristics
2.2 General Airplane Dimensions
2.3 Ground Clearances
2.4 Interior Arrangements
2.5 Cabin Cross Section
2.6 Lower Compartment

2.7 Door Clearances

2.0 AIRPLANE DESCRIPTION
2.1 General Airplane Characteristics — MD-11
Maximum Design Taxi Weight (MTW). Maximum weight for ground maneuvering as limited by aircraft
strength (MTOW plus taxi fuel).
Maximum Design Landing Weight (MLW). Maximum weight for landing as limited by aircraft strength
and airworthiness requirements.
Maximum Design Takeoff Weight (MTOW). Maximum weight for takeoff as limited by aircraft strength
and airworthiness requirements. (This is the maximum weight at the start of the takeoff run.)
Operating Empty Weight (OEW). Weight of structure, power plant, furnishing, systems, unusable fuel
and other unusable propulsion agents, and other items of equipment that are considered part of a
particular airplane configuration. OEW also includes certain standard items, personnel, equipment, and
supplies necessary for full operations, excluding usable fuel and payload.
Maximum Design Zero Fuel Weight (MZFW). Maximum weight allowed before usable fuel and other
specified usable agents must be loaded in defined sections of the aircraft as limited by strength and
airworthiness requirements.
Maximum Payload. Maximum design zero fuel weight minus operational empty weight.
Maximum Seating Capacity. The maximum number of passengers certified or anticipated for
certification.
Maximum Cargo Volume. The maximum space available for cargo.
Usable Fuel. Fuel available for aircraft propulsion.

2–1

148 F T 8 IN. (45.3 m) 44 FT 1 IN.
136 F T 6 IN. (41.6 m)* (13.4 m)

WING TIP DIME NS ION P OINT

75 FT 10 IN. 19 FT 9 IN.
(23.1 m) (6.0 m)

79 FT 6 IN. 59 FT 2 IN
(24.2 m) (18.0 m)

26 FT 10 IN. SEE
(8.2 m) S E C TION

9 FT 7 IN. 2.3
(2.9 m)

99 FT 4 IN.
(30.3 m)

27 FT 10 IN. 80 F T 9 IN. (24.6 m)
(8.5 m)

192 F T 5 IN. (58.6 m)

202 F T 2 IN. (61.6 m) WIT H C F 6-80C 2D1F E NG INE S
200 F T 11 IN. (61.2 m) WIT H P W4460 E NG INE S

170 F T 6 IN. (51.97 m)**

S CALE

* S PAN AT WING T IP DIME NS ION P OINT 0 5 10 m

= 165 F T 7 IN. (50.5m) WIT H F ULL F UE L LOAD 35 FT 0 IN. 0 10 20 30 FT

(10.7 m)
** WING LE T S PAN WIT H F ULL F UE L LOAD

2.2 GE NE R AL AIR PL ANE DIME NS IONS C hap2±T ext

MODE L MD-1 REV E

2-4

• MAXIMUM AND MINIMUM CLEARANCES OF INDIVIDUAL LOCATIONS

ARE GIVEN FOR COMBINATIONS OF AIRPLANE LOADING/UNLOADING

ACTIVITIES THAT PRODUCE THE GREATEST VARIATION AT EACH LOCATION.

ZERO ROLL ANGLE AND LEVEL GROUND WERE ASSUMED FOR ANALYSIS.

• IT IS RECOMMENDED THAT APPROXIMATELY ± 3 INCHES (0.1 m) BE ALLOWED

FOR VERTICAL EXCURSIONS DUE TO VARYING STRUT AND TIRE INFLATIONS, L

PAVEMENT UNEVENNESS, ETC.

K

AB

C VE J W

D F G X I/H

WINGLET DETAIL

76.15 IN.
36.89 IN.

R TU
S
P O R

GROUND

M N

VERTICAL CLEARANCE

MIN CLEARANCE MAX CLEARANCE
CRITICAL WT AND CG CRITICAL WT AND CG

FT – IN. METERS FT – IN. METERS
8.66 29 – 2 8.88
A 28 – 5 8.27 28 – 6 8.69
4.81 17 – 5 5.31
B 27 – 1 2.23 8 – 9 2.67
4.78 16 –11 5.16
C 15 – 9 2.80 10 – 3 3.14
4.75 16 – 3 4.96
D 7 – 4 2.64 9 – 9 2.96
2.64 9 – 9 2.96
E 15 – 8 4.57 16 – 3 4.94

8.73 30 – 9 9.38
F 9 – 2 58 – 10
17.31 8 – 5 17.93
G 15 – 7 2.38 4 – 5 2.57
0.96 10 – 5 1.25
H 8 – 8 2.93 11 – 7 3.17
3.25 13 – 4 3.52
I 8 – 8 3.77 25 – 7 4.07
6.89 33 – 6 7.49
J 15 – 0 9.83 38 – 2
11.23 17 – 1 10.20
K 28 – 8 4.80 11 – 4 11.63
3.03 16 – 3 5.21
L 56 – 9 4.61 3.44
4.94
M 7 – 10

N* 3 – 2

O 9 – 8

P 10 – 8

R 12 – 4

S 22 – 7

T 32 – 3

U 36 – 10

V 15 – 8

W 9 – 11

X 15 – 3

* = GE CF6–80C2 D1F V = FREIGHTER
H = STANDARD CENTER CARGO DOOR I = COMBI CENTER CARGO DOOR
X = COMBI MAIN DECK DOOR
DMC005-5
2.3 GROUND CLEARANCES
MODEL MD-11 REV D

2–5

SERVICE MODULE

0.50 IN. 8 IN. (TYP)
(1.3 cm) (20.3 cm)

21.50 IN. 95 IN.
(TYP) (241.3 cm)

57 IN. (TYP) 26.50 IN. 3 IN. (54.6 cm)
(144.8 cm) (67.3 cm) (TYP)
(7.6 cm)

CARGO

66 IN.
(167.6 cm)

125.5 IN. (318.8 cm) REV E
164 IN. (416.6 cm)

237 IN. (602.0 cm)

2.5 CABIN CROSS SECTION
2.5.1 FIRST CLASS
MODEL MD-11

2–12

0.50 IN. 95 IN.
(1.3 cm) (241.3 cm)

73.50 IN. (186.69 cm)

50 IN. (TYP) 11.75 IN. 20.50 IN.
(TYP)
(127 cm) 25.25 IN. (TYP)
3 IN. (TYP) (64.1 cm) (29.8 cm) (52.1 cm)

(7.6 cm)

CARGO

66 IN.
(167.6 cm)

125.5 IN. (318.8 cm)
164 IN. (416.6 cm)
237 IN. (602.0 cm)

2.5.2 BUSINESS CLASS REV E
MODEL MD-11

2–13

0.50 IN. 102 IN. (259.1 cm)
(1.3 cm)

42 IN. (TYP) 19 IN. 9.5 IN. (TYP) 95 IN. 18 IN. (TYP)
(106.7 cm) (TYP) (24.1 cm) (241.3 cm) (45.7 cm)

(48.3 2 IN. (TYP)
cm) (5.1 cm)

CARGO

66 IN.
(167.6 cm)

125.5 IN. (318.8 cm)
164 IN. (416.6 cm)
237 IN. (602.0 cm)

2.5.3 ECONOMY REV E
MODEL MD-11

2–14

0.50 IN. 95 IN.
(1.3 cm) (241.3 cm)

76 IN. (193.0 cm)

57.50 IN. (TYP) 16.50 IN. 2 IN. (TYP) 9.25 IN. 16.50 IN.
(146.1 cm) (TYP) (5.1 cm) (TYP) (TYP)
(23.5 cm) (41.9 cm)
(41.9
cm)

CARGO

66 IN.
(167.6 cm)

125.5 IN. (318.8 cm)
164 IN. (416.6 cm)
237 IN. (602.0 cm)

2.5.4 HIGH-DENSITY REV E
MODEL MD-11

2–15

1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13C
1L 2L 3L 4L 5L 6L 7L 8L 9L 10L 11L 12L 14C

BARRIER NET FREIGHTER (26) 88- BY 125-IN. PALLETS = 14,542 FT3 (411.8 m3)
CF (26) 96- BY 125-IN. PALLETS = 15,514 FT3 (439.3 m3)
(26) 88- BY 125-IN. PALLETS = 13,521 FT3 (382.9 m3)
(26) 96- BY 125-IN. PALLETS = 14,508 FT3 (410.8 m3)

1R 2R 3R 4R 5R 6R 7R 8R 9R 10R 11R 12R 13R 14R 15R 16R 17R
18C

1L 2L 4L 5L 6L 7L 8L 9L 10L 11L 12L 13L 14L 15L 16L 17L

FREIGHTER (34) 88- BY 108-INCH PALLETS = 15,537 FT3 (440.0 m3)

MAIN CARGO LOADED COMPARTMENT
LENGTH = 144 FT 4 IN. (44.0 m)
FLAT FLOOR AREA = 2,614.5 FT2 (242.9 m2)
BULK VOLUME = 22,048 FT3 * (624.3 m3)

* BULK VOLUME IS WATER VOLUME OF CABIN BETWEEN BARRIER
NET AND AFT BULKHEAD

TYPICAL CARGO SECTION

97.5-IN. (247.7 cm) 88 BY 125 IN. 102-IN.
STACK HEIGHT (223.5 BY 317.5 cm) (259.1 cm)
FREIGHTER
96 BY 125 IN. DOOR
(243.8 BY 317.5 cm)
88 BY 108 IN.
(223.5 BY 274.3 cm)

LD5

64 IN. LD7 LD3
(162.6 cm)
LD9 LD6

LD11

LD21

2.5.5 CROSS SECTION – CARGO DMC005-15
MODEL MD-11F/CF
REV D
2–16

104- BY 66-IN. (264.2 BY 167.6 cm) 70- BY 66-IN. (177.8 BY 167.6 cm)
CARGO DOOR RIGHT SIDE ONLY CARGO DOOR RIGHT SIDE ONLY 14
18 CONTAINERS CONTAINERS

BULK CARGO BULK CARGO DOOR
LEFT SIDE ONLY
30 BY 36 IN.
(76.2 BY 91.4 cm)

32 LD3 CONTAINERS 5,056 FT3 (143.04 m3)
BULK CARGO 510 FT3 (14.44 m3)

TOTAL 5,566 FT3 (157.48 m3)

16 FULL WIDTH CONTAINERS; 60.4 IN. 79.0 IN. 60.4 IN.
EACH 320 FT3 (9.06 m3) (153.4 cm) (200.7 cm) (153.4 cm)
TOTAL 5,120 FT3 (144.96 m3)
44 IN. 64 IN.
160 IN. (111.76 cm) (162.56 cm)
(406.4 cm)

64 IN. 125 IN. 61.5 IN.
(162.56 cm) (317.5 cm) (156.2 cm)

32 HALF WIDTH CONTAINERS;
EACH 158 FT3 (4.47 m3)
TOTAL 5,056 FT3 (143.04 m3)

LD6 CONTAINER LD3 CONTAINER

GROSS WEIGHT TARE WEIGHT GROSS WEIGHT TARE WEIGHT
7,000 LB EACH 600 LB EACH 3,500 LB EACH 320 LB EACH
(3,175 kg) (272.2 kg) (1,588 kg) (145.1 kg)

2.6 LOWER COMPARTMENT DMC005–16
2.6.1 CARGO COMPARTMENTS – CONTAINERS
REV B
MODEL MD-11

2–17

104- BY 66-IN. (264.2 BY 167.6 cm) 70- BY 66-IN. (177.8 BY 167.6 cm)
CARGO DOOR RIGHT SIDE ONLY OPTIONAL 104- BY 66-IN. (264.2 BY 167.6 cm)
6 PALLETS CARGO DOOR RIGHT SIDE ONLY

14 CONTAINERS

BULK CARGO DOOR
LEFT SIDE ONLY
30 BY 36 IN.
(76.2 BY 91.4 cm)

6–96 BY 125 PALLETS 2,667 FT3 (75.48 m3)
OR
2,268 FT3 (64.20 m3)
6–88 BY 125 PALLETS 2,212 FT3 (62.58 m3)
14 LD3 CONTAINERS
BULK CARGO 510 FT3 (14.44 m3)

TOTAL 4,990 FT3 (141.22 m3)

6–96 BY 125-IN. PALLETS 79.0 IN. CONTAINERS
EACH 444 FT3 (12.57 m3 ) (200.7 cm) CENTER COMPARTMENT
TOTAL 2,664 FT3 (75.41 m3)
PALLETS
OR FWD COMPARTMENT

6–88 x 125 PALLETS 60.4 IN.
EACH 378 FT3 (10.70 m3) (153.4 cm)
TOTAL 2,268 FT3 (64.2 m3)
64 IN.
64 IN. (162.56 cm)
(162.56 cm)

61.5 IN.

(156.2 cm)

88 IN. 125 IN. 14 HALF WIDTH CONTAINERS; (LD3)
(223.5 cm) (317.5 cm) EACH 158 FT3 (4.47 m3)

TOTAL 2,212 FT3 (62.58 m3)

88 BY 125-IN. PALLET (223.5 BY 317.5 cm) LD3 CONTAINER

GROSS WEIGHT TARE WEIGHT GROSS WEIGHT TARE WEIGHT DMC005–17
10,300 LB EACH 248 LB EACH 3,500 LB EACH 320 LB EACH
(4,672 kg) (113 kg) (1,588 kg) (145.2 kg)

2.6.2 CARGO COMPARTMENTS – CONTAINERS/PALLETS REV D
MODEL MD-11

2–18